(8645,'35-266','Saab AB','LATCH PROBE','G21025K06','424Z6101-1','','--A',1,'PA 1510 NEW PARTS-2','','39601','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Dig Mark Observed on Outer Diameter','While part handling time part dig mark on OD ','Separate try Introduced for handling between the process and rubber sleeves interduced to avoaid the metal to metal contact.','Rubber sleeves Introduced for this family parts.','Next batch found satisfactory.','','2015-06-29','Krishna(Chowdary.G.P.)','Yogesha K,Yarri Gowda,Vasu SN,Umesh B,Punith G S,Prashanth Kumar M,Paramesh K,Ningaraj A N,Nataraja C V,Manohara B.C.,Manjunatha N,Manjunath  M,KRISHNAMURTHY N,Gurukiran S M,GUNDEGOWDA H.G.,Girish Prasad P,Dhananjaya N,Bharath R,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','MakinoF5-4','Avinash(R.J.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8646,'35-138','Saab AB','FLCD_DS_SUPPORT_DEFLECT_S','R8H8','423Z6189-3','BAC1534-62C','---',1,'PA 1510 FORECAST','','44600','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','After treatment material layer chip out. ','Due to material bheaviour this was opened out.','1) We decided that this cannot be avoaided but we minimized by improving the handling methods.','1) We decided that this cannot be avoaided but we minimized by improving the handling methods.','CA/PA found satisfactory and material layer removal is decresed.','','2015-06-30','Avinash(R.J.)','Manjunath(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','18899','Post DN','no','Misc','Nagaraj(G. Nadiger)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8647,'18-324A','Magellan Aerospace Bournemouth','BRACKET ','559746','L575 53363 200','ABM3 1029','A00',1,'RP408269','','44950','','0000-00-00',NULL,'','','yes','','','','','','no','program wrong so part rejected [proved program tool name wrong ]','The program of this CRN was taken from BMV 45 , and with out editing the message the program has been run. So the Radius has not been formed.','Supervisor will check all the tools and messages in the program, after confirming that then the machining will takes place. And the parts has been segregated to specific machines so that change of program will not take place in future','Supervisor will check all the tools and messages in the program, after confirming that then the machining will takes place. And the parts has been segregated to specific machines so that change of program will not take place in future','CAPA found okay.','','2015-06-30','','        Diwakar R.B.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8648,'35-254','Saab AB','DRAIN CONNECTOR','431589A2','425Z0640-2','','--C',1,'PA 1510 NEW PARTS-1','','44108','','0000-00-00',NULL,'','','yes','','','','','','no','Dig mark observed on radius.','Due to part radius finish program running time dia 3 ball nose broken so dig mark found on radius.','Inform to operator 3 ball program running time check the tool  and roughing stock.Every part radius finish program running before and after check the tool mandatory. Corner radius finishing program some parameter adjusted, next part found okay and continue the production. ','Inform to operator 3 ball program running time check the tool  and roughing stock.Every part radius finish program running before and after check the tool mandatory. Corner radius finishing program some parameter adjusted, next part found okay,program saved.','CAPA found satisfactory','','2015-06-30','','        Girish Prasad P','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8649,'35-073','Saab AB','9900976-384','N38HA1B','L579 50519 200','TA11','A',1,'1600086480','','43292','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Base thickness minus side 0.1mm','Due to Part loading time clamping not properly, so base thickness minus side measured.  ','Instructed to operator every part loading time check the clamps and bolts. Part loading time clean the butting area and apply the air on face  ','Training to operator when part loading time cross check  all clamps, bolts and butting surface.','CAPA found okay','','2015-07-01','Lohith(K)','Lohith(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Lohith(K)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8650,'18-380B','Magellan Aerospace Bournemouth','GAMMA FITTINGS ','M523880 90950','NSA840020-350','','L',1,'RP401481_Amend No.-1','','44054','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','no','Total Length (A) 30.5, Dimension (N) 12.70 -0.1 and thickness (E) 1.60 measures 0.60 under size in one part out of 100 nos sample inspected.','1.We are run the inner diameter, inner grooves and total lenght finish in the operation no1,and we are check the inner diameter for every parts but total lenght and inner grooves checked after every 25 ns. 2.while clamping the part, in the butting face chips will butted so faceout occured in the running part and half of the part total lenght meassures 0.5 to 0.6 undersized but not observed the operator. ','while clamping time clean the jaws by using air, and after clamping the part for every part rotate\r\nthe chuck and cross check the butting fece visually and then run the part and after run the part\r\ncheck the total lenght for every parts hundred percently. ','next every batch we are check the total lenght hundred percent after 25 ns once cross check the inner groove depth and after clamping the part for every part rotate the chuck and cross check the butting fece visually and then run the part and after run the part check the total lenght for every parts hundred percently.and avoiding the this type of errores. ','Next batch found satisfactory.','','2015-07-02','Avinash(R.J.)','Nandishkumar(D.K.)','','2015-07-02','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','CUST END','no','Misc','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8651,'35-138','Saab AB','FLCD_DS_SUPPORT_DEFLECT_S','R8H8','423Z6189-3','BAC1534-62C','---',21,'PA 1510 FORECAST','','44593','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Material layer chip out','Due to material bheaviour this was opened out.','1) We decided that this cannot be avoaided but we minimized by improving the handling methods.','1) We decided that this cannot be avoaided but we minimized by improving the handling methods.','CA/PA found satisfactory and material layer removal is decreased','','2015-07-02','Lohith(K)','Theerthappa K.N.,Shivaraj K S,Lohith K,Hari Prasad,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','HAASVF2SS','Avinash(R.J.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8652,'34-015B','Magellan Aerospace Winnipeg','MOUNTING LUG- STRUT / STD','A1303X','400-12607-1-905','','EM104302 Iss A, EM104765 Iss G, EM105092 Iss F, EM106399 Iss B, EM106400 Iss B, EM106401 Iss A, EM106404 Iss A, EM106522 Iss A, EM106602 Iss A',1,'B91379 Rev.026','','44884','','0000-00-00',NULL,'yes','yes','yes','','','','','','no','Base thickness minus 0.8mm','The part was not butted in the fixture properly which was slightly lifted while finishing the base thickness.','Instructed to operator part loading time part butting properly during clamping.\r\n\r\n ','After loading the part into the fixture, using the feeler gauge and then start the machining.','CA/PA FOUND OK.','','2015-07-02','Lohith(K)','        Theerthappa K.N.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8653,'18-120C','Magellan Aerospace Bournemouth','HOUSING OUT B D BRG 3','CB872484','D275 56121 200','','E01,  ECN NG27011ST1KA83',1,'RP408158','','44748','','0000-00-00',NULL,'yes','yes','yes','','','','','','','4.75 thickness under size -2mm','In work offset instead of giving -2.45mm given -4.75mm so thickness unersize.','For next piece +1.8mm given in work offset and run the part ,part found ok then continue the production.','Instruction given to operator that whenever you withe the values in the work offset,cross check the work offset by facing any one of the tool z-offset.','CA/PA found satisfactory.','','2015-07-03','Dinakar(K)','        Dinakar K','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8654,'18-443A','Magellan Aerospace Wrexham','2.0','94452','L280 50067 206 PF','','A00',3,'RP137240 Amnd 1','','44897','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','ID Groove chatering.','1.2 ID grooving insert edge chipped out so part ID groove chattering,ID groove tool running before boring tool run that time chips not come out side after run the boring tool id groove tool run that time chips cover the    \r\ninsert insert is broken so full chatering in groove.\r\n.  \r\n','After boring tool run M00(program stop) code is addede in program and msg is edited in the program check and remove the chips in the part.next run the m/c m00 program stoped and checked as per msg given in program and run the part part found okay.','After boring tool run M00(program stop) code is addede in program and msg is edited in the program check and remove the chips in the part.next run the m/c m00 program stoped and checked as per msg given in program and run the part part found okay.','CA/PA found satisfactory.','','2015-07-03','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','1','no','Misc','Dinakar(K)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8655,'18-443A','Magellan Aerospace Wrexham','2.0','94452','L280 50067 206 PF','','A00',1,'RP137240 Amnd 1','','44897','','0000-00-00',NULL,'no','yes','yes','yes','no','no','no','no','no','Raw material deviation.','After machining found that RM was undersized\r\n','Instructed to RM cutter to have the process sheet and exact required dimension and then cut the RM\r\n','Instructed to RM cutter to have the process sheet and exact required dimension and then cut the RM\r\n','Next batch found okay\r\n','','2015-07-03','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','1','no','Misc','Narasimhamurthy(K.G.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8656,'42-003','RAFAEL','Clamp-1','746349','BA1E2002B','','38-576104_Rev-E, TILDOCS#172373_Rev-13,111.21_Rev 6,  PR603-2-3_Rev-16, ECN 57176 2014/08/05',4,'347592024','','39397','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','1)2-nos Threaded hole 6-32unc 2B position required dia0.20mm. Measured 0.257mm to 0.271mm.\r\n2)2-nos Threaded hole 8-32unc 2B position required dia0.20mm. Measured 0.220mm to 0.227mm.\r\n','1) We did depth analysis and found that hole position deviated due to material shrinkage after extra material removed.\r\n2) Material shrinked due to geometry of the part.','1) Same NC programe altered and minimized the depth of cut to avoaid the load to the part while machining.\r\n\r\n','1) Same method will be adopted for this geometry of parts.\r\n2) newely designed inspection holding fixture under manufacturing and this will be used for next batch.','CA/PA will be monitered closely when new inspection fixture is in place.','C36295','2015-07-04','Avinash(R.J.)','Sudhagar(V)','Thru maill','2015-03-12','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','With Treatment','0','Customer end','no','Misc','Sudhagar(V)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8657,'18-506A','Magellan Aerospace Wrexham','FITTING SPOILER','4399701','L575 51807 200','','A',1,'RM132922 Amnd 01','','43911','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','As per COS Drawing 2.40+0.10 Measured 3.20 mm.','Part drilled as per drawing not COS\r\n','Check the COS, as per COS drilled on part part found OK\r\n','Before starting FA, check the all customer document same same will updated on part\r\n','CAPA found okay\r\n','','2015-07-04','Ramesh(Poojary)','Ramesh(Poojary)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','Misc','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8658,'18-507A','Magellan Aerospace Wrexham','FITTING SPOILER','4399701','L575 51807 201','','A',1,'RM132922 Amnd 01','','43912','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','As per COS Drawing 2.40+0.10 Measured 3.20 mm.','Part drilled as per drawing not COS\r\n','Check the COS, as per COS drilled on part part found OK\r\n','Before starting FA, check the all customer document same same will updated on part\r\n','CAPA found okay\r\n','','2015-07-04','Ramesh(Poojary)','D.K.Pavan (Kumar)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','00','no','Misc','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8659,'35-266','Saab AB','LATCH PROBE','G21441K06','424Z6101-1','','--A',1,'1600114420','','44539','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dig mark observed on OD.','While part running time air pressure low.Air pressure alarm reset after running time Z axis value changed so part dig. ','Immediately inform the machine supplier,and all parameters checked and production starts with monitoring of tool offset.\r\n\r\n \r\n','Machine supplier is checking the Root cause and problem is air pressure low . Production running with\r\nmonitoring of Air pressure low.','We will review the effectivness after machine manufacturer feed back.','','2015-07-04','Lohith(K)','Yarri(Gowda)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','09','no','Misc','Lohith(K)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8660,'35-043','Saab AB','7605135-201','434961','L574 55135 201','ABM3 1029','A00',1,'1600115266','','44439','','0000-00-00',NULL,'yes','yes','yes','','','','','','','part profile shift 5mm.','wrong X-work offset taken(shank value not add) so profile 5mm shifted.','Check the wrong work offset identifies and stop the m/c. Again taken the work offset correctly then\r\nrun the machine. Inform to operator recheck the work offset again. \r\n','Instruct to operator every work offset taken cross check the work offset two times and run m/c.','CAPA found okay ','','2015-07-04','','        Girish Prasad P','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8661,'18-089B','Magellan Aerospace Wrexham','Plate Sealing','451688','D572 52999 200','ABM3 1029','B',1,'RP135247','','45007','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Runing time tool dig mark.','While taking z-offset for Face grooving tool (in jog mode with hand wheel There is 0.001,0.01,0.1 & 1mm mode for x and z axis movement) it was in 0.1mm whenever we take offset for any tool means in 0.01 mode by mistake it is in 1mm mode and it was not noticed by miss tool went and hit the part so part dig mark.','For next part offset taken for face grooving tool in jog mode with hand wheel control in 0.01mm mode correctly and run the part,part found ok and the continue the production.','Instruction given to operator that whenever you take the offset for any tool means it was in 0.01mm mode (hand wheel mode) and check whether the hand wheel is in 0.01 or 1mm before taking offset.','CA/PA found satisfatcory.','','2015-07-04','Narasimhamurthy(K.G.)','        Rajesh B D','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8662,'35-117','Saab AB','ALCD_STRUCT_INTERCOSTAL_L','425304B','423Z1177-4','7050-T7451 ALUMINUM ','--A',1,'PA-1300 2014-2','','44080','','0000-00-00',NULL,'no','yes','no','yes','no','yes','no','no','no','porosity observed on the part surface.','Due to rubbing of tool or material behavior Corrosion Pits  has been observed  in Treatment house\r\n','Apply PX-24 after machining, and polishing and rubbing of tool should be avoided\r\n','Apply of PX-24 is mandatory before sending the parts to treatment house.\r\n','Next parts and batches found okay\r\n','','2015-07-06','Avinash(R.J.)','Manjunath(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','18941','Post DN','no','Misc','Manjunath(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8663,'28-006A','Magellan Aerospace New York  Inc.','SHOULDER BOLT ','G21041','162A3109 -2','',' 	PL Iss A, PSDL Iss A, ECN C141079',10,'128183_R0_C1','','42819','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','OD Thread NOGO answered.  \r\n','Due to while thread running time thread insert brokened and broken insert is taking over cut and therad major dia will be undersize so thread NOGO answered.  \r\n','Next part thread insert changed and takened tool X-&Z-offset and maintained the thraed offsete effective dia and soot the thread gauge,Gauge is answered and run the part.  \r\n','Inform to operator every 50 nos will be completed changed the insert and takened tool X-offset&Z-offset and maintained the thraed effective dia and soot the thread gauge,Gauge is answered and run the part.  \r\n','Next batch found satisfactory.','','2015-07-06','Dinakar(K)','Theerthappa K.N.,Shivaraj K S,Seetharamu D,Dinakar K,Ashith B,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','0','FI','no','DX 200-2 ','Sudhagar(V)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8664,'35-077','Saab AB','BUSH','1112509740','D575 40147 200','DTD-197','B ECN NG29999ST2TT59',1,'PA 1217-Bushes (A320','','44791','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','OD undersized.\r\n','OD UNDER SIZE BY 0.020 TO 0.025MM IN 1NO. reduce the OD for 2 microns the operator has given correction for 20 microns.  \r\n','Readings will be written in paper and cross checked twice before corrections.  \r\n','Readings will be written in paper and cross checked twice before corrections.  \r\n','CA/PA found satisfactory.','','2015-07-07','Sandhesh D(S)','Seetharamu D,Dinakar K,Ashith B,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','With Treatment','','3','no','DX 200-2 ','Sandhesh D(S)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8665,'18-120C','Magellan Aerospace Bournemouth','HOUSING OUT B D BRG 3','CB872484','D275 56121 200','','E01,  ECN NG27011ST1KA83',1,'RP408158','','44748','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Pin NOGO answer.','Due to part drilling operation running time drill chip out so pin NO GO answered. ','Inform to operator drilling operation running time check the drills and after run the program.When drilling operation done before machining and  after machining check the drill mandatory.','Inform to operator drilling operation running time check the drills and after run the program.When drilling operation done before machining and  after machining check the drill mandatory.','CAPA found okay','','2015-07-07','Lohith(K)','        Yarri Gowda','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8666,'28-045','Magellan Aerospace New York  Inc.','LEVER','158524','65-51632-6','','PL_Rev - A + ADCN # 2 ; DL_Rev - N/C',36,'125339-2520_R0_C0','','39879','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','1)Slot width under size by 0.05 to 0.08MM.','1) After received the customer end part slot width under size.\r\n2) Slot with 0.05 to 0.07 mm taper end side width under size.','1) Next production batch we will inform to supervisor and operator to maintain the maximum limit in slot.\r\n2) we are checking method improve to check the free condition only.  ','1) Next production batch we are inform to supervisor and operator to maintain the maximum limit in slot.\r\n2) we are checking method improve to check the free condition only. ','CA/PA Found ok.','C35599','2015-07-07','Avinash(R.J.)','Sudhagar(V)','113932','2015-03-12','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Manufacture Only','0','Customer end','yes','Misc','Sudhagar(V)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8667,'35-165A','Saab AB','HOUSING PIN','442372','423Z1124-5-01','','--A',1,'May 2015','','43690','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','*Hole dia required 9.525(+.076),Measures 9.64 to 9.65*','Dia 9.55 hole mill using for dia 9.55 hole finish, this time operator not check tool run out, and tool holding in collect holder. ','Change tool holder and using hydraulic holder check tool run out ,taken offset then run production continued. ','Each tool holder loaded in m/c  check tool rut is mandatory. ','CA/PA FOUND OK.','','2015-07-07','Rangaswamy()','Manohara B.C.,Gurukiran S M,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','MakinoF5','Manjunath(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8668,'35-193','Saab AB','INTERCOSTAL CAM HOUSING','593789','423Z1190-1-01','','---',1,'1600102067','','42612','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Profile shift 0.4 To 0.5','Wrong correction given by the operator\r\n','Instructed to CAD dept to edit program and correct it and freeze \r\n','Instructed to CAD dept to edit program and correct it and freeze \r\n','Found okay with next batch\r\n','','2015-07-08','Rangaswamy()','Siddaramappa ,Shivashankar H.G.,Mahesh N,Karthineyan V.S.,Gajendra Singh C.,Basavaraja S. Jr.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','VMC 70L','Manjunath(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8669,'35-237A','Saab AB','JACK BRACKET 2 ','688933A1','D576 50010 206','','D00',1,'1600101900','','42999','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','3D profile point out off tolerance (0.4mm).','Due to put the center bolts not properly so part outer profile dig mark. \r\n','Put the center bolts properly and bolt tightness also checked then run the production. \r\n','Instructed operator to every part put the center bolts properly and bolt tightness also checked then run the production.  \r\n','Next batch found satisfactory\r\n','','2015-07-08','Rangaswamy()','Mahesh(N)','','0000-00-00','3D profile point out off tolerance (0.4mm). ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Rangaswamy()','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8670,'18-386A','Magellan Aerospace(Chalfont) Limited','NUT RING INNER','487664','D575 40039 200','','B',11,'P/074123','','41121','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dimensional Deviation Drawing dimension 2.8mm is measured 1.8 to 2.0 ','while butting the deburr found under the part and part got lifted while drilling','New process has been introduced , the butting surface will be checked with feeler gauge, the dimension is ensured with the scriber.','New process has been introduced , the butting surface will be checked with feeler gauge, the dimension is ensured with the scriber.','CAPA found okay','','2015-07-08','Nagaraju(T)','Bhuvaneshwar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','09','no','Misc','Nagaraju(T)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8671,'18-386A','Magellan Aerospace(Chalfont) Limited','NUT RING INNER','487664','D575 40039 200','','B',50,'P/074123','','43004','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dimensional Deviation Drawing diminstion 2.8mm is measured 1.8 to 2.0 ','while butting the deburr found under the part and part got lifted while drilling','New process has been introduced , the butting surface will be checked with feeler gauge, the dimension is ensured with the scriber.','New process has been introduced , the butting surface will be checked with feeler gauge, the dimension is ensured with the scriber.','CAPA found okay','','2015-07-08','Nagaraju(T)','Bhuvaneshwar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','09','no','Misc','Nagaraju(T)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8672,'18-386A','Magellan Aerospace(Chalfont) Limited','NUT RING INNER','487664','D575 40039 200','','B',10,'P/074123','','43003','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dimensional Deviation Drawing diminstion 2.8mm is measured 1.8 to 2.0','while butting the deburr found under the part and part got lifted while drilling','New process has been introduced , the butting surface will be checked with feeler gauge, the dimension is ensured with the scriber.','New process has been introduced , the butting surface will be checked with feeler gauge, the dimension is ensured with the scriber','CAPA found okay','','2015-07-08','Nagaraju(T)','Bhuvaneshwar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','09','no','Misc','Nagaraju(T)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8673,'18-251B','Magellan Aerospace Bournemouth','BUTTSTRAP INBD FIXED PNL','611729A5','L575 52464 200','ABM3 1029','A00',1,'RP408289','','45069','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Dig mark observed on base.','Due to dia 12 ball nose tool offset taken not properly so base thickness minus side measured. This error happen operator major mistake.  ','Instructed to operator, when tool offset taken after cross check once again.Every time tool offset or work offset taken time tool value or work offset value write down in  the reference book.Tool offset taken time clean the surface and holder. First part running time check the tool offset mandatory. Tool offset taken correctly and further part found okay.\r\n   ','Instructed to operator, when tool offset taken after cross check once again.Every time tool offset or work offset taken time tool value or work offset value write down in  the reference book.Tool offset taken time clean the surface and holder. First part running time check the tool offset mandatory. \r\n   ','CA/PA found ok.','','2015-07-08','Anjinamurthy(H)','        Diwakar R.B.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8674,'35-157A','Saab AB','INTERCOSTAL_VENT','446971C','423Z1172-3-01','','---',1,'April 2014','','44192','','0000-00-00',NULL,'yes','yes','yes','','','','','','','New program problem in cad/cam so part reject...','Cycle time was 2hrs for operation-03, planned to reduce the cycle time for continual improvement.\r\nWhile doing a roughing operation tool dig mark observed on part due to error in program.\r\nWhile selecting the target part in CAM, surface missed in window selection. all the surfaces not considered to generate tool path.\r\nSurface was missed and program generated and dig mark noticed in missed surface.\r\n','After part got rejected, causes for the error find out in CAM and discussed with software provider and as per his    selecting option was used was wrong.\r\nHe trained with new option in CAM (CAD section)which will not omit surfaces while multiple surface selecting.\r\nAll the CAD team checked and found that option was correct.\r\n','All the CAD team will select the CAD select option while selecting the multiple surfaces and this training is done and department head is monitoring the same in future.','CA/PA found satisfactory.','','2015-07-09','D.K.Pavan (Kumar)','        Umesh B','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8675,'18-211B','Magellan Aerospace(Chalfont) Limited','PLUNGER','405978','D321 40205 200','','H01, ECN NR29998ST1JB80',1,'P/078231','','44631','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Dia 8.5 hole over size.','Due to Drilling operation running time drill bent, so hole oblong.Operator not check the drill.','Inform to operator drilling operation running time check the drills and after run the program.When drilling operation done before machining and after machining check the drill mandatory.','Inform to operator drilling operation running time check the drills and after run the program.When drilling operation done before machining and after machining check the drill mandatory.','CA/PA found satisfactory.','','2015-07-09','Lohith(K)','        Yarri Gowda','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8676,'18-158A','Magellan Aerospace Wrexham','Strap Crackstopper','9385708','D572 50203 205','ABM3 1029','L',1,'RP135241','','44356','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Linear indications observed on part surface.','Due to rubbing of tool linear indications has been found in Treatment house. \r\n','Instructed to Production department to avoid rubbing of tool and polishing \r\n','Avoid polishing and try to finish the part  in machining stage itself.\r\n','Next parts and batches found okay\r\n','','2015-07-10','Avinash(R.J.)','Nandishkumar(D.K.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','18732','POST DN','yes','Misc','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL);
INSERT INTO `nc4qa` VALUES (8677,'18-418A','Magellan Aerospace(Blackpool) Limited','BRACKET','221829','PI55-2119010-00','','NIL',1,'P/501836','','43544','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Spot face not done.','','','','','','2015-07-11','Krishna(Chowdary.G.P.)','Siddaramappa ,Krishna Chowdary.G.P.,Gajendra Singh C.,Basavaraja S. Jr.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Manufacture Only','','FI','yes','VMC 70L','Nandishkumar(D.K.)','',NULL,'',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8678,'18-118B','Magellan Aerospace Bournemouth','BEARING HOUSING','247916','D275 40005 200','','C01',1,'RP408156','','44734','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','I.D OVALITY PROBLEMS SO PART REJECT.  \r\n','After running 50 to 60 parts insert tip will be worn out and running time chips not breaking properly so chips will rubbing inside the part and diameter will be oversized in the running part. \r\n','Remove the worn out insert and replace the new insert and newely offset taken and 0.2 (-) minous taken in the tool wear offset and run the part and then check the inner diameter and give the correction in wear offset and adjust the coolant correctly and run the part and checked found ok. \r\n','while setting time loading the new insert before running and after every 100 nos change the roughing insert and run the part.and every 25ns onece observe thetoolnoise,coolant floaing and chips while running.  \r\n','Next batch found satisfactory.','','2015-07-11','Dinakar(K)','Shivappa M B,Rajesh T,Devaraj K.C.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','1','no','DX 200-1','Narasimhamurthy(K.G.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8679,'35-138','Saab AB','FLCD_DS_SUPPORT_DEFLECT_S','R8H8','423Z6189-3','BAC1534-62C','---',2,'PA 1510 FORECAST','','44593','','0000-00-00',NULL,'no','no','no','no','no','yes','yes','yes','no','Material layer chip out.','Due to material bheaviour this was opened out.','1) We decided that this cannot be avoaided but we minimized by improving the handling methods.','1) We decided that this cannot be avoaided but we minimized by improving the handling methods.','CA/PA found satisfactory and material layer removal is decreased .','','2015-07-13','Avinash(R.J.)','Manjunath(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','19131','Post DN','no','Misc','Manjunath(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8680,'18-423A','Magellan Aerospace(Blackpool) Limited','BRACKET','20397 4208','PI201484604','','NIL',1,'P/501935','','43541','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Hole diameter 4.88/4.92 oversize by 0.06mm.','This problem is identified in jig boring setup,\r\nin jig boring operation 09 setup running time chf tool shank rub in dia 4.90 hole, so nogo enter,','After observing check tool, tool was runout problem, and change tool then next part\r\nproved and inspected and then production continued. ','Informed to operator to check the tool overhang  and run out . This is done mandatory to check the tool run out for all the part.','CA/PA found ok.','','2015-07-13','Rangaswamy()','Shivashankar H.G.,Manohara B.C.,Gurukiran S M,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','FI','no','A51nx-1','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8681,'18-414B','Magellan Aerospace Bournemouth','ACTUATOR HOUSING','7131','D278 50163 200','','D',1,'RP408293','','44760','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Part wrong loading.','While 05 operation running time part was wrong loaded.Part was  rotated So part inside bore over side maintained.This error happened operator mistake.','Inform to operator part loading time check the clamping condition after run the programs.Every part loading time clamping bush tightness checking after run the production.','Inform to operator part loading time check the clamping condition after run the programs.Every part loading time clamping bush tightness checking after run the production.','Next part found satisfactory.','','2015-07-14','Lohith(K)','        Dhananjaya N','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8682,'35-083','Saab AB','PIN-SIDE ROLLER','A0729X','F579 53066 200','S145 FHT','C',29,'PA 1226-Roller Housi','','43431','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','OD - SIDE 0.01 to 0.02','WHILE RUNNING TIME IN 500MM LENGTH ROD STARTING 2 TO 3NOS COMPLETION dEEP LINES FORM ON OD, AFTER REPASS AND FINISH THE  OD THE DIAMETER MEASURE -.01/.02    ','WHILE PUTTING NEW ROD FIRST 3NOS  MAINTIAN +.20 AND AFTER CHECK AND REPASS THE OD FINISHING TOOL ','WHILE PUTTING NEW ROD FIRST 3NOS  MAINTIAN +.20 AND AFTER CHECK AND REPASS THE OD FINISHING TOOL ,\r\nTHIS MESSEAGE WE WILL INSERT IN THE PROGRAM BEFORE OD TOOL FINISHING. ','CA/PA found satisfactory.','','2015-07-15','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','01','no','Misc','Dinakar(K)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8683,'18-414B','Magellan Aerospace Bournemouth','ACTUATOR HOUSING','7131','D278 50163 200','','D',2,'RP408293','','44759','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Thickness Undert size 0.1mm.','In 1st set up groove width oversize by 0.3mm (groove width tolerance is +/- 0.3mm)is in the tolerance. but in 2nd set up maintained total length 29.0 mm and 6mm thickness undersize by 0.1mm because groove width not maintained in middle tollerance.  \r\n','For next part check the groove width and thickness before loading the part and any deviation s found in groove width in 2nd set up it is adjusted in work offset.  \r\n','Instruction given to operator to check the dimension s of groove width and if any deviation s found that will adjsted in work offset before load that part.  \r\n','Next part found satisfactory.','','2015-07-16','Dinakar(K)','Sundar D.K.,Subramanya L Naik,Shivashankar H.G.,Shivanand D.B.,SHIVAKUMAR ,Raghavendra Rao R,Manukumar H M,Mahesh N,Karthineyan V.S.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','ST20','Narasimha Murthy(R)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8684,'35-229A','Saab AB','HINGE BRACKET 3','7599601','D576 50006 204','','D00',1,'1600093863 Rev-2','','39278','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','*Dig mark observed on slot.(*23.09 +/-0.03mm measures 24.1mm)','Due to put the center bolts not properly so part dig mark found. \r\n','Put the center bolts properly and bolt tightness also checked then run the production. \r\n','Put the center bolts properly and bolt tightness also checked then run the production. \r\n','Next batch found okay\r\n','','2015-07-16','Girish(Prasad P)','Girish(Prasad P)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','05','no','Misc','Krishna(Chowdary.G.P.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8685,'18-413B','Magellan Aerospace Bournemouth','ACTUATOR HOUSING','19223754','D278 50162 200','','A',1,'RP408292','','45187','','0000-00-00',NULL,'','','yes','','','','','','','6mm thickness -side 0.07','Part running time 5mm thickness blade insert chip out and over load taken so insert will be slipped and taper in the running part and 6mm thickness, 0.07 undersized so part will be rejected','Change the insert corner and  plus and minous taken in the program Z lenght. and run the part and check the taper and give the correction and run the part and part checked found ok. so continue the production. ','After running the 50ns, check the insert corner for next every parts before loading. and then run the part. if insert will chipped out we are change the insert and run the part.','Next batch found satisfactory.','','2015-07-16','','        SHIVAKUMAR ','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8686,'18-230B','Magellan Aerospace Bournemouth','CLAMP STRIP TOP OUTBD','447190','L572 52377 201','ABM3 1029','B00',1,'RP408282','','44659','','0000-00-00',NULL,'','','yes','','','','','','',' 7DIA HOLE +SIDE SO PART REJECTED [BUTT STRAP  PART BEND ]  ','Due to part running time part bend observed. So center of the part width minus side measured. ','Another part running time before bend removing after finish the outer profile and width dimension. Inform the operator every time part 2nd operation completed after remove bend then finish the final operation. \r\n','Inform the operator every time part 2nd operation completed after remove bend then finish the final operation. \r\n','CAPA found okay','','2015-07-17','','        Diwakar R.B.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8687,'28-006A','Magellan Aerospace New York  Inc.','SHOULDER BOLT ','G21041','162A3109 -2','',' 	PL Iss A, PSDL Iss A, ECN C141079',1,'128183_R0_C1','','44817','','0000-00-00',NULL,'','','yes','','','','','','','Part accepted.','','','','','','2015-07-17','','        KRISHNAMURTHY N','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8688,'35-295','Saab AB','VENT DOOR','434837','425Z0101-3','','---',1,'PA 1510 FORECAST-3','','45197','','0000-00-00',NULL,'','','yes','','','','','','','In Part Dig Mark Happen dut To Cutting Tool Length Disturbed...','While doing setting in operation-03, operator not set tool length correctly, Therefore holder\r\ntouches and rib and dig mark observed on rib top.','After observing check tool, was disturbed ,All the tool overhang cross checked and then next part\r\nproved and inspected and then production continued.','Informed to operator to check the tool overhang as per MPS and also cross check with machine\r\nreference book. This is done mandatory to check the tool overhang for all the part.','CA/PA FOUND OK.','','2015-07-18','','        Rangaswamy ','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8689,'18-413B','Magellan Aerospace Bournemouth','ACTUATOR HOUSING','19223754','D278 50162 200','','A',2,'RP408292','','45187','','0000-00-00',NULL,'','','yes','','','','','','no','clap change csk under size','JOB NOT BUTT PROPERLY TO THE CHUCK DURING CLAMPING. \r\n','INSTRUCTED OPERATOR TO BUTT THE JOB PROPERLY DURING CLAMPING\r\n','INSTRUCTED OPERATOR TO BUTT THE JOB PROPERLY DURING CLAMPING\r\n','Next batch found okay\r\n','','2015-07-18','','        Girish Prasad P','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8690,'35-241','Saab AB','HANDLE','431589A2','425Z0634-2','','--C',1,'PA 1510 NEW PARTS-1','','43241','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Part dig mark observed.','Due to put the center bolts not properly so part dig mark found. \r\n','Put the center bolts properly and bolt tightness also checked then run the production. \r\n','Put the center bolts properly and bolt tightness also checked then run the production. \r\n','Next batch found okay\r\n','','2015-07-20','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','05','no','Misc','Lohith(K)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8691,'28-006A','Magellan Aerospace New York  Inc.','SHOULDER BOLT ','G21041','162A3109 -2','',' 	PL Iss A, PSDL Iss A, ECN C141079',4,'128183_R0_C1','','44817','','0000-00-00',NULL,'','','yes','','','','','','','Dia 10.87 OD undersize -0.03mm.','In OD roughing setup running time insert will be breakage and part will OD oversize and that part not checking the operator and part not maintain in proper stock for finishing tool. So in the finishing setup that part loading time finishing tool get the more stock and coolant flows not correctly and chips will be over lapped in the outer diameter and part will be -0.03mm under sized.  \r\n','After roughing check the diameter and maintain the proper stock for the finishing tool and run the part and adjust the coolant in insert edge coolant will be avioded the chips over lapping and every 15 to 20 ns change the finished insert tip and run the part so this problem not repeated again .  ','After roughing check the diameter and maintain the proper stock for the finishing tool and run the part and adjust the coolant in insert edge coolant will be avioded the chips over lapping and every 15 to 20 ns change the finished insert tip and run the part so this problem not repeated again .  \r\n','CAPA found okay, next parts found good','','2015-07-20','','        Rajesh B D','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8692,'35-077','Saab AB','BUSH','1112509740','D575 40147 200','DTD-197','B ECN NG29999ST2TT59',53,'PA 1217-Bushes (A320','','44778','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','White patches abserved on parts after treatment.','Due to rubbing of tool white patches has been found in Treatment house\r\n','Instructed to Production department to avoid rubbing of tool and polishing \r\n','Avoid polishing and try to finish the part  in machining stage itself.\r\n','Next parts and batches found okay\r\n','','2015-07-20','Avinash(R.J.)','Nagaraj(G. Nadiger)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','19022','Post DN','yes','Misc','Nagaraj(G. Nadiger)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8693,'35-249','Saab AB','STANDOFF','G21441K06','423Z1916-3','','---',1,'May 2015','','43896','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Part was tightening time broken in to two parts. ','In this operation part was loaded in the fixture and fixture was clamped in the jaws and the part\r\nwas tightening using ring gauge(it acts like a lock nut).due to over tight part was broken in to\r\ntwo parts so part reject. ','For next part (all tools are running in ccw direction.so over tighting is not required because part\r\nwas RH thread and the ring gauge was RH thread so spanner tighting is not reqired.)part was\r\ntightened with minimum pressure and run the part found ok and continue the production. ','Instruction given to operator that whenever the tools as running in ccw direction over tightening is\r\nnot required because part was automatically locked so do not use any spanner for tightening just tight\r\nthe ring gauge with minimum pressure manually. ','CA/PA Found satisfactory.','','2015-07-20','Dinakar(K)','Shivanand D.B.,SHIVAKUMAR ,Raghavendra Rao R,Lohith K,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','ST20','Manjunath(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8694,'18-326A','Magellan Aerospace Bournemouth','ATTACHMENT ANGLE','432313','L572 53314 200','ABM3 1029','A00',1,'RP400946_Amnd_No.1','','43913','','0000-00-00',NULL,'','','yes','','','','','','no','base thickanes mines','Due to butting face not cleaned properly .So part thickness under size. \r\n','Before load the part of the butting face cleaned by air then load the part.\r\n','Before load the part of the butting face cleaned by air then load the part.\r\n','Found okay with next batch\r\n','','2015-07-22','','        Girish Prasad P','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8695,'30-094','Gardner Aerospace-Derby Limited','FITTING','442586C','L575 52127 201','','A00',1,'LPR0000734','','43472','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dia 6.45hole inside dig mark observed. \r\n','','','','Part accepted','','2015-07-23','Ravikumar(L)','Ravikumar(L)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','Manufacture Only','','07','no','Misc','Rangaswamy()','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8696,'18-379B','Magellan Aerospace Bournemouth','GAMMA FITTINGS ','M506580','NSA840020-300','','L',5,'RP401480_Amend No.-1','','43362','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Total length and 1.6 thickness undersize.','1.We are run the inner diameter, inner grooves and total lenght finish in the operation no1,and we are check the inner diameter for every parts but total lenght and inner grooves checked after every 25 ns. 2.while clamping the part, in the butting face chips will butted so faceout occured in the running part and half of the part total lenght meassures 0.4 to 0.5 undersized but not observed the\r\noperator.  \r\n','while clamping time clean the jaws by using air, and after clamping the part for every part rotate the chuck and cross check the butting fece visually and then run the part and after run the part check the total lenght for every parts hundred percently.  \r\n','next every batch we are check the total lenght hundred percent after 25 ns once cross check the inner groove depth and after clamping the part for every part rotate the chuck and cross check the butting fece visually and then run the part and after run the part check the total lenght for every parts hundred percently.and avoiding the this type of errores.  \r\n','Next batch found satisfactory.','','2015-07-23','Sandhesh D(S)','Nandeesha N,Dinakar K,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','3','no','QT100S-5','Sandhesh D(S)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8697,'18-414B','Magellan Aerospace Bournemouth','ACTUATOR HOUSING','7131','D278 50163 200','','D',1,'RP408293','','44760','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','Hole position out 0.15mm.','Due to 05 and 07  operation running time zero-point fixture used. So first part proving time hole position over.   ','Before next part running first off checking, after adjust the correction next part found OK and  continue the production.','Before next part running first off checking, after adjust the correction next part found OK and  continue the production.','Next part found satisfactory.','','2015-07-24','Lohith(K)','Lohith(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','00','no','Misc','Lohith(K)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8698,'18-278A','Magellan Aerospace(Chalfont) Limited','DOOR OUTER TYPE 25R','1867803','L572 53720 200','ABS5032A055','C00',1,'P/074116','','41795','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Part thickness minus side.','This is rework part, Due to process problem this deviation are coming. After operation-01 part bend and twist observing,\r\ncauses thickness variation by part by part in operation-02.','Planned to run the operation-01 and 02 parallel in two machines to avoid bend and twist. This\r\nprocess are working and part thickness measures ok and also finding consistency part by part.\r\n\r\n','But above corrective action will not permanent,planned and informed to CAD to change the process to\r\nget the consistency of the parts. Still for scheduling propose parts are running with above CA.','CAPA found okay','','2015-07-24','Rangaswamy()','Gurukiran S(M)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','03','no','Misc','Rangaswamy()','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8699,'34-018B','Magellan Aerospace Winnipeg','BRACKET STRUT  LH ','A1303X','400-12609-1-905','','EM105092 Iss F, EM104302 Iss A, EM104765 Iss G, EM106399 Iss B, EM106400 Iss B, EM106401 Iss A, EM106404 Iss A, EM106522 Iss A, EM106602 Iss A',1,'B91379 Rev.026','','45375','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Rib thickness minus side measured 0.5mm. ','While part setting time CRC value wrong enter so part rib thickness minus side measured.This error happened operator mistake.  ','Inform to operator first part setting time before check the process sheet and data sheet after start the setting.In case when CRC program in the part inform to concern supervisor after continue the production. ','Training given to operator CRC program adjusting. Inform to operator first part setting time before check the process sheet and data sheet after start the setting.In case when CRC program in the part inform to concern supervisor after continue the production. ','CA/PA found satisfactory.','','2015-07-25','Lohith(K)','        Lohith K','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8700,'18-211B','Magellan Aerospace(Chalfont) Limited','PLUNGER','405978','D321 40205 200','','H01, ECN NR29998ST1JB80',1,'P/078231','','44632','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Thread NOGO answered.','Wrong program and while giving repass problem occurred\r\n','Instructed to CAD dept to edit program and freeze it \r\n','Instructed to CAD dept to edit program and freeze it \r\n','Found okay with next batch\r\n','','2015-07-26','Dinakar(K)','Yarri Gowda,Vasu SN,Shivaraj K S,Ningaraj A N,Dhananjaya N,Bharath R,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','FI','no','QT100S-2','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8701,'35-178','Saab AB','SUPPORT-SEAL-RETAINER','593780','423Z1833-3-02','','---',1,'PA 1510 FORECAST','','44755','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','As per screen shot Bubble no 8 width of the part mesures 0.5 undersize','Due to put the center bolts not properly so part dig mark found. \r\n','Put the center bolts properly and bolt tightness also checked then run the production. \r\n','Put the center bolts properly and bolt tightness also checked then run the production , Extra heli coil bolts have been introduced for clamping \r\n','Next batch found okay\r\n','','2015-07-27','Rangaswamy()','Umesh B,Manohara B.C.,Gurukiran S M,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','MakinoF5','Nagaraj(G. Nadiger)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8702,'42-005A','RAFAEL','Clamp-3 ','G21267K06','BA1E2004B','','38-576104 Rev E, TILDOCS#172373 Rev 14, PR603-2-3 Rev 16, RAFDOCS#5224238 Rev 4, 111.21 Rev 7, 111.22 Rev 1, ECN63628 2015/01/13, ECN60821 2014/10/26',1,'347592024-5','','44466','','0000-00-00',NULL,'yes','yes','yes','','','','','','','PART WRONG LOADING','Due to part 03 operation loading time part wrong loading so part inside dig mark observed. New process running time this error happened.','Instructed to operator 03 operation part loading time check the 1st set up groove top side  after run the part. ','Next batch production running time process is small change and change the location hole depth.','CAPA found okay, next parts found good','','2015-07-27','Lohith(K)','        Lohith K','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8703,'18-279A','Magellan Aerospace(Chalfont) Limited','DOOR OUTER TYPE 23','6615804','L572 53721 200','ABS5032A055','B00',1,'P/078234','','45444','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Base thickness minus & taper measured 0.5mm.','RM bend so Running time vacuum not clamping properly so thickness plus.','Next batch production running time RM bend checked after load the part.','Next batch production running time RM bend checked after load the part.','CAPA found okay, next parts found good','','2015-07-27','Rangaswamy()','Manohara(B.C.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','03','no','Misc','Rangaswamy()','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8704,'18-091A','Magellan Aerospace Bournemouth','BUSH','K13746','D278 50164 202','S80 FHT','A',4,'RP400843','','43698','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','(OD OVALITY) Outer diameter one point 0.01 undersized.','In OD roughing setup running time insert will be chipped out and part will came in plus side and that part not checking the operator and for next part he found out part will become over sized and he change the insert and maintain the outer dia in required size. but previous part not maintain in proper diameter. So in the finishing setup that part loading time finishing tool get the more stock and chips will be rubbed in the outer diameter and part will be -0.005mm under sized. So part will become rejected.  \r\n','In the finished setup and change the previous insert checking the all parts outer diameter before loading tip and .2 plus taken in the wear offset and run the part and after check the diameter and give the proper correction and run the part and check the part found ok. and after every 50nos change the finished inserttip and run the part so this problem not repeated again.  \r\n','In roughing setup for every part check outer diameter for using air gauge. In finishing set up every 50nos change the finished insert tip and run the part so this problem not repeated again. \r\n','Next batch found satisfactory.','','2015-07-27','Dinakar(K)','Shivappa M B,Devaraj K.C.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','3','no','DX 200-1','Sandhesh D(S)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8705,'35-046','Saab AB','7605148-200','9378701 1','L574 55148 200','ABM3 1029','A00',1,'PA 1217 FORECAST','','45147','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Base thickness 4.5±0.2. measured 3.90mm to 4.00mm. ','While 05 operation running time base thickness under size. due to part clamping M6 bolt head cut.','After change M6 bolt we are check  the  remaining 3 part in this WO  and checked all dimensions found OK. Informed to operator to check the M6 bolt head before clamping part.','Informed to operator to check the M6 bolt head before clamping part. and check the part butting face in filer gauge.  ','CA/PA found OK.','','2015-07-28','','        Manukumar H M','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8706,'35-266','Saab AB','LATCH PROBE','G21506K02','424Z6101-1','','--A',2,'1600102192','','42132','','0000-00-00',NULL,'yes','no','no','no','no','yes','no','yes','no','Magnetic Particle Inspection failed.','During handling scoring marks witnessed on the parts.','Separate try and rubber sleeves introduced to avoaid the metal to metal contact that avoaids the marks on OD.','Separate try and rubber sleeves introduced to avoaid the metal to metal contact that avoaids the marks on OD.','Next batch found satisfactory.','','2015-07-28','Avinash(R.J.)','Manjunath(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','19108','post Dn','no','Misc','Manjunath(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8707,'18-572A','Magellan Aerospace Wrexham','PLATE TRAILING EDGE','D245732','L575 51795 200','','A',1,'RM132920 Amnd 1','','45387','','0000-00-00',NULL,'yes','yes','yes','','','','','','','part width 10.5mm(+/- 0.3) but messure value 10.85 at end point','part width pluse side by part angle fac not butting properly  ( firt batch in the production)','added 2 nos external clamps for clamping,\r\ncross checking the part width befor finishing program. ','added 2 nos external clamps for clamping,\r\ncross checking the part width befor finishing program.\r\nwe will be add part location pins on the fixture at next batch. ','Part was accepted after rework and CA/PA found satisfactory.','','2015-07-28','Narayanappa(G)','        Sathish Y.R.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','','','','','no','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8708,'07-007B','HAL-NASIK','Web 3 Route Portion ','BS-15434','11.2000.2.125.903-RH','','221.02141.00688',1,'NK/M/2513(4520)/MP/O','','45299','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Part rib top taper measured in pulse side.','tool broken & callet release the from the holding at reroughing program under running due to tool not holding proper lenth inside the holder.','changing the 110mm lenth cuuter in callet holder & continue the production.\r\ninsrtucted to all operator using 110mm lenth cutter  for  the reroughing program & using callet holder for over lenth tools.','giving m00  & message in the program.\r\n insrtucted to all operator using 110mm lenth cutter instead of 95mm lenth cutter for  the reroughing program & using callet holder for over lenth tools.','After Rework Part Accepted.','','2015-07-29','Narayanappa(G)','PAVAN KUMAR (S.K.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','Manufacture Only','','03','no','Misc','PAVAN KUMAR (S.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8709,'18-078A','Magellan Aerospace Wrexham','ADAPTOR ','19743493 A','A282 50081 200','','A',1,'RP135273','','44629','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Spot face depth over side maintained. ','While spot face running time chips clogged on spindle. So spot face depth over side measured 0.3mm. \r\n','Under investigation about how to solve this issue or else should give halt the machining regularly and air should blown so under discussion','Under investigation about how to solve this issue or else should give halt the machining regularly and air should blown so under discussion','Discussion held and next parts were okay.','','2015-07-29','Lohith(K)','Lohith(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','00','no','Misc','Lohith(K)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8710,'35-182A','Saab AB','EDGE HOUSING','593780','423Z1121-5-02','','--A',1,'NOV 2014 ','','43522','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','TOOL DIG MARK ON OUTER WALL.','This deviation is observed due to part not clamped in Vice in operation-01.\r\nPart lifts up and dig mark observed dia 10flat roughing program.','After observing the deviation in this part all the parts clamping checked and then manualy mallating done.\r\nAfter ensuring the tightness production running.\r\nVice functioning cross checked and mechanical movement observed. Vice is at good condition and there is no problem with Vice.Operator nned to check phisically while clamping the parts in vice.\r\n\r\n','PA is taken as checking the vice condition and also training given to all the operators in front of machine to check the vice clamping.\r\nSupervisor to monitior the operators and vice functioning regulerly.','CA/PA Found satisfactory.','','2015-07-30','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Girish(Prasad P)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8711,'35-182A','Saab AB','EDGE HOUSING','445293C','423Z1121-5-02','','--A',1,'NOV 2014 ','','43610','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','TOTAL HIGHT UNDER SIZE.','This divation is due to tool length not setted properly while doing a setting for operation-02.\r\nDue to tool overhang problem tool holder rubbed the part and dig mark observed on part.','After observing the deviation in firstoff part, all the tools overhang checked and changed the deviation tool and then continued production.','Informed to operator to check the MPS data sheet and hold the tool overhang as per mentioned length.\r\nAlso informed to cross check the machine refreance book to varify the tool details and tool overhangs.\r\nThe above 2 mentioned poins to be manitor by supervisor for all the parts.','CA/PA Found satisfactory.','','2015-07-30','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','3','no','Misc','Girish(Prasad P)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8712,'18-413B','Magellan Aerospace Bournemouth','ACTUATOR HOUSING','19223754','D278 50162 200','','A',2,'RP408292','','44983','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','dia 6mm hole over size.','Due to blunt in the drill hole got oversize\r\n','Next changed the holder then checked the run out by plunger dial the run out is 0.001 mm then continue the production\r\n','Instructed operator to first time proving the first part will checked the drill  before run the tool.This message entered in the program. \r\n','CAPA found okay','','2015-07-31','Girish(Prasad P)','Girish(Prasad P)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','07','no','Misc','Girish(Prasad P)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8713,'35-143A','Saab AB','BCD_LATCH_PROBE_FTG_HOUSI','653758A3','424Z6115-3-01','','--C',1,'April 2014','','43886','','0000-00-00',NULL,'yes','yes','yes','','','no','','','no','Wrong tool selection.\r\n(16flat runed instead off 6flat)','While loading a tool dia 16flat tool loaded instead of dia 6flat.\r\nOperator checked the datasheet and clearly mentioned the tool diameter, but misinterpretation the diameter and wrong tool loaded. ','When starting the program operator found deviation in material removal, then program stopped and checked the error and found the above problem.\r\nImmediately changed the tool and then continued production.','This error is due to lack of concentration. because in datasheet clearly mentioned the tool diameter and also in program.\r\nTraining conducted to Mr.Subramanya to check the MPS and informed to supervisor to monitor the operators and guide them regulatory to avoid such manual errors.','CA/PA Found satisfactory.','','2015-07-31','Girish(Prasad P)','        Subramanya L Naik','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8714,'35-182A','Saab AB','EDGE HOUSING','445293C','423Z1121-5-02','','--A',1,'NOV 2014 ','','43610','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','KC Profile point +/- .008Inch is measured .016Inch ','While running operation-01 part top surface ct not taken due to part not butted properly in vice.\r\nDue to this error part profile point not achieved.','Training given to operators to check the part butting while loading in vice.\r\nTraining effectiveness checked for all the operators and found ok.\r\nSupervisor is to be monitor the effectiveness in future.','Training given to operators to check the part butting while loading in vice.\r\nTraining effectiveness checked for all the operators and found ok.\r\nSupervisor is to be monitor the effectiveness in future.','CA/PA FOUND OK.','','2015-07-31','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','Misc','Manjunath(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8715,'35-182A','Saab AB','EDGE HOUSING','445293C','423Z1121-5-02','','--A',1,'NOV 2014 ','','43610','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Base Thickness + Side( 0.09 To 0.17) at over all surface','After operation-03 base thickness measures 0.17 plus due to tool offset not correctly taken.\r\n','After inspecting the part tool offset corrected and continued production.\r\nNext part found ok.','Informed to operator to check the tool offset before running the part.\r\nSupervisor to monitor the tool offset.','CA/PA FOUND OK.','','2015-07-31','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','','FI','yes','Misc','Manjunath(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8716,'35-193','Saab AB','INTERCOSTAL CAM HOUSING','581311','423Z1190-1-01','','---',1,'April 2014','','41324','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Dent mark Observed.  ','part was not handled softly, this was identified after coming from treatment house\r\n','Instructed to all persons to handle the part with care\r\n','Instructed to all persons to handle the part with care\r\n','CAPA found okay\r\n','','2015-08-01','Avinash(R.J.)','Manjunath(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','17807','Post DN','yes','Misc','Manjunath(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8717,'35-182A','Saab AB','EDGE HOUSING','601442','423Z1121-5-02','','--A',1,'May 2015','','43519','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','As per screen shot Bubble No31,Thickness 2.54 +/-.25 measures 0.1 To 0.2 undersize.','While running wall finish program in operatio-02, dia 16r3 cutter broken and dig mark observed on wall.\r\nTherefore thickness measures 0.25mm minus side.','Replaced the tool and checked the tool runout and radius with radius guage and then continued production.\r\nAll the tools which is running in this operation is checked phisically.( Flute condition chedked)','Informed to supervisor to check the tool condition regulerly and also mandaterly cross checked the tool while loading to tool magazine.\r\nBy monitoring the tool life and tool condition this problems will not repeat again.','CA/PA Found satisfactory.','','2015-08-01','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','Misc','Manjunath(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8718,'28-004A','Magellan Aerospace New York  Inc.','PIN','G16433R05','161A2332-1','15-5PH Steel Bar per','NA',1,'129350','','44686','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Running time insert broken od under size 0.02mm','In OD roughing setup running time insert will be breakage and part will OD oversize and that part not checking the operator and part not maintain in proper stock for finishing tool. So in the finishing setup that part loading time finishing tool get the more stock and coolant flows not correctly and chips will be over lapped in the outer diameter and part will be -0.02mm under sized. \r\n \r\n','After roughing check the diameter and maintain the proper stock for the finishing tool and run the part and adjust the coolant in insert edge coolant will be avioded the chips over lapping and every 15 to 20 ns change the finished insert tip and run the part so this problem not repeated again .  \r\n','After roughing check the diameter and maintain the proper stock for the finishing tool and run the part and adjust the coolant in insert edge coolant will be avioded the chips over lapping and every 15 to 20 ns change the finished insert tip and run the part so this problem not repeated again .  \r\n','ca/pa found satisfactory.','','2015-08-02','Dinakar(K)','        Seetharamu D','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8719,'18-119B','Magellan Aerospace Bournemouth','HOUSING OUT B DRG 3','A0360X','D275 40011 200','','D01',1,'RP408158','','45393','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Dig mark observed on outer profile.','Due to part outer profile roughing operation running time part was rotated so outer profile dig.','Inform to operator while part loading on fixture, part fully tight after run the programs.Before run the program cross check the clamping tightness.','Inform to operator while part loading on fixture, part fully tight after run the programs.Before run the program cross check the clamping tightness.','CA/PA found satisfactory.','','2015-08-02','Lohith(K)','        Yarri Gowda','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8720,'18-543A','Magellan Aerospace Wrexham','BRACKET LOWER STRUT','595421A9','L575 52898 201','','A',1,'RM132918 Amnd 1','','45419','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','wall theckness under size (0.05 to 0.08mm)','Due to run out in tool wall thickness got undersize','After checking the part, tool was changed and next part machined and found okay','Next changed the holder then checked the run out by plunger dial the run out is 0.001 mm then continue the production\r\n','CAPA found okay','','2015-08-02','Girish(Prasad P)','Girish(Prasad P)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Girish(Prasad P)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8721,'35-187','Saab AB','INTERCOSTAL_MIDSPAN_NO_1 ','450899B','423Z1169-2-03','','---',1,'1600112320','','44365','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Base Thickness undersize (4.06 +/-.25 Measures 2.86 To 3.26)','Due to butting face not cleaned properly .So part thickness under size. \r\n','Before load the part of the butting face cleaned by air then load the part.\r\n','Before load the part of the butting face cleaned by air then load the part.\r\n','Found okay with next batch\r\n','','2015-08-04','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','Misc','Avinash(R.J.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8722,'35-170','Saab AB','ALCD_STRUCT_SUPPORT-FTG_L','686906A9','423Z1200-11-01','','---',1,'PA 1510 FORECAST','','44609','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Dig mark observed on part. ','Part loadind time \"A00\" wrong taken in operation-05.This error happen operator mistake.  ','Inform to operator every part loading time cross check the reference(A00) after run the programs.  ','Inform to operator before running the porogram call for M00, massege to operator cross check the A00.Next batch part found okay.','CA/PA FOUND OK.','','2015-08-05','','        Yarri Gowda','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8723,'35-138','Saab AB','FLCD_DS_SUPPORT_DEFLECT_S','7543150','423Z6189-3','BAC1534-62C','---',7,'PA 1510 FORECAST','','45517','','0000-00-00',NULL,'no','no','no','yes','no','yes','no','yes','no','* Material layer chip pout.','Due to material bheaviour this was opened out.','1) We decided that this cannot be avoaided but we minimized by improving the handling methods.','1) We decided that this cannot be avoaided but we minimized by improving the handling methods.','CA/PA found satisfactory and material layer removal is decreased','','2015-08-05','Krishna(Chowdary.G.P.)','Theerthappa K.N.,Lohith K,Hari Prasad,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','HAASVF2SS','Nagaraj(G. Nadiger)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8724,'18-108A','Magellan Aerospace Bournemouth','FORK END OUT BD','249646','D575 41546 200','S80 FHT','B',1,'RP408151','','45504','','0000-00-00',NULL,'','','yes','','','','','','no','While production running time suddenly tool changed and bore found dig mark','While production running time suddenly tool changed and bore found dig mark','Checked the program thoroughly and no fault in the program found, switched off the machine and after restarting found okay ','Checked the program thoroughly and no fault in the program found, switched off the machine and after restarting found okay ','CAPA found okay','','2015-08-06','','        Ravi R','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8725,'18-499A','Magellan Aerospace Wrexham','FITTING','6482801','L575 54954 201','','A00',1,'RM132920 Amnd 1','','45538','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Part profile tool dig mark.','fixture wrong manufactured same will using on part manufacturing, part was rejected\r\n','Manufacture the new Fixture, validated and run the part\r\n','Manufacturing the correct fixture and validating the fixture, before part running cross check the fixture location holes and dimension\r\n','CAPA found okay\r\n','','2015-08-06','Ramesh(Poojary)','D.K.Pavan (Kumar)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Rangaswamy()','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8726,'28-006A','Magellan Aerospace New York  Inc.','SHOULDER BOLT ','G21041','162A3109 -2','',' 	PL Iss A, PSDL Iss A, ECN C141079',1,'128183_R0_C1','','44817','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Running time thread (-) side 0.05.  \r\n','Thread pitch micrometer was not set to zero properly (0.02MM error)and maintained effective dia 7.22 in pitch micrometer and when thread gauge checked NOGO answered.  ','Pitch micrometer is set to zero using master gauge and for next part maintained thread effective dia 7.24 and gauge found ok and run the production.  \r\n','Instructed to operator to check all the instruments whether it is set to zero or not before start the production.  \r\n','CA/PA found satisfactory.','','2015-08-07','Dinakar(K)','Shivaraj K S,Seetharamu D,Rajesh B D,Manohara M,KRISHNAMURTHY N,GUNDEGOWDA H.G.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','FI','no','DX 200-3','Sudhagar(V)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8727,'28-006A','Magellan Aerospace New York  Inc.','SHOULDER BOLT ','574049','162A3109 -2','',' 	PL Iss A, PSDL Iss A, ECN C141079',1,'130677','','44972','','0000-00-00',NULL,'yes','no','no','no','yes','yes','no','no','no','Dia 10.87 OD undersize -0.03mm.  \r\n','In OD roughing setup running time insert will be breakage and part will OD oversize and that part not checking the operator and part not maintain in proper stock for finishing tool. So in the finishing setup that part loading time finishing tool get the more stock and coolant flows not correctly and chips will be over lapped in the outer diameter and part will be -0.03mm under sized.  \r\n','After roughing check the diameter and maintain the proper stock for the finishing tool and run the part and adjust the coolant in insert edge coolant will be avioded the chips over lapping and every 15 to 20 ns change the finished insert tip and run the part so this problem not repeated again .  \r\n','After roughing check the diameter and maintain the proper stock for the finishing tool and run the part and adjust the coolant in insert edge coolant will be avioded the chips over lapping and every 15 to 20 ns change the finished insert tip and run the part so this problem not repeated again .','CA/PA found satisfactory.\r\n','','2015-08-07','Narasimhamurthy(K.G.)','Shivaraj K S,Rajesh B D,Manohara M,KRISHNAMURTHY N,GUNDEGOWDA H.G.,Dinakar K,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','FI','no','DX 200-3','Sudhagar(V)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8728,'28-006A','Magellan Aerospace New York  Inc.','SHOULDER BOLT ','574049','162A3109 -2','',' 	PL Iss A, PSDL Iss A, ECN C141079',1,'130677','','44972','','0000-00-00',NULL,'yes','no','no','no','yes','yes','no','no','no','Total length undersiz.','Tool offset wrong entry While operator work offset \"Z\" taken time operator not check the tool wear,total length  undersize. \r\n','Re-check the work offset, after continue the production. Instructed to operator every time work offset taken time cross check the wear offset.  \r\n','Instructed to every operator 1st part work offset taken time check the wear dimension in tool wear.  ','CA/PA found satisfactory.','','2015-08-07','Dinakar(K)','Shivaraj K S,Rajesh B D,Manohara M,KRISHNAMURTHY N,GUNDEGOWDA H.G.,Dinakar K,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','FI','no','DX 200-3','Sudhagar(V)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8729,'18-118B','Magellan Aerospace Bournemouth','BEARING HOUSING','K10860','D275 40005 200','','C01',1,'RP408156','','45531','','0000-00-00',NULL,'yes','','yes','','yes','','','','no','runing time part rotet so part dig mark','JOB NOT BUTT PROPERLY TO THE CHUCK DURING CLAMPING. \r\n','INSTRUCTED OPERATOR TO BUTT THE JOB PROPERLY DURING CLAMPING\r\n','INSTRUCTED OPERATOR TO BUTT THE JOB PROPERLY DURING CLAMPING\r\n','Next batch found okay\r\n','','2015-08-07','','        Devaraj K.C.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8730,'46-003','Mahindra Aerostructures Pvt.Ltd','BRACKET HYD','6591801','L579 51142 201 PF','','C00',1,'3100442124','','45523','','0000-00-00',NULL,'no','yes','yes','yes','no','no','no','no','no','Wall Thickness Measures minus side.','After machining found that RM was undersized\r\n','Instructed to RM cutter to have the process sheet and exact required dimension and then cut the RM\r\n','Instructed to RM cutter to have the process sheet and exact required dimension and then cut the RM\r\n','Next batch found okay\r\n','','2015-08-08','NagarAJU(g)','NagarAJU(g)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','03','no','Misc','Krishna(Chowdary.G.P.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8731,'35-138','Saab AB','FLCD_DS_SUPPORT_DEFLECT_S','R8H8','423Z6189-3','BAC1534-62C','---',5,'PA 1510 FORECAST','','44957','','0000-00-00',NULL,'no','yes','no','yes','no','yes','no','no','no','Material Layer chip out.','Due to material bheaviour this was opened out.','1) We decided that this cannot be avoaided but we minimized by improving the handling methods.','1) We decided that this cannot be avoaided but we minimized by improving the handling methods.','CA/PA found satisfactory and material layer removal is decreased','','2015-08-08','Lohith(K)','Theerthappa K.N.,Lohith K,Hari Prasad,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','HAASVF2SS','Nagaraj(G. Nadiger)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8732,'18-119B','Magellan Aerospace Bournemouth','HOUSING OUT B DRG 3','A0360X','D275 40011 200','','D01',1,'RP408158','','44887','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','OD dig mark.','Running time part rotating dig mark in outer diameter.  \r\n','OD finishing time using fixture in part locating & face locking in washer .the washer not locking in properly so part running time rotating .instruction given to operator before cycle start check the part tightening after running part.  \r\n','OD finishing time using fixture in part locating & face locking in washer .the washer not locking in properly so part running time rotating .instruction given to operator before cycle start check the part tightening after running part.  \r\n','CA/PA found satisfactory.','','2015-08-08','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','01','no','Misc','Narasimhamurthy(K.G.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8733,'46-003','Mahindra Aerostructures Pvt.Ltd','BRACKET HYD','6591801','L579 51142 201 PF','','C00',1,'3100442124','','45523','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Dimension 134.3 +0.25 Mesured 134.18/134.27.','Dimension 134.3 program generated to mean value and checking dimension mentioned in reference is +/- 0.25mm.\r\nOperator checked the parts with the tolerance mentioned in reference sheet and all parts are found ok.\r\nBut in FI part got rejected and tolerance in drawing is only +0.25mm.','After noticed the deviation, MPS checked and tolerance corrected and also all the dimensions cross checked with drawing.','Informed to CAD/CAM to validate the Reference sheets or MPS to main drawing and head engineer to approve the same.','CA/PA found ok.','','2015-08-08','Girish(Prasad P)','Sundar D.K.,Subramanya L Naik,Lohith K,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','FI','no','MakinoF5-2','Avinash(R.J.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8734,'18-120C','Magellan Aerospace Bournemouth','HOUSING OUT B D BRG 3','CB872484','D275 56121 200','','E01,  ECN NG27011ST1KA83',1,'RP408158','','45394','','0000-00-00',NULL,'yes','yes','yes','','','','','','','part running time rotate,part - 20mic','Running time part rotating dig mark in outer diameter.  \r\n','od finishing time using fixture in part locating & face locking in washer .the washer not locking in properly so part running time rotating .instruction given to operator before cycle start check the part tightening after running part.  \r\n','od finishing time using fixture in part locating & face locking in washer .the washer not locking in properly so part running time rotating .instruction given to operator before cycle start check the part tightening after running part.  \r\n','CA/PA found satisfactory.','','2015-08-08','','        Ningaraj A N','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8735,'18-118B','Magellan Aerospace Bournemouth','BEARING HOUSING','K10860','D275 40005 200','','C01',1,'RP408156','','45531','','0000-00-00',NULL,'yes','yes','yes','','','','','','','OD dig mark.  \r\n','Running time part rotating dig mark in outer diameter.  ','OD finishing time using fixture in part locating & face locking in washer .the washer not locking in properly so part running time rotating .instruction given to operator before cycle start check the part tightening after running part.  \r\n','OD finishing time using fixture in part locating & face locking in washer .the washer not locking in properly so part running time rotating .instruction given to operator before cycle start check the part tightening after running part.  \r\n','CAPA found okay','','2015-08-08','Dinakar(K)','        Dinakar K','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8736,'18-120C','Magellan Aerospace Bournemouth','HOUSING OUT B D BRG 3','CB872484','D275 56121 200','','E01,  ECN NG27011ST1KA83',1,'RP408158','','45394','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Running time part rotate so od -side.','Running time part rotating that time  outer diameter is undersized.  \r\n','od finishing time using fixture in part locating & face locking in washer .the washer not locking in properly so part running time rotating .instruction given to operator before cycle start check the part tightening after running part.  \r\n','od finishing time using fixture in part locating & face locking in washer .the washer not locking in properly so part running time rotating .instruction given to operator before cycle start check the part tightening after running part.  \r\n','CA/PA found satisfactory.','','2015-08-08','Sandhesh D(S)','Vasu SN,Ningaraj A N,','','0000-00-00','running time part rotate so od -side.','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','9','no','QT100S-2','Vasu(SN)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8737,'35-020','Saab AB','7605128-200','2778702','L574 55128 200','ABM3 1029','A00',1,'PA 1217 FORECAST','','45103','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Part wrong loading Dig mark observed on part. ','Part wrongly loaded in operation-05.Location pin is in diagonal and able to locate at both the orientations. Operator not noticed the loading of part and dig mark observed after running roughing tool because part was wrongly loaded. \r\n','Immediately checked and marked the front face for all the remaining parts. Informed to operators to ensure the front face after loading the part in fixture. Production continued and supervisor is monitoring. \r\n','The following PA action planned and implemented, 1.Location pins diameter changed and amended in MPS. 2.Dia 8 and Dia 10 mm locating pins introduced to avoid wrong locating of part in\r\noperation-03. 3.New program created for dia 10 H7 hole. \r\n','CA/PA FOUND OK','','2015-08-09','Anjinamurthy(H)','Girish(HP)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','05','no','Misc','Anjinamurthy(H)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8738,'18-372B','Magellan Aerospace Bournemouth','GAMMA FITTINGS ','M665370/3577','NSA840007-250 ','','N',1,'RP408523','','45730','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','ID ovality.','After running 50 to 60 parts insert tip will be worn out and running time chips not breaking properly so chips will rubbing inside the part and diameter will be oversized in the running part.\r\n ','Corrective Action:\r\nRemove the worn out insert and replace the new insert and newely offset taken and 0.2 (-) minous taken in the tool wear offset and run the part and then check the inner diameter and give the correction in wear offset and adjust the coolant correctly and run the part and checked found ok.  \r\n','while setting time loading the new insert before running and after every 100 nos change the roughing insert and run the part.and every 25ns onece observe thetoolnoise,coolant floaing and chips while running.  \r\n','CAPA found okay, next parts found good','','2015-08-10','Dinakar(K)','Shivappa M B,Rajesh T,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','3','no','DX 200-1','Narasimhamurthy(K.G.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8739,'35-020','Saab AB','7605128-200','2778702','L574 55128 200','ABM3 1029','A00',1,'PA 1217 FORECAST','','45103','','0000-00-00',NULL,'yes','yes','yes','','','','','','','part wroung loding so part rejct','Second NCR raised, Original NCR no. 08737','Second NCR raised, Original NCR no. 08737','Second NCR raised, Original NCR no. 08737','Ref NC#08737','','2015-08-10','Anjinamurthy(H)','        Girish HP','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8740,'18-090A','Magellan Aerospace Bournemouth','BUSH','K11581','D278 50164 200','S80 FHT','A',1,'RP408159','','45313','','0000-00-00',NULL,'','','yes','','','','','','','OD dig mark.','While part running time ovality occured in the running part so maintened chuck pressure in low. So part running time part was rotated. \r\n',' For Next part maintain the same chuck pressure and run the part and change the roughing insert corner so ovality will be avoided and continue the production.  ','inform to the operator for next batch production dnt change the chuck pressure while ovality occured.  ','CA/PA found satisfactory.','','2015-08-10','','        Manjunath  M','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8741,'35-035','Saab AB','7600298-201','427031','L574 50298 201','ABM3 1029','B00',1,'PA 1217 FORECAST','','45861','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Base thickness measures o.5mm minus side.','While running operation-02, in roughing operation while 16flat tool running part vibrates and dig mark observed on part.\r\nProcess was proved and production running with out any problem in vibration.\r\nAnalyzed the problem but next part running with same parameters and not find any problem.Clamping,tool condition all are checked and found ok.Production continued with under supervision.','Corrective action not taken due to proved process and next batch 09nos production done with out any changes and all the 9 nos are ok.( WO no.47220 and 47219)','Preventive action not taken due to above CA is observed. another one batch will analyzed and if found any problem then will plan for PM.','CAPA found okay, next parts found good','','2015-08-10','Girish(Prasad P)','        Sundar D.K.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8742,'18-621A','Magellan Aerospace Wrexham','FITTING AFT','444706A','L575 52123 200','','A00',1,'RM132920 Amnd 1','','45833','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','Inside will tool dig mark.','When interpolation program running time program error dig mark observed on inside the part , part was rejected\r\n','Corrected the program , same will using part fond Ok\r\n','Program before running on machine cross check with simulaton the transfer to machine\r\n','CAPA found okay\r\n','','2015-08-10','Ramesh(Poojary)','Rangaswamy()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','05','no','Misc','Rangaswamy()','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8743,'35-295','Saab AB','VENT DOOR','643815A4','425Z0101-3','','---',3,'PA 1510 FORECAST-3','','45198','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Tool dig mark in base.','In 2nd setup  wall finish dia 10r3 program running time part lifted & dig mark found in part base. ','This setup existing two m8 bolts for part clamping and we adopt two more m6 bolts for part clamping, then produce 150nos found ok.','same process will be continued in production with updated in process sheet. ','CA/PA Found satisfactory.','','2015-08-11','Rangaswamy()','Shivashankar(H.G.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Rangaswamy()','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8744,'35-295','Saab AB','VENT DOOR','643815A4','425Z0101-3','','---',2,'PA 1510 FORECAST-3','','45198','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Tool dig mark in base.','In 2nd setup  wall finish dia 10r3 program running time part lifted & dig mark found in part base. ','This setup existing two m8 bolts for part clamping and we adopt two more m6 bolts for part clamping, then produce 150nos found ok.','same process will be continued in production with updated in process sheet.','CA/PA Found satisfactory.','','2015-08-11','Rangaswamy()','Karthineyan(V.S.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Rangaswamy()','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8745,'34-015B','Magellan Aerospace Winnipeg','MOUNTING LUG- STRUT / STD','A1303X','400-12607-1-905','','EM104302 Iss A, EM104765 Iss G, EM105092 Iss F, EM106399 Iss B, EM106400 Iss B, EM106401 Iss A, EM106404 Iss A, EM106522 Iss A, EM106602 Iss A',1,'B91379 Rev.026','','44790','','0000-00-00',NULL,'yes','no','no','no','yes','yes','no','no','no','Ovality Upto 0.03mm in Bore','Due to part bore operation running time chips clocking so bore 3mm area over size. ','1.Adjusted the coolant nozzle on to the cutting edge so as to remove the chips while machining. ','Seperate station was provide into the programm to clean the chips before finishing the bore.','CAPA found okay, next parts found good','','2015-08-11','Lohith(K)','Umesh B,Theerthappa K.N.,Manohara B.C.,Lohith K,Hari Prasad,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','FI','no','HAASVF2SS','Sudhagar(V)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8746,'42-005A','RAFAEL','Clamp-3 ','746349','BA1E2004B','','38-576104 Rev E, TILDOCS#172373 Rev 14, PR603-2-3 Rev 16, RAFDOCS#5224238 Rev 4, 111.21 Rev 7, 111.22 Rev 1, ECN63628 2015/01/13, ECN60821 2014/10/26',1,'347592024-5','','43632','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','PART ACCEPTED','','','','','','2015-08-11','Sudhagar(V)','Yogesha K,Yarri Gowda,Theerthappa K.N.,Shivaraj K S,Punith G S,Prashanth Kumar M,Hari Prasad,Girish Prasad P,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','With Treatment','','FI','no','VM2-2','Sudhagar(V)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8747,'42-005A','RAFAEL','Clamp-3 ','746349','BA1E2004B','','38-576104 Rev E, TILDOCS#172373 Rev 14, PR603-2-3 Rev 16, RAFDOCS#5224238 Rev 4, 111.21 Rev 7, 111.22 Rev 1, ECN63628 2015/01/13, ECN60821 2014/10/26',1,'347592024-5','','43632','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1)PART DENT','Due to put the center bolts not properly so part outer profile dig mark. \r\n','Put the center bolts properly and bolt tightness also checked then run the production. \r\n','Instructed operator to every part put the center bolts properly and bolt tightness also checked then run the production.  \r\n','Next batch found satisfactory\r\n','','2015-08-11','Sudhagar(V)','Avinash(R.J.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','18572','POST DN','no','Misc','Sudhagar(V)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8748,'35-191','Saab AB','SUPPORT-FTG','428595B','423Z1202-13','','---',1,'1600114420','','44626','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Dig mark observed on part.  ','Due to first part setting time tool offset taken wrong.So part base dig mark.This error happen senior operator mistake. ','Next part loading time remeasure the tool offset and continue the production and next part found okay.  Inform to operator while tool offset taken time remeasure the tool offset after mention the value in the reference book then continue the production.   ','Inform to operator while tool offset taken time remeasure the tool offset after mention the value in the reference book then continue the production.','CA/PA FOUND OK','','2015-08-11','Lohith(K)','        Shivaraj K S','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8749,'18-118B','Magellan Aerospace Bournemouth','BEARING HOUSING','K10860','D275 40005 200','','C01',1,'RP408156','','46058','','0000-00-00',NULL,'yes','yes','yes','','','','','','','total length -.3mm   od finishing runing time thicknes under size -.3mm','While clamping the part, in the butting face chips will butted so faceout occured in the running part and half of the part total lenght meassures 0.28 to 0.3 undersized but not observed the operator.  \r\n','while clamping time clean the jaws by using air, and after clamping the part for every part rotate the chuck and cross check the butting fece visually and then run the part and after run the part check the total lenght for every parts hundred percently.  \r\n','next every batch we are check the total lenght hundred percent.after clamping the part for every part rotate the chuck and cross check the\r\nbutting face visually and then run the part and after run the part check the total lenght for every parts hundred percently.and avoiding the this type of errores.  \r\n','CA/PA found satisfactory.','','2015-08-11','','        Shivappa M B','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8750,'18-346A','Magellan Aerospace Bournemouth','LANDING TOP PANNEL','A595274','F574 50970 201 01','','C, ECN PG49998ST1TV37',1,'RP400947','','42447','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Linear indications observed on part surface.','Due to rubbing of tool linear indications has been found in Treatment house. \r\n','Instructed to Production department to avoid rubbing of tool and polishing \r\n','Avoid polishing and try to finish the part  in machining stage itself.\r\n','Next parts and batches found okay\r\n','','2015-08-11','Avinash(R.J.)','Nandishkumar(D.K.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','17630','POST DN','no','Misc','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8751,'18-605A','Magellan Aerospace Wrexham','BEAM STRUT FWD','442635A','L575 52212 200','','A00',1,'RP134149 Amnd 1','','45632','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dimension deviation. required 31.0mm from slot face to bore center.\r\nbut measured 31.80mm.','This deviation causes because of offset error.\r\nWhile doing setting for operation 07.Operator entered tool length compensation value in wrong  G-code.( Instead of G54 Work offset,value entered in G57 Work offset)\r\n\r\nDue to this manual error slot depth measures plus side.','This deviation observed while checking the first off part. Immediately supervisor checked the route cause and find error in offset.\r\nThen checked offset and corrected.\r\n ','This is due to manual error by operator, he not cross checked the tool offset.\r\n\r\nOperator also have good operating experience in machine.\r\n\r\nWe taken PA by checking the tool offset once again by supervisor till supervisor get confidence on operator.\r\n\r\nTraining is  given to operator to check the WO G-Code activation in machine control panel.','CA/PA FOUND SATISFACTORY.','','2015-08-12','Narayanappa(G)','Nithin(S)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','05','no','Misc','Nithin(S)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8752,'18-392B','Magellan Aerospace Bournemouth','END COVER','95482','D278 50167 200','','D',1,'RP408296','','44344','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Bore Over size.','ovality in the running part so it not entering the air gauge so polishing the inner diameter so it will become over sized.','If any ovality parts not entering the air gauge first check the part for using bore gauge then remove the ovality then polish the part and we avoid this type of mistakes  ','If any ovality parts not entering the air gauge first check the part for using bore gauge then remove the ovality then polish the part and we avoid this type of mistakes  ','CAPA found okay, next parts found good','','2015-08-12','Dinakar(K)','Shivanand D.B.,SHIVAKUMAR ,Raghavendra Rao R,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','ST20Y1','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8753,'35-138','Saab AB','FLCD_DS_SUPPORT_DEFLECT_S','R8H8','423Z6189-3','BAC1534-62C','---',1,'PA 1510 FORECAST','','44957','','0000-00-00',NULL,'no','no','no','no','no','yes','yes','yes','no','Material layer chip out. ','Due to material bheaviour this was opened out.','1) We decided that this cannot be avoaided but we minimized by improving the handling methods.','1) We decided that this cannot be avoaided but we minimized by improving the handling methods.','CA/PA found satisfactory and material layer removal is decresed.','','2015-08-13','Avinash(R.J.)','Manjunath(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','19822','Post DN','no','Misc','Nagaraj(G. Nadiger)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8754,'18-384A','Magellan Aerospace(Chalfont) Limited','NUT RING OUTER','Y11518','D575 40038 200','','A',1,'P/074123','','39958','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','ID Thread chatring.','Part running time for the threading operation tool screw will be loosed and thread chattering occured in the running part so part will be rejected. ','For the next part change the threading insert corner and screw and re-offset taken and 0.3 minous taken in the wear offset and run the part then check the part and proper correction given in wear offset and part will checked and found ok.','while setting time we are using the new insert corner so that time check the screw head and screw threads and if it is damaged we are using the new screw and run the production.','CA/PA FOUND SATISFACTORY.','','2015-08-13','Dinakar(K)','Vasu SN,Shivanand D.B.,SHIVAKUMAR ,Mohan Kumar C.M.,Bharath R,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','QT100S-2','Narasimha Murthy(R)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8755,'18-384A','Magellan Aerospace(Chalfont) Limited','NUT RING OUTER','Y11518','D575 40038 200','','A',1,'P/074123','','39958','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','dia 1.4mm hole oblong.','The part was drilled by using Jig. After drilling the hole did not answer the Pin. Again the drill was inserted to the part Manually. The Operator has not inserted the drill while doing manually in the correct angle. Hence the hole has got ablonged. ','The operator is trained to butt the part to the angled base plate in the correct angle. Then the operator is made to drill the part manually such that there will be no change in angle. ','The angle base plate is made aware to the operator for manually drilling. ','ca/pa found satisfactory.','','2015-08-13','Nagaraju(T)','Irappa(Badiger)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','11','no','Misc','Nagaraju(T)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8756,'35-231A','Saab AB','HINGE BRACKET 4 ','7600601','D576 50007 208','','E00',3,'1600115959','','44387','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','NDT Failed.','Due to rubbing of tool or material behaviour NDT failure has been found in Treatment house','Instructed to Production & fitting department to avoid rubbing of tool and polishing','Avoid polishing and try to finish the part in machining stage itself','CA/PA found satisfactory.','','2015-08-16','Avinash(R.J.)','Manjunath(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','Post DN','no','Misc','Nagaraj(G. Nadiger)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8757,'18-319A','Magellan Aerospace Bournemouth','HALF CLAMP ','8031','D574 50552 200','DTD 5014','B01',88,'RP408269','','44426','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Machine abuse observed inside holes.','1) This was happened due to blak mark witnessed on the parts due to temporary protection oil\r\nevoparated. ','1) Instructed to apply PX24 more and improved the packing method to sustain the PX24 till they\r\nare taking to process. 2) Informed to treatment supplier to take the parts within specified time. ','1) Instructed to apply PX24 more and improved the packing method to sustain the PX24 till they\r\nare taking to process. 2) Informed to treatment supplier to take the parts within specified time','Next batch found satisfactory. ','','2015-08-17','Avinash(R.J.)','Nandishkumar(D.K.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','19277','POST DN','yes','Misc','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8758,'18-319A','Magellan Aerospace Bournemouth','HALF CLAMP ','8031','D574 50552 200','DTD 5014','B01',88,'RP408269','','44427','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Machine abuse observed inside holes.','1) This was happened due to blak mark witnessed on the parts due to temporary protection oil evoparated.','1) Instructed to apply PX24 more and improved the packing method to sustain the PX24 till they are\r\ntaking to process. 2) Informed to treatment supplier to take the parts within specified time.','1) Instructed to apply PX24 more and improved the packing method to sustain the PX24 till they are\r\ntaking to process. 2) Informed to treatment supplier to take the parts within specified time','Next batch found satisfactory. ','','2015-08-17','Avinash(R.J.)','Nandishkumar(D.K.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','19278','POST DN','yes','Misc','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8759,'18-319A','Magellan Aerospace Bournemouth','HALF CLAMP ','8031','D574 50552 200','DTD 5014','B01',44,'RP408269','','44428','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Machine abuse observed inside holes.','1) This was happened due to blak mark witnessed on the parts due to temporary protection oil evoparated.','1) Instructed to apply PX24 more and improved the packing method to sustain the PX24 till they are\r\ntaking to process. 2) Informed to treatment supplier to take the parts within specified time.','1) Instructed to apply PX24 more and improved the packing method to sustain the PX24 till they are\r\ntaking to process. 2) Informed to treatment supplier to take the parts within specified time','Next batch found satisfactory. ','','2015-08-17','Avinash(R.J.)','Nandishkumar(D.K.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','19279','POST DN','yes','Misc','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8760,'18-516A','Magellan Aerospace Wrexham','FITTING SPOILER','6592801','L575 51917 200','','A',1,'RM132922 Amnd 01','','45871','','0000-00-00',NULL,'','','yes','','','','','','no','boring tool in running time chattering and ovality','RPM was not set properly and also insert was worn out also','Checked with CAD and set proper RPM and also check the worn out in the Inserts','Checked with CAD and set proper RPM and also check the worn out in the Inserts','CAPA found okay','','2015-08-17','','        Girish Prasad P','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8761,'35-238A','Saab AB','JACK BRACKET 2 ','688933A1','D576 50010 207','','D00',3,'1600099854','','40794','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','NDT Failed. ','Due to rubbing of tool or material behaviour NDT failure has been found in Treatment house','Instructed to Production & fitting department to avoid rubbing of tool and polishing','Avoid polishing and try to finish the part in machining stage itself.','CA/PA found satisfactory.','','2015-08-17','Avinash(R.J.)','Manjunath(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','16617','Post DN','no','Misc','Nagaraj(G. Nadiger)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8762,'35-076','Saab AB','9900976-434','427961','F579 54100 200','ABM3 1029','B',1,'PA 1217 FORECAST-2','','46003','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','chamfer  shifted.  ','While operation 03 run slitting saw tool used for cutout. but  this finish not accepted in quality so add another setup for base finish & 1.5mm chf finish.\r\nthis time operator butting not properly so chf shifted. 77 nos produced but one number rejected. ','Every part butting cross check using in feeler gauge. all parts found ok.','Every part butting cross check using in feeler gauge and mandatory.','CAPA found okay, next parts found good','','2015-08-18','Rangaswamy()','Rangaswamy()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','05','no','Misc','Rangaswamy()','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8763,'18-411A','Magellan Aerospace(Chalfont) Limited','PLUNGER','240136','D321 40205 200','','H01',1,'LTA _For Treatments','','40907','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1NOS Part missing.','','','','','','2015-08-19','Dinakar(K)','Theerthappa K.N.,Shivaraj K S,Shivappa M B,Rajesh T,Nataraja C V,Manjunatha N,Manjunath  M,Hari Prasad,Devaraj K.C.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','QT100S-1','Narasimha Murthy(R)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8764,'18-106A','Magellan Aerospace Bournemouth','EYE END INBOARD','620469','D575 41542 200','S98 FHT','D',1,'RP408155','','45509','','0000-00-00',NULL,'','','yes','','','','','','','thread running time power trip','Running time power tripped that time o.d was digmark.  \r\n','We are inform to the maintenence for the proper UPS connection.','We are inform to the maintenence for the proper UPS connection.','CA/PA found satisfactory.','','2015-08-19','','        Dinakar K','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8765,'35-176A','Saab AB','LATCH_ACT_PIVOT-FTG ','446972C','423Z1205-2-02','','--B',1,'PA 1510 FORECAST','','45371','','0000-00-00',NULL,'yes','yes','yes','','no','no','','','no','CRC problem bore (+) side','This part bore finish in CRC program, using 12fl for bore finish.this time operator CRC value wrong\r\nenter ,this operator good experience in cim tools, but crc value wrong enter, so part rejected.','Enter correct CRC value run production,71nos found ok.\r\n','Warning letter issued to operator, explain crc value & explain crc program.','CP/PA FOUND OK.','','2015-08-19','Rangaswamy(H A)','        Mahesh N','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8766,'18-566A','Magellan Aerospace Wrexham','FITTING SPIKE AFT','424802 C','L575 51783 200','','A',1,'RM132919 Amnd 1','1','46014','','2015-08-19',NULL,'yes','no','yes','no','yes','no','no','no','no','part dig mark by part vibration while on running the stage..','lake of clamping','2nos clamp added on the part.. ','2nos clamp added on the part.. ','','','2015-08-20','Krishna(Chowdary.G.P.)','Rangaswamy()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Rangaswamy()','no',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8767,'18-566A','Magellan Aerospace Wrexham','FITTING SPIKE AFT','7243801','L575 51783 200','','A',1,'RM132919 Amnd 1','','46016','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','2mm RIB THICKNESS UNDERSIZE & CORNER STEP UNCLEAR .','When 5 Axis program running time part step found on corner and for removing step program running and part thickness under sized','5 axis program fine tuned program, run the program on part and part found ok  ','before running the 5axis program fine tune the program and program running on part ','Next part found ok.','','2015-08-20','Ramesh(Poojary)','Ramesh(Poojary)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','05','no','Misc','Basavaraja S.(Jr.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8768,'18-566A','Magellan Aerospace Wrexham','FITTING SPIKE AFT','7243801','L575 51783 200','','A',1,'RM132919 Amnd 1','','46016','','0000-00-00',NULL,'','','yes','','','','','','no','18-566a  new process done dia 16 flat outer rough running time part shift  so rib thickness (-)0.2','Due to put the center bolts not properly so part outer profile dig mark. \r\n','Put the center bolts properly and bolt tightness also checked then run the production. \r\n','Instructed operator to every part put the center bolts properly and bolt tightness also checked then run the production.  \r\nNew clamping fixture has been manufactured already and parts found okay\r\n','CAPA found okay and next parts found good','','2015-08-20','','        Basavaraja S. Jr.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8769,'28-016','Magellan Aerospace New York  Inc.','STOP FITTING','571458-5','161A6119-1','15-5PH Per AMS 5659 ','N/C',1,'124982-3170_R0_C0','','44336','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Width taper upto 0.5 & in edge 0.020 to 0.030mm under size.','While part extra material removing time part butting not properly so part total width taper achieved.(Actual dim 19±.25 mm measured 18.72 mm end point). ','Informed to operator every part loading time butting properly and before clean the butting area after load the part and check the feeler gauge    ','Informed to operator every part loading time butting properly and before clean the butting area after load the part and check the feeler gauge.   ','CA/PA found satisfactory.','','2015-08-21','Lohith(K)','Theerthappa K.N.,Shivaraj K S,Lohith K,Hari Prasad,Dhananjaya N,','','2015-08-21','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','FI','no','HAASVF2SS-2','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8770,'35-238A','Saab AB','JACK BRACKET 2 ','688933A1','D576 50010 207','','D00',15,'1600101900','','42093','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','FPI failed  ','Due to rubbing of tool or material behaviour NDT failure has been found in Treatment house','Instructed to Production & fitting department to avoid rubbing of tool and polishing','Avoid polishing and try to finish the part in machining stage itself','CA/PA found satisfactory.','','2015-08-21','Avinash(R.J.)','Manjunath(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','Post DN','no','Misc','Nagaraj(G. Nadiger)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8771,'18-119B','Magellan Aerospace Bournemouth','HOUSING OUT B DRG 3','A0360X','D275 40011 200','','D01',1,'RP408158','','45393','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','5mm thickness under size.','JOB NOT BUTT PROPERLY TO THE CHUCK DURING CLAMPING. \r\n','INSTRUCTED OPERATOR TO BUTT THE JOB PROPERLY DURING CLAMPING\r\n','INSTRUCTED OPERATOR TO BUTT THE JOB PROPERLY DURING CLAMPING\r\n','Next batch found okay\r\n','','2015-08-21','Dinakar(K)','KRISHNAMURTHY(N)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','05','no','Misc','Ravi(M)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8772,'18-119B','Magellan Aerospace Bournemouth','HOUSING OUT B DRG 3','A0360X','D275 40011 200','','D01',1,'RP408158','','45393','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Thread gauge not answered.','Thread effective diameter oversize.Due to operator not checked in the m/c.  \r\n','Next production batch will be rework compelted.  \r\n','Instructed operator to every part checked in m/c then remove the part.  \r\n','CA/PA found satisfactory.','','2015-08-21','Dinakar(K)','Rajesh B D,KRISHNAMURTHY N,GUNDEGOWDA H.G.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Manufacture Only','','5','yes','DX 200-3','Ravi(M)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8773,'18-382A','Magellan Aerospace(Chalfont) Limited','SLEEVE BEARING ','A0671X','D575 40037 200','','A',1,'P/078238','','46233','','0000-00-00',NULL,'yes','yes','yes','','','','','','','OD threading chattering problem.','Due to operator checking eroor in micrometer not zero\r\nreading. ','Next micrometer set zero reading and master pin cross checked and run the part the OD found OK.','Inform to operator first instrument cross checked master gauge then after part checked. ','CAPA found okay','','2015-08-23','Narasimhamurthy(K.G.)','        Ningaraj A N','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8774,'18-382A','Magellan Aerospace(Chalfont) Limited','SLEEVE BEARING ','A0671X','D575 40037 200','','A',1,'P/078238','','46233','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Part wrong clamping so one extra hole done.','The jig is used to drill the part.  After clamping the part to the jig the part is twisted 22.5 Degree angle and then hole is drilled. 2 holes gets drilled at a time.  \r\nThe operator has twisted the part to in wider angler than 22.5 Degree. Hence one Additional hole is drilled. ','The operator is trained to use only one slot option in the jig as against more number of slots in the existing Jigs.   ','The jigs are made such that the operator cannot use more than one slot in a Jig.','CA/PA FOUND SATISFACTORY.','','2015-08-23','Nagaraju(T)','Bhuvaneshwar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','00','no','Misc','Nagaraju(T)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8775,'18-069C','Magellan Aerospace Bournemouth','M/C BRKT FWD WX 1727.0 ','7743','D575 40237 200','','N',2,'RP408279','','46365','','0000-00-00',NULL,'yes','yes','yes','','no','','','','','Slot width over size (0.1mm).','While part slot finishing time step observed.Step removing time slot width over size maintained.Due to insufficient tool and tool length  holding inside the holder,so this deviation occurred.This error senior operator mistake.   ','','Instructed to operator controlled dimension running time only use for schunk holder or sink fit holder. Every time tool loading time cross check the tool run out  after run the program.\r\n','CA/PA found satisfactory','','2015-08-24','Lohith(K)','        Hari Prasad','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8776,'35-234A','Saab AB','HINGE BRACKET 5 ','2012801','D576 50008 209','','D00',2,'1600118541','','45969','','0000-00-00',NULL,'yes','yes','yes','','','','','','no','Hand Tap problem (manual hand taping cores so slot center shift) ','While tapping manual the part got rotated and slot center got shifted','Tapping will be done in machines only.','Tapping will be done in machines only.','CAPA found okay','','2015-08-24','','        Sundar D.K.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8777,'35-138','Saab AB','FLCD_DS_SUPPORT_DEFLECT_S','7543150','423Z6189-3','BAC1534-62C','---',2,'PA 1510 FORECAST','','45517','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','MATERIAL LAYER CHIP OUT.','Due to material bheaviour this was opened out.','1) We decided that this cannot be avoaided but we minimized by improving the handling methods.','1) We decided that this cannot be avoaided but we minimized by improving the handling methods.','CA/PA found satisfactory and material layer removal is decresed.','','2015-08-25','Avinash(R.J.)','Manjunath(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','Post DN','no','Misc','Nagaraj(G. Nadiger)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8778,'18-215C','Magellan Aerospace(Chalfont) Limited','ROD END ASSMY - MALE ','254116','D321 53012 200','','F01, ECN NR29998ST1KH40',4,'P/078231','','43910','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Thread gauge NO GO answering.  \r\n','After threading operation in turning, In operation 07 Key way will complete, After key way thread gauge is not answering due to burr is folding in threads. Before Key way operation all the parts is checking with gauge and found ok. Due to problem facing in gauge entry after the key way, we planned to rework with OD thread Die and this operation is manually done.rejected due to NOGO answering.  \r\n','This operation is done by manually and  01 got deviation due to Die entry problem. Due to manually operation this will stabilize by experience and we need to conduct practical training.','Preventive action is as same as Corrective Action.  \r\n','CAPA found okay','','2015-08-25','Dinakar(K)','Narasimhamurthy(K.G.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','07','no','Misc','Narasimhamurthy(K.G.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8779,'18-372B','Magellan Aerospace Bournemouth','GAMMA FITTINGS ','M665370/3577','NSA840007-250 ','','N',1,'RP408523','','45729','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Part re running (2 time loading,)','Loaded the same part two times so another 3 hole added, part reject.','Checked the parts before loading whether that operation is done or not.','Instructions given to operator to check the parts whether that operation is done or not before loading .','CAPA found okay, next parts found good','','2015-08-26','Lohith(K)','Lohith(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','0','no','Misc','Lohith(K)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8780,'18-060B','Magellan Aerospace Bournemouth','TOP SKIN STIFFNER 3','0710701','L575 53251 200','','A00',2,'RP408137','','43974','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Machine abuse observed on part surface.','1) This was happened due to blak mark witnessed on the parts due to temporary protection\r\noil evoparated. ','1) Instructed to apply PX24 more and improved the packing method to sustain the PX24 till they are\r\ntaking to process. 2) Informed to treatment supplier to take the parts within specified time. ','1) Instructed to apply PX24 more and improved the packing method to sustain the PX24 till they are\r\ntaking to process. 2) Informed to treatment supplier to take the parts within specified time. ','Next batch found satisfactory. ','','2015-08-27','Avinash(R.J.)','Nandishkumar(D.K.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','19031','POST DN','yes','Misc','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8781,'18-060B','Magellan Aerospace Bournemouth','TOP SKIN STIFFNER 3','0710701','L575 53251 200','','A00',2,'RP408137','','43975','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Machine abuse observed on part surface.','1) This was happened due to blak mark witnessed on the parts due to temporary protection\r\noil evoparated. ','1) Instructed to apply PX24 more and improved the packing method to sustain the PX24 till they are\r\ntaking to process. 2) Informed to treatment supplier to take the parts within specified time. ','1) Instructed to apply PX24 more and improved the packing method to sustain the PX24 till they are\r\ntaking to process. 2) Informed to treatment supplier to take the parts within specified time. ','Next batch found satisfactory. ','','2015-08-27','Avinash(R.J.)','Nandishkumar(D.K.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','19030','POST DN','yes','Misc','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8782,'18-060B','Magellan Aerospace Bournemouth','TOP SKIN STIFFNER 3','0710701','L575 53251 200','','A00',4,'RP408137','','44040','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Machine abuse observed on part surface.','1) This was happened due to blak mark witnessed on the parts due to temporary protection\r\noil evoparated. ','1) Instructed to apply PX24 more and improved the packing method to sustain the PX24 till they are\r\ntaking to process. 2) Informed to treatment supplier to take the parts within specified time. ','1) Instructed to apply PX24 more and improved the packing method to sustain the PX24 till they are\r\ntaking to process. 2) Informed to treatment supplier to take the parts within specified time. ','Next batch found satisfactory. ','','2015-08-27','Avinash(R.J.)','Nandishkumar(D.K.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','19029','POST DN','yes','Misc','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8783,'18-605A','Magellan Aerospace Wrexham','BEAM STRUT FWD','9551801','L575 52212 200','','A00',1,'RP134149 Amnd 1','','45636','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','22.225/.245 BORE oversize by 13 microns.','This deviation observed in FI.Batch quantity 14nos manufactured and got 01no. deviation.\r\n22.225/22.245 bore ovelaity observed.Cause for this ovelaity is not found at this point of time.\r\nChecked the program,process and tools which is found OK. ','Out of 14nos 01no. got deviation.and causes for this deviation not found at this movement.\r\nWe will check the process, tools in next batch production.\r\nAs a CA we will incorporate one finish tool for bore finish in next batch production. ','As a PA will incorporate one finish tool for bore finish in next batch production. \r\nSupervisor will monitor this CA/PA in next batch.','CAPA found okay, next parts found good','','2015-08-27','Narayanappa(G)','PAVAN KUMAR  S.K.,Narayanappa G,Manjunath K.N.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','DMG 360L','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8784,'18-394A','Magellan Aerospace Bournemouth','VALVE BODY','238300','A284 40009 200','','A',3,'RP408277','','46142','','2015-08-27',NULL,'yes','yes','yes','no','no','no','no','no','no','Dia 1.5 drill bit brocken','While drilling operation drill bit cutting edge was worn out due to this drill bit was brokened.','Immediatelly drill bit replaced and checked the jig and not found any defect then one part processed\r\nand inspected and required dimension was achived,then contiued the process.','1)Instructed to operator to change the drill bit every 50th part. 2)Guide the operator to use the\r\ncoolant properlly and dont give the change to heat the drill bit. 3)Befor load the drill bit check\r\nthe cuuting angle and cutting edge if it is fit for use or not.','CA/PA FOUND SATISFACTORY.','','2015-08-27','Nagaraju(T)','Rakesh (KC)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','11','no','Misc','Nagaraju(T)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8785,'42-005A','RAFAEL','Clamp-3 ','G21267K06','BA1E2004B','','38-576104 Rev E, TILDOCS#172373 Rev 14, PR603-2-3 Rev 16, RAFDOCS#5224238 Rev 4, 111.21 Rev 7, 111.22 Rev 1, ECN63628 2015/01/13, ECN60821 2014/10/26',1,'347592024-5','','45183','','0000-00-00',NULL,'','','yes','','','','','','no','spindle to holder connecting problem in tool changing time chips formed in tool holder so error in tool length offset 0.4 down, total length -side, ','Informed Machine supplier and also maintenance department and investigation is under going on ','Informed Machine supplier and also maintenance department and investigation is under going on','Informed Machine supplier and also maintenance department and investigation is under going on.\r\nThis was happened only once.','CAPA under investigation','','2015-08-27','','        Dhananjaya N','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8786,'35-042','Saab AB','7605135-200','387289','L574 55135 200','ABM3 1029','A00',2,'1600108786','','44437','','0000-00-00',NULL,'no','yes','yes','yes','no','no','no','no','no','Total thickness measures minus side 96mm +/- 0.1mm measures 95mm.\r\n','This deviation happened while doing operation 01.\r\nThis problem is due to RM not parallel ( Right Angle), RM not clamped properly in Vise.\r\nAfter operation-01 completed part thinness measures minus side.','After checking the deviation in 2 parts immediately checked the RM in stores and find ok.\r\nonly 02 nos batch was problem and same was informed to RM supplier. ','Supplier has taken as PA that he will check before packing and also at CIM parts will check visually before creating the GRN.','CA/PA found ok.','','2015-08-28','Nagaraja (G)','Manohara(B.C.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','01','no','Misc','Rangaswamy()','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8787,'18-429A','Magellan Aerospace Bournemouth','CLEAT','0709701A','L575 52435 200','','A00',1,'RP404750','','46438','','0000-00-00',NULL,'yes','yes','yes','','','','','','','wall thickness under size 2.5+/-0.25 measured 2.0mm. 							\r\n','Due to Fixture part butting problem. This is manually error operator part not butting properly.							\r\n','Ensure the part butting properly by 50 micron feeler gauge after run the program.							\r\n','Ensure the part butting properly by 50 micron feeler gauge after run the part.							\r\n','CA/PA FOUND SATISFACTORY.','','2015-08-28','','        Girish Prasad P','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8788,'18-585A','Magellan Aerospace Wrexham','FITTING FWD SPAR','452923','L575 51871 200','','B00',1,'RM132921 Amnd 1','','46256','','0000-00-00',NULL,'','','yes','','','','','','no','process sheet roung so part thickaness mines','Wrong information created on Process sheet, Operator run the as per Process sheet, part was rejected due to offset mistake\r\n','Work offset information corrected on process sheet\r\n','Cross verify the Master Process sheet with programmer  before loading the CIM SOFT\r\n ','CAPA found okay\r\n','','2015-08-28','Ramesh(Poojary)','        Girish Prasad P','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8789,'18-416A','Magellan Aerospace(Blackpool) Limited','BRACKET','M626830 99515','PI55-2119004-00','','NIL',1,'P/501835','','44287','','0000-00-00',NULL,'yes','no','yes','no','yes','no','no','no','no','Dig mark on face.','','','','Part Acceptd.','','2015-08-29','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','Manufacture Only','','03','no','Misc','Krishna(Chowdary.G.P.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8790,'18-078A','Magellan Aerospace Wrexham','ADAPTOR ','19743493-B','A282 50081 200','','A',1,'RP135273','','46205','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','10.67 length undersize.','first part setting time length coolent probe was loading turret in id boring block id finish running time coolent probe was touch the part face so 10.67 length was undersize.','next part coolent probe was changing and id finishing tool was running part found ok.','next time instruction given to operator before running id boring tools check the coolent probe length before machining.','CAPA found okay, next parts found good','','2015-08-29','Ravi(M)','Raghavendra Rao(R)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','01','no','Misc','Ravi(M)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8791,'18-226B','Magellan Aerospace Bournemouth','BRKT - NUT RETAINER','10162768-A','F572 53828 200','','A',2,'RP408164','','45070','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Slot width 35.1/35.4mm oversize by 0.4mm. ','broacing not prooving in st20 m/c process devoloping time broaching diameter oversize.  \r\n','Next part offset -taken in wear offset and run the part and checking broaching diameter correction given to wear offset & run the part part found ok.  \r\n','Next batch instruction given to operator every batch setting time offset - taken in wear offset and run the part.  \r\n','CAPA found okay','','2015-08-29','Dinakar(K)','Theerthappa K.N.,Shivanand D.B.,SHIVAKUMAR ,S. Shiva Kumar,Raghavendra Rao R,Punith G S,Lohith K,Dinakar K,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','ST20','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8792,'18-617A','Magellan Aerospace Wrexham','TUBE DISTANCE','21973523','L575 55276 200','','A00',1,'RM132920 Amnd 1','','46532','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','OD Undersize by -0.32mm.','OD finishing insert changed & 0.3mm plus taken in the tool offset & run the OD finishing program & checked the dia of the part & 0.23mm plus found. in wear offset instead of giving -0.23mm given -0.32mm so OD undersize.  \r\n','for next part +0.09mm given in tool offset & run the part & checked the dia of part & found ok &continue the production.  \r\n','instructions given to operator to check the dimensions correctly whenever the inserts are changed & the dia is 0.2mm plus means give -0.2mm in tool offset instead of giving -0.3mm, otherwise just take the xoffset for that tool & run the part.  \r\n','CAPA found okay','','2015-08-29','Dinakar(K)','Bharath(R)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','1','no','Misc','Narasimhamurthy(K.G.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8793,'18-045B','Magellan Aerospace Bournemouth','ANGLE ATCH RSPAR UPR','3481901','L575 52440 201','','A00',1,'RP408128 Amnd 01','','46458','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','hole shift 1n 2MM.','this has happened due to wrong interpretation of the operator in the drawing','Operator corrected for the next part and found okay with other parts','Instructed operator to check twice before making drilling operation, and ensure with drawing requirements','CAPA found okay, next parts were good','','2015-08-29','Krishna(Chowdary.G.P.)','Jayarama(M.B.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','9','no','Misc','Anjinamurthy(H)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8794,'28-007A','Magellan Aerospace New York  Inc.','Shaft Support Lever','T31D','251A1747-1','Ti-6AL-4V Per Mil-T-','N/C',1,'127388_R0_C0','','44688','','0000-00-00',NULL,'yes','yes','yes','','','','','','','0.889 thicness (-0.05 mm) so parte reject...','07 operation running time part wallthickness not butting properly so od roughing tool running time thickness undersize.  \r\n','next part jaws changing part wallthickness full surface butting in jaws & part was running part found ok.  \r\n','instruction given to operator next time 07 operation setting time part wallthickness full butting in jaws face after setting part.  \r\n','Part accepted','','2015-08-31','Sandhesh D(S)','        GUNDEGOWDA H.G.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8795,'28-007A','Magellan Aerospace New York  Inc.','Shaft Support Lever','T31D','251A1747-1','Ti-6AL-4V Per Mil-T-','N/C',1,'127388_R0_C0','','44688','','0000-00-00',NULL,'yes','yes','yes','','','','','','','0.889 thicknes (-0.2)','07 operation running time part wallthickness not butting properly so od roughing tool running time thickness undersize.  \r\n','next part jaws changing part wallthickness full surface butting in jaws & part was running part found ok.  \r\n','instruction given to operator next time 07 operation setting time part wallthickness full butting in jaws face after setting part.  \r\n','CAPA found okay','','2015-08-31','Ravi(M)','        Rajesh B D','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8796,'18-295A','Magellan Aerospace Bournemouth','BOLT','237004','D577 56145 200','S80','A',2,'RP408165','','46194','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','TOTAL LENGHT MINOUS 0.3 TO 0.5','','','','Parts Accepted.','','2015-09-01','Dinakar(K)','Manjunath (M)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','Manufacture Only','','01','no','Misc','Sandhesh D(S)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8797,'18-117B','Magellan Aerospace Bournemouth','HOUSING-OUT BD BRG','K10257','D275 40004 200','','C01',2,'RP408156','','46574','','0000-00-00',NULL,'','','yes','','','','','','','program edited wrong. thread pitch change','1st set up setting time programme transfer cable not supported so programme manually edting thread 2 time running 1st time running programme thread pitch corret entry 2nd time running time thread pitch wrong entry so part reject.','next part 2nd time threading programme editing correctly part running part found ok.','next part 2nd time threading programme editing correctly part running part found ok.','CAPA found okay, next parts found good','','2015-09-01','','        Dinakar K','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8798,'18-413B','Magellan Aerospace Bournemouth','ACTUATOR HOUSING','2199','D278 50162 200','','A',2,'RP408292','','46578','','0000-00-00',NULL,'yes','yes','yes','','','','','','','WHILE RUNNING TIME TOOL HOLDER WILL BE LOOSED DOWN SO 6.0MM THICKNESS 0.6TO 0.7 UNDER SIZED.','Turret tool locking tap will wornout..so running time bolt will be loosed so tool taken the extra cut so 6mm thickness 0.6 to 0.7 mm undersized.','check the Z-offset that time we foundout tool  will be shifted and again we run the next part that time again tool will shifted for the next part we remove the tool and clean the blade then tightening time tool will not tighted because turret tap will wornout so change the tool pocket and taken the offset and run the part and part checked found ok     ','we are note down the tool pocket and that pocket only used for only anticlock wised tool because downward two taps are in good condition. after the tapping we are used the both taps or both directioned tools.','CA/PA FOUND SATISFACTORY.','','2015-09-01','Sandhesh D(S)','        Raghavendra Rao R','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8799,'35-293','Saab AB','SUPPORT HANDLE','4496941C','424Z1205-6-01','','--A',1,'PA 1510 FORECAST-3','','45185','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Wall thickness plus side maintained.  ','This part program & process proved. but 36nos manufactured but one number rejected. in this nc analyses.    ','In this nc analyses.','Next batch production before salve problem.','CAPA found okay, next parts found good','','2015-09-02','Rangaswamy()','Rangaswamy()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','00','no','Misc','Lohith(K)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8800,'18-088A','Magellan Aerospace Wrexham','PLATE SEALING','451690','D572 52998 200','ABM3 1029','A',1,'RP135247','','46549','','0000-00-00',NULL,'yes','yes','yes','','','','','','','running time part rotated so part outer diameter undersized','While setting time not adjusting the tailstock pressure properly so rough turning running time part rotated so outer diameter undersised.','Adjusting the tailstock pressure for the next part and run the part and adjust the stock for finishing part and check the part and found ok so run the production.','After the setting, before run the first part cross check the setting, tools, offset and insert then run the part and avoiding the these type of mistakes.   ','CA/PA Found OK.','','2015-09-03','Dinakar(K)','        Dinakar K','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8801,'35-232A','Saab AB','HINGE BRACKET 4 ','3861901','D576 50007 209','','E00',1,'1600118541','','46471','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Wrong tool selection. (6x100dig chf tool runed instead off 4.83 drill)			','While loading a tool dia 6x100dig chf tool runed instead off 4.83 drill. Operator checked the datasheet and clearly mentioned the tool diameter, but misinterpretation the diameter and wrong tool loaded.				','When starting the program operator found deviation in material removal, then program stopped and checked the error and found the above problem. Immediately changed the tool and then continued production.					','This error is due to lack of concentration. because in datasheet clearly mentioned the tool diameter and also in program. Training conducted to Mr.Manukumar H M to check the MPS and informed to supervisor to monitor the operators and guide them regulatory to avoid such manual errors.','CA/PA FOUND SATISFACTORY.','','2015-09-03','Girish(Prasad P)','        Manukumar H M','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8802,'18-421A','Magellan Aerospace(Blackpool) Limited','DIAPHRAGM','2210801 1','PI55-2117012-00','','NIL',1,'P/501907','','45700','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Part thickness under size. \r\n\r\nWHILE RUNNING  MACHINE THE CHIPS(SCRAP)FOUND IN SPINDLE','While Dia 16E/M running time chips clogged on spindle. So Base thickness minus side measured 1MM. ','Under investigation about how to solve this issue or else should give halt the machining regularly and air should blown so under discussion ','Under investigation about how to solve this issue or else should give halt the machining regularly and air should blown so under discussion.','NCR tentatively closed and effectivness will be found once they have taken the CA/PA.','','2015-09-04','Anjinamurthy(H)','        Anjinamurthy H','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8803,'35-272','Saab AB','PIN','970533','425Z0601-3','','--A',25,'PA 1510 NEW PARTS-2','','39589','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','1.The diameter is out of tolerance on one part, some tend to be at maximum as well.\r\n2.The straightness of the part measure > 0,10mm but requirement is 0,0762mm\r\n','Ref NC #08807','Ref NC #08807','Ref NC #08807','Ref NC #08807','C36665','2015-09-04','Avinash(R.J.)','Manjunath(G)','C36663,C36665','2015-09-01','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','CUSTOMER END','no','Misc','Manjunath(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8804,'18-617A','Magellan Aerospace Wrexham','TUBE DISTANCE','21973523','L575 55276 200','','A00',1,'RM132920 Amnd 1','','46647','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Pin nogo answerd.','Drill running time pin tight.then dril rework done time part hole pin nogo ansewrd.','Next batch using the correct size drill.pin enter the hole and run.','Next batch using the correct size drill.pin enter the hole and run.','CAPA found okay','','2015-09-04','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','Misc','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8805,'35-274','Saab AB','PIN','G21482K01','426Z2601-1','','--A',2,'PA 1510 FORECAST-3','','45290','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Strightness not achived 0.075 max,But measures 0.085/0.090','This problem is find out in Customer end, after checking the parts in FG 02nos got the above deviation.','After knowing the problem in straightness, process changed and roughing and finishing operation splited in OD.\r\nSame process proved in 35-272 and 35-275 and same was proven.\r\nSame process will implement in next batch production.\r\n','Process changed and roughing and finishing operation splited in OD.\r\nSame process will implement in next batch production and also MPS to be amended.','CA PA found ok.','','2015-09-04','Krishna(Chowdary.G.P.)','Sundar D.K.,Subramanya L Naik,Nataraja C V,Manukumar H M,Manjunatha N,Manjunath  M,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','QT100S-1','Avinash(R.J.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8806,'35-272','Saab AB','PIN','G19876K01','425Z0601-3','','--A',1,'PA 1510 NEW PARTS-2','','39587','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','The diameter on one location is >0.5991\" (>15,216 mm)\r\nSB: The diameter should be 0.5965 - .5990\" (15,1511 - 15,2146mm)\r\n','3)We requested customer to return the parts for further investigation.\r\n','1) We have 34nos in FG that parts are re inspected and found ok.\r\n2) OD diameter checked to full the length and minimum 8 places. Pictures attached.\r\n','Measuring method changed from feeler gauge to check the straightness by using V-Block with dial stand.','CA/PA found satisfactory.','C36663','2015-09-05','Avinash(R.J.)','Manjunath(G)','OF-000788,Issue 2','2015-09-01','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','DN17086','CUST END','no','Misc','Manjunath(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8807,'35-272','Saab AB','PIN','970533','425Z0601-3','','--A',25,'PA 1510 NEW PARTS-2','','39589','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','At least one part have a straightness measured to be >.0039\" ( >0,10 mm) Used both V-block and feeler gauge.\r\nShould be: Straightness max .0030\" ( 0,0762mm)\r\n','3)We requested customer to return the parts for further investigation.\r\n','1) We have 34nos in FG that parts are re inspected and found ok.\r\n2) OD diameter checked to full the length and minimum 8 places. Pictures attached.\r\n','Measuring method changed from feeler gauge to check the straightness by using V-Block with dial stand.','CA/PA found satisfactory.','C36665','2015-09-05','Avinash(R.J.)','Manjunath(G)','OF-000788,Issue 2','2015-09-01','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','DN17108','CUST END','no','Misc','Manjunath(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8808,'35-272','Saab AB','PIN','G21482K01','425Z0601-3','','--A',1,'1600102192','','42136','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','One part have a straightness measured to be >.0039\"       ( >0,10 mm) Used feeler gauge.\r\nShould be: Straightness max .0030\" ( 0,0762mm)\r\n','3)We requested customer to return the parts for further investigation.\r\n','1) We have 34nos in FG that parts are re inspected and found ok.\r\n2) OD diameter checked to full the length and minimum 8 places. Pictures attached.\r\n','Measuring method changed from feeler gauge to check the straightness by using V-Block with dial stand.','CA/PA found satisfactory.','C36729','2015-09-05','Avinash(R.J.)','Manjunath(G)','FO-000788,Issue 2','2015-09-01','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','DN17455','CUST END','no','Misc','Manjunath(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8809,'35-280','Saab AB','SUPPORT','424872','423Z1203-2-02','','---',1,'PA 1510 FORECAST-3','','45254','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','*Dia 3.3 hole over size by 0.12mm.','*While running production, due to drill blunt ole diameter measures 0.12mm plus side.','*New drill placed and deviation drill sent for re-grinding.Next part checked te diameter and ten continued production.','* Informed to operators and supervisors to check the tool tip before loading the tool while doing setting.\r\nTool life to be monitor and replace te tool after tool life completed.','CAPA found satisfactory','','2015-09-05','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Anjanappa()','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8810,'18-565A','Magellan Aerospace Wrexham','FITTING SPIKE FWD','9547801','L575 51782 201','','A',1,'RM132919 Amnd 1','','46022','','0000-00-00',NULL,'yes','yes','yes','','','','','','no','part bend so runinng time wall thickness dig mark','Due to put the center bolts not tightened properly because of outer profile dig mark.','Put the center bolts tightened properly and bolt tightness also checked then run the next part.','Instructed operator to every part tight the center bolts properly and run the production. New clamping fixture had been designed and continued production.','Next part found ok & correct.','','2015-09-05','','        Manohara M','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8811,'01-328','HAL-Helicopter','LONGITUDINAL BEAM - LH','H918-14/13','201S 533H 6100 201','LN 9073 - 3.1354T351','Nil',2,'ALHOS14-23','','45919','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','negetive wall thickness 4.0mm messure value 2.70\r\n','New negetive wall 5axis program recived from cad cam &  Prooved in the Machine. After the All operations Completed, The Part is Given To QAD for FIrst-off. the first off clearnce given by QAD as Part ok.As per the QAD clearence the Production Started. When  cross check the The Dimensios, the 2.0mm  wall thickness is mesured 2.15mm Found ok. but 4mm wall thickness is mesured 2.70mm due to new 5axis program  after the 2parts completed.  \r\n','correct program recived & run the program checking the 4.0mm wall thickness  & continue the production \r\n','correct program recived & run the program checking the 4.0mm wall thickness  & continue the production \r\n','CAPA found okay','','2015-09-05','Ramesh(Poojary)','Narayanappa(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','03','no','Misc','Narayanappa(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8812,'18-104A','Magellan Aerospace Bournemouth','BODY TURNBUCKLE','249646','D575 40490 200','S80 FHT','E',1,'RP408149','','46202','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Part All hole shifted.','while part x offset taken time shank value not moving so part hole shifted  this error happened to operator mistake.','Next part loading time remeasure the \"X\" offset and continue the production and next part found okay. Inform to operator while \"X\"  offset taken time remeasure the  \"X\"  offset after continue the production. ','Next part loading time remeasure the \"X\" offset and continue the production and next part found okay. Inform to operator while \"X\"  offset taken time remeasure the  \"X\"  offset after continue the production. ','CA/PA found satisfactory.','','2015-09-05','Anjinamurthy(H)','        Anjinamurthy H','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8813,'18-578A','Magellan Aerospace Wrexham','FITTING DRIVE SHAFT','634152','L575 51861 201','','B00',1,'RM132921 Amnd 1','','46694','','0000-00-00',NULL,'yes','yes','yes','','','','','','','running time dia 6 drill & 6.5 holemill broken so dia 6.8 part hole over size...','While running production Dia 6mm drill length varied due to holder problem. After the drill Dia 6.5mm hole mill broken due to pre-hole not done for holemill.\r\nReason for holemill broken is stock is more. ','checked the reason for dia 6mm drill length variation after several parts machining completes.\r\nHydraulic holder not clamped properly while we checked the holder after deviation observed.\r\nDeviation tool holder scraped and all the holders which is running for this part is cross checked and production continued.','Informed to all the operators and supervisors to check the tool holders regularly and monitor the usage and handling the holders.','CA/PA found ok.','','2015-09-05','Girish(Prasad P)','        Yogesha K','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8814,'28-005A','Magellan Aerospace New York  Inc.','SHOULDER BOLT ','G21041','162A3109-1','','PL Iss A, PSDL Iss A',1,'128794_R0_C1','','45941','','0000-00-00',NULL,'yes','yes','yes','','','','','','','28-005A O.D (-) side 0.02','In OD roughing setup running time insert will be breakage and part will OD oversize and that part not checking the operator and part not maintain in proper stock for finishing tool. So in the finishing setup that part loading time finishing tool get the more stock and coolant flows not correctly and chips will be over lapped in the outer diameter and part will be -0.03mm under sized. \r\n ','After roughing check the diameter and maintain the proper stock for the finishing tool and run the part and adjust the coolant in insert edge coolant will be avioded the chips over lapping and every 15 to 20 ns change the finished insert tip and run the part so this problem not repeated again .  \r\n','After roughing check the diameter and maintain the proper stock for the finishing tool and run the part and adjust the coolant in insert edge coolant will be avioded the chips over lapping and every 15 to 20 ns change the finished insert tip and run the part so this problem not repeated again .  \r\n','CAPA found okay','','2015-09-07','Narasimhamurthy(K.G.)','        KRISHNAMURTHY N','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8815,'18-069C','Magellan Aerospace Bournemouth','M/C BRKT FWD WX 1727.0 ','10162768-A','D575 40237 200','','N',7,'RP400948_Amnd-01','','41444','','0000-00-00',NULL,'no','yes','no','yes','no','yes','no','no','no','Ultrasonic inspection not done.','1)During receiving inspection they missed to inspect the RM condition against supplier purchase order.\r\n2)Current ERP system was not identified the RM condition and allowed for next step without crosschecking against supplier purchase order through ERP\r\n','1)Gate introduced for checking RM condition through ERP.\r\n2)Without entering raw material condition and verification by ERP, GRN creation cannot be done and if found any mismatch then it will not allowed for next step that goes to pending and decision has to be taken.\r\n','1)Gate introduced for checking RM condition through ERP.\r\n2)Without entering raw material condition and verification by ERP, GRN creation cannot be done and if found any mismatch then it will not allowed for next step that goes to pending and decision has to be taken.\r\n','CAPA found okay, next parts found good','','2015-09-08','NagarAJU(g)','Lohith K,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','yes','Manufacture Only','0','FI','no','VM2-3','Avinash(R.J.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8816,'18-069C','Magellan Aerospace Bournemouth','M/C BRKT FWD WX 1727.0 ','10162768-A','D575 40237 200','','N',16,'RP400948_Amnd-01','','42386','','0000-00-00',NULL,'no','yes','no','yes','no','yes','no','no','no','Ultrasonic inspection not done.','1)During receiving inspection they missed to inspect the RM condition against supplier purchase order.\r\n2)Current ERP system was not identified the RM condition and allowed for next step without crosschecking against supplier purchase order through ERP\r\n','1)Gate introduced for checking RM condition through ERP.\r\n2)Without entering raw material condition and verification by ERP, GRN creation cannot be done and if found any mismatch then it will not allowed for next step that goes to pending and decision has to be taken.\r\n','1)Gate introduced for checking RM condition through ERP.\r\n2)Without entering raw material condition and verification by ERP, GRN creation cannot be done and if found any mismatch then it will not allowed for next step that goes to pending and decision has to be taken.\r\n','CAPA found okay, next parts found good','','2015-09-08','NagarAJU(g)','Lohith K,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','yes','Manufacture Only','0','FI','no','VM2-3','Avinash(R.J.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8817,'18-069C','Magellan Aerospace Bournemouth','M/C BRKT FWD WX 1727.0 ','10162768-A','D575 40237 200','','N',1,'RP400948_Amnd-01','','42388','','0000-00-00',NULL,'no','yes','no','yes','no','yes','no','no','no','Ultrasonic inspection not done.','1)During receiving inspection they missed to inspect the RM condition against supplier purchase order.\r\n2)Current ERP system was not identified the RM condition and allowed for next step without crosschecking against supplier purchase order through ERP\r\n','1)Gate introduced for checking RM condition through ERP.\r\n2)Without entering raw material condition and verification by ERP, GRN creation cannot be done and if found any mismatch then it will not allowed for next step that goes to pending and decision has to be taken.\r\n','1)Gate introduced for checking RM condition through ERP.\r\n2)Without entering raw material condition and verification by ERP, GRN creation cannot be done and if found any mismatch then it will not allowed for next step that goes to pending and decision has to be taken.\r\n','CAPA found okay, next parts found good','','2015-09-08','NagarAJU(g)','Lohith K,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','yes','Manufacture Only','0','FI','no','VM2-3','Avinash(R.J.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8818,'28-007A','Magellan Aerospace New York  Inc.','Shaft Support Lever','T31D','251A1747-1','Ti-6AL-4V Per Mil-T-','N/C',1,'127388_R0_C0','','44688','','0000-00-00',NULL,'yes','yes','yes','','','','','','','0.889 thicknes (-0.2)','07 operation running time part wallthickness not butting properly so od roughing tool running time thickness undersize.','next part jaws changing part wallthickness full surface butting in jaws & part was running part found ok.','instruction given to operator next time 07 operation setting time part wallthickness full butting in jaws face after setting part.','CAPA found okay, next parts found good','','2015-09-09','Ravi(M)','        Rajesh B D','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8819,'35-192','Saab AB','SUPPORT-FTG','593789','423Z1202-14','','---',1,'PA 1510 FORECAST-2','','46675','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Dig mark observed on part.','While running wall finishing dia 16flat tool broken and dig mark observed on part.\r\n','New tool placed and checked the tool offset and wear value and then continued production.\r\nNext part checked the dimensions and then continued production.','Informed to operators and supervisors to check the tool condition before loading the tool to holders.\r\nOn going training implemented to get awerness to operators to check the tools geometry regulerlly for all the tools.','CAPA found okay, next parts found good','','2015-09-09','Rangaswamy()','        Rangaswamy ','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8820,'18-503A','Magellan Aerospace Wrexham','BRACKET HYD','2204801','L579 51022 200','','A00',1,'RM132921 Amnd 1','','46270','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','program problem. ','Long rib wall finishing time part thickness .15 to .2 mm minus measured in First article prooving time , part was rejected\r\n','Process changed and 0.2 stock created on long wall, then run the program part found ok\r\n','Same process will be adapted on long wall machining time and also supporting clamps  will be created on all process\r\n','CAPA found okay\r\n','','2015-09-09','Ramesh(Poojary)','Sathisha(K.C.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Anjinamurthy(H)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8821,'34-032C','Magellan Aerospace Winnipeg','BASE FITTING, F/D HINGE L','A12904','400-12780-1-905','','EM104302 Iss A, EM105092 Iss F, EM104765 Iss G, EM106399 Iss B, EM106400 Iss B, EM106401 Iss A, EM106404 Iss A, EM106522 Iss A, EM106602 Iss A',0,'B91379 Rev.026','','46392','','0000-00-00',NULL,'yes','yes','yes','','','','','','yes','DUMMY.','','','','DUMMY.','','2015-09-10','Lohith(K)','        Lohith K','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8822,'18-356A','Magellan Aerospace(Chalfont) Limited','PIN HINGE CON DRIVEN ','A0391U','L579 52909 200','','A00',1,'P/078232','','46692','','0000-00-00',NULL,'','','yes','','','','','','','chamfer oversize.','setting time id boring tool type wrong entry so chamfer oversize.','Next part tool type editing correctly and part running part found ok.','instruction given to operator next time part running before check the tool type and running the part.','CAPA found okay, next parts found good','','2015-09-10','','        Manjunath  M','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8823,'18-615A','Magellan Aerospace Wrexham','RECEPTACLE','442637C','L575 54240 200','','A00',1,'RM132921 Amnd 1','','46280','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Bore dia 6.00/6.012mm oversize by 0.01mm.','Dia 6.00(+0.010) bore finish using for 3fl with crc program.\r\nchecking in air gauge, but air gauge shank diameter 5.99mm\r\nbut operator every time 20 micron correction in crc value so 6mm bore maintain time air gauge not enter so operator again correction 20 micron.bore over size.  ','After One part finish correction another part. next part found ok. ','Next batch dia 6 reamer for bore finish.','Next parts found ok.','','2015-09-11','Rangaswamy()','Manohara B.C.,Gurukiran S M,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','MakinoF5','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8824,'18-069C','Magellan Aerospace Bournemouth','M/C BRKT FWD WX 1727.0 ','M511410-90018','D575 40237 200','','N',69,'RP400948_Amnd-01','','41443','','0000-00-00',NULL,'yes','no','no','no','no','yes','no','yes','no','A quantity of 4 off have been rejected back to the supplier in reference to the notification of escape email as attached due to no Ultrasonic testing being performed on the raw material.','1)During receiving inspection they missed to inspect the RM condition against supplier purchase order.\r\n2)Current ERP system was not identified the RM condition and allowed for next step without crosschecking against supplier purchase order through ERP\r\n','1)Gate introduced for checking RM condition through ERP.\r\n2)Without entering raw material condition and verification by ERP, GRN creation cannot be done and if found any mismatch then it will not allowed for next step that goes to pending and decision has to be taken.\r\n','1)Gate introduced for checking RM condition through ERP.\r\n2)Without entering raw material condition and verification by ERP, GRN creation cannot be done and if found any mismatch then it will not allowed for next step that goes to pending and decision has to be taken.\r\n','Next batch found satisfactory.','C37394','2015-09-11','Avinash(R.J.)','Nandishkumar(D.K.)','RDN 01643','2015-09-09','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','Customer End','no','Misc','Avinash(R.J.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8825,'34-016B','Magellan Aerospace Winnipeg','MOUNTING LUG-GEARBOX','A12904','400-12608-1-905','','EM104302 Iss A, EM104765 Iss G, EM105092 Iss F, EM106399 Iss B, EM106400 Iss B, EM106401 Iss A, EM106404 Iss A, EM106522 Iss A, EM106602 Iss A',1,'B91379 Rev.026','','46374','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1)Hole over size by 0.10MM.','Part drilling operation running time drill was broken.When sparking time drill removing hole over size observed.','Instructed to operator while drilling operation running check the drill and apply the coolant properly.\r\nDrill regrinding time check the cutting angal and tool run out.','Instructed to operator while drilling operation running check the drill and apply the coolant properly.\r\nDrill regrinding time check the cutting angal and tool run out.','CAPA found okay, next parts found good','','2015-09-11','Lohith(K)','Theerthappa K.N.,Lohith K,KRISHNAMURTHY N,Hari Prasad,GUNDEGOWDA H.G.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','0','FI','no','HAASVF2SS','Sudhagar(V)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8826,'18-226B','Magellan Aerospace Bournemouth','BRKT - NUT RETAINER','18401513','F572 53828 200','','A',1,'RP408164','','46384','','0000-00-00',NULL,'yes','no','yes','no','yes','no','no','no','no','c-axis problem dig mark observed.','C-axis position not locked in properly ','Inform to the maintenence and haas maintenence team','Inform to the maintenence and haas maintenence team','Maintenance done and next parts found okay ','','2015-09-11','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','09','no','Misc','Ravi(M)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8827,'18-377B','Magellan Aerospace Bournemouth','GAMMA FITTINGS ','M510590','NSA840020-200','','L',1,'RP408526','','45683','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Dia \"K\" undersize by 0.05mm.','Wrong offset taken\r\n','Instructed to operator to take offsets properly live on machines\r\n','Instructed to operator to take offsets properly live on machines\r\n','Next batch found okay\r\n','','2015-09-11','Dinakar(K)','Sathish G,Ravi C,Manjunatha P,Dinakar K,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','FI','no','QT100S-3','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8828,'35-284','Saab AB','REINFORCEMENT','431589B2','423Z1984-2-01','','--A',20,'PA 1510 NEW PARTS-2','','41202','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Step is approx. 0.004” however the radius is less than 50 times the step.','•See the picture below of untreated parts that clearly shows the different surfaces.\r\n•But clearly evident that line is merged during polishing to remove the step over in the picture sent by you.\r\n•Theoretically  first line ( showing by blue ) should be extend to second line ( showing by red ).\r\n•But difference between these two surfaces is hardly 0.020mm.\r\n•If we assume that, removed the line of two surfaces in that case also profile of the surface measures within limit.\r\n•See attached report and screen shot for previously supplied part and found within limit.\r\n','•We will not take a chance to send for bench work for polishing because this is the second time we had problem.\r\n•We will get required surface by machining itself from future batches except parts we have in WIP.\r\n','NC programe regenerated to get the required surface finish machine it self.','Next batch found satisfactory.','C37041','2015-09-11','Avinash(R.J.)','Manjunath(G)','OF-000851','2015-09-11','Pnr:423Z1984-2-01\r\nCim C OF C\r\nC37039\r\nC37040\r\nC37042\r\nC37059\r\nPnr:423Z1983-2-01\r\nCim C OF C\r\nC37038\r\nC37035\r\nC37037\r\nC37036\r\nC38373','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','17341','CUST END','no','Misc','Manjunath(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8829,'35-284','Saab AB','REINFORCEMENT','431589B2','423Z1984-2-01','','--A',20,'PA 1510 NEW PARTS-2','','41202','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Step is approx. 0.004” however the radius is less than 50 times the step.','REF NC#:08828','REF NC#:08828','REF NC#:08828','REF NC#:08828','C37041','2015-09-11','Avinash(R.J.)','Manjunath(G)','OF-000851','2015-09-11','Pnr:423Z1984-2-01\r\nCim C OF C\r\nC37039\r\nC37040\r\nC37042\r\nC37059\r\nPnr:423Z1983-2-01\r\nCim C OF C\r\nC37038\r\nC37035\r\nC37037\r\nC37036\r\nC38373','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','17341','CUST END','no','Misc','Manjunath(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8830,'18-414B','Magellan Aerospace Bournemouth','ACTUATOR HOUSING','2195','D278 50163 200','','D',1,'RP408293','','46660','','0000-00-00',NULL,'no','yes','yes','yes','','','','','','WHILE RUNNING TIME TOOL HOLDER WILL BE LOOSED DOWN SO 6.0MM THICKNESS 0.6TO 0.7 UNDER SIZED.  \r\n','Turret tool locking tap will wornout..so running time bolt will be loosed so tool taken the extra cut so 6mm thickness 0.6 to 0.7 mm undersized.  \r\n','check the Z-offset that time we foundout tool will be shifted and again we run the next part that time again tool will shifted for the next part we remove the tool and clean the blade then tightening time tool will not tighted because turret tap will wornout so change the tool pocket and taken the offset and run the part and part checked found ok.  \r\n','we are note down the tool pocket and that pocket only used for only anticlock wised tool because downward two taps are in good condition. after the tapping we are used the both taps or both directioned tools.  ','CAPA found okay','','2015-09-12','Dinakar(K)','        SHIVAKUMAR ','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8831,'35-262','Saab AB','ROD-END','970674','424Z3413-1','','--A',3,'PA 1510 FORECAST-2','','45292','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','BORE DIA OVER SIZE(0.1 MM.','While proving the first off part, this deviation coming.\r\nOperator not entered the CRC value in tool wear and bore measures plus side.\r\n(3nos parts loaded at one fixture)','To reminding to operators, the CRC values message entered in program with optional stop.\r\nThis type of messages are entred in all the program to avoid errors.\r\nBut due to negelegency operator not checked the CRC value and runned the program.','All the actions are taken to avoid such manuall errors. Again this errors are repeating. Planned to do a training to all the operators reagrding the checking the program.','CAPA found okay, next parts found good','','2015-09-12','Rangaswamy()','Manohara(B.C.)','','0000-00-00','BORE DIA OVER SIZE(0.1 MM).','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','05','no','Misc','Girish(Prasad P)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8832,'18-098B','Magellan Aerospace Bournemouth','VALVE- SEAT','66894/01/00','D282 50060 204','','D',1,'RP408160','','44272','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','After treatment dig mark observed on part.','This was happened during transit.','Informed to packing department and improved the packing method.','Informed to packing department and improved the packing method.','Next batch found satisfactory.','','2015-09-13','Avinash(R.J.)','Nandishkumar(D.K.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','POST DN','no','Misc','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8833,'18-098B','Magellan Aerospace Bournemouth','VALVE- SEAT','66894/01/00','D282 50060 204','','D',1,'RP408160','','44272','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','After treatment dig mark observed on part.','This was happened during transit.','Informed to supplier.','PA is not required.','After that not find any this type of issues.','','2015-09-13','Avinash(R.J.)','Nandishkumar(D.K.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','20033','POST DN','no','Misc','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8834,'18-463A','Magellan Aerospace Wrexham','FRAME GEAR RIB IFS','456897C','L575 51890 200 PF','','A00',1,'RP133570 Amnd 1','','46420','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','base thickness under size at one point of the part actual value 2.0 +0.2/-0.1 measured value 1.94 at on point..','Due to part butting problem part was not butted properly so at one point of the part base was under size..','while loading the part external clamp has been added and before running the part butting will be cross checked by the feller gauge and then only part will be machined..','after removing the bed. part will be cross checked in the surface table and the proper debarring will be done and then the part will be loaded after loading the part in machine by using feller gauge part butting will be  cross checked..','Parts accepted.','','2015-09-14','Narayanappa(G)','Siddaramappa ,Paramesh K,Manjunatha N.R.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','Manufacture Only','','9','no','VR11','Narayanappa(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8835,'18-465A','Magellan Aerospace Wrexham','FRAME MID RIB L','626250','L575 51892 200 PF','','A',1,'RP133570 Amnd 1','','46737','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','base thickness under size at one point of the part actual value 2.0 +0.2/-0.1 measured value 1.85 at on point\r\n','Due to part butting problem part was not butted properly so at one point of the part base was under size..\r\n','bolt length will be used as per the required length & while loading the part external clamp has been added and before running the part butting will be cross checked by the feller gauge and then only part will be machined..','after removing the bed. part will be cross checked in the surface table and the proper debarring will be done and then the part will be loaded after loading the part in machine by using feller gauge part butting will be  cross checked..','CAPA found okay, next parts found good','','2015-09-14','Narayanappa(G)','Siddaramappa ,Paramesh K,Manjunatha N.R.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','yes','no','Manufacture Only','','9','no','VR11','Narayanappa(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8836,'18-118B','Magellan Aerospace Bournemouth','BEARING HOUSING','K10860','D275 40005 200','','C01',1,'RP408156','','46058','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','OD undersize.','Due to ovality in part this deviation occur.\r\n','Instructed operator to check the ovality for every part,if\r\n','ovality observed set the part zero run out and than run the part\r\n','Found okay with next batch\r\n','','2015-09-14','Dinakar(K)','Shivappa M B,Rajesh T,Devaraj K.C.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','9','no','DX 200-1','Narasimhamurthy(K.G.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8837,'35-191','Saab AB','SUPPORT-FTG','428595B','423Z1202-13','','---',1,'PA 1510 FORECAST-2','','46674','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Wall charting & wall thickness minus side.','The pocket finishing program is in dia 18r5.60mm deep pocket running in single pass.\r\nProven tool helix angle is 38deg,but next tool supplied with 45deg and is running from past 4 batches and every batch parts are getting rejected.\r\nNew tool dia 16r5 ordred and informed to CAD to change the finishing program to 2 pass in depth to get consistancy. ','New tool dia 16r5 ordered and new program will do with multiple pass to avoid vibration in wall and get consistency.\r\n','New tool dia 16r5 ordered and new program will do with multiple pass to avoid vibration in wall and get consistency.\r\n','Next batch review & closed.','','2015-09-14','Rangaswamy()','Rangaswamy()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','07','no','Misc','Rangaswamy()','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8838,'35-191','Saab AB','SUPPORT-FTG','428595B','423Z1202-13','','---',1,'PA 1510 FORECAST-2','','46674','','0000-00-00',NULL,'yes','','yes','','','','','','no','DUMMY NC','DUMMY NC','DUMMY NC','DUMMY NC','DUMMY NC','','2015-09-14','Rangaswamy()','                Rangaswamy ','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8839,'35-230A','Saab AB','HINGE BRACKET 3 ','7600601','D576 50006 205','','D00',3,'1600108781','','44415','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','PFD Failure.','Due to rubbing of tool or material behaviour NDT failure has been found in Treatment house','Instructed to Production & fitting department to avoid rubbing of tool and polishing','Avoid polishing and try to finish the part in machining stage itself.','CA/PA found satisfactory.','','2015-09-14','Avinash(R.J.)','Manjunath(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','19002','DN','no','Misc','Manjunath(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8840,'35-230A','Saab AB','HINGE BRACKET 3 ','7600601','D576 50006 205','','D00',4,'1600115959','','44416','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','PFD Failure. ','Due to rubbing of tool or material behaviour NDT failure has been found in Treatment house','Instructed to Production & fitting department to avoid rubbing of tool and polishing','Avoid polishing and try to finish the part in machining stage itself.','CA/PA found satisfactory.','','2015-09-14','Avinash(R.J.)','Manjunath(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','19001','DN','no','Misc','Manjunath(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8841,'18-422A','Magellan Aerospace(Blackpool) Limited','BRACKET','21159 / 0964','PI201484603','','NIL',1,'P/501934','','46613','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Thickness under size 0.09mm.','this has happened due to wrong interpretation of the operator in the drawing','Operator corrected for the next part and found okay with other parts','Instructed operator to check twice before making drilling operation, and ensure with drawing requirements','CAPA found okay, next parts were good','','2015-09-15','Rangaswamy()','Umesh B,Rangaswamy ,Lohith K,Gurukiran S M,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','FI','no','MakinoF3','Narasimha Murthy(R)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8842,'18-419A','Magellan Aerospace(Blackpool) Limited','BRACKET','221829','PI55-2120010-00','','NIL',3,'P/501903','','43549','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','DIG MARK ON RADIUS','','','','Part accepted','','2015-09-15','Krishna(Chowdary.G.P.)','Rangaswamy ,Manohara M,Basavaraja S. Jr.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','Manufacture Only','','3','no','VMC 70L','Krishna(Chowdary.G.P.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8843,'18-419A','Magellan Aerospace(Blackpool) Limited','BRACKET','221829','PI55-2120010-00','','NIL',2,'P/501903','','43548','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','DIG MARK ON RADIUS','This deviation is due to program error. Program backup was deleted in machine and proved programs which is saved in server taken and runned the program.\r\nThis program have problem while proving the FAI and after FAI proving customer find the deviation and informed to modify the model and re-FAI done and then part was accepted. the accepted part program was not saved in server and due to this error this deviation coming.','After finding the deviation new programs(proved in CAD)taken and part manufactured and checked,Part found ok.\r\nNext production continued.\r\nProved program saved in server and informed to supervisor to monitor and give updated backup to CAD.','FAI proved programs to be saved as per processor and any modification done CAD and production supervisor to coordinate and save the programs in server. ','CA/PA found ok.','','2015-09-15','Krishna(Chowdary.G.P.)','Basavaraja S. Jr.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','3','no','VMC 70L','Krishna(Chowdary.G.P.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8844,'18-210B','Magellan Aerospace(Chalfont) Limited','BODY','5757','D321 40204 204','','D, ECN NR29999ST1KM15, NR29999ST2KF65, WQN DFB09775',1,'P/074113','','42335','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','yes','no','Machine abuse observed inside holes.','1) This was happened due to blak mark witnessed on the parts due to temporary protection oil evoparated.','1) Instructed to apply PX24 more and improved the packing method to sustain the PX24 till they are taking to process.\r\n2) Informed to treatment supplier to take the parts within specified time.','1) Instructed to apply PX24 more and improved the packing method to sustain the PX24 till they are taking to process.\r\n2) Informed to treatment supplier to take the parts within specified time.','Next batch found satisfactory.','','2015-09-16','Avinash(R.J.)','Nandishkumar(D.K.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','17795','POST DN','yes','Misc','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8845,'18-210B','Magellan Aerospace(Chalfont) Limited','BODY','5757','D321 40204 204','','D, ECN NR29999ST1KM15, NR29999ST2KF65, WQN DFB09775',2,'P/074113','','42334','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Machine abuse observed inside holes.','1) This was happened due to blak mark witnessed on the parts due to temporary protection oil evoparated.','1) Instructed to apply PX24 more and improved the packing method to sustain the PX24 till they are taking to process.\r\n2) Informed to treatment supplier to take the parts within specified time.','1) Instructed to apply PX24 more and improved the packing method to sustain the PX24 till they are taking to process.\r\n2) Informed to treatment supplier to take the parts within specified time.','Next batch found satisfactory.','','2015-09-16','Avinash(R.J.)','Nandishkumar(D.K.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','17794','POST DN','yes','Misc','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8846,'18-210B','Magellan Aerospace(Chalfont) Limited','BODY','5757','D321 40204 204','','D, ECN NR29999ST1KM15, NR29999ST2KF65, WQN DFB09775',1,'P/074113','','42337','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Machine abuse observed inside holes.','1) This was happened due to blak mark witnessed on the parts due to temporary protection oil evoparated.','1) Instructed to apply PX24 more and improved the packing method to sustain the PX24 till they are taking to process.\r\n2) Informed to treatment supplier to take the parts within specified time.','1) Instructed to apply PX24 more and improved the packing method to sustain the PX24 till they are taking to process.\r\n2) Informed to treatment supplier to take the parts within specified time.','Next batch found satisfactory.','','2015-09-16','Avinash(R.J.)','Nandishkumar(D.K.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','17797','POST DN','yes','Misc','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8847,'18-210B','Magellan Aerospace(Chalfont) Limited','BODY','5757','D321 40204 204','','D, ECN NR29999ST1KM15, NR29999ST2KF65, WQN DFB09775',3,'P/074113','','42337','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Machine abuse observed inside holes.','1) This was happened due to blak mark witnessed on the parts due to temporary protection oil evoparated.','1) Instructed to apply PX24 more and improved the packing method to sustain the PX24 till they are taking to process.\r\n2) Informed to treatment supplier to take the parts within specified time.','1) Instructed to apply PX24 more and improved the packing method to sustain the PX24 till they are taking to process.\r\n2) Informed to treatment supplier to take the parts within specified time.','Next batch found satisfactory.','','2015-09-16','Avinash(R.J.)','Nandishkumar(D.K.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','17797','POST DN','yes','Misc','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8848,'35-249','Saab AB','STANDOFF','G21441K06','423Z1916-3','','---',8,'May 2015','','43896','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Thread tight.','Thread effective diameter oversize.Due to operator not checked in the m/c.  \r\n','Next production batch will be rework compelted.  ','Instructed operator to every part checked in m/c then remove the part.  \r\n','CAPA found okay, rework done ','','2015-09-18','Dinakar(K)','Shivanand D.B.,SHIVAKUMAR ,Raghavendra Rao R,Lohith K,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','','FI','yes','ST20','Manjunath(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8849,'42-005A','RAFAEL','Clamp-3 ','G21267K06','BA1E2004B','','38-576104 Rev E, TILDOCS#172373 Rev 14, PR603-2-3 Rev 16, RAFDOCS#5224238 Rev 4, 111.21 Rev 7, 111.22 Rev 1, ECN63628 2015/01/13, ECN60821 2014/10/26',1,'347592024-5','','45183','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','yes','1)1-no Thread gauge broken in side the part. ','During gauge using this was happened.','Just informed about the cost of the insytrumnet.','Preventive action not required and just informed','Not required.','','2015-09-18','Sudhagar(V)','Avinash(R.J.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','0','DN','no','Misc','Sudhagar(V)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8850,'18-076A','Magellan Aerospace Wrexham','COUPLING ','16146122','D282 50074 200','','A',2,'RP135274','','46927','','0000-00-00',NULL,'','','yes','','','','','','','C- axis problem.','C-axis position not locked in properly. \r\n','Inform to the maintenence and haas maintenence team. \r\n','Inform to the maintenence and haas maintenence team  \r\n','CAPA found okay','','2015-09-19','Dinakar(K)','        Dinakar K','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8851,'18-076A','Magellan Aerospace Wrexham','COUPLING ','16146122','D282 50074 200','','A',1,'RP135274','','46927','','0000-00-00',NULL,'yes','no','yes','no','yes','no','no','no','no','C-Axis problem.','C-axis position not locked in properly.  \r\n','Inform to the maintenence and haas maintenence team.  \r\n','Inform to the maintenence and haas maintenence team.  \r\n','CAPA found okay','','2015-09-21','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Shivanand(D.B.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8852,'35-191','Saab AB','SUPPORT-FTG','428595B','423Z1202-13','','---',1,'PA 1510 FORECAST-2','','46674','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Bore taper so one end accept another end is over size by 0.010mm.','Dia 14.288/14.302 hole finishing with reamer. 26nos qty manufactured,One part dia measures 0.01mm plus side for 3mm depth.\r\nSuspecting the vibration while reaming operation is under process.','Checked the reamer runout and part clamping in fixture.Zero point clamping cross checked and all features realated to clamping are found ok.\r\nOut of 26 nos remaining 25nos 100% bore checked and found ok.','As per the above Corrective action all the suspected root causes checked and in next batch production again this will cross check before running the production.','CAPA found okay, next parts found okay','','2015-09-21','Lohith(K)','Yarri Gowda,Umesh B,Shivaraj K S,Rangaswamy ,Manohara B.C.,Gurukiran S M,Dhananjaya N,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','VM2-2','Nagaraj(G. Nadiger)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8853,'18-116B','Magellan Aerospace Bournemouth','ASSEMBLY FORKEND','5565','F575 51377 200','','A',4,'RP408155','','46055','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Key way wrong side machined.','When key way operation running time part was wrong loaded. this is totally operator mistake.','Inform to operator key way operation running time every part loading correctly as per process sheet before machining the part and check the bore all parts.','Inform to operator key way operation running time every part loading correctly as per process sheet before machining the part and check the bore all parts.','CAPA found okay','','2015-09-21','Lohith(K)','Lohith K,Hari Prasad,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','9','no','HAASVF2SS-2','Lohith(K)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8854,'35-162','Saab AB','BEAM-LOWER_INNER_AFT','582082','423Z1403-2-02','','---',1,'PA-1300 2014','','39367','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Paint release found up to length of 5 to 7.50mm\r\nwidth approximately 3.00mm\r\nDepth 0.1mm','1) At the first sight of the photos it appears to be improper handling of the part OR improper packing OR probably part might have been touched before assembly.\r\n2) We have reviewed the dispatch details in the packing with picture and found it is good.\r\n3)We have checked the stock parts and found ok. pictures attached. \r\n\r\n','1)We have checked the paint adhesion with 3M tape that witnesses the material not chipped off. pictures attached.\r\n2)Informed to our treatment supplier and their opinion in first sight is same what we suspected of transit OR other handling damages.','1)We will check 100% tape adhesion test for these parts in next consecutive 2 to 3 batches.','We will monitor next consecutive batch.   ','C36271','2015-09-22','Avinash(R.J.)','Manjunath(G)','OF-000882','2015-09-21','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','16127','CUSTOMER END','no','Misc','Avinash(R.J.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8855,'18-319A','Magellan Aerospace Bournemouth','HALF CLAMP ','8031','D574 50552 200','DTD 5014','B01',88,'RP408269','','44426','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Machine abuse observed inside holes.','1) This was happened due to blak mark witnessed on the parts due to temporary protection oil evoparated.','1) Instructed to apply PX24 more and improved the packing method to sustain the PX24 till they are\r\ntaking to process. 2) Informed to treatment supplier to take the parts within specified time.','1) Instructed to apply PX24 more and improved the packing method to sustain the PX24 till they are\r\ntaking to process. 2) Informed to treatment supplier to take the parts within specified time','Next batch found satisfactory. ','','2015-09-22','Avinash(R.J.)','Nandishkumar(D.K.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','19277','POST DN','yes','Misc','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8856,'18-229B','Magellan Aerospace Bournemouth','CLAMP STRIP TOP OUTBD','421008','L572 52377 200','ABM3 1029','B00',1,'RP401009','','41806','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Linear indications observed on part surface.','1) This was happened due to blak mark witnessed on the parts due to temporary protection\r\noil evoparated. ','1) Instructed to apply PX24 more and improved the packing method to sustain the PX24 till they are\r\ntaking to process. 2) Informed to treatment supplier to take the parts within specified time.','1) Instructed to apply PX24 more and improved the packing method to sustain the PX24 till they are\r\ntaking to process. 2) Informed to treatment supplier to take the parts within specified time.','Next batch found satisfactory.','','2015-09-22','Avinash(R.J.)','Nandishkumar(D.K.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','18002','POST DN','yes','Misc','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8857,'40-008A','Universal Engineering Limited','PLATE JOINT','573050A2','D574 55150 203','','B, ECN GN150294ST1KA06',1,'322859','','47004','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Program transfer problem.  ','This devition due to error in program transfer while program transfering through LAN from server to machine.','Problem informed to machine supplier and checked the programs whic is running in machine and after ensuring the program, production continued.','Program transfer stoped in F5-1 machine till this problem is rectify.\r\n','CAPA found okay','','2015-09-23','Rangaswamy()','Umesh(B)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','1','no','Misc','Rangaswamy()','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8858,'35-249','Saab AB','STANDOFF','G21441K06','423Z1916-3','','---',12,'PA 1510 FORECAST-2','','47254','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Thread gauge tight.','Wrong program and while giving repass problem occurred\r\n','Instructed to CAD dept to edit program and freeze it \r\n','Instructed to CAD dept to edit program and freeze it \r\n','Found okay with next batch\r\n','','2015-09-23','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','','FI','yes','Misc','Nagaraj(G. Nadiger)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8859,'18-382A','Magellan Aerospace(Chalfont) Limited','SLEEVE BEARING ','240136','D575 40037 200','','A',1,'P/078238','','46993','','0000-00-00',NULL,'yes','yes','yes','','','','','','no','ID ovality problem Given tolerance is 11 micron part achieved is 30 micron','Due to ovality in part this deviation occur.\r\n','Instructed operator to check the ovality for every part,if\r\novality observed set the part zero run out and than run the\r\npart.\r\n','Instructed operator to check the ovality for every part,if\r\novality observed set the part zero run out and than run the\r\npart.\r\n','Found okay with next batch\r\n','','2015-09-23','Dinakar(K)','        Bharath R','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8860,'35-186','Saab AB','CED_LATCH_FITTING-FWD','563503','425Z0610-18','','---',6,'PA 1510 FORECAST-2','','46670','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','part center thickness under size(2.50+/-0.25 measured 2.0 to 2.05)','This deviation is due to tool down while running production batch, In between production this deviation coming and operator not checked the dimension which is deviated.','All the parts 100% inspection done and out of 12nos 6nos got rejected and another 06nos thickness found 2.62/2.63mm.\r\nAll the tool offset checked and found ok.\r\nAfter ensuring the tool offset and tool holders condition, production continued.','Tool holders clamping area(Hydraulic and Collet/Sleeves) visually checked and mechanical bolts condition cross checked for all the holders.\r\nEnsuring all the above parameters production continued.','CAPA found okay','','2015-09-24','Girish(Prasad P)','Girish(Prasad P)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Girish(Prasad P)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8861,'18-412A','Magellan Aerospace(Chalfont) Limited','ROD END','A0607N','D321 53012 200','','F01',1,'P078229','','46969','','0000-00-00',NULL,'yes','yes','yes','','','','','','','od dig mark.','In first operation total length is maintained to 70mm and center is provided for supporting purpose and that is cleared in final set up.in 2nd set up 66.65mm length is maintained and 3.35mm step is maintained for next set up for supporting purpose.in threadding operation turning tool z-offset is taken  to 3.35mm step and when 3.35mm is\r\ngiven in work offset to maintain 66.65 total length.when 3.35mm is moved in work offset so od tool running time od dig mark. \r\n','For next part turning tool and threadding tool z-offset is taken to face of the part and 3.35 mm is moved in work offset and run the part ,part found okay and continue the production.  \r\n','Instruction given to operator and cross check tool offset wheather the offset is taken correctly.\r\n \r\n','CA/PA Found ok.','','2015-09-25','','        KRISHNAMURTHY N','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8862,'18-082A','Magellan Aerospace Wrexham','STUD PLATE','297622/001','D278 50007 200','ABM3 1029','D01',1,'RP135247','','47054','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','DIG mark observed on face.','While part running time part was lifted so dig mark on top face.','Inform to operator while 2nd operation part loading time cross check the butting area and clamping pressure in mandatory.  ','Inform to operator while 2nd operation part loading time cross check the butting area and clamping pressure in mandatory.','CA/PA found okay.','','2015-09-25','Lohith(K)','Yarri Gowda,Shivaraj K S,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','5','no','VM2-1','Lohith(K)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8863,'18-465A','Magellan Aerospace Wrexham','FRAME MID RIB L','6518801 1','L575 51892 200 PF','','A',1,'RP133570 Amnd 1','','46736','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Base thickness 2 +0.2/-0.1mm measureing 1 pocket under size 1.88 to 1.83.','1)Due to part not properly seated to the fixture that leads to took cut more material.\r\n2)This was noticed at our final inspection and internal NCR raised and communicated to production department.\r\n3)This was not spotted during line inspection due to that spot not picked. Since lugs will be there.\r\n4)Usually we are checking the thickness 2 to 3 places in the pocket but that area was not picked because the undersize area is locally around 50x30mm.\r\n5)Due to mis communication this was not informed to source quality representative.\r\n','1)We have checked the other parts and found ok.\r\n2)Manual clamping method will be changed to zero point air clamping fixture.\r\n3)Touch probe will be introduced in the machine itself to check the web thickness before removing the part from machine.\r\n','1)We have checked the other parts and found ok.\r\n2)Manual clamping method will be changed to zero point air clamping fixture.\r\n3)Touch probe will be introduced in the machine itself to check the web thickness before removing the part from machine.\r\n','CA/PA found satisfactory.','','2015-09-26','Narayanappa(G)','        Sathish Y.R.,PAVAN KUMAR  S.K.,Paramesh K,Narayanappa G,Manjunatha N.R.,Manjunath K.N.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Manufacture Only','','fi','yes','VR11','Avinash(R.J.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8864,'35-241','Saab AB','HANDLE','431589A2','425Z0634-2','','--C',1,'PA 1510 NEW PARTS-1','','43241','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','*Part dig mark observed.','* While running wall finish dia 8flat cutter broken and dig mark observed in part.','*New tool placed and checked the tool offset and wear value and then continued production. Next part\r\nchecked the dimensions and then continued production. ','Informed to operators and supervisors to check the tool condition before loading the tool to\r\nholders. On going training implemented to get awerness to operators to check the tools geometry\r\nregulerlly for all the tools. ','CAPA found okay, next parts found good','','2015-09-27','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','05','no','Misc','Lohith(K)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8865,'18-299A','Magellan Aerospace Bournemouth','SHAFT ','B4479A','L575 52465 200','S145FHT','A00',1,'RP408152','','46601','','0000-00-00',NULL,'yes','yes','yes','','','','','','','od dig mark 1 no','First we are run the facing program then run the center drill and give the center suport and run the the part then finally we are finishing dia 12.649. so check the stock for final pass and reset the program and run the part that time facing tool came and dig the part od so part will be rejected.   ','change the insert corner and taken the z and x offset and plus taken in the wear offset and check the stock and give the correction and run the part. ','After running the every part check the stock for the finishing tool before running the final pass and check the program which tool will be running then run the part.','CA/PA found satisfactory.','','2015-09-28','Sandhesh D(S)','        Devaraj K.C.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8866,'42-002','RAFAEL','PSA BASE','K10598','BA1E2001B','','38-576104_Rev-E, TILDOCS#172373_Rev-13, RE_804-1-5_Rev-11, 111.21_Rev-6, 23.36.59_Rev-F, ECN 57176 2014/08 /25; ECN 58483  2014/07/29',1,'347592024','','45381','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Part running time material chipped off.  ','1) Due to vibration of the part during machining this was happened.\r\n2) During trial stage this was happened.','1) Re-process done and parts accepted at customer end.','1) Re-process done and parts accepted at customer end.','CA/PA found satisfactory.','','2015-09-28','Ramesh(Poojary)','Ramesh(Poojary)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','07','no','Misc','Anjinamurthy(H)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8867,'18-113A','Magellan Aerospace Bournemouth','ADJUSTER','242096','D575 40496 200','S80 FHT','G',1,'RP408153','','46995','','0000-00-00',NULL,'yes','yes','yes','','','','','','no','4mm thickness & 16.68 under cut under size( -0.2mm)','Setting time  Tool nose radious not given in od finishing tool. thickness meassured in plus side correction given in wear offset and tool nose radious given and od finishing tool repass running, undercut and thickness undersized. ','Taken plus in wear offset and run the part found ok. ','instruction given to the operator while before running the part cross check the tool compensation. ','Next batch found satisfactory.','','2015-09-28','Sandhesh D(S)','                GUNDEGOWDA H.G.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8868,'18-460A','Magellan Aerospace Wrexham','RIB CLOSING OUTBOARD','626249','L575 59269 201 PF','','A00',4,'RP133603 Amnd 4','','46688','','0000-00-00',NULL,'yes','no','no','no','yes','yes','no','no','no','BORE DIA 52+0.3mm measure at 52.35/52.42.','Part hole machining done using dovetail cutter in first setup. the bore surface is in negative position so while completed the machining under the machine it was measuring dia 52.25/52.30. This dimension measured in Varner Caliper.Hole is in negative wall and cheking is verying by checking in varnier caliper. but after completing the second setup, hole dimension can check in variner. \r\nAfter completing tthe second setup hole diameter measures plus side. ','Immedeately checked all the parts machined and found all the same deviation in all the 4 parts.\r\nProblem analyzed and planned to manufacture Plug guage to check the dimension in operatio-01.\r\nProgram checked and found ok.Program already generated with centerline and we can able to control the diameter by given CRC value in machine.\r\n','Informed to operator to check the every part in plug gauge while doing operation -01.\r\nComment entered in program to remind the operator to check the part with plug guage.\r\nSupervisor will ensure the diameter for all the part before unloading the part.\r\n ','Next batch mandatory.','','2015-09-28','Narayanappa(G)','PAVAN KUMAR  S.K.,Narayanappa G,Manjunatha N.R.,Manjunath K.N.,Gajendra Singh C.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','Manufacture Only','','FI','no','DMG 360L','Avinash(R.J.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8869,'18-460A','Magellan Aerospace Wrexham','RIB CLOSING OUTBOARD','626249','L575 59269 201 PF','','A00',4,'RP133603 Amnd 4','','46688','','0000-00-00',NULL,'yes','no','no','no','yes','yes','no','no','no','thickness 2.2+0.2/-0.1mm measured at2.0 to 2.10 at local points (15x6mm area)','Thickness maintaining in conventional machine and have manual feed. While clamping the part in machine bed, part not butted properly.\r\nThickness maintained minimum side by operator, therefore locally thickness measures minus side due to part not butted properly.','Informed to operator to maintain the thickness in maximum side.\r\nPart butting to be ensure by feeler gauge before machining.\r\n\r\n','Informed to operator to maintain the thickness in maximum side.\r\nPart butting to be ensure by feeler gauge before machining.\r\nSupervisor will ensure the part 100% by checking while machining is under process in milling machine.','Next batch mandatory','','2015-09-28','Narayanappa(G)','PAVAN KUMAR  S.K.,Narayanappa G,Manjunatha N.R.,Manjunath K.N.,Gajendra Singh C.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','Manufacture Only','','fi','no','DMG 360L','Avinash(R.J.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8870,'40-002A','Universal Engineering Limited','JOINT PLATE ','573050A2','D574 50014 201','','A, ECN NG23774ST2KF47',1,'322870','','46318-1','','0000-00-00',NULL,'','','yes','','','','','','no',' Dig mark observed on part.','Part wrongly loaded in operation-03.Location pin is in diagonal and able to locate at both the orientations.Operator not noticed the loading of part and dig mark observed after running roughing tool because part was wrongly loaded. ','Immediately checked and marked the front face for all the remaining parts. Informed to operators to ensure the front face after loading the part in fixture. Production continued and supervisor is monitoring. ','The following PA action planned and implemented, 1.Location pins diameter changed and amended in MPS. 2.Dia 6 and Dia 5 mm locating pins introduced to avoid wrong locating of part inoperation-03. 3.New program created for dia 5 H7 hole.','CA/PA found satisfactory.','','2015-09-29','','        Anjinamurthy H','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8871,'18-090A','Magellan Aerospace Bournemouth','BUSH','259690','D278 50164 200','S80 FHT','A',2,'RP408159','','46152','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','OD under size','While running time chips not removed and air gauge not setting\r\nproperly So OD under size.','Next part running time chips removed.','Instructed operator to every part.','CA/PA found ok.','','2015-09-29','Dinakar(K)','Shivappa M B,Shivanand D.B.,SHIVAKUMAR ,Seetharamu D,Rajesh T,Raghavendra Rao R,Nataraja C V,Manjunatha N,Manjunath  M,Dinakar K,Devaraj K.C.,Ashith B,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','0','FI','no','QT100S-1','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8872,'18-419A','Magellan Aerospace(Blackpool) Limited','BRACKET','221829','PI55-2120010-00','','NIL',3,'P/501903','','47046','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Dig mark on R5.6 to R6.8.','This deviation is due to program error. Program backup was deleted in machine and proved programs\r\nwhich is saved in server taken and runned the program. This program have problem while proving the\r\nFAI and after FAI proving customer find the deviation and informed to modify the model and re-FAI\r\ndone and then part was accepted. the accepted part program was not saved in server and due to this\r\nerror this deviation coming. ','After finding the deviation new programs(proved in CAD)taken and part manufactured and checked,Part\r\nfound ok. Next production continued. Proved program saved in server and informed to supervisor to\r\nmonitor and give updated backup to CAD. ','FAI proved programs to be saved as per processor and any modification done CAD and production\r\nsupervisor to coordinate and save the programs in server. ','CA/PA found ok.','','2015-09-29','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','0','FI','no','Misc','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8873,'34-038B','Magellan Aerospace Winnipeg','FITTING HINGE LUG L/H','55591-1','400-12910-1-905','','EM105092 Iss F, EM104302 Iss A, EM104765 Iss G, EM106399 Iss B, EM106400 Iss B, EM106401 Iss A, EM106404 Iss A, EM106522 Iss A, EM106602 Iss A',1,'B91379 Rev.026','','47008','','0000-00-00',NULL,'yes','yes','yes','','','','','','no','Outer profile minus 0.3mm ','While doing machining tool holder run out was not checked that leads to thickness took more cut.','Informed to operator to check the tool holder run out before start the production.','Informed to operator to check the tool holder run out before start the production.','Next batch found satisfactory.','','2015-10-01','Lohith(K)','        Theerthappa K.N.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8874,'18-088A','Magellan Aerospace Wrexham','PLATE SEALING','451690','D572 52998 200','ABM3 1029','A',1,'RP135247','','47081','','0000-00-00',NULL,'yes','yes','yes','','','','','','no','wrong offset taken.','After running the CCGT boaring tool tip formed in the part so for the next part change the block and adjust the tool for removing the tip but not taken the Z offset and run the part that time boaring bar taken the extra cut so total lenght 1mm undersized.','For the next part re-offset taken the tool and run the part,part checked found ok. ','It is the manual error so warning given to the operator and trained. ','CA/PA found satisfactory.','','2015-10-01','','        Dinakar K','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8875,'18-105A','Magellan Aerospace Bournemouth','FORKEND ASSEMBLY','620469','D572 50462 200','S98 FHT','J01',1,'RP408148','','47432','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Runing time insert broken so O.D Dig mark part rejected','Part running time coolent was not flow to the insert tip so part was over heated and insert will be brocken and dig mark occured in the running part so part will be rejected.','Change the insert corner and taken the offset and plus taken in the wear offset and  Adjust the coolent for the insert corner and run the part and check the part and give the proper correction and part checked found ok.','While part running time check the coolent and before running the every part check the insert corner and then run the part.','Next part found ok.','','2015-10-01','','        Shivappa M B','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8876,'28-006A','Magellan Aerospace New York  Inc.','SHOULDER BOLT ','574049','162A3109 -2','',' 	PL Iss A, PSDL Iss A, ECN C141079',1,'130677','','45946','','0000-00-00',NULL,'','','yes','','','','','','','OD Under Size 0.01mm...','','','','part accepted.','','2015-10-01','','        Seetharamu D','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8877,'18-493A','Magellan Aerospace Wrexham','FITTING AFT','444706A','L575 52124 200','','A00',1,'RM132920 Amnd 1','','45837','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','Tool dig mark in rib top face, program fault.','The program and tool retraction value Increased more than part height. ','Immediate changed the program and tool retraction value Increased more than part height. \r\nRun the new program & no dig mark found on the part.','Here after any program Retraction value is more than part total height.\r\nBefore transferring program ensure the program retraction values.','Next production parts found satisfactory.','','2015-10-05','Ramesh(Poojary)','Rangaswamy()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Rangaswamy()','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8878,'18-499A','Magellan Aerospace Wrexham','FITTING','6482801','L575 54954 201','','A00',1,'RM132920 Amnd 1','','45539','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','Thickness undersize.','Base thick minus for program fault.\r\nFixture hight not maintain for required process and not cross check the fixture. Part program run on same fixture, part was rejected due to base thickness mesures undersize','Fixture hight maintained and validated the fixture , validation found ok and part run on the same fixture part found ok','before load the part , fixture validated and cross theck on machine fixture loction hole and fixture z hight.','CA/PA found OK.','','2015-10-05','Ramesh(Poojary)','Rangaswamy()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Rangaswamy()','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8879,'35-138','Saab AB','FLCD_DS_SUPPORT_DEFLECT_S','7543150','423Z6189-3','BAC1534-62C','---',2,'PA 1510 FORECAST','','47360','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Material layer chip out','Due to material behavior this was opened out.','1) We decided that this cannot be avoided but we minimized by improving the handling methods.','1) We decided that this cannot be avoided but we minimized by improving the handling methods.','CA/PA Found ok.','','2015-10-06','Krishna(Chowdary.G.P.)','Lohith K,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','HAASVF2SS-2','Nagaraj(G. Nadiger)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8880,'35-138','Saab AB','FLCD_DS_SUPPORT_DEFLECT_S','7543150','423Z6189-3','BAC1534-62C','---',1,'PA 1510 FORECAST','','47610','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Material layer chip out.','Due to material behavior this was opened out.','1) We decided that this cannot be avoided but we minimized by improving the handling methods.','1) We decided that this cannot be avoided but we minimized by improving the handling methods.','CA/PA Found ok.','','2015-10-06','Lohith(K)','Hari Prasad,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','HAASVF2SS-2','Nagaraj(G. Nadiger)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8881,'35-138','Saab AB','FLCD_DS_SUPPORT_DEFLECT_S','7543150','423Z6189-3','BAC1534-62C','---',8,'PA 1510 FORECAST','','47361','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Material layer chip out.','Due to material behavior this was opened out.','1) We decided that this cannot be avoided but we minimized by improving the handling methods.','1) We decided that this cannot be avoided but we minimized by improving the handling methods.','CA/PA Found ok.','','2015-10-06','Lohith(K)','Theerthappa K.N.,Lohith K,Hari Prasad,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','HAASVF2SS-2','Nagaraj(G. Nadiger)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8882,'18-615A','Magellan Aerospace Wrexham','RECEPTACLE','442637C','L575 54240 200','','A00',1,'RM132921 Amnd 1','','46280','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Bore dia 6.00/6.012mm oversize by 0.01mm.','Dia 6.00(+0.010) bore finish using for 3fl with crc program. checking in air gauge, but air gauge\r\nshank diameter 5.99mm but operator every time 20 micron correction in crc value so 6mm bore\r\nmaintain time air gauge not enter so operator again correction 20 micron.bore over size.','After that corrections One part finish part found ok.','Next batch using same dia 6 reamer for bore finish all parts found ok.','Next parts found ok.','','2015-10-06','Rangaswamy()','Manohara B.C.,Gurukiran S M,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','MakinoF5','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8883,'35-266','Saab AB','LATCH PROBE','G21506K02','424Z6101-1','','--A',1,'PA 1510 FORECAST-2','','47359','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Dig mark observed on OD','Running time z axis down so part dig mark.','Immediately inform the machine supplier, and all parameters checked and production starts with monitoring of tool offset. ','Inform to operator when running time Z axis down immediately stop the machine, inform to concern supervisor.  ','Regularlly monitoring the issue by operators and supervisor and still problem is not repeated again CA/PA found satisfactory.','','2015-10-06','Lohith(K)','        Yarri Gowda','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8884,'18-603A','Magellan Aerospace Wrexham','BRACKET','8077701','L575 52139 201','','A00',1,'RM132920 Amnd 1','','46941','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','3.00MM BASE THICKNESS UNDER SIZE BY 0.25 TO 0.30MM.','Due to Fixture part butting problem. This is manually error operator part not butting properly.','Ensure the part butting properly by 50 micron feeler gauge before start of production.			','Ensure the part butting properly by 50 micron feeler gauge before start of production.	','CA/PA found satisfactory.','','2015-10-07','Girish(Prasad P)','Girish Prasad P,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','MakinoF5-4','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8885,'35-263','Saab AB','EXTENSION ROD','970481','424Z3414-1','','--A',1,'PA 1510 FORECAST-2','','44877','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','no','Missing Solid film Lubricant on threads in accordance with BAC5811, Type VII Class 1.','1) We checked the stock parts and found parts with less Solid film lubricant.\r\n2) Again checked the treatment certificates and found they released and confirms to solid film lubricant.\r\n3) Again checked the screen shot for treatment and found correct.\r\n4) Immediately raised the non-conformance report to treatment house.\r\n4) This was escaped because inspector mis interpreted and thoughts and he assume that steel parts are less primer.\r\n5) This first Boeing787 part awarded for us which carries primer.\r\n','1) We will take the picture of finished part that helps to inspection after treatment.\r\n2) Same method adopted for checking and identifying part marking as well as Left hand and right hand part.\r\n','Same method will be adopted for all the parts.\r\nRefer treatment CAR report.','CA/PA found satisfactory.','C39148','2015-10-07','Avinash(R.J.)','Manjunath(G)','OF-000927','2015-10-06','Thread is damaged in 1no','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','19251','CUSTOMER END','no','Misc','Manjunath(K)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8886,'18-118B','Magellan Aerospace Bournemouth','BEARING HOUSING','244364','D275 40005 200','','C01',1,'RP408156','','47245','','0000-00-00',NULL,'yes','yes','yes','','','','','','','total length -.3mm od finishing runing time thicknes under size -.3mm  \r\n','While clamping the part, in the butting face chips will butted so faceout occured in the running part and half of the part total lenght meassures 0.28 to 0.3 undersized but not observed the operator.  \r\n','while clamping time clean the jaws by using air, and after clamping the part for every part rotate the chuck and cross check the butting fece visually and then run the part and after run the part check the total lenght for every parts hundred percently.','next every batch we are check the total lenght hundred percent.after clamping the part for every part rotate the chuck and cross check the butting face visually and then run the part and after run the part check the total lenght for every parts hundred percently.and avoiding the this type of errores.  \r\n','CA/PA found ok.','','2015-10-07','Ravi(M)','        Shivappa M B','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8887,'18-008A','Magellan Aerospace Wrexham','Plate Cover','497610','D572 52518 200','L97 T351','A',1,'RP135247','','47086','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','OD dig mark.','Part not centered in fixture properly so dig mark found on\r\npart.','Instructed to operator for checking centering of part in fixture or not then run the part.','Planned new fixture for avoiding such errors in for further\r\nbatches.','CA/PA found ok.','','2015-10-07','Ravi(M)','Shivanand(D.B.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Shivanand(D.B.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8888,'18-002A','Magellan Aerospace Wrexham','Bracket Support- RH','6518801 1','D361 50110 201','ABM3 1029 T7651','A',1,'RP135242','','47644','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Base thickness minus side maintained.   ','While part running time part was lifted so base thickness minus side.External clamp putting time not tight in properly This error happened operator mistake. ','Next part loading time check the all clamps and part butting properly.\r\nInform to operator every part loading time check the part butting area.  ','Next batch production running time change the external clamps.\r\n','Next batch found satisfactory.','','2015-10-07','Lohith(K)','        Dhananjaya N','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','no','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8889,'28-003A','Magellan Aerospace New York  Inc.','PIN-ATTACHMENT WALKING BE','970671-01','161A7305-1','','PL-Rev-NC, DL Rev-B',1,'126999_R0_C1','','46872','','0000-00-00',NULL,'yes','no','no','no','no','yes','no','yes','no','Thread no go answered.','Due to while thread running time thread insert brokened and broken insert is taking over cut and therad major dia will be undersize so thread NOGO answered.  \r\n','Next part thread insert changed and takened tool X-offset&Z-offset and maintained the thraed effective dia and soot the thread gauge,Gauge is answered and run the part.  \r\n','Inform to operator every 50 nos will be completed changed the insert and takened tool X-offset&Z-offset and maintained the thraed effective dia and soot the thread gauge,Gauge is answered and run the part.  \r\n','Next part found ok.','','2015-10-08','Avinash(R.J.)','Sudhagar(V)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','FI','no','Misc','Sudhagar(V)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8890,'35-170','Saab AB','ALCD_STRUCT_SUPPORT-FTG_L','452389B','423Z1200-11-01','','---',2,'PA 1510 FORECAST','','46302','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Slot width over size (required 28.7 +/- .012 measured 28.95 t0 26.06).','This problem is due to tool holder problem. tool got 0.5mm runout, therefore slot width measures 26.06 to 28.95.\r\nOperator not checked this dimension in first part and next part also got deviation, in second parts operator checked this dimension and stopped the machine to analyzed the problem.','While analyzing the reason for deviation, holder problem noticed.\r\nTool holder thread area have crack and clamping nut not clamped properly and tool have 0.5mm run out.\r\nImmediately all the tool holders(collet holders) condition checked and physically threads and nuts checked. ','Informed to supervisors and operators to check the tool holders regularly and find any problem in holders action to be taken and avoid such problem in future.,','Next Parts found okay','','2015-10-08','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Rangaswamy()','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8891,'35-169','Saab AB','ALCD_STRUCT_SUPPORT-FTG_L','452389B','423Z1200-12-01','','---',1,'PA 1510 FORECAST','','46300','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dimension 81.00 +/- 0.25 measured 79.45 so length minus side.','While running production this deviation coming due to part not butted properly to pins or Part\r\nmoving while running the program due to clamping error. \r\n','After checking the deviation next part butting checked with feller gauge and also clamps tightness\r\nchecked and found ok. Checking all the above and production continued. \r\n','One more location done to avoid part moving and also part straightness will achieve after loading\r\nthe part automatically. This new fixture introduced and checked the all the PA points and all are\r\nfound OK. \r\n','CA/PA Found satisfactory.','','2015-10-08','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Rangaswamy()','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8892,'35-182A','Saab AB','EDGE HOUSING','453560C','423Z1121-5-02','','--A',1,'PA 1510 FORECAST','','47332','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dig mark on part.','While running operation-02 dia 16flat cutter broken and deg mark observed on part wall.\r\nThis deviation is due to tool problem, dia 16r3 cutter taper in length and this causes vibration and made to cutter broken.','Changed the cutter taken approval from the CAD dept and after ensuring the taper continued production.\r\nAnd informed to cutter supplier to replace the cutter and check the cutter taper.','all the long series cutter taper to be checked internally and also informed to cutter supplier to check and validate the cutters before sending to us.\r\n\r\nWe are on trails of WIDIA make long endmill and after proving the cutters the above deviations will me avoided.','CA/PA found ok.','','2015-10-10','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','05','no','Misc','Krishna(Chowdary.G.P.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8893,'35-183A','Saab AB','EDGE HOUSING','119572B6','423Z1121-6-02','','--A',1,'PA 1510 FORECAST','','46748','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Operation 03 running time tool down so base thick minus (-1.0 mm).','While running operation-03 tool down because of tool holder problem.\r\nOperator ensured the tool clamping length and cuttter and holder visually.After ensuring only tool clamped in holder.\r\n\r\n','Defect Tool holder scraped and tool clamped with hydro grip and then continued production.\r\n\r\nAll the tool holders checked the condition like collet holders nut, collet condition, hydro grip diameter(any scratches) collets damage if any.\r\nInformed to all the supervisors/operators to monitor the holders/collets condition frequently.','Informed to all the supervisors/operators to monitor the holders/collets conditions frequently.\r\nTool grip persons will cross check the holders/collets every week.','CA/PA found ok.','','2015-10-10','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Rangaswamy()','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8894,'18-405C','Magellan Aerospace Bournemouth','RIB 14 AFT- RH ','2873901','PI L575 52364 20101','','E00',1,'RP408144','','47344','','0000-00-00',NULL,'','','yes','','','','','','no','tool dig mark observed on rib top of the part.\r\n','m/c z axis problem, alarms - 102  servos turned off\r\n830 -     z axis serial   data communication fault alarms appears at  dia 25R5 rib top finish program under running.','stop the production and informed to the service engineers,  change z axis  drive cable & continue the production.   \r\n','inform to the maintenance team chuck the every 3 month in all axis drive cable.   ','Next batch found satisfactory.','','2015-10-10','','        PAVAN KUMAR  S.K.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8895,'28-004A','Magellan Aerospace New York  Inc.','PIN','G19559K08','161A2332-1','15-5PH Steel Bar per','NA',1,'120243-3172','','30339','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','1) key way and flats on flange missing. ','1)We have thoroughly investigated and every stage witnessed the operation performed.\r\n2)After CIM inspection again these parts offered to Magellan Indian team.\r\n3)And we are concluded that this was escaped in all stages.\r\n4) During shift relieve this might be happened due to miscommunication between 1st shift operator and second shift operator by keeping the semi-finished parts in the finished parts area. ','1)We informed to all concerned personals about the escape.\r\n2)Specially informed to packing department to check to confirm all operation completed and also informed. if they found any un identical parts.\r\n3)We will improve the inspection lighting for final inspection.\r\n4)Now we changed our procedure for handling of rejected parts that during intermitted stages any part rejected then the part will be scrapped in the same time. If that part not require for any further analysis.','Same as above.','Next batch found satisfactory.','C37717','2015-10-13','Avinash(R.J.)','Sudhagar(V)','IRR 114063','2015-09-07','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','0','Customer End','no','Misc','Sudhagar(V)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8896,'18-445B','Magellan Aerospace Wrexham','PIPE END FITTING','M506580','L280 50067 210 PF','','A00',4,'RP140358','','47664','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Groove width oversize.','dial stand not setted zero properly so od undersize .','dial stand setted zero using master slip gauges & run the part\r\n,part found ok.','instructions given to operator to crosscheck the instruments at regular intervals .','Next Parts found okay','','2015-10-13','Narasimhamurthy(K.G.)','Ravi C,Dinakar K,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','3','no','QT100S-4','Narasimhamurthy(K.G.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8897,'18-497A','','','','','','',0,'','','','','0000-00-00',NULL,'no','no','no','no','no','no','no','no','no','','','','','','','2015-10-13','select','','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','','','02','no','','select','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8898,'18-090A','Magellan Aerospace Bournemouth','BUSH','259690','D278 50164 200','S80 FHT','A',2,'RP408159','','46602','','0000-00-00',NULL,'','','yes','','','','','','','OD 39.964/39.980 measures 39.957 to 39.960.','While running coolant not adjusted so due to wear out of\r\ninsert OD under size.','Instructed to operator for checking coolant for every tool and\r\ncheck insert wearout regularly.','Instructed to operator for checking coolant for every tool and\r\ncheck insert wearout regularly.','Next Parts found okay in Production','','2015-10-13','','        Devaraj K.C.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8899,'18-497A','Magellan Aerospace Wrexham','FITTING','442586A','L575 52127 201','','A00',1,'RM132920 Amnd 1','','47623','','0000-00-00',NULL,'yes','yes','yes','','','','','','no','fixture wrong loading so part reject. ','This is major mistake. operator not check fixture loading.\r\nfixture wrong loading so part reject. ','Train to operator, explained our process and our operation sheet after fixture loading once again cross check process sheet and offset.','This rejection is due to manual error, Explained to operator regarding the process. ','CA PA found ok.','','2015-10-13','Rangaswamy()','        Rangaswamy ','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8900,'35-266','Saab AB','LATCH PROBE','G21506K02','424Z6101-1','','--A',1,'PA 1510 FORECAST-2','','47359','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Part location pin not locket in part hole.','Part location pin not locket in part hole.operation 09 setup using in 35-266-JF02 fixture for part clamping.this fixture using one location pin for part locket but operator not locket pin so part shifted and rejected. ','Production supervisor will ask and train to operator about process cross checking before start of NC cycle for next two OR three batches.','Production supervisor will ask and train to operator about process cross checking before start of NC cycle for next two OR three batches.','CA/PA found satisfactory.','','2015-10-14','Rangaswamy()','Rangaswamy()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','07','no','Misc','Anjinamurthy(H)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8901,'18-404C','Magellan Aerospace Bournemouth','RIB 14 AFT- LH','444357','PI L575 52364 20001','','E00',1,'RP408144','','44711','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','part meeting face tool dig mark.','while program running time  air pressure to low spindle  rotation was not stopped so part positive wall dig mark in one place. ','stop the production,inform to the maintenance team, setting the air pressure gauge & continue the production. ',' inform to the maintenance team chuck the every shift air pressure gauge & maintain the all machine sufficient air pressure','CA/PA found satisfactory.','','2015-10-14','Narayanappa(G)','Sathish Y.R.,PAVAN KUMAR  S.K.,Manjunatha N.R.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','13','no','HAAS','Narayanappa(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8902,'18-232B','Magellan Aerospace Bournemouth','CLAMP STRIP BTM OUTBD','453024','L572 52378 201','ABM3 1029','B00',1,'RP408289','','47494','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Dig mark observed on radius. ','10 ball nose radius program running time part moving in back side part radius dig mark so part reject clamping problem.','Moving forward clamping method & one more pin located added & implemented in next part. Parts are accepted & process sheet will be updated in next batch production.','Same will be undated in process sheets & inform to operator as per process sheet clamped.','Next parts found ok.','','2015-10-14','Anjinamurthy(H)','        Girish HP','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8903,'18-210B','Magellan Aerospace(Chalfont) Limited','BODY','5757','D321 40204 204','','D, ECN NR29999ST1KM15, NR29999ST2KF65, WQN DFB09775',1,'P/078231','','47758','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','dia 32.56 bore oversized (+0.1).','Running time tool screw will be brocken, so id dia 32.56  0.1 oversized.','Screw will strucked inside the tool so change the tool and taken x and z offset and run the part part checked found ok.','while setting time check the all tools then do the setting and dont use any screw slipped tools. ','Parts accepted.','','2015-10-15','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','With Treatment','','01','no','Misc','Sandhesh D(S)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8904,'35-263','Saab AB','EXTENSION ROD','970481','424Z3414-1','','--A',1,'PA 1510 FORECAST-2','','44876','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Thread NOGO answerd.\r\n','After 25nos running threading insert will be wear out.for next part threading insert will be changedand 0.4 plus(+)taken in wear offset and run the part but thread gauge was not answered then 0.2 minous(-) taken to wear offset and run the part that time thread gauge was nogo answered.','For next part x-offset taken and taking 0.3 mm up in toolwear offset and run the part gauge not answerd,in x-offset give 0.1mm down and run the part and gauge not answered then in x-offset down0.05mm and run the part and then gauge answered and next part run in same reading &the part found okay.','Instruction given to operator to take x-offset & z-offset whenever the inserts are changed and monitor supervisors. ','Next production batch found okay.','','2015-10-16','Dinakar(K)','Ravi R,Nataraja C V,Mohan Kumar C.M.,Manjunath  M,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','QT100S-1','Nagaraj(G. Nadiger)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8905,'18-431A','Magellan Aerospace(Chalfont) Limited','SPRING RETAINER ','A0563X','D321 40203 220','','L',1,'P078229','','46971','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','ID Dia 17.51/17.53 measured 17.64 mm.','Chips cloted while finishing the bore due improper flow\r\nof coolent. ','Instructed operator to adjust the coolent and clean the chips\r\ninside the bore with pressurised air. ','Instructed operator to adjust the coolent and clean the chips\r\ninside the bore with pressurised air. ','Next Parts found okay in Production','','2015-10-16','Dinakar(K)','Shivanand D.B.,Seetharamu D,Raghavendra Rao R,GUNDEGOWDA H.G.,Dinakar K,Ashith B,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','DX 200-2 ','Narasimha Murthy(R)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8906,'18-411A','Magellan Aerospace(Chalfont) Limited','PLUNGER','237004','D321 40205 200','','H01',1,'P078230','','47820','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','yes','no','Dia 17.446 undersize by 0.01mm.','Due to problem in getting consistency in this part for this dimension this will happen.\r\n','Planned for other grade of inserts and incorporate one more tool between roughing and finishing.\r\n','After incorporate mentioned above that feed back was taken and same was updated.\r\n','CA/PA found satisfactory. ','','2015-10-16','Narasimhamurthy(K.G.)','KRISHNAMURTHY(N)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Narasimhamurthy(K.G.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8907,'18-054C','Magellan Aerospace Bournemouth','CLEAT ','455036','L575 52580 200','','A00',5,'RP408128 Amnd 01','','47810','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Thickness 2.5mm 0.4mm minus.\r\n','Operation 03 setup using 18-054B-JF01 fixture.in this fixture used  two crn machining with different location pin. but operator complete one crn change location pin to another crn but operator not change location pin. ','Next shift operator check part find the problem stop the m/c inform to supervisor,then correction offset then run production.','Next batch change the fixture and change process. \r\n','CA/PA found OK.','','2015-10-17','Rangaswamy()','Rangaswamy()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Rangaswamy()','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8908,'18-054C','Magellan Aerospace Bournemouth','CLEAT ','455036','L575 52580 200','','A00',2,'RP408128 Amnd 01','','47703','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Thickness 2.5mm 0.4mm minus.','Operation 03 setup using 18-054B-JF01 fixture.in this fixture two crn machining with different location pin. but operator complete one crn change location pin to another crn but operator not change location pin. ','Next shift operator check part find the problem stop the m/c inform to supervisor,then correction offset then run production. ','Next batch change the fixture and change process. ','CA/PA found OK.','','2015-10-17','Rangaswamy()','Rangaswamy()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Rangaswamy()','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8909,'18-617A','Magellan Aerospace Wrexham','TUBE DISTANCE','21973523','L575 55276 200','','A00',1,'RM132920 Amnd 1','','46841','','0000-00-00',NULL,'yes','yes','yes','','','','','','','id oversize +0.015.','setting time -.1 taken in wear offset and check the part part came in -.1 then 0.05 correction given and check the part using in airgauge part meassured -0.04  for next pass give the correction 0.04 and check the part it will .015 oversized.         ','For the next part -.015 taken the wear offset and run the part.part checked found ok.','Inform to the operator for the first part taken minimum    -0.3 and check the part and give the the correction 4 to 5 times and run the part.','Next part found ok.','','2015-10-17','','        Ningaraj A N','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8910,'18-087B','Magellan Aerospace Wrexham','Plate Sealing','9026802','D572 52914 200','ABM3 1029','B',1,'RP135239','','47560','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Tool offset wrong.','Due to first part setting time tool offset taken wrong.So part base dig mark.This error happen senior operator mistake. ','Next part loading time remeasure the tool offset and continue the production and next part found okay. Inform to operator strictly Warned as per the referance book value while tool offset taken time remeasure the tool offset next parts continued & found ok.','Inform to operator while tool offset taken time remeasure the tool offset after mention the value in the reference book then continue the production. ','Next parts found ok.','','2015-10-18','Anjinamurthy(H)','Prashanth Kumar(M)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Anjinamurthy(H)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8911,'35-233A','Saab AB','HINGE BRACKET 5 ','3858901','D576 50008 208','','D00',1,'1600121830','','47603','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Bore over size dia 22.225+/-0.012 measured 22.245 to 22.250.','This deviation found in between production running.\r\n120nos of slotting and boring operation done and there is no chance of manual deviation in between production,\r\n01no. got deviation in bore and operator checked after parts completed out side the machine.\r\nFor next part operator checked the bore with stock( boring bar reset) and next all the parts are found ok.','All the 120nos quantities bore checked.\r\nReason for deviation is not found.\r\nInformed to operators to analyzed the problem in further batches.','Reason for this deviation is not found.\r\nInformed to operators to analyzed the problem in further batches.','Next Parts found okay','','2015-10-18','Girish(Prasad P)','Shreekanth(L)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','05','no','Misc','Girish(Prasad P)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8912,'18-164B','Magellan Aerospace Bournemouth','Strut Mid Rib ','A631637','F574 50160 201','','B02, ECN PG49998ST1TW21, PG40011ST1KK22',1,'RP408163','','47897','','0000-00-00',NULL,'yes','yes','yes','','','','','','','part profile problem.\r\npart wrong loading.','Part Profile Problem.\r\nPart Wrong Loading.','Remaining Parts were Marked as Right & Left, Before Loading.','Another Location Hole done In fixture so part will never locate wrong.','CA/PA found ok.','','2015-10-18','','        Manjunath K.N.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8913,'35-166A','Saab AB','HOUSING PIN','459434A','423Z1124-6-01','','--A',3,'PA 1510 FORECAST','','46832','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Tool run out wall dig mark.','While running operation 3, dia 16r3 cutter run out observed. in between production running this problem occurred.\r\nOperator observed the deviation while stage inspection is carried out.','Immediately all the tool which is running for this operation is checked and found dia 16r3 holder cracked in threads.\r\nDue to this error tool run out observed and dig mark observed on part.\r\nDia 16 r3 cutter holder changed from collect holder to hydro grip.','All the collects holder checked and made mandatory that collect holder should not use for milling applications.\r\nOnly collects holders should use for drilling operation.\r\nThis will monitor by supervisors. ','CA/PA found ok.','','2015-10-19','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','01','no','Misc','Rangaswamy()','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8914,'35-241','Saab AB','HANDLE','455608C1','425Z0634-2','','--C',1,'PA 1510 FORECAST-2','','46851','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Position shift 0.3mm.','This deviation due to tool overhang. while doing operation-01 in rotary machine, dia 4.06mm hole operation is carried out, due to long reach of part, tool overhang is more and part wall thickness is also less.\r\nIf we start drilling part will bend and also part wall will vibrates.\r\nDue to this problems the above deviation coming.\r\n ','Immediately checked the process and discussed with CAD and decided to change the process.\r\nDia 4.06 hole operation will complete in operation-03.\r\nExtra operation added to overcome this deviation and same will in-corporate in MPS.\r\n','Dia 4.06 hole operation will complete in operation-03.\r\nExtra operation added to overcome this deviation and same will in-corporate in MPS.','CA/PA found ok.','','2015-10-19','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','00','no','Misc','Lohith(K)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8915,'18-605A','Magellan Aerospace Wrexham','BEAM STRUT FWD','424802 C','L575 52212 200','','A00',1,'RP134149 Amnd 1','','45318','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','4.00 +0.20-/.10 Thickness undersized by 3.76mm measured.','Due to part butting problem part was not butted properly so at one point of the part wall under size.  \r\n','bolt length will be used as per the required length & while loading the part external clamp has been\r\n added and before running the part butting will be cross checked by the feller gauge and then only\r\n part will be machined..  \r\n','bolt length will be used as per the required length & while loading the part external clamp has been\r\n added and before running the part butting will be cross checked and then only part will be machined..  \r\n','Next Parts found okay','','2015-10-19','Narayanappa(G)','Manjunath K.N.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','0','FI','no','DMG 360L','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8916,'18-209B','Magellan Aerospace(Chalfont) Limited','BODY','4842','D321 40204 202','','D, ECN NR29999ST1KM15, NR29999ST2KF65, WQN DFB09775',1,'P/078231','','46877','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Dig mark observed on face.','While 05 operation running,Operator re-loaded the finished parts again to machine.\r\nOperator not noticed the parts while loading the part to machine. \r\nthis deviation is due to negligence and in-discipline.\r\n \r\n ','All the parts arranged in machine rack with lean method and training conducted to operator to load and unload the parts to machine and inform to follow the instruction.\r\n','Penalty incorporated to operator due to negligence and also training conducted to build the discipline.\r\nSupervisor is to monitor the Lean method in all the machine to avoid such manual mistakes.  ','CA/PA found ok.','','2015-10-26','Lohith(K)','        Theerthappa K.N.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8917,'18-334A','Magellan Aerospace Bournemouth','LANDING UPPER OUTER','A547723','F574 50121 200','','C, ECN PG49998ST1TW17',3,'RP400947','','40587','','0000-00-00',NULL,'no','no','no','no','no','no','yes','yes','yes','A qty of 3 parts have been reported by GKN at Filton UK that the top coat of paint is peeling away from the primer coat. See pictures on the \"Photo\" tab','1) CIM have been releasing the parts  based on the supplier(API) CofC verification according to the requirement.\r\n2) CIM is not approved for the carrying the any tests OR checks for treated parts.','1) As per instruction from Magellan India, we have carried out the paint adhesion test  on all the parts was in stock including parts ready to dispatch for week 42 consignment.                                                2) As per our checks carried out they have passed the adhesion test with 3M tape.\r\n3) See attched excel file for the list of parts carried out the checks.\r\n','Refer 8D-307.','CA/PA found satisfactory.','C36800','2015-10-27','Avinash(R.J.)','Nandishkumar(D.K.)','MAG 8D 307','2015-10-15','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','16704','CUST END','no','Misc','Muniyappa(N)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8918,'42-008','RAFAEL','BOLT ENC','261935','BA1S5042A','','38-576104_Rev-E, TILDOCS#172373_Rev-13, 111.21 _Rev_6, 404-2-3_Rev-11,  ECN 57176 2014/08/05',4,'347592024-2','','47143','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Thread major dia mesaures minus side by 0.05mm.','','','','Parts accepted.','','2015-10-27','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','06','no','Misc','Dinakar(K)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8919,'18-210B','Magellan Aerospace(Chalfont) Limited','BODY','5757','D321 40204 204','','D, ECN NR29999ST1KM15, NR29999ST2KF65, WQN DFB09775',1,'P/078231','','47761','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Runing time 16mm boring tool screw broken bore + side  \r\n','Instead of maintain 0.3mm stock in ID it remove 0.4mm extra because of boring tool screw was loose during running time. ','Boring tool screw is replaced by new one and taking x and z offset for that tool and run the part.part found okay and continue the  production.  ','Instructed to all operator to dont use any slipped screws in the tools and it is compulsary to replace slipped screws before start the production.  \r\n','Next Parts found okay in Production','','2015-10-27','Dinakar(K)','        Shivappa M B','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8920,'18-605A','Magellan Aerospace Wrexham','BEAM STRUT FWD','6590801','L575 52212 200','','A00',1,'RP134149 Amnd 1','','45634','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Machine abuse observed on part surface.','Due to rubbing of tool Machine abuse has been found in Treatment house\r\n','Instructed to Production department to avoid rubbing of tool and polishing \r\n','Avoid polishing and try to finish the part  in machining stage itself.\r\n','Next parts and batches found okay\r\n','','2015-10-27','Avinash(R.J.)','Nandishkumar(D.K.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','20286','POST DN','yes','Misc','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8921,'18-445B','Magellan Aerospace Wrexham','PIPE END FITTING','M506580','L280 50067 210 PF','','A00',3,'RP140358','','48026','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','1.6mm thickness face out.','while clamping the part, in the butting face chips will butted so faceout occured in the running part and half of the part 1.6mm thickness meassures 0.5 to 0.6 undersized but not observed the operator.  \r\n','while clamping time clean the jaws by using air, and after clamping the part for every part rotate the chuck and cross check the butting fece visually and then run the part and after run the part check the 1.6mm thickness for every parts hundred percently.  \r\n','next every batch we are check the 1.6mm thickness hundred percent after clamping the part for every part rotate the chuck and cross check the butting fece visually and then run the part and after run the part check the 1.6mm thickness for every parts hundred percently.and avoiding the this type of errores.  \r\n','CA/PA found ok.','','2015-10-29','Dinakar(K)','Dinakar K,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','1','no','QT100S-3','Narasimhamurthy(K.G.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8922,'18-111A','Magellan Aerospace Bournemouth','BODY TURNBUCKLE INTMD','240136','D575 41544 200','S80 FHT','A',1,'RP408151','','47733','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Hole ablonged 1mm due to drill melt','During drilling of part which was inside the jig, the drill bit has got broken. the drill bit was taken out and the hole was drilled manually without jig.  The hole got ab longed. ','Decision was taken to change the drill bit after the planned production quantity such that the drill bit does not get damaged. \r\nThe operators have been made aware about that if the drill bit gets broken inside the Jig, second time the part to be loaded to Jig and then the part to be drilled.  Parts should never be drilled manually. ','To reduce the speed of the drilling machine and  the cutting angle to be checked after planned quantity such that drill bit does not gets damaged. \r\n\r\nProper proportion of coolant to be used during drilling.  ','CA/PA found ok.','','2015-10-29','Nagaraju(T)','Bhuvaneshwar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','07','no','Misc','Nagaraju(T)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8923,'35-244','Saab AB','RADIUS FILLER LARGE','G21013R05','423Z1456-2','','---',15,'May 2015','','42799','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','no','15 off 423Z1456-1 dispatched instead of 423Z1456-2.','Refer: 08924, Appendix1','Refer: 08924, Appendix1','Refer: 08924, Appendix1','Refer: 08924, Appendix1','C39825','2015-10-29','Avinash(R.J.)','Manjunath(G)','Mail received ','2015-10-29','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','Customer End','no','Misc','Avinash(R.J.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8924,'35-244','Saab AB','RADIUS FILLER LARGE','G21013R05','423Z1456-2','','---',15,'May 2015','','42799','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','no','15 off 423Z1456-1 dispatched instead of 423Z1456-2.','Refer: 08924, Appendix1','Refer: 08924, Appendix1','Refer: 08924, Appendix1','Refer: 08924, Appendix1','C39825','2015-10-29','Avinash(R.J.)','Manjunath(G)','Mail received ','2015-10-29','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','Customer End','no','Misc','Avinash(R.J.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8925,'18-099B','Magellan Aerospace Bournemouth','PLATE - TRAPPING','90415','D282 50062 200','','D',1,'RP408162','','46163','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Total lingh under size  drwing dimens 30.90 to 31.40 mesure 29.80mm.','Due to RM short length received so total length under size. ','Inform to operator before load the part check the RM size.\r\nWhen RM size deviation observed inform the concern supervisor or store department. ','Inform to operator before load the part check the RM size.\r\nWhen RM size deviation observed inform the concern supervisor or store department. ','CA/PA found satisfactory.','','2015-10-30','Lohith(K)','Theerthappa K.N.,Lohith K,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','HAASVF2SS-2','Narasimha Murthy(R)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8926,'35-138','Saab AB','FLCD_DS_SUPPORT_DEFLECT_S','7543150','423Z6189-3','BAC1534-62C','---',3,'PA 1510 FORECAST','','47611','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Material layer chipout.','Due to material behavior this was opened out.','1) We decided that this cannot be avoided but we minimized by improving the handling methods.','1) We decided that this cannot be avoided but we minimized by improving the handling methods.','CA/PA Found ok.','','2015-11-02','Lohith(K)','Theerthappa K.N.,Lohith K,Hari Prasad,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','fi','no','HAASVF2SS','Manjunath(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8927,'18-383A','Magellan Aerospace(Chalfont) Limited','SLEEVE BEARING ','207034','D575 40037 202','','A',1,'P/078238','','47608','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','ID oversized +0.02.','In the finishing setup id finishing tool running time part tighting washer will be slipped and part moved front and sound will came and insert will be brocken. so stop the machine and check the part.it will  -.1(minous) side so load the another new part and change the insert corner and -0.3 taken in wear offset and run the part but it will taken the extra cut and part will become +0.015 oversized. ','For the next part -0.02 taken in the wear offset and run the part. part checked found ok.','If running time insert will brocken, change the corner and taken the x and z offset then taken minous 0.3 in wear offset and give the proper correction and run the part and avoiding the this type of rejections.','Next Parts found okay in Production','','2015-11-02','Sandhesh D(S)','Vasu(SN)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','13','no','Misc','Sandhesh D(S)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8928,'18-003A','Magellan Aerospace Wrexham','BRACKET SUPPORT','5866801 7','D361 50111 200','ABM3 1029 T7651','A',1,'RP135242','','46699','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Dig Mark observed on part.','Due to put the center bolts not properly so part dig mark found. ','Put the center bolts properly and bolt tightness also checked then run the production. ','Put the center bolts properly and bolt tightness also checked then run the production. ','Next batch found okay','','2015-11-02','Avinash(R.J.)','Nandishkumar(D.K.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','20628','POST DN','no','Misc','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8929,'18-118B','Magellan Aerospace Bournemouth','BEARING HOUSING','244364','D275 40005 200','','C01',1,'RP408156','','47246','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','I.D OVALITY PROBLEMS SO PART REJECT.  \r\n','After running 50 to 60 parts insert tip will be worn out and running time chips not breaking properly so chips will rubbing inside the part and diameter will be oversized in the running part.\r\n \r\n','Remove the worn out insert and replace the new insert and newely offset taken and 0.2 (-) minous taken in the tool wear offset and run the part and then check the inner diameter and give the correction in wear offset and adjust the coolant correctly and run the part and checked found ok.  \r\n','while setting time loading the new insert before running and after every 100 nos change the roughing insert and run the part.and every 25ns onece observe thetoolnoise,coolant floaing and chips while running.  \r\n','Next Parts found okay in Production','','2015-11-03','Dinakar(K)','Shivanand(D.B.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','05','no','Misc','Shivanand(D.B.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8930,'35-183A','Saab AB','EDGE HOUSING','119572B6','423Z1121-6-02','','--A',1,'PA 1510 FORECAST','','46748','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','* DIA 9.525 and DIA 7.62 Part hole measure to DIA 9.69 and DIA   7.76 (Out of tolerance). ','* This deviation is due to program was running on part two times(twice) by negligence.\r\nIf re passes the tool twice in H7 holes,holes diameters will enlarge by 0.03 to 0.05mm.\r\noperator not checked the program list while running the series of programs. \r\n','* Informed to operator to check the completed programs in machine and run the programs listed as datasheet.\r\n\r\nInformed to supervisor to ensure the macro program calling in machines and also give training to operator to check the programs sequences.','*Informed to supervisor to ensure the macro program calling in machines and also give training to operator to check the programs sequences. ','CA/PA found ok.','','2015-11-04','Krishna(Chowdary.G.P.)','Umesh B,Gurukiran S M,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','MakinoF5','Manjunath(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8931,'18-473A','Magellan Aerospace Wrexham','RIB 2A AFT ','7243801','L575 58376 200 PF','','A00',1,'RP133571 Amnd 2','','45031','','0000-00-00',NULL,'yes','no','no','no','yes','yes','no','no','no','1 Pocket base thickness 1.60 +0.2/-0.1mm measured at 1.45 to 1.50 local area 50x20.','1)Due to part not properly butting to the M/C bed that leads to took cut more material.  2)This was not spotted during line inspection due to that spot not picked. Since lugs\r\n will be there. 3)Usually we are checking the thickness 2 to 3 places in the pocket but that area\r\n was not picked because the undersize area is locally around 50x30mm.   \r\n','1)We have checked the other parts and found ok.2)Touch probe will be introduced in the machine itself to check the web\r\n thickness before removing the part from machine.  \r\n','1)We have checked the other parts and found ok.2)Touch probe will be introduced in the machine itself to check the web\r\n thickness before removing the part from machine. ','CA/PA Found ok.','','2015-11-05','Narayanappa(G)','Sathish Y.R.,PAVAN KUMAR  S.K.,Manjunatha N.R.,Manjunath K.N.,Gajendra Singh C.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','Manufacture Only','','FI','no','HAAS','Avinash(R.J.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8932,'18-313A','Magellan Aerospace Wrexham','STUD ','453734','D278 50006 204 01','','D',4,'RP135260','','48125','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no',' OD under size by 0.014mm.','after running 5ns TNMG tool sim was brocken so insert will not seated properly so running time insert tip will be brocken and insert was rubbing the part and vibation started in the insert that time it will removing the extra material in outer diameter so outer diameter will be undersized.  \r\n','change the brocken sim,insert and screw and newely offset taken and 0.2 (+) plus taken in the tool wear offset and run the part and then check the outer diameter and give the correction in wear offset and run the part and checked found ok.  \r\n','before every part setting ,check the all tool sim, screws, pins and locks before tightening the tools to machine.then observe the noise every time while machining.  \r\n','Next Parts found okay in Production','','2015-11-05','Dinakar(K)','Shivanand D.B.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','FI','no','ST20','Narasimha Murthy(R)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8933,'18-473A','Magellan Aerospace Wrexham','RIB 2A AFT ','7243801','L575 58376 200 PF','','A00',1,'RP133571 Amnd 2','','45031','','0000-00-00',NULL,'yes','no','no','no','yes','yes','no','no','no','1 Pocket base thickness 1.60 +0.2/-0.1mm measured at 1.45 to 1.50 local area 50x20.','1)Due to part not properly butting to the M/C bed that leads to took cut more material.  2)This was not spotted during line inspection due to that spot not picked. Since lugs\r\n will be there. 3)Usually we are checking the thickness 2 to 3 places in the pocket but that area\r\n was not picked because the undersize area is locally around 50x30mm.   \r\n','1)We have checked the other parts and found ok.2)Touch probe will be introduced in the machine itself to check the web\r\n thickness before removing the part from machine.  \r\n','1)We have checked the other parts and found ok.2)Touch probe will be introduced in the machine itself to check the web\r\n thickness before removing the part from machine. ','CA/PA found satisfactory','','2015-11-05','Narayanappa(G)','Sathish Y.R.,PAVAN KUMAR  S.K.,Manjunatha N.R.,Manjunath K.N.,Gajendra Singh C.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','Manufacture Only','','FI','no','HAAS','Avinash(R.J.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8934,'18-117B','Magellan Aerospace Bournemouth','HOUSING-OUT BD BRG','K10860','D275 40004 200','','C01',1,'RP408156','','48189','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','OD Thread dammage.',' Operator part Handling problem.','sleeves put it on the thread.','Instruction given to operator.','Next Parts found okay in Production','','2015-11-05','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','03','no','Misc','Sandhesh D(S)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8935,'18-313A','Magellan Aerospace Wrexham','STUD ','453734','D278 50006 204 01','','D',1,'RP135260','','48126','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','OD undersize.','after running 5ns TNMG tool sim was brocken so insert will not seated properly so running time insert tip will be brocken and insert was rubbing the part and vibation started in the insert that time it will removing the extra material in outer diameter so outer diameter will be undersized. \r\n','change the brocken sim,insert and screw and newely offset taken and 0.2 (+) plus taken in the tool wear offset and run the part and then check the outer diameter and give the correction in wear offset and run the part and checked found ok.  ','before every part setting ,check the all tool sim, screws, pins and locks before tightening the tools to machine.then observe the noise every time while machining. ','Next Parts found okay in Production','','2015-11-06','Dinakar(K)','SHIVAKUMAR()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','03','no','Misc','SHIVAKUMAR()','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8936,'18-411A','Magellan Aerospace(Chalfont) Limited','PLUNGER','237004','D321 40205 200','','H01',1,'P078229','','47756','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','dia 9.965/9.975 od ovality 9.975 to 10.00. ','Due to problem in getting consistency in this part for\r\nthis dimension this will happen.','Planned for other grade of inserts and incorporate one\r\nmore tool between roughing and finishing.','After incorporate mentioned above that feed back was taken and\r\nsame was updated.','CA/PA found satisfactory. ','','2015-11-06','Dinakar(K)','Seetharamu(D)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Seetharamu(D)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8937,'18-277A','Magellan Aerospace(Chalfont) Limited','DOOR OUTER TYPE 27R','9171602','L572 53719 200','ABS5032A055','D00',3,'P/074116','','37228','','0000-00-00',NULL,'no','yes','no','yes','no','no','no','no','no','Rejected 3 off outer door doors for corrosion observed.','Minor mismatch buffed with zero emery. that looks as scratches and that they called as corrosion.','1) Later on the this parts accepted by the customer.\r\n2) The information passed to all concerned department.\r\n3) We are trying to avoaid the buffing wher ever possibale.\r\n4) If it is required then we can do with avoaid that avoaids to remove the rough area.','Same as above.','Next batch found satisfactory.','C40339','2015-11-06','Avinash(R.J.)','Nandishkumar(D.K.)','143679','2015-11-05','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','0','CUST END','no','Misc','Muniyappa(N)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8938,'18-111A','Magellan Aerospace Bournemouth','BODY TURNBUCKLE INTMD','240136','D575 41544 200','S80 FHT','A',2,'RP408151','','47734','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Thread NOGO answerd.  \r\n','After 25nos running threading insert will be wear out.for next part threading insert will be changedand 0.4 plus(+)taken in wear offset and run the part but thread gauge was not answered then 0.2 minous(-) taken to wear offset and run the part that time thread gauge was nogo answered.  \r\n','For next part x-offset taken and taking 0.3 mm up in toolwear offset and run the part gauge not answerd,in x-offset give 0.1mm down and run the part and gauge not answered then in x-offset down0.05mm and run the part and then gauge answered and next part run in same reading &the part found okay.','Instruction given to operator to take x-offset & z-offset whenever the inserts are changed and monitor supervisors.  \r\n','Next Parts found okay in Production','','2015-11-06','Dinakar(K)','Shivanand D.B.,SHIVAKUMAR ,Ravi R,Raghavendra Rao R,Punith G S,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','FI','no','ST20','Narasimha Murthy(R)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8939,'18-419A','Magellan Aerospace(Blackpool) Limited','BRACKET','221038','PI55-2120010-00','','NIL',1,'P/501903','','46344','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Dig Mark on Bottom Face.','While doing facing operation dia 10flat cutter broken due to part vibration.\r\nprocess was proved and production is running with same tool and parameters.\r\nBut this batch tool broken and caused deviation in part.','After finding the above problem, support block created to avoid part vibration when face machining is under process.\r\n\r\nNext part observed, Vibration is avoided and same process continued.\r\n\r\nall the other parts thickness is maintained consistently and vibration is avoided. ','To avoid such process related problem, support given to avoid vibration.\r\nNext batch part will run with same process and part vibration is avoided by giving support for part.\r\n\r\nPreventive action taken in existing batch only, and process proved.','CA/PA found ok.','','2015-11-07','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','FI','no','Misc','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8940,'18-419A','Magellan Aerospace(Blackpool) Limited','BRACKET','221829','PI55-2120010-00','','NIL',1,'P/501903','','46345','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Chamfer Operation Done Instead Of Debure.','while doing a chamfering for holes manually by using hand drilling machine, more load given and causes chamfer oversize.\r\n\r\nAs per drawing requirement all the sharp edges to be removed by 0.2R or Chamfer 0.5mm.\r\n\r\nBut chamfer measures 1mm.','Informed and training given to operator to understand the process and requirement.\r\n\r\nsupervisor demonstrate the operation and then after training supervisor witnessed the process done by operator.\r\n\r\nAll the other parts chamfer checked and found ok.','This operation to be completed in CNC machine. Chamfer tool introduced to avoid such manual errors.\r\n\r\n45 deg tool checked and dedicated kept in tool box and program added after drilling cycle.(there is no extra program added)\r\n\r\nNext batch this operation will carry in CNC machine and machine supervisor will monitor and prove the chamfer operation.','CA/PA found ok.','','2015-11-07','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','FI','no','Misc','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8941,'42-005A','RAFAEL','Clamp-3 ','G21267K06','BA1E2004B','','38-576104 Rev E, TILDOCS#172373 Rev 14, PR603-2-3 Rev 16, RAFDOCS#5224238 Rev 4, 111.21 Rev 7, 111.22 Rev 1, ECN63628 2015/01/13, ECN60821 2014/10/26',1,'347592024-5','','46339','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dia 6-32 thread NOGO answered.','While thread mill tool running time thread tight observed.So Thread rework time nogo answered.','Inform to operator thread tight observed time adjust the CRC value. \r\nWhile thread tight observed immediately inform the concern supervisor.\r\nEvery time part threading operation completed before remove the part check the thread gauge.','Inform to operator thread tight observed time adjust the CRC value. \r\nWhile thread tight observed immediately inform the concern supervisor.\r\nEvery time part threading operation completed before remove the part check the thread gauge.','CA/PA Found ok.','','2015-11-07','Lohith(K)','Yatheesh GL,Narasimhamurthy C,Lohith K,Kammar Nagaraj,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','7','no','VM2-3','Lohith(K)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8942,'35-237A','Saab AB','JACK BRACKET 2 ','927316','D576 50010 206','','D00',1,'1600115959','','48050','','0000-00-00',NULL,'yes','','yes','','yes','','','','','Bore over sized by 30 micron because small chips in boring bar holder taper...','A small chips in boring bar holder taper while tool changing from tool magazine so tool becomes run out and bore over size.','Inform to operator boring operation running before clean the tool pockets and spindle.\r\nEvery time boring operation running clean the ATC arm.','Inform to operator boring operation running before clean the tool pockets, ATC arm and spindle.\r\nReason for this deviation is not found. Informed to operators to analyzed the problem in further batches.','Next Parts found okay','','2015-11-08','Girish(Prasad P)','                Subramanya L Naik','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8943,'42-002','RAFAEL','PSA BASE','K10598','BA1E2001B','','38-576104_Rev-E, TILDOCS#172373_Rev-13, RE_804-1-5_Rev-11, 111.21_Rev-6, 23.36.59_Rev-F, ECN 57176 2014/08 /25; ECN 58483  2014/07/29',1,'347592024 Rel 9','','48400','','0000-00-00',NULL,'','','yes','','','','','','no','No Go gauge answered in 4-40 threaded holes to the full depth.\r\n\r\n\r\n\r\n\r\n\r\n\r\n\r\n\r\n\r\n\r\n\r\n','During production, chips clogged to 4-40 thread mill that leads to and removed the more material. So obviously No Go answered.','1)During line inspection operator himself found the problem and informed to concerned supervisors.\r\n2) Concerned supervisors analyzed and they instructed to clean the spindle and thereafter carryout the run out and continued the production parts.\r\n','The main problem is that the chips entered to tool magazine because wipers damaged in small area and same is replaced by new wipers. Same time instructed to maintenance team to check the tool magazine is free from chips and as well as wiper condition during their regular maintenance.','CA/PA found satifactory.','','2015-11-08','','        Basavaraja S. Jr.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8944,'18-113A','Magellan Aerospace Bournemouth','ADJUSTER','242096','D575 40496 200','S80 FHT','G',3,'RP408153','','47736','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','ID Thread nogo answered.','Machine tap clogged with chips hence this deviation occured ','Cleaned the tap and adjusted the coolant to flush the chips\r\noff the tap ','Instructed operator to clean the tap frequently and adjust the\r\ncoolant properly ','Next Parts found okay in Production','','2015-11-08','Dinakar(K)','Vishwanath Pavar,Theerthappa K.N.,Rajesh B D,KRISHNAMURTHY N,GUNDEGOWDA H.G.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','FI','no','DX 200-3','Narasimha Murthy(R)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8945,'18-120C','Magellan Aerospace Bournemouth','HOUSING OUT B D BRG 3','K10860','D275 56121 200','','E01,  ECN NG27011ST1KA83',1,'RP408158','','47367','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Running time part rotate so od -side.\r\n','Running time part rotating that time outer diameter is undersize.','OD finishing time using fixture in part locating & face locking in washer .the washer not locking in properly so part running time rotating .instruction given to operator before cycle start check the part tightening after running part.','OD finishing time using fixture in part locating & face locking in washer .the washer not locking in properly so part running time rotating .instruction given to operator before cycle start check the part tightening after running part. ','Next Parts found okay in Production','','2015-11-08','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','01','no','Misc','Anjinamurthy(H)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8946,'34-032C','Magellan Aerospace Winnipeg','BASE FITTING, F/D HINGE L','A12904','400-12780-1-905','','EM104302 Iss A, EM105092 Iss F, EM104765 Iss G, EM106399 Iss B, EM106400 Iss B, EM106401 Iss A, EM106404 Iss A, EM106522 Iss A, EM106602 Iss A',1,'B91379 Rev.026','','46392','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Part dig mark observed.','Due to part roughing operation running time dia 20 tipped cutter insert broken, so part base thick dig mark observed.\r\nStep matching time base thickness under side -0.3mm.\r\n','Inform to operator before run the part check the insert and screw every time.','Same as above','CA/PA found satisfactory.','','2015-11-09','Lohith(K)','Lohith(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','0','04','no','Misc','Lohith(K)','no',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8947,'18-110A','Magellan Aerospace Bournemouth','FORK END INTERMEDIATE','K11581','D575 40494 202','S80 FHT','J',1,'RP408153','','47838','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Part running time rotate causes dig mark on part flat surface. ','While running dia 50 face mill cutter( Facing Operation in A0 & A180)part rotates due to clamping not sufficient.\r\nClamping method is proved and effectvely running from 5years, after this deviation, \r\nDeviation analysis done and found clamping bush minor diameter measures plus by 0.05mm.This causes clamping regidity problem.','After this problem all the bushes which is using for clamping for all the parts checked with GO and NOGO guages and find 02 bushes problem.\r\nDeviation bushes scraped and new bushes manufactured and then continued production.','Informed to all the operators and also supervisors to check the clamping bushes with gauges before using, at every batch for all the parts.\r\n\r\n','Next production parts found satisfactory.','','2015-11-09','Anjinamurthy(H)','        Ravi R','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8948,'18-120C','Magellan Aerospace Bournemouth','HOUSING OUT B D BRG 3','K10860','D275 56121 200','','E01,  ECN NG27011ST1KA83',1,'RP408158','','47368','','0000-00-00',NULL,'yes','yes','yes','','','','','','','part rotated so OD -0.03mm.','While running OD finishing operation part rotates in chuck that causes OD undersize by 0.03mm.\r\n','OD finishing operation is carried by using fixture. Part clamped by butting the part face in fixture and clamped the part using washer on part ID.\r\nIf operator apply the more force to clamp the part,ovality is observed on OD.\r\nClamping force is varies person by person and also part to part due to manual tightening.\r\n\r\nDue to above mentioned points parts are getting rejected.Clamping method are not streamlined and process is also not consistent.','Tighting method change using by torquce wrinch.','Next batch found okay.','','2015-11-09','Dinakar(K)','        Bharath R','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8949,'35-237A','Saab AB','JACK BRACKET 2 ','927316','D576 50010 206','','D00',1,'1600121830','','48049','','0000-00-00',NULL,'yes','yes','yes','','','','','','','M/c running  time alarm- ATC TIME OUT SO TOOL INTERCHANGE  DIA 25RP8 AND DIA 22RP8 and rib thickness under size\r\n','M/c running  time alarm- ATC TIME OUT SO TOOL INTERCHANGE DIA 25RP8 AND DIA 22RP8 ','Immediately stop the machine and inform to machine maintence department, check the all parameters after continue the production.\r\nInform to operator every tool changing time give the optional stop or M00.\r\n','Reason for this deviation is not found. Informed to operators to analyzed the problem in further batches.','Next Parts found okay','','2015-11-11','Girish(Prasad P)','                Manukumar H M','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8950,'35-288','Saab AB','BEAM FITTING','443865C','424Z1140-2','','--B',1,'PA 1510 FORECAST-3','','45261','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','*Base thick minus. ','*Due to tool down when base finish operation is carried out.\r\nOperator not checked the tool offset properly.\r\n\r\n','*Operator knows the procedure of taking tool offsets and have much experience in machine operating.\r\nThis error due to negligence operator.\r\n\r\n*Tool offset corrected and continued production.\r\nSupervisor has given training and also he cross checked the tool offsets.','*This type of error due to negligence and supervisor as to monitor and give training to operators regularly and  monitor the same to avoid such manual errors.','CA/PA FOUND OK.','','2015-11-11','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Rangaswamy()','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8951,'35-277','Saab AB','BRACKET INTERMED','599462','423Z1123-4-02','','---',1,'PA 1510 FORECAST-3','','45250','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','*Tool dig mark in base.','* This error due to operator mistake while doing firstoff part.\r\nTool no. not entered correctly for all the programs.\r\nWrong tool coming and dig mark done while proving firstoff.','*After deviation found, operator knows the error and corrected, supervisor again all the tool corrected and firstoff proved and then continued production.','* This error due to negligence, operator should enter the tool no., tool overhang and description of tool to be entered in log book and same to be updated the tool no. in program.\r\noperator done error and informed to him to concentrate and follow the  procedure.\r\nSupervisor will monitor the operators and give training regularly to avoid such error in future.','CA/PA FOUND OK.','','2015-11-11','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Rangaswamy()','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8952,'46-002A','Mahindra Aerostructures Pvt.Ltd','BRACKET HYD ','6590801','L579 51142 200 PF','','C00',12,'3100507826','','48370','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','MPS wrong hole diameter enter,(dia 2.4 +0.1 for dia 4.0+0.1)','1) FAIR part checked against master process sheet and information in the process sheet is wrong and required diameter is Dia4.2mm instead of Dai4.0mm.\r\n2) Quality Inspector missed to check the FAIR part as per guide lines of AS9102.\r\n3) Quality inspector concentrated only on dimensionally as per process sheet.\r\n4) Process sheet not reviewed by the CAD/CAM and released without checking the changes of hole diameter.\r\n','1) Process sheet corrected as per the COS and updated the correct diameter.\r\n2) New batch launched to manufacture the correct part.\r\nQuality inspector instructed and trained about the FAIR part requirements.\r\n','1) CAD/CAM engineers they will review the process sheet by ticking each tab on hard copy.\r\n2) Quality alert displayed about the requirement of FAIR part.\r\n3) In quality alert each and every requirement of FAIR part noted and trained about those points.\r\n','Next Parts found okay','','2015-11-12','Ramesh(Poojary)','Ramesh(Poojary)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','03','no','Misc','Girish(Prasad P)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8953,'46-003A','Mahindra Aerostructures Pvt.Ltd','BRACKET HYD','6590801','L579 51142 201 PF','','C00',10,'3100507826','','48371','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','MPS wrong hole diameter enter,(dia 2.4 +0.1 for dia 4.0+0.1)','1) FAIR part checked against master process sheet and information in the process sheet is wrong and required diameter is Dia4.2mm instead of Dai4.0mm.\r\n2) Quality Inspector missed to check the FAIR part as per guide lines of AS9102.\r\n3) Quality inspector concentrated only on dimensionally as per process sheet.\r\n4) Process sheet not reviewed by the CAD/CAM and released without checking the changes of hole diameter.\r\n','1) Process sheet corrected as per the COS and updated the correct diameter.\r\n2) New batch launched to manufacture the correct part.\r\n3) Quality inspector instructed and trained about the FAIR part requirements.\r\n','1) CAD/CAM engineers they will review the process sheet by ticking each tab on hard copy.\r\n2) Quality alert displayed about the requirement of FAIR part.\r\n3) In quality alert each and every requirement of FAIR part noted and trained about those points.\r\n','Next Parts found okay','','2015-11-12','Ramesh(Poojary)','Ramesh(Poojary)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','03','no','Misc','Girish(Prasad P)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8954,'35-193','Saab AB','INTERCOSTAL CAM HOUSING','593823','423Z1190-1-01','','---',1,'PA 1510 FORECAST-2','','45210','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','FPI FAIL. ','During bench work, Deburring tool mark noticed on the part which was not passed the FPI process.','Informed to concerned department(bench work)and carried out the polishing and after that again send to treatment.','1) We are keeping the dedicated tryas for similar family parts to keep the parts and as well as in the transit.\r\n2) Instructed to keep the bench work area free from chipps.','Improvment noticed.','','2015-11-12','Avinash(R.J.)','Manjunath(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','20836','DN','yes','Misc','Manjunath(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8955,'35-157A','Saab AB','INTERCOSTAL_VENT','446972B','423Z1172-3-01','','---',1,'PA 1510 FORECAST','','47912','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','FPI FAIL.','Due to rubbing of tool or material behaviour NDT failure has been found in Treatment house','Instructed to Production  & fitting department to avoid rubbing of tool and polishing ','Avoid polishing and try to finish the part  in machining stage itself.','Next parts and batches found okay','','2015-11-12','Avinash(R.J.)','Manjunath(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','21332','DN','yes','Misc','Manjunath(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8956,'28-041','Magellan Aerospace New York  Inc.','LEVER ASSY-SECONDARY SPOI','158329','65-46358-16','','PL_E, DL_N/C, Sketch # 1',1,'130597','','46786','','0000-00-00',NULL,'yes','no','yes','no','yes','','','','','Tool dig mark observed on face.','While part running time \"Y\" axis shifted,so hole shift. \r\n','Immediately inform the machine supplier, and \"Y\" axis checked and production starts with monitoring of Y axis.\r\n','Inform to operator when running time Y axis not moving or axis shift immediately stop the machine, inform to concern supervisor.\r\n','CA/PA Found ok.','','2015-11-13','Lohith(K)','        Dhananjaya N','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8957,'46-003A','Mahindra Aerostructures Pvt.Ltd','BRACKET HYD','6590801','L579 51142 201 PF','','C00',2,'3100507826','','48371','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','MPS PROBLEM.(R/M SIZE PROBLEM)','1) FAIR part checked against master process sheet and information in the process sheet is wrong and required diameter is Dia4.2mm instead of Dai4.0mm.\r\n2) Quality Inspector missed to check the FAIR part as per guide lines of AS9102.\r\n3) Quality inspector concentrated only on dimensionally as per process sheet.\r\n4) Process sheet not reviewed by the CAD/CAM and released without checking the changes of hole diameter\r\n','1) Process sheet corrected as per the COS and updated the correct diameter.\r\n2) New batch launched to manufacture the correct part.\r\n3) Quality inspector instructed and trained about the FAIR part requirements.\r\n','1) CAD/CAM engineers they will review the process sheet by ticking each tab on hard copy.\r\n2) Quality alert displayed about the requirement of FAIR part.\r\n3) In quality alert each and every requirement of FAIR part noted and trained about those points.\r\n','Next part found ok.','','2015-11-13','Ramesh(Poojary)','Ramesh(Poojary)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','03','no','Misc','Girish(Prasad P)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8958,'18-412A','Magellan Aerospace(Chalfont) Limited','ROD END','247348','D321 53012 200','','F01',1,'P078230','','48031','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','OD Thread Flat.','Due to part running time insert broken.','New insert added and tool offset takened GO gauge adjested and\r\nrun the part. ','Instructed operator to every 50nos will be completed checked the insert.','Next Parts found okay in Production','','2015-11-14','Dinakar(K)','Seetharamu D,Ravi R,Dinakar K,Dhananjaya N,Anjinamurthy H,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','QT100S-4','Narasimha Murthy(R)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8959,'35-272','Saab AB','PIN','970533','425Z0601-3','','--A',1,'1600102192','','43211','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Strightness not achived,Required 0.075MM measures upto 0.10MM','This deviation find out at customer end and immediately we checked the Straightness of parts which is at our FG.\r\nWe find this deviation in one part.','After finding the problem at customer end, we introduced the straightness and roundness checking method and same was followed for all the batches.','Process changed to achieve the straightness and roundness consistently in production by splitting the roughing and finishing operation(OD.\r\nOnce all the operation is then final OD turning will complete.\r\nProcess was proved and same is followed and MPS amended as per new process.','CA/PA Found okay...','','2015-11-16','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','Misc','Nagaraj(G. Nadiger)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8960,'18-564A','Magellan Aerospace Wrexham','FITTING SPIKE FWD','9547801','L575 51782 200','','A',1,'RM132919 Amnd 1','','46021','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','5MM Thickness Under Size By 0.15.','This problem is not find out production running time, complete production after identified so next batch running time salve this p[problem. ','Next batch before identified problem salve this problem.','Next batch before identified problem salve this problem.','Next batch seeing after that closed.','','2015-11-16','Rangaswamy()','Rangaswamy ,Manohara M,Basavaraja S. Jr.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','VMC 70L','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8961,'35-288','Saab AB','BEAM FITTING','443866C','424Z1140-2','','--B',1,'PA 1510 FORECAST-3','','45259','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dia 7.00 (+0.035) hole \"NOGO\" enter.','This deviation observed while running production batch,02 holes measures 0.035mm plus side.\r\nReasons for the deviation is not identified. all the other parts in this batch checked 100% and all the holes are find ok. ','All the parts checked 100% and moved to final inspection.\r\nReasons for the deviations suspects Chips clocked in hole while running hole mill.','Informed to operator to check the chips clocking in holes while doing reaming holes.\r\nSufficient coolent to be adjusted to drill and hole mill to avoid chips clocking.\r\nThis PA will check and monitor for all the hole making parts.','CA/PA FOUND OK.','','2015-11-16','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Rangaswamy()','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8962,'18-431A','Magellan Aerospace(Chalfont) Limited','SPRING RETAINER ','A0563X','D321 40203 220','','L',1,'P078230','','48266','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','ID Ovality.','While running insert oversize and operator not checked\r\npart regularly.','Instructed to operator for checking ID for every part and\r\nchecking wearout regularly.','Instructed to operator for checking ID for every part and\r\nchecking wearout regularly.','Next Parts found okay in Production','','2015-11-17','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','3','no','Misc','Ravi(M)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8963,'18-411A','Magellan Aerospace(Chalfont) Limited','PLUNGER','A0860N','D321 40205 200','','H01',1,'P078230','','47818','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Thread NO GO answered.','While threading operation insert brokered so thread NO GO\r\nanswered.','Next insert changed and tool offset taken and run the part. part thread found OK.','Inform to operator every 80 nos will be completed the production then checked the insert.','CA/PA found satisfactory. ','','2015-11-17','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','','07','yes','Misc','Diwakar(S)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8964,'18-341A','Magellan Aerospace Bournemouth','LANDING TOP PANNEL','A641495','F574 50966 200 01','','E, ECN PG49998ST1TV38',1,'RP408276','','46753','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Linear indications observed on part surface.','Scratch mark moticed on the part which leads to fail the NDT','Informed to concerned department to take care during transit and packing.','Dedicated trays arranged for each family parts to avoaid the scratch and other FOD. ','Next batch found satisfactory.','','2015-11-18','Avinash(R.J.)','Nandishkumar(D.K.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','20559','POST DN','no','Misc','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8965,'18-109A','Magellan Aerospace Bournemouth','NUT','249646','D575 40498 200','S80 FHT','D01',1,'RP408154','','47109','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','NDT Failed.','Due to rubbing of tool or material behavior NDT failure has been found in Treatment house\r\n','Instructed to Production  & fitting department to avoid rubbing of tool and polishing \r\n','Avoid polishing and try to finish the part  in machining stage itself.\r\n','Next parts and batches found okay\r\n','','2015-11-18','Avinash(R.J.)','Nandishkumar(D.K.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','20974','POST DN','no','Misc','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8966,'18-414B','Magellan Aerospace Bournemouth','ACTUATOR HOUSING','2195','D278 50163 200','','D',1,'RP408293','','46660','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','NDT failure.','Due to rubbing of tool linear indications has been found in Treatment house. ','Instructed to Production department to avoid rubbing of tool and polishing ','Avoid polishing and try to finish the part  in machining stage itself.','Next parts and batches found okay','','2015-11-18','Avinash(R.J.)','Nandishkumar(D.K.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','20715','POST DN','no','Misc','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8967,'18-412A','Magellan Aerospace(Chalfont) Limited','ROD END','254116','D321 53012 200','','F01',3,'P078230','','48029','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Thread gauge NO GO answering.\r\n','After threading operation in turning, In operation 07 Key way will complete, After key way thread gauge is not answering due to burr is folding in threads. Before Key way operation all the parts is checking with gauge and found ok. Due to problem facing in gauge entry after the key way, we planned to rework with OD thread Die and this operation is manually done.rejected due to NOGO answering.','This operation is done by manually and 01 got deviation due to Die entry problem. Due to manually operation this will stabilize by experience and we need to conduct practical training.','Preventive action is as same as Corrective Action.','Next batch parts okay in production.','','2015-11-18','Dinakar(K)','Narasimhamurthy(K.G.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','07','no','Misc','Narasimhamurthy(K.G.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8968,'18-572A','Magellan Aerospace Wrexham','PLATE TRAILING EDGE','D245732','L575 51795 200','','A',1,'RM132920 Amnd 1','','45388','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Width 10.50mm Measured 10.07mm (Under Size By 0.13mm).','part width under size by part angle face not butting properly ( first batch in the production)  \r\n','added 2 nos external clamps for clamping, cross checking the part width befor finishing program.  \r\n','added 2 nos external clamps for clamping, cross checking the part width befor finishing program. we will be add part location pins on the fixture at next batch.  \r\n','Next Parts found okay','','2015-11-18','Narayanappa(G)','Sathish Y.R.,Karthineyan V.S.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','FI','no','Unipro5000','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8969,'18-085A','Magellan Aerospace Wrexham','BRACKET SUPPORT','17134955-B','D579 52009 200','L168','A',1,'RP135247','','47960','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Thickness under size 0.22mm.','Due to butting face not cleaned properly. and chips clocked in between part and butting face.So part thickness under size by 0.22mm. ','After finding this error, causes for this deviation analyzed and informed and discussed the process while loading the part in to machine.\r\nClearly clean the butting face by air/waste and after ensuring the above only part should be loaded and its need only concentration and dedication.\r\nInformed to operator to follow the above procedure for all the parts.\r\n ','Operators has to follow the common procedures and adhere to procedure for all the parts.\r\nInstructed to operator to check the butting face for every part before loading the part. and cleaned by air/waste then load the part and ensure by the butting by feeler gauge.','CA/PA found ok.','','2015-11-18','Krishna(Chowdary.G.P.)','Ravindra(Singh R)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','Misc','Narasimha Murthy(R)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8970,'18-106A','Magellan Aerospace Bournemouth','EYE END INBOARD','A1218X','D575 41542 200','S98 FHT','D',1,'RP408155','','47741','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','thread nogo answered.','','','','Parts accepted.','','2015-11-19','Dinakar(K)','Shivanand(D.B.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','Manufacture Only','','09','no','Misc','Sandhesh D(S)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8971,'18-461A','Magellan Aerospace Wrexham','SPAR FWD','6469801','L575 51827 200 PF','','A00',1,'RP133603 Amnd 4','','47044','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Did 6mm tooling hole Ablong, measured at (6.0+0.15)6.25/6.30.','while drilling operation time chips blocked so dia6.0 hole over size \r\n\r\n\r\n  \r\n  \r\n','before finishing the hole dia pilot hole will be done & coolant will be adjusted for that hole by that hole position will measure properly.. ','before finishing the hole dia pilot hole will be done & coolant will be adjusted for that hole by that hole position will measure properly and instruction given for the operator to check the hole before finishing the hole in roughing condition.. \r\n  \r\n  \r\n  \r\n','Next Parts found okay','','2015-11-20','Narayanappa(G)','Karthineyan V.S.,Gajendra Singh C.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','FI','no','Unipro5000','Avinash(R.J.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8972,'18-106A','Magellan Aerospace Bournemouth','EYE END INBOARD','620469','D575 41542 200','S98 FHT','D',1,'RP408155','','47740','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','OD Thread Taper problem so NOGO answerd.','During production batch running of 100nos, this deviation\r\noccured.','Instructed operator to check the dimensions prior to giving\r\nfinal cut during threading operation.','Instructed operator to check the dimensions prior to giving\r\nfinal cut during threading operation.','Next Parts found okay in Production','','2015-11-20','Dinakar(K)','Shivanand(D.B.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','09','no','Misc','Sandhesh D(S)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8973,'18-106A','Magellan Aerospace Bournemouth','EYE END INBOARD','620469','D575 41542 200','S98 FHT','D',1,'RP408155','','47740','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Thread end not open.','','','','Rework done part found okay.','','2015-11-20','Dinakar(K)','Shivanand(D.B.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Manufacture Only','','09','yes','Misc','Ravi(M)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8974,'18-616A','Magellan Aerospace Wrexham','BOLT LIFTING HOIST','5253949','L575 55223 200','','A00',8,'RM132921 Amnd 1','','44882','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Parts missing(Trail purpose for production).','Trail purpose','Trail purpose','Trail purpose','Trail purpose','','2015-11-21','Avinash(R.J.)','Shivanand D.B.,Raghavendra Rao R,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','FI','no','ST20Y1','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8975,'18-113A','Magellan Aerospace Bournemouth','ADJUSTER','242096','D575 40496 200','S80 FHT','G',1,'RP408153','','48521','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Id thread no go answered..','Single screw using for tightening the tool so thread GO not answered so 2 to 3 times thread re-pass running then GO gauge will be answered. so for the next part using the another screw and tight the tool and run the part that time thread will be NOGO answered.           ','for the next part taken the re-offset and taken -0.2 in wear offset and give the proper correction and run the part part checked found ok.','For the setting time check the all tools and screws and tightening the every tools properly and avoiding this type of errors.','Next Parts found okay in Production','','2015-11-21','Dinakar(K)','        Seetharamu D','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8976,'18-110A','Magellan Aerospace Bournemouth','FORK END INTERMEDIATE','K11581','D575 40494 202','S80 FHT','J',3,'RP408153','','47838','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Thread effective dia under size(thread taper).','','','','Next Parts found okay in Production','','2015-11-22','Dinakar(K)','SHIVAKUMAR()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','03','no','Misc','Dinakar(K)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8977,'28-041','Magellan Aerospace New York  Inc.','LEVER ASSY-SECONDARY SPOI','158329','65-46358-16','','PL_E, DL_N/C, Sketch # 1',1,'130597','','46786','','0000-00-00',NULL,'yes','yes','yes','','','','','','no','Dummy','Dummy ','Dummy','Dummy','Dummy','','2015-11-23','Lohith(K)','        Dhananjaya N','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8978,'28-041','Magellan Aerospace New York  Inc.','LEVER ASSY-SECONDARY SPOI','158329','65-46358-16','','PL_E, DL_N/C, Sketch # 1',1,'130597','','46786','','0000-00-00',NULL,'yes','no','yes','no','yes','no','no','no','no','Hole shifted 2.5mm','While part running time \"Y\" axis shifted,so hole shift.This error happened chips clocked on Y axis limit-switch.   \r\n','Immediately inform the machine supplier, and \"Y\" axis checked and production starts with monitoring of Y axis.\r\n','Inform to operator when running time Y axis not moving or axis shift immediately stop the machine, inform to concern supervisor.\r\n','CA/PA Found ok.','','2015-11-23','Lohith(K)','Yatheesh GL,Dhananjaya N,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','7','no','VM2-2','Lohith(K)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8979,'35-082','Saab AB','HOUSING-SIDE ROLLER','5027901 1','F579 53065 202','ABM3-1029 T7651','B, PG52307ST4KA80',2,'1600121617','','47040','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','*8.5 BASE THICKNESS MEASURED UPTO 8.15 (1NO)                                                 \r\n*BORE DIA OVER SIZE UP TO +10/+30 MICRON. ','1.This deviation is due to part not butted properly in fixture.\r\nWhile loading the part in moveable vice type fixture operator not observed the part butting.\r\n2.Due to chips clocking in reamer H7 hole measures 10 to 30 microns plus side.\r\n','1.Checked the design and clamping method in existing fixtures(02nos),part butting in fixture is ok if clamping bolt should not feel jerk due to threads wear out.\r\n2.Chips clocking will avoid by providing sufficient coolent to the reamer.\r\n','1 & 2) Both the above cases are studied and no problems with process, we need to train the operation to check and follow the process. ','CA/PA FOUND OK AND NEXT BATCH CHECKED FOUND OK.','','2015-11-23','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','Misc','Manjunath(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8980,'18-477A','Magellan Aerospace Wrexham','RIB 2 L/H ','9550801','L575 41322 200 PF','','A00',2,'RM133577 Amnd 3','','48461','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','medal wall rib hole position under size actual value 30.07 but measure value 29.60. ','drilling operation in fitting department used new fixture bush was problem so hole position is under size.','stop the production order to the new hardened bush in two types free size bush & finish size bush before finishing operation part hole position checked after the finish drilling operation ','inform to fitters you don\"t use without hardened bush in any drilling operation ','ca/pa found ok','','2015-11-24','Ravikumar(L)','Ravikumar(L)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','Manufacture Only','','7','no','Misc','Narayanappa(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8981,'35-179','Saab AB','SUPPORT-SEAL-RETAINER','593780','423Z1833-4-02','','---',1,'PA 1510 FORECAST','','48403','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Tool dig mark.','Operator run 1st part, dia 10 ballnose program  running time observe sound or vibration in machine, so stop the machine reset program select handle mode for \"z\" axis move home position, but select handle mode, by miss hand touch in hand wheel so \"Z\" axis in down so tool dig in part face.      ','stop the machine, remove the part, load next part run progrem as per process sheet.','This rejection is due to manual error, Explained and training to operator \"z\" axis moving time uing machine setup position return and one touch start buttons  . ','CA/PA FOUND OK.','','2015-11-24','Rangaswamy()','Rangaswamy()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Rangaswamy()','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8982,'28-004A','Magellan Aerospace New York  Inc.','PIN','G17210','161A2332-1','15-5PH Steel Bar per','NA',1,'130564','','46286','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Outer diameter 47.30 undersized 0.015 to 0.02.','In OD roughing setup running time insert will be breakage and part will OD oversize and that part not checking the operator and part not maintain in proper stock for finishing tool. So in the finishing setup that part loading time finishing tool get the more stock and coolant flows not correctly and chips will be over lapped in the outer diameter and part will be -0.02mm under sized.\r\n \r\n','After roughing check the diameter and maintain the proper stock for the finishing tool and run the part and adjust the coolant in insert edge coolant will be avioded the chips over lapping and every 15 to 20 ns change the finished insert tip and run the part so this problem not repeated again .  \r\n','After roughing check the diameter and maintain the proper stock for the finishing tool and run the part and adjust the coolant in insert edge coolant will be avioded the chips over lapping and every 15 to 20 ns change the finished insert tip and run the part so this problem not repeated again .  \r\n','CA/PA found satisfactory.','','2015-11-25','Dinakar(K)','Dinakar K,Ashith B,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','13','no','DX 200-2 ','Sandhesh D(S)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8983,'18-009A','Magellan Aerospace Wrexham','Plate Cover','497610','D572 52519 200','L97 T351','A',1,'RP135247','','48771','','0000-00-00',NULL,'yes','yes','yes','','','','','','','part reversed when M00 came but reset the program and run from starting program so drilling opn done in both side so part reject.\r\n','In this operation after turning and drilling operation M00 will come and reverse the part for facing and chamfer operation part reversed when M00 came but reset the program and run the program again turning and drilling instead of facing and chamfer.so both side drilling operation done so part reject.','For next part, part reversed and not reset the program and run the facing and chamfer program(next opn).','Instruction given to operator to follow the messages given in the program and run the program as per essage and where M00 came check the part and program before run the part. ','Next batch okay in production.','','2015-11-26','Dinakar(K)','        Shivanand D.B.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8984,'35-182B','Saab AB','EDGE HOUSING','626088','423Z1121-5-02','','--B',1,'PA 1510 FORECAST','','48578','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','\"KC\" Profile point out of tolerance 0.25mm','This is process problem so \"KC\" Profile point out of tolerance. ','Next batch change process.','process change.','Revision changed new process found okay with production\r\n','','2015-11-26','Rangaswamy()','Rangaswamy()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','','FI','yes','Misc','Nagaraj(G. Nadiger)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8985,'18-498A','Magellan Aerospace Wrexham','FITTING','6482801','L575 54954 200','','A00',1,'RM132920 Amnd 1','','48156','','0000-00-00',NULL,'yes','yes','yes','','','','','','','work offset wrong ','Operator \"Y\" offset wrong taken, because X0 toomb center, Y0 10h7 hole in fixture but operator taken M12 bolting hole. so shift offset part rejected. ','After 1st part operator check dimensions but not matching dimensions so identified reject, then once again take correct   offset then run production found ok.','This rejection is due to manual error, Explained to operator regarding the process. ','Next Parts found okay','','2015-11-26','','        Rangaswamy ','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8986,'18-376B','Magellan Aerospace Bournemouth','GAMMA FITTINGS ','5570','NSA840020-150','','L',2,'RP408525','','46106','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Total length undersize.\r\n','In first set up face was unclear thats why 0.2mm given in work offset and run the part part found ok. and in second set up 0.2mm not taken plus side in work offset so thickness 0.2mm under size.','Jaws bored neatly where the partface was butted to jaws and clamped on od and taking offset run the part ,part found ok and contionue the production.','Instruction given to operator to where the thickness is maintained for have to butt that face in the jaws not in the starting face. ','Next batch okay in production.','','2015-11-27','Dinakar(K)','Sathish(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','05','no','Misc','Sandhesh D(S)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8987,'35-077','Saab AB','BUSH','1112509740','D575 40147 200','DTD-197','B ECN NG29999ST2TT59',1,'PA 1217-Bushes (A320','','44778','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Short supply from treatment house(part missing)','This part was missed in treatment house.','Informed to treatment house(GET)and they also missed.','Informed treatment house about short supply of parts, then we will raise the credit note.','CA/PA found satisfactory.','','2015-11-30','Dayananda(K.G.)','Dayananda(K.G.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','19022','Post DN','no','Misc','Nagaraj(G. Nadiger)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8988,'35-138','Saab AB','FLCD_DS_SUPPORT_DEFLECT_S','7543150','423Z6189-3','BAC1534-62C','---',3,'PA 1510 FORECAST','','44968','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','Material layer chip out. \r\n','The Following Route causes analyzed for material chip off after outer profile machining. \r\n1. Due to RM deviations material will chip off. \r\n2. While running production, the finishing tool wear out causes light chip off in material. 3. Steel Butting sheet for part is not Flat.','The following Corrective Action/Preventive Action taken to avoid Materiel chip off. \r\n1. Raw Material will inspect visually before issuing to production. If found any problem visually RM will be quarantined. \r\n2. Dia 8 end mill life calculated, informed to operators to monitor the tool life.and change the tool after as mentioned. \r\n3. Steel butting plates flatness inspection done\r\nbefore production starts.\r\n','The following Corrective Action/Preventive Action taken to avoid Materiel chip off. \r\n1. Raw Material will inspect visually before issuing to production. If found any problem visually RM will be quarantined. \r\n2. Dia 8 end mill life calculated, informed to operators to monitor the tool life.and change the tool after as mentioned. \r\n3. Steel butting plates flatness inspection done before production starts. Taking all the above PA, rejections happened in material chip off. Out of 100nos production 5 to 6nos getting rejection. Due to customer requirement parts are manufactures with considering rejections.','CA/PA Found Ok. ','','2015-12-01','Lohith(K)','Dhananjaya N,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','1','no','VM2-1','Lohith(K)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8989,'35-182A','Saab AB','EDGE HOUSING','453560B','423Z1121-5-02','','--A',1,'PA 1510 FORECAST','','47333','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','0.375Inch Hole Position measures out of tolerance. Required 0.0039Inch measured 0.0127Inch.','After short peening part is expanding so hole position out of tolerance.  ','1)Reduce the intensity for the drawing requirement and continue the process.\r\n2)Maintain the hole position in minimum. ','1)Reduce the intensity for the drawing requirement and continue the process.\r\n2)Maintain the hole position in minimum. ','Next part check found ok. ','','2015-12-02','Avinash(R.J.)','Avinash(R.J.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','21576','Post DN','no','Misc','Nagaraj(G. Nadiger)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8990,'35-138','Saab AB','FLCD_DS_SUPPORT_DEFLECT_S','R8H8','423Z6189-3','BAC1534-62C','---',18,'PA 1510 FORECAST','','48821','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','* Material layer chippout.','The Following Route causes analyzed for material chip off after outer profile machining. \r\n1. Due to RM deviations material will chip off. \r\n2. While running production, the finishing tool wear out\r\ncauses light chip off in material. 3. Steel Butting sheet for part is not Flat.','The following Corrective Action/Preventive Action taken to avoid Materiel chip off. \r\n1. Raw Material will inspect visually before issuing to production. If found any problem visually RM will be quarantined. \r\n2. Dia 8 end mill life calculated, informed to operators to monitor the tool life.and change the tool after as mentioned. \r\n3. Steel butting plates flatness inspection done before production starts.','The following Corrective Action/Preventive Action taken to avoid Materiel chip off. \r\n1. Raw Material will inspect visually before issuing to production. If found any problem visually RM will be quarantined. \r\n2. Dia 8 end mill life calculated, informed to operators to monitor the tool life.and change the tool after as mentioned. \r\n3. Steel butting plates flatness inspection done before\r\nproduction starts. Taking all the above PA, rejections happened in material chip off. Out of 100nos production 5 to 6nos getting rejection. Due to customer requirement parts are manufactures with considering rejections.','CA/PA Found Ok. ','','2015-12-02','Lohith(K)','Lohith(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','Misc','Nagaraj(G. Nadiger)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8991,'18-099B','Magellan Aerospace Bournemouth','PLATE - TRAPPING','90415','D282 50062 200','','D',3,'RP408162','','46163','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Parts lost at treatment house.','Parts lost at treatment house.','Parts lost at treatment house.','Parts lost at treatment house.','Parts lost at treatment house.','','2015-12-02','Avinash(R.J.)','Nandishkumar(D.K.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','21315','POST DN','no','Misc','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8992,'18-114A','Magellan Aerospace Bournemouth','NUT','A0860N','D575 40499 200','S80 FHT','D01',1,'RP408154','','47113','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','NDT Fail','Due to rubbing of tool or material behaviour NDT failure has been found in Treatment house\r\n','Instructed to Production  & fitting department to avoid rubbing of tool and polishing \r\n','Avoid polishing and try to finish the part  in machining stage itself.\r\n','Next parts and batches found okay\r\n','','2015-12-02','Avinash(R.J.)','Nandishkumar(D.K.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','21478','POST DN','no','Misc','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8993,'35-017','Saab AB','9901503-075','666802A4','D576 50011 200','L167','A',21,'PA 1217 2015-2016','','48577','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Bend observed on part.','This deviation due bend observed in RM and this will reflect on part cutout. \r\nDue to RM bend vacuum clamping is not sufficient, this will causes base thickness to be maintained at maximum side.\r\nWhen base thickness(cutout base thickness) at maximum/out of tolerance side, this will causes problem in cutting the parts in fitting.(Parts splitting from 18 nos to individual parts)','This batch all the parts machined base thickness at maximum side only and information given to fitter to take care and handle smoothly for this batch while cutting operation is carried out.\r\nAll the parts bend checked in placing the parts at surface table with feeler gauge.\r\n\r\n','Next batch parts thickness will maintain at minimum side(Provided RM bend is less) and if not same procedure as mentioned in CA will done in next batches also.\r\n','CA/PA found ok.','','2015-12-03','Nagaraja (G)','Paramaeshappa ,Girish MS,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','','FI','yes','Slim-1','Nagaraj(G. Nadiger)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8994,'34-028C','Magellan Aerospace Winnipeg','BUSHING AFT MOUNT','E140728','400-12628-1-905','','EM104302 Iss A, EM104765 Iss G, EM105092 Iss F, EM106399 Iss B, EM106400 Iss B, EM106401 Iss A, EM106404 Iss A, EM106522 Iss A, EM106602 Iss A',1,'B91379 Rev.026','','45380','','0000-00-00',NULL,'yes','yes','yes','','','','','','no','Part running time part rotated so dig mark.','While running slot finishing operation, part rotates and dig mark observed.\r\nDue to clamping threads wear out, part not clamped rigidly and causes to rotate the part and dig mark observed in part.','17 nos production completed in this batch and find all the parts are found ok.\r\nPlanned to change the process due to thread dimensions are not achieving as per drawing after slot operation is completes.\r\n(due to force applying to part while slotting operation, this will cause thread gauge Go not answering).\r\nTherefore planed to complete the threads and slot in Turn Mill center in one setup.','Planned to change the process to complete the threads and slot in Turn Mill center in one setup.','Next batch found satisfactory.','','2015-12-03','Anjinamurthy(H)','        Diwakar R.B.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8995,'35-232A','Saab AB','HINGE BRACKET 4 ','3861901','D576 50007 209','','E00',11,'1600121830','','47601','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','NDT FAIL ','Due to rubbing of tool or material behaviour NDT failure has been found in Treatment house ','Instructed to Production & fitting department to avoid rubbing of tool and polishing ','Avoid polishing and try to finish the part in machining stage itself ','CA/PA found satisfactory. ','','2015-12-04','Avinash(R.J.)','Avinash(R.J.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','21069','Post DN','no','Misc','Nagaraj(G. Nadiger)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8996,'18-383A','Magellan Aerospace(Chalfont) Limited','SLEEVE BEARING ','K11581','D575 40037 202','','A',1,'P/078238','','48769','','0000-00-00',NULL,'yes','yes','yes','','','','','','','id oversize (0.02mm).','In the finishing setup id finishing tool running time part\r\ntightening washer will be slipped so part moved front and sound will came and insert will be broken. so stop the\r\nmachine and check the part.it will  -.1(minus) side so load the another new part and change the insert corner and -0.3 taken in wear offset and run the part but it will taken the extra cut and part will become +0.02 over sized. ','For the next part -0.025 taken in the wear offset and run the part. part checked found OK.','If running time insert will broken, change the corner and\r\ntaken the x and z offset then taken minus 0.3 in wear offset and give the proper correction and run the part and avoiding the this type of rejections.','Next Parts found okay in Production','','2015-12-04','Ravi(M)','        Manjunatha N','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8997,'28-016','Magellan Aerospace New York  Inc.','STOP FITTING','G22127K02','161A6119-1','15-5PH Per AMS 5659 ','N/C',2,'124982-3170_R0_C0','','47854','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Thickness .3950/.4050 inch measures .3925 inch in 02 nos.','Hole chamfer Dia is in maximum side to maintain this to minimum side we are not observed another one dimension which was close tolerance Thickness .3950/.4050 inch measures .3925 inch in 02 nos two parts get rejected.','operator get trained to hole chamfering & How to read the MPS in CIM soft while doing the fitting work and how to check the part before taking to fitting work.','Next batch produced and no part rejected for this CRN ','Next batch found ok.','','2015-12-06','Avinash(R.J.)','Sudhagar(V)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','0','ON SITE','no','Misc','Sudhagar(V)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8998,'28-039','Magellan Aerospace New York  Inc.','SPACER WASHER, BUSHING - ','L25018','161A2303-1','','PL _A, PSDL_ N/C',1,'130679-3183','','47944','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','total length undersize (-0.04mm)','Parting tool screw was not tightening properly so running time insert was slipped so total lenght -0.04 undersized.','changing the parting tool,screw and insert and tightening the screw properly and taking the z offset and running the part.   ','While setting time, check all the tools,screws,inserts and sim properly and then run the part.','Next Parts found okay in Production','','2015-12-06','Dinakar(K)','Rajesh B(D)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','7','no','Misc','Dinakar(K)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8999,'35-057','Saab AB','7605197-201','8-37-03651-1','L574 55197 201','ABS 5125 A 016 N','C, ECN - PG69999001',2,'PA 1217 FORECAST-2','','49083','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Profile shifted 2mm.','This rejection is due to operator error, while setting operation-02 operator not dialed the fixture and then loaded the parts and program runned.\r\nThis error is also due to miss communication between shift change operator.\r\nand shift operator is not cross checked the setting and also reliving operator is not informed the setting details.\r\n','Next parts supervisor checked the fixture straightness and then next part machining started.\r\n\r\nEmp no.400227 and 400144  training conducted for the procedure while changing the shift and methods to transfer the work while changing the shift.\r\n','Training conducted for the machine operators as per the above corrective action.\r\nSupervisor to monitor the shift record on daily basis for 01 month.','CA/PA Found Ok. ','','2015-12-07','Lohith(K)','Vishwanath(Pavar)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','3','no','Misc','Lohith(K)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9000,'28-003A','Magellan Aerospace New York  Inc.','PIN-ATTACHMENT WALKING BE','G22083K01','161A7305-1','','PL-Rev-NC, DL Rev-B',1,'126999_R0_C1','','47566','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1)Thread Effective Diameter under size by 0.14 mm.','1) Wrong instrument used and which they supposed to use M4 anvil instead of M3 anvil for thread pitch micrometer to check the effective diameter.\r\n2) Operator not checked the measuring instrument before usage.\r\n','1) During 1st off this was noticed and then changed the instrument and other parts manufacured and found ok.','1) Operator instructed and trained which they collect all the measuring instrument and cutting tools before start the process.','Next Parts found okay in Production','','2015-12-08','Narasimhamurthy(K.G.)','Narasimhamurthy(K.G.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','0','07','no','Misc','Sudhagar(V)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9001,'35-194','Saab AB','SUPPORT SEAL RETAINER','558386','423Z1834-1-01','','---',1,'PA 1510 FORECAST-3','','47851','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dig mark on part due to dia4R0.5mm cutter broken.','While doing first batch production, grove finish is done in Dia 4R0.5 end mill.\r\nFor this cutter more stock is available and cutter is not taking that muck load therefore causes tool breakage.\r\n','New program created by reducing the DOC and Stepover to overcome this problem. and check the tool load in machine and also observed the noise. After reducing the DOC dia 4R0.5 cutter running smoothly.\r\nNext all the parts running with same program and all the parts find ok.','New program proved and old program made absolute.\r\nNext batch again will check the consistency. \r\n\r\nWO No 50627,51084 & 51085 total 50nos production done with new tool path and monitored the load and cutter and same is find ok. ','CA/PA FOUND OK.','','2015-12-08','Rangaswamy()','Basavaraja S.(Jr.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','07','no','Misc','Krishna(Chowdary.G.P.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9002,'35-195','Saab AB','SUPPORT SEAL RETAINER','556560','423Z1834-2-01','','---',5,'PA 1510 FORECAST-3','','49104','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','Slot width shifted part was rejected.','Slot wall thickness not checked as per model, maintain slot wall thickness 1.5 mm equal but required dimension is one side 1.0mm another side 2.0mm','Immediately change the program as per model dimension, run the program on part and part dimensionally found ok same was accepted by QAD','Before send the program to machine, we cross check the simulation of the program as per Model or Drawing which is the master.\r\nAfter run the program on machine check the dimension as per Reference sheet.\r\n','CA/PA Found ok.','','2015-12-08','Ramesh(Poojary)','Ramesh(Poojary)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','07','no','Misc','Krishna(Chowdary.G.P.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9003,'35-195','Saab AB','SUPPORT SEAL RETAINER','556560','423Z1834-2-01','','---',2,'PA 1510 FORECAST-3','','49019','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','Slot width shifted and part was rejected','Slot wall thickness not checked as per model, maintain slot wall thickness 1.5 mm equal but required dimension is one side 1.0mm another side 2.0mm','Immediately change the program as per model dimension, run the program on part and part dimensionally found ok same was accepted by QAD','Before send the program to machine, we cross check the simulation of the program as per Model or Drawing which is the master.\r\nAfter run the program on machine check the dimension as per Reference sheet.\r\n','CA/PA Found ok.','','2015-12-08','Ramesh(Poojary)','Ramesh(Poojary)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','07','no','Misc','Krishna(Chowdary.G.P.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9004,'35-195','Saab AB','SUPPORT SEAL RETAINER','556560','423Z1834-2-01','','---',2,'PA 1510 FORECAST-3','','49099','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','Slot width shifted part was rejected','Slot wall thickness not checked as per model, maintain slot wall thickness 1.5 mm equal but required dimension is one side 1.0mm another side 2.0mm','Immediately change the program as per model dimension, run the program on part and part dimensionally found ok same was accepted by QAD ','Before create the program we check all dimension is ok and update the program as per Model or Drawing which is the master.\r\nAfter run the program on machine check the dimension as per Reference sheet.\r\n','CA/PA Found ok.','','2015-12-08','Ramesh(Poojary)','Ramesh(Poojary)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','07','no','Misc','Krishna(Chowdary.G.P.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9005,'35-187','Saab AB','INTERCOSTAL_MIDSPAN_NO_1 ','452275A','423Z1169-2-03','','---',1,'PA 1510 FORECAST-2','','49171','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Part base thickness 4.06 +/- 0.25 but measured \r\nvalue 3.70mm dig mark on part base\r\n','reducing cycle time in Unipro-5000 machine RPM  \r\nincreased  4000 to 8000 so base semi finish running \r\ntime dia 12 R3 bull nose broken. dig mark found on \r\nthe Part base thickness.','Proven tool dia 12r3 parameter reduced to 4000 and check the cutter load in machine and continued production.','Tried to reduce the cycle time by jack-up the parameters, but cutter sot supported for higher RPM and FEED.\r\nAll the production completed with proven parameters.\r\n\r\nWill check the tool geometry which can able to run with higher parameters.\r\n\r\nIf required will introduce the roughing program to avoid more stock for dia 12r3 cutter in next batch.','CA/PA found ok.','','2015-12-08','','        Karthineyan V.S.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9006,'18-209B','Magellan Aerospace(Chalfont) Limited','BODY','4842','D321 40204 202','','D, ECN NR29999ST1KM15, NR29999ST2KF65, WQN DFB09775',18,'P/078231','','46878','','2015-12-09',NULL,'yes','yes','yes','no','no','no','no','no','no','32.50+0.13 diameter oversize measured 32.75 mm.','Running time 16mm boring tool screw broken bore + side\r\nInstead of maintain 0.3mm stock in ID it remove 0.4mm extra because of boring tool screw was loose during running time.\r\n','Boring tool screw is replaced by new one and taking x and z offset for that tool and run the part.part found okay and continue the production.','Instructed to all operator to dont use any slipped screws in the tools and it is compulsary to replace slipped screws before start the production. ','Next batch okay in production.','','2015-12-09','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','01','no','Misc','Dinakar(K)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9007,'35-262','Saab AB','ROD-END','018796','424Z3413-1','','--A',1,'April 2014','','41158','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Thread tight.','1) We have checked the stock parts and found ok. See attached pictures.\r\n2) Both parts of 424z3413-1 and 424z3414-1 checked with thread plug gauge and thread ring gauge respectively and again these checked with each other.\r\n3) Gauges used: 0.500-20 UNJF 3A, standard thread plug gauge and 0.500-20UNJF 3B standard thread ring gauge.\r\n4)The thread on the picture seems damaged. So I am no doubt but there is a possibility of thread jam due to wrong entry. So please check at your end once again.\r\n','We went to SAAB and checked the parts and we cocluded that the samll hanging burrs leads to thread tight.','Instructed to check the thread features before and after the bench work.','Next batch found satisfactory.','C38511','2015-12-10','Avinash(R.J.)','Avinash(R.J.)','OF-001122','2015-11-30','1600119775-3-3           1 pc            C39813\r\n1600119775-3-2           10 pcs          C39812\r\n1600119775-3-1           10 pcs          C40016\r\n1600108796-9-4           1 pc            C39814\r\n\r\n','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','','Customer end','yes','Misc','Nagaraj(G. Nadiger)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9008,'35-079','Saab AB','BUSH FLANGED','234304','D575 40386 200','S80','B ECN NG29999ST2TT68',1,'1600104409','','48447','','2015-12-10',NULL,'yes','yes','no','no','no','yes','no','no','no','* ID Under size up to 0.025mm.After rework part ok.','','','','Part accepted.','','2015-12-10','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','With Treatment','','FI','no','Misc','Manjunath(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9009,'01-314','HAL-Helicopter','BRACKET FLOOR MOUNTING CY','H918-47/13','201C 671H 3113 201','3.4364.T7351','Nil',3,'ALHOS13-34','','46734','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','*1) 2nos dig on 12.2 angle rib.\r\n*2) 1no 4mm thick under size.','Problem for both is tool, Dia 12 flat long procured with BSR tools for trails and due to cutter re leaf angle is more in flutes and due to this cutter is broken.','Immediately production stooped and ordered the new cutter in WIDIA make.\r\nInformed to BSR tool supplier and rejected the 3 cutters and another 2nos which is at stock. ','New WIDIA make cutter checked and after confirming the cutting production continued.\r\nDedicated the same tools for this CRN.','Next part found ok.','','2015-12-10','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','00','no','Misc','Lohith(K)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9010,'18-309B','Magellan Aerospace(Chalfont) Limited','SPIGOT','K13746','F 575 51290 200','S80','B, ECN PG49999SMAKH49',1,'P/078237','','49024','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Dig mark observed on face (width under size 4mm).','Due to tool number not edit, so part 14mm width minus side.This error happen operator mistake.','Inform to operator every time do the setting cross check the tool number and tool offset.\r\nFirst part running time observe the program, ensure the tool diameter, tool number and work offset compulsory.  ','Inform to operator every time do the setting cross check the tool number and tool offset.\r\nFirst part running time observe the program, ensure tool diameter, tool number and work offset compulsory. ','CA/PA fonud ok.','','2015-12-10','Lohith(K)','        Theerthappa K.N.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9011,'18-164B','Magellan Aerospace Bournemouth','Strut Mid Rib ','A631637','F574 50160 201','','B02, ECN PG49998ST1TW21, PG40011ST1KK22',3,'RP408163','','47897','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','part profile problem','Part Profile Problem. Part Wrong Loading.  \r\n','Remaining Parts were Marked as Right & Left, Before Loading.  \r\n','Another Location Hole done In fixture so part will never locate wrong.  \r\n','Next Parts found okay','','2015-12-11','Narayanappa(G)','Manjunath(K.N.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','3','no','Misc','Narayanappa(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9012,'35-295','Saab AB','VENT DOOR','434837','425Z0101-3','','---',5,'PA 1510 NEW PARTS-2','','43268','','0000-00-00',NULL,'yes','no','no','no','no','no','no','yes','no','At least 1 of 4 holes are out of tolerance, probably due to too much paint/primer.\r\n','Paint over deposited on holes. These parts checked prior to treatment and after quality satisfactory parts dispatched to treatment.','1) Informed to treatment supplier and raised the non-conformance report.\r\n2) Rework carried out and accepted.','1) We will check the hole dimension even after treatment.\r\n2) Treatment house changed to ATPL from VMF.','Next batch found satisfactory.','C39155','2015-12-11','Avinash(R.J.)','Manjunath(G)','SCAR-001145 ','2015-12-08','Following batches of 425Z0101-3 will be returned.\r\n1600118002-6-2 - C39155      5pcs \r\n1600118002-6-3 - C39156      4pcs\r\n','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','','Cust End','yes','Misc','Avinash(R.J.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9017,'35-165B','Saab AB','HOUSING PIN','459433A','423Z1124-5-01','','--B',1,'PA 1510 FORECAST','','47674','','0000-00-00',NULL,'yes','yes','yes','no','no','yes','no','no','no','Step Observed inside of the Bore. ','This part production completed, before inspection  identified fitting department step in bore. this step generated in machine.  so analyze the problem then c/a , p/a complete.','Analyzethe problem then c/a , p/a complete. ','Analyze the problem then c/a , p/a complete.','Next Parts found okay','','2015-12-12','Rangaswamy()','Rangaswamy()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','Misc','Nagaraj(G. Nadiger)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9018,'18-411A','Magellan Aerospace(Chalfont) Limited','PLUNGER','W71530','D321 40205 200','','H01',5,'P078229','','49050','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Hole pitch 1mm shifted.','This deviation done while carrying drilling operation. Part Slot dimensions measures  plus side by 0.02mm. this slot will guide in jig for drilling operation. but this 0.02mm plus material is not allowed to guide perfectly in jig.\r\nFitter not checked the part guide and butting before manual drilling operation.  \r\nDue to this problem hole pitch 1mm shifted.','Immediately all the parts in this batch checked the pitch and found OK.\r\nSnap gauged (GO gauge) done to check the slot dimension while machining. ','Snap gauged (GO gauge) done to check the slot dimension while machining. \r\nInformed to fitters to check the parts butting while using the DRILL JIGS.','Next Parts found okay','','2015-12-12','Nagaraju(T)','Rajesh(K C)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','9','no','Misc','Nagaraju(T)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9019,'34-069','Magellan Aerospace Winnipeg','HINGE L/H','57034-4','400-12901-1','','EM104302 Iss A,EM105092 Iss G,EM104765 Iss G',1,'C46695','','47893','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Total length  under size 2.5mm.','Due to first part setting time \"X\" reference taken not properly so part was under size maintained.  ','Immediately stop the machine and cross check the \"X\" reference and find out the mistakes, after continue the production.\r\nInform to operator every CRN first part setting time take the work offset(X0,Y0&Z0)and cross check the work offset. ','Inform to operator every CRN first part setting time take the work offset(X0,Y0&Z0)and cross check the work offset. ','Next Parts found okay','','2015-12-14','Lohith(K)','        Vishwanath Pavar','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9020,'18-372B','Magellan Aerospace Bournemouth','GAMMA FITTINGS ','M665370 3577','NSA840007-250 ','','N',1,'RP408523','','49071','','0000-00-00',NULL,'','','yes','','','','','','','ID ovality 0.025mm.\r\n\r\n\r\n\r\n\r\n\r\n\r\n\r\n\r\n\r\n\r\n\r\n\r\n\r\n\r\n\r\n\r\n\r\n\r\n\r\n\r\n\r\n\r\n\r\n\r\n\r\n\r\n\r\n\r\n\r\n\r\n\r\n\r\n\r\n\r\n\r\n\r\n\r\n\r\n','After running 50 to 60 parts insert tip will be worn out and running time chips not breaking properly so chips will rubbing inside the part and diameter will be oversize in the running part.','Remove the worn out insert and replace the new insert and newly offset taken and 0.2 (-) minus taken in the tool wear offset and run the part and then check the inner diameter\r\nand give the correction in wear offset and adjust the coolant correctly and run the part and checked found okay.','while setting time loading the new insert before running and after every 100 nos change the roughing insert and run the part.and every 25ns once observe the tool noise,coolant flaoing and chips while running. ','Next batch okay in production.','','2015-12-15','','        Manjunatha N','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9021,'35-291','Saab AB','BEAM FITTING','452276B','424Z1143-2','','--B',1,'PA 1510 FORECAST-3','','48294','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Base thickness dig mark.','Base thickness open out because when ATC tool changing time wrong tool came  & runned. Actual tool is 12 F/l & runned toll is 10r3 \r\nThis error due to machine error.     \r\n','Immediately machine was stooped and informed to machine supplier and service engineer came and checked the cause for wrong tool picked by ATC.\r\nHe suspects that sensor malfunctioned and therefore wrong tool picked by ATC. \r\nChanged all the tool parameters and also reloaded the all the tools to tool magazine.Tool magazine cleaned and removed all the aluminum chips.\r\n','After this incident again this problem is not coming and also informed to operators and supervisor to clean the chips regularly in tool magazine.','CA/PA found ok.','','2015-12-15','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Rangaswamy()','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9022,'34-031A','Magellan Aerospace Winnipeg','PIN SHEAR ACCESS DOOR','426935','400-12748-1-905','','EM105092 Iss F, EM104302 Iss A, EM104765 Iss G, EM106399 Iss B, EM106400 Iss B, EM106401 Iss A, EM106404 Iss A, EM106522 Iss A, EM106602 Iss A',1,'B91379 Rev.026','','46996','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1)Thread damage.\r\n','Thread Effective dia over size, when doing rework thread damage. ','Each parts are checking with Thread pitch micrometer as well as thread ring gauge at production.','we are maintaining gauge usage record.  ','we are monitoring in next batch. ','','2015-12-15','Sudhagar(V)','Avinash(R.J.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','0','FI','no','Misc','Sudhagar(V)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9023,'35-282','Saab AB','GUIDE HARNESS LWR','599463','423Z1982-1','','---',1,'PA 1510 FORECAST-3','','49323','','0000-00-00',NULL,'yes','no','yes','no','yes','no','no','no','no','Tool dig mark on face.','production running time air presser low alarm coming and same time machine \"z\" axis came down by 30mm, so tool holder touch on part face and dig mark observed on part.','Immediately machine stopped and informed to machine supplier. Service engineer came and rectify the problem. Z-axis brake really failed and need to replace the same.\r\nBrake really replaced the same and check the z-axis down by creating the air pressure low and immediate power cutoff.','Brake really replaced the same and check the z-axis down by creating the air pressure low and immediate power cutoff.\r\nInformed to machine supplier and CIM maintenance team to ensure the relay working in parameters and also manual check while doing a PM.','CA/PA found ok.','','2015-12-17','Rangaswamy()','Govindraju(NR)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Rangaswamy()','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9024,'35-185','Saab AB','CED_LATCH_SERRAT_ED_PLATE','581787A9','425Z0610-17','','---',6,'PA 1510 FORECAST-2','','48274','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','part bend so serration depth not achieved.','This deviations found in all the serration parts and we tried to avoid bend in parts by changing the machining process, but its not achieving consistently.\r\nWhile doing the trails the above deviations coming and tried to rework the parts, but serration depth is not achieving.\r\nTherefore parts scraped.','While doing the trails to avoid bend, we observed the tool tip blunted and this was applying the load on the part and parts getting twisted after removing the parts from fixture.\r\nTool resharpened and machined 10nos of parts continuously and results are coming consistently and also bend is not observed.(0.05mm flatness achieved in all the parts)','Now process was proven and supervisor and operators will check the tool tip regularly and 01 extra tool kept in tool grip.\r\nMessage added in beginning of the program to trigger the user to check the tool tip.\r\n','CA/PA found ok.','','2015-12-17','Rangaswamy()','Shivashankar(H.G.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Rangaswamy()','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9025,'35-185','Saab AB','CED_LATCH_SERRAT_ED_PLATE','581148A4','425Z0610-17','','---',3,'PA 1510 FORECAST-2','','48275','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','part bend so serration depth not achieved.','This deviations found in all the serration parts and we tried to avoid bend in parts by changing the machining process, but its not achieving consistently.\r\nWhile doing the trails the above deviations coming and tried to rework the parts, but serration depth is not achieving.\r\nTherefore parts scraped.\r\n','While doing the trails to avoid bend, we observed the tool tip blunted and this was applying the load on the part and parts getting twisted after removing the parts from fixture.\r\nTool resharpened and machined 10nos of parts continuously and results are coming consistently and also bend is not observed.(0.05mm flatness achieved in all the parts)\r\n','Now process was proven and supervisor and operators will check the tool tip regularly and 01 extra tool kept in tool grip.\r\nMessage added in beginning of the program to trigger the user to check the tool tip.\r\n','CA/PA found ok.','','2015-12-17','Rangaswamy()','Mahesh(N)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Rangaswamy()','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9026,'28-045','Magellan Aerospace New York  Inc.','LEVER','158524','65-51632-6','','PL_Rev - A + ADCN # 2 ; DL_Rev - N/C',1,'135212-2520','','49374','','0000-00-00',NULL,'','','yes','','','','','','','Dia 25-0.3mm bore oversize by 0.25mm.','Running time 16mm boring tool screw broken bore + side Instead of maintain 0.3mm stock in ID it remove 0.4mm extra because of boring tool screw was loose during running time.\r\n\r\n','Boring tool screw is replaced by new one and taking x and z offset for that tool and run the part.part found okay and continue the production.\r\n','Instructed to all operator to dont use any slipped screws in the tools and it is compulsary to replace slipped screws before start the production. ','Next batch parts found okay in production.','','2015-12-17','','        Seetharamu D','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9027,'35-274','Saab AB','PIN','G21482K01','426Z2601-1','','--A',1,'PA 1510 FORECAST-3','','49168','','0000-00-00',NULL,'yes','yes','yes','no','no','yes','no','no','no','* Slot thickness under size up to -0.02mm','While running slot machining first off was proved and check and taken approval to run the production.\r\nProcess was proved and running production without any deviations.\r\nBut in between there is a problem of chips clocking in tool changer arm and have variation in tool length and also run out in tool.\r\nThis errors causes thickness measures minus side.','Immediately all the tools removed from magazine and cleaned.then cleaned the tool changer arm and magazine and then again reloaded the tools and runned the same proved program.\r\nNext part checked by QAD and again after approval production continued.','This problem is due to chips clocking in tool magazine and tool changer arm.Mandatory every week(Once we switched off the machines on Sunday morning). But still this was happened and will monitor the cleaning methods in every week.\r\nInformed to supervisors and operators to check and clean the arm frequently.\r\n','CA/PA Found ok.','','2015-12-17','Girish(Prasad P)','Vasu SN,Ningaraj A N,Bharath R,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','QT100S-2','Yashawantha(NH)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9028,'18-453A','Magellan Aerospace Wrexham','RIB 3 AFT OFW','445817C','L575 51776 200 PF','','A',1,'RP133571 Amnd 2','','46490','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Drawing requirement for Dia2.40mm hole is only deburring but it chamfered up to 0.5mm and also oblonged at one place.','Part Accepted','Part Accepted','Part Accepted','Part Accepted','C41716','2015-12-18','Narayanappa(G)','Siddaramappa ,Sathish Y.R.,Karthineyan V.S.,Gajendra Singh C.,','RDN0130','2015-12-02','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','Manufacture Only','','FI','no','HAAS','Avinash(R.J.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9029,'35-188','Saab AB','INTERCOSTAL_MIDSPAN_NO_2 ','452275A','423Z1170-1-05','','---',1,'PA 1510 FORECAST-2','','48000','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dia 3.20 hole shifted  by 2mm.','This deviation happened while drilling operation carried in fitting.( dia 3.2 hole operation is done in DRILL JIG).\r\nWhile loading the part using 05 pins part is locating in both X and Y axis.(01 pin at X-axis 04pins at Y-axis) One pin not butted and drilling operation done, fitter not cross checked the part butting in both the axis. ','After this deviation minor JIG design changed to avoid such manual errors.\r\nFull proof method done by adding one more pin in X-axis.\r\nThis new butting pin changed in MPS and production done with new butting method.\r\nNo deviations can happened in next bathes.another DRILL JIGS checked for the above errors and all are ok.','Full proof method done by adding one more pin in X-axis.\r\nThis new butting pin changed in MPS.','Next Parts found okay','','2015-12-18','Nagaraju(T)','Raghu(A.N.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','09','no','Misc','Nagaraju(T)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9030,'18-431A','Magellan Aerospace(Chalfont) Limited','SPRING RETAINER ','A0563X','D321 40203 220','','L',24,'P078230','','48266','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Parts rejected at treatment house(GET)due to processing error.','parts are rejected due to a processing error at treatment house(informed by supplier).','Debit note raised to treatment supplier.','Informed to supplier to take care in future batches while processing the parts.','Next batch found ok.','','2015-12-19','Avinash(R.J.)','Nandishkumar(D.K.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','21495','POST DN','no','Misc','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9031,'35-289','Saab AB','BEAM FITTING','443866D','424Z1141-2','','--B',1,'PA 1510 FORECAST-3','','45269','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','** Running time part shifted Wall thickness minus.','While running operation-03 part moved due to tool load in roughing operations.\r\nDue to this movement of part, wall thickness measures minus side.\r\n','Part will move due to in sufficient force to hold the part.\r\nChecked the clamping method and condition of clamps and bolts, \r\n35-287 to 35-291 parts process is same and all the parts clamping is sufficient to do the 3mm DOC and 4000 table feed.\r\nThis problem may be because of part not clamped properly by operator.','Parts clamping force checked, found ok.Informed to operator to clamp the bolts correctly and ensure the tightness once again.\r\nTorque winches will plan to tightened the bolts.  ','CA/PA found ok.','','2015-12-19','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','3','no','Misc','Lohith(K)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9032,'18-213A','Magellan Aerospace(Chalfont) Limited','END CAP ','M395260','D321 40209 200','','A, ECN NR29998ST1JA76',1,'P078229','','49057','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Dia 25-0.3mm bore oversize by 0.25mm.','Running time 16mm boring tool screw broken bore + side Instead of maintain 0.3mm stock in ID it remove 0.4mm extra because of boring tool screw was loose during running time.\r\n','Boring tool screw is replaced by new one and taking x and z offset for that tool and run the part.part found okay and continue the production.','Instructed to all operator to dont use any slipped screws in the tools and it is compulsary to replace slipped screws before start the production.','Next batch found okay in production.','','2015-12-21','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','0','01','no','Misc','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9033,'18-371B','Magellan Aerospace Bournemouth','GAMMA FITTINGS ','M305800','NSA840007-150','','N',1,'RP408523','','49413','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Total lenght 0.2 undersized.\r\n','In first set up face was unclear thats why 0.2mm given in work offset and run the part part found okay . and in second set up 0.2mm not taken plus side in work offset so thickness 0.2mm under size.','jaws bored neatly where the 1mm thickness face was butted to jaws and clamped on od and taking offset run the part ,part found ok and contionue the production.','Instruction given to operator to where the thickness is maintained for have to butt that face in the jaws not in the starting face. instruction given to operator to where the thickness is maintained for have to butt that face in the\r\njaws not in the starting face. ','Next batch found okay in production.','','2015-12-21','Sandhesh D(S)','Sandhesh D(S)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','01','no','Misc','Sandhesh D(S)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9034,'35-166A','Saab AB','HOUSING PIN','459434B','423Z1124-6-01','','--A',1,'PA 1510 FORECAST','','46831','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dia 36.523 +/- 0.010 bore unclear.','First part bore complied and check CMM  correction \"X\" axis 0.02mm and \"Y\" axis 0.05mm, bore dia found ok. after correction another part finish bore again check in CMM position found ok. but 3rd part same program & same tool running but bore unclear.','Another part again set bore then finish.','This type of problem first time, analyse next batch production. ','Next Parts found okay','','2015-12-22','Rangaswamy()','Umesh(B)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','11','no','Misc','Rangaswamy()','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9035,'18-326A','Magellan Aerospace Bournemouth','ATTACHMENT ANGLE','449658','L572 53314 200','ABM3 1029','A00',1,'RP408152','','49342','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Wall thickness minus. Wrong correction.','This error is by operator.Operator checked the firstoff part and thickness measures within tolerance, but operator tried and action taken to maintain in mean.\r\nbut while doing a correction in offset wear in machine wrong value entered.\r\n(Correction 0.5mm given instead of 0.05mm,so part rejected) ','After this error supervisor involved and cleared the offset wear value and continued production again next part thickness measures. Thickness is in tolerance limit.\r\n\r\nFor PA supervisor analyzed that program created to mean value and thickness measuring maximum side in both the ends of the part due to cutter load part wall will deflect.','After analyzing the PA,Finishing cutter parameter reduced and checked.\r\npart deflection is reduced and thickness measures at mean value in complete wall.','CA/PA found ok.','','2015-12-24','Rangaswamy()','Rangaswamy()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Rangaswamy()','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9036,'18-107B','Magellan Aerospace Bournemouth','LINK BODY','0163','D574 50553 200','','A',1,'RP408149','','48916','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Part lost at treatment house (API).','Part lost at treatment house (API).','Part lost at treatment house (API).','Part lost at treatment house (API).','Part lost at treatment house (API).','','2015-12-24','Avinash(R.J.)','Nandishkumar(D.K.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','21791','POST DN','no','Misc','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9037,'18-477A','Magellan Aerospace Wrexham','RIB 2 L/H ','9550801','L575 41322 200 PF','','A00',2,'RM133577 Amnd 3','','48462','','0000-00-00',NULL,'yes','no','no','no','no','yes','no','yes','no','Dia5.6 hole Hublong measure at Dia 5.85 on Flange side.','drilling operation in fitting department used new fixture bush was problem so hole position is under\r\nsize.','stop the production order to the new hardened bush in two types free size bush & finish size bush\r\nbefore finishing operation part hole position checked after the finish drilling operation','inform to fitters you don\"t use without hardened bush in any drilling operation ','ca/pa found ok','','2015-12-25','Ravikumar(L)','Paramesh K,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','Manufacture Only','','fi','no','HASS VR11','Avinash(R.J.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9038,'35-188','Saab AB','INTERCOSTAL_MIDSPAN_NO_2 ','452276C','423Z1170-1-05','','---',4,'PA 1510 FORECAST-2','','47999','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','* Totel hight, Rib hight and dig mark area thickness diamension under size up to -0.15, out of tolerance.','Actually 03rd operation fixture on machine bed but loaded on Zero point system base. At base finishing & rib thickness running program operator put the addition one manual clamp and tight it. So part top face paryalilty goes wrong and thickness of the part under sized.  ','In fixture only one extra hole made and added the clamp then parts have no problem.','In fixture only one extra hole made and added the clamp then parts have no problem.','Next batch found ok.','','2015-12-25','Narayanappa(G)','Sathish Y.R.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','UNIPRO 5000-1','Yashawantha(NH)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9039,'18-367A','Magellan Aerospace(Chalfont) Limited','STRAP JOINT CROWN','398807B','F572 55081 203','','C, ECN PG48437ST4KC60',1,'P/078237','','49416','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dig mark observed on part. ','Part wrongly loaded in operation-03.Location pin is in diagonal and able to locate at both the orientations. Operator not noticed the loading of part and dig mark observed after running roughing tool because part was wrongly loaded\r\n','Immediately checked and marked the front face for all the remaining parts. Informed to operators to ensure the front face after loading the part in fixture. Production continued and supervisor is monitoring. \r\n','The following PA action planned and implemented, 1.Location pins diameter changed and amended in MPS. 2.Dia 6 and Dia 5 mm locating pins introduced to avoid wrong locating of part in\r\noperation-03. 3.New program created for dia 5 H7 hole. \r\n','Next Parts found okay','','2015-12-25','Anjinamurthy(H)','S. Shiva(Kumar)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','03','no','Misc','Anjinamurthy(H)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9040,'35-187','Saab AB','INTERCOSTAL_MIDSPAN_NO_1 ','452275A','423Z1169-2-03','','---',1,'PA 1510 FORECAST-2','','49171','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Cutout not finish and rib thickness not finish.','This deviation is due to finish program tool tip was blunted while production batch running.\r\nOperator noticed when checking the parts thickness in stage and identified the part with tag.','Rework done by operator in presence of supervisor by clamping the part in same fixture by applying the external clamps.\r\nSame finishing program runned and thickness checked and found ok.\r\nProfile point check in CMM and all the drawing requirements are meeting.','Process,Program and Tools are proven for this part, Only operators need to monitor the tool tip to avoid such problems.\r\nSupervisor will check the tool life regularly.','CA/PA found ok.','','2015-12-26','Narayanappa(G)','Karthineyan(V.S.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','','03','yes','Misc','Narayanappa(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9041,'35-235A','Saab AB','JACK BRACKET 1 ','927318','D576 50009 206','','D00',1,'1600118541','','46026','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Tool dig mark on rib ( dia 16ripper broken).','Dia 16 ripper using for profile ruffing this time spindle coolant problem  so heat generate tool broken.part profile dig mark.','Stop the machine inform to maintenance department to clean the coolant filter.\r\nAfter cleaning coolant flow checked then production continued.','This problem is due to coolant filter blocked. so every 15days mandatory clean coolant filter in every machines.','CA/PA found ok.','','2015-12-26','Rangaswamy()','Shivashankar(H.G.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Rangaswamy()','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9042,'35-263','Saab AB','EXTENSION ROD','G22125K06','424Z3414-1','','--A',1,'PA 1510 FORECAST-2','','48485','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Step observed on ID threads.','part accepted.','','','part accepted.','','2015-12-26','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','With Treatment','','03','no','Misc','Krishna(Chowdary.G.P.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9043,'35-191','Saab AB','SUPPORT-FTG','581308','423Z1202-13','','---',1,'1600096186','','38876','','0000-00-00',NULL,'no','no','no','no','no','yes','yes','yes','no','FPI REJECT.','Due to rubbing of tool or material behavior FPI failure has been found in Treatment house','Instructed to Production  & fitting department to avoid rubbing of tool and polishing ','Avoid polishing and try to finish the part  in machining stage itself.','Next parts and batches found okay','','2015-12-29','Manjunath(G)','Yashawantha(NH)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','16007','Post DN','yes','Misc','Yashawantha(NH)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9044,'18-102A','Magellan Aerospace Bournemouth','BARREL-STRUT','A1564N','D572 50463 200','S98 FHT','F',1,'RP408147','','48840','','0000-00-00',NULL,'','','yes','','','','','','no','4.93 drill part top face dig mark so part reject ','Model call was activated so top face while drilling found dig mark','Learned the process of Model call and now we have not activated the Model call . ','Learned the process of Model call and now we have not activated the Model call . ','CA/PA found satisfactory.','','2015-12-29','','        Girish HP','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9045,'18-367A','Magellan Aerospace(Chalfont) Limited','STRAP JOINT CROWN','398807B','F572 55081 203','','C, ECN PG48437ST4KC60',1,'P/078237','','49416','','0000-00-00',NULL,'','','yes','','','','','','','Dummy','Dummy','Dummy','Dummy','Dummy','','2015-12-29','','        S. Shiva Kumar','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9046,'18-210B','Magellan Aerospace(Chalfont) Limited','BODY','6608','D321 40204 204','','D, ECN NR29999ST1KM15, NR29999ST2KF65, WQN DFB09775',4,'P/078231','','49035','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Thread tight.','Insert wear out.','Rework done part accepted.','Rework done part accepted.','part accepted','','2015-12-30','Dinakar(K)','Narasimhamurthy(K.G.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','With Treatment','','07','no','Misc','Narasimhamurthy(K.G.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9047,'47-009','GKN Aerospace Services Limited-Yeovil','SKIN INSERT M/C','4521801','D574 55151 200','','A, ECN NG35561ST4KA32',5,'GKN FORECAST','','49696','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1) Thickness under size by 0.05 to 0.08MM.','1) this deviation is due to thickness tolerance mentioned in MPS is not correct.\r\n1.6 +/-0.1mm mentioned in MPS and all the parts was maintained with in this tolerance.\r\nBut after checking the parts at FI thickness tolerance is 1.6 +0.1 only.Then all the parts ensured and got 05nos below drawing tolerance.','Changed the thickness tolerance in MPS.\r\nInformed to supervisor to cross check the MPS dimensions with drawing.','Informed to CAD to ensure the tolerance as per the drawing requirements while doing the MPS.\r\n','1)Process sheet found OK.\r\n2)CA/PA Found OK.','','2015-12-31','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','0','FI','no','Misc','Sudhagar(V)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9048,'47-005','GKN Aerospace Services Limited-Yeovil','JOINT PLATE','4519802','D574 50135 202','','C, ECN NG33264ST1KB44',1,'GKN FORECAST','','49683','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1) Tool dig mark on face','While doing production batch, parts loaded in two fixtures using change over zero point system.\r\nWhen operator changed the next part to zero point system, fixture not butted(clamped) properly in zero point system.this causes Z-Axis variation and this defect the part in roughing.','After finding the deviation when roughing tool running, operator checked the reasons and find the above root cause and re clamped the fixture again and continued production after ensuring the clamping in zero point system.','Informed to operator to check the clamping in zero point system visually and ensure once before running the program.\r\n\r\nAfter this deviation found monitored and checked the awareness of checked the clamping visually for every change over in zero point system.','CA/PA Found OK.','','2015-12-31','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','0','FI','no','Misc','Sudhagar(V)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9049,'47-014','GKN Aerospace Services Limited-Yeovil','STIFFENER BUTT STRAP','2904502','D575 41603 200','','C01, ECN HG29999ST1TE12',1,'GKN FORECAST','','49703','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Outer profile mismatch.','This d3eviation is due to locating pin size is not correct and this error causes mismatch in part from operation-01 and operation-02 machining faces.','After observed the deviation in firstoff part, immediately checked and changed the locating pin in fixture.\r\nNext part checked and all the parameters are control, then after taking approval from QAD production continued.','Fixture validation done by checking the flatness, diameter of pin, bolts condition.But operator not analyzed that pin is warn out.But after checking the firstoff again fixture validated.\r\nInformed to operator to check the pins and bolts condition before loading the fixture in to machine.','CA/PA Found OK.','','2016-01-01','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','0','FI','no','Misc','Sudhagar(V)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9050,'47-013','GKN Aerospace Services Limited-Yeovil',' 	STRAP ASSY BTM SKIN','6059702','D575 41103 200','',' 	A, ECN HG29999ST1PN57, NG30735ST1KA20',1,'GKN FORECAST','','49702','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Thickness under size by 1.0MM.','This deviation is due to operator error, part not loaded correctly.Orientation is WRONG.\r\n','Corrective action and Preventive action are taken while doing the FAI. Part not located and clamped with wrong loading, but operator loaded the fixture wrongly in zero point system.','Full proof to avoid wrong loading of fixture will implement in next batch by introducing the pin or butting.\r\nAfter this change fixture can not load wrongly. ','CA/PA Found OK.','','2016-01-01','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','0','FI','no','Misc','Sudhagar(V)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9051,'47-015','GKN Aerospace Services Limited-Yeovil','STIFFENER BUTT STRAP','2904502','D575 41603 201','','C01, ECN HG29999ST1TE12',1,'GKN FORECAST','','49705','','0000-00-00',NULL,'yes','no','no','no','yes','yes','no','no','no','Hole pitch shifted by 0.5mm ','While doing first off part, Drilling hole is not open out due to final drilling depth in program is Zero.\r\nAfter checked the firstoff part, changed the drilling depth in program and then continued production.\r\nThe parts which drilling hole is not opened is reworked in fitting manually and causes deviation in hole position.  ','All the other parts which manufactured with changed drilling depth are ok and ensures the same for all the parts.\r\n\r\nInformed to fitter to check the hole position and guide them with center to get parallel to part face.','Now drilling depth is proved( -1mm ) and saved.\r\nThis error will not happened in future.','CA/PA Found OK.','','2016-01-01','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','Misc','Sudhagar(V)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9052,'28-003A','Magellan Aerospace New York  Inc.','PIN-ATTACHMENT WALKING BE','G22083K01','161A7305-1','','PL-Rev-NC, DL Rev-B',1,'132019','','48224','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','OD thread damage.','Due to miss handling by operator.','Instructed operator to handle the parts carefully and properly\r\nplaced in trays.','Nylon sleeves will be introduced to avoid this type of deviations.','Next Parts found okay in Production ','','2016-01-01','Ravi(M)','Seetharamu(D)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','09','no','Misc','Ravi(M)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9053,'42-002','RAFAEL','PSA BASE','K10598','BA1E2001B','','38-576104_Rev-E, TILDOCS#172373_Rev-13, RE_804-1-5_Rev-11, 111.21_Rev-6, 23.36.59_Rev-F, ECN 57176 2014/08 /25; ECN 58483  2014/07/29',3,'347592024 Rel 9','','48401','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1) Angle out of tolerance by 1 to 2 Minutes.','Angle checked was CMM some error was occured.','CMM checking methodalogy to be changed & cross checking sent to Another source.','CMM checking method to be changed.','After receiving the parts we cross checking we will close the NC.','','2016-01-04','Sudhagar(V)','Avinash(R.J.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','DN21572','Post DN','yes','Misc','Sudhagar(V)','',NULL,'',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9054,'18-313A','Magellan Aerospace Wrexham','STUD ','453734','D278 50006 204 01','','D',1,'RP135260','','49615','','0000-00-00',NULL,'yes','yes','yes','','','','','','','OD Undersize.','after running 5ns TNMG tool sim was broken so insert will not seated properly so running time insert tip will be broken and insert was rubbing the part and vibration started in the insert that time it will removing the extra material in outer diameter so outer diameter will be undersized.\r\n','change the broken sim,insert and screw and newly offset taken and 0.2 (+) plus taken in the tool wear offset and run the part and then check the outer diameter and give the correction in wear offset and run the part and checked found okay.','before every part setting ,check the all tool sim, screws, pins and locks before tightening the tools to machine.then observe the noise every time while machining. ','Next part found ok.','','2016-01-04','','        KRISHNAMURTHY N','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9055,'18-313A','Magellan Aerospace Wrexham','STUD ','453734','D278 50006 204 01','','D',1,'RP135260','','49614','','0000-00-00',NULL,'','','yes','','','','','','','od -side 0.003 MM','','','','Parts accepted.','','2016-01-04','','        Dinakar K','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9056,'18-075A','Magellan Aerospace Wrexham','ADAPTOR ','20184116','D282 50044 200','','A',1,'RP135273','','49213','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Bore Over size 0.03mm.','This part rejected while running production batch and find out in FI.\r\nParts not checked 100% while running operation-01.As per our inspection sheet every parts to be ensure the bore diameter.\r\n','After finding the deviation all the parts checked and ensured.\r\nInformed to operators to check the parts while production is under process.\r\nSupervisor to ensure and monitor the operator for checking the parts.','Awareness build to check the parts and maintain the procedure at production.\r\nSupervisors to monitor and training to be impart regularly to avoid such problems.','CA/PA found OK.','','2016-01-04','Dinakar(K)','Shivanand D.B.,SHIVAKUMAR ,Raghavendra Rao R,Dinakar K,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','FI','no','ST20','Narasimha Murthy(R)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9057,'18-114A','Magellan Aerospace Bournemouth','NUT','240136','D575 40499 200','S80 FHT','D01',1,'RP408154','','48809','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','NDT Fail.','Due to rubbing of tool or material behaviour NDT failure has been found in Treatment house\r\n','Instructed to Production  & fitting department to avoid rubbing of tool and polishing \r\n','Avoid polishing and try to finish the part  in machining stage itself.\r\n','Next parts and batches found okay\r\n','','2016-01-04','Avinash(R.J.)','Nandishkumar(D.K.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','22062','POST DN','no','Misc','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9058,'28-006A','Magellan Aerospace New York  Inc.','SHOULDER BOLT ','574049','162A3109 -2','',' 	PL Iss A, PSDL Iss A, ECN C141079',2,'130775','','48204','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Thread Effective Diameter under size by 0.14 mm.\r\n','Wrong instrument used and which they supposed to use M4 anvil instead of M3 anvil for thread  pitch micrometer to check the effective diameter.  Operator not checked the measuring instrument before usage.',' During 1st off this was noticed and then changed the instrument and other parts manufactured and found ok.','Operator instructed and trained which they collect all the measuring instrument and cutting tools before start the process. ','CA/PA found ok.','','2016-01-06','Narasimhamurthy(K.G.)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','03','no','Misc','Narasimhamurthy(K.G.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9059,'18-120C','Magellan Aerospace Bournemouth','HOUSING OUT B D BRG 3','K10860','D275 56121 200','','E01,  ECN NG27011ST1KA83',1,'RP408158','','48859','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Running time part rotate so OD damage.','Running time part rotating that time outer diameter is damage and od undersize.\r\n','OD finishing time using fixture in part locating & face locking in washer .the washer not locking in properly so part running time rotating .instruction given to operator before cycle start check the part tightening after running part.','OD finishing time using fixture in part locating & face locking in washer .the washer not locking in properly so part running time rotating .instruction given to operator before cycle start check the part tightening after running part. ','CA/PA found ok.','','2016-01-06','','        Ningaraj A N','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9060,'18-245B','Magellan Aerospace Bournemouth','BUTTSTRAP LOW RS4X13100','451690','L575 50178 200','ABM3 1029','A00',1,'RP408289','','49642','','0000-00-00',NULL,'','','yes','','','','','','no','Base thickness 2.85 to 3.15mm measures 3.05/2.75mm locally','1) Zero point clamping fixture not holded the part fixture.\r\n2) Noticed the taper in fixture upto 0.15mm.','1)Re-loaded the fixture and located correctly. ','After loading part fixture to zero clamping system then that should be dialed.','Next batch found satisfactory.','','2016-01-07','','        Diwakar R.B.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9061,'34-052','Magellan Aerospace Winnipeg','MOUNTING LUG GEARBOX, RH','A12904','400-12608-2','','EM104302 Iss A,EM105092 Iss G,EM104765 Iss G',1,'C46695','','49513','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Thickness under size 0.2mm\r\n','While running production batch ball nose broken.','Replace the ball nose next part found ok.\r\nNext part loading time tool length and parameter adjusted after continue the production.\r\n ','Inform the operator tool holding time cross check the tool length and tool run out compulsory. ','CA/PA found ok.','','2016-01-07','Lohith(K)','Theerthappa(K.N.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','0','no','Misc','Lohith(K)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9062,'18-083A','Magellan Aerospace Wrexham','STUD PLATE','297622/001','D278 50007 201','ABM3 1029','D01',1,'RP135247','','49816','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Dig mark observed on face.','Wrong loading of part in final operation.','Informed to operator to check the process sheet and understand the process properly before running the job.','Informed to supervisor to take care this types of  errors,training given in machine that all should understand the process.','CA/PA found ok.','','2016-01-08','Lohith(K)','        Dhananjaya N','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9063,'35-182B','Saab AB','EDGE HOUSING','626088','423Z1121-5-02','','--B',1,'PA 1510 FORECAST','','48579','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','Material chip off.','During Program running time chips strucked on part,due to material chip off on part.','Next Part running time coolant flow was corrected.\r\n','Before running the part program coolant flow should be check.','Next Part found Ok.','','2016-01-08','Ramesh(Poojary)','Ramesh(Poojary)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','05','no','Misc','Krishna(Chowdary.G.P.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9064,'35-182B','Saab AB','EDGE HOUSING','626088','423Z1121-5-02','','--B',1,'PA 1510 FORECAST','','49376','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','Dig mark on outer wall.','For continual improvement change the new program and same program run on part for trail purpose dig mark found on outer wall part was rejected','Program changed and run on part , part found satisfactory','Any trail purpose before running program on part we cross check simulation on software, if found simulation verify Ok on software after run on part','CA/PA FOUND OK.','','2016-01-08','Ramesh(Poojary)','Ramesh(Poojary)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','05','no','Misc','Krishna(Chowdary.G.P.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9065,'44-003','Aerostructures Assemblies India Pvt. Ltd','7605450-200','4399701','L574 55450 200','','B00, ECN PG74415001JA02',1,'FORECAST','','48582','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','WEB THICKNESS UNDERSIZE UPTO 0.17MM','While program  running time part not butting in vacuum fixture,','Instruct to operator to check sufficient butting in vacuum fixture then only start the machining.','Added the external clamp at base finishing time and put the massage in base finish program. and give the training to operator how to check the vacuum pressure holding the part in vacuum fixture ','CA/PA FOUND OK.','','2016-01-09','Narayanappa(G)','Gajendra Singh C.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','Unipro5000','Yashawantha(NH)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9066,'18-445B','Magellan Aerospace Wrexham','PIPE END FITTING','M506580','L280 50067 210 PF','','A00',2,'RP140358','','49810','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','od ovality problem.','2nd setup running time using old fixture so part was ovality occured.','new fixture was make and running 2nd setup part found ok.','new fixture was make and running 2nd setup part found ok.','Next found ok.','','2016-01-10','Dinakar(K)','Manjunatha(N)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','01','no','Misc','Ravi(M)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9067,'18-314A','Magellan Aerospace Wrexham','STUD','245160','D278 50006 206 01','','D',1,'RP135260','','49618','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','od undersize by 8micron.','od finish running time chips rubbing part so od measuring +side so od finishing repass was running od undersize by 8micron.','next part od finish insert changing and correction given to wear offset part running part found ok.','next part od finish insert changing and correction given to wear offset part running part found ok.','Next part found ok.','','2016-01-10','Ravi(M)','KRISHNAMURTHY(N)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','03','no','Misc','Ravi(M)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9068,'43-017','Composite Industrie','BRACKET','454147 A','V251 11622 200','','A00, ECN PV100298ST1AD69',1,'ATA25_ACH-4128-1','','49847','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Rib thickness under size(4.0+/-0.2) measured 3.5 to 3.6 mm. ','Rib thickness under size(4.0+/-0.2). measured 3.5 to 3.6 mm due to Wrong tool selection.(16flat runed instead off 6flat)','When starting the program operator found deviation in material removal,then program stopped and checked the error and found the above problem. Immediately changed the tool and then continued production.		','This error is due to lack of concentration. because in datasheet clearly mentioned the tool diameter and also in program. Training conducted to Mr.SundarD.K to check the MPS and informed to supervisor to monitor the operators and guide them regulatory to avoid such manual errors.','Next part found ok.','','2016-01-11','Girish(Prasad P)','Sundar(D.K.)','','0000-00-00','Rib thickness under size(4.0+/-0.2). measured 3.5 to 3.6 mm. ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Girish(Prasad P)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9069,'43-017','Composite Industrie','BRACKET','454147 A','V251 11622 200','','A00, ECN PV100298ST1AD69',1,'ATA25_ACH-4128-1','','49847','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Bass thickness under size (2.0+/-0.2) measured 1.5 to 1.6mm.','This rejection is due to operator error, while setting operation-02 operator not dialed the \"A0\" and then loaded the parts and program runned. This error is also due to miss communication between shift change operator. and shift operator is not cross checked the setting and also reliving\r\noperator is not informed the setting details.','Next parts supervisor checked the \"A0\" and then next part machining started. Emp\r\nno.400189 and 300028 training conducted for the procedure while changing the shift and methods to transfer the work while changing the shift.\r\n','Training conducted for the machine operators as per the above corrective action. Supervisor to monitor the shift record on daily basis for 01 month.','Next part found ok.','','2016-01-11','Girish(Prasad P)','Manukumar(H M)','','0000-00-00','Bass thickness under size (2.0+/-0.2) measured 1.5 to 1.6mm. ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Girish(Prasad P)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9070,'18-610A','Magellan Aerospace Wrexham','PIN FLOATING ANG','739760','L575 54228 200','','A00',2,'RM132919 Amnd 1','','49739','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Running time power trip OD Dig mark.','','','','','','2016-01-12','Dinakar(K)','Rajesh B(D)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','5','no','Misc','Narasimhamurthy(K.G.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9071,'43-022','Composite Industrie','B BRACKET','70103508-2-1','V251 15024 200','','A00, PV100298ST1BQ16',1,'ATA25_ACH-4128','','49194','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Hole Diameter 4.20mm/4.30mm mesures 4.45mm/4.50mm.(oversize)','Due to reamer run out in the holder. ','Next changed the holder then checked the run out by plunger dial the run out is 0.001 mm then continue the production.','Instructed operator to first time proving the first part will checked the run out of the reamer before run the tool.This message entered in the program.','CA/PA found ok.','','2016-01-12','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','Misc','Avinash(R.J.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9072,'18-457A','Magellan Aerospace Wrexham','SPAR MID OFW ','9550801','L575 51780 200 PF','','B00',2,'RM133577 Amnd 3','','49962','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','part wall thickness under size.','dia 40 facemill insert shifted during roughing program running, all pocket wall thickness under size after roughing program completing.(regular using 40 facemill)','change dia 40 facemill cutter (make by seco)& continue the production. ','dedicated one 40face mill cutter in this CRN & inform to operator cross check standard tool screw insert & insert butting area ','CA/PA found OK.','','2016-01-12','Narayanappa(G)','Siddaramappa()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','03','no','Misc','Narayanappa(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9073,'42-002','RAFAEL','PSA BASE','J20552','BA1E2001B','','38-576104_Rev-E, TILDOCS#172373_Rev-13, RE_804-1-5_Rev-11, 111.21_Rev-6, 23.36.59_Rev-F, ECN 57176 2014/08 /25; ECN 58483  2014/07/29',1,'347592024 Rel 9','','48430','','0000-00-00',NULL,'yes','no','yes','no','yes','no','no','no','no','No Go gauge answered in 4-40specification threaded holes to the full depth.','During production, ATC problem noticed between the machining cycle and without noticing the alarm. For this spindle not gripped the holder properly. So obviously run out noticed and also variation in the Z-axis. Due to this reason No Go gauge answered.','Immediately informed to machine supplier about the ATC problem. Meanwhile planned to check the tool clamping manually (For every tool change operator has to check the tool clamping manually by DE-clamping and clamping the tool holder). After ensuring the correctness, production was continued.','Machine service engineer came and rectified the problem and changed the pneumatic connector and after\r\nseveral tool changes done and not found any problem again.\r\n','CA/PA found satisfactory.','','2016-01-13','Rangaswamy()','Govindraju NR,Basavaraja S. Jr.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','9','no','VMC 70L','Rangaswamy()','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9074,'35-138','Saab AB','FLCD_DS_SUPPORT_DEFLECT_S','R8H8','423Z6189-3','BAC1534-62C','---',24,'PA 1510 FORECAST','','49961','','0000-00-00',NULL,'no','yes','yes','yes','no','no','no','no','no','Layer chip out.','This deviation is due to RM and process problem.\r\nDue to cutter load to part while outer profile program is running, material chip off will happen and we are unable to fix the process.','Planned to change the process by,\r\n1. Outer profile and holes will run with o.5mm stock in operation-01.\r\n2. Change the fixture by sufficient clamping by pressing the part by aluminum plate.\r\n3. dedicated tools for outer profile and hole making.\r\n\r\nAfter changing the new process as above parts layer is not coming out.','Changed the process as mentioned in CA and layer chipoff problem is solved. ( 1 or 2 nos out of 144 batch qty parts are getting rejected by layer chip off)\r\n','CA/PA found satisfactory and next batch found OK. ','','2016-01-13','Lohith(K)','Vishwanath Pavar,Theerthappa K.N.,Hari Prasad,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','1','no','HAASVF2SS-2','Lohith(K)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9075,'18A-087A','Magellan Aerospace Wrexham','ASSY PLATE SEALING','','D572 52914 000','','B',1,'RP135239','','A05537','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','no','Part mark overcoat missing in 01nos out of 17nos.','1)This was the human error, he is missed the overcoat.\r\n2)Same was also not noticed by the inspector.\r\n','1)Concerned personal instructed to perform the overcoat as per process sheets.\r\n2)Concerned inspector instructed to overcoat check 100% & ensure in the WO.\r\n\r\n','1)Concerned personal instructed to perform the overcoat as per process sheets.\r\n2)Concerned inspector instructed to overcoat check 100% & ensure in the WO.\r\n\r\n','CA/PA found ok.','','2016-01-14','Muniyappa(N)','Nandishkumar(D.K.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Assembly','','on site','no','Misc','Muniyappa(N)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9076,'18-209B','Magellan Aerospace(Chalfont) Limited','BODY','71976','D321 40204 202','','D, ECN NR29999ST1KM15, NR29999ST2KF65, WQN DFB09775',1,'P/078231','','48721','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Machine abuse observed on part.','Due to rubbing of tool Machine abuse has been found in Treatment house\r\n','Instructed to Production department to avoid rubbing of tool and polishing \r\n','Avoid polishing and try to finish the part  in machining stage itself.\r\n','Next parts and batches found okay.\r\n','','2016-01-17','Avinash(R.J.)','Nandishkumar(D.K.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','22132','POST DN','yes','Misc','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9077,'18-210B','Magellan Aerospace(Chalfont) Limited','BODY','6608','D321 40204 204','','D, ECN NR29999ST1KM15, NR29999ST2KF65, WQN DFB09775',5,'P/078231','','49036','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Machine abuse observed on part.','Due to rubbing of tool Machine abuse has been found in Treatment house\r\n','Instructed to Production department to avoid rubbing of tool and polishing \r\n','Avoid polishing and try to finish the part  in machining stage itself.\r\n','Next parts and batches found okay\r\n','','2016-01-17','Avinash(R.J.)','Nandishkumar(D.K.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','22237','POST DN','yes','Misc','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9078,'18-615A','Magellan Aerospace Wrexham','RECEPTACLE','421122','L575 54240 200','','A00',2,'RM132921 Amnd 1','','46273','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Bore inside charting (dia 6.00 +0.012mm). ','Dia 6.00(+0.010) bore finish done with dia3Endmill with CRC program. but part bottom side cutter chartering mark observed and so NCR was raised.\r\nAfter NCR was raised hole diameter checked by production supervisor and rework done with dia6.00 reamer. Chartering mark is not appearing in bottom side and hole diameter is also in tolerance. ( Part accepted)\r\n',' Planned to complete the Hole diameter with reamer only.\r\nChanged the program in proved program folder by taking approval by CAD.',' Planned to complete the Hole diameter with reamer only.\r\nChanged the program in proved program folder by taking approval by CAD.\r\nMPS data sheet will change and delta FAI will complete in next batch production.','CA/PA found OK.','','2016-01-18','Rangaswamy()','Gurukiran S(M)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','02','no','Misc','Rangaswamy()','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9079,'18-415B','Magellan Aerospace Bournemouth','ACTUATOR HOUSING','M723310/8205 A','D278 50163 201','','D',3,'RP408294','','49243','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Thickness under size (0.07mm to 0.1mm)','While doing the production Countersink depth is not achieving due to face out in parts.To achieving Countersink depth parts rework carried,while doing rework chattering occurred in countersink.Again tried to remove the chattering in countersink.but part thickness undersized.therefore Parts rejected.','Inform to operator to check the face out for all the parts the part.\r\nMachining is completed and checked every part by slip gauge and also ensuring by putting the rivet. ','This deviations frequently observed in previous batches and now planned to change the process.\r\n20nos taken to prove the new process in turn mill center.(Face and countersink operation will complete in one setup in Turn mill center)\r\n  \r\n','CA/PA found OK.','','2016-01-18','Lohith(K)','Dhananjaya(N)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','07','no','Misc','Lohith(K)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9080,'35-313','Saab AB','BUTTSTRAP LWR 4 EXT','451690','F575 54787 200','','A, ECN PG205027001KC72',1,'1600134622','','50108','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','Chamfer tool dig mark.','During machining with Dia 8x45 chamfer tool part was vibarted. So part out side profile digged up to 0.50mm.Due to we kept 0.3mm stock for outer after cutout that stock is not enough.','Part profile & cut out finish 1mm stock then chamfer finish. part not vibrated and found ok.','Part profile & cut out finish 1mm stock then chamfer finish. part not vibrated and found ok. Save this program.','Next part found satisfactory.','','2016-01-19','Ramesh(Poojary)','Ramesh(Poojary)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','01','no','Misc','Rangaswamy()','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9081,'35-017','Saab AB','9901503-075','666802A4','D576 50011 200','L167','A',21,'PA 1217 2015-2016','','48577','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Bend observed on part.','While production running, due to cutout thickness maintained more due to vacuum problem.machining is completed without any problem, but while parts cutout operation is carried out in fitting.Parts bend observed.\r\n','After finding the deviations checked all the parts and found ok.Rework done for bend observed parts by applying the pneumatic force by butting the flat surface.\r\n(Parts is undergoing the NDT test in treatment house as per the drawing requirements)','Part base thickness will maintained and check as per the MPS.\r\nThere is no scope of change the process or tools.\r\nOnly time required more to cut the parts after machining in fitting.\r\nNext batch will monitor and will make sure that base thickness will maintained minimum as per MPS.','CA/PA found ok.','','2016-01-19','Nagaraja (G)','Paramaeshappa ,Girish MS,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','','FI','yes','Slim-1','Nagaraj(G. Nadiger)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9082,'18-414B','Magellan Aerospace Bournemouth','ACTUATOR HOUSING','2195','D278 50163 200','','D',2,'RP408293','','46659','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','NDT Dent observed on part surface.','Due to rubbing of tool linear indications has been found in Treatment house. ','Instructed to Production department to avoid rubbing of tool and polishing ','Avoid polishing and try to finish the part  in machining stage itself.','Next parts and batches found okay','','2016-01-19','Avinash(R.J.)','Nandishkumar(D.K.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','20748','POST DN','yes','Misc','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9083,'47-017','GKN Aerospace Services Limited-Yeovil','ANGLE SUPPORT','M374880','D924 50146 205','','J, ECN NW21405ST1KA27',0,'GKN FORECAST','','49904','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Dummy NC','','','','','','2016-01-19','Rangaswamy()','Shivashankar H.G.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','With Treatment','0','FI','no','A51nx-1','Sudhagar(V)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9084,'47-017','GKN Aerospace Services Limited-Yeovil','ANGLE SUPPORT','M374880','D924 50146 205','','J, ECN NW21405ST1KA27',1,'GKN FORECAST','','49904','','0000-00-00',NULL,'no','yes','yes','no','no','yes','yes','no','no','1) Part missing.','This part machining in two setups one setup completed after fitting work again next setup machine, so this moment time part missing.','Explain to operator and fitter value of part and this type of nc not acceptable so next moment time take care.   ','Explain to operator and fitter value of part and this type of nc not acceptable so next moment time take care.','CA/PA found ok.','','2016-01-19','Rangaswamy()','Shivashankar H.G.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','0','FI','no','A51nx-1','Sudhagar(V)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9085,'18-411A','Magellan Aerospace Bournemouth','PLUNGER','237004','D321 40205 200','','H01',3,'RP413360','','49576','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','id thread nogo answered.','Due to wear out of insert these error occurred','Instructed to operator for checking tool insert wear regularly and changing insert as mentioned in board placed on machine. \r\n\r\n\r\n\r\n\r\n','Instructed to operator for following instructions noticed in the board.','CA/PA found ok.','','2016-01-20','Ravi(M)','Seetharamu D,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','7','no','DX 200-2 ','Ravi(M)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9086,'28-045','Magellan Aerospace New York  Inc.','LEVER','158529','65-51632-6','','PL_Rev - A + ADCN # 2 ; DL_Rev - N/C',1,'135212-2520','','50162','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Bore over size by 0.005micron to 0.007micron. ','In ID roughing setup running time insert will be chipped out and part will came in plus side and\r\nthat part not checking the operator and for next part he found out part will become over sized and\r\nhe change the insert and maintain the Inner dia in required size. but previous part not maintain in\r\nproper diameter. So in the finishing setup that part loading time finishing tool get the more stock\r\nand chips will be rubbed in the inner diameter and part will be over size by 0.005mm So part will\r\nbecome Rejected. ','checking the all parts outer and inner diameter before loading in the finished setup and change the\r\nprevious insert tip and .2 plus taken in the wear offset and run the part and after check the\r\ndiameter and give the proper correction and run the part and check the part found ok. and after\r\nevery 40 to 50 nos change the finished insert tip and run the part so this problem not repeated\r\nagain','In roughing setup for every part check outer and inner diameter for using air gauge. In\r\nfinishing set up every 40 to 50 ns change the finished insert tip and run the part so this problem\r\nnot repeated again.','CA/PA Found OK.','','2016-01-21','','        Seetharamu D','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9087,'35-082','Saab AB','HOUSING-SIDE ROLLER','5010901 1','F579 53065 202','ABM3-1029 T7651','B, PG52307ST4KA80',3,'160018762','','47509','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','1no. Bore oversize.\r\n2no. dig mark on part.','1)One no. bore oversize due to, operator loaded the part twice when boring operation(OS/35-082/05)is running.\r\n2)2nos dig mark due to (a)One no. due to part not butted properly in operation-01.While loading the RM in fixture,RM not butted to dia 8 pin.(b)One no. due to part not butted properly in operation-02 in fixture.','1) Informed to operators and supervisors to arrange the parts properly in working table.( Maintain the 5S).\r\n2) Informed to operators to check the butting surfaces with feeler gauges and avoid such manual errors.','All the three parts rejected due to not maintaining the operating procedures by operators and need training for all regarding the \"Cross checking methods,Arrangement of semi finish and Finish parts in working table,Communication between operators\".\r\nSupervisor will impart training regarding the above points in machine and also monitor the same. ','CA/PA found ok.','','2016-01-22','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','05','no','Misc','Krishna(Chowdary.G.P.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9088,'18-324A','Magellan Aerospace Bournemouth','BRACKET ','461768','L575 53363 200','ABM3 1029','A00',1,'RP408269','','49509','','0000-00-00',NULL,'yes','no','yes','no','yes','no','no','no','no','Part profile shift to opposite side. ','Operator selected the wrong programe. He was selected right hand(RH)progarme instead of left hand(LH).','1) Supervisors instructed to delate the progame in machine while loading next programe.','1) Operator instructed by supervisors to ensure progame is deleated while taking next programe for respective parts.','Next part found satisfactory.','','2016-01-22','Anjinamurthy(H)','S. Shiva(Kumar)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Anjinamurthy(H)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9089,'18-386A','Magellan Aerospace(Chalfont) Limited','NUT RING INNER','487664','D575 40039 200','','B',1,'P/078239','','46740','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no',' OD Thread NOGO Answerd.','while thread running time insert chip out, gauge tight. after that threading insert changed for the same part & runned same threading program without correcting in wear offset & then gauge nogo answered.','for the next part correction given in wear offset & running threading program part found Ok.','Instruction given to the operator to take +0.3 in the wear offset & then to run the threading program...','CA/PA found OK.','','2016-01-23','Dinakar(K)','Nataraja C V,Manjunath  M,Ashith B,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','QT100S-1','Narasimha Murthy(R)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9090,'35-300','Saab AB','BRACKET, INTERMEDIATE FRA','452849B','423Z1125-5-02','','---',1,'PA 1510 FORECAST-3','','49002','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Tool dig mark on part profile.','Operator not clamped the part while cutout program is running(While clamp change in between process)Dia 16 end mill cutter and holder touches the top rib and part vibrates due to insufficient clamping force.','After observed the problem, Checked the tool overhang,tool holder for any deviations in holder or tool.\r\nClamp and bolt checked for any deviations, but not find any problem.Tap in fixture is also ok.\r\nThen analyzed the problem and decided that due to clamping not done correctly(Exact force)to the part in between clamp change in the process.\r\nAfter this analysis clamping force cross checked and continued production. ','This deviation is due to manual mistake, all the process related parameters are checked( like clamp condition, bolt condition, Tap in fixture, Allen key)not find any problem for this rejection.\r\nInformed to operator to check the clamp tightness twice and ensure before running the program.\r\nNext all the parts which is machined are cross checked by supervisor and all the parts are found ok.','CA/PA found ok.','','2016-01-25','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Rangaswamy()','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9091,'35-282','Saab AB','GUIDE HARNESS LWR','599463','423Z1982-1','','---',1,'PA 1510 FORECAST-3','','49585','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Dig mark on part.','While running production of 35-282 part, in operation 02 operator are doing a manual tool loading due to machine tool magazine problem.\r\nWhile entering the tool offset value in machine operator changed the tool value, But program not selected as per the tool loaded in machine.therefore dig mark observed on part.\r\n(There is a wrong selection of program)\r\n\r\nwrong program run dia8 flat instead of 12r3   ','Informed to operator to check the tool value,program name twice in such cases.\r\nThe tool magazine problem is investigating the causes for (ATC) failure by machine supplier.','All the other qty which is in the batch is completed. and operator taken care and checked the tool offset and program selection twice before starting the machine.\r\n\r\nSame will continue in next part which is loaded on machine.\r\nFollowing with machine supplier to solve the ATC problem ASAP.\r\n','CA/PA Found OK.','','2016-01-25','Rangaswamy()','        Govindraju NR','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9092,'35-233A','Saab AB','HINGE BRACKET 5 ','3858901','D576 50008 208','','D00',1,'1600118541','','50281','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Tool dig mark on rib top.(wrong program edit)','Dummy','Dummy','Dummy','DUMMY.','','2016-01-29','Rangaswamy()','Mahesh(N)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','05','no','Misc','Rangaswamy()','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9093,'18-109A','Magellan Aerospace Bournemouth','NUT','K10011','D575 40498 200','S80 FHT','D01',2,'RP408154','','48808','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','NDT FAIL','Due to rubbing of tool or material behaviour NDT failure has been found in Treatment house\r\n','Instructed to Production  & fitting department to avoid rubbing of tool and polishing \r\n','Avoid polishing and try to finish the part  in machining stage itself.\r\n','Next parts and batches found okay\r\n','','2016-01-29','Avinash(R.J.)','Nandishkumar(D.K.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','21980','POST DN','no','Misc','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9094,'18-114A','Magellan Aerospace Bournemouth','NUT','238300','D575 40499 200','S80 FHT','D01',1,'RP408154','','48810','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','NDT FAIL','Due to rubbing of tool or material behavior NDT failure has been found in Treatment house\r\n\r\n','Instructed to Production  & fitting department to avoid rubbing of tool and polishing \r\n\r\n','Avoid polishing and try to finish the part  in machining stage itself.\r\n','Next parts and batches found okay\r\n','','2016-01-29','Avinash(R.J.)','Nandishkumar(D.K.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','22201','POST DN','no','Misc','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9095,'35-170','Saab AB','ALCD_STRUCT_SUPPORT-FTG_L','453566-2','423Z1200-11-01','','---',1,'PA 1510 FORECAST','','49464','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Charting observed on bore and bore over size 0.010mm.','While doing boring operation this deviation coming due to chips locking in boring bar tip','1.Chips cleaned with air and continued production. \r\n2.Informed to operator to check the chips at every cycle to avoid this problem','1.Informed to operator to check the chips at every cycle to avoid this problem. \r\n2. Optional stop M-code entered in program and message entered in program to clean the chips for every part.','CAPA Found Ok','','2016-01-29','Girish(Prasad P)','Eranna(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','07','no','Misc','Rangaswamy()','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9096,'35-170','Saab AB','ALCD_STRUCT_SUPPORT-FTG_L','453566-2','423Z1200-11-01','','---',1,'PA 1510 FORECAST','','49465','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','*Base thickness under size.','*Deviation due dia 10ballnose cutter broken and dig mark observed.\r\nTried to clear the dig mark, but base thickness measures minus side.','* New tool placed and program runned with 1mm up in Z-axis to reduce the material removal.\r\ntime increased but material removal is smooth and continued production.\r\ninformed to CAD to reduce the DOC and avoid load for cutter.','New program done to reduce the cutter load and new program is saved with revision no. in proved program folder.\r\n','CAPA FOUND OKEY','','2016-01-29','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','05','no','Misc','Rangaswamy()','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9097,'35-233A','Saab AB','HINGE BRACKET 5 ','3858901','D576 50008 208','','D00',1,'1600118541','','50281','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Tool dig mark','While doing slotting operation operator not entered the correct Mirror  in machine.','Mirror corrected and continued production, next part check and found the all thickness as per drawing requirements.','Training conducted to (Mr. mahesh) to enter the Mirror in machine. and observed for 2 days of\r\nproduction done on machine. Now he have understand and entered the Mirror for all the parts. ','Next part found ok.','','2016-01-29','Rangaswamy()','        Mahesh N','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9098,'28-003A','Magellan Aerospace New York  Inc.','PIN-ATTACHMENT WALKING BE','G22134K01','161A7305-1','','PL-Rev-NC, DL Rev-B',1,'132019','','49370','','0000-00-00',NULL,'yes','yes','yes','','','','','','no','Tool dig mark noticed on the hole and extra material removed and it looks like round slot.','During machining, Clamping bolt broken which leads to tool over travelled and took extra material cut.','Informed to concerned personal and this is rare case happened. just informed and rejected the part.','1) We will segregate the damaged clamping bolts and we will monitoring every month.\r\n2) If any bolts start to broken then immediately replaced by new bolts.\r\n','CA/PA found satisfactory.','','2016-01-29','Anjinamurthy(H)','        Punith G S','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9099,'35-183B','Saab AB','EDGE HOUSING','626089','423Z1121-6-02','','--B',1,'PA 1510 FORECAST','','48395','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','yes','Chf Tool dig mark in profile','Program problem.','Program changed and run the part.','Before running the chf program we cross check the program by simulation software and transfer the program to production.','CA/PA FOUND OK.   ','','2016-01-29','Ramesh(Poojary)','Ramesh(Poojary)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','09','no','Misc','Rangaswamy()','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9100,'35-183B','Saab AB','EDGE HOUSING','626088','423Z1121-6-02','','--B',1,'PA 1510 FORECAST','','47682','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','3D profile face not clear. tool dig mark.','Tool dig mark observed on part face due to part lift from vice.\r\nThis deviation coming while process changed to reduce the part bend to get profile points consistently as per drawing requirements.\r\nWhen rough machining in operation-05, 40mm DOC high-machining program done for FAI part and also 03nos first batch production done with same program.\r\nBut second batch of new process 40mm DOC is not taking in machine(VF2SS-3)immediately we checked the tool, tool holder and machine spindle run out.all the parameters are ok.\r\n','Rough machining DOC changed from 40mm to 20mm and observed the spindle load and noise.\r\n \r\nProduction monitored this batch and all the parts are ok.','The above CA  taken in existing batch and as per changes new program added in MPS datasheet.\r\n\r\nWe also observe the machining in next batch production.','CA/PA found ok.','','2016-01-29','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','09','no','Misc','Rangaswamy()','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9101,'18-210B','Magellan Aerospace Bournemouth','BODY','0246','D321 40204 204','','D, ECN NR29999ST1KM15, NR29999ST2KF65, WQN DFB09775',1,'RP413360','','50250','','0000-00-00',NULL,'yes','yes','yes','','','','','','','od undersize (-1.2mm).','setting time offset not taken correctly and run the part od undersize.','Re offset taken,  and  taken + in wear offset and runned the part. and part checked and proper correction given in wear offset and run the part. part checked found ok ','Informed to operators that to take offset correctly and cross check the diameter... ','Next Parts found okay in Production ','','2016-01-30','Dinakar(K)','        Dinakar K','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9102,'18-210B','Magellan Aerospace Bournemouth','BODY','0246','D321 40204 204','','D, ECN NR29999ST1KM15, NR29999ST2KF65, WQN DFB09775',1,'RP413360','','50249','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','total length undersize by -0.5mm.','Operator error not set the zero in micrometer before checking the part.','Before checking the parts set the zero in micrometer & cross checked by master pin reading is correct & next parts found OK & continued to production.','Inform to operator first check the instrument correct set as zero & cross checked master pin gauge then after check the parts to continuing production.\r\n\r\n','CA/PA found OK.','','2016-01-31','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Sandhesh D(S)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9103,'28-006A','Magellan Aerospace New York  Inc.','SHOULDER BOLT ','574049','162A3109 -2','',' 	PL Iss A, PSDL Iss A, ECN C141079',1,'132973-3174','','50351','','0000-00-00',NULL,'yes','yes','yes','','','','','','','center drill over depth over size.','with out checking the center drill run the part.so center depth will over size.','we are add the depth of center drill will be added in the \r\nprocess sheet.','we are add the depth of center drill will be added in the \r\nprocess sheet.and given the instruction to the operator.','Next batch found ok.','','2016-02-01','','        Dinakar K','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9104,'35-157A','Saab AB','INTERCOSTAL_VENT','599461','423Z1172-3-01','','---',3,'PA 1510 FORECAST','','47914','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1 part flatness not achived,required 0.4 mm measured above 0.8 mm.2 parts bend removing time side wal bend.','This deviation find out after all the production batch is completed.\r\nDue to bend observed after operation-02 parts are getting rejected.\r\nWhen roughing operation running due to cutter load this deviation is coming.','Next batch cutter load monitored and checked the tool tip regularly when batch production is running.\r\nReduced the depth of cut for roughing tool.\r\nFlatness 100% inspection carried when production is running.\r\nWO no.49857, 49858 & 50373 total 78 nos production done with above CA and all the parts are accepted.\r\n','The above CA are taken and same will followed in future batches.','CA/PA found ok.','','2016-02-01','Krishna(Chowdary.G.P.)','Rangaswamy()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','Misc','Nagendra(SN)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9105,'35-195','Saab AB','SUPPORT SEAL RETAINER','556560','423Z1834-2-01','','---',1,'PA 1510 FORECAST-3','','50629','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Dig mark on part.','Part dig mark due to Z-axis done when power trips.\r\n\r\nWhen dia8flat cutter running in grove due to UPS problem power trips and machine Z-axis done by 0.6 to 0.8mm.','This deviation found in machine and cause for Z-axis down is not find at the movement,\r\nImmediately informed to machine supplier regarding the problem. ','Route cause for Z-axis done is due to Air contactor problem. This found when diagnose the problem.\r\nNew contactor  fitted and check the Z-axis down and find Ok.\r\n\r\nAfter ensuring as per above Preventive action, production continued.','CA/PA FOUND OK.','','2016-02-02','','        Manohara M','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9106,'47-008','GKN Aerospace Services Limited-Yeovil','PLATE JOINT','573050A2','D574 55150 203','','B, ECN GN150294ST1KA06',1,'GKN FORECAST','','50154','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Part outer profile tool dig mark.','While running operation-03, dia 8flat cutter broken. this causes dig mark on part.','New tool placed and next part continued, same outer wall thickness checked and taken approval from QAD.(first-off done for next part)','Cutter breakage is due to tool cutting edge blunted, therefore informed to tool manager and production supervisor to check the tool tip before loading the tool to machine.','CA/PA Found OK.','','2016-02-02','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Rangaswamy()','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9107,'35-166A','Saab AB','HOUSING PIN','459434B','423Z1124-6-01','','--A',1,'PA 1510 FORECAST','','46831','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dia 3.2 drilling hole shifted.','While doing Manual drilling operation,Part not butted to Jig face properly due to locating pin not guided properly.Fitter not observed the butting.\r\nThis error causes the above deviation. ','After finding the deviation in first part, supervisor involved to find out the root cause and find the above root cause.\r\nFitter done next part loading and same is cross checked by supervisor and after ensuring the part butting to Jig continued production.(Again First part inspection done and taken approval from QAD)','Drilling operation is carried in drill Jig with top clamp and process was proved, but this type of error find out in this batch.\r\nAgain to eliminate such error part butting is to be ensure by fitters using feeler gauge.\r\nProcess sketch(Instruction Photos) is displayed in fitting area to get awareness for all the fitters.','Next part found ok.','','2016-02-02','Nagaraju(T)','Raghu(A.N.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','15','no','Misc','Rangaswamy()','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9108,'28-006A','Magellan Aerospace New York  Inc.','SHOULDER BOLT ','574049','162A3109 -2','',' 	PL Iss A, PSDL Iss A, ECN C141079',1,'130775','','50350','','0000-00-00',NULL,'yes','yes','yes','','','','','','','OD Under size by -0.02mm','It is happened due to insert problem.New insert loaded but operator was not cross checked whether insert properly eatted or not.','For next piece supervisor loaded the insert properly & cross checked dimension for several components and found within\r\ntolerance.  ','Proper training given to the operators regarding the\r\nabove NC.','Next Parts found okay in Production ','','2016-02-03','Dinakar(K)','        Seetharamu D','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9109,'18-644A','Magellan Aerospace Wrexham','DOOR OUTER TYPE 23 ','7699903','L572 53721 200 PF','','B',1,'RP141267','','50283','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Base thickness under size.','Due to twist and Bend in part after operation-01, base thick measures 0.3 mm minus locally.( outer most in Y-axis).\r\nWhen base finishing operation is carried in operation 05, due to part not clamped properly (part not butted in vacuum)part thickness measures minus side.','After finding the deviation in part, new bolting introduced to clamp the part properly to maintain the thickness as per requirement.\r\nafter introducing the bolts at front and back side in y-axis, part butting improved and all the remaining parts thickness measures with in limit. ','New bolting method improved in process and if find any twist and bend in part after op-01, Parts thickness will not very due to mechanical clamping is also there with vacuum clamping.','CA/PA found ok.','','2016-02-03','Rangaswamy()','Rangaswamy()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','03','no','Misc','Rangaswamy()','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9110,'18-003A','Magellan Aerospace Wrexham','BRACKET SUPPORT','5866801 6','D361 50111 200','ABM3 1029 T7651','A',8,'RP135242','','46700','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Corosion Pits observed.','Due to rubbing of tool or material behavior Corrosion Pits  has been observed  in Treatment house','Apply PX-24 after machining, and polishing and rubbing of tool should be avoided','Apply of PX-24 is mandatory before sending the parts to treatment house.','Next parts and batches found okay','','2016-02-03','Avinash(R.J.)','Nandishkumar(D.K.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','20635','POST DN','no','Misc','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9111,'18-078A','Magellan Aerospace Wrexham','ADAPTOR ','19743493-C','A282 50081 200','','A',1,'RP135273','','50053','','0000-00-00',NULL,'yes','yes','yes','','','','','','','TOOL DIG MARK,','While part spot face rework time tool dig on outer diameter.','Inform to operator every part loading time check the  rib thickness.(3.8mm).\r\nInform to turning operator, turning operation doing time maintain the thickness in men-value.   ','Inform to operator every part loading time check the  rib thickness.(3.8mm).\r\nInform to turning operator, turning operation doing time maintain the thickness in men-value.   ','CA/PA found OK.','','2016-02-04','Lohith(K)','        Dhananjaya N','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9112,'28-045','Magellan Aerospace New York  Inc.','LEVER','158529','65-51632-6','','PL_Rev - A + ADCN # 2 ; DL_Rev - N/C',2,'135212-2520','','50162','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Bore over size by 0.005micron to 0.007micron.','In ID roughing setup running time insert will be chipped out and part will came in plus side and\r\nthat part not checking the operator and for next part he found out part will become over sized and\r\nhe change the insert and maintain the Inner dia in required size. but previous part not maintain in\r\nproper diameter. So in the finishing setup that part loading time finishing tool get the more stock\r\nand chips will be rubbed in the inner diameter and part will be over size by 0.005mm So part will\r\nbecome Rejected. ','checking the all parts outer and inner diameter before loading in the finished setup and change the\r\nprevious insert tip and .2 plus taken in the wear offset and run the part and after check the\r\ndiameter and give the proper correction and run the part and check the part found ok. and after\r\nevery 40 to 50 nos change the finished insert tip and run the part so this problem not repeated\r\nagain. ','In roughing setup for every part check outer and inner diameter for using air gauge. In\r\nfinishing set up every 40 to 50 ns change the finished insert tip and run the part so this problem\r\nnot repeated again. ','CA/PA Found OK.','','2016-02-04','Dinakar(K)','Nataraja C V,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','9','no','QT100S-1','Ravi(M)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9113,'18-382A','Magellan Aerospace(Chalfont) Limited','SLEEVE BEARING ','A12138','D575 40037 200','','A',1,'P/078238','','50635','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','running time powertrip id thread digmark.','running time powertrip','running time powertrip','running time powertrip','Next Parts found okay in Production ','','2016-02-06','Sandhesh D(S)','Vasu(SN)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','05','no','Misc','Sandhesh D(S)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9114,'18-295A','Magellan Aerospace Bournemouth','BOLT','242096','D577 56145 200','S80','A',1,'RP408165','','50291','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','OD thread undersize in 0.008 to 0.012 & gauge nogo answered.','This occurrence due to changing the insert that time correction not done OD undersize & thread gauge no go answered.  \r\n\r\n ','Immediate attack to Supervisor correct the offset to run the  part & part found OK & inform to operator as per the same method.','Informed to operators to check the insert regularly and\r\nwhen insert changes two passes to be make with stock to\r\ncheck the gauge. ','CA/PA found OK.','','2016-02-06','Ravi(M)','Ravi(M)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','07','no','Misc','Ravi(M)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9115,'18-382A','Magellan Aerospace(Chalfont) Limited','SLEEVE BEARING ','A12138','D575 40037 200','','A',1,'P/078238','','50635','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Id ovality.','id finish running time 3 washer will tight in part 1 washer will loose so part was rotate so id ovality occured.','Next part tightening pressure was more and run the part found ok.','instruction given to operator before running part check the tightening after running the part.','CA/PA found OK.','','2016-02-07','','        Nataraja C V','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9116,'35-246','Saab AB','WASHER LARGE','G21273K05','423Z1458-1','','--B',1,'PA 1510 FORECAST-2','','50582','','0000-00-00',NULL,'yes','no','yes','no','yes','no','no','no','no','Thickness minus 0.7 mm.','While machine running time \"Z\" axis down.So part was rejected.','Immediately stop the machine, Check the tool offset and work offset,After inform the machine suppliers. check the problem    machine condition is okay.\r\nHolder pull stud damaged, pull stud change after continue the production.      ','Inform to operator every day one time check all holder full stud,after continue the production.\r\nRunning time any deviation observed check the all procedure  in compulsory. ','CA/PA FOUND OK.','','2016-02-07','Lohith(K)','Lohith K,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','3','no','VM2-3','Lohith(K)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9117,'18-382A','Magellan Aerospace(Chalfont) Limited','SLEEVE BEARING ','A12138','D575 40037 200','','A',1,'P/078238','','50635','','2016-02-08',NULL,'yes','yes','yes','no','no','no','no','no','no','part wrong clamping so one extra hole done  ','The jig is used to drill the part. After clamping the part to the jig the part is twisted 22.5 Degree angle and then hole is drilled. 2 holes gets drilled at a time. The operator has twisted the part to in wider angler than 22.5 Degree. Hence one Additional hole is drilled','The operator is trained to use only one slot option in the jig as against more number of slots in the existing Jigs.','The jigs are made such that the operator cannot use more than one slot in a Jig. ','CA/PA found OK.','','2016-02-08','Nagaraju(T)','Yogeesha(R)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','08','no','Misc','Nagaraju(T)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9118,'18-210B','Magellan Aerospace Bournemouth','BODY','6608','D321 40204 204','','D, ECN NR29999ST1KM15, NR29999ST2KF65, WQN DFB09775',1,'RP413360','','50246','','0000-00-00',NULL,'yes','','yes','','yes','','','','','Bore over size (0.12mm).','While part running \"X\" axis 0.12mm shifted so part was rejected. This error happen machine ball screw damaged so machine X axis not going to the program homing.  ','Immediately stop the machine, inform to machine suppliers, check the X axis condition after continue the production. \r\nInform the operator every part boring operation completed  check the bore finishing dimension. Next part all dimension  okay.\r\n  ','Immediately stop the machine, inform to machine suppliers, check the X axis condition after continue the production. \r\nInform the operator every part boring operation completed  check the bore finishing dimension. Next part all dimension  okay.\r\n  ','Next part found ok.','','2016-02-08','Lohith(K)','        Ravi R','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9119,'18-075A','Magellan Aerospace Wrexham','ADAPTOR ','21823476','D282 50044 200','','A',1,'RP135273','','50597','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Bore diameter over sized.','Due to ID running time chips clogged & not removed so ID over sized.  ','Instructed operator to every ID operation remove the chips before the run the part. ','Instructed operator to every ID operation remove the  chips & ensure before the run the tool.','CA/PA found OK.','','2016-02-08','Sandhesh D(S)','Sandhesh D(S)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','01','no','Misc','Sandhesh D(S)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9120,'35-193','Saab AB','INTERCOSTAL CAM HOUSING','453566-2','423Z1190-1-01','','---',1,'PA 1510 FORECAST-2','','50513','','0000-00-00',NULL,'yes','yes','yes','','','no','','','no','Part base thickness under size in taper 0.1','Part not butted properly due to chips so part base thickness under size at 50mm distance (0.1 under size )','Before loading part & fixture faces will be cleaned properly, after loading the part cross checking will be done by the feeler gauge and operator will cross check by visually.','Before loading part & fixture faces will be cleaned properly, after loading the part will cross checking the feeler gauge & visually.\r\ninstruction given to the operator to check the all part butting properly before running the program.','Next batch found ok.','','2016-02-08','Narayanappa(G)','        Manjunatha N.R.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9121,'35-193','Saab AB','INTERCOSTAL CAM HOUSING','453566-2','423Z1190-1-01','','---',1,'PA 1510 FORECAST-2','','50513','','0000-00-00',NULL,'','','yes','','','','','','','part base thickness under size in taper 0.1\r\nRefer NC NO-09120, This NC Is Dummy','Refer NC NO-09120, This NC Is Dummy','Refer NC NO-09120, This NC Is Dummy','Refer NC NO-09120, This NC Is Dummy','Refer NC NO-09120, This NC Is Dummy.','','2016-02-08','','                        Manjunatha N.R.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9122,'18-382A','Magellan Aerospace(Chalfont) Limited','SLEEVE BEARING ','A12138','D575 40037 200','','A',1,'P/078238','','50635','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no',' Dummy','Dummy','Dummy','Dummy','Dummy.','','2016-02-08','Sandhesh D(S)','Vasu(SN)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','05','no','Misc','Sandhesh D(S)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9123,'18-295A','Magellan Aerospace Bournemouth','BOLT','242096','D577 56145 200','S80','A',1,'RP408165','','50291','','0000-00-00',NULL,'yes','no','no','no','no','yes','no','yes','no','THREAD LOCK.','while gauge checking time gauge was strucked inside the thread so using the C clamp to removing the\r\nthread gauge that time part was breakdown. ','Next every part checking by using the pitch micrometer and run the part. ','For the first part we are using the pitch micrometer to check the part and next every part using\r\nthread ring gauge to checking the part. next every batch we are check the part inside the machine by\r\nusing pitch micrometer and then remove the part. ','Next part found okay. ','','2016-02-09','Nandishkumar(D.K.)','Narasimha Murthy(R)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','09','no','Misc','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9124,'35-166A','Saab AB','HOUSING PIN','459433A','423Z1124-6-01','','--A',1,'PA 1510 FORECAST','','46835','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','After shot peening KC Profile points not achieved.','After short peening part is expand and compass so KC profile  out of tolerance. ','Reduce the intensity for the drawing requirement and continue the process.','Reduce the intensity for the drawing requirement and continue the process.','Next part check found ok. ','','2016-02-10','Yashawantha(NH)','Nagendra(SN)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','22134','Post DN','no','Misc','Nagendra(SN)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9125,'34-017B','Magellan Aerospace Winnipeg','MOUNTING LUG-GEARBOX','H2542','400-12608-2 -905','','EM105092 Iss F, EM104302 Iss A, EM104765 Iss G, EM106399 Iss B, EM106400 Iss B, EM106401 Iss A, EM106404 Iss A, EM106522 Iss A, EM106602 Iss A',1,'B91379 Rev.026','','49945','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Thickness undersize (-0.15mm)','Operator part not butted properly.','Part butting area cleaning properly using with air pressure & ensure the clean area & clamping the part.','Instruction given to operator to butt the job properly during butting and clamping the part.','CA/PA found OK.','','2016-02-10','Ravi(M)','GUNDEGOWDA(H.G.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','07','no','Misc','Ravi(M)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9126,'35-183B','Saab AB','EDGE HOUSING','626089','423Z1121-6-02','','--B',1,'PA 1510 FORECAST','','47683','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','yes','Base thickness pluse side 0.2mm.','While running operation-09, base  finishing not done. This deviation is due to program\r\nskipped when power failure.Operator not checked the sequence of programs which is already completed\r\nand from which program has to start after power failure. 0.2mm stock is measured and while\r\nchecking the part in stage operator find out this deviation and rework NCR was raised. ','Informed to operator to check the programs sequence when power failure and write done in program\r\nname in machine reference book and once restart the machine after power failure,Operator has to\r\nensure twice with the reference book.(sequence of programs) This will monitor by supervisor and\r\nmandaterlly operators has to write the sequence of programs when power failure. ','Informed to operator to check the programs sequence when power failure and write done in program\r\nname in machine reference book and once restart the machine after power failure,Operator has to\r\nensure twice with the reference book.(sequence of programs)','CA/PA FOUND OK.','','2016-02-10','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','','09','yes','Misc','Rangaswamy()','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9127,'18-044B','Magellan Aerospace Bournemouth','ANGLE ATCH RSPAR UPR','3481901','L575 52440 200','','A00',1,'RP408128 Amnd 01','','50826','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dia 4mm hole 1mm shift.','this has happened due to wrong interpretation of the operator in the drawing ','Operator corrected for the next part and found okay with other parts ','Instructed operator to check twice before making drilling operation, and ensure with drawing','Next part found ok.','','2016-02-10','Krishna(Chowdary.G.P.)','Jayarama(M.B.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','09','no','Misc','Anjinamurthy(H)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9128,'18-418A','Magellan Aerospace(Blackpool) Limited','BRACKET','221825','PI55-2119010-00','','NIL',1,'P/501836','','49180','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','HOLE DIAMETER 4.88/4.92MM MESURES 5.08MM.','After checking the part in FI this was noticed.\r\n\r\nDue to dia 4-flat cutter run out,while doing interpolation for finish the dia 4.88/4.92mm hole deviation observed in half of the depth in 3mm thickness.\r\n','Immediately checked all the which is in inspection and all holes diameters are found ok.\r\n\r\nreason for this deviation is only due to runout. this was corrected in next batch production of WO no 49178 & 49179.','Informed to all the operators to check the run out for any critical dimensions maintaining.\r\n\r\n and also ensured that all the holders, collects are maintain properly to avoid any UN-measured errors.\r\n','Next batch found ok.','','2016-02-15','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','FI','no','Misc','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9129,'18-318A','Magellan Aerospace Bournemouth','HALF CLAMP','18010107-A','D574 50551 200','DTD 5014','B01',1,'RP408269','','49913','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Hole positiion out of  0.08mm to 0.1mm','While first part running hole shifted so part was rejected.','Inform to operator every time first part running do the under size drill `check the hole position, after finish the hole diameter.','Inform to operator every time first part running do the under size drill `check the hole position, after finish the hole diameter.','CA/PA found ok.','','2016-02-15','Lohith(K)','Lohith K,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','5','no','VM2-3','Lohith(K)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9130,'18-008A','Magellan Aerospace Wrexham','Plate Cover','497610','D572 52518 200','L97 T351','A',1,'RP135247','','50908','','0000-00-00',NULL,'yes','yes','yes','','','','','','','part reversed when M00 came but reset the program and run from starting program so drilling opn done in both side so part reject.','In this operation after turning and drilling operation M00 will come and reverse the part for facing and chamfer operation part reversed when M00 came but reset the program and run the program again turning and drilling instead of facing and chamfer.so both side drilling operation done so part reject.\r\n','For next part, part reversed and not reset the program and run the facing and chamfer program(next opn).','Instruction given to operator to follow the messages given in the program and run the program as per essage and where M00 came check the part and program before run the part. ','Next Parts found okay in Production ','','2016-02-16','Dinakar(K)','        SHIVAKUMAR ','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9131,'35-025','Saab AB','7605125-201','743117A4','L574 55125 201','ABM3 1029','A00',1,'1600087350 Rev 1 ','','36475','','0000-00-00',NULL,'no','no','no','no','no','yes','yes','yes','no','As pre drawing requirement only primer but they did topcoat. ','We have Inform to supplier for stop the process.  ','We raise the supplier NCR. ','Change the supplier.','New rework order to be raise.','','2016-02-17','Yashawantha(NH)','Yashawantha(NH)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','15843','Post DN','yes','Misc','Nagendra(SN)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9132,'35-166B','Saab AB','HOUSING PIN ','927838B','423Z1124-6-01','','--B',1,'PA 1510 FORECAST','','50666','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','*part dig mark.\r\n','*Wrong program selection causes rejection. Operation 05 program called in operation-04 setup.\r\nWhile doing operation-04, 01 number rework observed.Rework part kept as it is and started operation-05 in same shift(night shift).\r\nNext day supervisor analyzed the rework part and informed the operator to completed the rework.then above manual error done by operator\r\nOperator changes the setting from op-05 to op-04, but same program which is running in machine is activated and started machining.this error causes the dig mark on part.','This is due to operator negligence and supervisor need to proactive and check the process.\r\n\r\nSupervisor will check and ensure before doing such reworks/changes in process.\r\n\r\nInformed to operator to understand the process and cross check once before doing any rework and also take approval from supervisor.','Operator responsibility as per Appendix-04 explained once again and test conducted after 2 week of training.\r\n\r\nall the operators are follows as per Appendix-04.','CA/PA FOUND OK.','','2016-02-17','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','00','no','Misc','Anjinamurthy(H)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9133,'18-003A','Magellan Aerospace Wrexham','BRACKET SUPPORT','2808701-3','D361 50111 200','ABM3 1029 T7651','A',1,'RP135242','','49397','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Corrosion Pits observed on part','Due to rubbing of tool or material behavior Corrosion Pits  has been observed  in Treatment house\r\n','Apply PX-24 after machining, and polishing and rubbing of tool should be avoided\r\n','Apply of PX-24 is mandatory before sending the parts to treatment house.\r\n','Next parts and batches found okay\r\n','','2016-02-17','Avinash(R.J.)','Nandishkumar(D.K.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','22755','POST DN','no','Misc','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9134,'35-228A','Saab AB','HINGE BRACKET 2 ','3859901','D576 50005 205','','D00',1,'1600115959','','50990','','0000-00-00',NULL,'yes','yes','yes','','','','','','','part wall dig mark.','operator part handling problem so part wall dig mark observed.','Instruct to operator to part handling and loading time take care. ','Instruct to operator to part handling and loading time take care.','CA/PA FOUND OK.','','2016-02-18','Girish(Prasad P)','        Subramanya L Naik','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9135,'35-228A','Saab AB','HINGE BRACKET 2 ','3859901','D576 50005 205','','D00',3,'1600115959','','50990','','0000-00-00',NULL,'yes','yes','yes','','','','','','','outer profile under size by 0.5MM.','while doing the 1st operation,fixture was tilted due to clamping bolt was broken so outer profile of the part was under sized.','change the fixture clamping bolt,reset and run the 1st operation set up,next part found within the specification. ','Before doing this 1 set up  i will ensure the fixture,bolt and other clamping tools are useable and same i will pass this information to operators.','CA/PA Found Ok','','2016-02-19','','        Sundar D.K.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9136,'35-149','Saab AB','CED_BS_HINGE_FTG-AFT','456869C','425Z0311-8','7050 - T7451 ALUMINU','--A',1,'PA 1510 FORECAST','','50620','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','bore diameter 17.462+0.018 over size 0.12mm','1)Bore is finished by using end mill and operator has to give the CRC value, during this operator entered the wrong value.','1)Next part was finished by giving the correct CRC value with supervision of supervisors by the same operator.','Reamer is planned to replace the end mill.target date:01/4/2015','Effectivness will be monitered once they replace endmill by reamer.','','2016-02-21','Girish(Prasad P)','ERANNA(KAYAKAD)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Girish(Prasad P)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9137,'35-275','Saab AB','PIN','G21482K01','426Z3601-1','','--A',3,'PA 1510 FORECAST-3','','48570','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no',' \"These parts sent for treatments for Saab Audit purposes only and not to be mounted on Aircraft. These shall be scrapped after the Saab Audit.\" ','This part was sent to ATPL for trials and is scrapped ','This part was sent to ATPL for trials and is scrapped ','This part was sent to ATPL for trials and is scrapped ','This part was sent to ATPL for trials and is scrapped ','','2016-02-23','Yashawantha(NH)','Yashawantha(NH)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','21400','Post DN','no','Misc','Nagendra(SN)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9138,'18-560A','Magellan Aerospace Wrexham','SPAR INBOARD OFW','445814A','L575 51779 200','','B00',1,'RM132919 Amnd 1','','51040','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Out side verticale flange 2.00+0.20/-0.1mm measures minus side by 0.50mm.','In second setup there are two locating holes of dia8.00 and 6.00mm and part has to be located with these holes using locating pin. But operator missed to loacte the part in the dia6.00mm hole. So part lifted and tool took more materail.','In 2nd setup dia 8 and dia 6 pin for part location, then dia 6.5drill for part clamping hole.this clamping hole done in 1st setup.  ','Clamping hole to be done in 1st setup. In this case if operator missed to locate the locating hole then hole not matched. This will be evidenced by eye sight.\r\n\r\n','CA/PA found satisfactory.','','2016-02-23','Rangaswamy()','Rangaswamy()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Rangaswamy()','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9139,'18-209B','Magellan Aerospace Bournemouth','BODY','M486350','D321 40204 202','','D, ECN NR29999ST1KM15, NR29999ST2KF65, WQN DFB09775',1,'RP413360','','50128','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Double thread in the part\r\n\r\n\r\n\r\n\r\n\r\n','Thread gauge not butted so in wear offset -.3 taken and run the part so double thread formed in the part and thread gauge NOGO answered','Change the Z lenght in program and offset taken and run the part.and part checked found ok.','Change the Z lenght in program and offset taken and run the part.and part checked found ok.','Next Parts found okay in Production ','','2016-02-24','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','07','no','Misc','Dinakar(K)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9140,'18-117B','Magellan Aerospace Bournemouth','HOUSING-OUT BD BRG','A12618','D275 40004 200','','C01',1,'RP408156','','50943','','0000-00-00',NULL,'','','yes','','','','','','','thred geauge no go answered','While running the production threading insert will be chip out and thread gauge was not answered so change the insert corner and taken plus side in wear offset and give the proper correction and run the part, for that part thread gauge was answered but gauge was not butted so for the same part operator will moves 0.1 minous side and run the part so double thread occured in the part and pitch was changed and thread NOGO answerad so part was rejected.  ','Load the next part and taken the X and Z offset again. and taken safer side and give the proper correction and run the part ','Instruction given to the operator to If any cause onece run the threading dnt move in the Z offset and about threading operations. ','Next batch found okay.','','2016-02-24','','        Dinakar K','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9141,'35-149','Saab AB','CED_BS_HINGE_FTG-AFT','456869C','425Z0311-8','7050 - T7451 ALUMINU','--A',1,'PA 1510 FORECAST','','50620','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Refer nc no:9136','Refer nc no:9136','Refer nc no:9136','Refer nc no:9136	','Refer nc no:9136','','2016-02-24','Girish(Prasad P)','ERANNA(KAYAKAD)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Girish(Prasad P)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9142,'18-412A','Magellan Aerospace Bournemouth','ROD END','A13598','D321 53012 200','','F01',3,'RP413360','','50192','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','PROFILE OUT, ','Tool Direction not given in geometry offset.','Tool Direction given in geometry offset and run the part part fund okay and continue the production.','Instruction given the operators whenever the setting before running the program cross check the given in tool direction and nose radius in geometry offset and wear offset.','Next batch found okay in production.','','2016-02-25','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','01','no','Misc','Dinakar(K)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9143,'18-121A','Magellan Aerospace Bournemouth','BARREL - STRUT','A0563X','D572 50463 201','S98 FHT','F',1,'RP408147','','50976','','0000-00-00',NULL,'yes','yes','yes','','','','','','','part running time 4.9 drill broken for no go  pin answer so part reject','','','','Parts accepted.','','2016-02-26','','        Girish HP','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9144,'18-341A','Magellan Aerospace Bournemouth','LANDING TOP PANNEL','A637658','F574 50966 200 01','','E, ECN PG49998ST1TV38',2,'RP408276','','50005','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Deep lines observed on part surface.','Scratch mark moticed on the part which leads to fail the NDT','Informed to concerned department to take care during transit and packing.','Dedicated trays arranged for each family parts to avoaid the scratch and other FOD. ','Next batch found satisfactory.','','2016-02-27','Avinash(R.J.)','Nandishkumar(D.K.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','23012','POST DN','no','Misc','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9145,'35-229A','Saab AB','HINGE BRACKET 3','7599601','D576 50006 204','','D00',1,'1600108781','','45479','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Part send to ATPL for trail.','This part was sent to ATPL for trials and is scrapped','This part was sent to ATPL for trials and is scrapped','This part was sent to ATPL for trials and is scrapped','This part was sent to ATPL for trials and is scrapped','','2016-03-01','Yashawantha(NH)','Yashawantha(NH)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','21077','Post DN','no','Misc','Yashawantha(NH)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9146,'35-195','Saab AB','SUPPORT SEAL RETAINER','569849','423Z1834-2-01','','---',1,'PA 1510 FORECAST-3','','51088','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Tool dig mark (Running time dia 8fl broken).','Will  operation 05 running,Dia 8fl cutter are used for slot roughing,\r\nDia 8lat cutter is not taking material load and causes tool breakage.\r\nDue to part not clamped rigidly in part outer side, causes minor vibrations, this is also causes for tool breakage.\r\nDue to tool breakage dig mark observed on part.\r\n\r\n\r\n\r\n done in Dia 4R0.5 end mill. For this more stock\r\nis there and dia4R0.5 cutter is not taking that load and causes tool breakage','This deviation is due to process problem.\r\nChanged the process by applying the clamps while dia 8flat cutter is running(roughing program)\r\nDia 8flat cutter roughing operation program is altered by reducing the DOC.\r\n\r\nAfter changing the above mentioned points, all the other parts are coming ok and observed the tool load and find ok.','Taking the above corrective actions process is proved and same as implemented in MPS.\r\nNext batch production completed and now process is proved.','CA/PA FOUND OK.','','2016-03-01','Rangaswamy()','Govindraju(NR)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','05','no','Misc','Rangaswamy()','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9147,'18-466A','Magellan Aerospace Wrexham','FRAME MID RIB R','626250','L575 51892 201 PF','','A',1,'RP133570 Amnd 1','','50490','','0000-00-00',NULL,'yes','no','yes','no','yes','no','no','no','no','part insid wall thickness under size    \r\n','Y axis Over Travel Alarm generated by the Machine due  to burr accumulation in Y axis Limit Switch \r\nwhen program End and home reference time of the previous cutter for Dia 25*R2. The Operator Not \r\nobserve  error Shift in Y axis due to the Burr Accumulation in Y axis Limit Switch. He Simply RESET \r\nthe Alarm and Run the machine. the Error Shift in Y Axis Affected the Rib Wall thickness when Dia \r\n25*R2 running time and Dimension measured under size from the lower limit Tolerance.  .\r\n','Machining Process Stopped. checked and Verified Further Dimensions. Informed to service Engineer. Related maintenance Carried out. After the conformation of correct repeatability reading in Y axis the \r\nMachining Process was started.','The operator was advised to remove the burr periodically and avoid the burr accumulation near by the Limit Switch area of the Y axis and Further axis. He was asked to stop the machining process when any alarm arise  and to inform to the Machine maintenance Team immediately.','CA/CP Found ok','','2016-03-01','Narayanappa(G)','Siddaramappa()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','9','no','Misc','Narayanappa(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9148,'35-286','Saab AB','REINFORCEMENT','614341A6','423Z1985-2','','--A',1,'PA 1510 FORECAST-3','','48299','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','1)Is condition: \r\n *Mark 0.0394\"x0.0200\" (1,0x0,5mm).\r\n *Mark, metal visible 0.0394\"x0.0394\" (1,0x1,0mm).\r\n\r\n2)Is condition:\r\n *Mark. 0.0200\"x0.0200\" (0,5x0,5mm) Bare metal visible.\r\n\r\n3)Is condition:\r\n *Part is damaged. Bare metal on a small spot.\r\n\r\n4)Is condition:\r\n *Bare metal visible. No signs of damages on the plastic           bag. Parts must have been damaged before sealed in the plastic bag at the supplier site.\r\n','See attached response from treatment house.','1) Informed to supplier and raised the non conformance report.\r\n2) See attached response from treatment house.','1) See attached response from treatment house.\r\n\r\n2) At CIM side packing method improved.\r\n\r\n3) Treatment house changed to ATPL from VMF & ATPL.','Next batch found satisfactory.','C42282','2016-03-01','Yashawantha(NH)','Nagendra(SN)','OF-001357','2016-02-29','1)425Z0311-10   CED_BS_HINGE_BUMPER_FITTING_AFT\r\n1600131812-5-1-3\r\nCIM W/O: 46672\r\nQuantity 2.\r\n\r\n2)425Z0301-6  CED_VENT_HINGE_FWD\r\n1600131812-7-1-1\r\nCIM W/O: 42756\r\nQuantity 1.\r\n\r\n3)423Z1170-1-05\r\n1600131812-39-1-4\r\nCIM WO: 47999\r\nQuantity 1.\r\n\r\n4)1600131812-21-1-3\r\n423Z1985-2   REINFORCEMENT\r\nCIM W/O: 48299\r\nRemarks on 1 out of 15 pcs.\r\n\r\n','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','CUSTOMER END','no','Misc','Yashawantha(NH)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9149,'35-193','Saab AB','INTERCOSTAL CAM HOUSING','599467','423Z1190-1-01','','---',4,'PA 1510 FORECAST-2','','45734','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Is condition: Insufficient surface treatment coverage.','1) Poor masking on the bore and masking tape spreed to the face that restricts the smooth primer flow.','1) Informed to the supplier(VMF) and raised the non conformance report. See attached NCR report.\r\n2) They are not responded.even after several follow up.','1) Treatment house changed to ATPL from VMF.\r\n\r\n2) We have arranged the good lighting system with dedicated area to inspect the treated parts.','Next batch found satisfactory.','C42296','2016-03-01','Yashawantha(NH)','Nagendra(SN)','OF-001362','2016-03-01','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','CUSTOMER END','no','Misc','Yashawantha(NH)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9150,'28-045','Magellan Aerospace New York  Inc.','LEVER','158529','65-51632-6','','PL_Rev - A + ADCN # 2 ; DL_Rev - N/C',2,'135212-2520','','50162','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','DUMMY','\r\n','','','','','2016-03-02','Dinakar(K)','Nataraja C V,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','9','no','QT100S-1','Ravi(M)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9151,'18-411A','Magellan Aerospace Bournemouth','PLUNGER','237004','D321 40205 200','','H01',3,'RP413360','','49576','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','id thread nogo answered.','After 25nos running threading insert will be wear out.for next part threading insert will be changed\r\nand 0.4 plus(+)taken in wear offset and run the part but thread gauge was not answered then 0.2\r\nminous(-) taken to wear offset and run the part that time thread gauge was nogo answer. ','For next part x-offset taken and taking 0.3 mm up in toolwear offset and run the part gauge not\r\nanswerd,in x-offset give 0.1mm down and run the part and gauge not answered then in x-offset down\r\n0.05mm and run the part and then gauge answered and next part run in same reading & the part found\r\nokay. ','For next part x-offset taken and taking 0.3 mm up in toolwear offset and run the part gauge not\r\nanswerd,in x-offset give 0.1mm down and run the part and gauge not answered then in x-offset down\r\n0.05mm and run the part and then gauge answered and next part run in same reading & the part found\r\nokay. ','Next batch found okay in production.','','2016-03-02','Ravi(M)','Seetharamu D,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','7','no','DX 200-2 ','Ravi(M)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9152,'18-415B','Magellan Aerospace Bournemouth','ACTUATOR HOUSING','M714010 7607 A','D278 50163 201','','D',3,'RP408294','','51051','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Part profile wrong.','When 07-operation running time part is wrongly loaded.\r\n\r\nFor Operation-05 & 07 the same fixture are used with different locations pins.\r\nOperator not referred the MPS and locating pin wrongly loaded in fixture.\r\n\r\nAfter running the first-off part operator find out the error.','Process was proven and details of each setup is mentioned in MPS to avoid manual mistakes, \r\nbut full proof method is not done due to the above errors not expected.','Independent fixtures done for both 05 & 07 operations and fixture designed such a way that operators will not change any pins or bolts.\r\n\r\nFor op-05 new fixture done and part can not load wrongly.(full proof method)\r\nFull proof method fixture done for op-07 by locating the part by using outer profile which is completed in op-05.\r\n\r\nAfter taken the above CA & PA, 1 batch production done and all the parts are coming ok.','next part found ok.','','2016-03-02','Lohith(K)','Shivaraj K S,Kammar Nagaraj,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','7','no','VM2-1','Lohith(K)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9153,'18-119B','Magellan Aerospace Bournemouth','HOUSING OUT B DRG 3','Y10211','D275 40011 200','','D01',1,'RP408158','','50934','','0000-00-00',NULL,'yes','yes','yes','','','','','','','5mm Thickness undersized(-0.4mm).','Operator job not butted correctly.\r\n','Part butting place cleaned neatly by using pressured air.take care operators to but the job properly during clamping the part.','Instruction given to operator to but the job properly during part butting and clamping the part.','Next batch found okay in production.','','2016-03-03','','        Dinakar K','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9154,'35-251','Saab AB','SPACER','G19260R02','423Z1987-1','','---',2,'PA 1510 NEW PARTS-1','','40040','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Parts send to ATPL for trials.','This parts was send to ATPL for trials and is scrapped.','This parts was send to ATPL for trials and is scrapped.','This parts was send to ATPL for trials and is scrapped.','This parts was send to ATPL for trials and is scrapped.','','2016-03-03','Yashawantha(NH)','Yashawantha(NH)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','23510','Post DN','no','Misc','Yashawantha(NH)','no',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9155,'35-182B','Saab AB','EDGE HOUSING','626088','423Z1121-5-02','','--B',2,'PA 1510 FORECAST','','47676','','0000-00-00',NULL,'no','no','no','no','no','yes','yes','yes','no','FPI FAIL.','Due to rubbing of tool or material behavior NDT failure has been found in Treatment house','Instructed to Production  & fitting department to avoid rubbing of tool and polishing ','Avoid polishing and try to finish the part  in machining stage itself.','Next parts and batches found okay','','2016-03-04','Yashawantha(NH)','Nagendra(SN)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','22822','POST DN','yes','Misc','Yashawantha(NH)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9156,'28-007A','Magellan Aerospace New York  Inc.','Shaft Support Lever','B5A71/66761','251A1747-1','Ti-6AL-4V Per Mil-T-','N/C',1,'131717-3186','','50565','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Groove undercut diameter 18.415+/-0.10mm undersize by -0.4mm.','1) During 1st off part, in process dimension 62.10+/-0.10mm measures 62.03mm.\r\n2) Operator tried to maintain this dimensions to mean in the next part.\r\n3) During this process operator adjusted the cutter compensation to maintain this dimension to mean but he had given wrong value.\r\n','Again he checked the next part and adjusted the cutter compensation correct.','Next part found okay and inform to operator when cutter compensation taken recheck after run the program.','Next batch found OK.','','2016-03-04','Narasimhamurthy(K.G.)','Seetharamu(D)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','05','no','Misc','Narasimhamurthy(K.G.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9157,'42-004A','RAFAEL','Clamp-2 ','072250','BA1E2003B','','38-576104 Rev E, TILDOCS#172373 Rev 14, PR603-2-3 Rev 16, RAFDOCS#5224238 Rev 4, 111.21 Rev 7, 111.22 Rev 1, ECN63628 2015/01/13, ECN60821 2014/10/26',1,'347592024-8','','50835','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Thickness minus side 0.3mm','While part running time total thickness under size.\r\nThis variation observed part turning operation completed time part was taper.\r\nShift operator not observe the taper so part total thickness under size.\r\nThis error happened operator mistake.   ','All part taper machining checked and segregated after continue the production.\r\nInform to operator when part dig mark ,taper or bend observed immediately inform to concern supervisor. ','Inform to the operator before load the part, check the taper or bend after continue the program.','CA/PA Found Ok','','2016-03-05','Lohith(K)','        Narasimhamurthy C','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9158,'18-392B','Magellan Aerospace Bournemouth','END COVER','5977','D278 50167 200','','D',1,'RP408296','','50258','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Hole position not achive.','We are using the drill with reamer so hole position was not achieved. ','For the next part we are using the the hole mill so hole position was achieved so continue the production.','For next every batch we are using the hole mill and avoide the this type of mistakes.','Next batch found okay in production.','','2016-03-06','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Narasimhamurthy(K.G.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9159,'18-118B','Magellan Aerospace Bournemouth','BEARING HOUSING','A12364','D275 40005 200','','C01',1,'RP408156','','50783','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','OD Thread flat.','While running time finishing insert will be brocken so change the insert and remove the part in the chuck and load the next part and taken safer side in wear offset and give the proper correction and run the part. part checked found ok.for the next loading the semi finished part and run the part so that part run out wiil be came and one side thread was flatted so part was rejected. ','For next every part holding in the chuck and check the run out, before running the part.','If any cause we removing the part in the chuck, for the next we are loading in the same part check the run out before running.','Next batch found okay in production.','','2016-03-06','Dinakar(K)','Devaraj(K.C.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','03','no','Misc','Narasimhamurthy(K.G.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9160,'18-475A','Magellan Aerospace Wrexham','RIB 1 L/H','9550801','L575 57325 200 PF','','A00',1,'RM133577 Amnd 3','','48471','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','no','Flange Thickness 4.0+0.2/-0.1 at zone C5 measured 4.30/4.32mm.','1)This was happened due to part was lifted during machining.\r\n2)We are using vacuum fixture for this family parts.\r\n3)Rubber gasket is broken which was used in the vacuum fixture. During machining that leads to air leakage which obviously effects and lose the holding strength of the part. \r\n','1)We noticed the thickness oversize our self and same was communicated to Magellan India source inspector.\r\n2)Operator instructed to check the rubber gasket continuity/Breakage before loading the fixture to machine.\r\n','1)We brought rubber gasket in one bundle around 1000metres that is inspected during receiving the item.\r\n2)We are checking the possibility of installing indicator/ signals which will give default message indication, \r\nIf air leakage in the fixture.\r\n','CA/PA found ok.','C42902','2016-03-07','Avinash(R.J.)','Nandishkumar(D.K.)','RDN 0152','2016-02-03','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','0','CUST END','no','Misc','Muniyappa(N)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9161,'18-098B','Magellan Aerospace Bournemouth','VALVE- SEAT','68488/01/01','D282 50060 204','','D',1,'RP408160','','50484','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','no','Depth 0.9 to 1 mm (zone-A3) measures .808 to .837mm (U/S by between 0.063 to 0.092mm) in 01 no out of 80 no’s.','1)These parts have been manufacturing with ageing (minimum aging time 1day) to avoid the bow in the part.\r\n2)Flatness around the groove should be 0.010mm and this achieving with buffing.\r\n3)These parts are inspected two times which is prior to buffing and after buffing. Mean time groove depth is also checked.\r\n4)Here noticed our self the depth undersize and moved to rework. After that he missed to re-ensure the part, weather the depth is achieved OR not.\r\n','1)Instructed to concerned personals to keep the rework parts separately with identification till inspector re-ensure.\r\n2)After rework, informed to re check the related dimensions. Because after rework might be chance of other related dimensions is changed.  \r\n','1)Instructed to concerned personals to keep the rework parts separately with identification till inspector re-ensure.\r\n2)After rework, informed to re check the related dimensions. Because after rework might be chance of other related dimensions is changed.  ','CA/PA found ok.','','2016-03-07','Avinash(R.J.)','Nandishkumar(D.K.)','RDN 0155','2016-02-16','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','0','on site','no','Misc','Muniyappa(N)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9162,'43-013','Composite Industrie','B BRACKET','586265-2A1','V251 11738 200','','A00, ECN PV100298ST1BP90',1,'ATA25_ACH-4649','','51067','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Part outer profile tool dig mark.','Operator taken work offset wrongly, so Part outer profile tool dig mark.part rejected.  ','Taken correct work offset and supervisor cross checked, then continued machining.\r\nNext part found ok and production continued after taking Firstoff clearance.   ','Error is due to man, operator have good experience on machine and he is good in taking offsets and operating the machine.\r\n\r\nWe given clear instruction that if found any deviation as above, will reduce your skill set in skill matrix.\r\n\r\nSupervisor is monitoring and cross checking the operator.\r\nSupervisor ensured the skill set again and found OK.\r\n','Next part found ok.','','2016-03-07','Rangaswamy()','Govindraju(NR)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Rangaswamy()','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9163,'35-195','Saab AB','SUPPORT SEAL RETAINER','558386','423Z1834-2-01','','---',1,'PA 1510 FORECAST-3','','51087','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','operator wrong correction.','This part wall finish in operation 07 & 09 setups, wall mismatch two setups. so operator correction for wall mismatch.this wrong correction so part rejected. ','Next part given correct correction match wall mismatch then run production.\r\n','Save this program and training to operator for enter offset and correction.','CA/PA FOUND OK.','','2016-03-07','Rangaswamy()','Rangaswamy()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','07','no','Misc','Rangaswamy()','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9164,'18-030A','Magellan Aerospace Bournemouth','PIN','Y11694','D278 50156 200','S130 FHT','A',1,'RP408145','','50121','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Due to rubbing of tool or material behavior Corrosion Pits  has been observed  in Treatment house\r\n','Apply PX-24 after machining, and polishing and rubbing of tool should be avoided\r\n','Apply PX-24 after machining, and polishing and rubbing of tool should be avoided\r\n','Apply of PX-24 is mandatory before sending the parts to treatment house.\r\n','Next parts and batches found okay\r\n','','2016-03-07','Avinash(R.J.)','Nandishkumar(D.K.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','23200','POST DN','no','Misc','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9165,'35-189','Saab AB','INTERCOSTAL_MIDSPAN_NO_2 ','582083','423Z1170-1-06','','---',2,'1600097307','','39011','','0000-00-00',NULL,'no','no','no','no','no','yes','yes','yes','no','NDT Fail.','Due to rubbing of tool or material behavior NDT failure has been found in Treatment house','Instructed to Production  & fitting department to avoid rubbing of tool and polishing ','Avoid polishing and try to finish the part  in machining stage itself.','Next parts and batches found okay','','2016-03-08','Yashawantha(NH)','Nagendra(SN)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','16181','Post DN','yes','Misc','Nagendra(SN)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9166,'35-036','Saab AB','7605122-200','425412','L574 55122 200','ABM3 1029','A00',1,'1600115266','','44495','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','NDT Fail.','Due to rubbing of tool or material behavior NDT failure has been found in Treatment house','Instructed to Production  & fitting department to avoid rubbing of tool and polishing ','Avoid polishing and try to finish the part  in machining stage itself.','Next parts and batches found okay','','2016-03-08','Yashawantha(NH)','Nagendra(SN)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','19227','Post DN','yes','Misc','Nagendra(SN)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9167,'18-114A','Magellan Aerospace Bournemouth','NUT','238300','D575 40499 200','S80 FHT','D01',2,'RP408154','','50199','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','NDT Failure.','Due to rubbing of tool or material behavior NDT failure has been found in Treatment house\r\n','Instructed to Production  & fitting department to avoid rubbing of tool and polishing \r\n','Avoid polishing and try to finish the part  in machining stage itself.\r\n','Next parts and batches found okay\r\n','','2016-03-08','Avinash(R.J.)','Nandishkumar(D.K.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','23170','POST DN','no','Misc','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9168,'35-076','Saab AB','9900976-434','527720','F579 54100 200','ABM3 1029','B',2,'1600076911','','33530','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','yes','After treatment part dig mark notes. ','1)Part handling time.\r\n2)insufficient packing.  ','1)Visited packing area and checked available parts for dent and damages and found none.\r\n2)Partitions trays used in FG.\r\n3)packing the parts in one by one.   ','1)Trained to operator how to handle the parts.\r\n2)Partitions trays used in FG.\r\n3)packing the parts in one by one and using the bubble sheet. ','CA/PA FOUND OK','','2016-03-08','Yashawantha(NH)','Nagendra(SN)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','13113','Post DN','no','Misc','Nagendra(SN)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9169,'35-300','Saab AB','BRACKET, INTERMEDIATE FRA','452849A','423Z1125-5-02','','---',1,'PA 1510 FORECAST-3','','49004','','0000-00-00',NULL,'no','no','no','no','no','yes','yes','yes','no','FPI Fail.','Due to rubbing of tool or material behavior NDT failure has been found in Treatment house','Instructed to Production  & fitting department to avoid rubbing of tool and polishing ','Avoid polishing and try to finish the part  in machining stage itself.','Next parts and batches found okay','','2016-03-08','Yashawantha(NH)','Nagendra(SN)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','22632','Post DN','yes','Misc','Nagendra(SN)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9170,'35-225A','Saab AB','HINGE BRACKET 1 ','425130','D576 50004 206','','D00',1,'1600093863 Rev-2','','38752','','0000-00-00',NULL,'no','no','no','no','no','yes','yes','yes','no','Part send to ATPL for trail and reject.','This part was sent to ATPL for trials and is scrapped','This part was sent to ATPL for trials and is scrapped','This part was sent to ATPL for trials and is scrapped','This part was sent to ATPL for trials and is scrapped','','2016-03-08','Yashawantha(NH)','Nagendra(SN)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','15575','Post DN','no','Misc','Nagendra(SN)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9171,'35-272','Saab AB','PIN','970533','425Z0601-3','','--A',1,'1600102192','','43211','','0000-00-00',NULL,'no','no','no','no','no','yes','yes','yes','no','MPI Fail.','MPI tests failed in treatment house due to material behavior.','1)Raise the rework order.\r\n2)Polishing the MPI reject place and send to treatment.   ','100% RM inspection will be carried out in future batches.','Next batches Found okay.','','2016-03-08','Yashawantha(NH)','Nagendra(SN)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','21439','Post DN','yes','Misc','Nagendra(SN)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9172,'35-236A','Saab AB','JACK BRACKET 1','927315','D576 50009 207','','D00',2,'1600115959','','44674','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','This part was sent to ATPL for trials and is scrapped','This part was sent to ATPL for trials and is scrapped','This part was sent to ATPL for trials and is scrapped','This part was sent to ATPL for trials and is scrapped','This part was sent to ATPL for trials and is scrapped','','2016-03-08','Yashawantha(NH)','Nagendra(SN)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','19472','Post DN','no','Misc','Nagendra(SN)','no',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9173,'18-105A','Magellan Aerospace Bournemouth','FORKEND ASSEMBLY','A1218X','D572 50462 200','S98 FHT','J01',1,'RP408148','','50790','','0000-00-00',NULL,'','','yes','','','','','','','under cut (-) side 0.18','wrong tool rotation given. while M04 tool rotation given place M03 rotation given so running time insert will be brocken and under cut dia 0.18 undersized.','For the next part change the tool rotation and insert. and Re-offset taken and plus taken in the wear offset and check the part and give the proper correction and run the part. Part checked foun ok and continue the production.  ','Instruction given to the operator about tool direction rotation and inserts. and every setting time before running the part check the all tools inserts program and then run the part. ','Next batch found okay in production.','','2016-03-08','','        KRISHNAMURTHY N','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9174,'35-166A','Saab AB','HOUSING PIN','541025','423Z1124-6-01','','--A',1,'PA 1510 FORECAST','','46830','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Tool dig mark notes by outer profile.','When doing part cutout part rotates causes dig mark on part outer profile.\r\nWhen cutout operation is carried, part clamped with bolt(bolt in center bore)on bore as per process.\r\nprocess was proved and clamping is enough for cutout,but in this case operator may not clamped properly( sufficient clamping force)may causes part moving.','Checked the threads in fixture, threads in bolt and also clamping force to hold the part while cutout.\r\nAll the features is ok and also next all the parts in this batch are machined with the same process.\r\n\r\nThis error is may due to insufficient clamping not done by operator.','As per the above mentioned CA all the process is ok.\r\n\r\nNext batch again will monitor the process and then will take action to prevent.\r\n\r\nAt the movement no PA planned/taken.','CA/PA FOUND OK.','','2016-03-08','Rangaswamy()','Rangaswamy ,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','MakinoF5','Yashawantha(NH)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9175,'35-166A','Saab AB','HOUSING PIN','541025','423Z1124-6-01','','--A',1,'PA 1510 FORECAST','','46830','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','KC profile plus side 0.30mm','While running operation-03, outer profile finishing not done.\r\n\r\nThis deviation is due to program skipped when power failure.Operator not checked the sequence of programs which is already completed and from which program has to start after power failure.\r\n \r\n0.3mm stock is measured and while checking the part in stage operator find out this deviation and rework NCR was raised.','Informed to operator to check the programs sequence when power failure and write done in program name in machine reference book and once restart the machine after power failure,Operator has to ensure twice with the reference book.(sequence of programs)\r\n\r\nThis will monitor by supervisor and mandaterlly operators has to write the sequence of programs when power failure.\r\n\r\nRework done by relocate the part after cutout and runned the same finishing program which was proved.\r\n\r\nCMM inspection done and QAD approves the part.(All the drawing requirements are met) ','Informed to operator to check the programs sequence when power failure and write done in program name in machine reference book and once restart the machine after power failure,Operator has to ensure twice with the reference book.(sequence of programs)\r\n','After rework part Accepted.','','2016-03-08','Rangaswamy()','Rangaswamy ,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','With Treatment','','FI','no','MakinoF5','Yashawantha(NH)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9176,'35-262','Saab AB','ROD-END','970674','424Z3413-1','','--A',3,'PA 1510 FORECAST-2','','45292','','0000-00-00',NULL,'no','no','no','no','no','yes','yes','yes','no','MPI FAIL.','1) We have checked visually and found no defects by eye sight.\r\n2) We dont have the exact reason of MPI not passed at this movment. But considering the commercial impact is very less. So rejected the parts.','1) Now we have our treatment house ATPL is approved and we will use this facility now onwards.','1) If something failled in treatment house then we can use another treatment house for re-certification.\r\n2) If the results of both the treatment is same then we will inform to material supplier.','CA/PA found satisfactory.','','2016-03-09','Yashawantha(NH)','Nagendra(SN)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','20478','Post DN','no','Misc','Nagendra(SN)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9177,'35-071','Saab AB','9900976-380','PUA2797','L579 50517 200','TA11','B00',1,'PA 1217 FORECAST-2','','50994','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Dig mark observed on face.','Dia 3 ball nose tool offset wrong taken.So part face dig mark noticed part rejected.','Tool offset correct taken after continue the production.\r\nNext part found okay. ','Train by operator two methods of tool offset taken and  cross checking done fond satisfactory','CA/PA FOUND OK.','','2016-03-09','Lohith(K)','        Mohan Kumar C.M.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9178,'34-015B','Magellan Aerospace Winnipeg','MOUNTING LUG- STRUT / STD','77837','400-12607-1-905','','EM104302 Iss A, EM104765 Iss G, EM105092 Iss F, EM106399 Iss B, EM106400 Iss B, EM106401 Iss A, EM106404 Iss A, EM106522 Iss A, EM106602 Iss A',1,'B91379 Rev.026','','50530','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Base thickness minus 0.08mm','The part was not butted in the fixture properly which was slightly lifted while finishing the base thickness.','Instructed to operator part loading time part butting properly during clamping.','After loading the part into the fixture, using the feeler gauge and then start the machining.','CA/PA Found Ok','','2016-03-09','Lohith(K)','Vishwanath(Pavar)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','05','no','Misc','Lohith(K)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9179,'18-372B','Magellan Aerospace Bournemouth','GAMMA FITTINGS ','M730890 8648','NSA840007-250 ','','N',1,'RP408523','','51360','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dig mark in outer diameter so part was rejected.','After running the roughing program for inner diameter chips was not brocken, for the next od finishing tool will be running that time the ID roughing stage  lenghthy chips will rotating the OD finishing tool and this tool running time chips observed the operator and holding the feed rate, that time dig mark occured in the part outer diameter so part was rejected. ','We are using chip breaking inserts for ID and OD roughing some times depends about materials hardness chips was not breaking that time we are changes the RPM and DEPTH of cut in the program in this batch also chips was not breaking properly so change the rpm and cuts and for check the after 5 parts then chips was break in to like small pieces then continue the production. ','Information passed to the operator after the setting while production running time if chips was not breaking properly or about insert life inform to the concerned shift incharge and avoid to the this type of mistakes.  ','CA/PA found OK.','','2016-03-10','Dinakar(K)','Dinakar K,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','1','no','QT100S-3','Sandhesh D(S)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9180,'35-138','Saab AB','FLCD_DS_SUPPORT_DEFLECT_S','7543150','423Z6189-3','BAC1534-62C','---',2,'PA 1510 FORECAST','','45517','','0000-00-00',NULL,'no','no','no','yes','no','yes','no','yes','no','Material layer chip out.','Due to material bheaviour this was opened out. ','1) We decided that this cannot be avoided but we minimized by improving the handling methods. ','1) We decided that this cannot be avoided but we minimized by improving the handling methods. ','CA/PA found satisfactory and material layer removal is decreased.','','2016-03-10','Yashawantha(NH)','Nagendra(SN)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','19766','Post DN','no','Misc','Yashawantha(NH)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9181,'35-170','Saab AB','ALCD_STRUCT_SUPPORT-FTG_L','569848','423Z1200-11-01','','---',1,'PA-1300 2014','','38471','','0000-00-00',NULL,'no','no','no','no','no','yes','yes','yes','no',' FPI Fail.','Due to rubbing of tool or material behavior FPI failure has been found in Treatment house','Instructed to Production  & fitting department to avoid rubbing of tool and polishing ','Avoid polishing and try to finish the part  in machining stage itself.','Next parts and batches found okay','','2016-03-10','Yashawantha(NH)','Nagendra(SN)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','15939','Post DN','no','Misc','Yashawantha(NH)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9182,'18-411A','Magellan Aerospace Bournemouth','PLUNGER','237004','D321 40205 200','','H01',3,'RP413360','','49576','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','DUMMY NC.','DUMMY NC.','DUMMY NC.','DUMMY NC.','Dummy NC.','','2016-03-11','Ravi(M)','Seetharamu D,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','7','no','DX 200-2 ','Ravi(M)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9183,'18-462A','Magellan Aerospace Wrexham','SPAR FWD','455101','L575 51827 201 PF','','A00',1,'RP133603 Amnd 4','','49860','','0000-00-00',NULL,'no','yes','yes','yes','no','no','no','no','no','Raw material cross cutting','While cutting the material as per layout, due to Machine blade was slack & wobbling so cross cut the\r\n material.  \r\n','Cutting process stopped and blade supplier was visited and verified the machine belt speed and blade\r\n & adjust the belt speed & change the blade.  \r\n','Frequent checked to be done for blade wobbling & blade speed for prior to cutting.  \r\nEffectiveness:\r\n \r\n','CA/PA Found ok','','2016-03-11','Sunil Kumar(K.R.)','Narayanappa(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','01','no','Misc','Narayanappa(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9184,'35-161','Saab AB','STOP SUPPORT','55524-1R','423Z6188-6','','---',1,'PA 1510 FORECAST','','49595','','0000-00-00',NULL,'yes','no','no','no','no','yes','no','yes','no','MPI Fail.','MPI tests failed in treatment house due to material behavior','100% RM inspection will be carried out in future batches','100% RM inspection will be carried out in future batches','Found okay in next batches.','','2016-03-11','Yashawantha(NH)','Nagendra(SN)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','Post DN','no','Misc','Nagendra(SN)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9185,'18-461A','Magellan Aerospace Wrexham','SPAR FWD','455101','L575 51827 200 PF','','A00',1,'RP133603 Amnd 4','','49859','','0000-00-00',NULL,'no','yes','yes','yes','no','no','no','no','no','25mm total length under size due to material cross cutting  ','While cutting the material as per layout, due to Machine blade was slack & wobbling so cross cut\r\nthe material.  \r\n','Cutting process stopped and blade supplier was visited and verified the machine belt speed and\r\nblade & adjust the belt speed & change the blade.  \r\n','Frequent checked to be done for blade wobbling & blade speed for prior to cutting. \r\n','CA/PA Found ok','','2016-03-11','Sunil Kumar(K.R.)','Sathish Y.R.,Karthineyan V.S.,Gajendra Singh C.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','1','no','UNIPRO 5000-1','Narayanappa(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9186,'35-344','Saab AB','RIB OUTBD CLOSING','6591801','F575 52067 201 00','','B',1,'1600139584','','51548','','0000-00-00',NULL,'','','yes','','','','','','','DUMMY NCR','DUMMY NCR\r\n35-343 PART 1 NOS REJECTED, BUT NC RAISED 35-344\r\nWrong program and wrong CRN givan by  CAD/CAM\r\n','DUMMY NCR','DUMMY NCR','DUMMY','','2016-03-13','Ramesh(Poojary)','        Karthineyan V.S.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9187,'18-117B','Magellan Aerospace Bournemouth','HOUSING-OUT BD BRG','A12426','D275 40004 200','','C01',2,'RP408156','','48832','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Controlled Outer Diameter undersize by 0.001mm to 0.005mm ','1) These parts have to be manufacturing with aging by minimum 2 days and maximum 1 week.\r\n2) Historically same method adopted and witnessed the repeatability good and found well within the limits.\r\n3) Particularly this batch we kept for aging that goes to one month due to some other work load.\r\n4) After that we noticed the ovality.\r\n','1) We instructed to manufacture the parts with aging of minimum 2 days and maximum 1 week.\r\n2) During aging these parts will be kept in controlled temperature.\r\n','These family parts we treat for same method.','CA/PA found satifactory.','','2016-03-14','Ravi(M)','Ravi(M)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','09','no','Misc','Ravi(M)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9188,'42-006','RAFAEL','Clamp Bridge','70129354','BA1E2005B','','38-576104_Rev-E,   TILDOCS#172373_Rev-13, 111.21 _Rev_6,  GEN_1111-1_Rev-A,  ECN 57176 2014/08/05',1,'347592024-6','','51144','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','6-32UNC-2B Thread gauge NO GO answered 2 holes.','Threading operation time chips was clogged thread over size gauge NO GO answered.','Next parts before threading time clean the parts with Air gun & next part found OK production will continued.','Before the threading operation massage will be showed in the program.  ','Next batch found OK.','','2016-03-14','Rangaswamy()','Rangaswamy()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','Misc','Sudhagar(V)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9189,'35-329','Saab AB','RIB INBD CLOSING AFT','1070901','F575 54804 200','','A, ECN PG205027001KC79',1,'1600134622','','51310','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dig mark due to tool offset problem','When taking the Cutting Tool Height offset, the A axis of the Machine is not zero position. The operator not observe the A axis Position. so Cutting tool Height offset input with 0.5mm error. ','A axis position of the Machine made Zero by using MDI Mode.. correct cutting tool Height offset entered in tool offset parameter. ','A Error proof Macro Program for Cutting Tool height offset created in Machine and Proper Training given to All Operators regarding the error proof Macro Program.','CA/PA FOUND OK.','','2016-03-14','Narayanappa(G)','Sathish(Y.R.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','06','no','Misc','Krishna(Chowdary.G.P.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9190,'18-083A','Magellan Aerospace Wrexham','STUD PLATE','297622/001','D278 50007 201','ABM3 1029','D01',1,'RP135247','','51581','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Thickness measures minus side 6.85 to 6.88.(drawing dimension 6.95 to 7.05)','Due to part not butted properly while doing operation 02(Operation-thickness maintain)\r\nThis process was provened and operator has to cautious while clamping and malleting. \r\nOperator has to do normal tightening and has to ensure the butting by mallet feeling.','The above mentioned instructions is not followed by operator due to 1)lack of knowledge of this instructions or 2)By negelengency operator not followed above instructions.\r\n\r\nTherefore we taken photos of clamping and malleting of part and same will display as instruction for next batches.\r\n\r\nThis will avoid such problems and everybody will aware of instructions.\r\n','1)The above Corrective actions are taken and same will implemented in next batches and also will ensure the instructions will pass to all the operators.\r\n\r\n2)Informed to operator to check & ensure the part butting for every part in fixture. \r\n\r\n3)Message entered in beginning of program to alert the operator to check the butting by giving optional stop(M00)','CA/PA found ok.','','2016-03-16','Lohith(K)','Lohith(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','0','no','Misc','Lohith(K)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9191,'35-232A','Saab AB','HINGE BRACKET 4 ','3861901','D576 50007 209','','E00',3,'1600121830','','47589','','0000-00-00',NULL,'no','no','no','no','no','yes','yes','yes','no','FPI Failed.Part sent to ATPL for Trails Purpose.','Part sent to ATPL for Trails Purpose.','Part sent to ATPL for Trails Purpose.','Part sent to ATPL for Trails Purpose.','Part sent to ATPL for Trails Purpose.','','2016-03-16','Yashawantha(NH)','Nagendra(SN)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','21068','Post DN','no','Misc','Nagendra(SN)','no',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9192,'35-232A','Saab AB','HINGE BRACKET 4 ','3861901','D576 50007 209','','E00',2,'1600121830','','48041','','0000-00-00',NULL,'no','no','no','no','no','yes','yes','yes','no','FPI Failed.Part sent to ATPL for Trails Purpose.','Part sent to ATPL for Trails Purpose.','Part sent to ATPL for Trails Purpose.','Part sent to ATPL for Trails Purpose.','Part sent to ATPL for Trails Purpose.','','2016-03-16','Yashawantha(NH)','Nagendra(SN)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','21344','Post DN','no','Misc','Nagendra(SN)','no',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9193,'35-232A','Saab AB','HINGE BRACKET 4 ','3861901','D576 50007 209','','E00',1,'1600121830','','47600','','0000-00-00',NULL,'no','no','no','no','no','yes','yes','yes','no','FPI Failed So Parts sent to ATPL For trails Purpose.',' Parts sent to ATPL For trails Purpose.',' Parts sent to ATPL For trails Purpose.',' Parts sent to ATPL For trails Purpose.',' Parts sent to ATPL For trails Purpose.','','2016-03-16','Yashawantha(NH)','Nagendra(SN)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','21071','Post DN','no','Misc','Nagendra(SN)','no',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),