(8114,'18-284A','Magellan Aerospace Bournemouth','SPINDLE FOR CLACK ALVES O','Y10819','A281-40019-200','S80 FHT','A',2,'RP400846','','39817','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dent marks found on OD','Burr folded in the part,part mixed up in the okay parts','After cut,chamfer operation will be done to avoid Burr\r\nproblems in the future','After finishing of the part , part will be covered with\r\npaper so that contact of the parts will no be there and\r\ndent marks can be avoided.','Next parts found okay','','2015-01-13','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','01','no','Misc','Dinakar(K)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8115,'18-078A','Magellan Aerospace Wrexham','ADAPTOR ','16146121','A282 50081 200','','A',1,'RP125890','','39475','','0000-00-00',NULL,'yes','no','no','no','yes','yes','no','no','no','ID Ovality.','After running 50 to 60 parts insert tip will be worn out and running time chips not breaking properly so chips will \r\nloked inside the part and ovality will be occure in the \r\nrunning part. So part one side shows reading -0.03 and \r\nanother side shows +0.02 so part will be rejected.\r\n','Remove the worn out insert and replace the new insert\r\nand newely offset taken and 0.2 (-) minous taken in the tool wear offset and run the part and then check the inner diameter and give the correction in  wear offset and run the part and checked found ok. \r\n','while setting time loading the new insert before running and after every 100 nos change the roughing insert and run the part. and every 25ns onece observe the tool noise and  chips while running. \r\n','CAPA found okay.Implementation is needed!','','2015-01-13','Dinakar(K)','Yarri Gowda,Shivanand D.B.,SHIVAKUMAR ,Rajesh B D,Raghavendra Rao R,Punith G S,Dhananjaya N,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','FI','no','ST20','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8116,'35-138','Saab AB','FLCD_DS_SUPPORT_DEFLECT_S','501721','423Z6189-3','BAC1534-62C','---',10,'1600101109','','40181','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Material layer chip out in middle of part. ','The Following Route causes analyzed for material chip off after outer profile machining. 1. Due to RM deviations material will chip off. 2. 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. 1. Raw Material will inspect visually before issuing to production. If found any problem visually RM will be quarantined. 2. Dia 8 end mill life calculated, informed to operators to monitor the tool life.and change the tool after as mentioned. 3. Steel butting plates flatness inspection done before production starts.','The following Corrective Action/Preventive Action taken to avoid Materiel chip off. 1. Raw Material will inspect visually before issuing to production. If found any problem visually RM will be quarantined. 2. Dia 8 end mill life calculated, informed to operators to monitor the tool life.and\r\nchange the tool after as mentioned. 3. 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.','CAPA found okay, next batch will be monitored','','2015-01-13','Lohith(K)','Theerthappa K.N.,Shivaraj K S,Hari Prasad,Chiranjeevi S,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','HAASVF2SS','Manjunath(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8117,'18-295A','Magellan Aerospace Bournemouth','BOLT','238302','D577 56145 200','S80','A',1,'RP400846','','40103','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','OD Dentmark.','Part Handling Problem. Identification is going on whether where it has happen.','Sleeves are being introduced for the parts to avoid scratches and dent marks','Training should be given to handle the parts and separate racks will be introduced so that metal to metal contact shall be avoided.Sleeves are being introduced for the parts to avoid scratches and dent marks','Left out parts found okay. And next batch will be taken care for the above CAPA','','2015-01-13','Ravi(M)','Vasu SN,Shivanand D.B.,SHIVAKUMAR ,Ravi R,Rajesh B D,Raghavendra Rao R,Mohan Kumar C.M.,Manohara M,Manjunatha N,KRISHNAMURTHY N,GUNDEGOWDA H.G.,Girish HP,Bharath R,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','FI','no','QT100S-2','Narasimha Murthy(R)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8118,'18-371B','Magellan Aerospace Bournemouth','GAMMA FITTINGS ','M305800','NSA840007-150','','N',1,'RP401477','','35046','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','OD Thread NOGO Answered.','Parts accepted','Parts accepted','Parts accepted','Parts accepted.','','2015-01-13','Kalakappa T(H)','Nandeesha N,Kalakappa T H,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','Manufacture Only','','FI','no','QT100S-3','Narasimha Murthy(R)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8119,'07-019','HAL-NASIK','SPAR','AS-14952','11.3120.3.800.001-1','','Technical Sheets',1,'NK/M/2513 (4440) ?MP','','38482','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Thickness under size by 0.1 to 1.00mm. (Nominal 2 +/-0.2 is Measured 0.80 to 1.70mm)','This NC generated twice so please Refer NCR NO 08068,\r\nThis part work order already NC 08068 raised, & part work order no 38483, but quality inspector offered to work order 38482.','Refer NCR NO.08068 & WORK ORDER NO.38483 ','Refer NCR NO.08068 & WORK ORDER NO.38483 ','Why did Quality Inspector took another work order?\r\nWhy was deviation not found in Production stage only?\r\nWhy was NC not mentioned in Work order?\r\n\r\nRoot cause shows deviation in procedure!','','2015-01-14','Narayanappa(G)','Sathish Y.R.,PAVAN KUMAR  S.K.,Narayanappa G,Manjunath K.N.,Gajendra Singh C.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','yes','Manufacture Only','','FI','no','DMG 360L','Avinash(R.J.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8120,'35-225A','Saab AB','HINGE BRACKET 1 ','688931A5','D576 50004 206','','D00',1,'1600099854','','40541','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Dig Mark on part. (Base radius)','CRN 35-225A regular production running at F5-1 machines which is dedicated to A320 Brackets. All programs proved and saved in server.\r\nDue to meet the schedule, planned to run in F5-1 and F5-4 machines at the same time.\r\nAll the program is proved, but due to adjust the step in wall by using TRANS, operator miscalculated the Z value in A90 and A270.This manual error causes dig mark on part.\r\n ','Trans value corrected and continued production.\r\nNext part found ok.','Due to thickness variation in 02 part nos in A320 brackets,this miscalculation happened.\r\nRegarding programming sequences, Process and Tools training conducted for operators to understand.\r\nTraining given to,\r\n1.Basavarju\r\n2.Subramanya\r\n3.Manu kumar\r\n4.Sundar\r\n5.Prashanth kumar\r\n6.Heranna\r\n7.Srikanth\r\n8.Girish','CAPA found good, next batch will be monitored ','','2015-01-14','Girish(Prasad P)','        Basavaraja S. Jr.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8121,'18-186A','Magellan Aerospace Bournemouth','BUSH','P1631','L575 50336 200','B23','B00',1,'RP401024','','39822','','0000-00-00',NULL,'yes','','yes','','','','','','','setting time ovelity probelm so part (-) side -0.004','CHIPS CLOGGED DURING FINAL PASS HENCE DEVIATION OCCURED. ','iNSTRUCTED OPERATOR TO CLEAN THE CHIPS NEAR THE TOOL OFTEN TO AVOID THIS DEVIATION. ','iNSTRUCTED OPERATOR TO CLEAN THE CHIPS NEAR THE TOOL OFTEN TO AVOID THIS DEVIATION. ','CAPA unsatisfactory. Repeated CAPA cannot be acceptable.','','2015-01-14','Ravi(M)','        Girish V M','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8122,'18-414B','Magellan Aerospace Bournemouth','ACTUATOR HOUSING','M563530','D278 50163 200','','D',1,'RP401021_Amnd No. 1','','40468','','0000-00-00',NULL,'yes','','yes','','yes','','','','','groove width over size by 0.35mm.','setting time for first part altering the program and then  \r\nrun the part  after roughing only 0.1 stock for finishing \r\ntool so chattering came in finished part so for that part \r\npolishing the chattering and it will become 0.1 over sized\r\nfor that part without identification move to for next setup.in that set up they are maintaining the total length for all parts in same size so thickness 6mm -0.1 under sized so part rejected.\r\n','check the program before running the next part and alter \r\nthe program for correct size (dimension). And run the part.\r\nand  proper stock given for finished tool and adjust the\r\ntool (blade) lenght if required size,so chattering  problem\r\nwill avoiding and check the groove width it will found ok.\r\n','marking the blade length, for next every batch all are maintaining the same length for this CRN. And maintain proper stock for finishing tool. insert not seated in the finishng tool so next batch new (blade) tool used for finishing pass.\r\n','Next parts found okay','','2015-01-16','','        Raghavendra Rao R','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8123,'35-225A','Saab AB','HINGE BRACKET 1 ','689008A1','D576 50004 206','','D00',1,'1600099854','','40546','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Base thickness and Total part width measures 0.6mm minus side.','This deviation coming due to Dia 63 face mill insert loosened and 0.3mm tool measurement varies, this causes thickness minus side. ','Tool insert changed and new Screws changed for all the insert seating(06nos),New offset taken and continued production.','Informed to operators, Supervisors, Tool in charge to monitor and check the screws regularly and also insert wear out.\r\n\r\nThis PA will avoid such errors in future.','Repeated problems like insert cut, screw loosened cannot be acceptable in future warned supervisors and next parts found okay but next batches also will be monitored.','','2015-01-16','Girish(Prasad P)','        Basavaraja S. Jr.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8124,'18-104A','Magellan Aerospace Bournemouth','BODY TURNBUCKLE','239338','D575 40490 200','S80 FHT','E',1,'RP400840','','39671','','0000-00-00',NULL,'yes','yes','yes','','','','','','','thread NO GO answering 01nos','Thread was damaged due to wear out of inserts. The operator intended to rework the damaged thread\r\nresulting in non conformance of ID. ','Insert was worn out at that stage which was replaced for the next job.','The block holding the tool shall be set by the Supervisor for every batch which is expected to\r\nextend the tool life and reduce these type of non conformances. ','CAPA found okay. Next batch will be monitored carefully.','','2015-01-17','Dinakar(K)','        Dinakar K','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8125,'40-016','Universal Engineering Limited','ANGLE SUPPORT ','169843/001','D924 50146 204','','J, ECN NW21405ST1KA27',1,'320402 - S1','','39775','','0000-00-00',NULL,'yes','yes','yes','','','','','','','part butting problem so part shift ','This part 1 setup  holding in vise, not proper butting in \"x\" axis so loading time operator shift the part, so part rejected.  ','Stop the production,Machining new block create in \"X\" axis butting then start production, found ok.  ','Next production batch using this block to avid rejection. next show in process sheet.','Next batch will be monitored','','2015-01-17','Rangaswamy()','        Mahesh N','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8126,'18-157A','Magellan Aerospace Wrexham','Strap Crackstopper','9384703','D572 50203 204','ABM3 1029','L',2,'RP125886','','39943','','0000-00-00',NULL,'no','yes','yes','yes','no','no','no','no','no','required thickness 1.2 but maser value 0.9 to 1.2mm part end to end 2side','This was taken on knowingly for trial,only one billet(4nos), \r\nraw material length 25mm short so vacuum not holding in end area lifted but 2nos was good and 2nos rejected.   ','1) This was taken on knowingly for trial,only one billet(4nos)\r\n2) raw material 25mm length short informed to store,\r\n','informed to RM supplier \r\nin future all material size will be taken as per process sheet.','Instead of Quarantine the RM, Parts took for machining.\r\nCAPA found okay and supplier informed about shortage of RM','','2015-01-18','Narayanappa(G)','Sathish Y.R.,PAVAN KUMAR  S.K.,Manjunath K.N.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','3','no','HAAS','Narayanappa(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8127,'18-210B','Magellan Aerospace(Chalfont) Limited','BODY','5757','D321 40204 204','','D, ECN NR29999ST1KM15, NR29999ST2KF65, WQN DFB09775',1,'P/074113','','39480','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','OD Thread Damage.','After 7th operation threading will be done and parts will placed in wooden pallet and sent to\r\nfitting department.Parts are under investigation regarding when the parts are being damaged.','Planned to put sleeve for the threads for future batches and same will be maintained during fitting\r\nand part marking stage.','Planned to put sleeve for the threads for future batches and same will be maintained during fitting\r\nand part marking stage.','Next batch should be monitored so this NC is being open','','2015-01-19','Dinakar(K)','Shivaraj K S,Rajesh T,Nandeesha N,Krishnanaik J N,Hari Prasad,Girish V M,Dinakar K,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','0','FI','no','DX 200-2 ','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8128,'18-210B','Magellan Aerospace(Chalfont) Limited','BODY','5757','D321 40204 204','','D, ECN NR29999ST1KM15, NR29999ST2KF65, WQN DFB09775',1,'P/074113','','39479','','0000-00-00',NULL,'yes','no','no','no','yes','yes','no','no','no','19.00+0.021 ID Bore oversize 19.050mm measured.','All stage operation are completed, part bore over size is not noticed in milling, turning and fitting department.Deviation noticed in inspection (1no).\r\nBoring operation done in milling machine and after boring operation threading, drilling operations are carried out.\r\nWhile running boring operation 100% inspection is carried for Bore dimension.After this in turning or fitting small dent mark done and polishing done in bore.\r\nDue to not finding any route cause for this, planned to check the bore dimension 100% in all the stages.','Next batch WO no.40511,40512 parts 100% inspection done in milling and also again after threading operation completes.all the parts found ok.\r\nAgain after manual drilling bore dimensions checked and found ok.\r\nWe analyzed that after this batch production, part process was ok and there is no possibility of deviation. But due to manual error this type of error can happen and all the concern supervisors need to be monitor in next batches,\r\n','We analyzed that,part process was ok and there is no possibility of deviation in process. But due to manual error this type of error can happen and all the concern supervisors need to be monitor in next batches.and also awareness of part handling, checking the parts in process.\r\n','CAPA analysed and next batch production found okay and next batches will also be monitored.','','2015-01-19','Lohith(K)','Theerthappa K.N.,Shivaraj K S,Shivappa M B,Seetharamu D,Rajesh T,Krishnanaik J N,Hari Prasad,Girish V M,Girish S,Dinakar K,Devaraj K.C.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','0','FI','no','HAASVF2SS-2','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8129,'18-317A','Magellan Aerospace(Chalfont) Limited','PIN SIDE ROLLER','A0587U','F579 53066 200','S145','C',2,'P/074118','','37598','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','2no of parts missing at treatment house(GET).','Hence the part is stuck in the tank which cannot be taken out so 2 nos part missed in treatment house','Informed Treatment house and asked them to take proper actions so that next time it will not repeat again.','Informed Treatment house and asked them to take proper actions so that next time it will not repeat again.','CAPA found okay.','','2015-01-20','Dayananda(K.G.)','Veerandra(H.R.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','15744','POSTDN','no','Misc','Muniyappa(N)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8130,'18-102A','Magellan Aerospace Bournemouth','BARREL-STRUT','247348','D572 50463 200','S98 FHT','F',1,'RP400839','','38961','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','1) Dia 4.88MM holes oblong.','This was happened in drilling the part for dia 4.9 mm. Both the inside and outside holes are being deburred this will fold the burrs and pin will not enter. So again 4.9 mm drilling is done while doing this hole got ob longed.','Previously it was doing with the help of hand now we have planned to keep the part in V Block and butt the part and do the drilling, This will avoid the hand shakes while drilling and chances of holes getting ob longed is very less','Previously it was doing with the help of hand now we have planned to keep the part in V Block and butt the part and do the drilling, This will avoid the hand shakes while drilling and chances of holes getting ob longed is very less','Next batch will be monitored carefully.','','2015-01-21','Nagaraju(T)','Nagaraju(T)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','0','04','no','Misc','Nagaraju(T)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8131,'28-016','Magellan Aerospace New York  Inc.','STOP FITTING','571458-5','161A6119-1','15-5PH Per AMS 5659 ','N/C',1,'124982-3170_R0_C0','','39458','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','1)Thickness under size by 0.20MM.','Actually the part consists of 2 holes which has chamfer of 0.3 which was maximum at that stage.Due to that the part was grinded to make the chamfer proper and thickness got undersized.','Thickness and Chamfer dia will regularly watched. Because the chamfer at one end will be done manually. Chamfer will be maintained by regular checking. ','Thickness and Chamfer dia will regularly watched. Because the chamfer at one end will be done manually. Chamfer will be maintained by regular checking.','Next parts found okay. ','','2015-01-21','Nagaraju(T)','Pinto(N.L.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','0','05','no','Misc','Nagaraju(T)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8132,'35-182A','Saab AB','EDGE HOUSING','581308','423Z1121-5-02','','--A',1,'PA-1300 2014','','39355','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','1)Hole oblong by 0.30MM.','The drill bit got cut while drilling and while sparking hole got ob longed by 0.30 mm.','Should calculate and change the drill bit according to the life of it.Because this drill will be carried out with 90 degree hand gun drilling machine.','Extra care will be taken and asked for CAD to develop any plan to drill the part. Pressure will be maintained at the end point of the drill to avoid these mistakes','Next batches found good.','','2015-01-21','Nagaraju(T)','Raghu(A.N.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','0','05','no','Misc','Nagaraju(T)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8133,'35-178','Saab AB','SUPPORT-SEAL-RETAINER','428596B','423Z1833-3-02','','---',1,'PA-1300 2014','','40177','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Wall thickness minus, (t-2.5 +/- 0.25mm but measured 2.10mm)','Operator not correct A0 or rotary zero in work offset, part machining in sum angles ,so wall thick measured taper, part rejected.  ','This is manual error, check wrong offset and identify , stop the m/c Again taken work offset correctly, and run the\r\nmachine.Instruct to value of operator work, responsibility of operator. ','Instruct to operator every work or tool offset taken cross check two times.','Repeated reasons! Since the operator was new warning has been issued. Next production batches will be keenly monitored','','2015-01-22','Rangaswamy()','Manohara(B.C.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Rangaswamy()','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8134,'40-002','Universal Engineering Limited','JOINT PLATE ','365430','D574 50014 201','','A, ECN NG23774ST2KF47',1,'320402 - S1','','39766','','0000-00-00',NULL,'yes','yes','yes','','','','','','','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, \r\n1.Location pins diameter changed and amended in MPS. \r\n2.Dia 6 and Dia 5 mm locating pins introduced to avoid wrong locating of part in operation-03. \r\n3.New program created for dia 5 H7 hole.','Process sheet updated, Next batch will be taken care','','2015-01-22','Anjinamurthy(H)','        Anjinamurthy H','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8135,'18-120C','Magellan Aerospace Bournemouth','HOUSING OUT B D BRG 3','230699','D275 56121 200','','E01,  ECN NG27011ST1KA83',1,'RP400843','','39254','','0000-00-00',NULL,'yes','no','yes','no','yes','no','no','no','no','Outer diameter -0.006micron.','In OD roughing setup  running time insert will be chipped\r\nout and part will came in plus side and that part not  \r\nchecking the operator and for next part he found out part \r\nwill become over sized and he change the insert and\r\nmaintain the outer dia in required size. but previous part \r\nnot maintain in proper diameter. So in the finishing setup that part loading time finishing tool get the more stock and chips will be rubbed in the outer diameter and part will be -.006 micron under sized. So part will become \r\nrejected.\r\n','checking the all parts outer and inner diameter before \r\nloading in the finished setup and change the previous \r\ninsert tip and .2 plus taken in the wear offset and run the part and after check the diameter and give the proper\r\ncorrection and run the part and check the part found ok. \r\nand after every 15 to 20 ns chnge the finished inserttip   \r\nand run the part so this problem not repeated again.\r\n','In roughing setup for every part check  outer and inner diameter for using air gauge. In finishing set up every 15 to 20 ns change the finished insert tip  and run the part so this problem not repeated again.\r\n','CAPA found satisfactory.Next batches found okay','','2015-01-23','Dinakar(K)','Bharath R,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','9','no','QT100S-2','Sandhesh D(S)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8136,'18-120C','Magellan Aerospace Bournemouth','HOUSING OUT B D BRG 3','230699','D275 56121 200','','E01,  ECN NG27011ST1KA83',1,'RP400843','','39253','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','outer diameter dig mark.','After finishing the milling operation we are done outer diameter and inner diameter finishing operation and check the all parts by using air gauge but not get the any deviation parts, after this parts moved to milling, for \r\ndrilling operation and then parts moved to fitting for \r\ndeburring.After all the operation parts moved to A/C mazak for part marking and this time we are check 100 percent for all the parts.and found out 1nr OD polished part and that one point part will -.012 undersize so part will be rejected.\r\n','After this issue we are desided and instruction given to\r\noperator  before loading the every part visually check the all parts before loading. and if get  any dammage or deviation parts don’t run the such type of parts and inform to concerned supervisors and clear the deviation parts. \r\n','After this issue we are desided and instruction given to\r\noperator  before loading the every part visually check the all parts before loading. and if get  any dammage or deviation parts don’t run the such type of parts and inform to concerned supervisors and clear the deviation parts. \r\n','CAPA found okay. Next batches also found okay.','','2015-01-23','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','09','no','Misc','Sandhesh D(S)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8137,'35-228A','Saab AB','HINGE BRACKET 2 ','108532B3','D576 50005 205','','D00',1,'1600099854','','40724','','0000-00-00',NULL,'yes','yes','yes','','','','','','','CHF measures plus side in dia 22.225 hole.','While proving the First off part, operator not entered the CRC value for dia 12 x 45 deg chf tool.\r\nSue to this manual error chamfer diameter measures 1mm plus side.','CRC value entered in machine tool wear and continued production and part inspected and found ok.','Planned to make dedicated tools for A320 brackets chamfering and program will alter to single line program to avoid manual errors.\r\nOnce we changed the program, chamfer diameter will control by program and tool. ','CAPA found okay.Implementation of planning to be done','','2015-01-23','Rangaswamy()','        Rangaswamy ','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8138,'35-228A','Saab AB','HINGE BRACKET 2 ','108532B3','D576 50005 205','','D00',2,'1600099854','','40724','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Bore chamfer over size by 0.3mm (Requred by +/-0.3mm)','Chamfer tool setting time chamfer over size, this is operator mistake  due to tool cutting edge height deviation. ','Under process..','Under process..','Rework will be done after booking new GRN from Stores and new work order issued.','','2015-01-23','Rangaswamy()','Sundar D.K.,Subramanya L Naik,Rangaswamy ,Punith G S,Manukumar H M,Manohara B.C.,Mahesh N,Karthineyan V.S.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','','FI','yes','BMV 45-1','Nagaraj(G. Nadiger)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8139,'30-016A','Gardner Aerospace-Derby Limited','FRAME MID RIB IFS - RH ','676083A9','L575 51892 201','7010 T7651 ABM3-1029','A, ECN:PG60049M01JA74',1,'LPR0000511','','40355','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','5Axis program problem,inside pocket wall broken.','1) Proved 3 sub program merged to single Program , re-Post and transfer to machine. Program running on machine that time tool dig on the part.\r\n2) proved NC program merged to reduce the cycle time. ','Informed and called the software application engineer.\r\n  ','Informed and called the software application engineer.','Under discussion with application engineer why that problem happened.','','2015-01-23','Ramesh(Poojary)','Siddaramappa ,Gajendra Singh C.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','3','no','VR11','Narayanappa(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8140,'30-016A','Gardner Aerospace-Derby Limited','FRAME MID RIB IFS - RH ','676083A9','L575 51892 201','7010 T7651 ABM3-1029','A, ECN:PG60049M01JA74',0,'LPR0000511','','40355','','0000-00-00',NULL,'yes','','yes','','','','','yes','no','Dummy NC refer NC No 8139','Dummy NC refer NC No 8139','Dummy NC refer NC No 8139','Dummy NC refer NC No 8139','Dummy NC refer NC No 8139','','2015-01-24','Narayanappa(G)','        Siddaramappa ','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8141,'18-319A','Magellan Aerospace Bournemouth','HALF CLAMP ','8031','D574 50552 200','DTD 5014','B01',1,'RP400946_Amnd_No.1','','40584','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Dig mark on outer profile.','Running time part clamp loosened and dig mark observed.\r\nThis deviation observed first time and due to process stability,this type of problem is not analyzed for this part.\r\n \r\n\r\n','Clamping method improved to improve strength.New clamps are manufacturing and same to be included in MPS.\r\nLocation holes introduced for clamp, this will not allow to move the clamp.','After changing the new clamp design, Production continued and process stabilized.\r\n','CAPA found okay. Regarding process stabilization next batch should be monitored','','2015-01-24','Anjinamurthy(H)','        Mohan Kumar C.M.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8142,'35-228A','Saab AB','HINGE BRACKET 2 ','108532B3','D576 50005 205','','D00',1,'1600099854','','40724','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Not edit \"D\" no  for dia 12 x 45 deg chf program.','While proving the First off part, operator not edit \"D\" no  for dia 12 x 45 deg chf program. Sue to this manual error chamfer diameter measures 1mm plus side.','Edit \"D\" no  for dia 12 x 45 deg chf programs and continued production and part inspected and found ok.','Planned to make dedicated tools for A320 brackets chamfering and program will alter to single line\r\nprogram to avoid manual errors. Once we changed the program, chamfer diameter will control by\r\nprogram and tool.','Repeated Preventive action. Before changing the program discuss with CAD and MR pls change MPS revision.','','2015-01-24','Rangaswamy()','        Rangaswamy ','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8143,'18-295A','Magellan Aerospace Bournemouth','BOLT','A0484U','D577 56145 200','S80','A',1,'RP400846','','40238','','0000-00-00',NULL,'yes','yes','yes','','','','','','no','running time 2.8 drill brocken so part nogo pin ansered so part rejected...','','','','Under discussion with customer and QAD, Chances of part getting okay is there very much so part under quarantined.','','2015-01-24','Anjinamurthy(H)','        Diwakar R.B.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8144,'35-230A','Saab AB','HINGE BRACKET 3 ','108532B3','D576 50006 205','','D00',1,'PA 1217 2014-2015','','40638','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Bore chamfer over size by 0.3mm (Required by +/-0.3mm)','Chamfer tool setting time chamfer over size, this is operator mistake due to tool cutting edge height deviation.','under process','under process','Rework under progress and New GRN, New Workorder to be raised so this NC is being Closed to do rework of the parts','','2015-01-24','Girish(Prasad P)','Sundar D.K.,Subramanya L Naik,Manukumar H M,Manjunath  M,Gurukiran S M,','','0000-00-00','BORE CHAMFER OVERSIZE.','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','','FI','yes','MakinoF5-2','Avinash(R.J.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8145,'18-003A','Magellan Aerospace Wrexham','BRACKET SUPPORT','6793701','D361 50111 200','ABM3 1029 T7651','A',56,'RP125887','01','40612','','0000-00-00',NULL,'no','yes','no','yes','no','yes','no','no','no','GF wrong marking.','Wrong marking done without checking GF & also cutting done & not checked as per layout from operator & authorized person, so parts rejected.','','Mark a billet for all CRN’s as per layout, get the same inspected and signed by store authorized person before cutting.  ','CAPA found okay. But Signing for the layout should be included in QMS.','','2015-01-27','Nagaraja (G)','Devaraja (M S)','','0000-00-00','GF wrong marking.','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','01','no','Misc','Anjinamurthy(H)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8146,'18-003A','Magellan Aerospace Wrexham','BRACKET SUPPORT','6793701','D361 50111 200','ABM3 1029 T7651','A',31,'RP125887','','40613','','0000-00-00',NULL,'no','yes','yes','yes','no','no','no','no','no','GF wrong marking.','Wrong marking done without checking GF & also cutting done & not checked as per layout from operator & authorized person, so parts rejected.','','Mark a billet for all CRN’s as per layout, get the same inspected and signed by store authorized person before cutting.  ','CAPA found okay. But Signing for the layout should be included in QMS.','','2015-01-27','Nagaraja (G)','Devaraja (M S)','','0000-00-00','GF wrong marking.','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','01','no','Misc','Anjinamurthy(H)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8147,'18-413B','Magellan Aerospace Bournemouth','ACTUATOR HOUSING','6957','D278 50162 200','','A',1,'RP401021_Amnd No. 1','','40547','','0000-00-00',NULL,'yes','yes','yes','','','','','','','6mm thikness (-side)5.91\r\n ','Setting time for first part altering the program and then run the part after roughing only 0.1 stock for finishing tool so chattering came in finished part so for that part polishing the chattering and it will become 0.1 over sized for that part without identification move to for next\r\nsetup.in that set up they are maintaining the total length for all parts in same size so thickness 6mm -0.1 under sized so part rejected. ','Check the program before running the next part and alter the program for correct size (dimension). And run the part. and proper stock given for finished tool and adjust the tool (blade)lenght if required size,so chattering problem will avoiding and check the groove width it will found ok. ','Marking the blade length, for next every batch all are maintaining the same length for this CRN. And maintain proper stock for finishing tool. insert not seated in the finishng tool so next batch new (blade) tool used for finishing pass.\r\n','Repeated rejections found on this CRN. CAPA accepted next parts also found okay. But next batch will be monitored.','','2015-01-27','Dinakar(K)','        Shivanand D.B.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8148,'42-002','RAFAEL','PSA BASE','K10597','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','','39403','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Part accepted.','Part accepted.','Part accepted.','Part accepted.','Part accepted.','','2015-01-27','Krishna(Chowdary.G.P.)','Lohith(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','With Treatment','','00','no','Misc','Lohith(K)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8149,'18-417A','Magellan Aerospace(Blackpool) Limited','BRACKET','M362250/72801','PI55-2120004-00','','NIL',1,'P/501902','','37879','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1)Hole pitch under size by 0.03MM. ','1) Hole enlarged in two stages due to controlled tolerance.During semi finishing hole was checked\r\nand found correct and checked by using CMM. 2) Later finishing operation was carried out in Jig\r\nboring machine and hole position out due to tool overhang.\r\n','Planned to carry out in one setup with carbide drill and hole mill that will eliminate the\r\naccumulating error of 2 set up. \r\nInspection method changed to CMM instead of 2D height gauge.','Planned to carry out in one setup with carbide drill and hole mill that will eliminate the\r\naccumulating error of 2 set up. \r\nInspection method changed to CMM instead of 2D height gauge.\r\n','Waiting for next batch to measure effectiveness.','','2015-01-27','Avinash(R.J.)','Sudhagar(V)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','0','FI','no','Misc','Sudhagar(V)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8150,'18-416A','Magellan Aerospace(Blackpool) Limited','BRACKET','M362250/72801','PI55-2119004-00','','NIL',1,'P/501835','','37878','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1)Hole pitch under size by 0.02MM.','1) Hole enlarged in two stages due to controlled tolerance.During semi finishing hole was checked and found correct and checked by using CMM.\r\n2) Later finishing operation was carried out in Jig boring machine and hole position out due to tool overhang.  ','1) Planned to carry out in one setup with carbide drill and hole mill that will eliminate the accumulating error of 2 set up.\r\n\r\n2) Inspection method changed to CMM instead of 2D height gauge.','1) Planned to carry out in one setup with carbide drill and hole mill that will eliminate the accumulating error of 2 set up.\r\n\r\n2) Inspection method changed to CMM instead of 2D height gauge.','Waiting for next batch to measure effectiveness.','','2015-01-27','Avinash(R.J.)','Sudhagar(V)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','0','FI','no','Misc','Sudhagar(V)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8151,'18-280A','Magellan Aerospace(Chalfont) Limited','DOOR OUTER TYPE 15','508103','L572 53722 200','ABS5032A055','B00',2,'P/074117','','39447','','0000-00-00',NULL,'no','yes','yes','yes','no','no','no','no','no','Materil bend op 03 pending.','After 1st operation part was bend, Part not butting in 2nd setup, so op03 pending .','under process','under process','Part bend removed and rework to be done for this new GRN along new work order to be raised so this NC is being closed','','2015-01-27','Rangaswamy()','Rangaswamy()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Manufacture Only','','03','yes','Misc','Rangaswamy()','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8152,'18-102A','Magellan Aerospace Bournemouth','BARREL-STRUT','247348','D572 50463 200','S98 FHT','F',19,'RP400839','','38617','','0000-00-00',NULL,'no','yes','no','yes','no','no','no','no','yes','Temporary protection not done.  Corrosion noticed on Qty 19 nos out of Total qty 60.','parts are Accepted','parts are Accepted','parts are Accepted','parts are Accepted','','2015-01-28','Nandishkumar(D.K.)','Narasimha Murthy(R)','RDN00102','2015-01-27','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','Manufacture Only','','CUST END','no','Misc','Muniyappa(N)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8153,'18-217A','Magellan Aerospace(Chalfont) Limited','BUSH SLIDING CON DRIVEN','B2851A','L579 51151 200','S145 FHT','A00',6,'P/068956','','32996','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Bore Diameter tapered & undersized 25.400/5.433','This was happened due to error in handling bore gauges and also while setting the pressure.\r\n','Air gauges has been introduced and parts in the production batches and Finished Goods found okay.','Air gauges has been introduced and parts in the production batches and Finished Goods found okay.','Next batches found okay','C32531','2015-01-28','Muniyappa(N)','Nandishkumar(D.K.)','CAR S-000384','2014-10-14','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','CUST END','no','Misc','Muniyappa(N)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8154,'18-219A','Magellan Aerospace(Chalfont) Limited','BUSH SLIDING DRIVEN ECC','B2275A','L579 51156 200','S145 FHT','A00',2,'P/074115','','34590','','0000-00-00',NULL,'yes','no','no','no','yes','no','no','no','yes','Bore Diameter tapered & undersized 26.721/26.700','','','','','C32533','2015-01-28','Muniyappa(N)','Nandishkumar(D.K.)','CAR S-000385','2014-10-14','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','CUST END','no','Misc','Muniyappa(N)','no',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8155,'18-219A','Magellan Aerospace(Chalfont) Limited','BUSH SLIDING DRIVEN ECC','B2851A','L579 51156 200','S145 FHT','A00',2,'P/074115','','34591','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Bore diameter tapered & undersized 26.721/26.700','','','','','C32533','2015-01-28','Muniyappa(N)','Nandishkumar(D.K.)','CAR S-000386','2014-10-14','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','CUST END','no','Misc','Muniyappa(N)','no',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8156,'18-392B','Magellan Aerospace Bournemouth','END COVER','5968','D278 50167 200','','D',1,'RP401023_Amend No.-1','','40479','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Hole oversize.','1)6.60/6.68 drill running time pin tight.\r\n2)6.64 drill not available.(available in 6.605)\r\n3)Reworktime step occured.\r\n4)Again Rework time part rotate hole will be ablounged.  \r\n','Inform to tools department to purchase Dia 6.64 drill.orderd by tools department next batch using\r\nthe correct size drill.\r\n','Next batch using the correct size drill and maintain any time stock 2nos.  \r\n','CAPA found okay but next batch will be monitored as per CAPA','','2015-01-29','Dinakar(K)','Raghavendra Rao(R)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Narasimhamurthy(K.G.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8157,'18-429A','Magellan Aerospace Bournemouth','CLEAT','0709701A','L575 52435 200','','A00',2,'RP404750','','40822','','0000-00-00',NULL,'yes','','yes','','yes','','','','','Rib thickness minus size 0.5mm\r\n','Makino m/c program running in hass m/c program running time x&y coordinate ate time not moving so part minus side.','Immediately inform  to Haas  engineer and change the program method.\r\nInform the operator, incase makino program taken Immediately inform to supervisor editing and after run  the program.\r\nWhen G00 activated in program change G01 F12000    \r\n','Immediately inform  to Haas  engineer and change the program method.\r\nInform the operator, incase makino program taken Immediately inform to supervisor editing and after run  the program.\r\nWhen G00 activated in program change G01 F12000    \r\n','CAPA found okay. Next batches also found okay.','','2015-01-30','Lohith(K)','                Punith G S','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8158,'18-030A','Magellan Aerospace Bournemouth','PIN','W72976','D278 50156 200','S130 FHT','A',14,'RP400838','','36864','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','14nos of parts missing at treatment house(API). ','14 numbers found short in the qty received from treatment supplier. ','Instructions given to Supplier, and asked for the root cause and also asked them not to happen this types of failures in futures.','As the part is very small in size, this problem happened, some times the parts will get stuck into the tanks during treatment house. Instructions has been passed to treatment house and if required Credit note and Supplier NC will be raised.','Missing of parts cannot be acceptable and even though the size the part is less but it will assemble to aircraft , asked respected department head to take necessary actions.','','2015-01-30','Dayananda(K.G.)','Veerandra(H.R.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','14773','postdn','no','Misc','Muniyappa(N)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8159,'18-101A','Magellan Aerospace Bournemouth','TUBE-STRUT','251469','D572 50464 202','T45','F',1,'RP400839','','38443','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','OD DIG MARK.','During RM cutting blade was loose & OD dig mark happened.','Check blade tightness & cutting should be done.','Check blade tightness & cutting should be done.','Next parts found good','','2015-01-30','Sunil Kumar(K.R.)','Shivanand D.B.,','','0000-00-00','RENUKA PRASDA.','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','FI','no','ST20','Narasimha Murthy(R)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8160,'18-210B','Magellan Aerospace(Chalfont) Limited','BODY','5757','D321 40204 204','','D, ECN NR29999ST1KM15, NR29999ST2KF65, WQN DFB09775',1,'P/074113','','39479','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','OD Thread damage.','After 7th operation threading will be done and parts will placed in wooden pallet and sent to fitting department.Parts are under investigation regarding when the parts are being damaged.','Planned to put sleeve for the threads for future batches and same will be maintained during fitting and part marking stage.','Planned to put sleeve for the threads for future batches and same will be maintained during fitting and part marking stage','Next batch should be monitored so this NC is being open','','2015-01-31','Avinash(R.J.)','Nandishkumar(D.K.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','16353','POST DN','no','Misc','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8161,'18-385A','Magellan Aerospace(Chalfont) Limited','NUT RING OUTER','242098','D575 40038 202','','A',1,'P/074123','','38415','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dia 1.3 drill bit broken.','While drilling 1.6 diameter burr got folded so drill got cut and dia oversize.Drill will happen the\r\ngrove section of the part hence it is very difficult to judge when drill get cut','Instructed operator to drill slowly and while grinding the tool check it properly and while drilling\r\nkeep the angle properly.','Instructed operator to drill slowly and while grinding the tool check it properly and while drilling\r\nkeep the angle properly.','Next parts found okay. Repeated NC should be avoided','','2015-02-01','Nagaraju(T)','Nagaraju(T)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','11','no','Misc','Nagaraju(T)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8162,'18-317A','Magellan Aerospace(Chalfont) Limited','PIN SIDE ROLLER','A0587U','F579 53066 200','S145','C',10,'P/074118','','38502','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dia 1.6 drill broken.','While drilling 1.6 diameter burr got folded so drill got cut and dia oversize.Drill will happen the grove section of the part hence it is very difficult to judge when drill get cut','Instructed operator to drill slowly and while grinding the tool check it properly and while drilling keep the angle properly.','Instructed operator to drill slowly and while grinding the tool check it properly and while drilling keep the angle properly.','Next parts found okay. Repeated NC should be avoided','','2015-02-01','Nagaraju(T)','Nagaraju(T)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','5','no','Misc','Nagaraju(T)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8163,'35-226A','Saab AB','HINGE BRACKET 1','688803A6','D576 50004 207','','D00',1,'1600099854','','40908','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Dig mark on part.','While running Dia 25r2 pocket roughing MIRROR activation not done and dig mark observed on part.\r\nAll the programs are Proved but due to RM thickness deviation, program altered. While altering the program manual error happened.\r\n','MIRROR activated and continued production, next part found ok.','Educated the Supervisor and Operators to use the options in machine.(MIRROR, TRANS, ROTATION)\r\nInformed to CAD/CAM to simulate the program before issuing to machine.\r\n\r\n\r\n','CAPA found okay','','2015-02-02','Girish(Prasad P)','        Sundar D.K.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8164,'01-312','HAL-Helicopter','CASING RING-AFT','FG14FY199','201C 637H 0000 211','7075.T 7351','NA',1,'ALHOS12-42','','37721','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','*part was rotted so rib thickens undersize.  ','* Due to part clamping not done correctly, this deviation coming.\r\nOperator done a mistake and he is not observed the part butting, bolts tightening while loading the part in fixture.\r\n','*We entered the message in program to alert the operator for every part. Optional stop given to check the part butting and clamping.\r\n','*We entered the message in program to alert the operator for every part. Optional stop given to check the part butting and clamping.\r\n','CAPA found okay. Next parts also found okay','','2015-02-02','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','05','no','Misc','Anjinamurthy(H)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8165,'01-312','HAL-Helicopter','CASING RING-AFT','FG13JY168','201C 637H 0000 211','7075.T 7351','NA',1,'ALHOS13-54','','37717','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','*tool offset not taken so part dig mark.','*  Due to operator mistake this error happened. Operator not taken tool offset while loading the tool to machine magazine.\r\n','* This type of manual error should avoid by following the methods.\r\nWe introduced a method that tool name, tool no and tool length compensation value to be entered in reference book.\r\nThis will avoid such manual errors in future. ','We introduced a method that tool name, tool no and tool length compensation value to be entered in reference book.\r\nThis will avoid such manual errors in future. \r\nSupervisor will monitor this method in all the machines.','Refrence copy needed to close this NC.','','2015-02-02','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','00','no','Misc','Anjinamurthy(H)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8166,'18-358A','Magellan Aerospace Bournemouth','FITTING HNG POINT SP 2 OB','547010','L575 52439 200','','A00',2,'RP400948_Amnd-01','','40755','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Part bore out-of tolerance. (10 to 15 mic).  ','While part running time bore chartering so bore over size .Due to process problem','Immediately stop the boring operation and Inform to operator when change the process after continue the production.  ','Next batch production running time new fixture and added one more extra operation. \r\nInform to operator when boring operation running time inform the concern the supervisor and load the new fixture.','Waiting for next batch for effectiveness and new fixture.','','2015-02-02','Girish(Prasad P)','        Prashanth Kumar M','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8167,'18-054B','Magellan Aerospace Bournemouth','CLEAT','452080','L575 52580 200','','A00',1,'RP400836','','40698','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Part bib thickness under size 1 mm..','Due to part 1st set up running time location hole 1 mm shifted. Operator 2nd setup part machining\r\ntime not observed.','Immediately inform to the concern supervisor and all 1st setup committed parts cross cheeked, then\r\nrun next part and inspect found ok.','In future 2nd setup loading time check the 1st setup location coordinates, after run the programs. Instructed\r\nto operator every part loading time observe in location pin and location hole over size. When\r\nLocation hole over size or shifted inform the concern supervisor immediately.','Next parts found okay','','2015-02-02','Girish(Prasad P)','                Prashanth Kumar M','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8168,'18-213A','Magellan Aerospace(Chalfont) Limited','END CAP ','20740','D321 40209 200','','A, ECN NR29998ST1JA76',25,'P/074114','','37792','','0000-00-00',NULL,'yes','no','no','no','yes','no','no','no','yes','batch of End caps where the anodize on the thread appears to be stripped off    by re-tapping process\r\n','','','','Under review','C33737','2015-02-02','Avinash(R.J.)','Muniyappa(N)','Through Mail.','2015-02-02','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','CUST END','no','Misc','Muniyappa(N)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8169,'35A-239A','Saab AB','L/H KIT FOR ARD HINGE / J','','9901503-993','','Exhibit-B',50,'1600093863 Rev-2','','K03794','','2014-12-27',NULL,'yes','yes','no','no','no','no','no','no','yes','1)All of HINGE 1 ASSY for -993 had chamfer size between 0,9-1,0mm. Should be 0,2-0,8mm.\r\n\r\n2)For -993 2/50 pcs of D57650009 did not line using our inspection tool so the hole diameter is under requirement.\r\n','1) The measuring method used for chamfer was not robust with which deviations of less than 0.1 mm was not being noticed.\r\n\r\n2) The diameter and the concentricity of the part were checked no sooner upon completion of the lapping of the part.  The part upon lapping will experience some heat and was found that they shrink after cooling by around 10~12 microns.  ','1) The parts in FG before and after assembly were quarantined immediate upon noticing the problem and were cross checked for the failed parameters.\r\n\r\n2) The process layout of manufacture and assembly of the parts were checked and found to have no variance with the process but in the inspection methods.','1) Checking the chamfer by calculated diameter of chamfer is introduced and also cross verification by profile projector.\r\n\r\n2) The bore diameters are to be verified after an hour of lapping of the parts.\r\n\r\n3) The bores shall be checked for diameters using air gauges apart from the concentric plug gauge.','A batch of 50-sets manufactured checked 100% by the above changed methods of inspection and found to be satisfactory.','C34413','2015-02-03','Avinash(R.J.)','Manjunath(G)','Through mail on 30th JAN 2015 by Marcus','2015-01-30','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','Customer End','yes','Misc','Manjunath(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8170,'35A-240A','Saab AB','R/H KIT FOR ARD HINGE / J','','9901503-994','','Exhibit-B',50,'1600093863 Rev-2','','K03795','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','1)All of HINGE 1 ASSY for -944 had chamfer size between 0,9-1,0mm. Should be 0,2-0,8mm.\r\n2)For -994 25/50 pcs od D57650010 did not line using our inspection tool so the hole diameter is under requirement.\r\n\r\n','1) The measuring method used for chamfer was not robust with which deviations of less than 0.1 mm was not being noticed.\r\n\r\n2) The diameter and the concentricity of the part were checked no sooner upon completion of the lapping of the part.  The part upon lapping will experience some heat and was found that they shrink after cooling by around 10~12 microns\r\n','1) The parts in FG before and after assembly were quarantined immediate upon noticing the problem and were cross checked for the failed parameters.\r\n\r\n2) The process layout of manufacture and assembly of the parts were checked and found to have no variance with the process but in the inspection methods.\r\n\r\n','1) Checking the chamfer by calculated diameter of chamfer is introduced and also cross verification by profile projector.\r\n\r\n2) The bore diameters are to be verified after an hour of lapping of the parts.\r\n\r\n3) The bores shall be checked for diameters using air gauges apart from the concentric plug gauge.\r\n\r\n\r\n','A batch of 50-sets manufactured checked 100% by the above changed methods of inspection and found to be satisfactory.','C34414','2015-02-03','Avinash(R.J.)','Manjunath(G)','Through mail on 30th JAN 2015 by Marcus','2015-01-30','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','cust end','yes','Misc','Manjunath(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8171,'18-392B','Magellan Aerospace Bournemouth','END COVER','M510610','D278 50167 200','','D',1,'RP401023_Amend No.-1','','36350','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dia 6.61 H0le ablonged.','1)6.60/6.68 drill running time pin tight.\r\n2)6.64 drill not available.(available in 6.605)\r\n3)Rework time step occured.\r\n4)Again Rework time part rotate hole will be ablounged.','Inform to tools department to purchase Dia 6.64 drill.orderd by tools department next batch using the correct size drill.','Next batch using the correct size drill.','New drill available. CAPA found okay. Next batches also found okay.','','2015-02-03','Narasimhamurthy(K.G.)','Narasimhamurthy(K.G.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','05','no','Misc','Narasimhamurthy(K.G.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8172,'18-386A','Magellan Aerospace(Chalfont) Limited','NUT RING INNER','487664','D575 40039 200','','B',1,'P/074123','','37622','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','1.30mm drill bit cut.','The drilling is done with an angle of 45 degrees.\r\nDue to coolant not flowing properly and might be chances of not clamping the part to jig','1)Drill bit grinding will be done and checked again and again.\r\n2)Proper flow of coolant is monitored regularly\r\n3)Clamping will be ensured twice before drilling','1)Drill bit grinding will be done and checked again and again.\r\n2)Proper flow of coolant is monitored regularly\r\n3)Clamping will be ensured twice before drilling','CAPA found okay.Next batches found okay','','2015-02-03','Nagaraju(T)','Nagaraju(T)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','11','no','Misc','Nagaraju(T)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8173,'18-317A','Magellan Aerospace(Chalfont) Limited','PIN SIDE ROLLER','A0587U','F579 53066 200','S145','C',10,'P/074118','','38502','','0000-00-00',NULL,'yes','no','no','no','yes','yes','no','no','no','1. Drill cut dia 1.6- 3 Nos\r\n2. OD undersize- 3 Nos\r\n2. ID Thread NOGO answer - 4 Nos\r\n','1)While drilling 1.6 diameter burr got folded so drill got cut and dia oversize.Drill will happen the grove section of the part hence it is very difficult to judge when drill get cut. \r\n2)Due to while OD operation running time insert brokened so OD under size.3)while running time carbide threading tool broken.','1)Instructed operator to drill slowly and while grinding the tool check it properly and while drilling keep the angle properly.\r\n2)New insert added and tool offset takened run the part and checked the od dimension is ok continuve the production.  \r\n3)after running the every part check the carbide threading tool and load the next part.','1)Instructed operator to drill slowly and while grinding the tool check it properly and while drilling keep the angle properly. \r\n2)every 50 nos will be completed checked the insert.  \r\n3)change the carbide threading tool for every 100nos parts.  \r\n\r\n','CAPA found okay,next parts found okay','','2015-02-03','Dinakar(K)','Ningaraj A N,Manjunath  M,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','QT100S-1','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8174,'18-358A','Magellan Aerospace Bournemouth','FITTING HNG POINT SP 2 OB','547010','L575 52439 200','','A00',1,'RP400948_Amnd-01','','40755','','0000-00-00',NULL,'','','yes','','','','','','yes','* Part profile shift.','* Trans program running time m/c reset so operator not observed trans.','We will be cancelling all Trans for machines at the starting and ending time. If its in middle means trans will be taking place.   ','We will be cancelling all Trans for machines at the starting and ending time. If its in middle means trans will be taking place.  ','CAPA found okay. Next parts found okay','','2015-02-03','Girish(Prasad P)','        Rangaswamy ','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8175,'18-211B','Magellan Aerospace(Chalfont) Limited','PLUNGER','W71530','D321 40205 200','','H01, ECN NR29998ST1JB80',2,'P/074114','','40669','','0000-00-00',NULL,'','','yes','','','','','','','O.D undersize by(-)0.005 mm and 0.006.','In OD roughing setup running time insert will be breakage and part will OD oversize and that part not checking the operator and  part not maintain in proper stock for   finishing tool. So in the finishing setup that part loading time finishing tool get the more stock and coolant flows not correctly and chips will be over lapped in the outer diameter and part will be -.006 micron under sized. ','After roughing check the diameter and maintain the proper  stock for the finishing tool and run the part and adjust the coolant in insert edge coolant will be avioded the chips over lapping and every 15 to 20 ns chnge the finished insert tip and run the part so this problem again not repeated.\r\nagain. ','After roughing check the diameter and maintain the proper  stock for the finishing tool and run the part and adjust the coolant in insert edge coolant will be avioded the chips over lapping and every 15 to 20 ns chnge the finished insert tip and run the part so this problem again not repeated.\r\n','CAPA found okay. Next batch found okay.','','2015-02-03','','        Manjunatha N','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8176,'35-066A','Saab AB','7605450-200 ','3420701 3','L574 55450 200','','B00, PG74415001JA02',1,'1600087247 Rev 1','','36400','','2014-12-30',NULL,'yes','yes','no','no','no','no','no','no','yes','One of L57455450200 in the latest shipment has a scratch that is 0,8-1,0 mm deep.','During the machining of 5-axis mismatch between the vertical and the horizontal flanges noticed.  The part was cleared for treatments since the mismatch being within acceptable limit of 0.5 mm as per drawing. ','1) Upon immediate notice of the mail, the parts that were in progress were checked.\r\n\r\n2) The concerned Operators and Supervisors were instructed that a mismatch between the faces are allowed as per drawing but the cutter travel in depth has to be to the face of the base and must not travel beyond.','Process sheet accordingly changed to incorporate the point 2) of the corrective action.','','C34880','2015-02-03','Avinash(R.J.)','Manjunath(G)','Through Mail by Marcus on 03rd Feb.','2015-02-03','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','yes','With Treatment','16014','Customer End','no','Misc','Avinash(R.J.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8177,'35-066A','Saab AB','7605450-200 ','3420701 3','L574 55450 200','','B00, PG74415001JA02',1,'1600087247 Rev 1','','36400','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','One of L574 55450200 in the latest shipment has a scratch that is 0,8-1,0 mm deep.','Dummy NC','Dummy NC','Dummy NC','Dummy NC refer NC 08176','C34880','2015-02-03','Avinash(R.J.)','Manjunath(G)','Through Mail.','2015-02-03','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','CUST END','no','Misc','Avinash(R.J.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8178,'18-279A','Magellan Aerospace(Chalfont) Limited','DOOR OUTER TYPE 23','1867801','L572 53721 200','ABS5032A055','B00',1,'P/074117','','40774','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Base thickness minus. ','Part 2nd setup clamping in M6 (4nos) bolts & vacuum. but part cutout time holding only for vacuum.that time vacuum presser down so part thickness minus so part rejected.','Inform to supervisor & maintenance department,stop the production, service the vacuum pump then check vacuum presser then found ok. set vacuum presser switch in every point.','Next maintenance department service vacuum pump every 3 month and set vacuum presser switch in every point.   ','CAPA found okay. Next batches also found okay.','','2015-02-04','Rangaswamy()','Manohara(B.C.)','','0000-00-00','Base thick minus for vacuum pump problem.','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','03','no','Misc','Rangaswamy()','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8179,'18-054B','Magellan Aerospace Bournemouth','CLEAT','452080','L575 52580 200','','A00',1,'RP400836','','40698','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Part bib thickness under size 1 mm..','Due to part 1st set up running time location hole 1 mm shifted. Operator 2nd setup part machining time not observed. ','Immediately inform to the concern supervisor and all 1st setup committed parts cross cheeked, then run next part and inspect found ok.   \r\n     ','In future 2nd setup loading time check the 1st setup location coordinates, after run the programs. Instructed\r\nto operator every part loading time observe in location pin and location hole over size. When\r\nLocation hole over size or shifted inform the concern supervisor immediately.    ','Next parts found okay','','2015-02-04','Girish(Prasad P)','Prashantha(H.G.)','','0000-00-00','part bib thickness under size 1mm..','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Girish(Prasad P)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8180,'18-358A','Magellan Aerospace Bournemouth','FITTING HNG POINT SP 2 OB','547010','L575 52439 200','','A00',1,'RP400948_Amnd-01','','40755','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Part bore out-of tolerance.(10 to 15 mic).','While part running time bore chartering so bore over size .Due to process problem.','Immediately stop the boring operation and Inform to operator when change the process after continue the production.','Next batch production running time new fixture and added one more extra operation. \r\nInform to operator when boring operation running time inform the concern the supervisor and load the new fixture.','Waiting for next batch and new fixture to be done','','2015-02-05','Girish(Prasad P)','Prashantha(H.G.)','','0000-00-00','bore division....','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Girish(Prasad P)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8181,'18-009A','Magellan Aerospace Wrexham','Plate Cover','497610','D572 52519 200','L97 T351','A',1,'RP125888','','40797','','0000-00-00',NULL,'','','yes','','','','','','no','opertar mistake','In this stage 2 operations will occur, while machining air pressure got low after 20 min when pressure got normal operator ran program from beginning.','A separate stop will be created for each operations for any reason program from start cannot be machined. And asked maintenance department to create backup for these issues ','A separate stop will be created for each operations for any reason program from start cannot be machined. And asked maintenance department to create backup for these issues','CAPA found Okay.. New compressor has been planned separately.','','2015-02-05','','        SHIVAKUMAR ','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8182,'18-392B','Magellan Aerospace Bournemouth','END COVER','M510610','D278 50167 200','','D',5,'RP401023_Amend No.-1','','36350','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','no','  Delta FAIR not done for the fixture of above part number which use to checks hole position and outer profile. There is no proper identification number and history card for the fixture.','','','','Under review','','2015-02-06','Muniyappa(N)','Nandishkumar(D.K.)','RDN00104','2015-02-03','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','CUST END','no','Misc','Muniyappa(N)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8183,'18-392B','Magellan Aerospace Bournemouth','END COVER','5968','D278 50167 200','','D',169,'RP401023_Amend No.-1','','40479','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','no','  Delta FAIR not done for the fixture of above part number which use to checks hole position and outer profile. There is no proper identification number and history card for the fixture.','','','','Under review','','2015-02-06','Muniyappa(N)','Nandishkumar(D.K.)','RDN00104','2015-02-03','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','CUST END','no','Misc','Muniyappa(N)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8184,'18-391B','Magellan Aerospace Bournemouth','END COVER','R3856','D278 50166 200','','A',13,'RP401022_Amend No 1','','39243','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','no','  Delta FAIR not done for the fixture of above part number which use to checks hole position and outer profile. There is no proper identification number and history card for the fixture.','','','','Under review','','2015-02-06','Muniyappa(N)','Nandishkumar(D.K.)','RDN00105','2015-02-03','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','CUST END','no','Misc','Muniyappa(N)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8185,'18-391B','Magellan Aerospace Bournemouth','END COVER','5672','D278 50166 200','','A',20,'RP401022_Amend No 1','','39241','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','no','  Delta FAIR not done for the fixture of above part number which use to checks hole position and outer profile. There is no proper identification number and history card for the fixture.','','','','Under review','','2015-02-06','Muniyappa(N)','Nandishkumar(D.K.)','RDN00105','2015-02-03','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','CUST END','no','Misc','Muniyappa(N)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8186,'18-086B','Magellan Aerospace Wrexham','PLATE SEALING','432758','D572 52913 200','ABM3 1029','B',62,'RP127524','','40718','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','no','It is found that Un-controlled gauge is used to certify Hole position. Validation of change of inspection method is not done.\r\n \r\n','','','','Under review','','2015-02-06','Muniyappa(N)','Nandishkumar(D.K.)','RDN00106','2015-02-06','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','CUST END','no','Misc','Muniyappa(N)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8187,'18-295A','Magellan Aerospace Bournemouth','BOLT','A0484U','D577 56145 200','S80','A',1,'RP400846','','40238','','0000-00-00',NULL,'yes','yes','yes','','','','','','','od thread no go answer','Thredding insert changing time Thread pitch micro meter error.operator not checking the micro meter the reading is eror in 0.05mm thread effective dia will undersize.so thread nogo answerd.','Next time supervisor instructed to operator threading insert changing time first checking the thread pitch micro meter master checking and adjusted zero after running the part.','Next time supervisor instructed to operator threading insert changing time first checking the thread pitch micro meter master checking and adjusted zero after running the part','CAPA found okay, next batch found satisfactory ','','2015-02-06','Dinakar(K)','        Nataraja C V','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8188,'18-102A','Magellan Aerospace Bournemouth','BARREL-STRUT','247348','D572 50463 200','S98 FHT','F',1,'RP400839','','39664','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','total lenght -0.5 undersized.','The Following route cause analyzed for the parts rejected, Jaws Boring is not good,part not butted properiy to the  jaws because of small chips are in Part butting faces.Roughing and Finishing inserts wear out.  \r\n','Roughing stage clean the jaws with the help of air and before loading the part.after clamping check the every part it was butted in the jaws face properly.','Roughing stage clean the jaws with the help of air and before loading the part.after clamping check the every part it was butted in the jaws face properly.','CAPA found okay. Next batches also found okay.','','2015-02-06','Dinakar(K)','Narasimhamurthy(K.G.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','05','no','Misc','Narasimhamurthy(K.G.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8189,'35-165A','Saab AB','HOUSING PIN','657736A5','423Z1124-5-01','','--A',1,'PA-1300 2014','','38000','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Black spot observed on the bore.','This was happened in Treatment house, due to some chemical mix up or some chemical dipped on this part black spot observed on bore','Instructed to treatment house and they are under investigation and also in our end','Instructed to treatment house and they are under investigation and also in our end','Under investigation, effectiveness will be reviewed after reply from Treatment house','','2015-02-07','Avinash(R.J.)','Manjunath(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','15731','Post DN','no','Misc','Manjunath(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8190,'30-110','Gardner Aerospace-Derby Limited','RIB CLOSING OUT BOARD L/H','434704 C','L575 59269 200-PF','','A00',1,'LPR0000645','','40853','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','wall thickness 2.00 +0.2/-0.1 mm measures 1.30 to 1.40mm','Wrong tool selection by the operator instead of Dia 6 ball nose,He had run Dia 8 ball nose.  ','Replace the tool & tool number with 6 ball nose,\r\nabsurve  the tool which has to be run.','Instructed to operator to cheek the tool & tool number before run the program. \r\nthe care will be taken to control the mistakes for the future quantities. ','CAPA found okay. Next batches also found okay.','','2015-02-07','Narayanappa(G)','Sathish Y.R.,PAVAN KUMAR  S.K.,Manjunath K.N.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','3','no','DMG 360L','Narayanappa(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8191,'40-004','Universal Engineering Limited','JOINT PLATE ','365428','D574 50016 203','','D, ECN NG23774ST2KE84',1,'320402 - S1','','40555','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Base thickness under size (0.25mm minus).','Due to  01 operation running time part bended so next (03)operation running time part not butting. ','Immediately  production stopped.Next part production running time cheang the programs and clamping method.\r\nInstructed to operator every part loading time check the butting face and observe the butting gap\r\nInstructed to operator every part loading time check the butting face and observe the gap. \r\nWhen part clamping time observe the gap remove the part  and inform the concern supervisor .    \r\n \r\n \r\n','Immediately  production stopped.Next part production running time cheang the programs and clamping method.\r\nInstructed to operator every part loading time check the butting face and observe the butting gap\r\nInstructed to operator every part loading time check the butting face and observe the gap. \r\nWhen part clamping time observe the gap remove the part  and inform the concern supervisor .    ','CAPA found okay. Next batches also found okay.','','2015-02-08','Lohith(K)','        Lohith K','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8192,'18-187A','Magellan Aerospace Bournemouth','BUSH','LO7469','L575 50337 200','B23','B00',1,'RP400846','','38785','','0000-00-00',NULL,'yes','no','no','no','yes','yes','no','no','no','ID bore 36.750mm/36.775mm measured 36.780mm','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.  ','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 the tool noise,coolant floaing and chips while running. ','CAPA found okay.Next parts found okay','','2015-02-09','Dinakar(K)','        Shivappa M B,SHIVAKUMAR ,Rajesh T,GUNDEGOWDA H.G.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','FI','no','DX 200-1','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8193,'18-104A','Magellan Aerospace Bournemouth','BODY TURNBUCKLE','239338','D575 40490 200','S80 FHT','E',2,'RP400840','','38881','','0000-00-00',NULL,'yes','no','no','no','yes','yes','no','no','no','ID Thread NOGO answered.','After 25nos running threading insert will be wear out.for next part threading insert will be changedand 0.4 plus(+)taken in wear offset and run the part but thread gauge was not answered then 0.2 minous(-) taken to wear offset and run the part that time thread gauge was nogo answered.  \r\n','For next part x-offset taken and taking 0.3 mm up in toolwear offset and run the part gauge not answerd,in x-offset give 0.1mm down and run the part and gauge not answered then in x-offset down0.05mm and run the part and then gauge answered and next part run in same reading &the part found okay.  \r\n','Instruction given to operator to take x-offset & z-offset whenever the inserts are changed and monitor supervisors. \r\n','CAPA found okay, next parts found good.','','2015-02-09','Dinakar(K)','S. Shiva Kumar,Rajesh B D,Manjunatha P,Manjunatha N.R.,KRISHNAMURTHY N,GUNDEGOWDA H.G.,Girish HP,Ashith B,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','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),(8194,'18-284A','Magellan Aerospace Bournemouth','SPINDLE FOR CLACK ALVES O','Y11518','A281-40019-200','S80 FHT','A',9,'RP400846','','40443','','0000-00-00',NULL,'yes','no','no','no','yes','yes','no','no','no','OD dent mark.\r\n','While doing OD turning operation part dig mark observed due to insert wear out.','Insert changed and checked the finishing of the part and then continued production.','As per insert chart displayed in machine, inform to operators to check the insert wear out and change the insert.','CAPA found okay','','2015-02-09','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','FI','no','Misc','Narasimha Murthy(R)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8195,'07-002A','HAL-NASIK','WALL 1 ROOT PART-LH','AS-3241','11.2000.2.101.004','V95pchT2','Nil',1,'NK/M/2513(4520)/MP/O','','37769','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','part negative wall dig  ','while running the negative wall in convention milling machine the spindle was running but in negative wall the spindle has to be taken safety side then he has to take the spindle to the home position, but he has not taken any safety position and he taken the spindle to home position, so wall dig.  ','instruction has been given to the operator to take care while running this type of part, and he has been guided by the supervisor how to take care while running this type of part. ','while running this type of part along with the operator the one another person who will be knowing about that part and machine will be given with operator he will instruct the operator and he will take care with the operator while machining. ','CAPA found okay, next batches found okay','','2015-02-09','Narayanappa(G)','Ravindra(Singh R)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','05','no','Misc','Narayanappa(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8196,'07-009','HAL-NASIK','HATCH COVER - RH','BS-24239','11.2000.2.151.001','V95pCHAT 1V-10','Nil',1,'NK/M/2513(4520)/MP/O','','36845','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','groove width over size ','groove width was 6.6mm but it was been running from standard cutter 6R1 it was taking long cycle time so tool was changed to 6.65mm cutter but in old program there was a trans when the new cutter changed operator should have removed the trans but with out removing trans machining done so groove width over size...','trans have been removed & continued the production ','in future before changing the tool instruction will be given to the cad cam and to the operator if there is any necessary to change it will be changed from the cad cam only operator will not edit any program.','CAPA found okay, next batches found good.','','2015-02-09','Narayanappa(G)','Paramesh(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','3','no','Misc','Narayanappa(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8197,'18-122A','Magellan Aerospace Bournemouth','FORKEND ASSEMBLY','518330','D572 50462 201','S98 FHT','J01',1,'RP400839','','38882','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','OD Thread NOGO answered.','Due to while thread running time thread insert brokened and broken insert is taking over cut and therad major dia will be undersize so thread NOGO answered.  \r\n','Next part thread insert changed and takened tool X-offset&Z-offset and maintained the thraed effective dia and soot the thread gauge,Gauge is answered and run the\r\npart.  \r\n','Inform to operator every 50 nos will be completed changed the insert and   takened tool X-offset&Z-offset and maintained the thraed effective dia and soot the thread gauge,Gauge is answered and run the part.  \r\n \r\n','CAPA found okay. Next batches also found okay.','','2015-02-09','Narasimhamurthy(K.G.)','Yarri Gowda,Shivanand D.B.,Seetharamu D,Ravi R,Raghavendra Rao R,Mohan Kumar C.M.,Manohara M,Girish V M,Dinakar K,Dhananjaya N,Ashith B,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','FI','no','DX 200-2 ','Narasimha Murthy(R)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8198,'18-415B','Magellan Aerospace Bournemouth','ACTUATOR HOUSING','95744A','D278 50163 201','','D',1,'RP401022_Amend No 1','','40581','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Bore Oversize SIZE BY (0.12MM).  \r\n','Insert was worn out operator failed to notice that and machined the part and found bore oversize.  ','Warned operators strictly to change the inserts after some quantity which is displayed in boards,and work ordershould entered regarding change of insert and first off should be done by qualityperson and get signed.  \r\n','Warned operators strictly to change the inserts after some quantity which is displayed in boards,and work ordershould entered regarding change of insert and first off should be done by qualityperson and get signed.  \r\n','CAPA found okay. After every 50 numbers Insert will be changed.','','2015-02-10','Narasimhamurthy(K.G.)','Devaraj(K.C.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Narasimhamurthy(K.G.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8199,'18-378B','Magellan Aerospace Bournemouth','GAMMA FITTINGS ','5348','NSA840020-250','','L',2,'RP401480_Amend No.-1','','40242','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','R/M lenght under sized.','While cutting blade teeth brokened so RM taper cut','Before cutting check blade teeth & tightness then cutting should be done.','Before cutting check blade teeth & tightness then cutting should be done.','Next parts found good.','','2015-02-10','Nagaraja (G)','Sunil Kumar(K.R.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','01','no','Misc','Sandhesh D(S)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8200,'18-119B','Magellan Aerospace Bournemouth','HOUSING OUT B DRG 3','CB894702','D275 40011 200','','D01',1,'RP391474-Amnd-1','','26502','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','od ovality 40 microns','These were from old rework parts, which was tried to rework but out of that 1 part was found too much ovality','Rework parts will be taken that time only and it will be kept for long time\r\n\r\nRecent batches ovality of the parts has not been found and the process is stabilized.','Rework parts will be taken that time only and it will be kept for long time\r\n\r\nRecent batches ovality of the parts has not been found and the process is stabilized.','Next batches found okay','','2015-02-11','Ravi(M)','Ravi(M)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','09','no','Misc','Ravi(M)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8201,'18-119B','Magellan Aerospace Bournemouth','HOUSING OUT B DRG 3','200068','D275 40011 200','','D01',1,'RP391474-Amnd-1','','26503','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','od ovality','These were from old rework parts, which was tried to rework but out of that 1 part was found too\r\nmuch ovality','Rework parts will be taken that time only and it will be kept for long time Recent batches\r\novality of the parts has not been found and the process is stabilized.','Rework parts will be taken that time only and it will be kept for long time Recent batches\r\novality of the parts has not been found and the process is stabilized.','Next batches found okay','','2015-02-11','Ravi(M)','Ravi(M)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','09','no','Misc','Ravi(M)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8202,'18-119B','Magellan Aerospace Bournemouth','HOUSING OUT B DRG 3','S71278','D275 40011 200','','D01',2,'RP391474-Amnd-1','','26505','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','od ovality','These were from old rework parts, which was tried to rework but out of that 1 part was found too\r\nmuch ovality','Rework parts will be taken that time only and it will be kept for long time Recent batches\r\novality of the parts has not been found and the process is stabilized.','Rework parts will be taken that time only and it will be kept for long time Recent batches\r\novality of the parts has not been found and the process is stabilized.','Next batches found okay','','2015-02-11','Ravi(M)','Ravi(M)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','09','no','Misc','Ravi(M)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8203,'18-119B','Magellan Aerospace Bournemouth','HOUSING OUT B DRG 3','B2483A','D275 40011 200','','D01',2,'RP391474-Amnd-1','','26510','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','od ovality','These were from old rework parts, which was tried to rework but out of that 1 part was found too\r\nmuch ovality','Rework parts will be taken that time only and it will be kept for long time Recent batches\r\novality of the parts has not been found and the process is stabilized.','Rework parts will be taken that time only and it will be kept for long time Recent batches\r\novality of the parts has not been found and the process is stabilized.','Next batches found okay','','2015-02-11','Ravi(M)','Ravi(M)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','09','no','Misc','Ravi(M)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8204,'18-119B','Magellan Aerospace Bournemouth','HOUSING OUT B DRG 3','219385','D275 40011 200','','D01',1,'RP391474-Amnd-1','','26509','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','od ovality','These were from old rework parts, which was tried to rework but out of that 1 part was found too\r\nmuch ovality','Rework parts will be taken that time only and it will be kept for long time Recent batches\r\novality of the parts has not been found and the process is stabilized.','Rework parts will be taken that time only and it will be kept for long time Recent batches\r\novality of the parts has not been found and the process is stabilized.','Next batches found okay','','2015-02-11','Ravi(M)','Ravi(M)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','09','no','Misc','Ravi(M)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8205,'18-211B','Magellan Aerospace(Chalfont) Limited','PLUNGER','456336','D321 40205 200','','H01, ECN NR29998ST1JB80',1,'P/068955_Amendment-3','','32953','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','85 mm deep bore measured approximately 47mm','While machining drill got broken both operators and inspectors missed to notice it','An 83.15 Plug gauge has been introduced to check the drill depth and 100% inspection will be carried out for upcoming parts','An 83.15 Plug gauge has been introduced to check the drill depth and 100% inspection will be carried out for upcoming parts','Next parts found okay','C29684','2015-02-11','Avinash(R.J.)','Muniyappa(N)','CAR S-000360','2014-06-13','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','CUST END','no','Misc','Muniyappa(N)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8206,'18A-306','Magellan Aerospace(Chalfont) Limited','HINGE O.W.P.ASSY MID.','','D572 59245  001','','B, ECN NG29999ST2TY72',1,'P/068961','','A02648','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Bush with internal diameter 11.1125/+11.1379 at zine E2 on the drawing measuring oversize','It was found in the assembly cell, the semi finished part and finished parts were kept close to each other, either operator or inspector have misplaced the parts','Separated and identified racks/trays for keeping the parts in assembly\r\nInspection method changed to air gauge to minimize the the man hour','Separated and identified racks/trays for keeping the parts in assembly\r\nInspection method changed to air gauge to minimize the the man hour','Next parts found okay','C27449','2015-02-11','Avinash(R.J.)','Muniyappa(N)','CAR S-000334','2014-02-11','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Assembly','','CUST END','no','Misc','Muniyappa(N)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8207,'18-376B','Magellan Aerospace Bournemouth','GAMMA FITTINGS ','M590350 97022','NSA840020-150','','L',31,'RP401478_Amend No.-1','','40878','','0000-00-00',NULL,'yes','yes','yes','','','','','','no','K dimension undersize by -0.025mm.','While running the emag machine, setting will came in the mazak-3 machine so that time inform to the mazak-5 machine operator for loading the part to emag machine that operator 2 times loading the parts for all the 15 pallets but not checking the parts. that time this problem will occured and rejected the all 31 parts.     ','After findout this problem check the all parts and seperate the rejected parts and cleaning the jaws and skin cut given to the jaws and change the insert and 0.3 plus taken to the wear offset and run the part and check the part and required currection given in wear offset and run the part then check the part and found ok. ','Warning given to the operator and check the all parts hundred percent in all stages ','CAPA found okay','','2015-02-12','Sandhesh D(S)','        Sathish G','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8208,'30-012A','Gardner Aerospace-Derby Limited','SPAR FWD - RH','2013801','L575 51827 201','ABM3-1029 T7651','A00, ECN:PG60049U01LC52',1,'LPR0000645','','40204','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Raw material cross cutting ','While cutting the material as per layout, due to Machine blade was slack & wobbling due to bearing\r\nbroken cross cutting the material.\r\n\r\n','Cutting process stopped and machine manufacturer was visited and verified the machine and informed\r\nto change the bearing & temporarily serviced.\r\n','Complete machine servicing are planned & contract given to machine manufacturer and hence forth regular machine maintenance will be planning\r\nand maintained.\r\n','Cutting machine maintenance done. Next parts found okay ','','2015-02-12','Sunil Kumar(K.R.)','Devaraja (M S)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','01','no','Misc','Narayanappa(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8209,'40-003','Universal Engineering Limited','JOINT PLATE ','434933','D574 50016 202','','D,  ECN NG23774ST2KE84',1,'320402 - S2','','40552','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Clamping Hole not opened, due to this operation-02 not completed.','This deviation done in first batch of production.After completion of FAI this was machined.The deviation as follows, \r\nClamping hole depth not controlled in program and operator not checked the through hole in part after completion of operation-01.','After checking the first off part, operator analyzed the problem and informed to supervisor regarding the deviation and after discussing with CAD/CAM, hole depth in program changed with new revision.','This program was proved and saved in CAD/CAM folder.\r\nComplete batch production runned and process was proved.','Under Review','','2015-02-12','Rangaswamy()','Rangaswamy()','','0000-00-00','op;03 pending because clamping hole not opened.','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','','01','yes','Misc','Rangaswamy()','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8210,'18-153B','Magellan Aerospace Wrexham','BRACKET','425411','F579 52514 200 48',' ABM3 1029','A',1,'RP127045','','39750','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Hole pitch undersize.','Due to final operation completed in conventional machine.When extra material removing time part butting not properly .So base to hole center distance minus side, part was rejected.   ','Next batch production running time first all part roughing operation completed after run the finishing operation.\r\nInstructed to conventional machine operator part butting properly and every part before given cut check the butting area and clamping tightness.\r\n ','Instructed to conventional machine operator part butting properly and every part before given cut check the butting area and clamping tightness.','Next batches found satisfactory.','','2015-02-12','Anjinamurthy(H)','Anjinamurthy(H)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','Misc','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8211,'28-044','Magellan Aerospace New York  Inc.','LINK ASSEMBLY UPPER UPLOC','A13434 ( WO No.-1432','161A6122-6','','PL_Rev-A, PSDL-Rev-N/C',2,'128961-3170','','41091','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dig mark on profile.','While doing operation 05, Operator wrong value moved in Y-Axis.(Instead of 35mm he moves 33mm). Due to this manual error Y reference shifted and dig mark observed on outer profile.\r\nBoth the parts was rejected and operator finding this deviation after roughing operation completes.','After checking the deviation, operator analyzed and checked the Offset and found error.He informed to supervisor regarding the deviation in parts.\r\nSupervisor checked the offset and found deviation and he changed the offset and continued production after once cross checking the parameters.','This error is due to operator. Process was proved and there is no problem with the process.\r\nTraining conducted to operator for Process pertaining to operation-05 and methods of cross checking the offset. \r\nInformed to supervisor to monitor the operators and train then regularly in front of machines to avoid manual errors.','CAPA found okay','','2015-02-12','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','05','no','Misc','Krishna(Chowdary.G.P.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8212,'18-001A','Magellan Aerospace Wrexham','BRACKET SUPPORT-LH','0778801','D361 50110 200','ABM3 1029 T7651','A',1,'RP125887','','40687','','0000-00-00',NULL,'','','yes','','','','','','','Hole deburr running time part dig mark observed.\r\n\r\n','Due to part clamping not properly.','Inform to operator when load the part check in location pin length.\r\nRemove the old location pin and replace the new location.\r\nInform to operator before run the programs check the  location pin and clamps \r\n\r\n','Inform to operator when load the part check in location pin length.\r\nRemove the old location pin and replace the new location.\r\nInform to operator before run the programs check the  location pin and clamps\r\n\r\n','CAPA found okay. Next parts found okay.','','2015-02-12','Lohith(K)','        Theerthappa K.N.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8213,'42-002','RAFAEL','PSA BASE','K10596','BA1E2001B','','38-576104_Rev-E, TILDOCS#172373_Rev-13, RE_804-1-5_Rev-11, 111.21_Rev-6, 23.36.59_Rev-F, ECN 57176 2014/08 /25; ECN 58483  2014/07/29',1,'347592024','','39951','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Tread mill tool running time part dig mark .','First pass went properly, while next pass thread mill went outside the required area.','Next part has not been machined under identification why that problem occurred even though its a proved program. Planning to prepare a new fixture and also informed CAD department regarding this problem occurred','Next part has not been machined under identification why that problem occurred even though its a proved program. Planning to prepare a new fixture and also informed CAD department regarding this problem occurred','Next batch found satisfactory.','','2015-02-12','Krishna(Chowdary.G.P.)','Lohith(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','0','00','no','Misc','Sudhagar(V)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8214,'28-044','Magellan Aerospace New York  Inc.','LINK ASSEMBLY UPPER UPLOC','A13434 ( WO No.-1432','161A6122-6','','PL_Rev-A, PSDL-Rev-N/C',3,'128961-3170','','39478','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','1no Material deviation outer profile not cleared.\r\n\r\n2nos tool dig on the outer profile.','Part were not clamped  properly due to machine pressure part was lifted.','Torque wrench will be procured to clamp the parts.','Torque wrench will be procured to clamp the parts.','After procuring torque wrench NC will be closed','','2015-02-15','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','00','no','Misc','Lohith(K)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8215,'18-110A','Magellan Aerospace Bournemouth','FORK END INTERMEDIATE','238302','D575 40494 202','S80 FHT','J',1,'RP400840','','41036','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Diameter 14.28 bore measures diameter 20.28 mm.','18-110A part have 02nos. bores with same diameter 14.28mm. \r\nThis machining is done with Circular interpolation by CRC program.\r\nTwo bores CRC values entered with 2 D-values in machine wear.\r\nWhile doing first off part, Operator D1 entered, but D2 not entered in machine wear. Due to this error program running with Zero CRC value. This manual error causes hole diameter 20.28mm in one bore.','Training given to operator to check the CRC values in machine control panel.\r\nTraining done on read the messages in program.\r\nTraining given to operator to write and check the D-values in machine reference book.\r\n','1.Informed to supervisor to monitor the above CA for 10 days and check the effectiveness.\r\n2.After 10 days of monitoring operator not done any manual mistakes and also he verify the CA points while doing part setting.\r\n\r\n','CAPA found satisfactory.Next parts found okay','','2015-02-16','Anjinamurthy(H)','        Manohara M','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8216,'18-226B','Magellan Aerospace Bournemouth','BRKT - NUT RETAINER','R3304','F572 53828 200','','A',1,'RP400846','','37693','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Slot width ovear size. 1mm. (Trail part)','Trail part','Trail part','Trail part','Trail part','','2015-02-17','Rakeshbabu(V)','Rakeshbabu(V)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','07','no','Misc','Anjinamurthy(H)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8217,'35-282','Saab AB','GUIDE HARNESS LWR','432903A','423Z1982-1','','---',1,'1600097231','','41032','','0000-00-00',NULL,'','','yes','','','','','','','Dig Mark observed on part.','While doing first batch production,Step observed on wall and program changed to avoid step.\r\nWhile doing new program in CAD, wrong program name entered(Dia 12FL entered instead of Dia 10FL). \r\nProgram was generated for Dia 10FL but program runnned with Dia 12FL.\r\nSupervisor also not checked the program name with program generated.','Dig mark observed and checked the deviation in program and Immediately new program generated in CAD and program proved in machine for next part.','Program Name with tool diameter will validate by CAD and Post possessor edited to give Optional stop option in program to check the tool diameter by supervisors.\r\nFor all the FAI or new programs to be checked by CAD engineers and Concern supervisors. \r\n','CAPA found okay','','2015-02-17','Ramesh(Poojary)','        Gajendra Singh C.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8218,'35-280','Saab AB','SUPPORT','744294A0','423Z1203-2-02','','---',1,'PA 1510 NEW PARTS-2','','41014','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','** Dia4.83 hole top chamfer is over size, measured out of tolerance.**','operator select wrong flute length tool & load. required flute length 27mm but load 23mm flute length. shank dia 6mm, so part top 6 shank dig.','Change another drill continue the  production. instruct operator tool selection before check flute length.','Detected tools for this CRN. ','CAPA found okay.Next parts found okay','','2015-02-17','Rangaswamy()','Rangaswamy()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','Misc','Manjunath(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8219,'18-278A','Magellan Aerospace(Chalfont) Limited','DOOR OUTER TYPE 25R','1867803','L572 53720 200','ABS5032A055','C00',1,'P/074116','','40771','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','operation:03 is pending, due to part bend after 01 operation. ','Route cause for all the AXIS PANELS is due to part thickness is less and parts will bend or twist after operation-01 is completes.\r\nThis we observed and checked all the parts while parts manufacturing.If parts bend is more, the parts thickness will vary and possible of rejection.','CA is carried at the moment that, Operation-03 is carried with extra clamping.\r\nComplete full prof process is not proved.','Planned to change the process to avoid more bend. and also part thickness will come consistent in new process.\r\n\r\nNew process fixture is manufactured for 18-277. Process to be proved.\r\n','For unfortunate reasons this NC being closed by after proving the process, NC will be validated','','2015-02-17','Girish(Prasad P)','Girish(Prasad P)','','0000-00-00','op:03 pending, due to after 01 operation part bend.','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Manufacture Only','','01','yes','Misc','Girish(Prasad P)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8220,'35-276','Saab AB','BRACKET INTERMED','581305','423Z1123-3-02','','--A',1,'1600097231','','40529','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Tool dig mark on rib...','Operator tool length holding problem,required length 80mm but holding length 70mm so tool holder dig in part top face.  ','check the  total hight, then holding 80mm tool then runned.','Next batch add tool length in process sheet & insert message & M0 in program inside.','After process sheet corrected NC will be closed until unless NC will not be closed (Raghuveer V G)','','2015-02-18','Rangaswamy()','Rangaswamy()','','0000-00-00','* Tool dig mark on rib...','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Girish(Prasad P)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8221,'35-277','Saab AB','BRACKET INTERMED','432903A','423Z1123-4-02','','---',2,'PA 1510 NEW PARTS-2','','40533','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Thickness 5.08mm Dimension measures 0.1 plus side.\r\n','While running first production batch after FAI approval,Set of proved program transferred to machine and operator not runned the wall finish program while doing a first off part.\r\nAfter checking First off part noticed thickness measures out of tolerance.','After checking First off part operator and supervisor analyzed the problem.\r\nChecked the Proved program folder as per MPS datasheet.and also cross checked the all the programs with CAD file in CAD/CAM.\r\nNext part produced and checked the dimensions as per MPS and all dimensions are found as per process.','Training conducted to operators to check the MPS date sheet properly and run all the programs while doing firstoff.\r\nSupervisors will check the list of programs for the first batch production to standardized the programs.','CAPA found okay (Under Rework)','','2015-02-18','Rangaswamy()','Rangaswamy()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','','FI','yes','Misc','Manjunath(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8222,'35-276','Saab AB','BRACKET INTERMED','581305','423Z1123-3-02','','--A',2,'1600097231','','40529','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Thickness measures 0.3mm more than the requirement.\r\n\r\n','While running first production batch after FAI approval,Set of proved program transferred to machine and operator not runned the wall finish program while doing a first off part.\r\nAfter checking First off part noticed thickness measures out of tolerance.\r\n','After checking First off part operator and supervisor analyzed the problem.\r\nChecked the Proved program folder as per MPS datasheet.and also cross checked the all the programs with CAD file in CAD/CAM.\r\nNext part produced and checked the dimensions as per MPS and all dimensions are found as per process.\r\n','Training conducted to operators to check the MPS date sheet properly and run all the programs while doing firstoff.\r\nSupervisors will check the list of programs for the first batch production to standardized the programs.\r\n','Under Review','','2015-02-18','Rangaswamy()','Rangaswamy()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','','DN','yes','Misc','Manjunath(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8223,'18-120C','Magellan Aerospace Bournemouth','HOUSING OUT B D BRG 3','CB872484','D275 56121 200','','E01,  ECN NG27011ST1KA83',1,'RP400843','','40766','','0000-00-00',NULL,'yes','yes','yes','','','','','','','2nd set up  problem so thickness (+)Side running time part rotating O D under size.','In 2nd set up thickness is maintained 0.1mm plus side.in finishing operation more stock measure part will rotate.when part rotated OD will undersize.','For next part check the thickness and any deviation came that will be adjusted in work offset and run the part.','For next part check the thickness and any deviation came that will be adjusted in work offset and run the part.instructed to operators to check the dimension of 2nd set up before loading the part.','CAPA found satisfactory, Next parts found okay','','2015-02-19','Dinakar(K)','        Manjunatha N','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8224,'18-098B','Magellan Aerospace Bournemouth','VALVE- SEAT','64442/01/00','D282 50060 204','','D',1,'RP400844','','38919','','0000-00-00',NULL,'yes','no','no','no','no','yes','no','yes','no','Flatness .01mm measures .083mm','Under review','Under review','Under review','Under review','','2015-02-19','Avinash(R.J.)','Nandishkumar(D.K.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','16592','POST DN','no','Misc','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8225,'18-188A','Magellan Aerospace Bournemouth','BUSH','H6928','L575 50397 200','B23','B00',10,'RP400846','','41277','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Drwing calls ruling dimension 101.6 but physically measured dia 103.30 so RM is quarantene.','','','','RM clarified through mail on 23-02-2015.','','2015-02-19','Nagaraja (G)','Sunil Kumar(K.R.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','Manufacture Only','0','01','no','Misc','Muniyappa(N)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8226,'18-188A','Magellan Aerospace Bournemouth','BUSH','H6928','L575 50397 200','B23','B00',15,'RP400846','','41288','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Drwing calls ruling dimension 101.6 but physically measured dia 103.30 so RM is quarantene.','','','','RM clarified through mail on 23-02-2015.','','2015-02-19','Nagaraja (G)','Sunil Kumar(K.R.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','Manufacture Only','0','01','no','Misc','Muniyappa(N)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8227,'18-188A','Magellan Aerospace Bournemouth','BUSH','H6928','L575 50397 200','B23','B00',10,'RP400846','','41289','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Drwing calls ruling dimension 101.6 but physically measured dia 103.30 so RM is quarantene.','','','','RM clarified through mail on 23-02-2015.','','2015-02-19','Nagaraja (G)','Sunil Kumar(K.R.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','Manufacture Only','0','01','no','Misc','Muniyappa(N)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8228,'35-300','Saab AB','BRACKET, INTERMEDIATE FRA','430772A','423Z1125-5-02','','---',1,'1600099840','','41397','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dig mark observed on wall.','Due to running time dia 12 flat end mill tool broken .\r\nSo part wall thickness 1MM minus  side measured . This problem created from program wrong direction. \r\n\r\n','Immediately stop the machine and inform to CAD/CAM department. CAD/CAM department change outer roughing program and add the new tool after continue the production.   ','Immediately change the program direction from CAD/CAM department. After balance Work Order qty 200 nos completed, all part found  ok. ','Next parts found okay','','2015-02-19','Anjinamurthy(H)','Anjinamurthy(H)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Anjinamurthy(H)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8229,'35-270','Saab AB','STOP INSERT','G20098K08','424Z6413-1','','--A',1,'1600097231','','40352','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','*Tool dig mark on part.','Due to part running time tool was broken so dig mark observed on the face.\r\n','Replace the new tool and continue the production.\r\nInstructed to operator every tool running time before check and after run the program.','Replace the new tool and continue the production.\r\nInstructed to operator every tool running time before check and after run the program.','Next parts found okay','','2015-02-19','Rangaswamy()','Rangaswamy()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','Misc','Manjunath(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8230,'28-005','Magellan Aerospace New York  Inc.','SHOULDER BOLT','G13088','162A3109-1','15-5PH Steel bar per','A',1,'120162_R0_C1','','38519','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','O.D undersize by(-)0.007mm.','OD roughing tool 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. finishing tool get the more stock.','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 and every 15 to 20 nos change the finished insert tip and run the part so this problem again not repeated.','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 and every 15 to 20 ns chnge the  finished insert tip and run the part so this problem again not repeated.  \r\n','CAPA found okay next parts found okay','','2015-02-20','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','FI','no','Misc','Sudhagar(V)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8231,'18-227B','Magellan Aerospace Bournemouth','CLAMP STRIP BTM','421007','L572 51299 200','ABM3 1029','A00',1,'RP401009','','39309','','0000-00-00',NULL,'yes','yes','yes','','','','','','','t-slit cutter crc pogaram running time thickness .1 - side ','','','','Parts Accepted.','','2015-02-20','Anjinamurthy(H)','        S. Shiva Kumar','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8232,'35-077','Saab AB','BUSH','1112509740','D575 40147 200','DTD-197','B ECN NG29999ST2TT59',63,'PA 1217-Bushes (A320','','39420','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Bore measures over size 10 to 20 micron.','Due to wear out of insert bore over size. \r\n.','Instructed to operator for checking insert wear our regularly and changing insert as mentioned in board.','All the machines tool life board was placed and instructed to operator for follow the same instruction.','Monitoring of CAPA should be done','','2015-02-20','Avinash(R.J.)','Manjunath(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','15914','post Dn','no','Misc','Manjunath(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8233,'18-318A','Magellan Aerospace Bournemouth','HALF CLAMP','8031','D574 50551 200','DTD 5014','B01',1,'RP400946_Amnd_No.1','','40058','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Corrosion pits and dent observed.','Due to rubbing of tool or material behavior Corrosion Pits  has been observed  in Treatment house\r\n','Apply PX-24 after machining, and polishing and rubbing of tool should be avoided\r\n','Apply of PX-24 is mandatory before sending the parts to treatment house.\r\n','Next parts found okay.','','2015-02-21','Avinash(R.J.)','Nandishkumar(D.K.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','16528','POST DN','no','Misc','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8234,'18-093A','Magellan Aerospace Bournemouth','PRESSURE RING','62588 / 01','D301 50085 202','L164 T4','A',5,'RP400844','','41043','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Corrosion pits observed on 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','','2015-02-21','Avinash(R.J.)','Nandishkumar(D.K.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','16590','POST DN','no','Misc','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8235,'18-098B','Magellan Aerospace Bournemouth','VALVE- SEAT','64442/01/00','D282 50060 204','','D',1,'RP400844','','41246','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Part wrong loading new operator (NANDEESHA M J) ','While 05 operation running time new operator part was wrong loading.','Before starting to the next part again training given to the operator and explained the process by supervisor.\r\nInstructed the new operator every part loading time inform to senior operator check and after run the programs.\r\nInstructed to senior operator part finishing time new operator loading every part check in all dimension.    ','Instructed the new operator every part loading time inform to senior operator check and after run the programs.\r\nInstructed to senior operator part finishing time new operator loading every part check in all dimension.\r\nFor upcoming batches before starting to the machining explaining the process for concerned operators\r\nby supervisor.  ','CAPA found okay. Next parts found okay','','2015-02-21','Lohith(K)','        Lohith K','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8236,'18-119B','Magellan Aerospace Bournemouth','HOUSING OUT B DRG 3','A0815N','D275 40011 200','','D01',1,'RP400842','','40966','','0000-00-00',NULL,'yes','yes','yes','','','','','','','running time part rotate od ovality.','od roughing running time part rotated because of 0.005mm more stock in face when the part rotated in the fixture it will slightly shifted and when finishing tool running ovality will occured because part slightly shifted during roughing.','check the thickness of all the parts and seperated the parts like 5.0,5.05,5.1 etc when 5mm thickness parts are running we dont take plus in wear  offset and 5.05 parts are running time 0.05 + taken in work offset and 5.1mm parts running time taken +0.1mm in work offset and run the production.','instruction  given to operator to check the thickness of every parts before loading in finishing operation for avoiding the ovality.','CAPA found okay, next parts/batches found okay','','2015-02-21','Dinakar(K)','        Manjunatha N','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8237,'35-185','Saab AB','CED_LATCH_SERRAT_ED_PLATE','581787A9','425Z0610-17','','---',6,'April 2014','','41131','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','* Serration depth crossed to out of tolerance, minus side by -0.03mm ','This deviation found in this batch only.Overall serration depth except at four corners is ok. Only at 04 corners deviation observed.\r\nWe are unable to find the route cause at the moment.\r\nWe will check the process in next batch and same will fix in next batch production. ','Informed to operators, Supervisors and CAD engineer to check the possibility of deviation and if finds any problem with process,Tool path etc.\r\nSame will fix in next batch production.  ','Informed to operators, Supervisors and CAD engineer to check the possibility of deviation and if finds any problem with process,Tool path etc.\r\nSame will fix in next batch production.  ','Next batch to be monitored','','2015-02-21','Rangaswamy()','Shivashankar H.G.,Mahesh N,Karthineyan V.S.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','','FI','yes','HMC 440','Manjunath(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8238,'35-185','Saab AB','CED_LATCH_SERRAT_ED_PLATE','581148A4','425Z0610-17','','---',3,'April 2014','','41133','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','* Serration depth crossed to out of tolerance, minus side by (-0.03mm)','This deviation found in this batch only.Overall serration depth except at four corners is ok. Only\r\nat 04 corners deviation observed. We are unable to find the route cause at the moment. We will\r\ncheck the process in next batch and same will fix in next batch production. \r\n','Informed to operators, Supervisors and CAD engineer to check the possibility of deviation and if\r\nfinds any problem with process,Tool path etc. Same will fix in next batch production. \r\n','Informed to operators, Supervisors and CAD engineer to check the possibility of deviation and if\r\nfinds any problem with process,Tool path etc. Same will fix in next batch production. \r\n','under review','','2015-02-21','Rangaswamy()','Umesh B,Shivashankar H.G.,Mahesh N,Karthineyan V.S.,Gurukiran S M,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','','FI','yes','HMC 440','Rangaswamy()','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8239,'18-359A','Magellan Aerospace Bournemouth','FITTING HNG POINT SP 2 OB','547010','L575 52439 201','','A00',1,'RP400948_Amnd-01','','40757','','0000-00-00',NULL,'yes','no','no','no','yes','yes','no','no','no','Part bore out-of tolerance. (10 to 15 mic).','While part running time bore chartering so bore over size .Due to process problem.','Immediately stop the boring operation and Inform to operator when change the process after continue the production.','Next batch production running time new fixture and added one more extra operation. Inform to operator when boring operation running time inform the concern the supervisor and load the new fixture.','If the process to changed means Rev should change until then NC will not be closed (Raghuveer V G)','','2015-02-22','Girish(Prasad P)','Rangaswamy ,Basavaraja S. Jr.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','0','FI','no','MakinoF5-4','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8240,'35-192','Saab AB','SUPPORT-FTG','428527C','423Z1202-14','','---',2,'PA-1300 2014','','40539','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','*Rib thickness 8.9mm measures 8.55mm for 01 part and dig mark observed on part in 01 part.','* This error is due to RM size deviation in width.RM size is measures only 0.2mm plus side,\r\nDue to clamping and butting errors this will affect the wall thickness of the final part.\r\nThis errors find out in this batch only and after finding the deviation, care taken and continued production.\r\nAll the RM in this batch are checked and found 0.2 to 0.35mm plus side.\r\n ','* This errors is due RM cutting while sizing the parts in 35-193.\r\nThe run out of the cutter should check and care to be taken of butting the RM and tool parameters.\r\nThis action will create 0.5 stock on wall and can produce the parts without deviation.\r\nWith 0.5mm stock 35-191 and 35-192 parts will manufacture with out any deviation.\r\n ','The run out of the cutter should check and care to be taken of butting the RM and tool parameters while RM cutting in 35-193.\r\nThis action will create 0.5 stock on wall and can produce the parts without deviation.\r\nWith 0.5mm stock 35-191 and 35-192 parts will manufacture with out any deviation.','CAPA found satisfactory','','2015-02-23','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','05','no','Misc','Krishna(Chowdary.G.P.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8241,'35-192','Saab AB','SUPPORT-FTG','428527C','423Z1202-14','','---',1,'PA-1300 2014','','40539','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','* Dia 19.05/19.067 bore measures 0.010mm bore over size.','* Production run 10nos, 11th part bore over size so Reset the bore run tool and next part fond ok.','* The bore finish program run in END MILL tool in next beach run in reamer.  ','* Next beach dedicate to reamer. ','After procuring Reamer NC will be closed','','2015-02-23','Girish(Prasad P)','Girish(Prasad P)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','07','no','Misc','Krishna(Chowdary.G.P.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8242,'35-192','Saab AB','SUPPORT-FTG','428527C','423Z1202-14','','---',1,'PA-1300 2014','','40540','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Thickness 8.90 measures 8.55mm','* This error is due to RM size deviation in width.RM size is measures only 0.2mm plus side,\r\nDue to clamping and butting errors this will affect the wall thickness of the final part.\r\nThis errors find out in this batch only and after finding the deviation, care taken and continued production.\r\nAll the RM in this batch are checked and found 0.2 to 0.35mm plus side.\r\n','The run out of the cutter should check and care to be taken of butting the RM and tool parameters.\r\nThis action will create 0.5 stock on wall and can produce the parts without deviation.\r\nWith 0.5mm stock 35-191 and 35-192 parts will manufacture with out any deviation.\r\n','The run out of the cutter should check and care to be taken of butting the RM and tool parameters while RM cutting in 35-193.\r\nThis action will create 0.5 stock on wall and can produce the parts without deviation.\r\nWith 0.5mm stock 35-191 and 35-192 parts will manufacture with out any deviation.\r\n','CAPA found okay','','2015-02-23','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','05','no','Misc','Krishna(Chowdary.G.P.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8243,'35-191','Saab AB','SUPPORT-FTG','581308','423Z1202-13','','---',1,'PA-1300 2014','','40538','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','* Bore pitch 1 mm out of tolerance, required 18.88+/-0.05 and measured 19.90/19.92.','* Due to wrong Work offset,hole pitch measures out of tolerance. operator \"Y\" offset taken in 3d surface.','* correct offset taken in next part and cross checked all offset and run, part found ok.','* In future XOY0 hole done in fixture, cross check X0 Y0 hole and run the parts. ','CAPA found okay.Next parts found okay','','2015-02-23','Girish(Prasad P)','Girish(Prasad P)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','07','no','Misc','Krishna(Chowdary.G.P.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8244,'18-210B','Magellan Aerospace(Chalfont) Limited','BODY','5757','D321 40204 204','','D, ECN NR29999ST1KM15, NR29999ST2KF65, WQN DFB09775',1,'P/074113','','40511','','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','','2015-02-23','Avinash(R.J.)','Nandishkumar(D.K.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','16564','POST DN','yes','Misc','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8245,'18-215C','Magellan Aerospace(Chalfont) Limited','ROD END ASSMY - MALE ','231418','D321 53012 200','','F01, ECN NR29998ST1KH40',1,'P/074113','','41284','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Thread nogo answered.','','','','Parts accepted.','','2015-02-23','Narasimhamurthy(K.G.)','Seetharamu(D)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','Manufacture Only','','07','no','Misc','Ravi(M)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8246,'18-210B','Magellan Aerospace(Chalfont) Limited','BODY','5757','D321 40204 204','','D, ECN NR29999ST1KM15, NR29999ST2KF65, WQN DFB09775',1,'P/074113','','40512','','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','','2015-02-23','Avinash(R.J.)','Nandishkumar(D.K.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','16565','POST DN','yes','Misc','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8247,'35-082','Saab AB','HOUSING-SIDE ROLLER','425389','F579 53065 202','ABM3-1029 T7651','B, PG52307ST4KA80',15,'PA 1226-Roller Housi','','38834','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1)Corrosion observed in faces (10 Nos).\r\n\r\n2)Deep lines observed in holes (5).\r\n','Due to rubbing of tool or material behavior Corrosion Pits  has been observed  in Treatment house\r\n','Apply PX-24 after machining, and polishing and rubbing of tool should be avoided\r\n','Apply of PX-24 is mandatory before sending the parts to treatment house.\r\n','Next parts and batches found okay\r\n','','2015-02-24','Avinash(R.J.)','Manjunath(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','15929','Post DN','yes','Misc','Manjunath(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8248,'35-229A','Saab AB','HINGE BRACKET 3','7599601','D576 50006 204','','D00',1,'1600093863 Rev-2','','38671','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Corrosion observed on the 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','','2015-02-24','Avinash(R.J.)','Manjunath(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','15774','Post Dn','yes','Misc','Manjunath(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8249,'35-040','Saab AB','7605129-200','2016701','L574 55129 200','ABM3 1029','A00',2,'April 2015 A380','','41345','','0000-00-00',NULL,'','','yes','','','','','','no','hole mill tool problem','This error is due to wrong tool identification on tool.( Engraved dia 5.7 Hole mill for dia 6.35 Hole mill).Operator checked the engraving and load the tool to machine and start production.\r\nAfter finding deviation, he informed to supervisor regarding the error.\r\n\r\n','xxxxx','informed to tool grip supervisor to check the tool diameter once receiving from supplier. Log book kept for incoming inspection of tools to monitor the errors. ','xxxx','','2015-02-24','','        Rangaswamy ','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8250,'18-188A','Magellan Aerospace Bournemouth','BUSH','H6928','L575 50397 200','B23','B00',1,'RP400846','','41288','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','ID bore 36.750mm/36.775mm measured 36.780mm  \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. ','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','CA/PA found satisfactory.','','2015-02-24','Narasimhamurthy(K.G.)','Ashith(B)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','03','no','Misc','Narasimhamurthy(K.G.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8251,'35-245','Saab AB','WASHER SMALL','G19730K05','423Z1457-1','','--C',1,'1600097231','','40155','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','* Part thickness crossed out of tolerance (-0.04/-0.05) in part edge and part is taper.','Due to part clamping not properly so part running time part edge thickness undersize. ','Instructed to operator every  part loading time check the part butting area.\r\nBefore run the finishing program part remove and re tight in every time.\r\n  ','In program given M00 and Message. \r\nAfter loading the part into the VICE,it will be checked for air gaps between the part and the vice using the feeler gauge and then start the machining.','CAPA found okay.Next parts found okay','','2015-02-24','Lohith(K)','Theerthappa K.N.,Shivaraj K S,Nataraja C V,Manjunath  M,Hari Prasad,,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','HAASVF2SS','Manjunath(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8252,'35-275','Saab AB','PIN','G21290K02','426Z3601-1','','--A',1,'PA 1510 NEW PARTS-2','','39592','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Total length measures undersize.','The Following route cause analyzed for the parts rejected, Jaws Boring is not good,part not butted properiy to the  jaws because of small chips are in Part butting faces.Roughing and Finishing inserts wear out.  \r\n','Roughing stage clean the jaws with the help of air and\r\nbefore loading the part.after clamping check the every part\r\nit was butted in the jaws face properly.','Roughing stage clean the jaws with the help of air and\r\nbefore loading the part.after clamping check the every part it was butted in the jaws face properly.','CAPA found satisfactory','','2015-02-25','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','DN','no','Misc','Manjunath(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8253,'35-275','Saab AB','PIN','G21290K02','426Z3601-1','','--A',2,'PA 1510 NEW PARTS-2','','39592','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Centering Mark observed on part.\r\nAfter total length maintain 0.2mm centering mark on part. \r\n\r\n','While doing production batch, in operation-01(Facing and Centering), Part centering done at maximum side.\r\nOperator not observed visually for 02nos.   ','After checking visually operator crosschecked the work offset and corrected and continued production.','Part Centering will not check with instruments due to centering is for support for long length parts.\r\nInformed to all the operators to check the tool offset and observe the centering depth for first part.\r\nCare to be taken in further batches.','CAPA found okay.','','2015-02-25','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','DN','no','Misc','Manjunath(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8254,'35-191','Saab AB','SUPPORT-FTG','428527C','423Z1202-13','','---',1,'PA-1300 2014','','40537','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','*Wall thickness 0.1 to 0.2 - side.','*While running operation 02 dia 80 face mill cutter insert wear out and causes thickness -0.1 to -0.2mm plus side.','*After checking the part in stage, operator analyzed the problem and check the tool offset and found deviation due to insert wear out.\r\nInsert indexed and taken new offset and continued production.\r\nNext part found thickness as per drawing requirement.\r\n','* Informed to operators and supervisors to check the tool insert at regular intervals.\r\nMonitoring of insert life will avoid such problem in further batches.\r\nPart rework to be carried in separate setup.\r\n','CA/PA found satisfactory.','','2015-02-25','Rangaswamy()','Rangaswamy()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','07','no','Misc','Girish(Prasad P)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8255,'18-295A','Magellan Aerospace Bournemouth','BOLT','238302','D577 56145 200','S80','A',1,'RP400846','','40550','','0000-00-00',NULL,'','','yes','','','','','','',' program editing problem od (-)side','In mazak machine program is transfered using pendrive.program not came because pen drive problem that time program is edited manually that time one line missed.so part rejected.','Check the program and and edited the missed line correctly and run the part part found okay. ','To check the program when you are edited manually before run the part and new card reader is taken by supervisor then send a program.','CAPA found satisfactory, Next parts found okay','','2015-02-25','','        Nataraja C V','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8256,'35-157A','Saab AB','INTERCOSTAL_VENT','581304','423Z1172-3-01','','---',1,'PA-1300 2014','','39363','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dig mark on base.','Due to Wrong offset taken by operator while doing a first off part, this deviation coming.','Tool offset corrected and cross checked by supervisor and continued production after cross checking once again.\r\nNext part find base thickness as per drawing requirement.\r\nAfter first off proving Training conducted for operator in front of machine to take the offset and also cross checking methods.\r\n','Training conducted for operator in front of machine to take the offset and also cross checking methods.\r\nSupervisor will cross check once while doing first off for 3 times and keep monitoring on to avoid manual errors.','CAPA found okay next parts/batches found good.','','2015-02-26','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Krishna(Chowdary.G.P.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8257,'35-274','Saab AB','PIN','970533','426Z2601-1','','--A',5,'PA 1510 NEW PARTS-2','','39595','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','OD measures undersize.','After running the some parts insert will be wear out and taper occured in the parts and its one side outer diameter under sized so part will be rejected. ','Change the insert corner and 0.4 plus taken in the wear offset and run the part and adjust the taper in running part and 0.2 (minous) currection given in the wear offset and run the part and check the taper in the part then given the proper currection and run the part so part checked found ok then continue the production.  ','While running the production if any line marks or noise will observed that time check the insert corner and change the insert and after every 25 to 30ns once changing the insert corner and avoiding this type of rejections.','CAPA found okay.','','2015-02-26','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','DN','no','Misc','Manjunath(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8258,'35-274','Saab AB','PIN','970533','426Z2601-1','','--A',2,'PA 1510 NEW PARTS-2','','39595','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Center hole(Dial stock center point mark)observed on oppsite side. ','Part accepted ','Part accepted ','Part accepted ','Part accepted ','','2015-02-26','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','yes','With Treatment','','DN','no','Misc','Manjunath(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8259,'18-328A','Magellan Aerospace Wrexham','NUT ANCHOR ','95599A','D572 51346 200','','A',7,'RP127045','','39678','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','After anodizing thread damage observed.','Before sending the parts to Treatment house parts was checked 100% but after treatment thread found damaged','Informed to Treatment supplier to handle the parts carefully especially threads either by wrapping collars or some other methods and keep the parts separately without having metal to metal contact','Informed to Treatment supplier to handle the parts carefully especially threads either by wrapping collars or some other methods and keep the parts separately without having metal to metal contact','CAPA found okay','','2015-02-26','Avinash(R.J.)','Nandishkumar(D.K.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','16175','POST DN','no','Misc','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8260,'40-004','Universal Engineering Limited','JOINT PLATE ','0001801 2','D574 50016 203','','D, ECN NG23774ST2KE84',1,'320402 - S3','','41370','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Operator mistake so part dig mark in base.','Due to part all operation completed. Step observed in part radius. Operator reload the part put the external clamps and rerun the radius finishing programs. operator mistake this error happened.   ','Instructed to operator part all operation complete time check the straight dialing and put the external clamps after run the rework program.      ','Any part deviation observed time inform the concern supervisor.   ','CAPA found okay.Next parts found okay','','2015-02-26','Lohith(K)','Rakesh (KC)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Anjinamurthy(H)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8261,'18-092A','Magellan Aerospace Bournemouth','PRESSURE RING','62588 / 01','D301 50085 200','L164 T4','A',3,'RP400844','','40751','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Corrosion pits observed on part surface.','Due to rubbing of tool or material behavior Corrosion Pits  has been observed  in Treatment house\r\n','Apply PX-24 after machining, and polishing and rubbing of tool should be avoided\r\n','Apply of PX-24 is mandatory before sending the parts to treatment house.\r\n','Next parts and batches found okay\r\n','','2015-02-26','Avinash(R.J.)','Nandishkumar(D.K.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','16567','POST DN','no','Misc','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8262,'18-195A','Magellan Aerospace Wrexham','M/C Bracket','571009A0','D572 59093 200 01','ABM3 1029 T7651','A',1,'RP125889','','40122','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Machining damage on part surface.','Before sending the parts to Treatment house parts was checked 100%and found okay but after treatment parts found\r\ndamaged','Informed to Treatment supplier to handle the parts carefully  and keep the parts separately without having metal to metal contact','Informed to Treatment supplier to handle the parts carefully  and keep the parts separately without having metal to metal contact','CAPA found okay','','2015-02-26','Avinash(R.J.)','Nandishkumar(D.K.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','16598','POST DN','no','Misc','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8263,'18-415B','Magellan Aerospace Bournemouth','ACTUATOR HOUSING','95744A','D278 50163 201','','D',1,'RP401022_Amend No 1','','40970','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','In first setup groove width taper problem, 6mm thickness -0.1mm.','For first part taken x&z offset for grooving tool and in wear offset taken 0.5mm up in x and groove width is program control(after finishing that program check the groove width and is adjusted in wear offset and groove width is adjusted in program)after running the groove program checked the groove diameter thicknes and width groove dia ok and thickness is 0.1mm taper 5.9mmto 6.0mm so part reject.','For next part taper is adjusted and run the part.part is found okay.','Instructed to operator  to check the dimensions in the program  at setting time and before  running the part.','CAPA found satisfactory, Next batches found okay','','2015-02-26','Dinakar(K)','SHIVAKUMAR()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Dinakar(K)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8264,'35-281','Saab AB','GUIDE HARNESS UPR','755659A0','423Z1929-3','','---',1,'1600097231','','40819','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Tool dig mark on part.','Mis interpretation of CAD Model while doing FAI part.FAI part passed and then,\r\nStep observed on part due to negative profile not machined in part in first batch production.\r\nWhile doing rework for 04nos, 01not dig mark observed.','Part Machining done as per CAD model and program proved and saved.\r\npart CMM done and found all the dimensions as per drawing.','Model validation to be check and approve by CAD.Engineer to check the all part profile programs completed before FAI machining starts.','CAPA found satisfactory. Model validation should be done before doing FAI.','','2015-02-26','Girish(Prasad P)','Girish(Prasad P)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','Misc','Manjunath(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8265,'35-249','Saab AB','STANDOFF','G21025K06','423Z1916-3','','---',1,'PA 1510 NEW PARTS-1','','40159','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','OD ovality.','when we are running the first batch production time we butting the part in the fixture and lock the part in using nut and tigtening the part in clockwise direction for using nut and using MTJNL tool so locking nut was loosed and ovality occure in the running part and part will rejected','Next part load  in the fixture using lock nut and MTJNR tool was loading the machine and take re offset and running  part found ok .','for next every batch we are using MTJNR & SVJNR tool both  roughing and finishing and (using only MTJNR & SVJNR tool) this comment written in the program. ','CAPA found okay, next parts/batches found okay','','2015-02-26','Dinakar(K)','Shivanand(D.B.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','05','no','Misc','Dinakar(K)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8266,'18-277A','Magellan Aerospace(Chalfont) Limited','DOOR OUTER TYPE 27R','508103','L572 53719 200','ABS5032A055','D00',1,'P/074116','','38055','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Outer surface of panel is rippled towards outer edge measuring up to 0.17 mm deep from peak to trough. 1 off of 46 off batch\r\nCIM 38055 certificate C33779 affected. Fault found after treatments.','As these parts requires fitting work (Buffing), this buffing operation has been missed in this part and in Final Inspection also','Further batches will be inspected 100% visually, after ensuring fitting work, parts will be taken to Final Inspection.','Further batches will be inspected 100% visually, after ensuring fitting work, parts will be taken to Final Inspection.','CAPA found okay','C33779','2015-02-26','Muniyappa(N)','Nandishkumar(D.K.)','CAR S-000404','2015-02-26','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','0','CUST END','no','Misc','Muniyappa(N)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8267,'18-385A','Magellan Aerospace(Chalfont) Limited','NUT RING OUTER','242098','D575 40038 202','','A',1,'P/074123','','38415','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dia 1.30 drill bit cut.','While drilling operation running in fitting section dia 1.3 drill broken.\r\nThe drilling is done with an angle of 45 degrees. Due to coolant not flowing properly and might be chances of not clamping the part to jig','1)Drill bit grinding will be done and checked again and again.\r\n2)Proper flow of coolant is monitored regularly. \r\n3)Clamping will be ensured twice before drilling.','1)Drill bit grinding will be done and checked again and again.\r\n2)Proper flow of coolant is monitored regularly. \r\n3)Clamping will be ensured twice before drilling.','Repeated CAPA.','','2015-02-26','Nagaraju(T)','Nagaraju(T)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','12','no','Misc','Irappa(Badiger)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8268,'35-035','Saab AB','7600298-201','24541012','L574 50298 201','ABM3 1029','B00',6,'1600099837','','39990','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','yes','Incorrect marking location ','We have discussed with our and he was mis interpreted the drawing and most of the drawings calls for “Far side & Near side” \r\n\r\nBut in this case drawing not addressed the far OR near side that leads to him misinterpreted.\r\n','I assume that there are three ways to correct these parts and I would request you to prioritize the point-1.\r\n\r\n1)	If you agree I will release DR for these parts.\r\n\r\n2)	I would request you to part mark at SAAB on opposite side.\r\n\r\n3)	Please return these parts to CIM for remarking.\r\n','Please find the attached sheet that is part of existing process sheet that calls only part marking with reference to drawing.  \r\n\r\nSee attached new plan to implement and that will goes to part of process sheet that is better clarity for operator to carry out the part marking.\r\n\r\nI will attempt all A380 parts and I will make list which needs part marking instruction separately for both right hand and left hand.\r\n\r\nI will give you the other parts instruction shortly.\r\n','This batch reviewed and found correct and these parts were reworked at customer end','C35082','2015-02-26','Avinash(R.J.)','Manjunath(G)','Through mail','2015-02-26','NCR received through mail dated 26/02/2015','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','With Treatment','','CU','no','Misc','Avinash(R.J.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8269,'35-035','Saab AB','7600298-201','24541012','L574 50298 201','ABM3 1029','B00',6,'1600099837','','39990','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','yes','Incorrect marking location ','We have discussed with our and he was mis interpreted the drawing and most of the drawings calls for “Far side & Near side” \r\n\r\nBut in this case drawing not addressed the far OR near side that leads to him misinterpreted.\r\n','I assume that there are three ways to correct these parts and I would request you to prioritize the point-1.\r\n\r\n1)	If you agree I will release DR for these parts.\r\n\r\n2)	I would request you to part mark at SAAB on opposite side.\r\n\r\n3)	Please return these parts to CIM for remarking.\r\n','Please find the attached sheet that is part of existing process sheet that calls only part marking with reference to drawing.  \r\n\r\nSee attached new plan to implement and that will goes to part of process sheet that is better clarity for operator to carry out the part marking.\r\n\r\nI will attempt all A380 parts and I will make list which needs part marking instruction separately for both right hand and left hand.\r\n\r\nI will give you the other parts instruction shortly.\r\n','This batch reviewed and found correct and these parts were reworked at customer end','C35082','2015-02-26','Avinash(R.J.)','Manjunath(G)','Through mail','2015-02-26','NCR received through mail dated 26/02/2015','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','With Treatment','','CU','no','Misc','Avinash(R.J.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8270,'35-023','Saab AB','7605120-201','553979','L574 55120 201','ABM3 1029','C00',9,'1600099837','','39989','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','yes','Incorrect marking location','We have discussed with our team and he was mis interpreted the drawing and most of the drawings calls for “Far side & Near side” \r\n\r\nBut in this case drawing not addressed the far OR near side that leads to him misinterpreted.\r\n','I assume that there are three ways to correct these parts and I would request you to prioritize the point-1.\r\n\r\n1)	If you agree I will release DR for these parts.\r\n\r\n2)	I would request you to part mark at SAAB on opposite side.\r\n\r\n3)	Please return these parts to CIM for remarking.\r\n','Please find the attached sheet that is part of existing process sheet that calls only part marking with reference to drawing.  \r\n\r\nSee attached new plan to implement and that will goes to part of process sheet that is better clarity for operator to carry out the part marking.\r\n\r\nI will attempt all A380 parts and I will make list which needs part marking instruction separately for both right hand and left hand.\r\n\r\nI will give you the other parts instruction shortly.\r\n','Next batch found ok and these effetced parts were reworked at SAAB.','C35086','2015-02-26','Avinash(R.J.)','Manjunath(G)','Through mail','2015-02-26','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','With Treatment','','Cu','no','Misc','Avinash(R.J.)','no',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8271,'18-383A','Magellan Aerospace(Chalfont) Limited','SLEEVE BEARING ','Y11518','D575 40037 202','','A',1,'P/074123','','41467','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Thread Pitch changed.','While running time thread chatering came to avoid that chatering RPM is decreased that time pitch changed and thraed NOGO answerd.','Threadding insert changed and Run the parts in using Changed RPM the part is found okay.','Instruction given to all operators to not edit the program or RPM while running time in mazak machines.','CAPA found satisfactory, Next parts found okay','','2015-02-26','Narasimhamurthy(K.G.)','Narasimhamurthy(K.G.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','03','no','Misc','Ravi(M)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8272,'18-090A','Magellan Aerospace Bournemouth','BUSH','B4599A','D278 50164 200','S80 FHT','A',1,'RP400843','','40847','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','OD undersize by -0.005mm.','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\r\nand 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','CA/PA found satisfactory.','','2015-02-27','Dinakar(K)','Nandeesha(N)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','03','no','Misc','Sandhesh D(S)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8273,'35-299','Saab AB','SERRATED PLATE','564847A2','425Z0312-4','','--A',1,'1600098209','','41521','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','part bend so roughening time part lift,  ','Operation 03 running in vacuum fixture,using dia 16fl for roughing operation . this time over load in part face so release vacuum  part thick minus. ','change the program ,taken \"I\" machining program using in 8 fl roughing operation material removed smoothly,not effect balance parts .','Save this program ,next batch run same program. change in MPS sheet.  ','If MPS to be changed, Revision should be changed until then NC will not be closed','','2015-02-27','Rangaswamy()','Gurukiran S(M)','','0000-00-00','part bend so thickness -ve side,(-0.10)','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Gurukiran S(M)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8274,'18-340A','Magellan Aerospace Bournemouth','LANDING TOP PANNEL','A605640','F574 50961 200 01','','E, ECN PG49998ST1TV45',2,'RP400947','','40810','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Corrosion pits and deep dent marks observed on 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','','2015-02-27','Avinash(R.J.)','Nandishkumar(D.K.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','16660','POST DN','no','Misc','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8275,'18-341A','Magellan Aerospace Bournemouth','LANDING TOP PANNEL','A605640','F574 50966 200 01','','E, ECN PG49998ST1TV38',1,'RP400947','','40095','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Corrosion pits and deep dent marks observed on part surface.','Due to rubbing of tool or material behavior Corrosion Pits  has been observed  in Treatment house\r\n','Apply PX-24 after machining, and polishing and rubbing of tool should be avoided\r\n','Apply of PX-24 is mandatory before sending the parts to treatment house.\r\n','Next parts and batches found okay\r\n','','2015-02-27','Avinash(R.J.)','Nandishkumar(D.K.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','16636','POST DN','no','Misc','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8276,'35-230A','Saab AB','HINGE BRACKET 3 ','7599601','D576 50006 205','','D00',4,'1600093863 Rev-2','','38672','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','NDT failed.','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','','2015-02-28','Avinash(R.J.)','Manjunath(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','15771','POST DN','yes','Misc','Manjunath(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8277,'35-250','Saab AB','WASHER','9341','423Z1954-1','','--A',4,'1600097231','','40128','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','OD measures undersize(-0.03/0.08)','Chips cloted while finishing due to insuffiecient coolent.','Instructed operator to set the proper coolent and clean the chips before run the part.','Instructed operator to set the proper coolent and clean the chips before run the part.','CAPA found okay','','2015-02-28','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','FI','no','Misc','Manjunath(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8278,'18-226B','Magellan Aerospace Bournemouth','BRKT - NUT RETAINER','M424960','F572 53828 200','','A',1,'RP400846','','36693','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Part Width measures 0.2 plus. ','For continual improvements machining strategy changed from milling to Broaching. \r\nWhile doing Trails of new process this deviation observed.','Trails are under process. Process not proved yet.','Trails are under process. Process not proved yet.','Under Investigation','','2015-02-28','Rakeshbabu(V)','Manjunatha N.R.,Dhananjaya N,Anjinamurthy H,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','BMV 60-2','Narasimha Murthy(R)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8279,'18-098B','Magellan Aerospace Bournemouth','VALVE- SEAT','64442/01/00','D282 50060 204','','D',1,'RP400844','','41246','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Dig mark observed on part edge face.','While part final operation (top facing) running time part bend so part running time lifted.                                                                         ','Inform to operator before load the part check the bend.\r\nEvery part loading time clean the surface after load the part.\r\nWhen part bend observed immediately inform to concern supervisor.   ','Inform to operator before load the part check the bend.\r\nEvery part loading time clean the surface after load the part.\r\nWhen part bend observed immediately inform to concern supervisor.','CAPA found okay.Next parts found okay','','2015-02-28','Lohith(K)','Yarri Gowda,Rakesh  KC,Lohith K,Chiranjeevi S,Anjinamurthy H,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','VM2-2','Narasimha Murthy(R)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8280,'18-414B','Magellan Aerospace Bournemouth','ACTUATOR HOUSING','95744A','D278 50163 200','','D',1,'RP401021_Amnd No. 1','','41593','','0000-00-00',NULL,'yes','yes','yes','','','','','','no','Thickness under size by 0.1mm.  \r\n','In 5mm Blade groove tool(roughing)insert not seated properly.so 6mm thickness undersize','Instruction given to operator to change the insert .before setting and check the insert whether it is seated properly or not.  \r\n','Instruction given to operator to change the insert .before setting and check the insert whether it is seated properly or not.  \r\n','CAPA found okay, next parts found okay','','2015-02-28','Dinakar(K)','        Shivanand D.B.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8281,'18-412A','Magellan Aerospace(Chalfont) Limited','ROD END','245160','D321 53012 200','','F01',1,'LTA _For Treatments','','40624','','0000-00-00',NULL,'no','yes','yes','yes','no','no','no','no','no','R/M lenght 2mm under sized.','Store operator has to inspect the random Work Order qty, so one number was   missed  &  issue for production. ','All the qty  to  required size RM was inspected and end pieces/ under size RM were  identified and segregated separately. ','However Store Assistance shall be cross check the 100%  Raw material Dimension  before issuing  to  Production.','CAPA found okay','','2015-02-28','Sunil Kumar(K.R.)','Sunil Kumar(K.R.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','01','no','Misc','Sandhesh D(S)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8282,'18-314A','Magellan Aerospace Wrexham','STUD','551603','D278 50006 206 01','','D',1,'RP125889','','39965','','0000-00-00',NULL,'yes','','yes','','','','','','no','Edge chamfer to be SL4083, Chamfer size measures 0.5 x 45 deg. ','While doing chamfer adjustment in machine wear, operator entered the wrong value in machine wear.','Standard tools will be procured.','Operator instructed to select the standard tools.','Next batch found satisfactory.','','2015-03-02','Anjinamurthy(H)','        ','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8283,'18-377B','Magellan Aerospace Bournemouth','GAMMA FITTINGS ','M534700 91638','NSA840020-200','','L',1,'RP401479_Amend No-1','','40649','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','chips in butting face so total lenght -.1 and OD dent mark.','part not butting properly because small chips come from the master jaws so part butted cross and run the part so totel length under size.','for next part clean the jaws using air gun and before clamping check the chips inside the jaws and if any remove using the air gun or with waste after jaws found ok and load the part and running.','instruction given to operator to clean the jaws using air gun it is compulsary to use air gun to clean the jaws before loading the part.','CAPA found okay, next parts/batches found okay','','2015-03-02','Sandhesh D(S)','Nandeesha(N)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','03','no','Misc','Sandhesh D(S)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8284,'18-083A','Magellan Aerospace Wrexham','STUD PLATE','518635','D278 50007 201','ABM3 1029','D01',1,'RP125888','','41682','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Hole position is shifting(0.2mm)','While part running time part butting not properly. This is one of the operator mistake.   ','Inform to operator but the surface properly.','After loading the part into the fixture,it will be checked for air gaps between the part and the fixture using the feeler gauge and then start the machining.','CAPA found okay.Next parts found okay','','2015-03-02','Lohith(K)','        Yarri Gowda','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8285,'18-105A','Magellan Aerospace Bournemouth','FORKEND ASSEMBLY','241622','D572 50462 200','S98 FHT','J01',3,'RP400839','','38788','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Keyway wrong side machined.','When keyway operation running time part was wrong loaded. this is totally operator mistake.','Inform to operator keyway operation running time every part loading correctly as per process sheet before machining the part and check the thread all parts.  ','Inform to operator keyway operation running time every part loading correctly as per process sheet before machining the part and check the thread all parts. ','Next parts found okay','','2015-03-02','Lohith(K)','Punith G S,Dhananjaya N,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','9','no','VM2-1','Lohith(K)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8286,'18-003A','Magellan Aerospace Wrexham','BRACKET SUPPORT','0778801','D361 50111 200','ABM3 1029 T7651','A',1,'RP125887','','40897','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dent mark observed on the bottom face. ','Due to 05 operation part loading time location pin not guiding. Part top clamping time part dent mark observed on bottom face.  ','Immediately stop the machine and change the location pin after run the production.\r\nInstructed to operator every part loading time check the part hole and location pin. \r\nAny deviation observed time inform to concern supervisor.   ','Immediately stop the machine and change the location pin after run the production.\r\nInstructed to operator every part loading time check the part hole and location pin. \r\n','Next parts found okay','','2015-03-03','Lohith(K)','Yarri Gowda,Rakesh  KC,Punith G S,Lohith K,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','5','no','VM2-1','Anjinamurthy(H)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8287,'35-286','Saab AB','REINFORCEMENT','614086A7','423Z1985-2','','--A',1,'PA 1510 NEW PARTS-2','','41007','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dig mark on part.','Due to wrong loading of part in operation-02, this deviation coming.\r\nFirst batch production done and find this deviation in first off part.','Locating pin introduced to avoid wrong loading in operation-02.\r\nThis change mentioned in MPS and note added.','Locating pin introduced to avoid wrong loading in operation-02.\r\nThis change mentioned in MPS and note added.\r\nThis PA will not allow for wrong loading in both 35-285 and 35-286 parts.','CAPA found okay next parts/batches found good.','','2015-03-03','Rangaswamy()','Rangaswamy()','','0000-00-00','part wrong loading.','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Rangaswamy()','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8288,'35A-239','Saab AB','L/H KIT FOR ARD HINGE / J','','9901503-993','','Exhibit-B',2,'1600082519','','K03425','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Paint release after Dry Adhesion test.Part D57650004...is also suspected to have deviating distance between body and flange.','We have carriedout the 5 why analysis and found that the distance between slot is undersize by 0.05mm in untreated condition.','1) We have replaced this part from kit and put the acceptaed part as per assembly instruction.\r\n\r\n2) We will strip this part and to be maintain the slot dimensions as per drawing during untreated condition.\r\n\r\n3) Then we will carryout the surface treatemt operaion and assembly.','1) We kept dedicated snap gauge to check the slot width during assembly.','Next batch found ok.','C31336','2015-03-03','Avinash(R.J.)','Manjunath(G)','31336 and E-Mail','2014-12-12','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','cust end','yes','Misc','Manjunath(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8289,'35A-240','Saab AB','R/H KIT FOR ARD HINGE / J','','9901503-994','','Exhibit-B',3,'1600082519','','K03426','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Paint release after Dry Adhesion test.Part D57650004...is also suspected to have deviating distance\r\nbetween body and flange. ','We have carriedout the 5 why analysis and found that the distance between slot is undersize by 0.05mm in untreated condition.','1) We have replaced this part from kit and put the acceptaed part as per assembly instruction.\r\n\r\n2) We will strip this part and to be maintain the slot dimensions as per drawing during untreated condition.\r\n\r\n3) Then we will carryout the surface treatemt operaion and assembly.','1) We kept dedicated snap gauge to check the slot width during assembly.','Next batch found ok.','C31337','2015-03-03','Avinash(R.J.)','Manjunath(G)','31337 and Email.','2014-12-12','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','cust end','yes','Misc','Manjunath(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8290,'18-386A','Magellan Aerospace(Chalfont) Limited','NUT RING INNER','487664','D575 40039 200','','B',1,'P/074123','','41120','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Thicknees under size by (-0.05MM).','after running the key way setup we are done the parting for next setup so after 20 to 25 parts parting insert will be brocken or blented. In this setup after running a 15 parts parting insertedge chiped out and insert will rubbing the part so 0.1 taper occure in the next part so that part\r\nwill be rejected. ','next batch after every 20 nos one time parting insert will be checked thoroughly and before loadingthe next part parting insert checking after running. ','next batch after every 20 nos one time parting insert will be checked thoroughly and before loadingthe next part parting insert checking after running. ','CAPA found okay, next parts/batches found okay','','2015-03-03','Dinakar(K)','Manjunatha(N)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','07','no','Misc','Dinakar(K)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8291,'18-120C','Magellan Aerospace Bournemouth','HOUSING OUT B D BRG 3','CB872484','D275 56121 200','','E01,  ECN NG27011ST1KA83',1,'RP400843','','40767','','0000-00-00',NULL,'yes','yes','yes','','','','','','','2nd set up  problem so thickness (+)Side running time part rotating O D under size. \r\n\r\n','In 2nd set up thickness is maintained 0.1mm plus side.in finishing operation more stock measure part will rotate.when part rotated OD will undersize.  \r\n','For next part check the thickness and any deviation came that will be adjusted in work offset and run the part.  \r\n','For next part check the thickness and any deviation came that will be adjusted in work offset and run the  part.instructed to operators to check the dimension of 2nd set up before loading the part.  ','CAPA found satisfactory, Next parts found okay','','2015-03-03','Dinakar(K)','        Bharath R','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8292,'28-005A','Magellan Aerospace New York  Inc.','SHOULDER BOLT ','G21123','162A3109-1','','PL Iss A, PSDL Iss A',1,'124961_R0_C1','','39696','','0000-00-00',NULL,'yes','yes','yes','','','','','','no','running time thread (-) side 0.05','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.','Instructed to operator to check all the instruments whether it is set to zero or not before start the production.','CAPA found not okay, Basic checking of the part should be done properly cannot be said as CAPA','','2015-03-03','Narasimhamurthy(K.G.)','        KRISHNAMURTHY N','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8293,'35-183A','Saab AB','EDGE HOUSING','581308','423Z1121-6-02','','--A',1,'NOV 2014 ','','41568','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','*Bore inside tool dig mark.*','*Program Dia 16fl running at center bore,extra material hit to finish part and dig mark observed on part.\r\nReason for the dig mark is due to clamping not done for extra material. ','* Checked the tap on fixture and cross checked the tightness and rigidity of  clamping while running a cutout.\r\nTap damaged and Helicoil inserted and then continued production.','* Informed to all the operators to check the Tap and Bolts condition while doing firstoff part and Supervisors should monitor the same frequently.','CAPA found okay','','2015-03-03','Rangaswamy()','Rangaswamy()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Rangaswamy()','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8294,'35-251','Saab AB','SPACER','571610','423Z1987-1','','---',12,'PA 1510 NEW PARTS-1','','41477','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','dia 5.08 hole id taper hole center shift 0.2 to o.35. ','programme drilling operation running   before center bit operation not running so drill shifted to 0.35.','Next batch before drilling operation running centre bit opera tion was running in programme,this programme was save.','Next batch before drilling operation running centre bit opera tion was running in programme,this programme was save.','CAPA found okay','','2015-03-04','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','01','no','Misc','Dinakar(K)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8295,'18-057B','Magellan Aerospace Bournemouth','Top Skin Stiffener ','447026A6','L575 53249 201','','A00',1,'RP400837','','39284','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Linear indications observed on part surface.','Due to rubbing of tool linear indications has been found in Treatment house. \r\n','Instructed to Production department to avoid rubbing of tool and polishing \r\n','Avoid polishing and try to finish the part  in machining stage itself.\r\n','Next parts and batches found okay\r\n','','2015-03-04','Avinash(R.J.)','Nandishkumar(D.K.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','16881','POST DN','yes','Misc','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8296,'18-386A','Magellan Aerospace(Chalfont) Limited','NUT RING INNER','487664','D575 40039 200','','B',1,'P/074123','','41120','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','1.3mm drill bet cut','The drilling is done with an angle of 45 degrees. Due to coolant not flowing properly and might bechances of not clamping the part to jig 							\r\n','1)Drill bit grinding will be done and checked again and again.\r\n2)Proper flow of coolant is monitored regularly\r\n3)Clamping will be ensured twice before drilling 							\r\n','1)Drill bit grinding will be done and checked again and again. \r\n2)Proper flow of coolant is monitored regularly \r\n3)Clamping will be ensured twice before drilling 							\r\n','Next parts found okay','','2015-03-04','Nagaraju(T)','Nagaraju(T)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','09','no','Misc','Nagaraju(T)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8297,'28-045','Ellanef Manufacturing Corporation','LEVER','158511','65-51632-6','','PL_Rev - A + ADCN # 2 ; DL_Rev - N/C',5,'115865_Rel-0_Ch-0','','29045','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Slot width under size by 0.05 to 0.10 MM. ','We have inspected at our end 100% and found ok after that again offered to Magellan India and they have checked randomly.','1) We will moniter closly in the next production batch. ','1) We will arrange dedicated snap gauge to check slot width','To be measured','C27353','2015-03-04','Avinash(R.J.)','Sudhagar(V)','IRR113916','2015-02-27','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','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),(8298,'40-014','Universal Engineering Limited','STIFFENER BUTT STRAP ','4402102','D575 41603 200','','C01, ECN HG29999ST1TE12',2,'318176','','36667','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Countersinks over size by 0.7MM.','1) We have analyzed the problem and found that this was happened due to drawing mis interpretaion.\r\n2) During FAIR stage customer visited us and accepted the part.\r\n3) Based on the customer approval we have dispatched the item.','1) We have possibality to rework the parts.\r\n2) We will supply new FAIR to cover the omission of CSK holes.','New COS realesd to omit the CSK holes. ','Next batch found ok.','C32616','2015-03-04','Avinash(R.J.)','Sudhagar(V)','Thru maill','2015-03-03','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','0','Customer end','no','Misc','Sudhagar(V)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8299,'40-015','Universal Engineering Limited','STIFFENER BUTT STRAP','4402102','D575 41603 201','','C01, ECN HG29999ST1TE12',2,'318176','','36668','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','countersinks over size by 0.7MM.','We have analyzed the problem and found that this was happened due to drawing mis interpretaion.','1) We have possibality to rework the parts.\r\n2) We will supply new FAIR to cover the omission of CSK holes.','New COS realesd to omit the CSK holes.','Next batch found ok.','C32617','2015-03-04','Avinash(R.J.)','Sudhagar(V)','Thru maill','2015-03-03','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','0','Customer end','no','Misc','Sudhagar(V)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8300,'35-047','Saab AB','7605148-201','2016701','L574 55148 201','ABM3 1029','A00',1,'April 2015 A380','','41351','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','dia 5.7+/-0.2 hole out of Tolerance...  ','* Wrong tool selection by operator instead of dia 5.7 drill tool, he had run dia 6.35 drill.','* Operator not checked tool diameter. next part correct tool load and run part and hole diameter checked ok.','* Instructed to operator next time load the drill,hole mill or reamer, first check the tool diameter and prove the extra materiel.','CAPA found okay, next parts found okay','','2015-03-05','Girish(Prasad P)','Girish(Prasad P)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Girish(Prasad P)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8301,'28-044','Magellan Aerospace New York  Inc.','LINK ASSEMBLY UPPER UPLOC','A13435 ( WO No.-1432','161A6122-6','','PL_Rev-A, PSDL-Rev-N/C',1,'128961-3170','','40815','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','*Tool dig mark observed.','While doing operation 05, Operator wrong value moved in Y-Axis.(Instead of 35mm he moves 33mm). Due\r\nto this manual error Y reference shifted and dig mark observed on outer profile. Both the parts was\r\nrejected and operator finding this deviation after roughing operation completes. \r\n','After checking the deviation, operator analyzed and checked the Offset and found error.He informed\r\nto supervisor regarding the deviation in parts. Supervisor checked the offset and found deviation\r\nand he changed the offset and continued production after once cross checking the parameters. \r\n','This error is due to operator. Process was proved and there is no problem with the\r\nprocess. Training conducted to operator for Process pertaining to operation-05 and methods of cross\r\nchecking the offset. Informed to supervisor to monitor the operators and train then regularly in\r\nfront of machines to avoid manual errors. \r\n','CAPA holds good next parts or batches found okay','','2015-03-05','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','3','no','Misc','Lohith(K)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8302,'35-238A','Saab AB','JACK BRACKET 2 ','688933A1','D576 50010 207','','D00',1,'1600104409','','41237','','0000-00-00',NULL,'yes','yes','yes','','','','','','','* Wall thickness under size 1 mm.(3.82+/-0.25) (MSR 2.6 to 2.8mm)','* Wrong tool selection by operator instead of dia 6X45CHF tool, he had run dia 8 ball nose.','* Correct tool no enter in program then run next part and operator cross checked tool diameter, next part found ok.','* Instructed to operator m/c inside tool removing time inform to supervisor. \r\n* M/c inside tool remove time enter \"M0\" to all program.\r\n* All program running time cross check tool diameter. ','Next parts found okay.','','2015-03-05','Girish(Prasad P)','        Manukumar H M','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8303,'35-272','Saab AB','PIN','970533','425Z0601-3','','--A',4,'PA 1510 NEW PARTS-2','','39589','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','od undersize (-0.03mm to -0.05mm)','Due to while OD operation running time insert brokened so OD under size. ','New insert added and tool offset takened run the part and checked the od dimension is ok continuve the production.','Instructed operator to every 15 nos will be completed\r\nchecked the insert. ','CAPA acceptable.','','2015-03-05','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Dinakar(K)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8304,'35-272','Saab AB','PIN','970533','425Z0601-3','','--A',2,'PA 1510 NEW PARTS-2','','39589','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no',' 1 no operation missing    1 no od step.','','','','under investigation','','2015-03-05','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','','03','yes','Misc','Dinakar(K)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8305,'18-118B','Magellan Aerospace Bournemouth','BEARING HOUSING','240866','D275 40005 200','','C01',2,'RP400842','','40953','','0000-00-00',NULL,'yes','yes','yes','','','','','','','I.D over size by+0.01mm.','In ID roughing setup running time insert will be chipped out and part will came in plus side and that part not checking the operator and for next part he found out part will become over sized and he change the insert and maintain the Inner dia in required size. but previous part not maintain in proper diameter. So in the finishing setup that part loading time finishing tool get the more stock and chips will be rubbed in the inner diameter and part will be over size by 0.01mm So part will become rejected.  \r\n','checking the all parts outer and inner diameter before loading in the finished setup and change the previous insert tip and .2 plus taken in the wear offset and run the part and after check the diameter and give the proper correction and run the part and check the part found ok. and after every 15 to 20 ns chnge the finished inserttip and run the part so this problem not repeated again.  \r\n','In roughing setup for every part check outer and inner diameter for using air gauge. In finishing set up every 15 to 20 ns change the finished insert tip and run the part so this problem not repeated again.  \r\n','CAPA found satisfactory, Next parts found okay','','2015-03-05','Dinakar(K)','        Shivappa M B','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8306,'40-016','Universal Engineering Limited','ANGLE SUPPORT ','M374880','D924 50146 204','','J, ECN NW21405ST1KA27',1,'320402 - S3','','41084','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dig mark observed on part.','As per Process part machining will complete in 03 setup.Slitting done after machining completion.\r\nWhile slitting operation completes, Flatness is not achieving as per drawing requirements.\r\nTherefore process changed and one more operation added to get the flatness as per requirements.\r\nWhile doing this change, Part lifts from vice and dig mark observed on part.\r\n\r\n\r\n ','Due to this problem, Butting clock planned to strengthening the part clamping and continued production. \r\n50nos production done and checked the consistency of the parts and found that process was OK.\r\n','New process proved and MPS up-issued rev-00 to rev-01.','CAPA found okay','','2015-03-06','Rangaswamy()','Shivashankar(H.G.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Rangaswamy()','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8307,'18-161C','Magellan Aerospace Bournemouth','STRUT AFT INNER','A615341','F574 50156 206','','E, PG41301ST1KA70, PG49998ST1TW43, PG40011ST1KF25',1,'RP400845','','41750','','0000-00-00',NULL,'yes','yes','yes','','','','','','','part profile cutout.','part wrong side loading by new operator.\r\nreloading the 01st operation finishing part.','* gave instruction to operator about part loading,\r\n* senior operator monitored the new operator, \r\n* giving proper training to  operator about part loading,\r\n* giving training to operator about drawing and process sheet.   ','* gave instruction to operator about part loading,\r\n* senior operator monitored the new operator, \r\n* giving proper training to  operator about part loading,\r\n* giving training to operator about drawing and process sheet.   ','Next parts found okay','','2015-03-06','Narayanappa(G)','        Narayanappa G','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8308,'07-002A','HAL-NASIK','WALL 1 ROOT PART-LH','AS-12327','11.2000.2.101.004','V95pchT2','Nil',1,'NK/M/2513(4520)/MP/O','','41601','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','After rework Part accepted.',' ','','','','','2015-03-06','Narayanappa(G)','Manjunath(K.N.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Manufacture Only','','03','yes','Misc','Narayanappa(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8309,'18-161C','Magellan Aerospace Bournemouth','STRUT AFT INNER','A615341','F574 50156 206','','E, PG41301ST1KA70, PG49998ST1TW43, PG40011ST1KF25',1,'RP400845','','41750','','0000-00-00',NULL,'yes','yes','yes','','','','','','','part profile cutout.','Refer NCR no.08307 ','Refer NCR no.08307 ','Refer NCR no.08307 ','Next parts found okay','','2015-03-06','Narayanappa(G)','        Narayanappa G','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8310,'18-414B','Magellan Aerospace Bournemouth','ACTUATOR HOUSING','95744A','D278 50163 200','','D',1,'RP401021_Amnd No. 1','','41593','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Part wrong loaded so 6.05 thickness (-2.0mm)','Instead of loading 2nd side loaded 1st side, in first side 6mm thickness finished and the same will be loaded in second side 2mm stock for 2nd side is maintaining that 2mm under size in 1st side.so 6mm thickness undersize by 2mm.','For next part check the part whether it is loaded.first side or second side and run the part.','instructed operator to check the part whether it is loaded properly.in 1st set up using marker to write 1st on the face and identify the second set up and load that face is second set up.','CAPA found satisfactory, Next batches found okay','','2015-03-06','Dinakar(K)','        Bharath R','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8311,'18-319A','Magellan Aerospace Bournemouth','HALF CLAMP ','8031','D574 50552 200','DTD 5014','B01',1,'RP400946_Amnd_No.1','','40583','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Machine abuse observed inside the hole.','Due to rubbing of tool Machine abuse has been found in Treatment house\r\n','Instructed to Production department to avoid rubbing of tool and polishing \r\n','Avoid polishing and try to finish the part  in machining stage itself.\r\n','Next parts and batches found okay\r\n','','2015-03-06','Avinash(R.J.)','Nandishkumar(D.K.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','16786','POST DN','no','Misc','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8312,'35A-239','Saab AB','L/H KIT FOR ARD HINGE / J','','9901503-993','','Exhibit-B',1,'1600091593','','K03714','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Paint release on part D576 50004 002.','Little bit primer breakage noticed at customer due to less adhesion in the anodizing.','1) Cusomer accepted to rework the parts at their facility.\r\n2) Informed to treatemt supplier and recomnded to use good gloves during handling after anodizing.\r\n3) Customer accepted the part after rework.','1) We will carry out we adhesion test after assembly prior to dispatch at CIM.','Next batch found ok.','C33586','2015-03-08','Avinash(R.J.)','Manjunath(G)','Through mail dated 05th Mar2015 from Marcus','2015-03-05','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','Assembly','','cust end','no','Misc','Manjunath(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8313,'35-169','Saab AB','ALCD_STRUCT_SUPPORT-FTG_L','581311','423Z1200-12-01','','---',1,'1600096186','','40360','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','*Chamfer oversize 4mm (required 8.85 measured 13.90)*\r\n ','* While running operation-02, Dia 10ballnose tool offset not taken by operator to due misinterpretation of data sheet in MPS>','* After checking the first off part, error noticed in tool offset and corrected and then next part machined and check the chamfer and found as per drawing requirement.','* Informed to operator and supervisor to check the tool and work offset once and after ensuring both run the programs.\r\nSupervisor to monitor and train the operator to avoid manual errors.','CAPA found okay.','','2015-03-09','Rangaswamy()','Rangaswamy()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','DN','no','Misc','Manjunath(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8314,'35-082','Saab AB','HOUSING-SIDE ROLLER','682234A0','F579 53065 202','ABM3-1029 T7651','B, PG52307ST4KA80',1,'1600087350 Rev 1 ','','41118','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Total thickness minus 2mm','Due to outer profile program running time clamping washer broken so part was lifted.  ','Immediately stop the machine, change the clamping washer after continue the production.\r\nInform to operator every part loading and unloading time observe the clamping washer. ','Next batch production running time added all new clamps.\r\n','Next parts found okay','','2015-03-09','Lohith(K)','        Lohith K','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8315,'18-209B','Magellan Aerospace(Chalfont) Limited','BODY','4842','D321 40204 202','','D, ECN NR29999ST1KM15, NR29999ST2KF65, WQN DFB09775',1,'P/074113','','41822','','0000-00-00',NULL,'yes','yes','yes','','','','','','','U DRILL FARM PROVEING TIME BORE DIG MARK SO PART REJECT.','Dia 32.56 and dia 25.34mm bore is finished using dia 20.0 drill,12mm special tool and 16mm and 20mm boring tool and to finish the bore it will taken 10minutes,to reduce the cycle time new tool loaded(Form Tool)and taken offsets run the part,while running time chips not coming outside and rubbed inside the bore.so bore dig mark found.','For next part Form Tool is replaced and old process  is run and part found okay.','Instruction given to operator to dont use the new tools when they are not prooved.','CAPA found okay. Next batch found okay','','2015-03-09','Dinakar(K)','        Dinakar K','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8316,'18-102A','Magellan Aerospace Bournemouth','BARREL-STRUT','247348','D572 50463 200','S98 FHT','F',2,'RP400839','','39664','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','ID Thread NOGO Answerad.','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.  \r\n','Instruction given to operator to take x-offset & z-offset whenever the inserts are changed and monitor supervisors.  \r\n','CAPA found satisfactory, Next parts found okay','','2015-03-09','Dinakar(K)','Seetharamu D,Ravi R,Narasimhamurthy K.G.,Mohan Kumar C.M.,Manohara M,GUNDEGOWDA H.G.,Girish V M,Dinakar K,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','FI','no','DX 200-2 ','Narasimha Murthy(R)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8317,'18-078A','Magellan Aerospace Wrexham','ADAPTOR ','18178771','A282 50081 200','','A',1,'RP125890','','41251','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','ID Oversize by 0.02mm.(58.12/58.16 Measure 58.18)','Chips clogged during the final pass,hence the deviation is occured.','Inform the operator to clean the chips near the tool and neatly flowing the coolant at the insert edge to avoid this deviation.','Inform the operator to clean the chips near the tool and neatly flowing the coolant at the insert edge to avoid this deviation.','CAPA found satisfactory, Next parts found okay','','2015-03-09','Sandhesh D(S)','Manjunatha(P)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','01','no','Misc','Ravi(M)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8318,'18-295A','Magellan Aerospace Bournemouth','BOLT','238302','D577 56145 200','S80','A',1,'RP400846','','40550','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','face dentmark.','Production batch running time after running the some parts he clamp the parts in the jaws and he press the declamp pad but not pick the part that time part will sliped to chip conveyor and chips blented in the part face so part will be rejected..  ','Handling time this problem will be occured inform to the all about handling the parts and this problem not repeated again.','We are done the or used the so many methods for avoiding the rejection in handling the job ex:wooden pallets, sleeves, covers and using the partition box etc but in this problem will came in slip the job so this problem not repeated again.  ','CAPA found okay','','2015-03-10','Ravi(M)','Manjunatha(N)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','01','no','Misc','Ravi(M)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8319,'35-251','Saab AB','SPACER','571610','423Z1987-1','','---',4,'PA 1510 NEW PARTS-1','','41477','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','ID over size by 0.05mm.','Insert was worn out so this problem occurred. \r\n \r\n','Check insert status regularly and know the life of inserts and change inserts according instructions.\r\n','Check insert status regularly and know the life of inserts and change inserts according instructions.\r\n','CAPA found okay','','2015-03-10','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','fi','no','Misc','Dinakar(K)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8320,'18-415B','Magellan Aerospace Bournemouth','ACTUATOR HOUSING','95744A','D278 50163 201','','D',1,'RP401022_Amend No 1','','40872','','0000-00-00',NULL,'yes','yes','yes','','','','','','','* Part profile shift.','* Trans program running time m/c reset so operator not observed trans.','* We will be cancelling all Trans for machines at the starting and ending time. Trans instead in program middle will be taking place.','* We will be cancelling all Trans for machines at the starting and ending time. Trans instead in program middle will be taking place.','Repeated CAPA cannot be acceptable','','2015-03-10','Girish(Prasad P)','        Yogesha K','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8321,'18-210B','Magellan Aerospace(Chalfont) Limited','BODY','5757','D321 40204 204','','D, ECN NR29999ST1KM15, NR29999ST2KF65, WQN DFB09775',1,'P/074113','','40780','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Part total length undersize.(-0.05mm)part total 187.7lmm length.measure length 187.33mm. ','Due to part butting problem so total length under size.  \r\n','Next Load the part and rotate the part in MDI mode and checking the thru and run the part the total length found OK. ','Next Load the part and rotate the part in MDI mode and checking the thru and run the part the total length found OK.','CAPA found satisfactory, Next parts found okay','','2015-03-11','Dinakar(K)','KRISHNAMURTHY(N)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Narasimhamurthy(K.G.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8322,'18-412A','Magellan Aerospace(Chalfont) Limited','ROD END','245160','D321 53012 200','','F01',1,'LTA _For Treatments','','40624','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Thread NOGO Gauge no go answered.   \r\n   \r\n  ','After 25nos running threading insert will be wear out.for next part threading insert will be changed and 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\r\n  \r\n','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 0.05mm and run the part and then gauge answered and next part run in same reading & the part found okay.  \r\n  \r\n','Instruction given to operator to take x-offset & z-offset whenever the inserts are changed.  \r\n','CAPA found satisfactory, Next parts found okay','','2015-03-12','Dinakar(K)','        Manjunatha N','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8323,'35-082','Saab AB','HOUSING-SIDE ROLLER','682234A0','F579 53065 202','ABM3-1029 T7651','B, PG52307ST4KA80',1,'1600087350 Rev 1 ','','41118','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Running time bore over size.','Due to bore operation running time chips clotted so bore 20 micron over size. \r\n','Instructed to operator every part bore running time before clean the bore  after run the program \r\n','Instructed to operator every part bore running time before clean the bore  after run the program \r\n','Next parts found okay','','2015-03-12','Lohith(K)','Lohith(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','00','no','Misc','Lohith(K)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8324,'18-328A','Magellan Aerospace Wrexham','NUT ANCHOR ','8900','D572 51346 200','','A',10,'RP125889','','40828','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Tread NOGO answered.  ','Due to operator negligence this error happened. While threading operation running,Operator not checking the treads by gauge,so 10nos thread NO GO answered.\r\nReason for the error is not found now, due to machine parameter error for threading cycles. ','The action taken for both errors as follows,\r\n1. Operator is to be inspect the parts 100% in gauges.\r\n2. Informed to machine supplier to check the parameters and train us for the concept of threading cycles in machine.\r\n    ','Preventive Action is pending.\r\nTo analyzed the problem checking activity planned in machine and same will complete before 30/04/2015','Under review','','2015-03-12','Lohith(K)','Rakesh (KC)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','3','no','Misc','Lohith(K)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8325,'35-138','Saab AB','FLCD_DS_SUPPORT_DEFLECT_S','501721','423Z6189-3','BAC1534-62C','---',1,'1600101109','','40181','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','MATERIAL LAYER CHIP OUT.','It was happening while doing the part marking or packing in supplier end,Now we are given a instruction about this material and to handle this material very carefully. ','It was happening while doing the part marking or packing in supplier end,Now we are given a instruction about this material and to handle this material very carefully. ','It was happening while doing the part marking or packing in supplier end,Now we are given a instruction about this material and to handle this material very carefully. ','Next batch found satisfactory.','','2015-03-12','Avinash(R.J.)','Manjunath(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','Post DN','no','Misc','Manjunath(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8326,'35-178','Saab AB','SUPPORT-SEAL-RETAINER','428596B','423Z1833-3-02','','---',1,'PA-1300 2014','','40177','','0000-00-00',NULL,'no','yes','no','yes','no','yes','no','no','no','Deep hole observed on part. (blow Holes)','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','','2015-03-12','Avinash(R.J.)','Manjunath(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','Post DN','no','Misc','Manjunath(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8327,'18-001A','Magellan Aerospace Wrexham','BRACKET SUPPORT-LH','0778801','D361 50110 200','ABM3 1029 T7651','A',1,'RP125887','','40687','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Hole deburr running time part dig mark observed. ','Due to part clamping not properly. ','Inform to operator when load the part check in location pin length. Remove the old location pin and replace the new location. Inform to operator before run the programs check the location pin and clamps ','Inform to operator when load the part check in location pin length. Remove the old location pin and replace the new location. Inform to operator before run the programs check the location pin and clamps ','Next parts found okay','','2015-03-12','Lohith(K)','Theerthappa(K.N.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','00','no','Misc','Lohith(K)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8328,'35-283','Saab AB','REINFORCEMENT','563339A1','423Z1983-2-01','','--A',1,'PA 1510 NEW PARTS-2','','41992','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Thickness minus min3.48 measures 3.42 (0.05minus)','Thickness minus side find out in Final inspection.\r\n72 nos production done in a batch and identified 01no. deviation and reason was not found.\r\nAsked the operators regarding the problem and all 3 are not aware of deviation.\r\nTherefore reasons for reject is not found, and same will analyzed in next batch production.','Process checked and tried to analyzed the problem, but only manual error will cause the error.\r\nTherefore reasons for reject is not found, and same will analyzed in next batch production.','Preventive action not taken and same will check in next batch production.','Under Review','','2015-03-13','Rangaswamy()','Rangaswamy()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','DN','no','Misc','Manjunath(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8329,'18-056B','Magellan Aerospace Bournemouth','Top Skin Stiffener ','447026A6','L575 53249 200','','A00',1,'RP400837','','40683','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Linear indications observed on part surface.','Due to rubbing of tool linear indications has been found in Treatment house. \r\n','Instructed to Production department to avoid rubbing of tool and polishing \r\n','Avoid polishing and try to finish the part  in machining stage itself.\r\n','Next parts and batches found okay\r\n','','2015-03-13','Avinash(R.J.)','Nandishkumar(D.K.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','17002','POST DN','yes','Misc','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8330,'35-284','Saab AB','REINFORCEMENT','431589B2','423Z1984-2-01','','--A',1,'PA 1510 NEW PARTS-2','','41202','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Hole chamfer oversize 0.5mm at hole.\r\nOut of tolerance as per standard.','While doing chamfering operation in fitting, this manual error happened. \r\nWhile doing manual deburring, in drilling machine fitter put more pressure and causes more chamfer on hole.','Informed to fitter to check the pressure and concentrate while doing manual work.\r\nFitting supervisor is monitoring and guide them to avoid such manual errors','Planned to complete the hole chamfer in manual low RPM drilling machine to avoid such problems.','Under Review','','2015-03-13','Rangaswamy()','Rangaswamy()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','DN','no','Misc','Manjunath(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8331,'18-162C','Magellan Aerospace Bournemouth','STRUT AFT INNER','A615341','F574 50156 207','','E, PG41301ST1KA70, PG49998ST1TW43, PG40011ST1KF25',1,'RP400845','','41752','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Dig mark.','When the parts was shifting to packing section through lift after coming from Treatment house by miss placing 1 part got stuck to wall while moving in shift','Instructed packing individuals to keep the parts in such a manner that the should not touch anywhere since these extrusions are bit lengthy parts, or else carry manually by hand.','Instructed packing individuals to keep the parts in such a manner that the should not touch anywhere since these extrusions are bit lengthy parts, or else carry manually by hand.','CAPA found okay','','2015-03-14','Dayananda(K.G.)','Dayananda(K.G.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','00','05','no','Misc','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8332,'18-309B','Magellan Aerospace(Chalfont) Limited','SPIGOT','Y12196','F 575 51290 200','S80','B, ECN PG49999SMAKH49',1,'P/074122','','40922','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Base thickness 0.1 mainess','Due to roughing operation tool offset wrong taken. This is new operator mistake.  ','Training given to new operator how to take in tool offset and work offset.\r\nInform to senior operator every time new operator take the offset or any operation running time check after run the machine. ','Inform to senior operator every time new operator take the offset or any operation running time check after run the machine. ','CAPA found okay, next batches by the new operator will be monitored','','2015-03-16','Lohith(K)','        Rakesh  KC','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8333,'18-333B','Magellan Aerospace Bournemouth','PLATE COVER','2889503','D282 50280 200','','A',1,'RP400947','','42120','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Dig mark observed on radius. ','Due to operator mistake this error happened. Operator not given correct cutter composition value (CRC) in tool parameters.Operator not check the machine setting graph. \r\n        ','Inform to operator crc program running time give correct CRC value.\r\nInstruction given to operator, every time first part setting time or running time check the graph   ','Training given to operator every time 1st off  part running time how to check program, setting graph, work offset trans and mirror.','Next parts found okay','','2015-03-17','Lohith(K)','        Dhananjaya N','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8334,'18-090A','Magellan Aerospace Bournemouth','BUSH','221668','D278 50164 200','S80 FHT','A',277,'RP400843','','38887','','0000-00-00',NULL,'no','no','no','no','no','yes','yes','yes','no','Diffrence in material colour.','Informed RM supplier ','Informed RM supplier ','Informed RM supplier ','Informed RM supplier ','','2015-03-17','Nagaraja (G)','Sunil Kumar(K.R.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Manufacture Only','','04','yes','Misc','Avinash(R.J.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8335,'35-238A','Saab AB','JACK BRACKET 2 ','688933A1','D576 50010 207','','D00',2,'1600104409','','41237','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Bore dia measured out of tolerance.','Dia 16FL using for Bore finish.in this tool running crc program so operator enter wrong value,part rejected. ','Enter correct CRC value then production run. every part bore checked.','Next batch bore finish not using 16fl or crc program,using  30.175 reamer.','Reamer to be procured then NC will be closed','','2015-03-17','Rangaswamy()','Mahesh(N)','','0000-00-00','Bore dia measured out of tolerance.','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','05','no','Misc','Rangaswamy()','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8336,'28-041','Magellan Aerospace New York  Inc.','LEVER ASSY-SECONDARY SPOI','158327','65-46358-16','','PL_E, DL_N/C, Sketch # 1',2,'126288-3186_R0_C1','','39530','','0000-00-00',NULL,'yes','no','no','no','yes','yes','no','no','no','Hole pitch shifted by 1.00 mm. ','This deviation found first time through the production batches.\r\nwhile running Boring operation, The dia 10 x 6.34 location pin in the fixture went inside the fixture and part not located in fixture while doing boring operation, causes shift of control bore.\r\nThe hole to hole pitch shifted by 1mm.','After finding the deviation in parts at FI, Problem analyzed and find a CA/PA as follows,\r\n1.Locating Pin brazed to fixture to avoid movement of Pins.\r\n2.This CA will avoid this type of error in further batches.\r\n\r\n','Next batch production done, pin movement cross checked and find no deviation in movement.\r\nThis CA will not cause errors in further batches.\r\n','CAPA found okay, next parts/batches found okay','','2015-03-17','Dinakar(K)','Yarri Gowda,Vasu SN,Theerthappa K.N.,Shivaraj K S,Shivappa M B,Ravi R,Rajesh T,Punith G S,Ningaraj A N,Mohan Kumar C.M.,Manohara M,Dhananjaya N,Devaraj K.C.,Chiranjeevi S,Bharath R,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','QT100S-2','Sudhagar(V)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8337,'18-333B','Magellan Aerospace Bournemouth','PLATE COVER','2889503','D282 50280 200','','A',1,'RP400947','','42120','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Slot width over size.','While part running time dia 8R2.5 concave cutter automatically down. So part slot width  over size.    ','Immediately stop the machine and check the tool offset, all offset check after continue the production.\r\nInform to operator every program completed time apply the air on part.\r\nWhen Combined program running use the optional stop in every program. ','When use Special tools check and after run the next program.\r\n ','Next parts found okay','','2015-03-17','Lohith(K)','        Lohith K','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8338,'18-413B','Magellan Aerospace Bournemouth','ACTUATOR HOUSING','9161','D278 50162 200','','A',1,'RP401021_Amnd No. 1','','40567','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Thickness undersize by -0.1mm(6.0mm thickness measure 5.9mm).','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 0.3mm because groove width not maintained in middle tollerance. ','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.','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.','CAPA found okay. Next batch found okay','','2015-03-18','Dinakar(K)','SHIVAKUMAR()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Narasimhamurthy(K.G.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8339,'18-414B','Magellan Aerospace Bournemouth','ACTUATOR HOUSING','M563530','D278 50163 200','','D',1,'RP401021_Amnd No. 1','','40568','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Thickness under size by 0.1mm','In 5mm Blade groove tool(roughing)insert not seated properly.so 6mm thickness undersize.','For next part grooving insert is replaced by new one and seated correctly and taking x and z offset run the partspart found ok.','Instruction given to operator to change the insert .before setting and check the insert whether it is seated prooerly or n0t.','Repeated CAPA. NC will not be closed.','','2015-03-18','Dinakar(K)','Shivashankar H.G.,Shivappa M B,Shivanand D.B.,SHIVAKUMAR ,Rangaswamy ,Rajesh T,Raghavendra Rao R,Prashanth Kumar M,Karthineyan V.S.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','DX 200-1','Narasimha Murthy(R)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8340,'18-313A','Magellan Aerospace Wrexham','STUD ','247348','D278 50006 204 01','','D',1,'RP125889_Amnd-01','','42091','','0000-00-00',NULL,'yes','','yes','no','','no','','yes','','part runninge time flat thinkness under size by (-0.06)','Due to work offset not taken to the exact value.','During 1st off should keep 0.10mm up side then it take in to the correct value.','Operator instructed to check the work offset during 1st off.','Next batch found satisfactory.','','2015-03-18','','        S. Shiva Kumar','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8341,'35-140','Saab AB','BCD_DR_BEAM_FTG_UPR_FWD_4','434837','424Z1130-14-01','7050 - T7451 ALUMINU','--B',1,'1600082632','','41896','','0000-00-00',NULL,'yes','yes','yes','','','no','','','no','Dig mark observed on part.   ','Part wrongly loaded in operation-03.Clamping bolt diagonally and able to clamp at both the orientations. Operator not noticed the loading of part and dig mark observed after running roughing tool because part was wrongly loaded.','Immediately checked and marked the front face for all the remaining parts. \r\nInformed to operators to ensure the front face after loading the part in fixture.\r\nImmediately LH  part clamping hole blocked production continued and supervisor is monitoring.','The following PA action planned and implemented, next batch production running time  fixture changed and amended in MPS. \r\n','CAPA found okay. For LH part new fixture can be done and MPS should be changed.','','2015-03-18','Anjinamurthy(H)','        Anjinamurthy H','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8342,'18-090A','Magellan Aerospace Bournemouth','BUSH','B4599A','D278 50164 200','S80 FHT','A',1,'RP400843','','40847','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','OD undersize by -0.1mm.','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 -0.1mm 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','CA/PA found satisfactory.','','2015-03-19','Narasimhamurthy(K.G.)','Narasimhamurthy(K.G.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','01','no','Misc','Sandhesh D(S)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8343,'18-121A','Magellan Aerospace Bournemouth','BARREL - STRUT','247348','D572 50463 201','S98 FHT','F',5,'RP400839','','39666','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','3Ns ID thread gauge not answered and 2ns milling operation pending.','1)Thread was damaged due to wear out of inserts. The perator intended to rework the damaged thread\r\nresulting in non conformance of ID. 2)The Following route cause analyzed for the parts rejected,\r\nJaws Boring is not good,part not butted properiy to the jaws because of small chips are in Part\r\nbutting faces.Roughing and Finishing inserts wear out.','1)Insert was worn out at that stage which was replaced for the next job. 2)The Following CA/PA\r\ntaken to avoid the rejections.Sizes and Tolerance for Roughing stage clean the jaws with the help\r\nof air and before loading the part.after clamping the every part check the part it was butted in\r\nthe jaws face properly.','1)The block holding the tool shall be set by the Supervisor for every batch which is expected to\r\nextend the tool life and reduce these type of non conformances. 2)The Following CA/PA taken to\r\navoid the rejections.Sizes and Tolerance for Roughing stage clean the jaws with the help of air and\r\nbefore loading the part.after clamping the every part check the part it was butted in the jaws face\r\nproperly.','CA/PA found satisfactory.','','2015-03-19','Narasimhamurthy(K.G.)','Seetharamu(D)','','0000-00-00','3Ns ID thread gauge not answered.and 2ns milling operation pending.','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Manufacture Only','','03','yes','Misc','Sandhesh D(S)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8344,'18-260C','Magellan Aerospace Bournemouth','BUTTSTRAP UPP RS4X9356','436556','L575 53341 201','','B00',1,'RP401009','','42187','','0000-00-00',NULL,'yes','','yes','','','','','yes','no','18-260c 1nos center thinkness 0.1(+side) rework time center thinkness -side (-0.3) so part rejected.','During bench work this was happened. \r\nRework noticed due to bend in the material','Before loading to machine, bend will be checked by the operator OR concerned person.','Same as above','Next batch found satisfactory.','','2015-03-19','Anjinamurthy(H)','        Girish HP','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8345,'18-353A','Magellan Aerospace(Chalfont) Limited','PLATE ASSY SLIDE','B4479A','F575 51138 202','S145','E01, ECN PG49999ST1QC77',1,'P/074122','','40917','','0000-00-00',NULL,'yes','yes','yes','','','','','','no','Dia 6.6 drill running time tip chip out hole (+)side','While part running time dia 6.6 drill chip out.So part hole diameter 0.2mm over size. Tool manager not given new drill. Re sharping drill running time drill chip out observed.    ','Instructed to operator every part when drilling operation done check the drill visually.\r\nInform to tool manager grinding drill angle and cutting edges check after give the production.     ','Before run the drilling program and program end added in M00.\r\nInform to tool manager S145 material part production running time grinding drill angle and cutting edges check after give the production.','Next parts found okay','','2015-03-19','Lohith(K)','        Hari Prasad','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8346,'35-176A','Saab AB','LATCH_ACT_PIVOT-FTG ','581304','423Z1205-2-02','','--B',2,'1600101109','','40170','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','ID BORE OVER SIZE BY 0.008 TO 0.010MM.','This has happened due to Airgauge Problem, the Airgauge which was checked in the Inprocess was having deviation of 10 microns.','Instrument was calibrated and ensured that all the instruments which are near to calibration will not be issued and the Quality Inspector should ensure the First off of these types of instruments like Airgauges, Faro etc','Instrument was calibrated and ensured that all the instruments which are near to calibration will not be issued and the Quality Inspector should ensure the First off of these types of instruments like Airgauges, Faro etc','CAPA found okay','','2015-03-19','Avinash(R.J.)','Manjunath(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','With Treatment','','Post DN','no','Misc','Manjunath(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8347,'35-176A','Saab AB','LATCH_ACT_PIVOT-FTG ','564338','423Z1205-2-02','','--B',38,'1600101109','','40169','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','ID BORE OVER SIZE BY 0.006 TO 0.009MM.','This has happened due to Airgauge Problem, the Airgauge which was checked in the Inprocess was having deviation of 10 microns.','Instrument was calibrated and ensured that all the instruments which are near to calibration will not be issued and the Quality Inspector should ensure the First off of these types of instruments like Airgauges, Faro etc','Instrument was calibrated and ensured that all the instruments which are near to calibration will not be issued and the Quality Inspector should ensure the First off of these types of instruments like Airgauges, Faro etc','CAPA found okay','','2015-03-19','Avinash(R.J.)','Manjunath(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','With Treatment','','Post DN','no','Misc','Manjunath(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8348,'35-176A','Saab AB','LATCH_ACT_PIVOT-FTG ','614048A7','423Z1205-2-02','','--B',3,'1600101109','','40171','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','ID BORE OVER SIZE BY 0.008 TO 0.010MM.','This has happened due to Airgauge Problem, the Airgauge which was checked in the Inprocess was having deviation of 10 microns.','Instrument was calibrated and ensured that all the instruments which are near to calibration will not be issued and the Quality Inspector should ensure the First off of these types of instruments like Airgauges, Faro etc','Instrument was calibrated and ensured that all the instruments which are near to calibration will not be issued and the Quality Inspector should ensure the First off of these types of instruments like Airgauges, Faro etc','CAPA found okay','','2015-03-19','Avinash(R.J.)','Manjunath(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','With Treatment','','Post DN','no','Misc','Manjunath(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8349,'35-183A','Saab AB','EDGE HOUSING','581308','423Z1121-6-02','','--A',2,'1600097307','','39034','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1) Base thickness minus side -0.43 for out of tolerance. \r\n2) Bore dia plus side (+0.010) for out of tolerance.','1) While running base finish program, dia 16r3 cutter down and base thickness measures 0.4mm minus side.\r\n2) Dia 124.14 mm bore measures ovelality after completion of operation in machine.Bore was measures with in tolerance in clamping condition, but after removing clamps bore measures 0.010mm out of tolerance due to bend and twist in part.','1)After checking the part in stage, checked the tool offset and find deviation, therefore holder changed and taken new offset and continued production with Z-offset crosschecking for every part.\r\n2)All parts flatness checked with blue in surface table and continued production, further parts found ok.','1)All the tool holders and collects condition checked and found ok, except another 1 no. holder quarantined due problem suspected in rigid clamping.\r\n2)Mandatory parts flatness to be check for 35-182A and 35-183A due to bore diameter is more and chances of ovality in bore.','CAPA found okay','','2015-03-22','Girish(Prasad P)','Gurukiran S M,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','MakinoF5','Manjunath(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8350,'18-112A','Magellan Aerospace Bournemouth','BODY TURNBUCKLE INNER','A0484U','D575 41541 200','S80 FHT','A',1,'RP400841','','41695','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Thread NOGO answerd.','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\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','CA/PA found satisfactory.','','2015-03-23','Dinakar(K)','Dinakar K,Ashith B,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','3','no','DX 200-2 ','Narasimhamurthy(K.G.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8351,'18-188A','Magellan Aerospace Bournemouth','BUSH','1203522407','L575 50397 200','B23','B00',1,'RP400846','','42342','','0000-00-00',NULL,'yes','yes','yes','','','','','','','OD under size(-0.006m).','In OD roughing setup running time insert will be chipped out and part will came in plus side and that part not checking the operator and for next part he found out part will become over sized and he change the insert and maintain the outer dia in required size. but previous part not maintain in proper diameter. So in the finishing setup that part loading time finishing tool get the more stock and chips will be rubbed in the outer diameter and part will be -.006 micron under sized. So part will become rejected.  \r\n  \r\n','checking the all parts outer and inner diameter before loading in the finished setup and change the previous insert tip and .2 plus taken in the wear offset and run the part and after check the diameter and give the proper correction and run the part and check the part found ok. and after every 15 to 20 ns chnge the finished inserttip and run the part so this problem not repeated again.','In roughing setup for every part check outer and inner diameter for using air gauge. In finishing set up every 15 to 20 ns change the finished insert tip and run the part so this problem not repeated again.  \r\n','CAPA found satisfactory, Next parts found okay','','2015-03-23','','        Dinakar K','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8352,'18-411A','Magellan Aerospace(Chalfont) Limited','PLUNGER','240136','D321 40205 200','','H01',1,'LTA _For Treatments','','40907','','0000-00-00',NULL,'no','yes','yes','no','no','no','yes','no','no','Dent mark observed on OD.','While part running time dia 8.5 H.S.S. drill  broken. Trial run time drill broken. \r\nWhile drill removing time part OD dig mark. ','Next part running time Hitachi make drill loaded and after continue the production.\r\nInform to operator next batch production running time only use for Hitachi Dia8.5H.S.S drill.  ','Next part running time Hitachi make drill loaded and after continue the production.\r\nInform to operator next batch production running time only use for Hitachi Dia8.5H.S.S drill.','CAPA found okay, next parts found okay','','2015-03-23','Lohith(K)','Theerthappa K.N.,Shivaraj K S,Hari Prasad,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','5','no','HAASVF2SS-2','Lohith(K)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8353,'35-284','Saab AB','REINFORCEMENT','431589B2','423Z1984-2-01','','--A',19,'PA 1510 NEW PARTS-2','','41993','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','After treatment polishing marks observed on the surface.','Due to rubbing of tool Polishing marks has been found in Treatment house. \r\n','Instructed to Production department to avoid rubbing of tool and polishing \r\n','Avoid polishing and try to finish the part  in machining stage itself.\r\n','Next parts and batches found okay\r\n','','2015-03-24','Avinash(R.J.)','Manjunath(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','17370','Post Dn','yes','Misc','Manjunath(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8354,'35-283','Saab AB','REINFORCEMENT','563339A1','423Z1983-2-01','','--A',6,'PA 1510 NEW PARTS-2','','41992','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','After treatment polishing marks observed on the surface.','Due to rubbing of tool polishing marks 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','','2015-03-24','Avinash(R.J.)','Manjunath(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','17340','Post Dn','yes','Misc','Manjunath(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8356,'28-007A','Magellan Aerospace New York  Inc.','Shaft Support Lever','0-25-06718','251A1747-1','Ti-6AL-4V Per Mil-T-','N/C',3,'127388_R0_C0','','41490','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','1)2-nos OD under size by 0.003MM.\r\n2)1-no Thickness under size by 0.04MM.','After running 50 to 60 parts insert tip will be worn out and it will rub the part so ovality will be occure in the \r\nrunning part. So part one side shows reading -0.003 and \r\nanother side shows +0.002 so part will be rejected.\r\n','remove the worn out insert and replace the new insert\r\nand newely offset taken and 0.2 (+)plus taken in the tool wear offset and run the part and then check the outer diameter and give the correction in  wear offset and run the part and checked found ok. \r\n','while setting time loading the new insert before running and after every 50 nos change the  insert and run the part. and every 25ns onece observe the tool insert while running. \r\n','Repeated CAPA cannot be accepted','','2015-03-24','Ravi(M)','Vasu SN,Ningaraj A N,Narasimhamurthy K.G.,Bharath R,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','11','no','QT100S-2','Ravi(M)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8357,'28-007A','Magellan Aerospace New York  Inc.','Shaft Support Lever','0-25-06718','251A1747-1','Ti-6AL-4V Per Mil-T-','N/C',1,'125338_R0_C1','','41278','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Undercut tool dig mark.','1mm thickness plus side so again that part taken to rework. after the rework dig mark observed in the undercut diameter so part will be rejected.     ','while doing rework time dialing the every rework part before running program. ','while doing rework time dialing the every rework part before running program. ','Next parts found okay','','2015-03-24','Dinakar(K)','Vasu SN,Rajesh B D,Ningaraj A N,Nataraja C V,Narasimhamurthy K.G.,Nandeesha N,Manjunatha N,Manjunath  M,KRISHNAMURTHY N,GUNDEGOWDA H.G.,Bharath R,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','0','FI','no','DX 200-3','Sudhagar(V)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8358,'18-121A','Magellan Aerospace Bournemouth','BARREL - STRUT','247348','D572 50463 201','S98 FHT','F',5,'RP400839','','39666','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dummy','Dummy','Dummy','Dummy','Dummy','','2015-03-25','Narasimhamurthy(K.G.)','Seetharamu(D)','','0000-00-00','3Ns ID thread gauge not answered.and 2ns milling operation pending.','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','Manufacture Only','','03','no','Misc','Sandhesh D(S)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8359,'18-121A','Magellan Aerospace Bournemouth','BARREL - STRUT','247348','D572 50463 201','S98 FHT','F',5,'RP400839','','39666','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dummy','Dummy','Dummy','Dummy','Dummy','','2015-03-25','Narasimhamurthy(K.G.)','Seetharamu(D)','','0000-00-00','3Ns ID thread gauge not answered.and 2ns milling operation pending.','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','Manufacture Only','','03','no','Misc','Sandhesh D(S)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8360,'35-080','Saab AB','PLAIN BUSH','H7233','S64 2S385','DTD-197','7-S64',31,'PA 1217-Bushes (A320','','29136','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','ID bore oversize by 0.010mm and Ovality.','After wear out of insert operator as to give minor correction for adjustment for that time it was gone wrong so this divination was occurred. \r\n\r\n','Planned for incorporate one more tool between rough and finish cut for maintain same reading for finishing tool.\r\n \r\n','After proving this method feed back will be taken and\r\nsame will be updated.  \r\n \r\n','CAPA found okay','','2015-03-25','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','15909','Post DN','no','Misc','Manjunath(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8361,'35-080','Saab AB','PLAIN BUSH','H7233','S64 2S385','DTD-197','7-S64',21,'PA 1217-Bushes (A320','','29137','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','ID bore oversize by 0.010mm and Ovality.  ','After wear out of insert operator as to give minor correction for adjustment for that time it was gone wrong so this divination was occurred. \r\n\r\n','Planned for incorporate one more tool between rough and finish cut for maintain same reading for finishing tool.\r\n \r\n','After proving this method feed back will be taken and\r\nsame will be updated.  \r\n \r\n','CAPA found okay','','2015-03-25','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','15910','Post DN','no','Misc','Manjunath(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8362,'18-210B','Magellan Aerospace(Chalfont) Limited','BODY','5757','D321 40204 204','','D, ECN NR29999ST1KM15, NR29999ST2KF65, WQN DFB09775',2,'P/074113','','42334','','0000-00-00',NULL,'','','yes','','','','','','','Runing time 16mm boring tool screw broken  bore + side','Instead of maintain 0.3mm stock in ID it remove 0.4mm extra because of boring tool screw was loose during running time.','Boring tool screw is replaced by new one and taking x and z offset for that tool and run the part.part found okay and continue the production.','Instructed to all operator to dont use any slipped screws in the tools and it is compulsary to replace slipped screws before start the production.','CAPA found okay, next parts/batches found okay','','2015-03-25','','        Devaraj K.C.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8363,'18-104A','Magellan Aerospace Bournemouth','BODY TURNBUCKLE','239338','D575 40490 200','S80 FHT','E',1,'RP400840','','39671','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','ID Thread nogo answer.','Thread was damaged due to wear out of inserts.  Bcause machine cenre height not correct.The operator intended to rework the damaged thread resulting in non conformance of ID.  \r\n','Insert was worn out at that stage which was replaced for the next job and adjusted the machine centre heigt to extend the tool and insert life.  \r\n','The block holding the tool shall be set by the Supervisor for every batch which is expected to extend the tool life and reduce these type of non conformances and supervisors give to training  to operators.  \r\n','CAPA found satisfactory, Next parts found okay','','2015-03-25','Dinakar(K)','Seetharamu D,Ravi R,Mohan Kumar C.M.,Manohara M,Girish V M,Dinakar K,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','FI','no','DX 200-2 ','Narasimha Murthy(R)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8364,'18-394A','Magellan Aerospace Bournemouth','VALVE BODY','405978','A284 40009 200','','A',3,'RP400947','','40860','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','ID Radius not found.','In ID face step is obtained,to remove that step taken for rework and manual program done and in that program radius is not given so radius came that is the reason.','Radius given in the program and run the part .part found okay and continue the rework.','To check all the parts visually after machining for steps marks etc,and when doing rework check the program and run the part.','CAPA found okay, next parts/batches found okay','','2015-03-25','Ravi(M)','Vasu SN,Shivanand D.B.,Raghavendra Rao R,Ningaraj A N,Nataraja C V,Bharath R,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','FI','no','QT100S-2','Narasimha Murthy(R)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8365,'18-382A','Magellan Aerospace(Chalfont) Limited','SLEEVE BEARING ','240136','D575 40037 200','','A',1,'P/074123','','42455','','0000-00-00',NULL,'','','yes','','','','','','','ID Ovality bore 0.006micron plus.\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','CAPA found satisfactory, Next parts found okay','','2015-03-25','','        Manjunatha N','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8366,'18-090A','Magellan Aerospace Bournemouth','BUSH','K10011','D278 50164 200','S80 FHT','A',1,'RP400843','','42328','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','outer diameter dig mark.','After roughing Not maintaining the proper stock for finishing tool so finishing tool running time part rotated and dent mark observed in outer diameter so part will be rejected.','Check the every part finishing stock and then load the part.and skin cut given to the jaws and set the proper chuck pressure and change the insert and 0.4 plus taken in the wear offset and run the part then check the part and  given proper currection in wear offset and run the part and part checked found ok.','maintain the all parts in same size and maintain the equal stock for the finishing tool and maintain the proper chuck pressure and avoiding the these type of rejections.','CAPA found okay','','2015-03-25','Dinakar(K)','Vasu(SN)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','03','no','Misc','Sandhesh D(S)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8367,'18-034B','Magellan Aerospace Bournemouth','CARRIER SEAL','1149303 1','D575 55658 201','','C',21,'RP400836','','39135','','0000-00-00',NULL,'yes','no','no','no','no','yes','no','yes','no','That there is a Up-issue of COS from Iss-B to Iss-C due to the inclusion of “Coarse grain material removal note”.\r\nThe manufacturing Document to suitably address this change.\r\nPart No: D575 55658 200/201\r\nAttachments: Part iss: C, Dwg iss: D, COS ISS:C\r\n','The Existing Manufacturing document MPS/18-033B Iss-00 and MPS/18-034B Iss-00 was reviewed against the requirement of the New COS Iss-C and the requirement is not addressed but this again reviewed in the NC-Program and found new COS Iss-C requirement met .\r\nSo these parts manufactured with the above manufacturing documents can be released to COS Iss-C\r\n','we will carry out the Delta FAIR for new PO for higher configuration. ','We will request customer to take the stcok parts with ordered old PO.','Under Review','','2015-03-26','Avinash(R.J.)','Manjunatha N.R.,Girish HP,Diwakar R.B.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','With Treatment','15827','FI','no','BMV 60-2','Muniyappa(N)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8368,'34-032A','Magellan Aerospace Winnipeg','FITTING BASE HINGE FWD AC','A120091','400-12780-1-905','','EM 104302_Iss A, 105092_Iss E',2,'B91379-Rev-016','','33406','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','COC and Final inspection reports PAS 09967 Revision called as B against  A . ','1. We had discussed and got the clearance from Magellan India through mail dated 09/06/2014 to dispatch the parts with holes for that batch but misunderstanding we released the parts to \"PAS B\" instead of \"PAS A\"\r\n2.Part was manufactured  as per PAS Rev A and customer approval was obtained to dispatch the parts with old PAS rev. Parts dispatched against  Po C30793, which  calls for a blanket order B91379 Rev 024 in which PAS Rev B is called. due to miss understanding of customer approval documents was  corrected to match the PO. \r\n','In future all old configuration parts if any will be quarantined. Parts will be dispatched to customer only after obtaining special approval from customer and remarks on the COC.\r\nQuality alert will be issued.\r\n','In future all old configuration parts if any will be quarantined. Parts will be dispatched to customer only after obtaining special approval from customer and remarks on the COC.\r\nQuality alert will be issued.\r\n','Will be monitoring future batch   ','C35431','2015-03-26','Avinash(R.J.)','Sudhagar(V)','Thru maill','2015-03-26','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','Manufacture Only','0','Customer end','no','Misc','Sudhagar(V)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8369,'28-006','Magellan Aerospace New York  Inc.','SHOULDER BOLT','G19699K04','162A3109 2','15-5PH Bar,Per AMS56','NA',101,'120168_R0_C0','','34509','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','1)Thread gauge not answer.','•	Gauge found oversize and came to know only after calibration\r\n•	Initially CIM Gauge no-17 was used in the stage and later came to know the gauge found oversize. So parts again re-ensured by thread pitch micrometer\r\n•	After parts were passed from TPM, then we released the parts to next stage\r\n•	Thread ring gauge procured from local supplier(Thread gauge product) is not consistent in the quality\r\n•	This make sometimes it works for hundred numbers and sometimes it goes to five hundred numbers and later we did came to know by experience\r\n','•	Thread Pitch micrometer calibrator not available at our local certify to NABL\r\n•	So TPM self checked by ourselves with \" Master Thread Plug Gauge \" of different frequencies for usage and this is to be done every time for new batches of production.\r\n•	We will enquire TPM calibrator and they are approved to NABL or other standard.\r\n•	Based on our experience and current issue, we will use measuring frequency of TRG for hundred to one fifty numbers only, after that we will send for calibration\r\n•	After calibration and based on the results/wear out in gauge, we will fix the frequency for next usage up to fifty to hundred numbers.\r\n•	Any time we will keep three gauges, one is to production and one is to inspection and another one for stock.\r\n•	Mean time we will enquire for other makes also. \r\n','•	Thread Pitch micrometer calibrator not available at our local certify to NABL\r\n•	So TPM self checked by ourselves with \" Master Thread Plug Gauge \" of different frequencies for usage and this is to be done every time for new batches of production.\r\n•	We will enquire TPM calibrator and they are approved to NABL or other standard.\r\n•	Based on our experience and current issue, we will use measuring frequency of TRG for hundred to one fifty numbers only, after that we will send for calibration\r\n•	After calibration and based on the results/wear out in gauge, we will fix the frequency for next usage up to fifty to hundred numbers.\r\n•	Any time we will keep three gauges, one is to production and one is to inspection and another one for stock.\r\n•	Mean time we will enquire for other makes also. \r\n','Rework done and found okay ','C30883','2015-03-26','Avinash(R.J.)','Sudhagar(V)','IRR113772','2014-08-20','','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),(8370,'28-006','Magellan Aerospace New York  Inc.','SHOULDER BOLT','G19876K01','162A3109 2','15-5PH Bar,Per AMS56','NA',19,'120168_R0_C0','','35965','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','1)Thread gauge not answer.','\r\n•	Gauge found oversize and came to know only after calibration\r\n•	Initially CIM Gauge no-17 was used in the stage and later came to know the gauge found oversize. So parts again re-ensured by thread pitch micrometer\r\n•	After parts were passed from TPM, then we released the parts to next stage\r\n•	Thread ring gauge procured from local supplier(Thread gauge product) is not consistent in the quality\r\n•	This make sometimes it works for hundred numbers and sometimes it goes to five hundred numbers and later we did came to know by experience\r\n','•	Thread Pitch micrometer calibrator not available at our local certify to NABL\r\n•	So TPM self checked by ourselves with \" Master Thread Plug Gauge \" of different frequencies for usage and this is to be done every time for new batches of production.\r\n•	We will enquire TPM calibrator and they are approved to NABL or other standard.\r\n•	Based on our experience and current issue, we will use measuring frequency of TRG for hundred to one fifty numbers only, after that we will send for calibration\r\n•	After calibration and based on the results/wear out in gauge, we will fix the frequency for next usage up to fifty to hundred numbers.\r\n•	Any time we will keep three gauges, one is to production and one is to inspection and another one for stock.\r\n•	Mean time we will enquire for other makes also. \r\n','•	Thread Pitch micrometer calibrator not available at our local certify to NABL\r\n•	So TPM self checked by ourselves with \" Master Thread Plug Gauge \" of different frequencies for usage and this is to be done every time for new batches of production.\r\n•	We will enquire TPM calibrator and they are approved to NABL or other standard.\r\n•	Based on our experience and current issue, we will use measuring frequency of TRG for hundred to one fifty numbers only, after that we will send for calibration\r\n•	After calibration and based on the results/wear out in gauge, we will fix the frequency for next usage up to fifty to hundred numbers.\r\n•	Any time we will keep three gauges, one is to production and one is to inspection and another one for stock.\r\n•	Mean time we will enquire for other makes also. \r\n','Rework done and found okay with the parts','C32115','2015-03-26','Avinash(R.J.)','Sudhagar(V)','IRR113786','2014-09-11','','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),(8371,'28-006','Magellan Aerospace New York  Inc.','SHOULDER BOLT','G19699K04','162A3109 2','15-5PH Bar,Per AMS56','NA',20,'120168_R0_C0','','34533','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','1)Thread gauge not answer.','\r\n•	Gauge found oversize and came to know only after calibration\r\n•	Initially CIM Gauge no-17 was used in the stage and later came to know the gauge found oversize. So parts again re-ensured by thread pitch micrometer\r\n•	After parts were passed from TPM, then we released the parts to next stage\r\n•	Thread ring gauge procured from local supplier(Thread gauge product) is not consistent in the quality\r\n•	This make sometimes it works for hundred numbers and sometimes it goes to five hundred numbers and later we did came to know by experience\r\n','•	Thread Pitch micrometer calibrator not available at our local certify to NABL\r\n•	So TPM self checked by ourselves with \" Master Thread Plug Gauge \" of different frequencies for usage and this is to be done every time for new batches of production.\r\n•	We will enquire TPM calibrator and they are approved to NABL or other standard.\r\n•	Based on our experience and current issue, we will use measuring frequency of TRG for hundred to one fifty numbers only, after that we will send for calibration\r\n•	After calibration and based on the results/wear out in gauge, we will fix the frequency for next usage up to fifty to hundred numbers.\r\n•	Any time we will keep three gauges, one is to production and one is to inspection and another one for stock.\r\n•	Mean time we will enquire for other makes also. \r\n','•	Thread Pitch micrometer calibrator not available at our local certify to NABL\r\n•	So TPM self checked by ourselves with \" Master Thread Plug Gauge \" of different frequencies for usage and this is to be done every time for new batches of production.\r\n•	We will enquire TPM calibrator and they are approved to NABL or other standard.\r\n•	Based on our experience and current issue, we will use measuring frequency of TRG for hundred to one fifty numbers only, after that we will send for calibration\r\n•	After calibration and based on the results/wear out in gauge, we will fix the frequency for next usage up to fifty to hundred numbers.\r\n•	Any time we will keep three gauges, one is to production and one is to inspection and another one for stock.\r\n•	Mean time we will enquire for other makes also. \r\n','Rework done and found okay with the parts','C32116','2015-03-26','Avinash(R.J.)','Sudhagar(V)','IRR113784','2014-09-10','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Manufacture Only','','Customer end','yes','Misc','Sudhagar(V)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8372,'28-006','Magellan Aerospace New York  Inc.','SHOULDER BOLT','G19876K01','162A3109 2','15-5PH Bar,Per AMS56','NA',46,'120168_R0_C0','','35967','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','1)Thread gauge not answer.','•	Gauge found oversize and came to know only after calibration\r\n•	Initially CIM Gauge no-17 was used in the stage and later came to know the gauge found oversize. So parts again re-ensured by thread pitch micrometer\r\n•	After parts were passed from TPM, then we released the parts to next stage\r\n•	Thread ring gauge procured from local supplier(Thread gauge product) is not consistent in the quality\r\n•	This make sometimes it works for hundred numbers and sometimes it goes to five hundred numbers and later we did came to know by experience\r\n','•	Thread Pitch micrometer calibrator not available at our local certify to NABL\r\n•	So TPM self checked by ourselves with \" Master Thread Plug Gauge \" of different frequencies for usage and this is to be done every time for new batches of production.\r\n•	We will enquire TPM calibrator and they are approved to NABL or other standard.\r\n•	Based on our experience and current issue, we will use measuring frequency of TRG for hundred to one fifty numbers only, after that we will send for calibration\r\n•	After calibration and based on the results/wear out in gauge, we will fix the frequency for next usage up to fifty to hundred numbers.\r\n•	Any time we will keep three gauges, one is to production and one is to inspection and another one for stock.\r\n•	Mean time we will enquire for other makes also. \r\n','•	Thread Pitch micrometer calibrator not available at our local certify to NABL\r\n•	So TPM self checked by ourselves with \" Master Thread Plug Gauge \" of different frequencies for usage and this is to be done every time for new batches of production.\r\n•	We will enquire TPM calibrator and they are approved to NABL or other standard.\r\n•	Based on our experience and current issue, we will use measuring frequency of TRG for hundred to one fifty numbers only, after that we will send for calibration\r\n•	After calibration and based on the results/wear out in gauge, we will fix the frequency for next usage up to fifty to hundred numbers.\r\n•	Any time we will keep three gauges, one is to production and one is to inspection and another one for stock.\r\n•	Mean time we will enquire for other makes also. \r\n','Rework done and found okay with the parts','C32116','2015-03-26','Avinash(R.J.)','Sudhagar(V)','IRR113784','2014-09-10','','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),(8373,'18-371B','Magellan Aerospace Bournemouth','GAMMA FITTINGS ','M305800 66010','NSA840007-150','','N',2,'RP401477_Amend No.-1','','40473','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Total lenght 0.2 undersized.','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 offsetso 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.','CAPA found okay next parts/batches found good.','','2015-03-27','Dinakar(K)','Nandeesha(N)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','03','no','Misc','Sandhesh D(S)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8375,'18-380B','Magellan Aerospace Bournemouth','GAMMA FITTINGS ','M498560 88629','NSA840020-350','','L',28,'RP397607','','31460','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','K,G,J& H dimension all are undersize in 0.010 to 0.030.','The Following route cause analyzed for the parts rejected, 1. Ovality in RM. 2. Total Length Minus in RM. 3. Improper Butting in Jaws. 4. Jaws Boring is not good( Flatness is not achieved. 5. RM unclear on OD and ID. 6. Ovality More than 0.05mm in billet stage. 7. Chips clocking at the Jaws ,In Part butting faces. 8. Roughing and Finishing inserts wear out. ','The Following CA/PA taken to avoid the rejections, 1.Sizes and Tolerance for Roughing stage.(Sample\r\nparts made to check the parts visually also for reference) 2. Compulsorily use 6-Jaw chuck for all\r\nthe Gamma for both roughing and Finishing operations. 3.Plan for Parts to be inspect for Face out\r\nand Ovelity before loading for finishing operations. 4.Methods of tightening the part on to the\r\nMandril in operation-02. 5.create the rough surface on OD in roughing operation to strengthening\r\nthe clamping.','The Following CA/PA taken to avoid the rejections, 1.Sizes and Tolerance for Roughing stage.(Sample\r\nparts made to check the parts visually also for reference) 2. Compulsorily use 6-Jaw chuck for all\r\nthe Gamma for both roughing and Finishing operations. 3.Plan for Parts to be inspect for Face out\r\nand Ovelity before loading for finishing operations. 4.Methods of tightening the part on to the\r\nMandril in operation-02. 5.create the rough surface on OD in roughing operation to strengthening\r\nthe clamping.','CAPA found okay, next parts/batches found okay','','2015-03-27','Dinakar(K)','Nandeesha N,Kalakappa T H,Girish S,Dinakar K,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','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),(8376,'35-238A','Saab AB','JACK BRACKET 2 ','688933A1','D576 50010 207','','D00',2,'1600101900','','41379','','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\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','','2015-03-27','Avinash(R.J.)','Nagaraj(G. Nadiger)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','17404','POST DN','yes','Misc','Manjunath(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8377,'35-238A','Saab AB','JACK BRACKET 2 ','688933A1','D576 50010 207','','D00',13,'1600104409','','41237','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','NDT FAILE.','Due to rubbing of tool or material behaviour NDT failure has been found in Treatment house\r\n','Instructed to Production  & fitting department to avoid rubbing of tool and polishing \r\n','Avoid polishing and try to finish the part  in machining stage itself.\r\n','Next parts and batches found okay\r\n','','2015-03-27','Avinash(R.J.)','Nagaraj(G. Nadiger)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','17405','POST DN','yes','Misc','Manjunath(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8378,'18-388A','Magellan Aerospace Bournemouth','ACTUATOR HOUSING','M397520 76863A','D278 50162 200','','A',3,'RP393593','','26774','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','FAIR Proved part at the time get rejected.','FAIR Proved part at the time get rejected.','FAIR Proved part at the time get rejected.','FAIR Proved part at the time get rejected.','next part found ok.','','2015-03-28','Muniyappa(N)','SHIVAKUMAR ,Nagaraju K.S.,Manjunatha S N,MALLIKARJUNA Gowda,Ashith B,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','ST20','Muniyappa(N)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8379,'18-098B','Magellan Aerospace Bournemouth','VALVE- SEAT','64442/01/00','D282 50060 204','','D',6,'RP400844','','41139','','0000-00-00',NULL,'no','no','no','yes','yes','yes','no','no','no','Flatness out of tolerance in 0.062 to 0.1mm.','','','','Under review','','2015-03-28','Muniyappa(N)','Nandishkumar(D.K.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','16996','POSTDN','no','Misc','Muniyappa(N)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8380,'35-188','Saab AB','INTERCOSTAL_MIDSPAN_NO_2 ','599430','423Z1170-1-05','','---',1,'1600102067','','41676','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','profile point out off tolerance & base thick minus.','This was happened due to clamping problem, due to not clamping properly step was found the base side while reworking it manually base thickness found minus side','Informed to operators to clamp the parts correctly and ensure the butting face with feeler gauge and ensure twice about clamping of the part','Informed to operators to clamp the parts correctly and ensure the butting face with feeler gauge and ensure twice about clamping of the part','CAPA found okay','','2015-03-28','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','profile point out off tolerance & base thick minus. ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Rangaswamy()','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8381,'18-098B','Magellan Aerospace Bournemouth','VALVE- SEAT','64442/01/00','D282 50060 204','','D',1,'RP400844','','41245','','0000-00-00',NULL,'no','no','no','yes','yes','yes','no','no','no','Flatness out of tolerance in 0.062 to 0.1mm.','','','','Under review','','2015-03-28','Muniyappa(N)','Nandishkumar(D.K.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','16998','POSTDN','no','Misc','Muniyappa(N)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8382,'18-098B','Magellan Aerospace Bournemouth','VALVE- SEAT','64442/01/00','D282 50060 204','','D',7,'RP400844','','41245','','0000-00-00',NULL,'no','no','no','yes','yes','yes','no','no','no','Flatness out of tolerance in 0.062 to 0.1mm.','','','','Under review','','2015-03-28','Muniyappa(N)','Nandishkumar(D.K.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','16998','POSTDN','no','Misc','Muniyappa(N)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8383,'18-413B','Magellan Aerospace Bournemouth','ACTUATOR HOUSING','9161','D278 50162 200','','A',1,'RP401021_Amnd No. 1','','40567','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Machine abuse observed on part surface.','Due to rubbing of tool Machine abuse has been found in Treatment house\r\n','Instructed to Production department to avoid rubbing of tool and polishing \r\n','Avoid polishing and try to finish the part  in machining stage itself.\r\n','Next parts and batches found okay\r\n','','2015-03-29','Avinash(R.J.)','Nandishkumar(D.K.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','17429','POST DN','no','Misc','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8384,'18-414B','Magellan Aerospace Bournemouth','ACTUATOR HOUSING','95744A','D278 50163 200','','D',1,'RP401021_Amnd No. 1','','41593','','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','','2015-03-29','Avinash(R.J.)','Nandishkumar(D.K.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','17472','POST DN','no','Misc','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8385,'28-041','Magellan Aerospace New York  Inc.','LEVER ASSY-SECONDARY SPOI','158327','65-46358-16','','PL_E, DL_N/C, Sketch # 1',1,'129853','','40874','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Running time chips rubbing so bore diameter 0.02 over sized.','When doing ID finishing, chips clocking in insert and chips rubbed and chatter mark observed on part. Tryed to remove chatter mark and find ID diameter plus side by  0.02mm.  \r\n  \r\n \r\n','Informed to operator to check the insert wear out and coolant flow regularly to avoid chips clogging.  \r\n \r\n','Informed to operator to check the insert wear out and coolant flow regularly to avoid chips clogging.  \r\n','Repeated CAPA cannot be accpetable','','2015-03-29','Dinakar(K)','GUNDEGOWDA(H.G.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','07','no','Misc','Sandhesh D(S)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8386,'18-122A','Magellan Aerospace Bournemouth','FORKEND ASSEMBLY','518330','D572 50462 201','S98 FHT','J01',1,'RP400839','','40845','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','program editing problem undercut dia undersize.  \r\n','In Dx2002 machine program is not transfered that time program is edited manually that time one line missed.so part rejected. ','Check the program and and edited the missed line correctly and run the part part found okay. ','To check the program when you are edited manually before run the part and supervisor will be cross checked the  program.  \r\n','CA/PA found ok and also further batches found satisfactory.','','2015-03-29','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','03','no','Misc','Narasimhamurthy(K.G.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8387,'40-019','Universal Engineering Limited','SPACER','94479','D924 50147 200','','A, ECN NW20011ST1KB22, HG20002ST1KB68',2,'320402 - S3','','41591','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dig Marks found on the part','After finishing of the part, parts fell down and dig marks found on the surface','After finishing parting tool will be introduced and with the help of gauge the part will be taken out without falling down ','After finishing parting tool will be introduced and with the help of gauge the part will be taken out without falling down','CAPA found okay','','2015-03-29','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Krishna(Chowdary.G.P.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8388,'40-019','Universal Engineering Limited','SPACER','94478','D924 50147 200','','A, ECN NW20011ST1KB22, HG20002ST1KB68',10,'320402 - S3','','41705','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dig Marks found on the surface','After finishing of the part, parts fell down and dig marks found on the surface','After finishing parting tool will be introduced and with the help of gauge the part will be taken\r\nout without falling down','After finishing parting tool will be introduced and with the help of gauge the part will be taken\r\nout without falling down','CAPA found okay','','2015-03-29','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Krishna(Chowdary.G.P.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8389,'18-032A','Magellan Aerospace Bournemouth','BUSH','W72421','D278 50165 200','S80 FHT','A',80,'RP400838','','41295','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','ID Over size 0.01 to 0.025mm.','Chips clogged during the final pass,hence the deviation is\r\noccured.','Inform the operator to clean the chips near the tool and neatly flowing the coolant at the insert edge to avoid this\r\ndeviation.','Inform the operator to clean the chips  near the tool and neatly flowing the coolant at the insert edge to avoid this\r\ndeviation.','CAPA found okay','','2015-03-29','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','FI','no','Misc','Narasimha Murthy(R)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8390,'18-213A','Magellan Aerospace(Chalfont) Limited','END CAP ','20740','D321 40209 200','','A, ECN NR29998ST1JA76',26,'P/074114','','37803','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Corrosion pits obsereved inside thread.','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','','2015-03-30','Avinash(R.J.)','Nandishkumar(D.K.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','15966','POST DN','no','Misc','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8391,'18-030A','Magellan Aerospace Bournemouth','PIN','W71720','D278 50156 200','S130 FHT','A',8,'RP400838','','41087','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Dig marks observed on part surface.','Before sending the parts to Treatment house parts was checked 100%and found okay but after treatment\r\nparts found damaged','Informed to Treatment supplier to handle the parts carefully and keep the parts separately without\r\nhaving metal to metal contac','Informed to Treatment supplier to handle the parts carefully and keep the parts separately without\r\nhaving metal to metal contac','CAPA found okay','','2015-03-30','Avinash(R.J.)','Nandishkumar(D.K.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','17013','POST DN','no','Misc','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8392,'18-030A','Magellan Aerospace Bournemouth','PIN','W71720','D278 50156 200','S130 FHT','A',2,'RP400838','','41087','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Part found Damaged after treatment.','Before sending the parts to Treatment house parts was checked 100%and found okay but after treatment\r\nparts found damaged','Informed to Treatment supplier to handle the parts carefully and keep the parts separately without\r\nhaving metal to metal contact','Informed to Treatment supplier to handle the parts carefully and keep the parts separately without\r\nhaving metal to metal contact','CAPA found okay','','2015-03-30','Avinash(R.J.)','Nandishkumar(D.K.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','17013','POST DN','no','Misc','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8393,'18-422A','Magellan Aerospace(Blackpool) Limited','BRACKET','M498460 88620A','PI201484603','','NIL',1,'P/501934','','41385','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','part dig mark noticed. ','when cutout program running time lug not strength and vibrate the part. Dig mark found on part rib. Part was rejected','Change the program same process. Build the more stock on lug . Part found ok','Same program will update on the Process Sheet. Check the full production parts all are found ok','CA/PA found satisfactory.','','2015-03-30','Ramesh(Poojary)','Umesh B,Karthineyan V.S.,Gurukiran S M,','','0000-00-00','sathish k.c','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','FI','no','MakinoF3','Narasimha Murthy(R)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8394,'35-284','Saab AB','REINFORCEMENT','431589B2','423Z1984-2-01','','--A',9,'PA 1510 NEW PARTS-2','','41202','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','After treatment polishing marks observed on the surface.','Rough embry paper was used to remove the mismatches on the part surface. ','1)Informed to Fitters after completion of rough embry polishing once agian polish the surface to\r\nimprove the surface finish by using smooth grade embry paper. 2)Informed and discuss with\r\nprogramers and supervisors to avoid the mismatches and steps in machine while doing the production. ','1)Informed to Fitters after completion of rough embry polishing once agian polish the surface to\r\nimprove the surface finish by using smooth grade embry paper. 2)Informed and discuss with\r\nprogramers and supervisors to avoid the mismatches and steps in machine while doing the production. ','CA/PA found satisfactory. ','','2015-03-30','Avinash(R.J.)','Manjunath(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','17341','POST DN','yes','Misc','Manjunath(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8395,'35-285','Saab AB','REINFORCEMENT','582084','423Z1985-1','','--A',1,'PA 1510 NEW PARTS-2','','41006','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','After treatment polishing marks observed on the surface.','Rough embry paper was used to remove the mismatches on the part surface. ','1)Informed to Fitters after completion of rough embry polishing once agian polish the surface to\r\nimprove the surface finish by using smooth grade embry paper. 2)Informed and discuss with\r\nprogramers and supervisors to avoid the mismatches and steps in machine while doing the production. ','1)Informed to Fitters after completion of rough embry polishing once agian polish the surface to\r\nimprove the surface finish by using smooth grade embry paper. 2)Informed and discuss with\r\nprogramers and supervisors to avoid the mismatches and steps in machine while doing the production. ','CA/PA found satisfactory.','','2015-03-30','Avinash(R.J.)','Manjunath(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','17217','POST DN','yes','Misc','Manjunath(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8396,'35-283','Saab AB','REINFORCEMENT','431589B2','423Z1983-2-01','','--A',1,'PA 1510 NEW PARTS-2','','41199','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','After treatment polishing marks observed on the surface.','Rough embry paper was used to remove the mismatches on the part surface. ','1)Informed to Fitters after completion of rough embry polishing once agian polish the surface to\r\nimprove the surface finish by using smooth grade embry paper. 2)Informed and discuss with\r\nprogramers and supervisors to avoid the mismatches and steps in machine while doing the production. ','1)Informed to Fitters after completion of rough embry polishing once agian polish the surface to\r\nimprove the surface finish by using smooth grade embry paper. 2)Informed and discuss with\r\nprogramers and supervisors to avoid the mismatches and steps in machine while doing the production. ','CA/PA found satisfactory. ','','2015-03-30','Avinash(R.J.)','Manjunath(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','17376','POST DN','yes','Misc','Manjunath(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8397,'35-283','Saab AB','REINFORCEMENT','563339A1','423Z1983-2-01','','--A',1,'PA 1510 NEW PARTS-2','','41196','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','After treatment polishing marks observed on the surface.','Rough embry paper was used to remove the mismatches on the part surface.','1)Informed to Fitters after completion of rough embry polishing once agian polish the surface to improve the surface finish by using smooth grade embry paper.\r\n2)Informed and discuss with programers and supervisors to avoid the mismatches and steps in machine while doing the production. ','1)Informed to Fitters after completion of rough embry polishing once agian polish the surface to improve the surface finish by using smooth grade embry paper.\r\n2)Informed and discuss with programers and supervisors to avoid the mismatches and steps in machine while doing the production.','CA/PA found satisfactory.','','2015-03-30','Avinash(R.J.)','Manjunath(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','17380','POST DN','yes','Misc','Manjunath(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8398,'18-090A','Magellan Aerospace Bournemouth','BUSH','K10011','D278 50164 200','S80 FHT','A',1,'RP400843','','42326','','0000-00-00',NULL,'yes','yes','yes','','','','','','','part wrong  loaded, so OD dig mark.','In finishing operation 2ODs are finished in one setup first side OD finished and that part to be reversed.but loaded new part so od dig mark and part came out from the jaws.','For next part jaws bored neatly and inserts are changed and taking x&z offset and run the part after finishing first set up OD,reverse that part and 2nd od finished part found okay and continue the production.','Instructed to all operators to cross check the part whether the operation is completed or not before loading another part.','CAPA found okay','','2015-03-30','','                Manjunath  M','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8399,'18-090A','Magellan Aerospace Bournemouth','BUSH','K10011','D278 50164 200','S80 FHT','A',1,'RP400843','','42328','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','outer diameter dig mark.','More stock in the finishing part so Part running time part will be rotated so dig mark observed in the  outer diameter so part will be rejected.','same stock given to the all finished parts  setting the Proper pressure and skin cut given to the jaws and change the insert corner and 0.4 plus taken to the wear offset and run the part and then check the part and proper currection given in wear offset and run the part then part inspection done part checked found ok.                ','after the roughing setup for finishing only 0.3 stock maintain in the all the parts and set the proper and same pressure for all times  ','CAPA found satisfactory.','','2015-03-30','Dinakar(K)','Vasu(SN)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','03','no','Misc','Sandhesh D(S)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8400,'18-056B','Magellan Aerospace Bournemouth','Top Skin Stiffener ','447026A6','L575 53249 200','','A00',1,'RP400837','','40684','','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','','2015-03-30','Avinash(R.J.)','Nandishkumar(D.K.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','17001','POST DN','yes','Misc','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8401,'18-121A','Magellan Aerospace Bournemouth','BARREL - STRUT','247348','D572 50463 201','S98 FHT','F',1,'RP400839','','42486','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Running Time Power Trip So Part OD is Dig mark...  ','Running time power tripped that time o.d was digmark.  \r\n','We are inform to the maintenence for the proper UPS connection.  \r\n','We are inform to the maintenence for the proper UPS connection.  \r\n','UPS repaired and found okay','','2015-03-31','','        Shivappa M B','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8402,'18-415B','Magellan Aerospace Bournemouth','ACTUATOR HOUSING','95744A','D278 50163 201','','D',1,'RP401022_Amend No 1','','40873','','0000-00-00',NULL,'yes','no','no','no','yes','yes','no','no','no','Dia 6.00 Hole diameter inside dig mark.','Dia 6.0 hole find out in Final inspection. 50 nos production done in a batch and identified\r\n01no. deviation and reason was not found. using dia 5.9 drill & dia 6.03 hole mill in hole finish. Therefore reasons for reject is not found, and same will analyzed in next\r\nbatch production.\r\n','Process checked and tried to analyzed the problem, but only manual error will cause of hole debarring time. Therefore reasons for reject is not found, and same will analyzed in next batch production.\r\n','Preventive action check process & tooling good condition. \r\nNext batch produced 216nos production found ok.\r\n','CAPA found satisfactory.','','2015-03-31','Rangaswamy()','Shivanand D.B.,SHIVAKUMAR ,Raghavendra Rao R,Prashanth Kumar M,Mahesh N,Gurukiran S M,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','0','FI','no','MakinoF5','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8403,'34-037B','Magellan Aerospace Winnipeg','HINGE R/H','250044','400-12901-2-905','','EM104302 Iss A, EM105092 Iss F, EM104765 Iss G, EM106399 Iss B, EM106400 Iss B, EM106401 Iss A, EM106404 Iss A, EM106522 Iss A, EM106602 Iss A',1,'B91379 Rev.026','','42118','','0000-00-00',NULL,'yes','no','yes','','yes','','','','','Part dig mark observed on radius.\r\n','While running batch production, when tool changes from magazine to machine spindle, Tool holder not seated at correct orientation.\r\nand Machine alarm not coming and program running with the error.\r\nThis causes tool offset variation in Z and dig mark observed on part.\r\n','Immediately  inform the machine supplier,and all parameters checked and production starts with monitoring of tool change with MOO optional stop.\r\n\r\n ','Machine supplier is checking the Root cause and problem is not sorted.\r\nProduction running with monitoring of tool change from ATC with optional stop.','Machine maintenance done and next parts found okay','','2015-03-31','Lohith(K)','        Hari Prasad','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8404,'18-259C','Magellan Aerospace Bournemouth','BUTTSTRAP UPP RS4X9356','436556','L575 53341 200','','B00',1,'RP401009','','42411','','0000-00-00',NULL,'','','yes','','','','','','','18-259c 1nos base thinkness (-0.4)side  so part rejected. ','Due to butting face not cleaned properly .So part thickness under size. ','Before load the part of the butting face cleaned by air per sure then load the part ','Before load the part of the butting face cleaned by air per sure then load the part ','CA/PA Found ok.','','2015-04-01','Anjinamurthy(H)','        Manjunatha N.R.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8405,'18-209B','Magellan Aerospace(Chalfont) Limited','BODY','4842','D321 40204 202','','D, ECN NR29999ST1KM15, NR29999ST2KF65, WQN DFB09775',1,'P/074113','','41822','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','centerlity  mesureing 0.36mm.','Proper root cause has not been identified yet might be chips clogged while machining.','Checking gauge will be manufactured to check the centrality & air will blow to avoid chips clogging.','Checking gauge will be manufactured to check the centrality & air will blow to avoid chips clogging.','Manufacture checking gauge and ensure it and then NC will be closed','','2015-04-01','Anjinamurthy(H)','Shivappa M B,Ravi R,Rajesh T,Mohan Kumar C.M.,Manohara M,Dinakar K,Devaraj K.C.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','BMV 45-2','Narasimha Murthy(R)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8406,'30-011A','Gardner Aerospace-Derby Limited','SPAR FWD - LH','9599701','L575 51827 200','ABM3-1029 T7651','A00, ECN:PG60049U01LC52',1,'LPR0000687','','42162','','0000-00-00',NULL,'yes','no','yes','no','yes','no','no','no','no','3mm cross cutting ','While cutting the material as per layout, due to Machine blade was slack & wobbling so cross cut the material.\r\n\r\n','Cutting process stopped and blade supplier was visited and verified the machine belt speed and blade & adjust  the belt speed & change the blade.\r\n\r\n','Frequent checked to be done for blade wobbling & blade speed for  prior to cutting.\r\n','CAPA found okay','','2015-04-02','Sunil Kumar(K.R.)','Devaraja (M S)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','01','no','Misc','Narayanappa(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8407,'34-037B','Magellan Aerospace Winnipeg','HINGE R/H','250044','400-12901-2-905','','EM104302 Iss A, EM105092 Iss F, EM104765 Iss G, EM106399 Iss B, EM106400 Iss B, EM106401 Iss A, EM106404 Iss A, EM106522 Iss A, EM106602 Iss A',1,'B91379 Rev.026','','42118','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Rib thickness minus side.(Actual dim 2.5mm +/-0.25 Measured 2.1 mm).  ','Due to operator negligence this error happened.\r\nOperator not clamped the bolt in fixture.\r\n\r\n ','Inform to operator, every part loading time before run the programs check the all bolts.\r\nAfter roughing program completed, re-check the bolts.\r\n\r\n','Inform to operator, every part loading time before run the programs check the all bolts.\r\nAfter roughing program completed, re-tight the bolts.\r\nAlready give the M00 and messages in program last 4 production batches.    \r\n','CAPA found okay.','','2015-04-06','Lohith(K)','        Theerthappa K.N.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8408,'18-295A','Magellan Aerospace Bournemouth','BOLT','A0671X','D577 56145 200','S80','A',1,'RP400846','','42340','','0000-00-00',NULL,'','','yes','','','','','','','2.8 DRILL PART RUNNING TIME DRIIL BREKEN HOLE + SIDE SO PART REJ ','This problem is due to not monitor Carbide drill tool life and operator not checking tool condition so running time tool broken, part rejected.								\r\n','Arrange our tool manager another new special drill run production but not set tool life, because that batch qty only 110nos,after drill condition very good. more components run then set drill life. ','More components run then set drill life. ensure drill life or number of parts. 							\r\n								\r\n','CAPA found okay','','2015-04-06','','        Girish HP','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8409,'18-412A','Magellan Aerospace(Chalfont) Limited','ROD END','245160','D321 53012 200','','F01',1,'LTA _For Treatments','','40624','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Thread Length over size.','In first operation total length is maintained to 70mm and center is provided for supporting purpose and that is cleared in final set up.in 2nd set up 66.65mm length is maintained and 3.35mm step is maintained for next set up for supporting purpose.in threadding operation turning tool z-offset is taken to face of the part and threadding tool offset is taken to 3.35mm step and when 3.35mm is given in work offset to maintain 66.65 total length.when 3.35mm is moved in work offset  thread length also 3.35mm is move so thread length oversize part reject.','For next part turning tool and threadding tool z-offset is taken to face of the part and 3.35 mm is moved in work offset and run the part ,part found okay and continue the production.','Instruction given to operator and cross check tool offset wheather the offset is taken correctly or not as shown in the operation sketch(x0&z0).','CAPA found satisfactory. next parts found okay','','2015-04-06','Dinakar(K)','Theerthappa K.N.,Shivaraj K S,Shivappa M B,Ravi R,Rajesh T,Ningaraj A N,Nataraja C V,Mohan Kumar C.M.,Manohara M,Manjunatha N,Manjunath  M,Hari Prasad,Devaraj K.C.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','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),(8410,'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','','39458','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','1)Thickness under size by 0.20MM.','Actually the part consists of 2 holes which has chamfer of 0.3 which was maximum at that stage.Due\r\nto that the part was grinded to make the chamfer proper and thickness got undersized.','Thickness and Chamfer dia will regularly watched. Because the chamfer at one end will be done\r\nmanually. Chamfer will be maintained by regular checking.','Thickness and Chamfer dia will regularly watched. Because the chamfer at one end will be done\r\nmanually. Chamfer will be maintained by regular checking.','CAPA found okay.','','2015-04-06','Nagaraju(T)','Pinto(N.L.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','0','fitting','no','Misc','Nagaraju(T)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8411,'18-121A','Magellan Aerospace Bournemouth','BARREL - STRUT','247348','D572 50463 201','S98 FHT','F',1,'RP400839','','42486','','0000-00-00',NULL,'','','yes','','','','','','','running time dia 4.9 drill breakan so no go pin answer','This problem is due to not monitor Carbide drill tool life and operator not checking tool condition so running time tool broken, part rejected.    							\r\n','change another drill run the production. instruct to operator check the drill condition  before cycle start.   ','This problem is due to not monitor Carbide drill tool life .discuses to our tool manger & suppler please arrange special drill & ensure the tool life or number of parts. ','CAPA found okay','','2015-04-07','','                Ravi R','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8412,'30-008','Gardner Aerospace Burnley Limited','SPAR MID OFW - RH ','6518801 3','L575 51780 201','ABM3-1029 T7651','B00,PG60049N01LB38',2,'LTA','','42715','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','2mm negative wall broken in 2nos','dia 25R3dove tail cutter enter changing time caret offset  not taken by operator, ','1)strictly warn the operator \r\n2)Instructed to operator to ensure the tool wear offset entries, & cross checking tool wear offset regularly,  before run the program,\r\n3)Dedicated all tools numbers in Haas control.  ','1)strictly warn the operator \r\n2)Instructed to operator to ensure the tool wear offset entries, & cross checking tool wear offset regularly,  before run the program,\r\n3)Dedicated all tools numbers in Haas control.','CAPA found okay.(Warning letter issued from QAD)','','2015-04-07','Narayanappa(G)','Narayanappa(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','03','no','Misc','Narayanappa(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8413,'35-182A','Saab AB','EDGE HOUSING','581309','423Z1121-5-02','','--A',1,'1600097307','','39032','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Dent mark observed on face.','Before sending the parts to Treatment house parts was checked 100%and found okay but after treatment\r\nparts found damaged','Informed to Treatment supplier to handle the parts carefully and keep the parts separately without\r\nhaving metal to metal contact','Informed to Treatment supplier to handle the parts carefully and keep the parts separately without\r\nhaving metal to metal contact','CAPA found okay','','2015-04-08','Avinash(R.J.)','Manjunath(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','17564','Post DN','no','Misc','Manjunath(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8414,'35-241','Saab AB','HANDLE','424872','425Z0634-2','','--C',3,'PA 1510 NEW PARTS-1','','41829','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dig mark on profile.','Under investigation','Under investigation','Under investigation','Under investigation','','2015-04-08','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Krishna(Chowdary.G.P.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8415,'35-274','Saab AB','PIN','G21411K03','426Z2601-1','','--A',1,'April 2014','','42619','','0000-00-00',NULL,'yes','yes','yes','','','','','','','running time power cut so od dig mark..','Running time power tripped that time o.d was digmark.  \r\n','We are inform to the maintenence for the proper UPS connection. \r\n','We are inform to the maintenence for the proper UPS connection. \r\n','CA/PA found satisfactory.','','2015-04-08','Dinakar(K)','        Nataraja C V','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8416,'18-090A','Magellan Aerospace Bournemouth','BUSH','K10011','D278 50164 200','S80 FHT','A',1,'RP400843','','42326','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','total length undersize ','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 2.8mm 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\r\njaws not in the starting face. ','CAPA found satisfactory. next parts found okay','','2015-04-08','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','01','no','Misc','Dinakar(K)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8417,'34-031A','Magellan Aerospace Winnipeg','PIN SHEAR ACCESS DOOR','L1N1','400-12748-1-905','','EM105092 Iss F, EM104302 Iss A, EM104765 Iss G, EM106399 Iss B, EM106400 Iss B, EM106401 Iss A, EM106404 Iss A, EM106522 Iss A, EM106602 Iss A',1,'B91379 Rev.026','','42116','','0000-00-00',NULL,'yes','','yes','','yes','','','','','C-AXIS problemC-axis problem,so profile shift.  \r\n','C-axis position not locked in properly','Inform to the maintenence and haas maintenence team. ','Inform to the maintenence and haas maintenence team. ','Machine Maintenance done and next parts found okay','','2015-04-08','','        SHIVAKUMAR ','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8418,'35-241','Saab AB','HANDLE','424872','425Z0634-2','','--C',2,'PA 1510 NEW PARTS-1','','41829','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dia 4.06mm Hole pitch oversize.','While doing Rework of parts in jig boring machine this deviation coming.\r\nMis interpretation of process sketch, part loaded wrongly and causes hole pitch oversize.','After finding the deviation, Process sketch verified in CAD and 3D print taken from CAD to understand the process sketch and continued production.','New fixture and process planned to machine the dia 4.06 hole in operation-01 to avoid such mistakes.\r\nInternal delta FAI to be carried for next batch.','Complete the jig and delta FAI then NC will be closed after proving process','','2015-04-09','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Krishna(Chowdary.G.P.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8419,'35-073','Saab AB','9900976-384','N38HA1B','L579 50519 200','TA11','A',1,'1600099837','','41638','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dig mark on part.','','','','Under investigation','','2015-04-09','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','04','no','Misc','Krishna(Chowdary.G.P.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8420,'07-012','HAL-NASIK','HATCH  COVER - LH','BS-24239','11.2000.2.156.002','V95pCHAT 1V-10','NIL',1,'NK/M/2513(4520)/MP/O','','41499','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1)Thickness under size by 0.70mm.','Raw material was bend noticed by operator & informed to store ,bend removed for outside, then we loading the part program running time lifted so part base thickness under size. ','1) apply in the more clamps & dialing the part top face within tolerance. \r\n2) ofter completed the roughing program checking the base thickness & maintain the within tolerance. \r\n','1) informed to store issued the raw material without bend\r\n2) changing the new clamping process','CAPA found okay.','','2015-04-09','Narayanappa(G)','Sathish Y.R.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','0','FI','no','DMG 360L','Sudhagar(V)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8421,'18-562A','Magellan Aerospace Wrexham','SPAR OUTBOARD OFW','5865801 6-10','L575 51781 200','','A',1,'RM132919 Amnd 1','','42699','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','Wall thickness measures minus side.','Under Investigation \r\n','Under Investigation \r\n','Under Investigation \r\n','Under Investigation \r\n','','2015-04-09','Ramesh(Poojary)','Ramesh(Poojary)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Krishna(Chowdary.G.P.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8422,'18-001A','Magellan Aerospace Wrexham','BRACKET SUPPORT-LH','0778801','D361 50110 200','ABM3 1029 T7651','A',2,'RP125887','','42371','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dig mark observed on hole. ','While part 05 operation running time new operator not located the part. So part running time part was rotated. ','Instructed to new operator when load the part check and inform the senior operator.   ','Informed to operator and supervisor to check the tool and work offset once and after ensuring both run the programs. Supervisor to monitor and train the operator to avoid manual errors.','CAPA found okay','','2015-04-10','Lohith(K)','Lohith(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','05','no','Misc','Lohith(K)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8423,'18-317A','Magellan Aerospace(Chalfont) Limited','PIN SIDE ROLLER','A0587U','F579 53066 200','S145','C',32,'P/074118','','37595','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Face groove problem.','Face grooving tool problem after running for several number of parts ','Grooving Tool has kept in stock, Operator should watch the tool in regular intervals and should change if any deviation is found ','Grooving Tool has kept in stock, Operator should watch the tool in regular intervals and should change if any deviation is found ','CAPA found okay','','2015-04-10','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','1','no','Misc','Dinakar(K)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8424,'34-018B','Magellan Aerospace Winnipeg','BRACKET STRUT  LH ','A1384U','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',10,'B91379 Rev.026','','39614','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','yes','1)schedule PO number was wrongly called on tag.','1)miss interpretation of selecting schedule PO while preparing tag.\r\n2)Typing Error. \r\n','1)  Printed tag will be stamped by quality before  handing over to shipping dept.\r\n2) Quality alerts will be issued.\r\n3)  Instruction given to shipping to attach the tag received with inspector stamp only.\r\n\r\n','1)Above action will be extended to all parts.\r\n','Next batch should be monitored.','C35254','2015-04-10','Avinash(R.J.)','Sudhagar(V)','DDR 16307','2015-04-10','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','Manufacture Only','0','Customer end','no','Misc','Sudhagar(V)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8425,'35-165A','Saab AB','HOUSING PIN','427287','423Z1124-5-01','','--A',1,'1600078597','','41148','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Tool dig mark in bore top face.','There was stock in the Bore by manually it was tried to clear the stock and found dig mark in bore top face\r\n','stock in the bore have been reduced and made it easy to finish the stock in the bore easily\r\n','stock in the bore have been reduced and made it easy to finish the stock in the bore easily\r\n','CAPA found okay','','2015-04-13','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','05','no','Misc','Rangaswamy()','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8426,'18-101A','Magellan Aerospace Bournemouth','TUBE-STRUT','251469','D572 50464 202','T45','F',1,'RP400839','','42873','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Total length undersize by 0.5mm(211mm measured 210.45mm measured).','For 1st part x&z offset for turning and boring tool is taken and run the part. after operation part is removed from the jaws because to check the total length and the same loaded for completing boring operation but the program is run from starting i.e.from facing and the boring.In 2nd operation 1mm stock is maintained for next operation(212mm).in third operation part is butted to stopper in stopper program 1mm stock is given for facing purpose,that 1mm stock is cleared in facing operation when same part is running two times total length is undersized. ','for next part x and z offset taken for turning and boring tool and run the part and both facing and boring operation is completed,then removed that part and check that part.part found okay and then continue the production.','Instruction given to operator to run all the operations before unloading the part and check the part.if any deviation found adjust in stopper program and run all the operation.','CAPA found okay.','','2015-04-13','','        Shivanand D.B.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8427,'35-230A','Saab AB','HINGE BRACKET 3 ','7600601','D576 50006 205','','D00',23,'1600101900','','40963','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','NDT Failed.','Due to rubbing of tool or material behaviour NDT failure has been found in Treatment house ','Instructed to Production & fitting department to avoid rubbing of tool and polishing ','Avoid polishing and try to finish the part in machining stage itself. ','CA/PA found satisfactory.','','2015-04-14','Avinash(R.J.)','Manjunath(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','16622','Post Dn','yes','Misc','Manjunath(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8428,'35-230A','Saab AB','HINGE BRACKET 3 ','7600601','D576 50006 205','','D00',4,'1600101900','','40962','','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.','','2015-04-14','Avinash(R.J.)','Manjunath(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','16621','Post Dn','yes','Misc','Manjunath(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8429,'35-226A','Saab AB','HINGE BRACKET 1','688803A6','D576 50004 207','','D00',5,'1600099854','','40909','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','NDT Failed.','Due to rubbing of tool or material behaviour NDT failure has been found in Treatment house ','Instructed to Production & fitting department to avoid rubbing of tool and polishing ','Avoid polishing and try to finish the part in machining stage itself. ','CA/PA found satisfactory.','','2015-04-14','Avinash(R.J.)','Manjunath(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','16620','Post Dn','yes','Misc','Manjunath(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8430,'35-226A','Saab AB','HINGE BRACKET 1','688803A6','D576 50004 207','','D00',9,'1600099854','','40908','','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.','','2015-04-14','Avinash(R.J.)','Manjunath(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','16619','Post Dn','yes','Misc','Manjunath(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8431,'35-228A','Saab AB','HINGE BRACKET 2 ','7600601','D576 50005 205','','D00',1,'PA 1217 2014-2015','','39607','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','NDT Failed.','Due to rubbing of tool or material behaviour NDT failure has been found in Treatment house ','Instructed to Production & fitting department to avoid rubbing of tool and polishing ','Avoid polishing and try to finish the part in machining stage itself. ','CA/PA found satisfactory.','','2015-04-14','Avinash(R.J.)','Manjunath(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','15787','Post Dn','yes','Misc','Manjunath(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8432,'35-234A','Saab AB','HINGE BRACKET 5 ','425129','D576 50008 209','','D00',1,'1600093863 Rev-2','','38763','','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.','','2015-04-14','Avinash(R.J.)','Manjunath(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','15579','Post Dn','yes','Misc','Manjunath(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8433,'35-178','Saab AB','SUPPORT-SEAL-RETAINER','653650A2','423Z1833-3-02','','---',1,'1600093935','','38596','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','NDT Failed','Small dent mark was observbed on the part surface.','Instructed to inspectors and fitters to remove and check the dent marks if it is very small dent also.','1)Instructed to operatorts and fitters to handling the part very carefully to avoid the dent marks.\r\n2)Instructed to inspectors and fitters to remove and check the dent marks if it is very small dent also.','CA/PA found satisfacory.','','2015-04-14','Avinash(R.J.)','Manjunath(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','15637','Post Dn','yes','Misc','Manjunath(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8434,'18-561A','Magellan Aerospace Wrexham','SPAR INBOARD OFW','437515A0','L575 51779 201','','B00',1,'RM132919 Amnd 1','','42607','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','* Dia 5.60+0.1 hole abblong.','While drill operation fixture was not produced bigger dia hole in fixture.\r\n','introduced bigger dia hole in fixture .\r\n','Introduce bigger dia hole before start first part in fixture .\r\n','CAPA found okay','','2015-04-14','D.K.Pavan (Kumar)','Girish(Prasad P)','','0000-00-00','* Dia 5.60+0.1 hole abblong.','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Girish(Prasad P)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8435,'18-619A','Magellan Aerospace Wrexham','BRACKET APPU MTG','6679701-1','L575 55376 200','','A00',1,'RM132920 Amnd 1','','42420','','0000-00-00',NULL,'no','no','no','yes','yes','yes','no','no','no','FAIR Part machine Abuse rejected at API.','Due to rubbing of tool Machine abuse has been found in Treatment house\r\n','Instructed to Production department to avoid rubbing of tool and polishing \r\n','Avoid polishing and try to finish the part  in machining stage itself.\r\n','Next parts and batches found okay\r\n','','2015-04-15','Avinash(R.J.)','Muniyappa(N)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','','POSTDN','yes','Misc','Muniyappa(N)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8436,'18-620A','Magellan Aerospace Wrexham','BRACKET APPU MTG','6679701-1','L575 55376 201','','A00',1,'RM132920 Amnd 1','','42419','','0000-00-00',NULL,'no','no','no','yes','yes','yes','no','no','no','FAIR Part machine Abuse rejected at API.','Due to rubbing of tool Machine abuse 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','','2015-04-15','Avinash(R.J.)','Muniyappa(N)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','','POSTDN','yes','Misc','Muniyappa(N)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8437,'35A-239','Saab AB','L/H KIT FOR ARD HINGE / J','','9901503-993','','Exhibit-B',48,'1600082519','','K03425','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','yes','There are bare patches in the chrome on flange bushing in Jack 1 and Jack 2 that are part of the kit 9901503-993 and 9901503-994. Where the chrome is missing you can see the cadmium plating(white area). There have been so far (2015-04-10) five (5) cases of bare patches in the chrome when removing masking after painting at Saab. \r\n\r\nAt receiving inspection, Saab have noted bare patches on the bushing and it´s also schratches on the surface and edges of the bushing. Very common is a circle close to the hole of the bushing as per picture Before start of assembly. \r\n','1) All bushes are 100% inspected and no failures were recorded, either by physical testing or visually.\r\n2) Unassembled bushes show no sign of patchy passivation.\r\n3) Post treatments handling or further process could have a detrimental effect on the passivate, namely the tape used to mask the bush head prior to top coat paint application ot certain types of coolant/compound used during boring/lapping hence the concentartion around the main bore','1) Immediatly inspected the parts those were in stock and found no such defects.\r\n2) Immediatly informed to supplier and raised the formal non conformance.\r\n3) Affected parts can be lightly abaded and application of passivate solution can be applied to reinstate the colour.','1) Additional tape test sample per batch will be carried out to assertain a secure passivate coating.','Next batch found satisfactory.','C31336','2015-04-15','Avinash(R.J.)','Manjunath(G)','C31336 and E-Mail','2015-04-10','Reference to CIM CoC of affected parts:\r\nC27781\r\nC27784\r\nC34534\r\nC35853\r\nC35854\r\n','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Assembly','','FI','no','Misc','Avinash(R.J.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8438,'35-284','Saab AB','REINFORCEMENT','431589B2','423Z1984-2-01','','--A',9,'PA 1510 NEW PARTS-2','','41202','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','After treatment polishing marks observed on the surface.','Rough embry paper was used to remove the mismatches on the part surface. ','1)Informed to Fitters after completion of rough embry polishing once agian polish the surface to\r\nimprove the surface finish by using smooth grade embry paper. 2)Informed and discuss with\r\nprogramers and supervisors to avoid the mismatches and steps in machine while doing the production. ','1)Informed to Fitters after completion of rough embry polishing once agian polish the surface to\r\nimprove the surface finish by using smooth grade embry paper. 2)Informed and discuss with\r\nprogramers and supervisors to avoid the mismatches and steps in machine while doing the production. ','CA/PA found satisfactory. ','','2015-04-15','Avinash(R.J.)','Manjunath(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','17341','POST DN','yes','Misc','Manjunath(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8439,'35-284','Saab AB','REINFORCEMENT','431589B2','423Z1984-2-01','','--A',9,'PA 1510 NEW PARTS-2','','41202','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','After treatment polishing marks observed on the surface.','Rough embry paper was used to remove the mismatches on the part surface. ','1)Informed to Fitters after completion of rough embry polishing once agian polish the surface to\r\nimprove the surface finish by using smooth grade embry paper. 2)Informed and discuss with\r\nprogramers and supervisors to avoid the mismatches and steps in machine while doing the production. ','1)Informed to Fitters after completion of rough embry polishing once agian polish the surface to\r\nimprove the surface finish by using smooth grade embry paper. 2)Informed and discuss with\r\nprogramers and supervisors to avoid the mismatches and steps in machine while doing the production. ','CA/PA found satisfactory. ','','2015-04-15','Avinash(R.J.)','Manjunath(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','17341','POST DN','yes','Misc','Manjunath(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8440,'','','','','','','',0,'','','','','0000-00-00',NULL,'','','','','','','','','','','','','','','','2015-04-15','','','','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),(8441,'18-107B','Magellan Aerospace Bournemouth','LINK BODY','0163','D574 50553 200','','A',1,'RP400839','','42319','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','OD Bulged.','For final operation jaws all milled sharp and that jaws are bored after boring jaws all put one teeth outside becouse to enter that 6.3mm dia in to the jaws by doing this jaws play will came and part easily enter in to the jaws after boring part clamped in the jaws using stoper part is first clamped in the jaws and then call the stoper and butt the part to that stoper and clamp the jaws.\r\nwhen clamping time part kept cross and only 2 jaws are holding that time od dig mark will occur. ','For next part first clamp the part face to jaws face and call the stoper and but the part to the stoper by just declamp and clamp then run the part. part found ok then continue the produation .','instruction given to the operator to first clamp the part to the jaws and butting the part to the stoper by just declamp and clamp. ','CAPA found okay.','','2015-04-15','Dinakar(K)','Shivappa M B,Seetharamu D,Ravi R,Rajesh T,Nataraja C V,Mohan Kumar C.M.,Manohara M,Manjunatha N,Manjunath  M,Dinakar K,Devaraj K.C.,Ashith B,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','DX 200-1','Narasimha Murthy(R)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8442,'18-107B','Magellan Aerospace Bournemouth','LINK BODY','0163','D574 50553 200','','A',1,'RP400839','','42317','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','OD Dig Mark.','For final operation jaws all milled sharp and that jaws are bored after boring jaws all put one teeth outside becouse to enter that 6.3mm dia in to the jaws by doing this jaws play will came and part easily enter in to the jaws after boring part clamped in the jaws using stoper part is first clamped in the jaws and then call the stoper and butt the part to that stoper and clamp the jaws. when clamping time part kept cross and only 2 jaws are holding that time od dig mark will occur.    ','For next part first clamp the part face to jaws face and call the stoper and but the part to the stoper by just declamp and clamp then run the part. part found ok then continue the produation   ','instruction given to the operator to first clamp the part to the jaws and butting the part to the stoper by just declamp and clamp','CAPA found okay','','2015-04-15','Dinakar(K)','Shivappa M B,Seetharamu D,Ravi R,Rajesh T,Rajesh B D,Mohan Kumar C.M.,Manohara M,KRISHNAMURTHY N,GUNDEGOWDA H.G.,Dinakar K,Devaraj K.C.,Ashith B,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','DX 200-1','Narasimha Murthy(R)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8443,'18-104A','Magellan Aerospace Bournemouth','BODY TURNBUCKLE','239338','D575 40490 200','S80 FHT','E',2,'RP400840','','41717','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','LH ID Thread nogo answard.','After 25nos running threading insert will be wear out.for next part threading insert will be changed and 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 answer.','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 down 0.05mm 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. ','CAPA found okay','','2015-04-16','Diwakar(S)','Seetharamu D,Ravi R,Mohan Kumar C.M.,Dinakar K,Ashith B,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','FI','no','DX 200-2 ','Narasimha Murthy(R)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8444,'18-309B','Magellan Aerospace(Chalfont) Limited','SPIGOT','Y12196','F 575 51290 200','S80','B, ECN PG49999SMAKH49',2,'P/074122','','40922','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','OD Under size 0.008 to 0.013mm.','after running 5ns TNMG tool sim was brocken so insert will not seated properly so running time insert tip will be brocken and insert was rubbing the part and vibation started in the insert that time it will removing the extra material in outer diameter so outer diameter will be undersized.','Change the brocken sim,insert and screw and newely offset taken and 0.2 (+) plus taken in the tool wear offset and run the part and then check the outer diameter and give the correction in wear offset and run the part and checked found ok. ','Before every part setting ,check the all tool sim, screws, pins and locks before tightening the tools to machine.then observe the noise every time while machining. ','CA/PA found okay','','2015-04-16','Dinakar(K)','Rakesh  KC,Lohith K,KRISHNAMURTHY N,GUNDEGOWDA H.G.,Dhananjaya N,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','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),(8445,'18-189A','Magellan Aerospace Bournemouth','BUSH HINGE BRKT FWD','L07584','L575 52328 200','BS 23','A00',6,'RP401024','','39813','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','no','Depth undersize,Dimension 9.9/9.7 measures 9.63 to 9.65 in 08 nos out of 18 nos. ','under review','under review','under review','under review','','2015-04-16','Nandishkumar(D.K.)','SHIVAKUMAR ,','113','2015-04-13','WO NO:39815 & 39816 QTY-2NOS.','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Manufacture Only','0','FI','yes','ST20','Muniyappa(N)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8446,'28-003A','Magellan Aerospace New York  Inc.','PIN-ATTACHMENT WALKING BE','970608-03','161A7305-1','','PL-Rev-NC, DL Rev-B',1,'126999_R0_C1','','42065','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Thread NOGO answer.','Due to while thread running time thread insert brokened and broken insert is taking over cut and therad major dia will be undersize so thread NOGO answered.','Next part thread insert changed and takened tool X-offset&Z-offset and maintained the thraed effective dia and soot the thread gauge,Gauge is answered and run the part. ','Inform to operator every 50 nos will be completed changed the insert and takened tool X-offset&Z-offset and maintained the thraed effective dia and soot the thread gauge,Gauge is answered and run the part. ','CA/PA found okay','','2015-04-16','Dinakar(K)','Seetharamu D,S. Shiva Kumar,Rajesh B D,Manjunatha N.R.,KRISHNAMURTHY N,GUNDEGOWDA H.G.,Girish HP,Diwakar R.B.,Dinakar K,Ashith B,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','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),(8447,'42-002','RAFAEL','PSA BASE','K10597','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',6,'347592024','','39403','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1) Hole position out of tolerance ','Due to wrong interpreation in the drawing.','Tolerance changed/increased after that re-checked then found ok.','Tolerance changed/increased after that re-checked then found ok.','Next batch found ok','','2015-04-16','Avinash(R.J.)','Siddaramappa ,Rangaswamy ,Paramesh K,Narayanappa G,Gajendra Singh C.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','With Treatment','0','FI','no','VMC 70L','Sudhagar(V)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8448,'42-002','RAFAEL','PSA BASE','K10596','BA1E2001B','','38-576104_Rev-E, TILDOCS#172373_Rev-13, RE_804-1-5_Rev-11, 111.21_Rev-6, 23.36.59_Rev-F, ECN 57176 2014/08 /25; ECN 58483  2014/07/29',3,'347592024','','39951','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1) Hole position out of tolerance','Due to wrong interpreation in the drawing.','Tolerance changed/increased after that re-checked then found ok.','Tolerance changed/increased after that re-checked then found ok.','Next batch found ok.','','2015-04-16','Avinash(R.J.)','Siddaramappa ,Rangaswamy ,Paramesh K,Narayanappa G,Gajendra Singh C.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','With Treatment','0','FI','no','VMC 70L','Sudhagar(V)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8449,'35-191','Saab AB','SUPPORT-FTG','581312','423Z1202-13','','---',1,'April 2014','','42617','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Running time air pressure low so bore dig mark.','While bore operation running air pressure low.That time bore dig mark observed.  ','We are inform to the maintenance department for the proper UPS connection every time in air compressor machine. ','We are inform to the maintenance department for the proper UPS connection every time in air compressor machine. ','CA/PA found satisfactory.','','2015-04-17','Lohith(K)','        Punith G S','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8450,'43-010','Composite Industrie','BRACKET','577298','V251 13497 202','','A00, ECN PV100298ST1BK24',1,'ATA25_ACH-2945','','42059','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1)Thickness under size by 0.50MM.','This was the first trail order and during devlopment stage this was happened','Next parts was prooved and found ok.','Next parts was prooved and found ok.','Next set of parts in the trail order found ok.','','2015-04-19','Avinash(R.J.)','Sudhagar(V)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','0','FI','no','Misc','Sudhagar(V)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8451,'18-108A','Magellan Aerospace Bournemouth','FORK END OUT BD','A0860N','D575 41546 200','S80 FHT','B',1,'RP400840','','42568','','0000-00-00',NULL,'','','yes','','','','','','no','hole pitch problem ','Under Investigation','Under Investigation','Under Investigation','Under Investigation','','2015-04-19','','        Manohara M','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8452,'35-191','Saab AB','SUPPORT-FTG','581312','423Z1202-13','','---',1,'April 2014','','42617','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Dig Mark on R5 radius on Pocket.','This deviation due to load taken by Dia 10 ball nose in Base radius. Tool broken and dig mark observed on part.\r\n','In radius stock meterel is more when we checked in CAD,May this deviation coming. Ruffing program 0.6 to 0.3mm reduces and regenerated the program and checked the tool load while Dia 10 ball nose program running. Smoothly program was running now and continued production.							','Cutters condition will check before loading the tools to machine while doing setting and Dedicated tools.							','CAPA found satisfactory. next parts found okay','','2015-04-19','Girish(Prasad P)','        Girish Prasad P','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8453,'18-489A','Magellan Aerospace Wrexham','FITTING MID','6471701','L575 52122 200','','A00',1,'RM132920 Amnd 1','','42940','','0000-00-00',NULL,'','','yes','','','','','','no','Tool length problem so part dig mark.','Operator not holding (105mm) required tool length, tool holder touch part rib top face. so part rejected.','change tool length then run production.','In this part dia 16R3 105 mm holding is overhang the holder ,but no relief in shank 105 mm,so operator chances of holding to minimum,now detected tool & relief 105 mm shank.operator not holding in minimum.','CAPA found okay.','','2015-04-20','','        Mahesh N','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8454,'18-101A','Magellan Aerospace Bournemouth','TUBE-STRUT','251469','D572 50464 202','T45','F',2,'RP400839','','42718','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','4.9 hole over size o.05mm','1)While drilling the hole by drill bit dia 4.9 hole measures oversize by 0.05mm due to runout observed on Drill and missed to check the Runout by operator before start the drlling operation.\r\n2)During continious drilling operations drill bit got worn out of cutting edge after that operator grinded the drill but that was not meet to the required angle.','1)Immediatelly replace the drill bit and before atart the drill checked all the parameters of drill.\r\n2)Instructed to operator to check the drill bit angles after the grinding.\r\n3)Instructed to operator completion of  every 50nos replace the Drill bit.  ','1)Instructed to operator to check the drill bit angles after the grinding.\r\n2)Instructed to operator completion of  every 50nos replace the Drill bit by new drill bit.  ','CAPA found okay.','','2015-04-21','Nagaraju(T)','Bhuvaneshwar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','07','no','Misc','Nagaraju(T)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8455,'18-313A','Magellan Aerospace Wrexham','STUD ','453734','D278 50006 204 01','','D',2,'RP125889_Amnd-01','','42803','','0000-00-00',NULL,'yes','yes','yes','','','','','','','runing time od (-side 0.005 to 0.01 ) ','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 \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','CA/PA found okay','','2015-04-21','','        Devaraj K.C.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8456,'35-191','Saab AB','SUPPORT-FTG','581312','423Z1202-13','','---',1,'April 2014','','42617','','0000-00-00',NULL,'yes','yes','yes','','','','','','','* Dig Mark on R5 radius on Pocket.			','* This deviation due to load taken by Dia 10 ball nose in Base radius. Tool broken and dig mark.			','* In radius stock meterel is more when we checked in CAD,May this deviation coming. Ruffing program 0.6 to 0.3mm reduces and regenerated the program and checked the tool load while Dia 10 ball nose program running. Smoothly program was running now and continued production.			','* Cutters condition will check before loading the tools to machine while doing setting and Dedicated tools.	\r\n','CAPA found okay.','','2015-04-21','Girish(Prasad P)','        Yogesha K','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8457,'18-327A','Magellan Aerospace Bournemouth','ATTACHMENT ANGLE ','432313','L572 53314 201','ABM3 1029','A00',2,'RP400946_Amnd_No.1','','43064','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Base thickness -ve side(-0.1) so part rejected,','operator setting time 18-326a fixture top face dialing tapper.\r\nso part base thickness one end minus, another end with in tolerance.       ','Every setting time operator check straight dialing,top dialing is mandterlly , every fixture setting in rotary setup checking fixture top height. but this CRN not show in process sheet.so possible of height variation.','Next, every setting in rotary setup, height checking rotary center to fixture top face,and show in process sheet.','CAPA found okay.','','2015-04-22','Rangaswamy()','Manohara(B.C.)','','0000-00-00','Base thickness -ve side(-0.1)..','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Gurukiran S(M)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8458,'18-391B','Magellan Aerospace Bournemouth','END COVER','R3856','D278 50166 200','','A',2,'RP401022_Amend No 1','','42984','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dia 6.426 hole diameter over sized.','while running the production, after running the facing turning and outer profile finishing program not running the 6.426 hole profile program and declamp the part before running the hole program, so rework this part in using another finished part in drilling machine that time part will little bit rotated so hole ablonged and hole size will be over sized so part will be rejected. ','After this problem check the every part before declamping the part and run the production.and message given in the program.   ','In program top given the message before unclamp the part check the all the parts.','CAPA found okay.','','2015-04-22','Dinakar(K)','SHIVAKUMAR()','','0000-00-00','Dia 6.426 hole diameter over sized.','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Sandhesh D(S)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8459,'35-192','Saab AB','SUPPORT-FTG','428596B','423Z1202-14','','---',1,'May 2015','','42471','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Dig mark noticed on the part.			','while re-rest program running time dia 16flat tool down so part base dig.','collect scrap and loaded in new collect,offset taken and continued production.					','All the collects & holders condition checked and informed to operators and supervisor to monitor the collects,holders at regular, if found any deviations inform to concern person.','CAPA found okay','','2015-04-22','','        Girish Prasad P','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8460,'35-246','Saab AB','WASHER LARGE','G17953R03','423Z1458-1','','--B',1,'May 2015','','42931','','0000-00-00',NULL,'yes','yes','yes','','','','','','no','Total thickness minus  side.','Due to Z offset taken not properly. Operator negligence this error happened. ','Next part loading time Z offset cross checking after continue the production.\r\nInform to operator every part loading time butting area and tool checking mandatory.  ','Inform to operator next batch production setting time inform the concern supervisor, after continue the production and necessary training gave live in Machines','CAPA found okay','','2015-04-23','Lohith(K)','        Hari Prasad','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8461,'35-017','Saab AB','9901503-075','96746','D576 50011 200','L167','A',1,'1600099854','','42192','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Dent mark observed on face.','Before sending the parts to Treatment house parts was checked 100%and found okay but after treatment\r\nparts found damaged','Informed to Treatment supplier to handle the parts carefully and keep the parts separately without\r\nhaving metal to metal contact','Informed to Treatment supplier to handle the parts carefully and keep the parts separately without\r\nhaving metal to metal contact','CAPA found okay','','2015-04-24','Avinash(R.J.)','Manjunath(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','17715','Post DN','no','Misc','Manjunath(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8462,'18-110A','Magellan Aerospace Bournemouth','FORK END INTERMEDIATE','238302','D575 40494 202','S80 FHT','J',1,'RP400840','','42884','','0000-00-00',NULL,'yes','yes','yes','','','','','','','total length [-0.5mm side]','The Following route cause analyzed for the parts rejected, Jaws Boring is not good,part not butted properiy to the jaws because of small chips are in Part butting faces. Roughing and Finishing inserts wear out. ','Roughing stage clean the jaws with the help of air and before loading the part.after clamping check the every part it was butted in the jaws face properly.','Roughing stage clean the jaws with the help of air and before loading the part.after clamping check the every part it was butted in the jaws face properly.','After milling operation completed Total length achived part accepted.','','2015-04-25','Dinakar(K)','        GUNDEGOWDA H.G.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8463,'28-003A','Magellan Aerospace New York  Inc.','PIN-ATTACHMENT WALKING BE','970608-03','161A7305-1','','PL-Rev-NC, DL Rev-B',1,'126999_R0_C1','','42809','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Thread nogo 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.','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. ','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. ','CA/PA found okay','','2015-04-26','Dinakar(K)','        Dinakar K','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8464,'35-138','Saab AB','FLCD_DS_SUPPORT_DEFLECT_S','NE14','423Z6189-3','BAC1534-62C','---',9,'PA-1300 2014-2','','43019','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Thickness under size(1),layer chip out(4),dent marks on face(4)','The Following Route causes analyzed for material chip off after outer profile machining. \r\n1. Due to RM deviations material will chip off. \r\n2. While running production, the finishing tool wear out causes light chip off in material. \r\n3. Steel Butting sheet for part is not Flat.','The following Corrective Action/Preventive Action taken to avoid Materiel chip off. \r\n1. Raw Material will inspect visually before issuing to production. If found any problem visually RM will be\r\nquarantined. \r\n2. Dia 8 end mill life calculated, informed to operators to monitor the tool life.and change the tool after as mentioned. \r\n3. Steel butting plates flatness inspection done before\r\nproduction starts.','The following Corrective Action/Preventive Action taken to avoid Materiel chip off. \r\n1. Raw Material will inspect visually before issuing to production. If found any problem visually RM will be\r\nquarantined. \r\n2. Dia 8 end mill life calculated, informed to operators to monitor the tool life.and change the tool after as mentioned. \r\n3. Steel butting plates flatness inspection done before production starts. Taking all the above PA, rejections happened in material chip off. Out of 100nos production 5 to 6nos getting rejection. Due to customer requirement parts are manufactures with considering rejections.','CAPA found okay','','2015-04-26','Lohith(K)','Theerthappa K.N.,Shivaraj K S,Hari Prasad,','','0000-00-00','Thickness under size(1),layer chip out(4),dent marks on face(4)','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','HAASVF2SS','Manjunath(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8465,'18-560A','Magellan Aerospace Wrexham','SPAR INBOARD OFW','437515A0','L575 51779 200','','B00',1,'RM132919 Amnd 1','','42606','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','hole diameter 5.55+/-0.12 and measured dia5.70.','While drill operation fixture was not produced bigger dia hole in fixture.\r\n','introduced bigger dia hole in fixture .\r\n','introduced bigger dia hole in fixture .\r\n','CAPA found okay','','2015-04-26','D.K.Pavan (Kumar)','Girish(Prasad P)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','04','no','Misc','Girish(Prasad P)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8466,'18-533A','Magellan Aerospace Wrexham','STOP DOOR','4527101','L575 52004 200','','A',1,'RM132922 Amnd 01','','43167','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Bore dia oversize. (dia16.20+/-0.03) measured dia 16.25 to 16.26. ','After running several parts from Boring Bar this deviation found ','Reamer has been introduced and trails have been done and found okay with the trails ','Reamer has been introduced and trails have been done and found okay with the trails ','CAPA found okay','','2015-04-27','Krishna(Chowdary.G.P.)','Jayarama(M.B.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','04','no','Misc','Girish(Prasad P)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8467,'18-118B','Magellan Aerospace Bournemouth','BEARING HOUSING','A1129U','D275 40005 200','','C01',1,'RP400842','','42593','','0000-00-00',NULL,'yes','yes','yes','','','','','','','running time od under size...','Due to while OD operation chips not removed. ','Before the OD operation remove the chips every part then run the production. ','Instructed operator to before the OD operation remove the chips every part then run the production.','CAPA found okay','','2015-04-27','','        Devaraj K.C.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8468,'18-591A','Magellan Aerospace Wrexham','FITTING HOIS FWD','6679701-1','L575 51923 200','','A00',2,'RM132921 Amnd 1','','43114','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','Dig mark observed on part at outer profile.','When running on FA part dig mark obsvered on part profile.In roughing program this deviation came and after finishing program dig mark observed on part.\r\nImmedetely checked the program by simulation and also gouges in CAD.Problem not found and again reposted the program with 3-Axis post and program checked and running in machine.\r\n ','Inform to Softwear proverder regarding the deviation and validated the post by different parts and found ok.\r\nCA/PA not found for this deviation at the movement.','CA/PA not found for this deviation at the movement.','Based on the CA/PA in the next part we will moniter the effectivness.','','2015-04-28','Ramesh(Poojary)','Ramesh(Poojary)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','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),(8469,'18-121A','Magellan Aerospace Bournemouth','BARREL - STRUT','247348','D572 50463 201','S98 FHT','F',2,'RP400839','','42486','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','ID Thread NOGO answered.','Thread was damaged due to wear out of inserts. Bcause machine cenre height not correct.The operator intended to rework the damaged thread resulting in non conformance of ID.  \r\n\r\n','Insert was worn out at that stage which was replaced for the next job and adjusted the machine centre heigt to extend the tool and insert life.','The block holding the tool shall be set by the Supervisor for every batch which is expected to extend the tool life and reduce these type of non conformances and supervisors give to training to operators. ','CA/PA found okay','','2015-04-28','Dinakar(K)','Shivappa M B,Shivanand D.B.,SHIVAKUMAR ,Ravi R,Rajesh T,Raghavendra Rao R,Mohan Kumar C.M.,Manohara M,Devaraj K.C.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','FI','no','DX 200-1','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8470,'18-121A','Magellan Aerospace Bournemouth','BARREL - STRUT','247348','D572 50463 201','S98 FHT','F',1,'RP400839','','42487','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','ID Thread NOGO answered.','Thread was damaged due to wear out of inserts. Bcause machine cenre height not correct.The operator intended to rework the damaged thread resulting in non conformance of ID.  \r\n','Insert was worn out at that stage which was replaced for the next job and adjusted the machine centre heigt to extend the tool and insert life.','The block holding the tool shall be set by the Supervisor for every batch which is expected to extend the tool life and reduce these type of non conformances and supervisors give to training to operators. \r\n','CA/PA found okay','','2015-04-28','Dinakar(K)','Shivappa M B,Shivanand D.B.,SHIVAKUMAR ,Ravi R,Rajesh T,Raghavendra Rao R,Mohan Kumar C.M.,Manohara M,Devaraj K.C.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','FI','no','DX 200-1','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8471,'18-122A','Magellan Aerospace Bournemouth','FORKEND ASSEMBLY','245160','D572 50462 201','S98 FHT','J01',1,'RP400839','','42562','','0000-00-00',NULL,'yes','yes','yes','','','','','','','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. ','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. ','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','CA/PA found okay','','2015-04-28','','        Rajesh T','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8472,'18-611A','Magellan Aerospace Wrexham','FITTING FWD SPAR','6772701','L575 54237 200','','A00',1,'RM132922 Amnd 01','','43112','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Wall thickness under size. ( 7.87+0.26 measured dim 7.79 to 8.05).','After finishing 1st setup part found bend and while finishing wall thickness, thickness found under size.','After roughing the part will be aged and wall thickness will be in plus side so that later we can finish the thickness','After roughing the part will be aged and wall thickness will be in plus side so that later we can finish the thickness','CAPA found okay, Next FAI part found okay','','2015-04-28','Girish(Prasad P)','Girish(Prasad P)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Girish(Prasad P)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8473,'28-006A','Magellan Aerospace New York  Inc.','SHOULDER BOLT ','G21041','162A3109 -2','',' 	PL Iss A, PSDL Iss A, ECN C141079',1,'128183_R0_C1','','42819','','0000-00-00',NULL,'','','yes','','','','','','','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.  \r\n','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.','Training for Basic handling instruments should be given that was witnessed practically in front of the machine.','','2015-04-28','','        Seetharamu D','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8474,'18-102A','Magellan Aerospace Bournemouth','BARREL-STRUT','247348','D572 50463 200','S98 FHT','F',1,'RP400839','','42555','','0000-00-00',NULL,'','','yes','','','','','','','Total lenght -0.09 undersized.  \r\n','The Following route cause analyzed for the parts rejected, Jaws Boring is not good,part not butted properiy to the jaws because of small chips are in Part butting faces.Roughing and Finishing inserts wear out.','Roughing stage clean the jaws with the help of air and before loading the part.after clamping check the every part it was butted in the jaws face properly. ','Roughing stage clean the jaws with the help of air and before loading the part.after clamping check the every part it was butted in the jaws face properly.  \r\n','CA/PA found okay','','2015-04-28','','        Rajesh B D','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8475,'18-561A','Magellan Aerospace Wrexham','SPAR INBOARD OFW','437515A0','L575 51779 201','','B00',1,'RM132919 Amnd 1','','43190','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','Crack observed on part.\r\n','While cut out operation lugs was not clamped so part get cracked.\r\n','introduced M5 bolts for clamping purpose in lugs. \r\n','introduced M5 bolts for clamping purpose in lugs. ','CAPA found okay','','2015-04-29','Ramesh(Poojary)','Ramesh(Poojary)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','04','no','Misc','Krishna(Chowdary.G.P.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8476,'30-011A','Gardner Aerospace-Derby Limited','SPAR FWD - LH','9599701','L575 51827 200','ABM3-1029 T7651','A00, ECN:PG60049U01LC52',1,'LPR0000687','','42162','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','outer flange thickness 2.5mm (+0.2/-0.1mm) so measures 2.05 to 2.85 taper noticed in part after machining.','happened due to part clamping not sufficient tight in the part, so dia 16 flat cutter program running time part was shifted.    ','plane to intraduse sufficient clamps to hold the part & continue the production','operator ware strictly warned & suggested to clamping & clamp tightness & visual checking once again clamp righting. message instead in program M0 active.\r\nput the extra clamps for proper outer wall butting face. ','CAPA found okay. Next batches taken care','','2015-04-29','Narayanappa(G)','Gajendra Singh(C.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','5','no','Misc','Narayanappa(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8477,'35-140','Saab AB','BCD_DR_BEAM_FTG_UPR_FWD_4','434837','424Z1130-14-01','7050 - T7451 ALUMINU','--B',2,'PA-1300 Group-1','','43138','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','wall thickens -side For  operator mistake. ','Wrong tool added instead of 12R3 dovetail cutter he used 12R3 End mill','Training has been given to operator regarding knowledge of Tool , and also monitoring effectiveness.','Training has been given to operator regarding knowledge of Tool , and also monitoring effectiveness.','CAPA found okay,','','2015-04-29','Anjinamurthy(H)','Anjinamurthy(H)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Anjinamurthy(H)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8478,'18-119B','Magellan Aerospace Bournemouth','HOUSING OUT B DRG 3','230699','D275 40011 200','','D01',1,'RP400842','','42596','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Id ovality problem +0.006 mm.','After running 50 to 60 parts insert tip will be worn out and running time chips not breaking properly so chips will rubbing inside the part and diameter will be oversized in the running part.\r\n','Remove the worn out insert and replace the new insert and newely offset taken and 0.2 (-) minous taken in the tool wear offset and run the part and then check the inner diameter and give the correction in wear offset and adjust the coolant correctly and run the part and checked found ok. \r\n','while setting time loading the new insert before running and after every 100 nos change the roughing insert and run the part.and every 25ns onece observe thetoolnoise,coolant floaing and chips while running ','CAPA found okay','','2015-04-29','Dinakar(K)','Ningaraj A(N)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','11','no','Misc','Sandhesh D(S)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8479,'18-119B','Magellan Aerospace Bournemouth','HOUSING OUT B DRG 3','230699','D275 40011 200','','D01',1,'RP400842','','42596','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','dig mark in outer diameter.','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.','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.','CAPA found okay','','2015-04-30','Dinakar(K)','Manjunath (M)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','09','no','Misc','Sandhesh D(S)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8480,'18-310A','Magellan Aerospace(Chalfont) Limited','STOP - U/C HINGED DOOR ','421943','F575 51392 200','','A, ECN PG49999SMAKG01',20,'P/074122','','40384','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Machine abuse observed on part surface.','Due to rubbing of tool Machine abuse has been found in Treatment house\r\n','Instructed to Production department to avoid rubbing of tool and polishing \r\n','Avoid polishing and try to finish the part in machining stage itself to avoid bench work activities','Next parts and batches found okay\r\n','','2015-05-04','Avinash(R.J.)','Nandishkumar(D.K.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','17278','POST DN','yes','Misc','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8481,'18-310A','Magellan Aerospace(Chalfont) Limited','STOP - U/C HINGED DOOR ','2552501','F575 51392 200','','A, ECN PG49999SMAKG01',5,'P/074122','','40383','','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','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','','2015-05-04','Avinash(R.J.)','Nandishkumar(D.K.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','17284','POST DN','yes','Misc','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8482,'18-310A','Magellan Aerospace(Chalfont) Limited','STOP - U/C HINGED DOOR ','417436','F575 51392 200','','A, ECN PG49999SMAKG01',10,'P/074122','','40387','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Machine abuse observed on part surface.','Instructed to Production department to avoid rubbing of tool and polishing ','Avoid polishing and try to finish the part in machining stage itself to avoid bench work activities','Next parts and batches found okay\r\n','','','2015-05-04','Avinash(R.J.)','Nandishkumar(D.K.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','17279','POST DN','yes','Misc','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8483,'35-233A','Saab AB','HINGE BRACKET 5 ','4746701','D576 50008 208','','D00',1,'1600108781','','43188','','0000-00-00',NULL,'','','yes','','','','','','no','part wall thickness under size so 1no reject.','This has happened due to not changing the fixture for next setup\r\n','Training has been imported to operators live on the machines and did tests also to ensure the operators efficiency\r\n','Training has been imported to operators live on the machines and did tests also to ensure the operators efficiency\r\n','CAPA found satisfactory','','2015-05-05','','        Manukumar H M','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8484,'18-098B','Magellan Aerospace Bournemouth','VALVE- SEAT','66894/01/00','D282 50060 204','','D',5,'RP400844','','42412','','0000-00-00',NULL,'no','no','yes','yes','no','no','no','yes','yes','RM bend observed. ','Did trails ','Did trails','Did trails','Did Trails','','2015-05-05','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','00','no','Misc','Lohith(K)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8485,'35-292','Saab AB','BEAM FITTING','599430','424Z1144-2','','--B',1,'1600099682','','41537','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','*Base thickness minus(-0.06).*','production run 72nos , but one number base thickness minus (-0.06mm).\r\nthis erorr bolt not currct tight or chips lock in part bottem face.','cleaning fixture before part clamping & insert moo in progrem starting .','cleaning fixture before part clamping & insert moo in progrem starting .','CAPA found okay','','2015-05-06','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Rangaswamy()','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8486,'35-280','Saab AB','SUPPORT','431589A2','423Z1203-2-02','','---',1,'May 2015','','42811','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','*Total height 0.2mm minus.*','After Machining found chamfer oversize and to make it proper facing done and found part length under size\r\n','Chamfer program added to avoid these kinds of problem\r\n','Chamfer program added to avoid these kinds of problem\r\n','CAPA found okay','','2015-05-06','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','*Total height 0.2mm minus.*','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Rangaswamy()','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8487,'35-276','Saab AB','BRACKET INTERMED','599462','423Z1123-3-02','','--A',1,'May 2015','','42104','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','*Part radius 1mm minus side*','','','','Under investigation','','2015-05-06','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','*Part radius 1mm minus side*','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Rangaswamy()','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8488,'18-210B','Magellan Aerospace(Chalfont) Limited','BODY','4842','D321 40204 204','','D, ECN NR29999ST1KM15, NR29999ST2KF65, WQN DFB09775',1,'P/074113','','40782','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Rounded indications observed on part surface.','Due to rubbing of tool Machine abuse has been found in Treatment house','Instructed to Production department to avoid rubbing of tool and polishing \r\n','Avoid polishing and try to finish the part in machining stage itself to avoid bench work activities','Next parts and batches found okay\r\n','','2015-05-06','Avinash(R.J.)','Nandishkumar(D.K.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','17259','POST DN','yes','Misc','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8489,'35-268','Saab AB','PIN-SPRING-RETAINER','G21357K05','424Z6114-1','','---',1,'May 2015-2','','43347','','0000-00-00',NULL,'yes','yes','yes','','','','','','no','Running time M6 bolt head broken so part rotate.','Operation 09 running in rotary setup,but this setup using M6 bolts in part clamping ,that time bolt head broken, so realize clamping force and part rotate.','Change another M6 bolt continue production , after produce  15nos production to change M6 bolts.','Next batch change bolt make add using torue Allen key.','CAPA unsatisfactory Pls give proper Preventive action','','2015-05-07','Girish(Prasad P)','                Sundar D.K.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8490,'35-017','Saab AB','9901503-075','95855','D576 50011 200','L167','A',18,'1600108781','','43444','','0000-00-00',NULL,'yes','yes','yes','','','','','','','35-017 1bilit 18 nos rejected due to vacum problem.part left.\r\ntotal length under size.\r\nactual dimension 48.60\r\nmeasure dimensions 48.20','while part running time vacuum pressure problem so part total length under size,','put the external clamp 1 nos done,\r\nchange new vacuum rubber chord, \r\nvacuum pipe change\r\n','change the new vacuum fixture.','CAPA found okay','','2015-05-07','','        Siddaramappa ','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','no','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8491,'35-079','Saab AB','BUSH FLANGED','229234','D575 40386 200','S80','B ECN NG29999ST2TT68',4,'PA 1217-Bushes (A320','','42876','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','yes','1) OD UNDER SIZE BY 0.020 TO 0.025MM IN 3NOS. \r\n2) STEP NOTICED ON ID IN 1NO.','To 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','CAPA found okay','','2015-05-08','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','Misc','Manjunath(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8492,'35-231A','Saab AB','HINGE BRACKET 4 ','4746701','D576 50007 208','','E00',1,'1600108781','','42904','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','* Dig mark on 3D wall Face, not fit for rework.','While part taking out of the machine, the part has dropped down causing dig mark on 3D surface','Strictly instructed to operators to take of the part and blow the air properly after finishing, so that it would avoid slippery condition of the part.','Strictly instructed to operators to take of the part and blow the air properly after finishing, so that it would avoid slippery condition of the part.','CAPA found okay','','2015-05-08','Girish(Prasad P)','Sundar D.K.,Subramanya L Naik,Manukumar H M,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','MakinoF5-2','Manjunath(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8493,'35-078','Saab AB','BUSH','1111506738','D575 40149 200','DTD-197','B ECN NG29999ST2TT60',7,'PA 1217-Bushes (A320','','42882','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','OD measures undersize.','To reduce the OD for 2 microns the operator has given correction for 20 microns ','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','CAPA found okay','','2015-05-08','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','Misc','Manjunath(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8494,'35-078','Saab AB','BUSH','1111506738','D575 40149 200','DTD-197','B ECN NG29999ST2TT60',17,'PA 1217-Bushes (A320','','42882','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','ID measures ovality upto 20 to 25microns.','To reduce the OD for 2 microns the operator has given correction for 20 microns ','Readings will be written in paper and cross checked twice before corrections\r\n','Readings will be written in paper and cross checked twice before corrections\r\n','CAPA found okay','','2015-05-08','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','Misc','Manjunath(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8495,'35-251','Saab AB','SPACER','571467','423Z1987-1','','---',1,'PA 1510 NEW PARTS-1','','42863','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','ID over size by 0.05mm. ','Insert was worn out so this problem occurred. ','Check insert status regularly and know the life of inserts and change inserts according instructions. ','Check insert status regularly and know the life of inserts and change inserts according instructions.  ','CA/PA found okay','','2015-05-08','Avinash(R.J.)','Nagaraj(G. Nadiger)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','17833','POST DN','no','Misc','Manjunath(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8496,'35-251','Saab AB','SPACER','571610','423Z1987-1','','---',1,'PA 1510 NEW PARTS-1','','41477','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','dia 5.08 hole id taper hole center shift 0.2 to o.35.  \r\n','programme drilling operation running before center bit operation not running so drill shifted to 0.35.  \r\n','Next batch before drilling operation running centre bit operation was running in program.  \r\n','Next batch before drilling operation running centre bit opera tion was running in program.  \r\n','CA/PA found okay','','2015-05-08','Avinash(R.J.)','Nagaraj(G. Nadiger)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','17835','POST DN','no','Misc','Manjunath(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8497,'35-249','Saab AB','STANDOFF','G21441K06','423Z1916-3','','---',1,'May 2015','','42792','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','* Center OD under size up to 0.010mm.','While machining chips clogged to insert and center OD found under size\r\n','Proper flow of coolant will be made and airblown at regular intervals of time \r\n','Proper flow of coolant will be made and airblown at regular intervals of time \r\n','CAPA satisfactory','','2015-05-09','Dinakar(K)','Shivanand D.B.,SHIVAKUMAR ,Raghavendra Rao R,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','ST20Y1','Manjunath(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8498,'35-017','Saab AB','9901503-075','95855','D576 50011 200','L167','A',18,'1600108781','','43443','','0000-00-00',NULL,'yes','yes','yes','','','','','','','35-017 running time vacuum presser problem so part left.\r\nactual dimensions 48.60\r\nmeasure dimension 48.20','while part running time vacuum pressure problem so part total length under size.','put the external clamp 1nos done\r\nchange the new vacuum rubber chord\r\nvacuum pipe change & continue the production    ','change the new vacuum fixture ','CAPA found okay, ','','2015-05-10','','        Basavaraja S. Jr.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','no','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8499,'35-084','Saab AB','WASHER-SIDE ROLLER ','222','F579 53067 200','S535','A',9,'PA 1226-Roller Housi','','33208','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Part Damage. ','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. ','CA/PA found okay','','2015-05-11','Dinakar(K)','Rajesh T,Narasimhamurthy K.G.,KRISHNAMURTHY N,GUNDEGOWDA H.G.,Devaraj K.C.,','','0000-00-00','Dent marks observed','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','DX 200-1','Manjunath(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8500,'28-005A','Magellan Aerospace New York  Inc.','SHOULDER BOLT ','G21123','162A3109-1','','PL Iss A, PSDL Iss A',8,'124961_R0_C1','','40738','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Running time thread (-) side 0.05.  \r\n','Thread pitch micrometer was not set to zero properly (0.02MM error)and maintained effective dia 7.22\r\nin pitch micrometer and when thread gauge checked NOGO answered.  ','Pitch micrometer is set to zero using master gauge and for next part maintained thread effective dia 7.24 and gauge found ok and run the production.  \r\n','Instructed to operator to check all the instruments  whether it is set to zero or not before start the production.  \r\n','CA/PA found okay','','2015-05-11','Dinakar(K)','Shivaraj K S,Rajesh B D,Narasimhamurthy K.G.,KRISHNAMURTHY N,Hari Prasad,GUNDEGOWDA H.G.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','0','FI','no','DX 200-3','Sudhagar(V)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8501,'18-570A','Magellan Aerospace Wrexham','PLATE RUBBING RIB 4','50005301','L575 51785 200','','A',1,'RM132920 Amnd 1','','42995','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','De burr chamfer over sized by 2mm.','As these are PTFE parts which is very soft in condition at some portion of the part chamfer got oversize.','Got corrected in doing deburring and did deburring for next 20 PTFE parts and got to know about with how much pressure should carry out deburring. ','Got corrected in doing deburring and did deburring for next 20 PTFE parts and got to know about with how much pressure should carry out deburring. ','CAPA found okay, Next parts gone well.','','2015-05-11','Nagaraju(T)','Nagaraju(T)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','0','01','no','Misc','Muniyappa(N)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8502,'18-569A','Magellan Aerospace Wrexham','PLATE RUBBING RIB 3','50005301','L575 51784 201','','A',1,'RM132919 Amnd 1','','42992','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Profile rework time part dig mark on the part surface.','When rework  Program running on the Part, part was lifted and dig mark on the part surface\r\n','Process was changed at a time 2 RH parts machined not 1 LH and 1 RH.\r\n','Program Proved and part found ok Same Process will be updated all the PTFE part\r\n','CAPA found okay','','2015-05-11','Ramesh(Poojary)','Ramesh(Poojary)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','0','01','no','Misc','Muniyappa(N)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8503,'28-006','Magellan Aerospace New York  Inc.','SHOULDER BOLT','G19876K01','162A3109 2','15-5PH Bar,Per AMS56','NA',12,'120168_R0_C0','','35967','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','1)Thread gauge not answer.','•	Gauge found oversize and came to know only after calibration •	Initially CIM Gauge no-17 was used\r\nin the stage and later came to know the gauge found oversize. So parts again re-ensured by thread\r\npitch micrometer •	After parts were passed from TPM, then we released the parts to next\r\nstage •	Thread ring gauge procured from local supplier(Thread gauge product) is not consistent in\r\nthe quality •	This make sometimes it works for hundred numbers and sometimes it goes to five\r\nhundred numbers and later we did came to know by experience','•	Thread Pitch micrometer calibrator not available at our local certify to NABL •	So TPM self\r\nchecked by ourselves with \" Master Thread Plug Gauge \" of different frequencies for usage and this\r\nis to be done every time for new batches of production. •	We will enquire TPM calibrator and they\r\nare approved to NABL or other standard. •	Based on our experience and current issue, we will use\r\nmeasuring frequency of TRG for hundred to one fifty numbers only, after that we will send for\r\ncalibration •	After calibration and based on the results/wear out in gauge, we will fix the\r\nfrequency for next usage up to fifty to hundred numbers. •	Any time we will keep three gauges, one\r\nis to production and one is to inspection and another one for stock. •	Mean time we will enquire\r\nfor other makes also.','•	Thread Pitch micrometer calibrator not available at our local certify to NABL •	So TPM self\r\nchecked by ourselves with \" Master Thread Plug Gauge \" of different frequencies for usage and this\r\nis to be done every time for new batches of production. •	We will enquire TPM calibrator and they\r\nare approved to NABL or other standard. •	Based on our experience and current issue, we will use\r\nmeasuring frequency of TRG for hundred to one fifty numbers only, after that we will send for\r\ncalibration •	After calibration and based on the results/wear out in gauge, we will fix the\r\nfrequency for next usage up to fifty to hundred numbers. •	Any time we will keep three gauges, one\r\nis to production and one is to inspection and another one for stock. •	Mean time we will enquire\r\nfor other makes also.','Rework done and found okay with the parts','C32116','2015-05-11','Avinash(R.J.)','Sudhagar(V)','IRR113784','2014-09-10','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Manufacture Only','0','Customer end','yes','Misc','Sudhagar(V)','no',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8504,'35-017','Saab AB','9901503-075','95855','D576 50011 200','L167','A',3,'1600108781','','43443','','0000-00-00',NULL,'yes','yes','yes','','','','','','','running time part lifted 3nos reject due to outer profile dig mark.','* while part ruining  time vacuum pressure was low part got lifted up from fixture & dig mark at outer profile of the part.\r\n* vacuum rubber chord got weak.  ','put external clamp 1 nos at edge of the part. \r\n\r\nchange the vacuum rubber chord.','next batch change the new vacuum fixture. ','CA/PA found okay','','2015-05-11','','        Krishna Chowdary.G.P.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8505,'18-104A','Magellan Aerospace Bournemouth','BODY TURNBUCKLE','239338','D575 40490 200','S80 FHT','E',1,'RP400840','','42565','','0000-00-00',NULL,'','','yes','','','','','','','Thread NoGo answerd Running time.','After 25nos running threading insert will be wear out.for next part threading insert will be changed and 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 answer. ','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 down 0.05mm and run the part and then gauge answered and next part run in same reading & the part found okay.  \r\n \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 down 0.05mm and run the part and then gauge answered and next part run in same reading & the part found okay.  \r\n \r\n','CA/PA found okay','','2015-05-11','','        KRISHNAMURTHY N','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8506,'35-262','Saab AB','ROD-END','G21409K03','424Z3413-1','','--A',1,'April 2014','','43196','','0000-00-00',NULL,'','','yes','','','','','','','sphere od step.','Part 2nd setup running time part clamping area very small.part butting in jaws frount so Od running time part come frount so sphere od was step observed.','Changing the jaws and boring in step in back side in jaws and clamping part re offset taking and running part was ok.instruction given to operator part was clamping in backside in jaws in every batch.','Changing the jaws and boring in step in back side in jaws and clamping part re offset taking and running part was ok.instruction given to operator part was clamping in backside in jaws in every batch.','CAPA found okay','','2015-05-12','','        Ningaraj A N','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8507,'35-275','Saab AB','PIN','G21411K03','426Z3601-1','','--A',1,'1600099682','','43006','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Taper problem outer dia undersized by 0.020mm.','The length of the parts was 225mm at one end OD found Taper\r\n','Machine changed to mazak and part found okay\r\n','Machine changed to mazak and part found okay\r\n','CAPA found okay','','2015-05-12','Ravi(M)','Manjunatha(N)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Ravi(M)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8508,'18-611A','Magellan Aerospace Wrexham','FITTING FWD SPAR','9401601','L575 54237 200','','A00',1,'RM132922 Amnd 01','','43336','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Hole pitch oversize by 0.5mm.','This is manual error\r\n','Same Program running on another RM , Part found OK\r\n','Before running the program cross check the all offset and location hole co ordinate\r\n','CAPA found okay','','2015-05-12','Ramesh(Poojary)','Ramesh(Poojary)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','0','FI','no','Misc','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8509,'35-186','Saab AB','CED_LATCH_FITTING-FWD','627578A8','425Z0610-18','','---',1,'1600068243','','43209','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dia 25.400 +0.017 bore MESURED 25.415 to 25.427.','part running time bore chattering. Bore finishing not ok. so part reject.After running 10 to 15 parts chattering found on the Bore.','Reamer has been introduced to solve this problem. Trails have done and found okay with the bore in terms of both reproducible and reproductive.','Reamer has been introduced to solve this problem. Trails have done and found okay with the bore in terms of both reproducible and reproductive.','CAPA found okay','','2015-05-12','Girish(Prasad P)','Prashanth Kumar(M)','','0000-00-00','Dia 25.400 +0.017 bore MESURED 25.415 to 25.427.','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','05','no','Misc','Girish(Prasad P)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8510,'35-169','Saab AB','ALCD_STRUCT_SUPPORT-FTG_L','581312','423Z1200-12-01','','---',1,'May 2015','','42477','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Tool holder dig mark in wall,,','1st part proving time dia 10 ball nose tool holder dig in part surface,in this setup using 2 ball for part finish . short ball using taper finish & long ball using base finish ,but operator inter change ball nose so part rejected.','Interchanged ballnose run production. explain to operator check Description program inside.\r\n','instructed to operator every 1st part proving time check Description in every program. & add M00 (program stop) at program beginning. ','CAPA satisfactory','','2015-05-12','','        Gurukiran S M','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8511,'18-413B','Magellan Aerospace Bournemouth','ACTUATOR HOUSING','9161','D278 50162 200','','A',1,'RP401021_Amnd No. 1','','43299','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Bore oversize 0.012mm.','running time chips was locked in part so id oversize.','Next part running semi finishing tool using in id finish. after id roughing running 0.3 stock in id.After semi finishing running 0.04 stock in id.after running semi finish clean the chips after running id finishing tool part was ok. ','Next part running semi finishing tool using in id finish. after id roughing running 0.3 stock in id.After semi finishing running 0.04 stock in id.after running semi finish clean the chips after running id finishing tool part was ok. ','CAPA found okay','','2015-05-12','Dinakar(K)','Shivanand D.B.,SHIVAKUMAR ,Raghavendra Rao R,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','3','no','ST20','Dinakar(K)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8512,'18-284A','Magellan Aerospace Bournemouth','SPINDLE FOR CLACK ALVES O','Y11518','A281-40019-200','S80 FHT','A',1,'RP400846','','43296','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','OD Under size by 0.18mm.','','','','Under Investigation','','2015-05-12','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','FI','no','Misc','Narasimha Murthy(R)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8513,'35-082','Saab AB','HOUSING-SIDE ROLLER','682234A0','F579 53065 202','ABM3-1029 T7651','B, PG52307ST4KA80',2,'1600090315','','43314','','0000-00-00',NULL,'yes','yes','yes','','','no','','','no','10r1 tool running time chips lock so rib thinness 0.2 (-)side','This was happened due to chips clogging while machining the part.The pressure of coolant flow is very down so chances of chips clogging is very high.','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','Under investigation','','2015-05-12','','        Anjinamurthy H','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8514,'18-542A','Magellan Aerospace Wrexham','BRACKET LOWER STRUT','4527101','L575 52898 200','','A',1,'RM132918 Amnd 1','','42603','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Hole position out of tolerance (0.03)','Method was wrongly defined.\r\n','introduced datum based methods in all stages.\r\n','introduced datum based methods in all stages.\r\n','CAPA found okay','','2015-05-13','Ramesh(Poojary)','Ramesh(Poojary)','','0000-00-00','Hole position out of tolerence (0.03)','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','Misc','Muniyappa(N)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8515,'18-603A','Magellan Aerospace Wrexham','BRACKET','547010','L575 52139 201','','A00',1,'RM132920 Amnd 1','','42731','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Hole position out of tolerence (0.1mm)','Carbide drilled on the part, Hole position out of tolerance','First free drill and after hole mill used the Hole position found ok','Introduced hole mill for all part holes','CA/PA found satisfactory.','','2015-05-13','Ramesh(Poojary)','Ramesh(Poojary)','','0000-00-00','Hole position out of tolerence (0.1mm)','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','Misc','Muniyappa(N)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8516,'18-378B','Magellan Aerospace Bournemouth','GAMMA FITTINGS ','M590350 97020','NSA840020-250','','L',1,'RP401480_Amend No.-1','','42098','','0000-00-00',NULL,'yes','no','no','no','yes','yes','no','no','no','corroson abserved.','Due to over polishing and rubbing of tool corrosion found on the surface','Due to over polishing and rubbing of tool corrosion found on the surface','Due to over polishing and rubbing of tool corrosion found on the surface','Under investigation','','2015-05-13','Dinakar(K)','Ravi C,Krishnanaik J N,Dinakar K,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','0','FI','no','QT100S-5','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8517,'18-108A','Magellan Aerospace Bournemouth','FORK END OUT BD','A0860N','D575 41546 200','S80 FHT','B',1,'RP400840','','42568','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Thread tight, thread gauge not butted. ','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','CA/PA found okay','','2015-05-13','Dinakar(K)','Seetharamu(D)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Manufacture Only','','05','yes','Misc','Sandhesh D(S)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8518,'18-102A','Magellan Aerospace Bournemouth','BARREL-STRUT','247348','D572 50463 200','S98 FHT','F',1,'RP400839','','42555','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','1nos rejected reason tool off set wrong so part dig mark so part rejected. ','Due to manual error by operator this deviation coming. Tool offset not taken by operator when\r\nchanging the drill in between production running. ','Operator to work seriously and concentrate while doing offset, program calling and checking the parts. Supervisor will monitor operator to guide them to avoid such problems. Tool offset taken and production running.  \r\n \r\n','Informed to operator to work seriously and concentrate while doing offset, program calling and checking the parts. Supervisor will monitor operator to guide them to avoid such problems. ','CA/PA found okay','','2015-05-13','Dinakar(K)','Rajesh B(D)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','05','no','Misc','Sandhesh D(S)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8519,'18-119B','Magellan Aerospace Bournemouth','HOUSING OUT B DRG 3','CB872484','D275 40011 200','','D01',1,'RP400842','','42541','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','thread gauge not answered.','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.  ','CAPA Satisfactory','','2015-05-13','Dinakar(K)','Shivanand(D.B.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Manufacture Only','','01','yes','Misc','Sandhesh D(S)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8520,'18-122A','Magellan Aerospace Bournemouth','FORKEND ASSEMBLY','245160','D572 50462 201','S98 FHT','J01',2,'RP400839','','42563','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Thread Effective diameter oversize.','Due to operator not checked in the m/c.  \r\n \r\n','Next production batch will be rework compelted.  \r\n','Instructed operator to every part checked in m/c then remove the part.  \r\n','CAPA satisfactory','','2015-05-13','Dinakar(K)','Yarri Gowda,Shivappa M B,Shivanand D.B.,SHIVAKUMAR ,Ravi R,Rajesh T,Raj Kumar,Raghavendra Rao R,Punith G S,Mohan Kumar C.M.,Dhananjaya N,Devaraj K.C.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Manufacture Only','0','FI','yes','ST20','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8521,'18-041B','Magellan Aerospace Bournemouth','EDGE BEAM BRACKET 2','427158','L575 52324 201','','A00',1,'RP400836_Amnd_01','','42634','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Tool dig mark an rib top.','Tool length made minimum due to wrong interpretation due to this reason dig mark occurred. ','Display message will be popped out and this will display while program is running. Necessary training given to the operator','Display message will be popped out and this will display while program is running. Necessary training given to the operator','CAPA found okay','','2015-05-14','Anjinamurthy(H)','Girish(HP)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','05','no','Misc','Anjinamurthy(H)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8522,'18-118B','Magellan Aerospace Bournemouth','BEARING HOUSING','A1129U','D275 40005 200','','C01',1,'RP400842','','42594','','0000-00-00',NULL,'yes','yes','yes','','','','','','','I.D OVALITY PROBLEMS SO PART REJECT.\r\n','After running 50 to 60 parts insert tip will be worn out and running time chips not breaking properly so chips will rubbing inside the part and diameter will be oversized in the running part.  \r\n \r\n','Remove the worn out insert and replace the new insert and newely offset taken and 0.2 (-) minous taken in the tool wear offset and run the part and then check the inner diameter and give the correction in wear offset and adjust the coolant correctly and run the part and checked found ok.  \r\n','while setting time loading the new insert before running and after every 100 nos change the roughing insert and run the part.and every 25ns onece observe thetoolnoise,coolant floaing and chips while running. ','CA/PA found okay','','2015-05-16','','        Shivappa M B','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8523,'28-003A','Magellan Aerospace New York  Inc.','PIN-ATTACHMENT WALKING BE','970608-03','161A7305-1','','PL-Rev-NC, DL Rev-B',1,'126999_R0_C1','','42065','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','DUMMY','DUMMY','DUMMY','DUMMY','DUMMY','','2015-05-16','Dinakar(K)','Seetharamu D,S. Shiva Kumar,Rajesh B D,Manjunatha N.R.,KRISHNAMURTHY N,GUNDEGOWDA H.G.,Girish HP,Diwakar R.B.,Dinakar K,Ashith B,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','0','FI','no','DX 200-2 ','Sudhagar(V)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8524,'28-003A','Magellan Aerospace New York  Inc.','PIN-ATTACHMENT WALKING BE','970608-03','161A7305-1','','PL-Rev-NC, DL Rev-B',1,'126999_R0_C1','','42065','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','DUMMY','DUMMY','DUMMY','DUMMY','DUMMY','','2015-05-16','Dinakar(K)','Seetharamu D,S. Shiva Kumar,Rajesh B D,Manjunatha N.R.,KRISHNAMURTHY N,GUNDEGOWDA H.G.,Girish HP,Diwakar R.B.,Dinakar K,Ashith B,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','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),(8525,'35-251','Saab AB','SPACER','571610','423Z1987-1','','---',1,'PA 1510 NEW PARTS-1','','41477','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','DUMMY ','DUMMY  \r\n','DUMMY ','DUMMY ','DUMMY','','2015-05-16','Avinash(R.J.)','Nagaraj(G. Nadiger)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','17835','POST DN','no','Misc','Manjunath(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8526,'28-005A','Magellan Aerospace New York  Inc.','SHOULDER BOLT ','G21123','162A3109-1','','PL Iss A, PSDL Iss A',8,'124961_R0_C1','','40738','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','DUMMY ','DUMMY ','DUMMY  ','DUMMY ','DUMMY','','2015-05-16','Dinakar(K)','Shivaraj K S,Rajesh B D,Narasimhamurthy K.G.,KRISHNAMURTHY N,Hari Prasad,GUNDEGOWDA H.G.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','0','FI','no','DX 200-3','Sudhagar(V)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8527,'18-118B','Magellan Aerospace Bournemouth','BEARING HOUSING','A1129U','D275 40005 200','','C01',1,'RP400842','','42594','','0000-00-00',NULL,'yes','yes','yes','','','','','','','DUMMY ','DUMMY ','DUMMY ','DUMMY ','DUMMY','','2015-05-16','','        Shivappa M B','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8528,'18-083A','Magellan Aerospace Wrexham','STUD PLATE','518635','D278 50007 201','ABM3 1029','D01',1,'RP125888','','41963','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dig mark observed on face.','While running operation 03 18-082A LH part, RH part 18-083A loaded due to mis interpretation of LH and RH part. Operator not maintained the discipline of parts segregation and causes error.','All parts LH and RH part identified and kept separately in racks and informed to operators and supervisors to maintain the discipline. ','Informed to operators to identified the parts when doing LH and RH parts supervisors to monitor the discipline in machines to avoid such errors.  \r\n','DUMMY','','2015-05-16','Lohith(K)','Dhananjaya(N)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','3','no','Misc','Lohith(K)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8529,'35-083','Saab AB','PIN-SIDE ROLLER','A0729X','F579 53066 200','S145 FHT','C',2,'PA 1226-Roller Housi','','42875','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','2nos dia 4.10 drill cut.','sumitomo drill trialed  used 50nos run 1st dril broken rpm feed not set,2nd drill 150nos run and broken.','Rpm feed adjust the sumitomo person and set feed and rpm drill life 300nos.','Rpm feed adjust the sumitomo person and set feed and rpm drill life 300nos.','CA/PA found okay','','2015-05-16','Ravi(M)','Nataraja C V,Manjunatha N,Manjunath  M,,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','3','no','QT100S-1','Narasimhamurthy(K.G.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8530,'18-582A','Magellan Aerospace Wrexham','FITTING AFT SPAR','444451','L575 51866 201','','A00',2,'RM132921 Amnd 1','','43575','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','Base thickness minus 9.0+/-0.2 measured 8.65mm.','Due to Fixture Issue. Used the Existing Fixture of 18-595A_JF01. basically it was Vise concept fixed Jaw & movable Jaw.Movable jaw was more play with Dowell pins,Dowell pins also  short length , movable jaw sliding length was less.it was lifting the part during tightening.\r\n','Change the Dowel Pins, Movable jaw locate the  dowel pins correct position.\r\n','Ensure the part butting properly by 50 micron feeler gauge after loading the part on fixture.\r\n','CAPA found okay','','2015-05-16','Ramesh(Poojary)','Rangaswamy()','','0000-00-00','Base thickness minus 9.0+/-0.2 measured 8.65mm.','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Rangaswamy()','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8531,'35-080','Saab AB','PLAIN BUSH','H7501','S64 2S385','DTD-197','7-S64',41,'PA 1217-Bushes (A320','','43509','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1)OD undersize-15nos.\r\n2)ID ovality-18nos.\r\n3)length undersize-8nos.','1)While doing a first off part operator entered wrong value to proving the bore diameter.  \r\n2)After wear out of insert operator as to give minor  correction for adjustment for that time it was gone wrong so this divination was occurred.  \r\n3)Operator did not take the offset correctly.  \r\n','1)Next part bore adjusted and continued production.Next produced parts are found OK.  \r\n2)Planned for incorporate one more tool between rough and finish cut for maintain same reading for finishing tool.  \r\n3)Instructed Operator to take the offset correctly.  \r\n','1)After proving this method feed back will be taken and same will be updated.\r\n2)Informed to operator to check the bore diameter correctly in bore gauge and entered the correct value in machine while proving the first off part. Need to monitor the operator while doing first off parts.\r\n3)Instructed Operator to take the offset correctly.  \r\n  \r\n ','CA/PA found okay','','2015-05-16','Krishna(Chowdary.G.P.)','Dinakar(K)','','0000-00-00','OD undersize-15nos,ID ovality-18nos,length undersize-8nos','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','Misc','Manjunath(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8532,'18-192A','Magellan Aerospace Bournemouth','BUSH FAILSAFE UPPER-RH','P1631','L575 58369 201','BS 23','A00',1,'RP400846','','43604','','0000-00-00',NULL,'no','no','yes','','','','','','','RUNING TIME O D -SIDE 0.04','Due to operator checking eroor in micrometer not zero reading.  \r\n','Next micrometer set zero reading and master pin cross checked and run the part the OD found OK.  \r\n','Inform to operator first instrument cross checked master gauge then after part checked.  \r\n','CA/PA found okay','','2015-05-16','','        Devaraj K.C.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8533,'35-166A','Saab AB','HOUSING PIN','427288','423Z1124-6-01','','--A',1,'1600096186','','39689','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Tool Dig mark observed on the face that was found after surface treatment.','Due to tool offset tool over travelled and took the extra material.','Senior Operator did the mistake and just warned about the mistake in the meeting.','Weekly training conducted about the on going issues and to make operator knowledgable.','Next part found satisfactory.','','2015-05-19','Avinash(R.J.)','Manjunath(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','Post DN','no','Misc','Avinash(R.J.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8534,'18-382A','Magellan Aerospace(Chalfont) Limited','SLEEVE BEARING ','240136','D575 40037 200','','A',1,'P/074123','','42456','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Gauge strucked inside the id thread.','after running the id threading operation we are checking the part in inside the machine but in this part after running the threading operation not remove the burr and check the part that time gauge will strucked inside the thread so part will rejected..  ','After running the threading operation remove the burr in every part before checking the part, and avoiding the this type of rejections.','after running the inside or outer diameter threading check the every parts in inside the machine but check the parts after removing the burr. and avoiding the same type of rejections and this type of rejection not repeated again. ','CAPA found okay','','2015-05-21','Dinakar(K)','Manjunatha(N)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','05','no','Misc','Sandhesh D(S)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8535,'18-509A','Magellan Aerospace Wrexham','BUSH SPOILER','10074680055','L575 51809 200','','A',1,'RM132922 Amnd 01','','43786','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','OD Undersize.','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\r\nand chips will be rubbed in the outer diameter and part will be under sized. So part will become rejected.  \r\n','checking the all parts outer and inner diameter before loading in the finished setup and change the previous insert 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 40 chnge the finished inserttip and run the part so this problem not repeated again.  \r\n','In roughing setup for every part check outer and inner diameter for using air gauge. In finishing set up every 40nos change the finished insert tip and run the part so this problem not repeated again.  \r\n','CA/PA found satisfactory.','','2015-05-22','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','Misc','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8536,'18-609A','Magellan Aerospace Wrexham','BUSHING','A0072X','L575 54165 200','','A00',2,'RM132922 Amnd 01','','43787','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','OD Undersize.','In OD roughing setup running time insert will be chipped out and part will came in plus side and that part not checking the operator and for next part he found out part will become over sized and he change the insert and maintain the outer dia in required size. but previous part not maintain in proper diameter. So in the finishing setup that part loading time finishing tool get the more\r\nstock and chips will be rubbed in the outer diameter and part will be under sized. So part will become rejected.  \r\n','checking the all parts outer and inner diameter before loading in the finished setup and change the previous insert tip and .2 plus taken in the wear offset and run the part and after check the diameter and give the proper correction and run the part and check the part found ok. and after every 40 chnge the finished inserttip and run the part so this problem not repeated again.  \r\n','In roughing setup for every part check outer and inner diameter for using air gauge. In finishing set up every 40nos change the finished insert tip and run the part so this problem not repeated again.  \r\n','CA/PA found satisfactory.','','2015-05-22','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','Misc','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8537,'35-298','Saab AB','SERRATED PLATE','581148A4','425Z0312-3','','--A',14,'1600097231','','41186','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Parallilism out of specification (0.05mm T0 0.3mm)','Flatness as per drawing is 0.05mm and due to bend and also twist in part. 0.05mm flatness not\r\nachieved. ','After checking the flatness, New process planed and run. but not avoid bend aging done for both the operations\r\nand checked the flatness. After this process change flatness achieved below drawing tolerance.  ','Again change process,  proved procss after taken production batch','CA/PA found satisfactory.','','2015-05-22','Rangaswamy()','Umesh B,Gurukiran S M,','','0000-00-00','Parallilism out of specification (0.05mm T0 0.3mm)','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','MakinoF3','Manjunath(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8538,'35-298','Saab AB','SERRATED PLATE','581148A4','425Z0312-3','','--A',3,'1600098209','','41187','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Parallilism out of specification (0.05mm T0 0.3mm)','Flatness as per drawing is 0.05mm and due to bend and also twist in part. 0.05mm flatness\r\nnot achieved.','checking the flatness, New process planed and run. but not avoid bend aging done for both the\r\noperations and checked the flatness. After this process change flatness achieved below drawing\r\ntolerance.','Again change process, proved procss after taken production batch ','CA/PA found satisfactory','','2015-05-22','Rangaswamy()','Umesh B,','','0000-00-00','Parallilism out of specification (0.05mm T0 0.3mm)','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','MakinoF3','Manjunath(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8539,'35-298','Saab AB','SERRATED PLATE','564847A2','425Z0312-3','','--A',3,'1600098209','','41520','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Parallilism out of specification (0.05mm T0 0.3mm)','Flatness as per drawing is 0.05mm and due to bend and also twist in part. 0.05mm flatness\r\nnot achieved. ','After checking the flatness, New process planed and run. but not avoid bend aging done for both the\r\noperations and checked the flatness. After this process change flatness achieved below drawing\r\ntolerance.','Again change process, proved procss after taken production batch ','CA/PA found satisfactory.','','2015-05-22','Rangaswamy()','Umesh B,Rangaswamy ,Gurukiran S M,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','MakinoF3','Manjunath(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8540,'35-298','Saab AB','SERRATED PLATE','564847A2','425Z0312-3','','--A',7,'1600097231','','41185','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Parallilism out of specification (0.05mm T0 0.3mm)','Flatness as per drawing is 0.05mm and due to bend and also twist in part. 0.05mm flatness\r\nnot achieved.','After checking the flatness, New process planed and run. but not avoid bend aging done for both the\r\noperations and checked the flatness. After this process change flatness achieved below drawing\r\ntolerance.','Again change process, proved procss after taken production bath.','CA/PA found satisfactory.','','2015-05-22','Rangaswamy()','Gurukiran S M,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','MakinoF3','Manjunath(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8541,'35-299','Saab AB','SERRATED PLATE','564847A2','425Z0312-4','','--A',14,'1600097231','','41178','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Parallilism out of Tolorance(0.05mm T0 0.3mm)','Flatness as per drawing is 0.05mm and due to bend and also twist in part. 0.05mm flatness\r\nnot achieved. ','After checking the flatness, New process planed and run. but not avoid bend aging done for both the\r\noperations and checked the flatness. After this process change flatness achieved below drawing\r\ntolerance.','Again change process, proved procss after taken production bath.','CA/PA found satisfactory.','','2015-05-22','Rangaswamy()','Umesh B,Manohara B.C.,Gurukiran S M,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','MakinoF3','Manjunath(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8542,'35-299','Saab AB','SERRATED PLATE','564847A2','425Z0312-4','','--A',2,'1600098209','','41179','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Parallilism out of Tolorance(0.05mm T0 0.3mm)','Flatness as per drawing is 0.05mm and due to bend and also twist in part. 0.05mm flatness\r\nnot achieved. ','After checking the flatness, New process planed and run. but not avoid bend aging done for both the\r\noperations and checked the flatness. After this process change flatness achieved below drawing\r\ntolerance','Again change process, proved procss after taken production bath.','CA/PA found satisfactory.','','2015-05-22','Rangaswamy()','Manohara B.C.,Gurukiran S M,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','MakinoF3','Manjunath(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8543,'35-299','Saab AB','SERRATED PLATE','564847A2','425Z0312-4','','--A',2,'1600098209','','41521','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Parallilism out of Tolorance(0.05mm T0 0.3mm)','Flatness as per drawing is 0.05mm and due to bend and also twist in part. 0.05mm flatness\r\nnot achieved.','After checking the flatness, New process planed and run. but not avoid bend aging done for both the\r\noperations and checked the flatness. After this process change flatness achieved below drawing\r\ntolerance. ','Again change process, proved procss after taken production batch','REV to be changed if the process is changes!','','2015-05-22','Rangaswamy()','Umesh B,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','MakinoF3','Manjunath(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8544,'35-059','Saab AB','7605198-201','8-42-06609-2','L574 55198 201','ABS 5125 A 016','C',1,'1600076911','','40413','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','yes','Steps notes on faces. ','During receiving inspection found mismatch then NCR was raised.','After reviewed and found within specification limit.','Qlaity alert dispalyed for the acceptance criteria in the receiving inspection.','CA/PA found satisfactory.','','2015-05-22','Avinash(R.J.)','Manjunath(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','With Treatment','17446','Post DN','no','Misc','Avinash(R.J.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8545,'35-059','Saab AB','7605198-201','8-42-06609-2','L574 55198 201','ABS 5125 A 016','C',1,'1600101615','','41238','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Steps notes on faces. ','Mismatch noticed after surface treatment.','1)Quality alert displayed in the final inspection area about the acceptance criteria.\r\n2) Informed to fitting and production about this issues.\r\n3) If in case we find any mismatch then we will smoothened in the bench work.\r\n','1) If in case we find any mismatch then we will smoothened in the bench work.\r\n','CA/PA found satisfactory.','','2015-05-22','Avinash(R.J.)','Manjunath(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','17447','Post DN','no','Misc','Avinash(R.J.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8546,'28-004A','Magellan Aerospace New York  Inc.','PIN','G17210','161A2332-1','15-5PH Steel Bar per','NA',1,'128068-3172','','43322','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','dia 47.38 undersized by 0.006 to 0.01.','In OD roughing setup running time insert will be breakage and part will OD oversize and that part not checking the operator and part not maintain in proper stock for finishing tool. So in the finishing setup that part loading time finishing tool get the more stock and coolant flows not correctly and chips will be over lapped in the outer diameter and part will be -.006to0.01 micron under\r\nsized.  \r\n','After roughing check the diameter and maintain the proper stock for the finishing tool and run the part and adjust the coolant in insert edge coolant will be avioded the chips over lapping and every 15 to 20 ns change the finished insert tip and run the part so this problem not repeated again . ','After roughing check the diameter and maintain the proper stock for the finishing tool and run the part and adjust the coolant in insert edge coolant will be avioded the chips over lapping and every 15 to 20 ns change the finished insert tip and run the part so this problem not repeated again .  \r\n','CAPA found okay','','2015-05-22','Dinakar(K)','KRISHNAMURTHY(N)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','13','no','Misc','Sandhesh D(S)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8547,'18-641A','Magellan Aerospace Wrexham','BOLT SPECIAL','B2241A','L575 55266 200','','A00',1,'RP134149 Amnd 1','','43795','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','OD undersize.','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.','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','CA/PA found satisfactory.','','2015-05-22','Dinakar(K)','Sandhesh D(S)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','01','no','Misc','Sandhesh D(S)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8548,'18-317A','Magellan Aerospace(Chalfont) Limited','PIN SIDE ROLLER','A0729X','F579 53066 200','S145','C',9,'P/074118','','42625','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','1) 5nos drill brocken.\r\n2) 4nos face groove chattering noticed. ','1)sumitomo drill trialed used 50nos run 1st dril broken rpm feed not set,2nd drill 150nos run and broken.  \r\n2)Face grooving tool problem after running for several number of parts.  \r\n','1)Rpm feed adjust the sumitomo person and set feed and rpm drill life 300nos. 2)Grooving Tool has kept in stock, Operator should watch the tool in regular intervals and should change if any deviation is found.  \r\n \r\n','1)Rpm feed adjust the sumitomo person and set feed and rpm drill life 300nos.2)Grooving Tool has kept in stock, Operator should watch the tool in regular intervals and should change if any deviation is found.  \r\n  \r\n','CAPA found okay','','2015-05-22','Dinakar(K)','Nataraja C V,Manjunatha N,Manjunath  M,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','3','no','QT100S-1','Sandhesh D(S)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8549,'18-091A','Magellan Aerospace Bournemouth','BUSH','K13746','D278 50164 202','S80 FHT','A',3,'RP400843','','43697','','0000-00-00',NULL,'yes','yes','yes','','','','','','','OD undersized by -0.006micron.','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\r\nand chips will be rubbed in the outer diameter and part will be -.006 micron under sized. So part will become rejected.  \r\n','checking the all parts outer and inner diameter before loading in the finished setup and change the previous insert 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 15 to 20 ns chnge the finished inserttip and run the part so this problem not repeated again.  \r\n','In roughing setup for every part check outer and inner diameter for using air gauge. In finishing set up 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 okay','','2015-05-23','Dinakar(K)','                Dinakar K','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8550,'35-177','Saab AB','ALCD_STRUCT_BEAM-LOWER_OU','582084','423Z1404-5-02','','---',1,'1600082632','','42661','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Tool dig mark on base thickness.','While doing firstoff part in operation-02, operator not taken the Z-offset correctly for dia 3ballnose.\r\nOffset wrongly taken and started machining. due to offset mistake tool dig mark observed on part base(near to countersink)','Tool offset corrected and checked all the tools which is running for this part and all are found ok.\r\nNext part machined and found ok, Production continued.','Informed to operators to take the work offset correctly and crosscheck once before running the program.','Next part produced correctlly and CA/PA found satisfactory.','','2015-05-23','Krishna(Chowdary.G.P.)','Rangaswamy()','','0000-00-00','Tool dig mark on base thickness.','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Girish(Prasad P)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8551,'35-189','Saab AB','INTERCOSTAL_MIDSPAN_NO_2 ','599430','423Z1170-1-06','','---',1,'NOV 2014 ','','42311','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Part rib top face tool dig mark.','While doing setting in operation-05, operator not setted tool overhang correctly, Therefore holder touches and rib and dig mark observed on rib top.\r\n','After observing the dig in first off part,All the tool overhang cross checked and then next part proved and inspected and then production continued.','Informed to operator to check the tool overhang as per MPS and also cross check with machine reference book.\r\nThis is done mandatory to check the tool overhang for all the part.','Next part produced with any defect CA/PA found satisfactory.','','2015-05-23','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Rangaswamy()','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8552,'18-229B','Magellan Aerospace Bournemouth','CLAMP STRIP TOP OUTBD','447190','L572 52377 200','ABM3 1029','B00',1,'RP401009','','43808','','0000-00-00',NULL,'yes','','yes','','','','','','','Total width 0.2 mm minus.\r\n','Due to part running time part bend  observed. So center of the part width minus side measured.','Another part running time before bend removing after finish the outer profile and width dimension.\r\nInform the operator every time part 2nd operation completed after remove bend then finish the final operation. ','Inform the operator every time part 2nd operation completed after remove bend then finish the final operation. ','CAPA found okay','','2015-05-23','','                Diwakar R.B.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8553,'18-090A','Magellan Aerospace Bournemouth','BUSH','K10011','D278 50164 200','S80 FHT','A',1,'RP400843','','43694','','0000-00-00',NULL,'','','yes','','','','','','','running time power trip O.D dig mark .... ','','','','Part accepted.','','2015-05-23','','        Manjunatha N','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8554,'35-298','Saab AB','SERRATED PLATE','564847A2','425Z0312-3','','--A',5,'1600098209','','43460','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','PARALLISM OUT OF TOLARANCE(0.05 TO 0.3)','Flatness as per drawing is 0.05mm and due to bend and twist in part after machining, \r\n0.05mm flatness not achieved.\r\n ','1.Planned to create flatness by machining both the sides in thickness and also blue match the butting face of the part to get the flatness after serration machining.\r\n2. serration depth of cut reduced to reduce load on part while machining.\r\nThe above CA/PA actions planned to reduce deviation in next batch production.\r\n','1.Planned to create flatness by machining both the sides in thickness and also blue match the butting face of the part to get the flatness after serration machining.\r\n2. serration depth of cut reduced to reduce load on part while machining.\r\nThe above CA/PA actions planned to reduce deviation in next batch production.','CA/PA Found OK.','','2015-05-25','Rangaswamy()','Umesh B,Gurukiran S M,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','MakinoF3','Manjunath(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8555,'18-186A','Magellan Aerospace Bournemouth','BUSH','P1631','L575 50336 200','B23','B00',29,'RP401024','','39822','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','This 30-nos were batch mix up during the tenure of Operator Girish and as safety Srikanth G S has taken a decision to scrap these without looking further into the details','Not required','Just informed about the improtance of batch mixing.','Not required','Not REQUIRED','','2015-05-25','Dinakar(K)','Girish V(M)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','04','no','Misc','Avinash(R.J.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8556,'18-120C','Magellan Aerospace Bournemouth','HOUSING OUT B D BRG 3','CB872484','D275 56121 200','','E01,  ECN NG27011ST1KA83',2,'RP400843','','42979','','0000-00-00',NULL,'','','yes','','','','','','','While running part rotated, So OD u/s (-0.015)','In 2nd set up bore diameter is maintained not controlled 0.05mm plus side.in finishing operation fixture is not tigtend correctly so part will rotate.when part rotated OD will undersize.  \r\n','For next  production batch is conbtrolled bore diameter and change diameter for next operation purpose.','For next  production batch is conbtrolled bore diameter and change diameter for next operation purpose. \r\n','CAPA found okay','','2015-05-25','','                Bharath R','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8557,'18-091A','Magellan Aerospace Bournemouth','BUSH','K13746','D278 50164 202','S80 FHT','A',1,'RP400843','','43698','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','part wrong loading, ','In finishing operation 2ODs are finished in one setup first side OD finished and that part to be reversed.but loaded new part so od dig mark and part came out from the jaws.  \r\n','For next part jaws bored neatly and inserts are changed and taking x&z offset and run the part after finishing first set up OD,reverse that part and 2nd od finished part found okay and continue the production.  \r\n ','Instructed to all operators to cross check the part whether the operation is completed or not before\r\nloading another part.  \r\n','CAPA found okay','','2015-05-26','Dinakar(K)','Devaraj(K.C.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','03','no','Misc','Sandhesh D(S)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8558,'18-091A','Magellan Aerospace Bournemouth','BUSH','K13746','D278 50164 202','S80 FHT','A',1,'RP400843','','43697','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','running time part rotated, so od dig mark.','More stock in the finishing part so Part running time part will be rotated so dig mark observed in the outer diameter so part will be rejected.  \r\n','same stock given to the all finished parts setting the Proper pressure and skin cut given to the jaws and change the insert corner and 0.4 plus taken to the wear offset and run the part and then check the part and proper currection given in wear offset and run the part then part inspection done part checked found ok.','after the roughing setup for finishing only 0.3 stock maintain in the all the parts and set the proper and same pressure for all times.  \r\n','CAPA found okay','','2015-05-26','Dinakar(K)','Vasu(SN)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','03','no','Misc','Sandhesh D(S)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8559,'35-176A','Saab AB','LATCH_ACT_PIVOT-FTG ','593778','423Z1205-2-02','','--B',1,'May 2015','','41809','','0000-00-00',NULL,'yes','no','yes','no','yes','no','no','no','no','Total length minus (-0.05mm) & position not achived.','While running operation-05 operator not taken offset correctly.\r\n0.1mm wrong correction given in Z-Axis by manual error.\r\n\r\n','After checking the first off part. operator changed the correction and then checked the thickness and after approving from QAD, production continued.','This rejection is due to manual error, Explained to operator regarding the process.\r\nNext batch 50nos production done with out correction and all the parts total length checked and all are found ok.\r\n','CA/PA found satisfactory.','','2015-05-26','Rangaswamy()','Gurukiran S(M)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Rangaswamy()','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8560,'35-288','Saab AB','BEAM FITTING','755659A0','424Z1140-2','','--B',1,'1600102067','','42656','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','* Tool dig mark on base, In dig area base thickness is -0.12(Crossed out of tolerance)','While doing first off part in operation-02, operator not taken the Z-offset correctly for dia\r\n 10r3 bullnose. Offset wrongly taken and started machining. due to offset mistake tool dig mark observed\r\n on part base.','Tool offset corrected and checked all the tools which is running for this part and all are found ok.\r\n Next part machined and found ok, Production continued.  ','Informed to operators to take the work offset correctly and crosscheck once before running the program.   ','Next part found ok.','','2015-05-27','Girish(Prasad P)','Mahesh N,Karthineyan V.S.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','A51nx-1','Manjunath(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8561,'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 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. ','','2015-05-27','Avinash(R.J.)','Nandishkumar(D.K.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','18002','POST DN','yes','Misc','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8562,'18-082A','Magellan Aerospace Wrexham','STUD PLATE','281099/001','D278 50007 200','ABM3 1029','D01',1,'RP135247','','43869','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Base thickness minus 0.3 mm','While operator work offset \"Z\" taken time operator not check the tool wear. So base thickness minus.\r\n  ','Re-check the work offset, after continue the production.\r\nInstructed to operator every time work offset taken time cross check the wear offset.\r\n','Instructed to every operator 1st part work offset taken time check the wear dimension in tool wear.  ','CAPA found okay','','2015-05-27','Anjinamurthy(H)','        Manohara M','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8563,'18-414B','Magellan Aerospace Bournemouth','ACTUATOR HOUSING','95744A','D278 50163 200','','D',1,'RP401021_Amnd No. 1','','41595','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','yes','Machine abuse observed on part surface.','Rust preventive oil Evaporated during the time gap for taking the process. That leads to black marks and that marks not passed the Machine abuse check.','We informed to treatment house and also taken care to apply PX24 more before send to treatment.','Same as above.','Next batch found satisfactory.','','2015-05-27','Avinash(R.J.)','Nandishkumar(D.K.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','18206','POST DN','yes','Misc','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8564,'18-186A','Magellan Aerospace Bournemouth','BUSH','C3348','L575 50336 200','B23','B00',1,'RP401024','','43852','','0000-00-00',NULL,'yes','no','no','no','yes','yes','no','no','no','ID Oversize 0.010 mm.','After running 50 to 60 parts insert tip will be worn out and running time chips not breaking properly so chips will rubbing inside the part and diameter will be oversized in the running part. \r\n','Remove the worn out insert and replace the new insert and newely offset taken and 0.2 (-) minous taken in the tool wear offset and run the part and then check the inner diameter and give the correction in wear offset and adjust the coolant correctly and run the part and checked found ok.  ','while setting time loading the new insert before running and after every 100 nos change the roughing insert and run the part.and every 25ns onece observe thetoolnoise,coolant floaing and chips while running.  \r\n','CAPA found okay','','2015-05-28','Dinakar(K)','Seetharamu D,Ashith B,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','FI','no','DX 200-2 ','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8565,'18-116B','Magellan Aerospace Bournemouth','ASSEMBLY FORKEND','96287','F575 51377 200','','A',4,'RP400841','','43735','','0000-00-00',NULL,'','','yes','','','','','','no','Repeatability not found in the reamer. DIA +side','Due to not getting repeatablity in the Reamer dia found plus side, ','Reamer has been replaced by interpolation and parts found okay and production is carrying out','Reamer has been replaced by interpolation and parts found okay and production is carrying out','CAPA found okay','','2015-05-28','','        Ravi R','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8566,'18-077A','Magellan Aerospace Wrexham','COUPLING ','4023','D282 50075 200','','A',1,'RP125890','','43706','','0000-00-00',NULL,'','','yes','','','','','','','Deburr champer dig mark.','For first part,part butted to part face and complete all operation 0.2 face out come to avoid that face out one bush inseeted in the part and part butted to that bush face and run the next part.profile chamfer tool offset not taken and run the chamfer program.bushing collar width is 1mm and part 1mm came outside and chamfer 1mm more.so instead of deburr chamfer, 1mm chamfer appear on the part so part reject.','chamfer tool offset taken and run the part.','Instruction given to operator to take offset for all the tools whenever you disturb the previous setting or change the setting.','CAPA found okay','','2015-05-29','','        Shivanand D.B.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8567,'18-098B','Magellan Aerospace Bournemouth','VALVE- SEAT','66894/01/00','D282 50060 204','','D',2,'RP400844','','43169','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Part bend observed.','While part final operation (top facing) running time part bend so part running time lifted. ','Inform to operator before load the part check the bend. Every part loading time clean the surface after load the part. When part bend observed immediately inform to concern supervisor.','Inform to operator before load the part check the bend. Every part loading time clean the surface after load the part. When part bend observed immediately inform to concern supervisor.','CAPA found okay','','2015-05-29','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','00','no','Misc','Lohith(K)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8568,'35-165A','Saab AB','HOUSING PIN','427286','423Z1124-5-01','','--A',1,'1600078597','','41831','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Total theckness under size 104.55+/-0.25 mesured 104.15 to 104.19.','This NC for operator negligence, because operator not clean  part butting face or fixture top face ,one end thickness nominal measured and other end 0.2mm mines side because chips lock in part butting face.so thickness minus.','This part after operation completed, then operator dimension checking time observed, so analyse the problem & clean fixture top then production run. ','Informed to operator every time before loading the part clean fixture top surface .','CA/PA found satisfactory.','','2015-05-29','Krishna(Chowdary.G.P.)','Krishna(K)','','0000-00-00','Total theckness under size 104.55+/-0.25 mesured 104.15 to 104.19.','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','04','no','Misc','Girish(Prasad P)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8569,'18-031A','Magellan Aerospace Bournemouth','BLANKING PLUG','223981','D278 50157 200','S130 FHT','H01',5,'RP400838','','42553','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','OD Thread NOGO 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. ','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','CAPA found okay','','2015-05-30','Dinakar(K)','Shivanand D.B.,SHIVAKUMAR ,Raghavendra Rao R,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','ST20Y1','Narasimha Murthy(R)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8570,'42-002','RAFAEL','PSA BASE','K10597','BA1E2001B','','38-576104_Rev-E, TILDOCS#172373_Rev-13, RE_804-1-5_Rev-11, 111.21_Rev-6, 23.36.59_Rev-F, ECN 57176 2014/08 /25; ECN 58483  2014/07/29',1,'347592024','','43111','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','Wrong imformation given cad department so part base thickness minus 0.3mm.','Part was rejected due to Process changed Datum face stock created but Fixture not reworked\r\n','Fixture  reworked as per new process (Datum stock removed on fixture plate) part fond OK\r\n','Before loading the part ensure the fixture and part butting face.\r\n','CAPA found okay','','2015-06-02','Ramesh(Poojary)','Ramesh(Poojary)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','00','no','Misc','Basavaraja S.(Jr.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8571,'35-297','Saab AB','HINGE FITTING','755659A0','425Z0311-12','','---',1,'PA 1510 NEW PARTS-2','','43216','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','*Rib thickness and Base (Serration) thickness is crossed out of tolerance up to -0.5 mm. ','First part proved & found ok , but production running time one part base thickness minus because of part not butting properly so thickness minus side.','In 03 operation run first program in dia 16 fl, after this tool insert M00 in next program because after first program chances of part lifted ,so once again mallet.   ','M00 insert in program, after first program once again mallet. ','CA/PA found satisfactory.','','2015-06-03','Girish(Prasad P)','Shivashankar H.G.,Mahesh N,Karthineyan V.S.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','A51nx-1','Manjunath(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8572,'18-407A','Magellan Aerospace Bournemouth','STIFFENER EDGE BEAM','404744','L575 53248 200','','A00',1,'RP401021_Amnd No. 1','','36712','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Hole position out of tolerance.','Due to reamer run out in the holder, hole position was out of tolerance \r\n','Next changed the holder then checked the run out by plunger dial the run out is 0.001 mm then continue the production\r\n','Instructed operator to first time proving the first part will checked the run out of the reamer before run the tool.This message entered in the program. \r\n','Next batch found okay\r\n','','2015-06-03','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','Hole position out of tolerance.','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Girish(Prasad P)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8573,'35-292','Saab AB','BEAM FITTING','434837','424Z1144-2','','--B',5,'May 2015-2','','42816','','0000-00-00',NULL,'no','no','no','no','no','no','yes','yes','yes','*Florescent Penetrant Inspected Failed.','Dent marks observed on the butting face and it is very small dent it is not identify by only eye. ','Given the instruction to inspector to perform the usual inspection under the more light focus area and if any difficulties to judge plaese check that part using magnifing glass.','Given the instruction to inspector to perform the usual inspection under the more light focus area and if any difficulties to judge plaese check that part using magnifing glass.','Next batch parts FPI inspection 100% passed.','','2015-06-03','Avinash(R.J.)','Manjunath(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','18049','Post DN','yes','Misc','Nagaraj(G. Nadiger)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8574,'18-383A','Magellan Aerospace(Chalfont) Limited','SLEEVE BEARING ','Y11518','D575 40037 202','','A',2,'P/078238','','44073','','0000-00-00',NULL,'','','yes','','','','','','','running time part rotate so t/l (-)side 0.1mm ','In 2nd set up thickness is maintained 0.1mm plus side.in finishing operation more stock measure part will rotate.when part rotated OD will undersize.  \r\n','For next part check the thickness and any deviation came that will be adjusted in work offset and run the part.  \r\n','For next part check the thickness and any deviation came that will be adjusted in work offset and run the  part.instructed to operators to check the dimension of 2nd set up before loading the part. \r\n','CAPA found okay','','2015-06-03','','        Nataraja C V','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8575,'35-242','Saab AB','BUSHING ','1465374','423Z1416-2','','---',6,'PA 1510 NEW PARTS-1','','39914','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','ID Radius not formed correctly.','Due to part inside radius finishing time tool composition not given. This error happen operator mistake. ','Informed to operator when setting time check the tool composition and direction before run the part.   ','Next batch production we are mention the tool and tool corner radius in the program. ','Next parts found okay.','','2015-06-04','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','3','no','Misc','Narasimhamurthy(K.G.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8576,'18-226B','Magellan Aerospace Bournemouth','BRKT - NUT RETAINER','10162768-A','F572 53828 200','','A',1,'RP400846','','41854','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Brouched width oversize.','broacing 1st time prooving time in st20 broaching diameter oversize.','next part offset -taken in wear offset and run the part and checking broaching diameter correction given to wear offset & run the part part found ok.','next batch instruction given to operator every batch setting time offset - taken in wear offset and run the part.','CA/PA found satisfactory.','','2015-06-04','Dinakar(K)','SHIVAKUMAR ,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','9','no','ST20','Dinakar(K)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8577,'18-226B','Magellan Aerospace Bournemouth','BRKT - NUT RETAINER','10162768-A','F572 53828 200','','A',2,'RP400846','','41852','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','0.4mm brouched surface offside.','broacing 1st time prooving time in st20 broaching diameter oversize. ','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. ','next batch instruction given to operator every batch setting time offset - taken in wear offset and run the part. ','CA/PA found satisfactory.','','2015-06-04','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','9','no','Misc','Dinakar(K)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8578,'18-009A','Magellan Aerospace Wrexham','Plate Cover','497610','D572 52519 200','L97 T351','A',1,'RP125888','','44038','','0000-00-00',NULL,'yes','yes','yes','','','','','','','part reversed when M00 came but reset the program and run from starting program so drilling opn done in both side  so part reject.','In this operation after turning and drilling operation M00 will come and reverse the part for facing and chamfer operation part reversed when M00 came but reset the program and run the program again turning and drilling instead of facing and chamfer.so both side drilling operation done so part reject.','For next part, part revesed and not reset the program and run the facing and chamfer program(next opn).','Instruction given to operator to follow the messages given in the program and run the program as per message and where M00 came check the part and program before run the part.','CAPA found okay','','2015-06-04','Dinakar(K)','                Shivanand D.B.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8579,'18-226B','Magellan Aerospace Bournemouth','BRKT - NUT RETAINER','10162768-A','F572 53828 200','','A',1,'RP400846','','41854','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Dimension 35.1mm to 35.4mm measures 35.8mm.','broacing 1st time prooving time in st20 broaching diameter oversize','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. ','next batch instruction given to operator every batch setting time offset - taken in wear offset and run the part. ','CA/PA found satisfactory.','','2015-06-04','Dinakar(K)','SHIVAKUMAR ,Raghavendra Rao R,Diwakar R.B.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','ST20','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8580,'18-226B','Magellan Aerospace Bournemouth','BRKT - NUT RETAINER','10162768-A','F572 53828 200','','A',1,'RP400846','','41852','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Dimension 35.1mm to 35.4mm measures 35.60mm.','broacing 1st time prooving time in st20 broaching diameter oversize','next part offset -taken in wear offset and run the part and checking broaching diameter correction given to wear offset & run the part part found ok. ','next batch instruction given to operator every batch setting time offset - taken in wear offset and run the part. ','CA/PA found satisfactory.','','2015-06-04','Dinakar(K)','Shivanand D.B.,S. Shiva Kumar,Mohan Kumar C.M.,Lohith K,Girish HP,Diwakar R.B.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','ST20Y1','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8581,'18-596A','Magellan Aerospace Wrexham','FITTING AFT INBD','4527101','L575 52000 201','','A',2,'RM132918 Amnd 1','','42907','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','FAI part Hole position not achieved.','3 Datum Single Setup not Finished, Hole position not achieved','3 Datum Faces finished last setup','3 Datum Faces finished last setup Or Single Setup for All Parts','CAPA found okay next parts found good','','2015-06-04','Ramesh(Poojary)','Rangaswamy()','','0000-00-00','Position not achieved.','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Rangaswamy()','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8582,'18-598A','Magellan Aerospace Wrexham','FITTING FWD INBD','4527101','L575 52001 201','','A',2,'RM132918 Amnd 1','','42909','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','FAI part Hole position not achieved.','3 Datum Single Setup not Finished, Hole position not achieved','3 Datum Faces finished last setup','3 Datum Faces finished last setup Or Single Setup for All Parts','CAPA found okay next parts found good','','2015-06-05','Ramesh(Poojary)','Ramesh(Poojary)','','0000-00-00','Position not achieved.','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Rangaswamy()','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8583,'18-597A','Magellan Aerospace Wrexham','FITTING FWD INBD','4527101','L575 52001 200','','A',2,'RM132918 Amnd 1','','42908','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','FAI part Hole position not achieved.','3 Datum Single Setup not Finished, Hole position not achieved','3 Datum Faces finished last setup','3 Datum Faces finished last setup Or Single Setup for All Parts','CAPA found okay next parts found good','','2015-06-05','Ramesh(Poojary)','Rangaswamy()','','0000-00-00','Position not achieved.','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Rangaswamy()','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8584,'18-578A','Magellan Aerospace Wrexham','FITTING DRIVE SHAFT','6950401','L575 51861 201','','B00',1,'RM132921 Amnd 1','','42605','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Hole dia over size.','While running FAI part, dia 9.8 +0.015mm hole measures 9.82mm for a depth of 5mm in 10mm through hole.\r\nNew reamer ordered and operator not checked the tool runout before proving the reamer in part.\r\nImmedeately runout checked and found problem.(0.04mm runout observed), then removed the tool and cleaned the tool holding area and clamped again and checked.After reclamping 0.015mm runout observed and then reamer proved with dunny block.','After proving the tool with dummy block new part manufactured and next FAI part found ok.\r\n','Informed to tools supervisor and machine supervisor to prove the new reamer with dummy block before running the part.\r\ncheck the runout for every batch production for proved tools.\r\n','CA/PA Found satisfactory.','','2015-06-05','Ramesh(Poojary)','Rangaswamy()','','0000-00-00','Hole dia over size.','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Rangaswamy()','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8585,'18-102A','Magellan Aerospace Bournemouth','BARREL-STRUT','247348','D572 50463 200','S98 FHT','F',1,'RP400839','','42556','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','ID Thread NOGO answered.  \r\n','Thread was damaged due to wear out of inserts. Bcause machine cenre height not correct.The operator intended to rework the damaged thread resulting in non conformance of ID.  ','Insert was worn out at that stage which was replaced for the next job and adjusted the machine centre heigt to extend the tool and insert life.  \r\n','The block holding the tool shall be set by the Supervisor for every batch which is expected to extend the tool life and reduce these type of non conformances and supervisors give to training to operators.  \r\n','CAPA found okay','','2015-06-05','Dinakar(K)','Rajesh B D,Manjunatha N.R.,KRISHNAMURTHY N,GUNDEGOWDA H.G.,Diwakar R.B.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','FI','no','DX 200-3','Narasimha Murthy(R)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8586,'18-117B','Magellan Aerospace Bournemouth','HOUSING-OUT BD BRG','K10257','D275 40004 200','','C01',2,'RP400841','','42538','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Thread effective diameter oversize.  \r\n','Due to operator not checked in the m/c.  \r\n','Next production batch will be rework compelted.  ','Instructed operator to every part checked in m/c then remove the part.  \r\n','Rework done CAPA found okay','','2015-06-06','Ravi(M)','Ravi(M)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Manufacture Only','','05','yes','Misc','Ravi(M)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8587,'18-117B','Magellan Aerospace Bournemouth','HOUSING-OUT BD BRG','K10257','D275 40004 200','','C01',1,'RP400841','','42537','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','I.D over sized..  \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 \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.','','2015-06-06','Ravi(M)','Vasu SN,Bharath R,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','5','no','QT100S-2','Ravi(M)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8588,'18-110A','Magellan Aerospace Bournemouth','FORK END INTERMEDIATE','238302','D575 40494 202','S80 FHT','J',2,'RP400840','','42884','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Thread effective diameter oversize.','Due to operator not checked in the m/c.  \r\n','Next production batch will be rework compelted.  ','Instructed operator to every part checked in m/c then remove the part.  \r\n','Rework done CAPA found okay','','2015-06-06','Dinakar(K)','Shivanand D.B.,Ravi R,Rajesh B D,Raghavendra Rao R,Mohan Kumar C.M.,Manohara M,KRISHNAMURTHY N,GUNDEGOWDA H.G.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Manufacture Only','','FI','yes','ST20','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8589,'18-378B','Magellan Aerospace Bournemouth','GAMMA FITTINGS ','M590350 97022','NSA840020-250','','L',3,'RP401480_Amend No.-1','','40247','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','G dimension -0.025    ( 2 degree angle rewoking time od undersize)','','','','Parts accepted.','','2015-06-06','Ravi(M)','Krishnanaik J N,Dinakar K,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','Manufacture Only','','3','no','QT100S-4','Ravi(M)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8590,'18-376B','Magellan Aerospace Bournemouth','GAMMA FITTINGS ','4659','NSA840020-150','','L',5,'RP401478_Amend No.-1','','42247','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Total length undersize.  ','In first set up face was unclear thats why 0.2mm given in work offset and run the part part found ok. and in second set up 0.2mm not taken plus side in work offset so thickness 0.2mm under size.  \r\n','Jaws bored neatly where the partface was butted to jaws and clamped on od and taking offset run the part ,part found ok and contionue the production.  ','Instruction given to operator to where the thickness is maintained for have to butt that face in the jaws not in the starting face.  \r\n','CAPA found okay, next parts found okay','','2015-06-06','Ravi(M)','Sathish G,Manjunatha P,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','5','no','EMAG-1','Ravi(M)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8591,'35-185','Saab AB','CED_LATCH_SERRAT_ED_PLATE','564847A2','425Z0610-17','','---',1,'1600067952','','43224','','0000-00-00',NULL,'','','yes','','','','','','',' running time part lifted,vacuum holding not properly. ','This part operation 05 running in vacuum fixture,this operation finish in dia 6.35 hole & serration. in this setup hole not opened, because holding in vacuum presser.but one  part hole opened,because 1st operation in vice , after operation part bend coming, this setup effected ,so part lifted.','Dia 6.35 hole finish,  using dia 5fl tool, so this tool 0.1mm up  in tool wear,so hole not opened. run production.','After first operation completed blue match in operation 03 butting face,so butting face properly butted.','CAPA found okay, next parts found okay','','2015-06-07','','        Shivashankar H.G.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8592,'28-003A','Magellan Aerospace New York  Inc.','PIN-ATTACHMENT WALKING BE','970608-03','161A7305-1','','PL-Rev-NC, DL Rev-B',1,'126999_R0_C1','','43768','','0000-00-00',NULL,'','','yes','','','no','','','','tool number  not changed , instead of threadding tool turning tool done the threadding operation so thread major dia undersize & thread nogo answered.','After threadding operation grooving operation is done to remove burr.after grooving threadding operation is done because to enter gauge freely at the end for first part tool no not entered corectly for threading in last pass.instead of tool not entered tool no 8.tool no 8 is od finishing tool so finishing toll done the threadding opern/ so major dia undersize and thread nogo answerd.','For next part change the tool number and run the part.','Instruction given to operator to check the tool and tool number in the turret and enter same tool number correctly in the program and cross checked the tool whether for an enter correctly or not in the program before running the part.','CA/PA found ok','','2015-06-07','Sandhesh D(S)','        Dinakar K','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8593,'18-380B','Magellan Aerospace Bournemouth','GAMMA FITTINGS ','M526650 91696','NSA840020-350','','L',1,'RP401481_Amend No.-1','','43400','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','0.5 grooving insert break down so part od groove dig mark.\r\n','The Following route cause analyzed for the parts rejected, 1. Ovality in RM. 2. Total Length Minus in RM. 3. Improper Butting in Jaws. 4. Jaws Boring is not good( Flatness is not achieved. 5. RM unclear on OD and ID. 6. Ovality More than 0.05mm in billet stage. 7. Chips clocking at the Jaws , In Part butting faces. 8. Roughing and Finishing inserts wear out.','The Following CA/PA taken to avoid the rejections, 1.Sizes and Tolerance for Roughing stage.(Sample parts made to check the parts visually also for reference) 2. Compulsorily use 6-Jaw chuck for all the Gamma for both roughing and Finishing operations. 3.Plan for Parts to be inspect for Face out and Ovelity before loading for finishing operations. 4.Methods of tightening the part\r\non to the Mandril in operation-02. 5.create the rough surface on OD in roughing operation to strengthening the clamping.','The Following CA/PA taken to avoid the rejections, 1.Sizes and Tolerance for Roughing stage.(Sample parts made to check the parts visually also for reference) 2.  compulsorily use 6-Jaw chuck for all the Gamma for both roughing and Finishing operations. 3.Plan for Parts to be inspect for Face out and Ovelity before loading for finishing operations. 4.Methods of tightening the part\r\non to the Mandril in operation-02. 5.create the rough surface on OD in roughing operation to strengthening the clamping. ','CAPA found okay','','2015-06-07','Sandhesh D(S)','Dinakar K,Chandre  Gowda,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','1','no','QT100S-4','Narasimhamurthy(K.G.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8594,'18-443A','Magellan Aerospace Wrexham','2.0','4760','L280 50067 206 PF','','A00',2,'RP137240 Amnd 1','','44110','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','profile out problem.','program problem so editing the program that time program profile problem occurred.  \r\n','editing the program and run the part and check the angle and radious and part found ok and run the production.','editing the program and run the part and check the angle and radious and part found ok and run the production.and that same program save in the system that same program run for next every batch.  \r\n','CAPA found okay','','2015-06-08','Dinakar(K)','Dinakar K,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','3','no','QT100S-3','Dinakar(K)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8595,'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','','43710','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','DUMMY','','','','DUMMY','','2015-06-08','Rangaswamy()','Umesh(B)','','0000-00-00','Dia 15.895 bore 30 micron over size.','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','Manufacture Only','','07','no','Misc','Rangaswamy()','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8596,'34-015B','Magellan Aerospace Winnipeg','MOUNTING LUG- STRUT / STD','A1303X','400-12607-1-905','','EM104302 Iss A, EM104765 Iss G, EM105092 Iss F, EM106399 Iss B, EM106400 Iss B, EM106401 Iss A, EM106404 Iss A, EM106522 Iss A, EM106602 Iss A',1,'B91379 Rev.026','','43710','','0000-00-00',NULL,'','yes','yes','','','yes','','','no','part bore (+) side in 0.03  ','This part bore finish in CRC program, using 10fl for bore finish.this time operator CRC value wrong enter ,so part rejected. ','Enter correct value run production,71nos found ok.','Warning letter issued to operator, explain crc value & explain crc program.\r\n','Warning letter issued, next parts found okay by same operator','','2015-06-09','','        Umesh B','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8597,'18-517A','Magellan Aerospace Wrexham','FITTING SPOILER','6772701','L575 51917 201','','A',1,'RM132922 Amnd 01','','43677','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','Bore problem.','Due to reamer run out in the holder. \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 run out of the reamer before run the tool.This message entered in the program. \r\n','Next batch found okay\r\n','','2015-06-09','Rangaswamy()','Rangaswamy()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','5','no','Misc','Rangaswamy()','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8598,'35-266','Saab AB','LATCH PROBE','G21025K06','424Z6101-1','','--A',1,'PA 1510 NEW PARTS-2','','39601','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dia 9.535 hole chamfer over size.','While proving the chamfer,drilling cycle reference point  wrongly entered,so chamfer dig mark observed in dia 9.535 hole, so part rejected.','Production stooped and drilling operation splited in process and program to be validate by CAM and Production supervisor for new setup. ','New setup proved and program validated before running in machine and program proved and saved.','CA/PA found satisfactory.','','2015-06-09','Rangaswamy()','Gurukiran S(M)','','0000-00-00','Dia 9.535 hole chamfer over size.','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','09','no','Misc','Rangaswamy()','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8599,'35-266','Saab AB','LATCH PROBE','G21025K06','424Z6101-1','','--A',1,'PA 1510 NEW PARTS-2','','39601','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dia 6.35 hole over size.','After FAIR, first batch production,first part proving  operator edit reaming  cycle but  enter reference plain value wrong edit so dia 9.30 hole mill plunging in dia 6.35 hole place, so dia 6.35 hole over size, FAIR time hole mill  or reamer not available.','Edit correct reference plain value then run production.','After start FAIR check all tools or hole mills & reamers then proving . ','IN FAIR part also we are producing the part with using this MPS Rev00 and instruction given in datasheet to use the Reamer dia 9.52.CA/PA not satisfy.','','2015-06-10','Rangaswamy()','Gurukiran S(M)','','0000-00-00','Dia 6.35hole over size.','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','09','no','Misc','Rangaswamy()','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8600,'18-444A','Magellan Aerospace Wrexham','2.5','7459','L280 50067 208 PF','','A00',9,'RP137240 Amnd 1','','44264','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','7.35 width not achieved.','program problem so editing the program that time program profile problem occurred.','editing the program and run the part and check the angle and radious and part found ok and run the production.     (wo no 44264)  ','editing the program and run the part and check the angle and radious and part found ok and run the production.and that same program save in the system that same program run for next every batch.   ','CAPA found okay','','2015-06-10','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','3','no','Misc','Narasimhamurthy(K.G.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8601,'18-317A','Magellan Aerospace(Chalfont) Limited','PIN SIDE ROLLER','A0729X','F579 53066 200','S145','C',206,'P/074118','','42624','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Parts sent to without source inspection GET.','Parts were accepted as the parts sent to Treatment house with out source inspection an NC has been raised.','Parts were accepted as the parts sent to Treatment house with out source inspection an NC has been raised.Next time parts will be offered to Source Inspection .','Parts were accepted as the parts sent to Treatment house with out source inspection an NC has been raised.Next time parts will be offered to Source Inspection .','Parts were accepted as the parts sent to Treatment house with out source inspection an NC has been raised.Next time parts will be offered to Source Inspection .','','2015-06-10','Avinash(R.J.)','Vasu SN,Ningaraj A N,Nataraja C V,Manjunatha N,Manjunath  M,Bharath R,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','With Treatment','18160','FI','no','QT100S-2','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8602,'18-561A','Magellan Aerospace Wrexham','SPAR INBOARD OFW','437515A0','L575 51779 201','','B00',1,'RM132919 Amnd 1','','43329','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Hole pitch shifted.','COS Issue-07 was received but have clarification in the COS,Due to urgency profile machining planned to complete the FAI.Part manufactured without drilling holes.\r\nAfter receiving the Calcification from customer planned to finish the drilling holes in jig boring machine..\r\nWhile doing rework in Jig boring machine, Due to manual error this part got rejected.\r\nWhile doing a Hole in the part, datum not fixed properly and causes hole pitch shifted.\r\n\r\n','The FAI part got rejected and then New FAI proved with COS issue-07.\r\nDrilling co-ordinate program taken from CAD and proved in CNC machine. \r\nNew FAI done with WO 44432 and Drilling program added in MPS.\r\n(Datasheet-0215(18-561A-0215-5P66DR-R00)','This error due to manual error, Therefore informed to operator to check the datum in reference sheet and cross check the the Zero values in DRO.\r\nAfter ensuring the zero values in X and Y axis machining should start.\r\n','CAPA found okay next parts found good','','2015-06-10','Krishna(Chowdary.G.P.)','Jayarama(M.B.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Krishna(Chowdary.G.P.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8603,'35-249','Saab AB','STANDOFF','G21441K06','423Z1916-3','','---',1,'May 2015','','43896','','0000-00-00',NULL,'','','yes','','','','','','','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 was tighting using ring gauge(it acts like a lock nut).due to over tighting part was broken in to two parts so part reject.','For next part (all tools are running in ccw direction.so over tighting is not required because part was RH thread and the ring gauge was RH thread so spanner tighting is not reqired.)part was tightened 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 tighting is not required because part was automatically locked so do not use any spanner for tighting just tight the ring gauge with minimum pressure manually.','CAPA found okay, next parts found okay','','2015-06-10','','        Shivanand D.B.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8604,'35-249','Saab AB','STANDOFF','G21441K06','423Z1916-3','','---',1,'May 2015','','43897','','0000-00-00',NULL,'yes','yes','yes','','','','','','','While running time part small diameter 4.825 broken so part reject.','Roughing insert changed & x offset taken & when offset taken time spindle rotated in cw direction that time part loosen & 4mm came out from the fixture & roughing tool running time tool came & hit the part that time 4.825dia broken.','For next part x & z offset taken for all tools & run the part , part found ok then continued the production.','Instructions given to operator that for crn 35-249 donot rotate the spindle in cw direction because when it rotates in cw direction part loosend from the fixture & above deviation occur , to avoid this deviation rotate the spindle in ccw direction. ','CAPA found okay, next parts found okay','','2015-06-10','Dinakar(K)','        Raghavendra Rao R','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8605,'01-328','HAL-Helicopter','LONGITUDINAL BEAM - LH','H918-05/13','201S 533H 6100 201','LN 9073 - 3.1354T351','Nil',1,'ALHOS14-23','','38929','','0000-00-00',NULL,'yes','yes','yes','no','no','yes','no','no','no','part base thickness minus 2.0 +/- 0.2 but maure value 1.45 to 1.60','ATC tool changing time chips locked in tool holder & tool length pulse so [art base thickness minus.   ','ATC All tool pocket full fill in the holder & weekly once all pocket  cleaning ','ATC All tool pocket full fill in the holder & weekly once all pocket  cleaning','NEXT PART CHECKED FOUND OK.','','2015-06-11','Krishna(Chowdary.G.P.)','Narayanappa(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','7','no','Misc','Narayanappa(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8606,'18-227B','Magellan Aerospace Bournemouth','CLAMP STRIP BTM','421008','L572 51299 200','ABM3 1029','A00',1,'RP401009','','43301','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Linear indications observed on part surface.','This was heppened during handling in the transit.','Informed to packing department and improved the packing method.','Qulaity alert dispaled for packing by grouping family of parts.','This part reworked and found ok and Next batch found satisfactory.','','2015-06-12','Avinash(R.J.)','Nandishkumar(D.K.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','18543','POST DN','yes','Misc','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8607,'18-079B','Magellan Aerospace Bournemouth','TOP SKIN STIFFNER 3','547010','L575 53251 201','','A00',2,'RP400837','','42501','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Machine abuse observed.','After treatments machine abuse was checked and found \r\n','New Fair is carrying out and fair documents will be approved by source inspectors, 100% visual inspection will be done before sending to treatments.\r\n','New Fair is carrying out and fair documents will be approved by source inspectors, 100% visual inspection will be done before sending to treatments.\r\n','CAPA found okay','','2015-06-12','Avinash(R.J.)','Nandishkumar(D.K.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','18580','POST DN','yes','Misc','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8608,'40-014','Universal Engineering Limited','STIFFENER BUTT STRAP ','5230102','D575 41603 200','','C01, ECN HG29999ST1TE12',50,'320402 - S3','','41071','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1)CSK Over size.','Part was manufactured and later cos was issued by the customer ','Part was manufactured and later cos was issued by the customer ','Part was manufactured and later cos was issued by the customer ','Part was manufactured and later cos was issued by the customer ','','2015-06-12','Anjinamurthy(H)','Chiranjeevi S,Anjinamurthy H,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','With Treatment','0','FI','no','Slim-2','Sudhagar(V)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8609,'40-015','Universal Engineering Limited','STIFFENER BUTT STRAP','5230102','D575 41603 201','','C01, ECN HG29999ST1TE12',50,'320402 - S3','','41072','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1)CSK Over size.','Part was manufactured and later cos was issued by the customer ','Part was manufactured and later cos was issued by the customer ','Part was manufactured and later cos was issued by the customer ','Part was manufactured and later cos was issued by the customer ','','2015-06-12','Anjinamurthy(H)','Chiranjeevi S,Anjinamurthy H,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','With Treatment','0','FI','no','Slim-2','Sudhagar(V)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8610,'18-415B','Magellan Aerospace Bournemouth','ACTUATOR HOUSING','95744A','D278 50163 201','','D',2,'RP401022_Amend No 1','','42061','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dia 5.15 to 5.30 CSK over size.(Measured 5.40 to 5.45) ','Due to CSK program running time CSK diameter plus side.this error happened for surface area not parallel.This is process problem.\r\n','Instructed to operator before part load to machine check the surface area in every part.\r\n ','Inform the turning supervisor next batch production running time avoid the top and bottom surface face out within 0.010mm maintained and waiting for process analysis.  ','CA/PA found satisfactory.','','2015-06-13','Girish(Prasad P)','Girish(Prasad P)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','00','no','Misc','Girish(Prasad P)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8611,'18-415B','Magellan Aerospace Bournemouth','ACTUATOR HOUSING','95744A','D278 50163 201','','D',1,'RP401022_Amend No 1','','42061','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Hole Champer over size during deburring.','This part 0.5mm hole chf required, but chf over side, identified in checking time(production) , but analysis then corrective action taken. ','Analysis to be made for next batch of production.','Analysis to be made for next batch of production.','CA/PA found satisfactory.','','2015-06-13','Rangaswamy()','Rangaswamy()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','00','no','Misc','Rangaswamy()','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8612,'35-286','Saab AB','REINFORCEMENT','582084','423Z1985-2','','--A',1,'PA 1510 NEW PARTS-2','','42851','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Rib thickness minus. ','Due to tool overhang, tool vibrates while running wall finishing program running.\r\nthis causes rib thickness minus side.\r\n\r\n','After checking the part in stages, operator analyzed and checked the error and find deviation in tool overhang.\r\nimmediately changed the tool and checked to tool overhang as per MPS and also checked the tool run out and then continued production.\r\n','Informed to all the operators and supervisors to check the MPS datasheet and also crosscheck the reference book for tool overhang.\r\nThis procedure to be follow for all the setup and supervisor should monitor.\r\n','CA/PA found satisfactory.','','2015-06-13','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','Rib thickness minus. ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Rangaswamy()','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8613,'35-170','Saab AB','ALCD_STRUCT_SUPPORT-FTG_L','425803A','423Z1200-11-01','','---',1,'1600096186','','43980','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Slot width over side measured 0.05 mm (From Top face 20mm  depth measures minus side)','While slot roughing program running time step observed due to tool vibration or incorrect tool parameter.After running the Slot finishing program step not cleared.\r\nThis problem due to roughing tool over hang.   ','Immediately stooped the machine and checked the tool and holder visually and then tool holding length checked, tool run out checked and found ok..\r\nThen for next part tool parameter adjusted and checked the slot width after roughing program and found ok.\r\nAfter ensuring the stock after slotting operation production continued.  ','Parameter proved and same is allowable in MPS.Therefore RPM setted and continued production.\r\nNext WO qty 70nos produced and checked 100% after roughing operation and all parts slot width is under tolerance.\r\n   ','CA/PA found satisfactory.','','2015-06-13','Lohith(K)','Lohith(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','With Treatment','','3','no','Misc','Lohith(K)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8614,'18-595A','Magellan Aerospace Wrexham','FITTING AFT INBD','4527101','L575 52000 200','','A',2,'RM132918 Amnd 1','','42906','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no',' FAI part Hole position not achieved.','3 Datum Single Setup not Finished, Hole position not achieved','3 Datum Faces finished last setup ','3 Datum Faces finished last setup Or Single Setup for All Parts','CAPA found okay, next parts found good','','2015-06-15','Ramesh(Poojary)','Rangaswamy()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Rangaswamy()','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8615,'35-183A','Saab AB','EDGE HOUSING','593780','423Z1121-6-02','','--A',1,'May 2015','','43599','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dia 124.142 Bore position 0.15mm shifted.','In 05 operation while finishing the dia 124.142 bore,Process is to dial the locating pin and then move X 83.355 & Y 20.017 to set the X0 Y0.\r\nBut operator not done the correct shifting of the above dimensions by manual mistake.\r\nThis deviation causes 0.15mm shift in y-axis. ','While checking the part in first off deviation observed and then checked the X0 Y0 again and found deviation. \r\nFor second part machined with stock in new offset, part inspected in CMM and found ok.\r\nThen continued the production.\r\n\r\n ','Note added to cross check the hole shifting after X0 Y0 taken in machine.\r\nAlso informed to operators to check the PCD after roughing pass. ','2nd part checked with cmm and found ok.','','2015-06-15','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','05','no','Misc','Rangaswamy()','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8616,'18-607A','Magellan Aerospace Wrexham','FITTING FWD SPAR','547010','L575 52218 200','','A00',1,'RM132922 Amnd 01','','43083','','0000-00-00',NULL,'no','no','no','no','no','yes','yes','yes','no','Corrosion pits observed on bore.','Due to rubbing of tool or material behavior Corrosion Pits  has been observed  in Treatment house\r\n','Apply PX-24 after machining, and polishing and rubbing of tool should be avoided\r\n','Apply of PX-24 is mandatory before sending the parts to treatment house.\r\n','Next parts and batches found okay\r\n','','2015-06-17','Avinash(R.J.)','Nandishkumar(D.K.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','','DN','yes','Misc','Avinash(R.J.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8617,'18-608A','Magellan Aerospace Wrexham','FITTING FWD SPAR','547010','L575 52218 201','','A00',1,'RM132922 Amnd 01','','43084','','0000-00-00',NULL,'no','no','no','no','no','yes','yes','yes','no','Corrosion pits observed on bore.','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','','2015-06-17','Avinash(R.J.)','Nandishkumar(D.K.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','','DN','yes','Misc','Avinash(R.J.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8618,'18-612A','Magellan Aerospace Wrexham','FITTING FWD SPAR','6772701','L575 54237 201','','A00',1,'RM132922 Amnd 01','','43113','','0000-00-00',NULL,'no','no','no','no','no','yes','yes','yes','no','Machine abuse corrosion marks found on the part.','Due to rubbing of tool or material behavior Corrosion Pits  has been observed  in Treatment house\r\n','Apply PX-24 after machining, and polishing and rubbing of tool should be avoided\r\n','Apply of PX-24 is mandatory before sending the parts to treatment house.\r\n','Next parts and batches found okay\r\n','','2015-06-17','Avinash(R.J.)','Nandishkumar(D.K.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','','DN','yes','Misc','Avinash(R.J.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8619,'18-314A','Magellan Aerospace Wrexham','STUD','453734','D278 50006 206 01','','D',1,'RP135260','','44171','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','od thread nogo answer.','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. ','Next part thread insert changed and takened tool X&Z offset and maintained the thraed offset effective dia and soot the thread gauge,Gauge is answered and run the part. ','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. ','CA/PA found satisfactory.','','2015-06-17','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','03','no','Misc','Narasimhamurthy(K.G.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8620,'18-155B','Magellan Aerospace Wrexham','BRACKET','409899','F579 53174 200 47',' ABM3 1029','B',1,'RP125889','','41688','','0000-00-00',NULL,'yes','yes','yes','','','','','','','CSK diameter over size Actual dimension 4.5 to 4.6x100deg measured 4.75x98deg .','Due to operator wrong tool loaded.Actual running tool Dia 6x100deg CHF tool but operator selected tool was dia 6x98deg','Immediately check the tool and after continue the production.\r\nInform to operator every setting time check the tool and tool angle mandatory.  ','Immediately check the tool and after continue the production.\r\nInform to operator every setting time check the tool and tool angle mandatory.Dedicated tools in this CRN.','CAPA found okay. Next parts found good','','2015-06-18','Lohith(K)','                        Hari Prasad','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8621,'18-565A','Magellan Aerospace Wrexham','FITTING SPIKE FWD','6772701','L575 51782 201','','A',1,'RM132919 Amnd 1','','43686','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','FAIR part,Inside wall tool dig mark observed.','Length tool required for this wall radius R3, we used 6ball for 5axis radius Finishing, this Program running time part vibrated, dig mark found on wall then part was rejected\r\n','Before 6ball program one more program adapted for remove the rest material for 12R3 cutter, after run the 12R3 program 6 Ballnose base radius finish program running pat found ok \r\n','When small dia cutter (Dia  6 or less than 6) using before more than 8 one more cutter tool adapted for reducing load for smaller dia cutter\r\n','CAPA found okay\r\n','','2015-06-18','Ramesh(Poojary)','Basavaraju(S. Sr.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Rangaswamy()','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8622,'28-016','Magellan Aerospace New York  Inc.','STOP FITTING','571458-5','161A6119-1','15-5PH Per AMS 5659 ','N/C',4,'124982-3170_R0_C0','','44336','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Total width minus side maintained (1mm) . ','While part running time Z offset wrongly taken.\r\nDue to manual error this deviation coming.\r\nOperator not checked the parts 100% after operation-03 completes.\r\nThis error causes in between production running. Due to tool blunt operator changed the tool and while taking the WO this error happened.','Operator noticed the deviation while checking the parts in stages and found the error in tool offset.Then new Z-offset taken and continued production.\r\n100nos WO qty checked and found 04 nos found deviation.','Informed to operator to check the tool offset correctly and cross check once while loading the tool.\r\nTraining given to operator to check the tool offset.\r\nSupervisor to monitor the manual errors and guide the operator in shifts. ','CA/PA found satisfactory.','','2015-06-19','Krishna(Chowdary.G.P.)','Ravindra(Singh R)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','00','no','Misc','Lohith(K)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8623,'18-098B','Magellan Aerospace Bournemouth','VALVE- SEAT','66894/01/00','D282 50060 204','','D',1,'RP408160','','44273','','0000-00-00',NULL,'yes','yes','yes','','','','','','','PART BEND SO DIG MARK,','While part final operation (top facing) running time part bend so part running time lifted. ','Inform to operator before load the part check the bend. Every part loading time clean the surface after load the part. When part bend observed immediately inform to concern supervisor.','Inform to operator before load the part check the bend. Every part loading time clean the surface after load the part. When part bend observed immediately inform to concern supervisor.','CAPA found okay','','2015-06-19','Lohith(K)','        Dhananjaya N','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8624,'18-394A','Magellan Aerospace Bournemouth','VALVE BODY','405978','A284 40009 200','','A',1,'RP400947','','43564','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','yes','Dia 2.4 drill bit brocken','While drilling operation drill bit cutting edge was worn out due to this drill bit was  brokened.','Immediatelly drill bit replaced and checked the jig and not found any defect then one part processed and inspected and required dimension was achived,then contiued the process.','1)Instructed to operator to change the drill bit every 50th part.\r\n2)Guide the operator to use the coolant properlly and dont give the chance to heat the drill bit.\r\n3)Befor load the drill bit check the cuuting angle and cutting edge if it is fit for use or not.','CA/PA found satisfactory.','','2015-06-19','Nagaraju(T)','Nagaraju(T)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','07','no','Misc','Nagaraju(T)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8625,'18-098B','Magellan Aerospace Bournemouth','VALVE- SEAT','66894/01/00','D282 50060 204','','D',1,'RP408160','','44272','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Running time part lift','While part final operation (top facing) running time part bend so part running time lifted. ','Inform to operator before load the part check the bend. Every part loading time clean the surface after load the part. When part bend observed immediately inform to concern supervisor.','Inform to operator before load the part check the bend. Every part loading time clean the surface after load the part. When part bend observed immediately inform to concern supervisor.','CAPA found okay','','2015-06-19','Lohith(K)','        Yarri Gowda','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8626,'35-138','Saab AB','FLCD_DS_SUPPORT_DEFLECT_S','R8H8','423Z6189-3','BAC1534-62C','---',1,'PA 1510 FORECAST','','44600','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','* Crack and dived in leyer part.','The Following Route causes analyzed for material chip off after outer profile machining. 1. Due to\r\nRM deviations material will chip off. \r\n2. While running production, the finishing tool wear out\r\ncauses light chip off in material. \r\n3.Steel Butting sheet for part is not Flat.','The following Corrective Action/Preventive Action taken to avoid Materiel chip off. \r\n1. Raw Material will inspect visually before issuing to production. If found any problem visually RM will be quarantined. \r\n2. Dia 8 end mill life calculated, informed to operators to monitor the tool life. and change the tool after as mentioned. \r\n3. Steel butting plates flatness inspection done before\r\nproduction starts.','The following Corrective Action/Preventive Action taken to avoid Materiel chip off. \r\n1. Raw Material will inspect visually before issuing to production. If found any problem visually RM will be\r\nquarantined. \r\n2. Dia 8 end mill life calculated, informed to operators to monitor the tool life.and change the tool after as mentioned. \r\n3. Steel butting plates flatness inspection done before production starts. Taking all the above PA, rejections happened in material chip off. Out of 100nos\r\nproduction 5 to 6nos getting rejection. Due to customer requirement parts are manufactures with\r\nconsidering rejections.','Effectiveness to be monitored','','2015-06-20','Rangaswamy()','Theerthappa K.N.,Shivaraj K S,Hari Prasad,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','HAASVF2SS','Manjunath(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8627,'18-319A','Magellan Aerospace Bournemouth','HALF CLAMP ','8031','D574 50552 200','DTD 5014','B01',1,'RP408269','','44426','','0000-00-00',NULL,'yes','','yes','','','','','','','Dia 5.5 drill problem ','','','','Part accepted','','2015-06-20','','        Manohara M','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8628,'35-193','Saab AB','INTERCOSTAL CAM HOUSING','425803B','423Z1190-1-01','','---',1,'1600102067','','42613','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Screen shot bubble no-46,Thickness required 3.0482 To 3.556mm is Measureds 2.87 To 3.09mm','This deviation observed at particular area and while inspecting at stage, deviation not found.\r\nWhen checking the part at FI deviation found.\r\nThe following route causes action analyzed,\r\n1.This deviation may be part not butting properly in operation-02.\r\n2.Chances of chips allocated at part butting. this causes part thickness minus side.','The following corrective action taken,\r\n1.Check the part butting by feller gauge and ensure the part butting. \r\n2.Check the chips in the butting area visually before loading the part in fixture in operation-02.\r\n','This deviation observed now after 250nos of production done after FAI approval.\r\nFor next batch part butting will ensure by educating operators and also message will enter in machine and MPS to cross check the part butting and chips in butting area. ','CA/PA found satisfactory.','','2015-06-21','Krishna(Chowdary.G.P.)','Shivashankar H.G.,Mahesh N,Krishna Chowdary.G.P.,Karthineyan V.S.,Basavaraja S. Jr.,','','2015-06-22','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','VMC 70L','Avinash(R.J.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8629,'18-113A','Magellan Aerospace Bournemouth','ADJUSTER','424402','D575 40496 200','S80 FHT','G',2,'RP400840','','43721','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','ID thread nogo answer.','After 25nos running threading insert will be wear out.for next part threading insert will be changed and 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 answer.  \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 down 0.05mm and run the part and then gauge answered and next part run in same reading & the part found okay.  \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 down 0.05mm and run the part and then gauge answered and next part run in same reading & the part found okay.  \r\n','CA/PA found ok.','','2015-06-22','Ravi(M)','Rajesh B D,KRISHNAMURTHY N,GUNDEGOWDA H.G.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','1','no','DX 200-3','Ravi(M)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8630,'18-370B','Magellan Aerospace Bournemouth','SPACER','19915275','L281 50314 200','','A00',1,'RP408279','','44751','','0000-00-00',NULL,'yes','yes','yes','','','','','','no','WHILE RUNNING TIME ,PROGRAM WAS WRONG SELECTED','There was setting in another BM60 Machine , so due to confusion selected 2nd program instead of 1st Program.','Select the program carefully, and these types of errors happen very occasionally and extra care will be taken care while selecting the program. ','Select the program carefully, and these types of errors happen very occasionally and extra care will be taken care while selecting the program.','CAPA found okay because these types of errors happen rarely. ','','2015-06-22','Anjinamurthy(H)','        S. Shiva Kumar','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8631,'18-310A','Magellan Aerospace(Chalfont) Limited','STOP - U/C HINGED DOOR ','444838','F575 51392 200','','A, ECN PG49999SMAKG01',1,'P/078237','','44725','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Dig mark observed on wall.','While part roughing program running time part was lifted so part dig due to RM width under size.','All work order qty RM width and length checked, Fixture modified and continue the production.\r\nInform the operator before load the part check the RM size mandatory.  ','All work order qty RM width and length checked, Fixture modified and continue the production.\r\nInform the operator before load the part check the RM size mandatory.  ','Checking of RM is being done, if the RM length is under size machining will not be done.','','2015-06-22','Lohith(K)','        Hari Prasad','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8632,'28-045','Magellan Aerospace New York  Inc.','LEVER','158524','65-51632-6','','PL_Rev - A + ADCN # 2 ; DL_Rev - N/C',1,'125339-2520_R0_C0','','41523','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Outer Profile not cleared.(Machining cut not taken on outer profile)','While doing the batch production, one no. RM deviation observed on part in operation-03.\r\nDue to RM is not correct on outer profile, finishing cut not taken and step observed on outer profile.\r\nThis deviation is observed after 02 operation completes and in 03 operation this was observed.','RM is forged material and RM dimension is not able to check and this deviation observed for 01no only.\r\nTherefore CA/PA not planned yet and in next batch production method of inspection the forged material will plan. ','RM is forged material and RM dimension is not able to check and this deviation observed for 01no only.\r\nTherefore CA/PA not planned yet and in next batch production method of inspection the forged material will plan. ','CA/PA Found ok.','','2015-06-22','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','00','no','Misc','Anjinamurthy(H)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8633,'18-090A','Magellan Aerospace Bournemouth','BUSH','K10011','D278 50164 200','S80 FHT','A',1,'RP400843','','43858','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Running time powertrip OD dig mark.','running time power tripped that time o.d was digmark.  \r\n','We are inform to the maintenence for the proper UPS connection.  \r\n','We are inform to the maintenence for the proper UPS connection.  \r\n','Maintenance done UPS connection ensured. ','','2015-06-22','Dinakar(K)','Nataraja C V,Manjunatha N,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','3','no','QT100S-1','Ravi(M)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8634,'18-382A','Magellan Aerospace(Chalfont) Limited','SLEEVE BEARING ','237004','D575 40037 200','','A',2,'P/063165','','24279','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','yes','running time part rotate so t/l (-)side 0.1mm  \r\n','In 2nd set up thickness is maintained 0.1mm plus side.in finishing operation more stock measure part will rotate.when part rotated OD will undersize.  \r\n','For next part check the thickness and any deviation came that will be adjusted in work offset and run the part.  \r\n','For next part check the thickness and any deviation came that will be adjusted in work offset and run the  part.instructed to operators to check the dimension of 2nd set up before loading the part.\r\n \r\n','CA/PA will be monitored in the next batch.','','2015-06-23','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','1','no','Misc','Dinakar(K)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8635,'18-442A','Magellan Aerospace Wrexham','1.5','4659','L280 50067 204 PF','','A00',1,'RP137240 Amnd 1','','44796','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Total length undersize.','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.  \r\n','Jaws bored neatly where the part face was butted to jaws and clamped on od and taking offset run the part ,part found ok and continue the production.  \r\n','Instruction given to operator to where the thickness is maintained for have to butt that face in the jaws not in the starting face.  \r\n','Next production parts found satisfactory.','','2015-06-24','Narasimhamurthy(K.G.)','Narasimhamurthy(K.G.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','03','no','Misc','Narasimhamurthy(K.G.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8636,'35-138','Saab AB','FLCD_DS_SUPPORT_DEFLECT_S','R8H8','423Z6189-3','BAC1534-62C','---',2,'PA 1510 FORECAST','','44592','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Part layer chip out','Due to material bheaviour this was opened out.','1) We decided that this cannot be avoaided but we minimized by improving the handling methods.','1) We decided that this cannot be avoaided but we minimized by improving the handling methods.','CA/PA found satisfactory and material layer removal is decreased','','2015-06-24','Lohith(K)','Shivaraj K S,Hari Prasad,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','HAASVF2SS','Avinash(R.J.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8637,'18-098B','Magellan Aerospace Bournemouth','VALVE- SEAT','66894/01/00','D282 50060 204','','D',1,'RP408160','','44272','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Part bend so slot nogo answer','Due to part 2nd operation and 3rd operation completed time part bend observed after part bend removing time slot width over size.','Inform to operator Next batch before part bend removed after run the 3rd operation.When part bend observed immediately inform to concern supervisor.','Inform to operator Next batch before part bend removed after run the 3rd operation.When part bend observed immediately inform to concern supervisor.','CAPA found okay','','2015-06-24','Lohith(K)','        Yarri Gowda','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8638,'18-098B','Magellan Aerospace Bournemouth','VALVE- SEAT','66894/01/00','D282 50060 204','','D',1,'RP408160','','44272','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Part bend so slot width over size maintained (0.04 mm) .','Due to part 2nd operation and 3rd operation completed time part bend observed after part bend removing time slot width over size.   ','Inform to operator Next batch before part bend removed after run the 3rd operation.When part bend observed immediately inform to concern supervisor.','Inform to operator Next batch before part bend removed after run the 3rd operation.When part bend observed immediately inform to concern supervisor.','CAPA found okay','','2015-06-25','Lohith(K)','Yarri Gowda,Shivaraj K S,Punith G S,Dhananjaya N,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','5','no','VM2-1','Lohith(K)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8639,'18-610A','Magellan Aerospace Wrexham','PIN FLOATING ANG','739760','L575 54228 200','','A00',1,'RM132919 Amnd 1','','44608','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dig mark on outer profile.','While running Dia 10fl tool on outer profile, part rotate and dig mark observed.\r\nAs per process part clamped with thread lock and there is no support to withstand the cutter load.\r\nDue to this part can rotate and causes problem in profile.\r\n','After observing this error, support given to withstand the cutter load by applying M5 bolt on part hole and then outer profile program will run.\r\nBy this new method 07nos manufactured and found ok.\r\nAfter machining the outer profile, Part CSK operation will complete by removing the m5 bolt.\r\n\r\n','Program sequence changed as per new process and bolting method incorporated.\r\nMPS to be changed as per new process. ','CAPA found okay next parts found good','','2015-06-25','Rangaswamy()','Manohara(B.C.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','07','no','Misc','Rangaswamy()','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8640,'18-211B','Magellan Aerospace(Chalfont) Limited','PLUNGER','W71530','D321 40205 200','','H01, ECN NR29998ST1JB80',1,'P/078231','','44630','','0000-00-00',NULL,'','','yes','','','','','','','part running time o.d - 0.008micorn..','In OD roughing setup running time insert will be breakage and part will OD oversize and that part not checking the operator and part not maintain in proper stock for finishing tool. So in the finishing setup that part loading time finishing tool get the more stock and coolant flows not correctly and chips will be over lapped in the outer diameter and part will be -.008 micron under\r\nsized.  \r\n','After roughing check the diameter and maintain the proper stock for the finishing tool and run the part and adjust the coolant in insert edge coolant will be avioded the chips over lapping and every 50ns chnge the finished insert tip and run the part so this problem again not\r\nrepeated. again.  \r\n','After roughing check the diameter and maintain the proper stock for the finishing tool and run the part and adjust the coolant in insert edge coolant will be avioded the chips over lapping and every 50ns chnge the finished insert tip and run the part so this problem again not repeated.  \r\n','CA/PA found satisfactory.','','2015-06-25','','        Ningaraj A N','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8641,'18-069C','Magellan Aerospace Bournemouth','M/C BRKT FWD WX 1727.0 ','16221760','D575 40237 200','','N',2,'RP408279','','44740','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Slot width over side (actual dim 15.75mm to 15.79mm measured dim 16.09)  ','While 1st part running time operator not adjust the CRC value, So part slot width over side maintained.This error happen operator mistake.\r\n','Enter correct value and run production,50nos found ok.','Training to operator, explain crc value & explain crc program.','Training imparted, CAPA found okay','','2015-06-25','Lohith(K)','        Yarri Gowda','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8642,'18-380B','Magellan Aerospace Bournemouth','GAMMA FITTINGS ','M523880 90950','NSA840020-350','','L',2,'RP401481_Amend No.-1','','44054','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1)Total Length 30.5, \r\n2)Dimension (N) 12.70 -0.1 \r\n3)thickness (E) 1.60 measures 0.60 under size. ','1.We are run the inner diameter, inner grooves and total lenght finish in the operation no1,and we are check the inner diameter for every parts but total lenght and inner grooves checked after every 25 ns.                     2.while clamping the part, in the butting face chips will butted so faceout occured in the running part and half of the part total lenght meassures 0.5 to 0.6 undersized but not observed the operator.    ','while clamping time clean the jaws by using air, and after clamping the part for every part rotate the chuck and cross check the butting fece visually and then run the part and after run the part check the total lenght for every parts hundred percently.','next every batch we are check the total lenght hundred percent after 25 ns once cross check the inner groove depth and after clamping the part for every part rotate the chuck and cross check the butting fece visually and then run the part and after run the part check the total lenght for every parts hundred percently.and avoiding the this type of errores. ','Next batch found satisfactory','','2015-06-27','Dinakar(K)','Nandeesha N,Dinakar K,Chandre  Gowda,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','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),(8643,'18-610A','Magellan Aerospace Wrexham','PIN FLOATING ANG','739760','L575 54228 200','','A00',1,'RM132919 Amnd 1','','44608','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','wrong dimension given in proces sheet,that dimension rework done that time part rotate OD dig mark found so part reject.','Treatment dimension not consider in drawing, part getting stock , when reworking same dimension part was rotated due to part rejected\r\n','Treatment dimension consider and same will updated on process sheet\r\n','Before loading the part cross check the drawing dimension, process sheet dimension and is the final dimension was before or after treatment. same will be updated on Process Sheet\r\n','CAPA found okay\r\n','','2015-06-27','Ramesh(Poojary)','Nagaraju(K.S.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','07','no','Misc','Dinakar(K)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8644,'18-105A','Magellan Aerospace Bournemouth','FORKEND ASSEMBLY','563177','D572 50462 200','S98 FHT','J01',1,'RP408148','','44224','','0000-00-00',NULL,'','','yes','','','','','','no','tool offset wrong entry','While operator work offset \"Z\" taken time operator not check the tool wear. So base thickness\r\nminus','Re-check the work offset, after continue the production. Instructed to operator every time work\r\noffset taken time cross check the wear offset.','Instructed to every operator 1st part work offset taken time check the wear dimension in tool wear. ','CAPA found satisfactory','','2015-06-29','','        Ravi R','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),