(7548,'35-291','Saab AB','BEAM FITTING','426692 B','424Z1143-2','','--B',1,'PA 1510 AL','','36464','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','Position Not Achived.','Wrong correction given by the operator\r\n','Instructed to CAD dept to edit program and correct it and freeze \r\n','Instructed to CAD dept to edit program and correct it and freeze \r\n','Rework under progress','','2014-08-12','Rangaswamy()','Mahesh(N)','','0000-00-00','Position Not Achived.(FAIR Part)','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','','03','yes','Misc','Rangaswamy()',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7549,'18-282A','Magellan Aerospace Bournemouth','Funk Pin','245160','A572 43263 200','BS S98 FHT','H',1,'RP400846','','36256','','0000-00-00',NULL,'yes','yes','yes','','','','','','no','O.D (-)sid 0.005micron','Due to ovality in part this deviation occur.\r\n','Instructed operator to check the ovality for every part,if\r\novality observed set the part zero run out and than run the\r\npart.\r\n','Instructed operator to check the ovality for every part,if\r\novality observed set the part zero run out and than run the\r\npart.\r\n','Found okay with next batch\r\n','','2014-08-12','Dinakar(K)','        Manjunatha N','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7550,'18-211B','Magellan Aerospace(Chalfont) Limited','PLUNGER','238302','D321 40205 200','','H01, ECN NR29998ST1JB80',1,'P/074114','','36524','','0000-00-00',NULL,'yes','yes','yes','','','','','','no','dia9.7mm OD(-)side0.008mm.','Due to ovality in part this deviation occur.\r\n','Instructed operator to check the ovality for every part,if\r\novality observed set the part zero run out and than run the\r\npart.\r\n','Instructed operator to check the ovality for every part,if\r\novality observed set the part zero run out and than run the\r\npart.\r\n','Found okay with next batch\r\n','','2014-08-12','Dinakar(K)','                Dinakar K','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7551,'18-360A','Magellan Aerospace Bournemouth','BUSH PLAIN','L12366','L575 53194 200','','A00',1,'RP400948','','36517','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no',' It was observed during source inspection ,thickness 5.88 ~ 5.96 mm measures  4.89mm in 01 No, out of 14No’s','1)improper work offset given 2)total length not meassuring properly. 3)micrometer error 4)micrometer zero not checking.\r\n','befor checking the every part check the slip and cross check the micrometer.\r\n\r\n\r\n\r\n\r\n','befor checking the every part check the slip and cross check the micrometer.\r\n\r\n\r\n\r\n\r\n','Next batch found okay','','2014-08-12','Dinakar(K)','Devaraj K.C.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','FI','no','DX 200-1','Narasimha Murthy(R)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7552,'34-014B','Magellan Aerospace Winnipeg','STAND-OFF, RH LOWER ','H0535-2A','400-12603-2-905','','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-024','','35480','','0000-00-00',NULL,'yes','yes','yes','','','','','','','running time base thickness minus side (actual dimension 2.30 mm to 2.75 mm measured dimension 1.7 mm to 1.90 mm ).','Due to running time part was lifted. The part was not butted in the fixture properly which was slightly lifted while finishing the base thickness.','1)The part was kept separately for further investigation and NC was raised . \r\n2)The program was studied in brief so as to avoid the escapes 3)All the tool offset was resettled.','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.','Found okay with next batch\r\n','','2014-08-12','Lohith(K)','        Dhananjaya N','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7553,'34-033B','Magellan Aerospace Winnipeg','BASE FITTING, F/D HINGE R','52304-2','400-12780-2-905','','EM104302 Iss A, EM105092 Iss F, EM104765 Iss G, EM106399 Iss B, EM106400 Iss B, EM106401 Iss A, EM106404 Iss A, EM106522 Iss A',1,'B91379 Rev-024','','35621','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1)Hole position under size by 0.15 MM.','Raw material is not in right angle, RM is unclear after outer profile machining.\r\nWhile cutting the RM in Gas cutting taper coming and due to this part deviation coming.  ','1).Instructed to stores to check the received RM as per requirements.\r\n2).Instructed to operator check the RM size properly.\r\n3).Raw material size deviation time inform to the supervisor or store department.    ','1).Instructed to stores to check the received RM as per requirements.\r\n2).Instructed to operator check the RM size properly.\r\n3).Raw material size deviation time inform to the supervisor or store department.    ','Found okay with next batch\r\n','','2014-08-12','Lohith(K)','Theerthappa K.N.,Shivaraj K S,Hari Prasad,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','0','FI','no','HAASVF2SS','Sudhagar(V)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7554,'18-211B','Magellan Aerospace(Chalfont) Limited','PLUNGER','240136','D321 40205 200','','H01, ECN NR29998ST1JB80',1,'P/074114','','36510','','0000-00-00',NULL,'yes','yes','yes','','','','','','no','running time chips rub so od (-)side..','Insert was worn out so this problem occurred\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 satisfactory\r\n','','2014-08-13','Sandhesh D(S)','        Nataraja C V','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7555,'18-247B','Magellan Aerospace Bournemouth','BUTTSTRAP LOW RS4X13600','387854','L575 50179 200','ABM3 1029','A00',1,'RP401009','','34284','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Machine Abuse rejected at API.','After treatments machine abuse was checked and found \r\n','New Fair is carrying out and fair documents will be approved by source inspectors, 100% visual inspection will be done before sending to treatments.\r\n','New Fair is carrying out and fair documents will be approved by source inspectors, 100% visual inspection will be done before sending to treatments.\r\n','Fair carried out and found okay\r\n','','2014-08-14','Muniyappa(N)','Nandishkumar(D.K.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','13685','POSTDN','no','Misc','Muniyappa(N)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7556,'35-185','Saab AB','CED_LATCH_SERRAT_ED_PLATE','581148A4','425Z0610-17','','---',1,'1600086478','','36640','','0000-00-00',NULL,'yes','yes','yes','','','','','','no','part bend vaccum not holding proparly so 1 side thikness minus.','JOB NOT BUTT PROPERLY TO THE CHUCK DURING CLAMPING. \r\n','INSTRUCTED OPERATOR TO BUTT THE JOB PROPERLY DURING CLAMPING\r\n','INSTRUCTED OPERATOR TO BUTT THE JOB PROPERLY DURING CLAMPING\r\n','Next batch found okay\r\n','','2014-08-14','Rangaswamy()','        Shivashankar H.G.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7557,'18-086B','Magellan Aerospace Wrexham','PLATE SEALING','419747','D572 52913 200','ABM3 1029','B',5,'RP125884','','35454','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Outer profile Radious steep formation.','Due to put the center bolts not properly so part outer Profile step found\r\n','Put the center bolts properly and bolt tightness also checked then run the production. \r\n','Put the center bolts properly and bolt tightness also checked then run the production. \r\n','Rework done and found okay','','2014-08-14','Anjinamurthy(H)','Anjinamurthy(H)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','','FI','yes','Misc','Narasimha Murthy(R)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7558,'18-007A','Magellan Aerospace Wrexham','PLATE COVER ','375714','D572 52517 200 ','','A, ECN HG29999ST1TP78',1,'RP127045','','35327','','0000-00-00',NULL,'yes','no','no','no','yes','yes','no','no','no','Dig mark on total thickness.','Due to put the center bolts not properly so part dig mark found. \r\n','Put the center bolts properly and bolt tightness also checked then run the production. \r\n','Put the center bolts properly and bolt tightness also checked then run the production. \r\n','Next batch found okay\r\n','','2014-08-17','Anjinamurthy(H)','Anjinamurthy(H)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','0','FI','no','Misc','Nandishkumar(D.K.)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7559,'18-270C','Magellan Aerospace Bournemouth','BUTTSTRAP UPP RS4X2820 ','404510','L575 54337 201','','B00',1,'RP400948','','34176','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Center distance 7.73/8.03 measure undersize 7.63 mm.','JOB NOT BUTT PROPERLY TO THE CHUCK DURING CLAMPING. \r\n\r\n','INSTRUCTED OPERATOR TO BUTT THE JOB PROPERLY DURING CLAMPING\r\n','INSTRUCTED OPERATOR TO BUTT THE JOB PROPERLY DURING CLAMPING\r\n','Next batch found okay\r\n','','2014-08-18','Anjinamurthy(H)','Anjinamurthy H,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','0','FI','no','BMV 60-1','Nandishkumar(D.K.)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7560,'18-318A','Magellan Aerospace Bournemouth','HALF CLAMP','M205070 / 57435','D574 50551 200','DTD 5014','B01',3,'RP400946','','33858','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','Outer profile dig mark found','Due to put the center bolts not properly so part outer profile dig mark. \r\n','Put the center bolts properly and bolt tightness also checked then run the production. \r\n','Put the center bolts properly and bolt tightness also checked then run the production. \r\nEnsure the butting surface with feeler gauge.','Next batch will be monitored.','','2014-08-18','Ramesh(Poojary)','Ramesh(Poojary)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Anjinamurthy(H)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7561,'28-003A','Magellan Aerospace New York  Inc.','PIN-ATTACHMENT WALKING BE','G20527K07','161A7305-1','','PL-Rev-NC, DL Rev-B',1,'120240_R0_C0','','35242','','0000-00-00',NULL,'yes','yes','yes','','','','','','no','1NO.S bore (+) side 0.005','When doing ID finishing, chips clocking in insert and chips rubbed and chatter mark observed on part.\r\nTryed to remove chatter mark and find ID diameter plus side by 0.005mm.','Checked the Drawing tolerance and as per requirement ID diameter tolerance is 0.040. therefore part is accepted.\r\nInformed to operator to check the insert wear out and coolant flow regularly to avoid chips clogging.','Informed to operator to check the insert wear out and coolant flow regularly to avoid chips clogging.','Part accepted','','2014-08-18','Narasimhamurthy(K.G.)','        KRISHNAMURTHY N','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7562,'18-319A','Magellan Aerospace Bournemouth','HALF CLAMP ','M205070 / 57435','D574 50552 200','DTD 5014','B01',3,'RP400946','','33819','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','Outer profile not finished.','As it was proving part slight correction in program was required','Program corrected and part found okay in next batch','Program corrected and part found okay in next batch','Found okay with next batch','','2014-08-18','Ramesh(Poojary)','Ramesh(Poojary)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','','03','yes','Misc','Anjinamurthy(H)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7563,'18-319A','Magellan Aerospace Bournemouth','HALF CLAMP ','M205070 / 57435','D574 50552 200','DTD 5014','B01',5,'RP400946','','33818','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Hole under size.','Due to reamer run out in the holder. \r\n','Next changed the holder then checked the run out by plunger dial the run out is 0.001 mm then continue the production\r\n','Instructed operator to first time proving the first part will checked the run out of the reamer before run the tool.This message entered in the program. \r\n\r\n','Rework under progress','','2014-08-18','Anjinamurthy(H)','Mohan Kumar(C.M.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','','03','yes','Misc','Lohith(K)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7564,'18-104A','Magellan Aerospace Bournemouth','BODY TURNBUCKLE','242098','D575 40490 200','S80 FHT','E',1,'RP400840','','35532','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Thread nogo answeard.','Wrong program and while giving repass problem occurred\r\n','Instructed to CAD dept to edit program and freeze it \r\n','Instructed to CAD dept to edit program and freeze it \r\n','Found okay with next batch\r\n','','2014-08-18','Dinakar(K)','Ravi M,Rajesh B D,Mohan Kumar C.M.,Manohara M,KRISHNAMURTHY N,GUNDEGOWDA H.G.,Anjinamurthy H,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','FI','no','DX 200-3','Narasimha Murthy(R)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7565,'18-104A','Magellan Aerospace Bournemouth','BODY TURNBUCKLE','242098','D575 40490 200','S80 FHT','E',1,'RP400840','','35532','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Thread gauge not answered.','Insert was worn out so this problem occurred\r\n','Check insert status regularly and know the life of inserts and change inserts according instructions \r\n','Check insert status regularly and know the life of inserts and change inserts according instructions \r\n','Rework under Progress','','2014-08-18','Dinakar(K)','Ravi M,Rajesh B D,Mohan Kumar C.M.,Manohara M,KRISHNAMURTHY N,GUNDEGOWDA H.G.,Anjinamurthy H,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Manufacture Only','','FI','yes','DX 200-3','Narasimha Murthy(R)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7566,'18-111A','Magellan Aerospace Bournemouth','BODY TURNBUCKLE INTMD','238300','D575 41544 200','S80 FHT','A',1,'RP400840','','35939','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Thread NOGO answeared.','Wrong program and while giving repass problem occurred\r\n','Instructed to CAD dept to edit program and freeze it \r\n','Instructed to CAD dept to edit program and freeze it \r\n\r\n','Found okay with next batch\r\n','','2014-08-19','Dinakar(K)','Rajesh T,Rajesh B D,Mohan Kumar C.M.,Manohara M,KRISHNAMURTHY N,GUNDEGOWDA H.G.,Dinakar K,Devaraj K.C.,Anjinamurthy H,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','FI','no','ST20Y1','Narasimha Murthy(R)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7567,'18-075A','Magellan Aerospace Wrexham','ADAPTOR ','94063A','D282 50044 200','','A',1,'RP125890','','36538','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','thread gauge not betted. ','Insert was worn out so this problem occurred\r\n','Check insert status regularly and know the life of inserts and change inserts according instructions \r\n','Check insert status regularly and know the life of inserts and change inserts according instructions \r\n','Rework under progress\r\n','','2014-08-19','Dinakar(K)','Ashith(B)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Manufacture Only','','01','yes','Misc','Sandhesh D(S)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7568,'35-076','Saab AB','9900976-434','421135','F579 54100 200','ABM3 1029','B',1,'1600087350 Rev 1 ','','36473','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','* Thickness under size .','JOB NOT BUTT PROPERLY TO THE CHUCK DURING CLAMPING. \r\n','INSTRUCTED OPERATOR TO BUTT THE JOB PROPERLY DURING CLAMPING\r\n','INSTRUCTED OPERATOR TO BUTT THE JOB PROPERLY DURING CLAMPING\r\n','Next batch found okay\r\n','','2014-08-19','Girish(Prasad P)','Girish(Prasad P)','','0000-00-00','* Thekness under size .','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Girish(Prasad P)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7569,'35-297','Saab AB','HINGE FITTING','426692 B','425Z0311-12','','---',1,'PA 1510 AL','','36666','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','FAI Part, Wrong progrem Given From CAD/CAM. ****// NC should be Raised against CAD/CAM department ****//','Program given by the CAD dept was found wrong ','Instructed to CAD dept to correct program and freeze it \r\n','Instructed to CAD dept to correct program and freeze it ','Found okay with next batch\r\n','','2014-08-19','Rangaswamy()','Mahesh(N)','','0000-00-00','FAI Part, Wrong progrem Given From CAD/CAM.','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','01','no','Misc','Rangaswamy()',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7570,'35-167','Saab AB','ALCD_STRUCT_SUPPORT-FTG_L','541705','423Z1202-11-01','','---',1,'1600086478','','36629','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Rib Thickness 8.89 Under Size.','JOB NOT BUTT PROPERLY TO THE CHUCK DURING CLAMPING. \r\n','INSTRUCTED OPERATOR TO BUTT THE JOB PROPERLY DURING CLAMPING\r\n','INSTRUCTED OPERATOR TO BUTT THE JOB PROPERLY DURING CLAMPING\r\n','Next batch found okay\r\n','','2014-08-19','Rangaswamy()','Rangaswamy()','','0000-00-00','Rib Thickness 8.89 Under Size.','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Rangaswamy()',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7571,'35-167','Saab AB','ALCD_STRUCT_SUPPORT-FTG_L','541703','423Z1202-11-01','','---',1,'1600086478','','36630','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Tool Dig Mark in  Rib 3d face.','Due to put the center bolts not properly so part dig mark found. \r\n','Put the center bolts properly and bolt tightness also checked then run the production. \r\n','Put the center bolts properly and bolt tightness also checked then run the production. \r\n','Next batch found okay\r\n','','2014-08-19','Girish(Prasad P)','Basavaraja S.(Jr.)','','0000-00-00','Tool Dig Mark in  Rib 3d face.','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','07','no','Misc','Rangaswamy()',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7572,'35-167','Saab AB','ALCD_STRUCT_SUPPORT-FTG_L','541703','423Z1202-11-01','','---',1,'1600086478','','36630','','0000-00-00',NULL,'yes','yes','yes','','','','','','no','CHF tool deg mark.','Due to put the center bolts not properly so part dig mark found. \r\n','Put the center bolts properly and bolt tightness also checked then run the production. \r\n','Put the center bolts properly and bolt tightness also checked then run the production. \r\n','Next batch found okay\r\n','','2014-08-19','Rangaswamy()','        Basavaraja S. Jr.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7573,'18-382A','Magellan Aerospace(Chalfont) Limited','SLEEVE BEARING ','238302','D575 40037 200','','A',1,'P/074123','','36542','','0000-00-00',NULL,'yes','yes','yes','','','','','','no','Thread Groove dig mark','Insert was worn out so this problem occurred\r\n','Check insert status regularly and know the life of inserts and change inserts according instructions \r\n','Check insert status regularly and know the life of inserts and change inserts according instructions \r\n','CAPA found satisfactory\r\n','','2014-08-20','Dinakar(K)','        Ningaraj A N','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7574,'28-004A','Magellan Aerospace New York  Inc.','PIN','G20466K08','161A2332-1','15-5PH Steel Bar per','NA',1,'120243-3172','','33543','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','while running time boring tool was broken so bore was over size by +0.03.','Tool was broken while machining ','Check Tool status regularly and know the life of inserts and change inserts according instructions \r\n','Check Tool status regularly and know the life of inserts and change inserts according instructions \r\n','CAPA found satisfactory\r\n','','2014-08-20','Dinakar(K)','Rajesh B(D)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','07','no','Misc','Sandhesh D(S)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7575,'18-054B','Magellan Aerospace Bournemouth','CLEAT','452080','L575 52580 200','','A00',2,'RP400836','','35193','','0000-00-00',NULL,'no','no','no','yes','yes','yes','no','no','no','Machine Abuse rejected at API,black marks observed on the part surface.','After treatments machine abuse was checked and found \r\n','New Fair is carrying out and fair documents will be approved by source inspectors, 100% visual inspection will be done before sending to treatments.\r\n','New Fair is carrying out and fair documents will be approved by source inspectors, 100% visual inspection will be done before sending to treatments.\r\n','Fair carried out and found okay\r\n','','2014-08-20','Muniyappa(N)','Nandishkumar(D.K.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','POSTDN','no','Misc','Muniyappa(N)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7576,'35-138','Saab AB','FLCD_DS_SUPPORT_DEFLECT_S','500738','423Z6189-3','BAC1534-62C','---',4,'1600086478','','36643','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','part chipout. ','JOB NOT BUTT PROPERLY TO THE CHUCK DURING CLAMPING. \r\n','INSTRUCTED OPERATOR TO BUTT THE JOB PROPERLY DURING CLAMPING\r\n','INSTRUCTED OPERATOR TO BUTT THE JOB PROPERLY DURING CLAMPING\r\n','Next batch found okay\r\n','','2014-08-20','Rangaswamy()','Rangaswamy()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','02','no','Misc','Rangaswamy()',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7577,'18-328A','Magellan Aerospace Wrexham','NUT ANCHOR ','92163A','D572 51346 200','','A',1,'RP125889','','36610','','0000-00-00',NULL,'yes','yes','yes','','','','','','no','Dia 11.5 drill depth over side.','Due to reamer run out in the holder. \r\n','Next changed the holder then checked the run out by plunger dial the run out is 0.001 mm then continue the production\r\n','Instructed operator to first time proving the first part will checked the run out of the reamer before run the tool.This message entered in the program. \r\n','Next batch found okay\r\n','','2014-08-20','Lohith(K)','        Lohith K','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7578,'18-375B','Magellan Aerospace Bournemouth','GAMMA FITTINGS ','1663','NSA840020-100','','L',1,'RP401477','','36200','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','It was observed during source inspection ,diameter “K” 29.26 ~29.31 mm measures  29.47mm over size in    01 No, out of 40 No’s','As it was the first part of that work order, operator found it out and gave necessary corrections but missed to separate that part in shift relieving.','1)First off part will be stacked with stickers and strictly instructed operator and line inspectors to set the dial gauge properly and destroy the part if there is any deviation found. \r\n\r\n2)Separate rejection box is kept inside the Gamma cell and we will take to QAD control once in a week.','1)First off part will be stacked with stickers and strictly instructed operator and line inspectors to set the dial gauge properly and destroy the part if there is any deviation found. \r\n\r\n2)Separate rejection box is kept inside the Gamma cell and we will take to QAD control once in a week.\r\n','Next batch found okay\r\n','','2014-08-20','Muniyappa(N)','Nandishkumar(D.K.)','RDN00085','2014-08-21','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','CUST END','no','Misc','Muniyappa(N)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7579,'18-279A','Magellan Aerospace(Chalfont) Limited','DOOR OUTER TYPE 23','217769 001','L572 53721 200','ABS5032A055','B00',1,'P/068958','','28634','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','* base thickness under size.','JOB NOT BUTT PROPERLY TO THE CHUCK DURING CLAMPING. \r\n','INSTRUCTED OPERATOR TO BUTT THE JOB PROPERLY DURING CLAMPING\r\n','INSTRUCTED OPERATOR TO BUTT THE JOB PROPERLY DURING CLAMPING\r\n','Next batch found okay\r\n','','2014-08-21','Girish(Prasad P)','Girish(Prasad P)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','03','no','Misc','Girish(Prasad P)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7580,'18-382A','Magellan Aerospace(Chalfont) Limited','SLEEVE BEARING ','230330','D575 40037 200','','A',1,'P/074123','','36544','','0000-00-00',NULL,'yes','','yes','','yes','','','','no','running time part rotated so OD (-)side.','Due to ovality in part this deviation occur.\r\n','Instructed operator to check the ovality for every part,if\r\novality observed set the part zero run out and than run the\r\npart.\r\n','Instructed operator to check the ovality for every part,if\r\novality observed set the part zero run out and than run the\r\npart.\r\n','Found okay with next batch\r\n','','2014-08-21','Dinakar(K)','        Dinakar K','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7581,'35-185','Saab AB','CED_LATCH_SERRAT_ED_PLATE','564847A2','425Z0610-17','','---',1,'PA-1300 2014','','36852','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dig noticed on serration. ','While running final  set up  operator not butted he part in jaws\r\n','Training given to operator to take care while loading the part\r\npart.\r\n','Training given to operator to take care while loading the part\r\npart.\r\n','Next batch found okay\r\n','','2014-08-21','Rangaswamy()','Shivashankar(H.G.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Rangaswamy()',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7582,'18-318A','Magellan Aerospace Bournemouth','HALF CLAMP','M205070 / 57435','D574 50551 200','DTD 5014','B01',5,'RP400946','','33817','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','1)Radius rework R38.10. Under size by 0.20MM.','Radius was not formed properly while finishing setup ( Tool prob)','Check the life of the tool and check the radius for every part ','Check the life of the tool and check the radius for every part ','Found okay with next part','','2014-08-21','Anjinamurthy(H)','Anjinamurthy(H)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','0','00','no','Misc','Anjinamurthy(H)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7583,'18-279A','Magellan Aerospace(Chalfont) Limited','DOOR OUTER TYPE 23','217769 001','L572 53721 200','ABS5032A055','B00',7,'P/068958','','28634','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Thickness plus side (0.15mm to 0.2mm)','RM bend so Running time vacuum not clamping properly so thickness plus. ','Next batch production running time RM bend checked after load the part. ','Next batch production running time RM bend checked after load the part. ','Rework under progress','','2014-08-21','Girish(Prasad P)','Girish(Prasad P)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Manufacture Only','','4','yes','Misc','Girish(Prasad P)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7584,'28-041','Magellan Aerospace New York  Inc.','LEVER ASSY-SECONDARY SPOI','158325','65-46358-16','','PL_E, DL_N/C, Sketch # 1',1,'122693','','35841','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1)Bore unmasked at one side. Requirement bore free from paint.										\r\n','Returned to rework for API','Returned to rework for API','Returned to rework for API','Returned to rework for API','','2014-08-21','Avinash(R.J.)','Sudhagar(V)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','0','DN','yes','Misc','Sudhagar(V)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7585,'35-157A','Saab AB','INTERCOSTAL_VENT','554773','423Z1172-3-01','','---',1,'1600086478','','35796','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Base thickness measures undersize out of tolerance 0.2mm.','Due to butting face not cleaned properly .So part thickness under size. \r\n','Before load the part of the butting face cleaned by air then load the part.\r\n','Before load the part of the butting face cleaned by air then load the part.\r\n','CAPA found satisfactory\r\n','','2014-08-21','Rangaswamy()','Shivashankar H.G.,Rangaswamy ,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','A51nx-1','Manjunath(G)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7586,'18-214A','Magellan Aerospace(Chalfont) Limited','SPECIAL WASHER ','472203','D321 40210 202','','E01, ECN NR29999ST1JB79',10,'P/074114','','35505','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Broaching id dig mark.','While Broaching part was not butted properly','Training given to operator to take care while loading the part\r\npart.\r\n','Training given to operator to take care while loading the part\r\npart.\r\n','Next batch found satisfactory\r\n','','2014-08-22','Anjinamurthy(H)','S. Shiva Kumar,Nandeesha N,Manjunatha N.R.,Krishnanaik J N,Kalakappa T H,Anjinamurthy H,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','FI','no','BMV 60-1','Narasimha Murthy(R)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7587,'35-185','Saab AB','CED_LATCH_SERRAT_ED_PLATE','564847A2','425Z0610-17','','---',1,'1600086478','','36639','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','csk over size.','Chamfer tool was worn out so this problem occurred\r\n','Check Chamfer tool status regularly and know the life of tool and change tools according instructions \r\n','Check Chamfer tool status regularly and know the life of tool and change tools according instructions ','Next part found okay','','2014-08-23','Rangaswamy()','Rangaswamy()','','0000-00-00','csk over size.','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Girish(Prasad P)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7588,'35-185','Saab AB','CED_LATCH_SERRAT_ED_PLATE','564847A2','425Z0610-17','','---',1,'PA-1300 2014','','36852','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','serration deg.','While running final  set up  operator not butted he part in jaws\r\n','Training given to operator to take care while loading the part\r\npart.\r\n','Training given to operator to take care while loading the part\r\npart.\r\n','Next batch found okay\r\n','','2014-08-23','Rangaswamy()','Rangaswamy()','','0000-00-00','serration deg.','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Girish(Prasad P)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL);
INSERT INTO `nc4qa` VALUES (7589,'18-295A','Magellan Aerospace Bournemouth','BOLT','A0484U','D577 56145 200','S80','A',2,'RP400846','','36638','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Thread damage.','Insert was worn out so this problem occurred\r\n','Check insert status regularly and know the life of inserts and change inserts according instructions \r\n','Check insert status regularly and know the life of inserts and change inserts according instructions \r\n','CAPA found satisfactory\r\n','','2014-08-23','Dinakar(K)','Kalakappa T(H)','','0000-00-00','1)1no dia 2.9 pin nogo answered(milling).','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','09','no','Misc','Narasimhamurthy(K.G.)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7590,'18-123A','Magellan Aerospace Bournemouth','FORK END OUT BD','479202','D575 41546 202','S80 FHT','B',1,'RP400840','','36691','','0000-00-00',NULL,'yes','yes','yes','','','','','','no','bore + side running time','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','','2014-08-23','Anjinamurthy(H)','        Manohara M','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7591,'18-382A','Magellan Aerospace(Chalfont) Limited','SLEEVE BEARING ','230330','D575 40037 200','','A',1,'P/074123','','36543','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','RAW MATERIAL PROBLEM TOTAL LENGTH UNDER SIZE','After machining found that RM was undersized\r\n','Instructed to RM cutter to have the process sheet and exact required dimension and then cut the RM\r\n','Instructed to RM cutter to have the process sheet and exact required dimension and then cut the RM\r\n','Next batch found okay\r\n','','2014-08-23','Nagaraja (G)','Sunil(R)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','01','no','Misc','Diwakar(R.B.)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7592,'18-075A','Magellan Aerospace Wrexham','ADAPTOR ','94063A','D282 50044 200','','A',1,'RP125890','','36607','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','running time c axis problem od dig mark.','Machine was having C axis problem ','Instructed to maintenance department to repair the M/C and if possible give AMC to respective companies \r\n','Instructed to maintenance department to repair the M/C and if possible give AMC to respective companies ','CA PA found okay\r\n','','2014-08-24','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','03','no','Misc','Ravi(M)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7593,'01-317','HAL-Helicopter','SWINGING ARM','H 918-78/13','201C 671H 5111 201','3.321 4T451-80','Nil',1,'ALHOS14-22','','36891','','0000-00-00',NULL,'yes','yes','yes','','','','','','no','CUTTER COMPONSETION IS NOT CANCELLED SO RIB THICKNESS 0.4(-) SIDE','Machine didnot call for cutter compensation while giving re pass thickness got undersize ','Machine serviced and next parts found okay','Machine serviced and next parts found okay','Machine serviced and next parts found okay','','2014-08-24','Narayanappa(G)','        Siddaramappa ','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7594,'18-090A','Magellan Aerospace Bournemouth','BUSH','B4599A','D278 50164 200','S80 FHT','A',1,'RP400843','','36937','','0000-00-00',NULL,'yes','yes','yes','','','','','','no','running time part rotete so od (-)','JOB NOT BUTT PROPERLY TO THE CHUCK DURING CLAMPING. \r\n','INSTRUCTED OPERATOR TO BUTT THE JOB PROPERLY DURING CLAMPING\r\n','INSTRUCTED OPERATOR TO BUTT THE JOB PROPERLY DURING CLAMPING\r\n','Next batch found okay\r\n','','2014-08-25','Dinakar(K)','        Nataraja C V','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7595,'18-284A','Magellan Aerospace Bournemouth','SPINDLE FOR CLACK ALVES O','Y10819','A281-40019-200','S80 FHT','A',25,'RP400846','','36602','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1)OD undersize 0.04 to 0.07mm 23 no\'s\r\n2)Total Length undersize 2 no\'s\r\n ','Due to ovality in part this deviation occur.\r\n','Instructed operator to check the ovality for every part,if\r\novality observed set the part zero run out and than run the\r\npart.\r\n','Instructed operator to check the ovality for every part,if\r\novality observed set the part zero run out and than run the\r\npart.\r\n','Found okay with next batch\r\n','','2014-08-25','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','0','FI','no','Misc','Nandishkumar(D.K.)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7596,'18-046B','Magellan Aerospace Bournemouth','ANGLE ATCH RSPAR LWR','420577','L575 52441 200','','A00',1,'RP400836','','36063','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Base thickness minus side (-.8mm t0 1mm)','While running final  set up  operator not butted he part in jaws\r\n','Training given to operator to take care while loading the part\r\npart.\r\n','Training given to operator to take care while loading the part\r\npart.\r\n','Next batch found okay\r\n','','2014-08-25','Anjinamurthy(H)','Manjunatha(N.R.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Narasimha Murthy(R)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7597,'28-042','Magellan Aerospace New York  Inc.','GUIDE BUNGEE SPOILER - MI','745442','69-40332-1','','PL_A + ADCN #1, PSDL_N/C',6,'120844','','36812','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1)Thread NOGO answer.','Wrong program and while giving repass problem occurred\r\n','Instructed to CAD dept to edit program and freeze it \r\n','Instructed to CAD dept to edit program and freeze it \r\n','Found okay with next batch\r\n','','2014-08-26','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','0','DN','no','Misc','Sudhagar(V)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7598,'28-042','Magellan Aerospace New York  Inc.','GUIDE BUNGEE SPOILER - MI','745442','69-40332-1','','PL_A + ADCN #1, PSDL_N/C',7,'120844','','36813','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1)Thread NOGO answer.','Wrong program and while giving repass problem occurred\r\n','Instructed to CAD dept to edit program and freeze it \r\n','Instructed to CAD dept to edit program and freeze it \r\n','Found okay with next batch\r\n','','2014-08-26','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','0','DN','no','Misc','Sudhagar(V)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7599,'35-170','Saab AB','ALCD_STRUCT_SUPPORT-FTG_L','558386','423Z1200-11-01','','---',1,'1600086478','','35906','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Bore measures oversize.','Due to reamer run out in the holder. \r\n','Next changed the holder then checked the run out by plunger dial the run out is 0.001 mm then continue the production\r\n','Instructed operator to first time proving the first part will checked the run out of the reamer before run the tool.This message entered in the program. \r\n','Next batch found okay\r\n','','2014-08-26','Rangaswamy(H A)','Rangaswamy(H A)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','DN','no','Misc','Manjunath(G)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7600,'35-071','Saab AB','9900976-380','26910-1','L579 50517 200','TA11','B00',2,'1600082589','','35990','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Part missing.','Carelessness of the Operators, Supervisors.\r\n','Strictly warned to all personals not to happen like this type of mistake\r\n','Strictly warned to all personals not to happen like this type of mistake\r\n','Warned seriously\r\n','','2014-08-26','Lohith(K)','Lohith(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','DN','no','Misc','Manjunath(G)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7601,'18-090A','Magellan Aerospace Bournemouth','BUSH','B4599A','D278 50164 200','S80 FHT','A',1,'RP400843','','36937','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','13.6 to 13.4 length measures to 13.298 to 13.31','After machining found that RM was undersized\r\n','Instructed to RM cutter to have the process sheet and exact required dimension and then cut the RM\r\n','Instructed to RM cutter to have the process sheet and exact required dimension and then cut the RM\r\n','Next batch found okay\r\n','','2014-08-26','Dinakar(K)','Ashith(B)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','01','no','Misc','Sandhesh D(S)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7602,'18-314A','Magellan Aerospace Wrexham','STUD','238172','D278 50006 206 01','','D',5,'RP125889','','34827','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Thread tight.','Insert was worn out so this problem occurred\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','Rework under Progress','','2014-08-27','Dinakar(K)','Shivappa M B,S. Shiva Kumar,Rajesh T,Mohan Kumar C.M.,Manjunatha N.R.,Girish V M,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Manufacture Only','','FI','yes','DX 200-1','Narasimha Murthy(R)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7603,'28-003A','Magellan Aerospace New York  Inc.','PIN-ATTACHMENT WALKING BE','G20527K07','161A7305-1','','PL-Rev-NC, DL Rev-B',61,'120240_R0_C0','','36932','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1)Slot in side stepmark.','It has happened due to tool runout & chipps clogged to tool holder while machining.\r\n\r\n','Ensuring the tool runout before loading and keep on checking the runout for several numbers,chipps movment should be smooth flow in the machining.','Instructed to CAD/CAM department to use i machining software for proper simulation of the tool path for proper chipping of part.\r\nEnsuring the tool runout before loading and keep on checking the runout for several numbers','CA/PA found ok.','','2014-08-27','Anjinamurthy(H)','Anjinamurthy(H)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','Manufacture Only','','FI','no','Misc','Sudhagar(V)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7604,'18-377B','Magellan Aerospace Bournemouth','GAMMA FITTINGS ','M504210','NSA840020-200','','L',1,'RP401479_Amend No-1','','36830','','0000-00-00',NULL,'yes','yes','yes','','','','','','no','SETTING TIME CHAMFER 0.7','Wrong offset taken\r\n','Instructed to operator to take offsets properly live on machines\r\n','Instructed to operator to take offsets properly live on machines\r\n','Next batch found okay\r\n','','2014-08-28','Dinakar(K)','        Dinakar K','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7605,'18-120C','Magellan Aerospace Bournemouth','HOUSING OUT B D BRG 3','230699','D275 56121 200','','E01,  ECN NG27011ST1KA83',1,'RP400843','','36675','','0000-00-00',NULL,'yes','yes','yes','','','','','','no','While running time tool offset was changed so part was dig mark on o.d.','Wrong offset taken\r\n','Instructed to operator to take offsets properly live on machines\r\n','Instructed to operator to take offsets properly live on machines\r\n','Next batch found okay\r\n','','2014-08-28','Dinakar(K)','        Ravi M','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7606,'35-169','Saab AB','ALCD_STRUCT_SUPPORT-FTG_L','558386','423Z1200-12-01','','---',5,'1600086478','','37127','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','1.Dig mark on Bore for 01 no.\r\n2.Bore oversize by 20~40 microns\r\n','JOB NOT BUTT PROPERLY TO THE CHUCK DURING CLAMPING. \r\nDue to reamer run out in the holder. \r\n','INSTRUCTED OPERATOR TO BUTT THE JOB PROPERLY DURING CLAMPING\r\nNext 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 BUTT THE JOB PROPERLY DURING CLAMPING\r\nInstructed 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','','2014-08-31','Rangaswamy()','Rangaswamy()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','06','no','Misc','Krishna(Chowdary.G.P.)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7607,'35-170','Saab AB','ALCD_STRUCT_SUPPORT-FTG_L','556561','423Z1200-11-01','','---',3,'1600086478','','37152','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dig mark on outer profile.','Due to put the center bolts not properly so part outer profile dig mark. \r\n','Put the center bolts properly and bolt tightness also checked then run the production. \r\n','Instructed operator to every part put the center bolts properly and bolt tightness also checked then run the production.  \r\n','Next batch found satisfactory\r\n','','2014-08-31','Rangaswamy()','Rangaswamy()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','06','no','Misc','Krishna(Chowdary.G.P.)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7608,'18-318A','Magellan Aerospace Bournemouth','HALF CLAMP','M205070 / 57435','D574 50551 200','DTD 5014','B01',2,'RP400946','','36971','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','In side raidus trail parts.','TRAIL ACCEPTED','TRAIL ACCEPTED','TRAIL ACCEPTED','TRAIL ACCEPTED','','2014-09-01','Anjinamurthy(H)','Anjinamurthy(H)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','With Treatment','','00','no','Misc','Anjinamurthy(H)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7609,'18-102A','Magellan Aerospace Bournemouth','BARREL-STRUT','237154','D572 50463 200','S98 FHT','F',1,'RP400839','','33658','','0000-00-00',NULL,'no','yes','no','yes','no','yes','no','no','no','Corrosion observed on the all out side diameters.','Found corrosion fits in FI stage\r\n','Instructed to clean the part with solution PX-24 after machining.\r\n','Instructed to clean the part with solution PX-24 after machining.\r\n','Found okay with next batch\r\n','','2014-09-01','Sunil Kumar(K.R.)','Devaraja (M S)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','FI','no','Misc','Narasimha Murthy(R)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7610,'18-318A','Magellan Aerospace Bournemouth','HALF CLAMP','M205070 / 57435','D574 50551 200','DTD 5014','B01',1,'RP400946','','37176','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Inner radius trail parts.','Radius tool was worn out operator failed to noticed it','Check tool status regularly and know the life of tool and change tool according instructions \r\n','Check tool status regularly and know the life of tool and change tool according instructions \r\n','Next part found ok','','2014-09-02','Anjinamurthy(H)','Anjinamurthy(H)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','00','no','Misc','Anjinamurthy(H)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7611,'35-162','Saab AB','BEAM-LOWER_INNER_AFT','426692 B','423Z1403-2-02','','---',1,'PA-1300 2014','','35948','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Scraches observed on the surface.','part was not handled softly\r\n','Instructed to all persons to handle the part with care\r\n','Instructed to all persons to handle the part with care\r\n','Parts were reworked and found okay','','2014-09-02','Avinash(R.J.)','Manjunath(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','14469','POST DN','yes','Misc','Avinash(R.J.)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7612,'35-143A','Saab AB','BCD_LATCH_PROBE_FTG_HOUSI','616621','424Z6115-3-01','','--C',1,'1600072156','','32274','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Step observed on datum face.\r\nHole pitch not achieved.\r\n','Due to part not butted properly step noticed on the surface \r\n','Training given to operator to take care while loading the part\r\npart.\r\n','Training given to operator to take care while loading the part\r\npart.\r\n','Next batch found okay\r\n','','2014-09-02','Rangaswamy()','Rangaswamy()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','06','no','Misc','Krishna(Chowdary.G.P.)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7613,'18-009A','Magellan Aerospace Wrexham','Plate Cover','497610','D572 52519 200','L97 T351','A',1,'RP127045','','37190','','0000-00-00',NULL,'yes','yes','yes','','','','','','no','total length [-side] 6 mm found for 6.4','After machining found that RM was undersized\r\n','Instructed to RM cutter to have the process sheet and exact required dimension and then cut the RM\r\n','Instructed to RM cutter to have the process sheet and exact required dimension and then cut the RM\r\n','Next batch found okay\r\n','','2014-09-02','Dinakar(K)','        Ravi M','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7614,'28-004A','Magellan Aerospace New York  Inc.','PIN','G20551K01','161A2332-1','15-5PH Steel Bar per','NA',17,'120243-3172','','35844','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Hole Over Size by 0.02mm','Hole got oversize because of drill run out','After drilling operation the drill dia will be checked before boring and after boring also the dia will be checked.','Drilling operation will be done with short distance after ensuring the runout, whole drilling operation will be done','Part accepted','','2014-09-03','Dinakar(K)','Rajesh B D,KRISHNAMURTHY N,Krishna Chowdary.G.P.,GUNDEGOWDA H.G.,Dinakar K,Devaraj K.C.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','Manufacture Only','','FI','no','DX 200-3','Sudhagar(V)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7615,'35-138','Saab AB','FLCD_DS_SUPPORT_DEFLECT_S','500738','423Z6189-3','BAC1534-62C','---',3,'PA-1300 2014-2','','36644','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Material layer chipout.','Insert was worn out so this problem occurred\r\n','Check insert status regularly and know the life of inserts and change inserts according instructions \r\n','Check insert status regularly and know the life of inserts and change inserts according instructions \r\n','CAPA found satisfactory\r\n','','2014-09-03','Avinash(R.J.)','Manjunath(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','14526','post DN','no','Misc','Manjunath(G)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7616,'18-314A','Magellan Aerospace Wrexham','STUD','238172','D278 50006 206 01','','D',1,'RP125889','','36858','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dummy NC','Dummy NC','Dummy NC','Dummy NC','Dummy NC','','2014-09-03','Dinakar(K)','KRISHNAMURTHY(N)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','Manufacture Only','','01','no','Misc','Dinakar(K)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7617,'18-314A','Magellan Aerospace Wrexham','STUD','238172','D278 50006 206 01','','D',1,'RP125889','','36857','','2014-09-03',NULL,'yes','yes','yes','no','no','no','no','no','no','OD Under size by 0.01mm.','Due to ovality in part this deviation occur.\r\n','Instructed operator to check the ovality for every part,if\r\novality observed set the part zero run out and than run the\r\npart.\r\n','Instructed operator to check the ovality for every part,if\r\novality observed set the part zero run out and than run the\r\npart.\r\n','Found okay with next batch\r\n','','2014-09-03','Dinakar(K)','KRISHNAMURTHY(N)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','01','no','Misc','Sandhesh D(S)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7618,'35-162','Saab AB','BEAM-LOWER_INNER_AFT','426692 A','423Z1403-2-02','','---',1,'PA-1300 2014','','35947','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','NDT failed.','NDT tests has been failed, Parts to be stripped and reworked and again sent to treatments.','NDT tests has been failed, Parts to be stripped and reworked and again sent to treatments.','NDT tests has been failed, Parts to be stripped and reworked and again sent to treatments.','Parts have been stripped and reworked and sent for treatments','','2014-09-03','Avinash(R.J.)','Manjunath(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','14470','post DN','yes','Misc','Manjunath(G)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7619,'18-120C','Magellan Aerospace Bournemouth','HOUSING OUT B D BRG 3','230699','D275 56121 200','','E01,  ECN NG27011ST1KA83',1,'RP400843','','36674','','0000-00-00',NULL,'yes','yes','yes','','','','','','no','Dig marks found on the face','Due to put the center bolts not properly so part dig mark found. \r\n','Put the center bolts properly and bolt tightness also checked then run the production. \r\n','Put the center bolts properly and bolt tightness also checked then run the production. \r\n','Next batch found okay\r\n','','2014-09-03','Lohith(K)','        Lohith K','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7620,'34-012B','Magellan Aerospace Winnipeg','STAND-OFF RH CENTRE ','53840-2','400-12602-2-905','','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-024','','36292','','0000-00-00',NULL,'yes','yes','yes','','','','','','no','IM/C Program running time base  thinknes - side.','Due to butting face not cleaned properly .So part thickness under size. \r\n','Before load the part of the butting face cleaned by air then load the part.\r\n','Before load the part of the butting face cleaned by air then load the part.\r\n','Found okay with next batch\r\n','','2014-09-03','Lohith(K)','        Dhananjaya N','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7621,'35-244','Saab AB','RADIUS FILLER LARGE','G20109K01','423Z1456-2','','---',1,'PA 1510 STEEL','','36650','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Dimension 0.100 +/- 0.0050 measures over size. ','Due to butting face not cleaned properly','Before load the part of the butting face cleaned by air per sure then load the part\r\n','Before load the part of the butting face cleaned by air per sure then load the part\r\n','Next batch found okay\r\n','','2014-09-04','Lohith(K)','Punith G S,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','VM2-1','Manjunath(G)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7622,'35-157A','Saab AB','INTERCOSTAL_VENT','614011A5','423Z1172-3-01','','---',1,'1600086478','','35795','','0000-00-00',NULL,'yes','no','no','no','no','yes','no','yes','no','NDT Failed','NDT tests has been failed, Parts to be stripped and reworked and again sent to treatments.','NDT tests has been failed, Parts to be stripped and reworked and again sent to treatments.','NDT tests has been failed, Parts to be stripped and reworked and again sent to treatments.','Parts have been stripped and reworked and sent for treatments','','2014-09-04','Avinash(R.J.)','Rangaswamy ,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','0','FI','yes','A51nx-1','Manjunath(G)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7623,'35-046','Saab AB','7605148-200','548108','L574 55148 200','ABM3 1029','A00',8,'1600087350 Rev 1 ','','36491','','0000-00-00',NULL,'yes','no','no','no','no','yes','no','yes','no','1)NDT Failure.','NDT tests has been failed, Parts to be stripped and reworked and again sent to treatments.','NDT tests has been failed, Parts to be stripped and reworked and again sent to treatments.','NDT tests has been failed, Parts to be stripped and reworked and again sent to treatments.','Parts have been stripped and reworked and sent for treatments','','2014-09-04','Avinash(R.J.)','Yogesha K,Prashanth Kumar M,Girish Prasad P,Basavaraja S. Jr.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','0','FI','yes','MakinoF5-3','Manjunath(G)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7624,'35-189','Saab AB','INTERCOSTAL_MIDSPAN_NO_2 ','541686','423Z1170-1-06','','---',1,'1600082632','','35307','','0000-00-00',NULL,'yes','no','no','no','no','yes','no','yes','no','NDT Failed.','NDT tests has been failed, Parts to be stripped and reworked and again sent to treatments.','NDT tests has been failed, Parts to be stripped and reworked and again sent to treatments.','NDT tests has been failed, Parts to be stripped and reworked and again sent to treatments.','Parts have been stripped and reworked and sent for treatments','','2014-09-04','Avinash(R.J.)','Yogesha K,Umesh B,Prashanth Kumar M,Mahesh N,Gurukiran S M,Basavaraja S. Jr.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','0','FI','yes','MakinoF5-4','Manjunath(G)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7625,'35-191','Saab AB','SUPPORT-FTG','675763A7','423Z1202-13','','---',1,'1600086478','','36592','','0000-00-00',NULL,'yes','no','no','no','no','yes','no','yes','no','NDT Failur.','NDT tests has been failed, Parts to be stripped and reworked and again sent to treatments.','NDT tests has been failed, Parts to be stripped and reworked and again sent to treatments.','NDT tests has been failed, Parts to be stripped and reworked and again sent to treatments.','Parts have been stripped and reworked and sent for treatments','','2014-09-04','Avinash(R.J.)','Yogesha K,Umesh B,Rangaswamy ,Prashanth Kumar M,Gurukiran S M,Basavaraja S. Jr.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','0','FI','yes','MakinoF5-4','Manjunath(G)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7626,'35-017','Saab AB','9901503-075','65646/01/00','D576 50011 200','L167','A',7,' PA1217 (Earthing Li','','34572','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dig mark on outer profile.\r\n\r\n(07nos are missing)','Carelessness of the Operators, Supervisors.\r\n','Strictly warned to all personals not to happen like this type of mistake\r\n','Strictly warned to all personals not to happen like this type of mistake\r\n','Warned seriously\r\n','','2014-09-04','Rangaswamy()','Rangaswamy()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','04','no','Misc','Krishna(Chowdary.G.P.)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7627,'35-226','Saab AB','HINGE BRACKET 1','420589','D576 50004 207','','D00',4,'1600086552','','35960','','0000-00-00',NULL,'yes','no','no','no','no','yes','no','yes','no','NDT Failure.','NDT tests failed in treatment house due to material behavior\r\n','100% RM inspection will be carried out in future batches\r\n','100% RM inspection will be carried out in future batches\r\n','Found okay in next batches\r\n','','2014-09-04','Avinash(R.J.)','Subramanya L Naik,Shivarajakumar T M,Krishna Chowdary.G.P.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','0','FI','yes','MakinoF5-2','Manjunath(G)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7628,'18-120C','Magellan Aerospace Bournemouth','HOUSING OUT B D BRG 3','230699','D275 56121 200','','E01,  ECN NG27011ST1KA83',1,'RP400843','','36674','','0000-00-00',NULL,'yes','yes','yes','','','','','','no','While running part rotated so OD U/S -0.01...','JOB NOT BUTT PROPERLY TO THE CHUCK DURING CLAMPING. \r\n','INSTRUCTED OPERATOR TO BUTT THE JOB PROPERLY DURING CLAMPING\r\n','INSTRUCTED OPERATOR TO BUTT THE JOB PROPERLY DURING CLAMPING\r\n','Next batch found okay\r\n','','2014-09-04','Dinakar(K)','        Bharath R','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7629,'18-382A','Magellan Aerospace(Chalfont) Limited','SLEEVE BEARING ','238302','D575 40037 200','','A',1,'P/074123','','36542','','0000-00-00',NULL,'yes','yes','yes','','','','','','no','While running Chips rubbed So ID +0.02','Insert was worn out so this problem occurred\r\n','Check insert status regularly and know the life of inserts and change inserts according instructions \r\n','Check insert status regularly and know the life of inserts and change inserts according instructions \r\n','CAPA found satisfactory\r\n','','2014-09-04','Dinakar(K)','        Ningaraj A N','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7630,'18-379B','Magellan Aerospace Bournemouth','GAMMA FITTINGS ','M492970','NSA840020-300','','L',1,'RP401480_Amend No.-1','','37237','','0000-00-00',NULL,'yes','yes','yes','','no','','','','no','J&G - side 0.1mm ....','Due to ovality in part this deviation occur.\r\n','Instructed operator to check the ovality for every part,if\r\novality observed set the part zero run out and than run the\r\npart.\r\n','Instructed operator to check the ovality for every part,if\r\novality observed set the part zero run out and than run the\r\npart.\r\n','Found okay with next batch\r\n','','2014-09-04','Dinakar(K)','        Krishnanaik J N','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7631,'18-120C','Magellan Aerospace Bournemouth','HOUSING OUT B D BRG 3','230699','D275 56121 200','','E01,  ECN NG27011ST1KA83',1,'RP400843','','36669','','0000-00-00',NULL,'yes','yes','yes','','','','','','no','runing time part rotated','JOB NOT BUTT PROPERLY TO THE CHUCK DURING CLAMPING. \r\n','INSTRUCTED OPERATOR TO BUTT THE JOB PROPERLY DURING CLAMPING\r\n','INSTRUCTED OPERATOR TO BUTT THE JOB PROPERLY DURING CLAMPING\r\n','Next batch found okay\r\n','','2014-09-04','Dinakar(K)','        Dinakar K','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7632,'01-317','HAL-Helicopter','SWINGING ARM','H 918-78/13','201C 671H 5111 201','3.321 4T451-80','Nil',1,'ALHOS14-22','','36891','','0000-00-00',NULL,'yes','no','no','no','yes','yes','no','no','no','Diameter 32.0+.1/-0.1 Measure at (35.52/60)','Under review, Diameter doesnot comes in this part itself ','Under review, Diameter doesnot comes in this part itself ','Under review, Diameter doesnot comes in this part itself ','Under review, Diameter doesnot comes in this part itself ','','2014-09-04','Anjinamurthy(H)','Siddaramappa ,S. Shiva Kumar,Manjunatha N.R.,Diwakar R.B.,','','2014-09-05','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','fi','no','BMV 60-1','Avinash(R.J.)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7633,'18-044B','Magellan Aerospace Bournemouth','ANGLE ATCH RSPAR UPR','420577','L575 52440 200','','A00',1,'RP400836','','37139','','0000-00-00',NULL,'yes','yes','yes','','','','','','no','part butting problem so wall thickness under size','While running final  set up  operator not butted he part in jaws\r\n','Training given to operator to take care while loading the part\r\n','Training given to operator to take care while loading the par\r\n','Next batch found okay\r\n','','2014-09-05','Krishna(Chowdary.G.P.)','        Krishna Chowdary.G.P.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7634,'18-379B','Magellan Aerospace Bournemouth','GAMMA FITTINGS ','M492970','NSA840020-300','','L',1,'RP401480_Amend No.-1','','37237','','0000-00-00',NULL,'yes','yes','yes','','','','','','no','part rotate so ID Dig mark','JOB NOT BUTT PROPERLY TO THE CHUCK DURING CLAMPING. \r\n','INSTRUCTED OPERATOR TO BUTT THE JOB PROPERLY DURING CLAMPING\r\n','INSTRUCTED OPERATOR TO BUTT THE JOB PROPERLY DURING CLAMPING\r\n','Next batch found okay\r\n','','2014-09-05','Dinakar(K)','        Kalakappa T H','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7635,'18-211B','Magellan Aerospace(Chalfont) Limited','PLUNGER','240136','D321 40205 200','','H01, ECN NR29998ST1JB80',1,'P/074114','','36511','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','OD under size by 0.012mm.','Due to ovality in part this deviation occur.\r\n','Instructed operator to check the ovality for every part,if\r\novality observed set the part zero run out and than run the\r\npart.\r\n','Instructed operator to check the ovality for every part,if\r\novality observed set the part zero run out and than run the\r\npart.\r\n','Found okay with next batch\r\n','','2014-09-05','Dinakar(K)','Ningaraj A N,Nataraja C V,Dinakar K,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','3','no','QT100S-1','Narasimhamurthy(K.G.)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7636,'18-092A','Magellan Aerospace Bournemouth','PRESSURE RING','66900/01/00','D301 50085 200','L164 T4','A',5,'RP400844','','35126','','0000-00-00',NULL,'no','yes','no','yes','no','yes','no','no','no','Corrosion marks observed on the parts.','Found corrosion fits in F I stage\r\n','Instructed to clean the part with solution PX-24 after machining.\r\n','Instructed to clean the part with solution PX-24 after machining.\r\n','Found okay with next batch\r\n','','2014-09-05','Mohan(E)','Mohan(E)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','14364','POSTDN','no','Misc','Muniyappa(N)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7637,'18-211B','Magellan Aerospace(Chalfont) Limited','PLUNGER','240136','D321 40205 200','','H01, ECN NR29998ST1JB80',1,'P/074114','','36511','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Dia 8.66 pin nogo answeard.','Drill bit was ab-longed while machining ','Check the status of drill bit regularly after machining of each part and check the diameter with pin gauge regularly','Check the status of drill bit regularly after machining of each part and check the diameter with pin gauge regularly','Next batch found okay','','2014-09-05','Anjinamurthy(H)','Theerthappa K.N.,Shivaraj K S,SHIVAKUMAR ,Ravi M,Ningaraj A N,Nataraja C V,Lohith K,Kalakappa T H,Dinakar K,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','FI','no','HAASVF2SS','Narasimha Murthy(R)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7638,'35-104','Saab AB','ALCD_STRUCT_BUSHING-LATCH','L16028','423Z1141-1','Al-Ni-Bronze (UNS C6','--A',4,'1600080762','','33770','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1)Digmark noticed on the part.\r\n2)I/D measures oversize.qty 3nos.','Due to ovality in part this deviation occur.\r\n','Instructed operator to check the ovality for every part,if\r\novality observed set the part zero run out and than run the\r\npart.\r\n','Instructed operator to check the ovality for every part,if\r\novality observed set the part zero run out and than run the\r\npart.\r\n','Found okay with next batch\r\n','','2014-09-05','Dinakar(K)','Nataraja C V,Mohan Kumar C.M.,Manohara M,Dinakar K,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','FI','no','QT100S-1','Manjunath(G)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7639,'35-104','Saab AB','ALCD_STRUCT_BUSHING-LATCH','L16028','423Z1141-1','Al-Ni-Bronze (UNS C6','--A',2,'1600080762','','33770','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1)Hole missing qty 1no.\r\n2)ID undersize qty 1no.','New operator got confused to load the part\r\n','Instructed new operator to load the proper side of the part and showed him live demo in machine \r\n','Instructed new operator to load the proper side of the part and showed him live demo in machine \r\n','Rework under progress','','2014-09-05','Dinakar(K)','Nataraja C V,Mohan Kumar C.M.,Manohara M,Dinakar K,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Manufacture Only','','FI','yes','QT100S-1','Manjunath(G)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7640,'18-281A','Magellan Aerospace(Chalfont) Limited','Door Outer','9170602','L575 53119 200','ABS5032A055','A00',1,'P/074118','','37222','','0000-00-00',NULL,'yes','yes','yes','','','','','','no','csk 1hole 0.3 over size.','CSK tool was worn out so this problem occurred\r\n','Check Tools status regularly and know the life of Tool and change Tool according instructions \r\n','Check Tools status regularly and know the life of Tool and change Tool according instructions \r\n','CAPA found satisfactory\r\n','','2014-09-05','Krishna(Chowdary.G.P.)','        Basavaraja S. Jr.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7641,'18-003A','Magellan Aerospace Wrexham','BRACKET SUPPORT','409899','D361 50111 200','ABM3 1029 T7651','A',2,'RP125887','','35124','','0000-00-00',NULL,'no','no','no','yes','yes','yes','no','no','no','Machine abuse block mark observed.','After treatments machine abuse was checked and found \r\n','New Fair is carrying out and fair documents will be approved by source inspectors, 100% visual inspection will be done before sending to treatments.\r\n','New Fair is carrying out and fair documents will be approved by source inspectors, 100% visual inspection will be done before sending to treatments.\r\n','Fair carried out and found okay\r\n','','2014-09-05','Anjinamurthy(H)','Anjinamurthy(H)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','14329','POST DN','no','Misc','Muniyappa(N)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7642,'35-273','Saab AB','LATCH PIN','G19876K01','426Z1601-1','','--A',1,'PA 1510 STEEL','','36574','','0000-00-00',NULL,'yes','no','yes','no','yes','no','no','no','no','Hole Dia Over Size.','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','','2014-09-06','Rangaswamy()','Rangaswamy()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','05','no','Misc','Rangaswamy()',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7643,'35-293','Saab AB','SUPPORT HANDLE','617315A7','424Z1205-6-01','','--A',1,'PA 1510 AL','','36707','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Part Rib Under Size.','While running final  set up  operator not butted he part in jaws\r\n','Training given to operator to take care while loading the part\r\n','Training given to operator to take care while loading the part\r\n','Next batch found okay\r\n','','2014-09-06','Rangaswamy()','Jayarama(M.B.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Rangaswamy()',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7644,'18-211B','Magellan Aerospace(Chalfont) Limited','PLUNGER','238302','D321 40205 200','','H01, ECN NR29998ST1JB80',1,'P/074114','','36525','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','ID Thread Nogo answeard.','1) running time gauge tight so thread re-pass running.\r\n2) threading insert changed. \r\n3) threading insert wear out \r\n4) running time chips rubbing\r\n','after running the every part check the insert and load the next part\r\n\r\n\r\n\r\n\r\n','change the insert for every 40 parts.\r\n\r\n\r\n\r\n\r\n','Next batch found okay','','2014-09-08','Dinakar(K)','Theerthappa K.N.,Shivaraj K S,SHIVAKUMAR ,Ningaraj A N,Lohith K,Dinakar K,Bharath R,Ashith B,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','FI','no','QT100S-2','Narasimha Murthy(R)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7645,'18-211B','Magellan Aerospace(Chalfont) Limited','PLUNGER','238302','D321 40205 200','','H01, ECN NR29998ST1JB80',2,'P/074114','','36524','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','ID thread not answer.','Thread gauge was not butting.','Next time thread gauge kept to be free.','Any threaded parts after machining checked in machine before removing.','Next batch found okay','','2014-09-08','Dinakar(K)','Ningaraj A N,Nataraja C V,Dinakar K,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Manufacture Only','','3','yes','QT100S-1','Narasimhamurthy(K.G.)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7646,'18-211B','Magellan Aerospace(Chalfont) Limited','PLUNGER','238302','D321 40205 200','','H01, ECN NR29998ST1JB80',4,'P/074114','','36525','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dia 8.5hole nogo answer in 8.73pin.\r\ndia 8.5 drill not isse in tool manager.','While running drill bit broken,due to improve the drill grainding. ','1. First time drill load prove out in steel block.\r\n2. Drill regrinding time check the coon angle in grinding operator.\r\n3. While first part running time check the holder and calets\r\n4. Adjust coolant properly to tool.\r\n\r\n\r\n\r\n\r\n ','Instructed to operator when change the drill bit check the run   out and prove out in steel block.\r\nInstructed to tool grinding operator Drill regrinding time check the coon angle.   ','Z axis should be keep up so that part cut program will go proper. The correction has been in program only','','2014-09-08','Lohith(K)','Theerthappa(K.N.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','05','no','Misc','Anjinamurthy(H)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7647,'18-295A','Magellan Aerospace Bournemouth','BOLT','221668','D577 56145 200','S80','A',15,'RP378291','','12043','','0000-00-00',NULL,'yes','yes','yes','','','','','','','1)THREED DAMAGE','time insert damaged.','insert changed.','cross checking done.','Part found okay','','2014-09-08','Dinakar(K)','Dinakar K','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','no','','','','','yes','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7648,'18-382A','Magellan Aerospace(Chalfont) Limited','SLEEVE BEARING ','238302','D575 40037 200','','A',2,'P/074123','','36542','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1)1.30 Drill bit cut. 2)Id groov dia 63.50 to 63.60 mesure 64.0','1.This was happened during drilling of parts, After several parts machining drill bit got blunt.				\r\n2. When the grinding of the drill bit after blunting is not proper means chances of drill getting cut may occur				','1.Drill bit should be changed for every 50 to 60 no\'s once even its not worn out.		\r\n2.Ensuring proper grinding of drill bit after blunting		','1.Drill bit should be changed for every 50 to 60 no\'s once even its not worn out.		\r\n2.Ensuring proper grinding of drill bit after blunting		','Next batch found okay.','','2014-09-08','Nagaraju(T)','Shivarajakumar T M,Ningaraj A N,Nataraja C V,Krishna Chowdary.G.P.,Kalakappa T H,Dinakar K,Bharath R,','','0000-00-00','Nagaraju T.','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','FI','no','QT100S-1','Narasimha Murthy(R)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7649,'35-170','Saab AB','ALCD_STRUCT_SUPPORT-FTG_L','556561','423Z1200-11-01','','---',2,'1600086478','','35905','','0000-00-00',NULL,'yes','no','no','no','no','yes','no','yes','no','NDT Failure.','NDT tests failed in treatment house due to material behavior\r\n','100% RM inspection will be carried out in future batches , and informed to RM supplier\r\n','100% RM inspection will be carried out in future batches , and informed to RM supplier\r\n','Found okay in next batches\r\n','','2014-09-08','Avinash(R.J.)','Manjunath(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','0','FI','yes','Misc','Manjunath(G)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7650,'35-082','Saab AB','HOUSING-SIDE ROLLER','3966601 2','F579 53065 202','ABM3-1029 T7651','B, PG52307ST4KA80',15,'1600073867','','34264','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Bore measured oversize with ovality.','While running production bore oversize coming due to part bend after clamping for boring operation.\r\nThis problem accrues in between production running and in one orientation ovality observed.Same is not find out in checking with bore gauge by operator.','1. New clamps manufactured to clamp the part with sufficient force.( Parts should not twist after clamping). Parts twist and bend checked in machine and found Ok after new clamps introduced.\r\n2. Air gauge ordered and next batches parts will check in Airguage with 360 deg orientation.','1. New clamps manufactured to clamp the part with sufficient force.( Parts should not twist after clamping)\r\n2. Air gauge Procured and Parts manufactures and checked 792 quantities (WO no. 38832,38833,38834)and all the parts Bore dimension measures 15.915/15.917.','Next batch found okay','','2014-09-08','Rangaswamy()','Mahesh(B.T.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','Misc','Manjunath(G)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7651,'35-169','Saab AB','ALCD_STRUCT_SUPPORT-FTG_L','556561','423Z1200-12-01','','---',1,'1600086478','','35901','','0000-00-00',NULL,'yes','no','no','no','yes','yes','no','no','no','NDT Failure','NDT tests failed in treatment house due to material behavior\r\n','100% RM inspection will be carried out in future batches , and informed to RM supplier\r\n','100% RM inspection will be carried out in future batches , and informed to RM supplier\r\n','Found okay in next batches\r\n','','2014-09-08','Avinash(R.J.)','Manjunath(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','0','FI','yes','Misc','Manjunath(G)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7652,'18-211B','Magellan Aerospace(Chalfont) Limited','PLUNGER','238302','D321 40205 200','','H01, ECN NR29998ST1JB80',1,'P/074114','','36524','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Id Thread tight.','Thread gauge was not butting. ','Next time thread gauge kept to be free.','Any threaded parts after machining checked in machine before removing. ','Next batch found okay','','2014-09-08','Dinakar(K)','Theerthappa K.N.,Shivaraj K S,SHIVAKUMAR ,Ningaraj A N,Nataraja C V,Manjunatha N,Lohith K,Kalakappa T H,Dinakar K,Bharath R,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Manufacture Only','','FI','yes','QT100S-2','Narasimha Murthy(R)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7653,'34-012B','Magellan Aerospace Winnipeg','STAND-OFF RH CENTRE ','54200-1','400-12602-2-905','','EM104302 Iss A, EM104765 Iss G, EM105092 Iss F, EM106399 Iss B, EM106400 Iss B, EM106401 Iss A, EM106404 Iss A, EM106522 Iss A, EM106602 Iss A',1,'B91379 Rev-024','','35431','','0000-00-00',NULL,'yes','yes','yes','','','','','','no','2.5 thickness 0.2 (-) side','Fixture 5 deg  angle wear out so part running time part lifted \r\nout so part running time part lifted \r\n','New Fixture already manufacturing done. Fixture used in next batch production.','New Fixture already manufacturing done. Fixture used in next batch production.','Next batch will be monitored','','2014-09-08','Lohith(K)','        Theerthappa K.N.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7654,'34-012B','Magellan Aerospace Winnipeg','STAND-OFF RH CENTRE ','54200-1','400-12602-2-905','','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-024','','35431','','0000-00-00',NULL,'yes','yes','yes','','','','','','no','2.5 thickness 0.2 (-)side','Fixture 5 deg  angle wear out so part running time part lifted\r\n  \r\n','New Fixture already manufacturing done. Fixture used in next batch production.','New Fixture already manufacturing done. Fixture used in next batch production.','Next batch will be monitored ','','2014-09-08','Lohith(K)','        Theerthappa K.N.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7655,'18-303A','Magellan Aerospace(Chalfont) Limited','BUTT STRAP','489668','F575 50908 201 ','','A, ECN PG40011ST1QJ23',1,'P/074120_Amnd-04','','37297','','0000-00-00',NULL,'yes','yes','yes','','','','','','no','running time part lift so deburr oversize.','For cut out program the Z axis should be keep up that has not done so part got rejected.','Z axis should be keep up so that part cut program will go proper. The correction has been in program only','Z axis should be keep up so that part cut program will go proper. The correction has been in program only','Next batch will be monitored','','2014-09-08','Lohith(K)','        Lohith K','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7656,'18-387A','Magellan Aerospace(Chalfont) Limited','NUT RING INNER','224312','D575 40039 202','','B',3,'P/068966','','29064','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','1.3mm drill bit broken','1.This was happened during drilling of parts, After several parts machining drill bit got blunt.			\r\n2. When the grinding of the drill bit after blunting is not proper means chances of drill getting cut may occur\r\n3.As the requirement is 40 degree angled hole the chances of drill getting worn out is very often\r\n4.As the coolant flow is manual in these drilling operation the improper flow may cause drill cut			','1.Drill bit should be changed for every 50 to 60 no\'s once even its not worn out.		\r\n2.Ensuring proper grinding of drill bit after blunting	\r\n3.While drilling , we have planned for often blowing of air and proper channelize of coolant to the hole so that the drill may not worn out easily	','1.Drill bit should be changed for every 50 to 60 no\'s once even its not worn out.		\r\n2.Ensuring proper grinding of drill bit after blunting	\r\n3.While drilling , we have planned for often blowing of air and proper channelize of coolant to the hole so that the drill may not worn out easily','CA PA found satisfactory and next batches found good','','2014-09-09','Nagaraju(T)','Nagaraju(T)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','09','no','Misc','Nagaraju(T)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7657,'18-117B','Magellan Aerospace Bournemouth','HOUSING-OUT BD BRG','493023','D275 40004 200','','C01',1,'RP400841','','36135','','0000-00-00',NULL,'yes','yes','yes','','','','','','','running time chips rub so od (-)side','1) chips rubbing.2) single tool running 3)in data sheet have single tool so single tool running.\r\n','additional tool added and run the part\r\n\r\n\r\n\r\n\r\n','additional tool added in datd sheet and run the the part for next every batch.\r\n\r\n\r\n\r\n\r\n','Next batch found okay','','2014-09-09','Dinakar(K)','        Dinakar K','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7658,'35-238','Saab AB','JACK BRACKET 2','8356701','D576 50010 207','','D00',1,'1600076514','','33345','','0000-00-00',NULL,'yes','no','no','no','no','yes','no','yes','no','NDT Failure.','NDT tests has been failed, Parts to be stripped and reworked and again sent to treatments.','NDT tests has been failed, Parts to be stripped and reworked and again sent to treatments.','NDT tests has been failed, Parts to be stripped and reworked and again sent to treatments.','NDT tests has been failed, Parts to be stripped and reworked and again sent to treatments.','','2014-09-09','Avinash(R.J.)','Shivashankar H.G.,MALLIKARJUNA Gowda,Krishna Chowdary.G.P.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','0','FI','yes','HMC 440','Manjunath(G)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7659,'35-238','Saab AB','JACK BRACKET 2','387416','D576 50010 207','','D00',1,'1600071764-Rev2','','33900','','0000-00-00',NULL,'yes','no','no','no','no','yes','no','yes','no','NDT Failure.','NDT tests has been failed, Parts to be stripped and reworked and again sent to treatments.','NDT tests has been failed, Parts to be stripped and reworked and again sent to treatments.','NDT tests has been failed, Parts to be stripped and reworked and again sent to treatments.','NDT tests has been failed, Parts to be stripped and reworked and again sent to treatments.','','2014-09-09','Avinash(R.J.)','Prashanth Kumar M,Krishna Chowdary.G.P.,Basavaraja S. Jr.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','0','FI','yes','MakinoF5-2','Manjunath(G)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7660,'18-415B','Magellan Aerospace Bournemouth','ACTUATOR HOUSING','20005','D278 50163 201','','D',1,'RP401022_Amend No 1','','36616','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','*Dia 6mm hole angle shift. (10dig)','dummy nc','dummy nc','dummy nc','dummy nc','','2014-09-09','Girish(Prasad P)','Girish(Prasad P)','','0000-00-00','*Dia 6mm hole angle shift. (10dig)','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','07','no','Misc','Girish(Prasad P)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7661,'28-041','Magellan Aerospace New York  Inc.','LEVER ASSY-SECONDARY SPOI','158325','65-46358-16','','PL_E, DL_N/C, Sketch # 1',1,'116750_R0_C3','','31625','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1)Bore over size by 0.010 to 0.012MM.','Pit mark observed  in bore. part rework  after  that bore over size.','Instructed to production changed the coolant.','Instructed to production changed the coolant.','Under review.  ','','2014-09-09','Avinash(R.J.)','Punith G S,Manjunatha N,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','0','FI','no','QT100S-2','Sudhagar(V)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7662,'35-238','Saab AB','JACK BRACKET 2','427071','D576 50010 207','','D00',4,'1600074206','','32531','','0000-00-00',NULL,'yes','no','no','no','no','yes','no','yes','no','NDT FAILED','NDT tests has been failed, Parts to be stripped and reworked and again sent to treatments.','NDT tests has been failed, Parts to be stripped and reworked and again sent to treatments.','NDT tests has been failed, Parts to be stripped and reworked and again sent to treatments.','NDT tests has been failed, Parts to be stripped and reworked and again sent to treatments.','','2014-09-09','Avinash(R.J.)','Shivashankar H.G.,Nagaraju K.S.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','','FI','yes','HMC 440','Manjunath(G)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7663,'35-238','Saab AB','JACK BRACKET 2','8356701','D576 50010 207','','D00',1,'1600076514','','33346','','0000-00-00',NULL,'yes','no','no','no','no','yes','no','yes','no','NDT Failure.','NDT tests has been failed, Parts to be stripped and reworked and again sent to treatments.','NDT tests has been failed, Parts to be stripped and reworked and again sent to treatments.','NDT tests has been failed, Parts to be stripped and reworked and again sent to treatments.','Parts have been stripped and reworked and sent for treatments','','2014-09-09','Avinash(R.J.)','Shivashankar H.G.,Shivarajakumar T M,Nagaraju K.S.,Manjunatha S N,Krishna Chowdary.G.P.,Basavaraja S. Jr.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','0','FI','yes','A51nx-1','Manjunath(G)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7664,'28-041','Magellan Aerospace New York  Inc.','LEVER ASSY-SECONDARY SPOI','158326','65-46358-16','','PL_E, DL_N/C, Sketch # 1',6,'122693','','35843','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1)Bore over size by 0.010 to 0.012MM.','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','Next batch found okay','','2014-09-09','Avinash(R.J.)','Theerthappa K.N.,Shivaraj K S,Shivappa M B,S. Shiva Kumar,Rajesh T,Punith G S,Mohan Kumar C.M.,Manjunatha N.R.,Manjunatha N,Lohith K,Hari Prasad,Diwakar R.B.,Dinakar K,Dhananjaya N,Devaraj K.C.,Bharath R,Anjinamurthy H,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','DX 200-1','Sudhagar(V)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7665,'28-041','Magellan Aerospace New York  Inc.','LEVER ASSY-SECONDARY SPOI','158326','65-46358-16','','PL_E, DL_N/C, Sketch # 1',3,'122693','','35843','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1)Bore over size by 0.010 to 0.012MM.','In first setup runout will occured so time problem came.','First setup run the part without runout and correct this problem. ','First setup run the part without runout and correct this problem given the guidence to the operator.   ','Next batch found okay','','2014-09-09','Avinash(R.J.)','Theerthappa K.N.,Shivaraj K S,Shivappa M B,S. Shiva Kumar,Rajesh T,Punith G S,Mohan Kumar C.M.,Manjunatha N.R.,Manjunatha N,Lohith K,Hari Prasad,Diwakar R.B.,Dinakar K,Dhananjaya N,Devaraj K.C.,Bharath R,Anjinamurthy H,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','DX 200-1','Sudhagar(V)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7666,'18-044B','Magellan Aerospace Bournemouth','ANGLE ATCH RSPAR UPR','420577','L575 52440 200','','A00',1,'RP400836','','37140','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Thikness under size 0.05mm.','As the clamping this setup cannot achieve all time(thickness under size occurs regularly)','Clamping should be verified by feeler gauge and should confirm twice that the clamping is fully completed and no gap left.After this verification machining should be carried out.','Requested CAD department to change the clamping method or Machine in 4 axis if the CAPACITY is available.\r\n','Next batch found satisfactory','','2014-09-10','Anjinamurthy(H)','Shivarajakumar T M,Lohith K,Anjinamurthy H,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','BMV 60-1','Narasimha Murthy(R)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7667,'18-413B','Magellan Aerospace Bournemouth','ACTUATOR HOUSING','3440','D278 50162 200','','A',0,'RP401021_Amnd No. 1','','34553','','0000-00-00',NULL,'yes','no','no','no','yes','yes','no','no','no','Thickness undersize 6.00 to 6.10 mm measured 5.93 to 5.95mm.','1)rough tool running time thickness undersize 2)single tool running 3)tool shortage.\r\n','new tool orderd\r\n\r\n\r\n\r\n\r\n','additon tool adedd  this process mention in data sheet.\r\n\r\n\r\n\r\n\r\n','Part accepted','','2014-09-10','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','With Treatment','','FI','no','Misc','Nandishkumar(D.K.)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7668,'18-428A','Magellan Aerospace Wrexham','NUT ANCHOR','4732','D572 40470 200','','A',1,'RP130270','','37575','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Wrong Program given from CAD department Dia 4.76 hole pitch shift ','FAI first part checking time hole pitch dimension not achieve in drawing.  . ','Immediately inform to CAD department check the hole coordinate and change new program.         ','Drawing sheet with hole coordinate hard copy received after manufacturing.\r\n   ','Next part found okay.','','2014-09-11','Ramesh(Poojary)','Lohith(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','00','no','Misc','Anjinamurthy(H)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7669,'40-018','Universal Engineering Limited','SPIGOT','221858','D925 50006 200','','B, ECN NW23774ST1KA01',46,'318176','','36911','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Hole pitch problem.','After given the correction hole pitch not checked.  ','new fixture done to check the hole pitch and run the part.','Next every bacth we are using the fixture for checking the hole pitch.','Warned seriously and next batch found okay','','2014-09-11','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Dinakar(K)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7670,'28-007A','Magellan Aerospace New York  Inc.','Shaft Support Lever','8-17-03699','251A1747-1','Ti-6AL-4V Per Mil-T-','N/C',1,'123424-3186_R0_C0','','36351','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','1)Od under size by 0.005MM.','1) chips rubbing.2) single tool running 3)in data sheet have single tool so single tool running.\r\n','additional tool added and run the part.\r\n\r\n\r\n\r\n\r\n','additional tool added in datd sheet and run the the part for next every batch.\r\n\r\n\r\n\r\n\r\n','Process sheet updated according to requirement, Next batch found okay','','2014-09-11','Dinakar(K)','Ningaraj A N,Dinakar K,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','0','11','no','QT100S-1','NIRANJAN(N  )',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7671,'28-007A','Magellan Aerospace New York  Inc.','Shaft Support Lever','8-17-03699','251A1747-1','Ti-6AL-4V Per Mil-T-','N/C',2,'119635-3186-R0-C0','','36291','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dimension Ø .7494/.7497\r\n','Operator did not take the offset correctly.','Instructed operator to take the offset correctly.','Instructed operator to take the offset correctly.','CAPA found not evident.But next parts found good\r\n','','2014-09-11','Dinakar(K)','Sunil Kumar(K.R.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','0','01','no','Misc','NIRANJAN(N  )',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7672,'18-413B','Magellan Aerospace Bournemouth','ACTUATOR HOUSING','6067','D278 50162 200','','A',2,'RP401021_Amnd No. 1','','34608','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Thickness under size 0.05mm.','1) rough tool running time thickness undersize\r\n2) single tool running\r\n3) tool shortage\r\n','new tool orderd\r\n\r\n\r\n\r\n\r\n','additon tool adedd  this process mention in data sheet.\r\n\r\n\r\n\r\n\r\n','Next batch found satisfactory','','2014-09-11','Dinakar(K)','Shivashankar H.G.,SHIVAKUMAR ,Sathish G,Rangaswamy ,Nagaraju K.S.,GUNDEGOWDA H.G.,Dinakar K,Ashith B,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','ST20','Dinakar(K)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7673,'18-413B','Magellan Aerospace Bournemouth','ACTUATOR HOUSING','3440','D278 50162 200','','A',1,'RP401021_Amnd No. 1','','34553','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Thickness under size 0.05mm.','1) rough tool running time thickness undersize\r\n2) single tool running\r\n3) tool shortage\r\n','new tool orderd\r\n\r\n\r\n\r\n\r\n','additon tool adedd  this process mention in data sheet.\r\n\r\n\r\n\r\n\r\n','Found okay with next batches','','2014-09-11','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','Misc','Narasimha Murthy(R)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7674,'18-317A','Magellan Aerospace(Chalfont) Limited','PIN SIDE ROLLER','A0044U','F579 53066 200','S145','C',1,'P/068960','','31613','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Dia 12.654 to 12.665 measure 12.599.','1) chips rubbing.2)single tool running 3)in data sheet have single tool so single tool running.\r\n','additional tool added and run the part\r\n\r\n\r\n\r\n\r\n','additional tool added in datd sheet and run the the part for next every batch.\r\n\r\n\r\n\r\n\r\n','Next batch found okay','','2014-09-11','Dinakar(K)','Rajesh B D,Nataraja C V,Manjunatha N,KRISHNAMURTHY N,Dinakar K,Bharath R,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','QT100S-1','Narasimha Murthy(R)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7675,'35-237','Saab AB','JACK BRACKET 2','9030101','D576 50010 206','','D00',1,'1600086552','','36321','','0000-00-00',NULL,'yes','no','no','no','no','yes','no','yes','no','NDT Failure.','NDT tests has been failed, Parts to be stripped and reworked and again sent to treatments.','NDT tests has been failed, Parts to be stripped and reworked and again sent to treatments.','NDT tests has been failed, Parts to be stripped and reworked and again sent to treatments.','NDT tests has been failed, Parts to be stripped and reworked and again sent to treatments.','','2014-09-12','Avinash(R.J.)','Subramanya L Naik,Shivashankar H.G.,Shivarajakumar T M,Rangaswamy ,Mahesh N,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','0','FI','yes','MakinoF5-2','Manjunath(G)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7676,'18-317A','Magellan Aerospace(Chalfont) Limited','PIN SIDE ROLLER','A0044U','F579 53066 200','S145','C',23,'P/068960','','31613','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dia 12.654 to 12.665 measure 12.599. 							\r\n','1) chips rubbing.2)single tool running 3)in data sheet have single tool so single tool running. 							\r\n','additional tool added and run the part 							\r\n','additional tool added in datd sheet and run the the part for next every batch. 							\r\n','Next parts are okay 							\r\n						','','2014-09-12','Dinakar(K)','Dinakar K,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','1','no','QT100S-1','Narasimhamurthy(K.G.)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7677,'40-014','Universal Engineering Limited','STIFFENER BUTT STRAP ','4403102','D575 41603 200','','C01, ECN HG29999ST1TE12',1,'318176','','36899','','0000-00-00',NULL,'yes','yes','yes','','','','','','','required drill dia was 2.35 but measured dimension was 6.1 dia\r\n','requirement drill dia was 2.35 but program wrong editied and 6x100deg chamfer tool runned and dig mark noticed on part.','while program editing time care to be taken and edit proper tool number and identify the proper tool required.there fore check the tool which is on running and ensure that its a required tool.','.while program editing time care to be taken \r\n.edit proper tool number \r\n.identify the proper tool required. \r\n.check the tool which is on running and ensure that its a required tool.','Next batches found good','','2014-09-12','Narayanappa(G)','        Siddaramappa ','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7678,'18-392B','Magellan Aerospace Bournemouth','END COVER','M510610','D278 50167 200','','D',2,'RP401023_Amend No.-1','','37290','','0000-00-00',NULL,'yes','yes','yes','','','','','','','C-AXIS problem ','C-axis position  not locked in properly.','inform to the maintenence and haas maintenence team.','inform to the maintenence and haas maintenence team.','Next batch found okay','','2014-09-12','Dinakar(K)','        SHIVAKUMAR ','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7679,'18-267C','Magellan Aerospace Bournemouth','BUTTSTRAP UPP RS4X4110','2339303-2','L575 54105 200','','B00',6,'RP391492_Amnd 3','','31998','','0000-00-00',NULL,'no','no','no','yes','yes','yes','no','no','no','Machine abuse & corrosion observed on the part surface rejected at API.','Due to polishing or tool rubbing marks machine abuse was found in treatment house','Polishing should be avoided, speed and depth of cutting and tool marks should be avoided. Instructed CAD and Production to modify the program and run with low RPM','Polishing should be avoided, speed and depth of cutting and tool marks should be avoided. Instructed CAD and Production to modify the program and run with low RPM','Machine abuse FAIR done and next batch found okay','','2014-09-12','Avinash(R.J.)','Muniyappa(N)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','12170','POSTDN','no','Misc','Muniyappa(N)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7680,'18-418A','Magellan Aerospace(Blackpool) Limited','BRACKET','M390880/76561','PI55-2119010-00','','NIL',1,'P/501836','','36435','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','Profile Problem.','Model made wrong, so profile problem occured','Received Model from customer and model validated accordingly ','Validation of Model will be done by other CAD Engineers and flag notes will be keenly included in model made.','Next batch found okay','','2014-09-12','Ramesh(Poojary)','Sathisha(K.C.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','04','no','Misc','Krishna(Chowdary.G.P.)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7681,'18-419A','Magellan Aerospace(Blackpool) Limited','BRACKET','M390880/76561','PI55-2120010-00','','NIL',1,'P/501903','','36678','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','Profile Problem.','Model made wrong, so profile problem occured','Received Model from customer and model validated accordingly ','Validation of Model will be done by other CAD Engineers and flag notes will be keenly included in model made.','Next batch found okay','','2014-09-12','Ramesh(Poojary)','Sathisha(K.C.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','04','no','Misc','Krishna(Chowdary.G.P.)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7682,'18-423A','Magellan Aerospace(Blackpool) Limited','BRACKET','M498460/88620A','PI201484604','','NIL',1,'P/501935','','36397','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','Radius problem.','Chamfer done instead of Radius, wrong interpretation of Drawing and both model.','Discussed with customer and changed accordingly the model and next parts found okay','Discussed with customer and changed accordingly the model and next parts found okay','Next batch found okay','','2014-09-12','Ramesh(Poojary)','Sathisha(K.C.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','04','no','Misc','Krishna(Chowdary.G.P.)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7683,'18-422A','Magellan Aerospace(Blackpool) Limited','BRACKET','20397/4208','PI201484603','','NIL',1,'P/501934','','36396','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','Profile problem.','Chamfer done instead of Radius, wrong interpretation of Drawing and both model.','Discussed with customer and changed accordingly the model and next parts found okay','Discussed with customer and changed accordingly the model and next parts found okay','Next batch found okay','','2014-09-12','Ramesh(Poojary)','Sathisha(K.C.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','04','no','Misc','Krishna(Chowdary.G.P.)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7684,'30-114','Gardner Aerospace-Derby Limited','RIB 4 OFW - LH','5440602','L575 53502 200','','A00',1,'LPR0000020*','','36997','','0000-00-00',NULL,'yes','no','yes','no','yes','no','no','no','no','part rib top thickness in -side ','machine nc control problem','stop the production and in informed to the service engineers','1)ask for preventive maintenance for every 3 month from service person\r\n2)plan for check machine at regular intervals of period','CA/PA Satisfaction ok','','2014-09-13','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,'$','Closed','no','yes','no','Manufacture Only','','3','no','HAAS','Narayanappa(G)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7685,'28-041','Magellan Aerospace New York  Inc.','LEVER ASSY-SECONDARY SPOI','158320','65-46358-16','','PL_E, DL_N/C, Sketch # 1',1,'122999_R0_C0','','37181','','0000-00-00',NULL,'yes','yes','yes','','','','','','no','Thickness under size due to clamping problem','This setup consists of facing of the part, and while doing this setup the slot will be packed by wax.By the force of coolant or the vibration of the part, if the wax slips down means thickness under size may happen.','As this case happens very rarely , the waxing is ensured twice so that it should not slip down. \r\n','As this case happens very rarely , the waxing is ensured twice so that it should not slip down. ','Next batch found satisfactory','','2014-09-13','Anjinamurthy(H)','        Manohara M','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7686,'18-387A','Magellan Aerospace(Chalfont) Limited','NUT RING INNER','224312','D575 40039 202','','B',8,'P/068966','','29064','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','5mm Thickness undersize(-0.3mm).','1) running time parting insert brocken\r\n2) that time parting tool will be blented\r\n3) parting insert not locking properly\r\n4) that time taper will occure.\r\n','process changed first parting done then keyway done.\r\n\r\n\r\n\r\n\r\n','This process is continue for next every batch.','Next Batches found okay','','2014-09-15','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','1','no','Misc','Narasimhamurthy(K.G.)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7687,'35A-239','Saab AB','L/H KIT FOR ARD HINGE / J','','9901503-993','','Exhibit-B',6,'1600082175','','K00051','','0000-00-00',NULL,'no','no','no','no','no','no','yes','yes','yes','Primer breakage noticed.','1)primer breakage noticed due to lack of adesion during anodising process.','1)Refer MOM dated 12th june 2013.','1)Refer MOM dated 12th june 2013.','Next batch found correct.','C30441','2014-09-15','Avinash(R.J.)','Avinash(R.J.)','Through mail from SAAB','2014-07-04','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','Assembly','','FI','no','Misc','Avinash(R.J.)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7688,'35A-239','Saab AB','L/H KIT FOR ARD HINGE / J','','9901503-993','','Exhibit-B',8,'1600076514','','k00049','','0000-00-00',NULL,'no','no','no','no','no','no','yes','yes','yes','Primer breakage noticed.','1)primer breakage noticed due to lack of adesion during anodising process.','1)Refer MOM dated 12th june 2013.','1)Refer MOM dated 12th june 2013.','Next batch found correct.','C29708','2014-09-15','Avinash(R.J.)','Avinash(R.J.)','Through mail from SAAB','2014-07-04','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','Assembly','0','FI','no','Misc','Avinash(R.J.)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7689,'35A-239','Saab AB','L/H KIT FOR ARD HINGE / J','','9901503-993','','Exhibit-B',1,'1600074206','','K00047','','0000-00-00',NULL,'no','no','no','no','no','no','yes','yes','yes','Primer breakage noticed.','1)primer breakage noticed due to lack of adesion during anodising process.','1)Refer MOM dated 12th june 2013.','1)Refer MOM dated 12th june 2013.','Next batch found correct.','C28962','2014-09-15','Avinash(R.J.)','Avinash(R.J.)',' 	Through mail from SAAB','2014-07-04','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','Assembly','0','FI','no','Misc','Avinash(R.J.)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7690,'35A-240','Saab AB','R/H KIT FOR ARD HINGE / J','','9901503-994','','Exhibit-B',5,'1600082175','','K00052','','0000-00-00',NULL,'no','no','no','no','no','no','yes','yes','yes','Primer breakage noticed. ','1)primer breakage noticed due to lack of adesion during anodising process.','1)Refer MOM dated 12th june 2013.','1)Refer MOM dated 12th june 2013.','Next batch found correct.','C30440','2014-09-15','Avinash(R.J.)','Avinash(R.J.)','Through mail from SAAB','2014-07-04','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','Assembly','0','FI','no','Misc','Avinash(R.J.)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7691,'35A-240','Saab AB','R/H KIT FOR ARD HINGE / J','','9901503-994','','Exhibit-B',11,'1600076514','','K00050','','0000-00-00',NULL,'no','no','no','no','no','no','yes','yes','yes','Primer breakage noticed.','1)primer breakage noticed due to lack of adesion during anodising process. ','1)Refer MOM dated 12th june 2013.','1)Refer MOM dated 12th june 2013.','Next batch found correct.','C29709','2014-09-15','Avinash(R.J.)','Avinash(R.J.)','Through mail from SAAB','2014-07-04','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','Assembly','0','FI','no','Misc','Avinash(R.J.)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7692,'18-383A','Magellan Aerospace(Chalfont) Limited','SLEEVE BEARING ','Y11518','D575 40037 202','','A',1,'P/074123','','37245','','0000-00-00',NULL,'yes','yes','yes','','','','','','','bore gauge problem.','Due to problem in process  these error was occurred.','Instructed to operator for dialing every part and then\r\nrun the part and adding one more tool before finishing.','Some minor changes was planed for further batches and same feed back will be taken and updated.','Next batch found satisfactory','','2014-09-16','Dinakar(K)','        Manjunatha N','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7693,'28-041','Magellan Aerospace New York  Inc.','LEVER ASSY-SECONDARY SPOI','158326','65-46358-16','','PL_E, DL_N/C, Sketch # 1',1,'122999_R0_C0','','37180','','0000-00-00',NULL,'yes','yes','yes','','','','','','no','ID (+)side0.05mm.',' Pit mark observed  in bore. part rework  after  that bore over size.','Instructed to production changed the coolant.','Instructed to production changed the coolant.','Under review.  ','','2014-09-16','Dinakar(K)','        Dinakar K','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7694,'35-166A','Saab AB','HOUSING PIN','657639A1','423Z1124-6-01','','--A',1,'1600086478','','35807','','0000-00-00',NULL,'yes','no','no','no','no','yes','no','yes','no','NDT Failure.','Dent mark observer on the part.','Dent mark removed by using polishing method.','instructed to concerned inspector to check the part usaualy carefully.','CA/PA found satisfactory.','','2014-09-16','Avinash(R.J.)','Yogesha K,Prashanth Kumar M,Basavaraja S. Jr.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','0','FI','yes','MakinoF5-3','Manjunath(G)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7695,'35-046','Saab AB','7605148-200','548108','L574 55148 200','ABM3 1029','A00',2,' PA1226-1 (Aluminium','','37323','','0000-00-00',NULL,'no','no','no','yes','no','yes','no','yes','no','NDT Failure.','NDT tests failed in treatment house due to material behavior\r\n','100% RM inspection will be carried out in future batches , and informed to RM supplier\r\n','100% RM inspection will be carried out in future batches , and informed to RM supplier\r\n','Next RM was checked and found okay in treatment house also','','2014-09-16','Avinash(R.J.)','Rangaswamy(H A)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','0','FI','yes','Misc','Manjunath(G)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7696,'18-123A','Magellan Aerospace Bournemouth','FORK END OUT BD','238300','D575 41546 202','S80 FHT','B',3,'RP400840','','36938','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Thread effective dia o.03 oversize.','Thread gauge was not butting.','Next time thread gauge kept to be free.','Any threaded parts after machining checked in machine before removing.','Next batch found okay','','2014-09-16','Dinakar(K)','Ravi M,Girish V M,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Manufacture Only','','3','yes','DX 200-2 ','Narasimhamurthy(K.G.)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7697,'18-277A','Magellan Aerospace(Chalfont) Limited','DOOR OUTER TYPE 27R','9170604','L572 53719 200','ABS5032A055','D00',1,'P/074116','','37226','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Base thickness measures 0.05mm.','Due to process problem this deviation are coming.\r\nAfter operation-01 part bend and twist observing, causes thickness variation by part by part in operation-02.','Planned to run the operation-01 and 02 parallel in two machines to avoid bend and twist.\r\nThis process are working and part thickness measures ok and also finding consistency part by part.','But above corrective action will not permanent,planned and informed to CAD to change the process to get the consistency of the parts.\r\nStill for scheduling propose parts are running with above CA.','Next part found okay','','2014-09-16','Girish(Prasad P)','        Girish Prasad P','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7698,'35-238','Saab AB','JACK BRACKET 2','601496A3','D576 50010 207','','D00',2,'1600086552','','36225','','0000-00-00',NULL,'yes','no','no','no','no','yes','no','yes','no','NDT Failure.','NDT tests has been failed, Parts to be stripped and reworked and again sent to treatments.','NDT tests has been failed, Parts to be stripped and reworked and again sent to treatments.','NDT tests has been failed, Parts to be stripped and reworked and again sent to treatments.','Parts have been stripped and reworked and sent for treatments','','2014-09-17','Avinash(R.J.)','Subramanya L Naik,Shivashankar H.G.,Shivarajakumar T M,Rangaswamy ,Nagaraju K.S.,Mahesh N,Krishna Chowdary.G.P.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','0','FI','yes','MakinoF5-2','Manjunath(G)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7699,'35-235','Saab AB','JACK BRACKET 1','131202','D576 50009 206','','D00',1,'1600086552','','35955','','0000-00-00',NULL,'yes','no','no','no','no','yes','no','yes','no','NDT Failure.','NDT tests failed in treatment house due to material behavior\r\n','100% RM inspection will be carried out in future batches , and informed to RM supplier\r\n','100% RM inspection will be carried out in future batches , and informed to RM supplier\r\n','Found okay in next batches\r\n','','2014-09-17','Avinash(R.J.)','Subramanya L Naik,Shivashankar H.G.,Shivarajakumar T M,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','0','FI','yes','MakinoF5-2','Manjunath(G)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7700,'28-004A','Magellan Aerospace New York  Inc.','PIN','G20551K01','161A2332-1','15-5PH Steel Bar per','NA',1,'120243-3172','','37092','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','od undersize by 0.05 to 0.02 mm','While doing OD turning chips clocking on part and chattering coming then to avoid chattering again re pass done for this part,then deviation coming.  ','For next part OD turning operation done with stock,then inspected the part.After checking then  run the finishing pass.','Program changed to cut with stock for first pass.Then after\r\nroughing operation finishing pass running to avoid such\r\nproblem.','Next batch found good.','','2014-09-17','Dinakar(K)','Devaraj(K.C.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','09','no','Misc','Sandhesh D(S)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7701,'18-382A','Magellan Aerospace(Chalfont) Limited','SLEEVE BEARING ','226100','D575 40037 200','','A',1,'P/074123','','36599','','0000-00-00',NULL,'yes','yes','yes','','','','','','','ID ovality problem (+ 5 Microns)','while running the id finishing program scrap rubbed in\r\ndiameter.','one more finishing pass added , 2nd pass will be complete the dimension.','One more finishing pass added for finishing , do not skip that pass.','Next batch found good','','2014-09-17','Dinakar(K)','        Bharath R','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7702,'18-416A','Magellan Aerospace(Blackpool) Limited','BRACKET','M362250/72801','PI55-2119004-00','','NIL',1,'P/501835','','36502','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','2mm Profile shifted.','This deviation for FAI part, As per RM master RM taken for proving the part, But CAD file generated for wrong dimension.\r\nRM master dimension and CAD file dimensions are not matching.\r\n','After rejected the FAI part, Immediately deleted the CAD file and checked the RM master with part model and found Ok.\r\nThen regenerated the CAD file as per RM master dimension.\r\n','Informed to CAD to check the RM master dimensions before starting the CAM program.','Next part found okay','','2014-09-17','Ramesh(Poojary)','Lokesh(B.D.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','06','no','Misc','Krishna(Chowdary.G.P.)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7703,'18-417A','Magellan Aerospace(Blackpool) Limited','BRACKET','M362250/72801','PI55-2120004-00','','NIL',1,'P/501902','','36394','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','2mm Profile shifted.','This deviation for FAI part, As per RM master material taken for proving the part, But CAD file generated for wrong dimension.\r\nRM master dimension and CAD file dimensions are not matching.\r\n','After rejected the FAI part, Immediately deleted the CAD file and checked the RM master with part model and found Ok.\r\nThen regenerated the CAD file as per RM master dimension.\r\n','Informed to CAD to check the RM master dimensions before starting the CAM program.','Next part found okay','','2014-09-17','Ramesh(Poojary)','Lokesh(B.D.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','06','no','Misc','Krishna(Chowdary.G.P.)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7704,'18-423A','Magellan Aerospace(Blackpool) Limited','BRACKET','M498460/88620A','PI201484604','','NIL',1,'P/501935','','37739','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dig mark observed on face','Chamfer done instead of Radius, wrong interpretation of Drawing and both model.','Discussed with customer and changed accordingly the model and next parts found okay','Discussed with customer and changed accordingly the model and next parts found okay','Next batch found okay','','2014-09-17','Krishna(Chowdary.G.P.)','Rangaswamy()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','04','no','Misc','Krishna(Chowdary.G.P.)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7705,'30-081','Gardner Aerospace-Derby Limited','FITTING FWD','467340','L575 52120 201','','A00',1,'LPR0000576','','36361','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Running time 16r3 tool down  so thicknes (-) side.','Tool holding length problem ,holding in hydrogrip holder, so tool running time down.','Change the holder Using collet holder then run.','To change tool length , using length 110mm, change tool length 130mm. so holding 20mm extra.','CA/PA CHECKED FOUND OK.','','2014-09-17','Rangaswamy()','        Mahesh N','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7706,'18-221A','Magellan Aerospace(Chalfont) Limited','PIN CON N/DRIVEN','B4479A','L579 51163 200','S145 FHT','A00',1,'P/074115','','34045','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','bore (+) side','while offset taken time, he give a cut for finished bore. so part will over sized.','give the instruction for operator and run the part. ','training give the operator. before setting check the process sheet and then do the setting.','Next batch found okay.','','2014-09-18','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','03','no','Misc','Dinakar(K)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7707,'18-087B','Magellan Aerospace Wrexham','Plate Sealing','420582','D572 52914 200','ABM3 1029','B',21,'RP127045','','35501','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Conductivity under size.','After machining RAW Material conductivity found low to required spec.','Conductivity and Material certificates should be checked by stores quality person and should put seal for the document. Instructions given to RM supplier to check the conductivity twice and send the parts.','Conductivity and Material certificates should be checked by stores quality person and should put seal for the document. Instructions given to RM supplier to check the conductivity twice and send the parts.','Next RM found okay with the conductivity','','2014-09-18','Avinash(R.J.)','Muniyappa(N)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','14294','Post DN','yes','Misc','Muniyappa(N)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7708,'18-382A','Magellan Aerospace(Chalfont) Limited','SLEEVE BEARING ','226100','D575 40037 200','','A',1,'P/074123','','36599','','0000-00-00',NULL,'yes','yes','yes','','','','','','','running time part ratated','1) grooving tool running time part rotating.2) chuck pressure low 3)if high pressure given ovality will occure\r\n4)becouse itz have a closed tollerance.\r\n','mention the chuck pressure and same pressure used for every batch \r\n\r\n\r\n\r\n\r\n','mention the chuck pressure and same pressure used for every batch \r\n\r\n\r\n\r\n\r\n','Next batch found okay','','2014-09-18','Dinakar(K)','                Dinakar K','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7709,'18-392B','Magellan Aerospace Bournemouth','END COVER','M510610','D278 50167 200','','D',3,'RP401023_Amend No.-1','','37290','','0000-00-00',NULL,'yes','no','yes','no','yes','no','no','no','no','C-axis problem,so profile shift.','C-axis position not locked in properly. \r\n','inform to the maintenence and haas maintenence team.','inform to the maintenence and haas maintenence team.','AMC gave to Haas Team itself and next batch found okay','','2014-09-18','Dinakar(K)','SHIVAKUMAR ,Dinakar K,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','3','no','ST20','Narasimhamurthy(K.G.)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7710,'35-192','Saab AB','SUPPORT-FTG','675763A7','423Z1202-14','','---',1,'1600087079','','36779','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dig mark on part due to wrong loading in operation-05.','Loading time operator wrong loading.','This setup using zero point system to locket fixture in dia 10 location in both side ,next change location dia 10 & dia 12 using.fixture not locket wrong loading.','This setup using zero point system to locket fixture in dia 10 location in both side ,next change location dia 10 & dia 12 using.fixture not locket wrong loading.','Next part found okay','','2014-09-18','Krishna(Chowdary.G.P.)','Rangaswamy()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','05','no','Misc','Krishna(Chowdary.G.P.)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7711,'18-415B','Magellan Aerospace Bournemouth','ACTUATOR HOUSING','20005','D278 50163 201','','D',1,'RP401022_Amend No 1','','37216','','0000-00-00',NULL,'yes','yes','yes','','','','','','no','A0 not giving from program so part profile dig mark.','A0 not giving from program so part profile dig mark.','Training given to operator regarding A0 and training was success and operator found good , and before setting time supervisor will be witnessing the whole process of setting','Training given to operator regarding A0 and training was success and operator found good , and before setting time supervisor will be witnessing the whole process of setting','Next part found okay','','2014-09-18','Girish(Prasad P)','        Basavaraja S. Jr.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7712,'18-381B','Magellan Aerospace Bournemouth','GAMMA FITTINGS ','M510650 89213A','NSA840020-400','','L',2,'RP401481_Amend No.-1','','37203','','0000-00-00',NULL,'yes','yes','yes','','','','','','','12.7 lathu prebiem and ovruliyt','The Following route cause analyzed for the parts rejected, 1. Ovality in RM. 2. Total Length Minus\r\nin RM. 3. Improper Butting in Jaws. 4. Jaws Boring is not good( Flatness is not achieved. 5. RM\r\nunclear on OD and ID. 6. Ovality More than 0.05mm in billet stage. 7. Chips clocking at the Jaws ,\r\nIn 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. ','Very next parts found okay','','2014-09-18','Dinakar(K)','                Girish L N','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7713,'18-252B','Magellan Aerospace Bournemouth','BUTTSTRAP INBD FIXED PNL','409898','L575 52464 201','ABM3 1029','A00',1,'RP401009','','37755','','0000-00-00',NULL,'yes','yes','yes','','','','','','no','Dig mark found on the outer profile ','As this setup is of cut out of the profile the clamping cannot be done here, 0.1 mm stock is left out in this setup. Due to vibration , dig mark observed on the face ','Tool wear edited for the next part stock left was adjusted for 0.3 stock of the part so that if any vibration occurs also chances of dig mark is very less','2 clamping holes are being introduced and clamping is made so that the part is fully butted to the part and tool wear is also adjusted and taken care of future batches','Next batch found satisfactory','','2014-09-18','Anjinamurthy(H)','        S. Shiva Kumar','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7714,'18-093A','Magellan Aerospace Bournemouth','PRESSURE RING','66900/01/00','D301 50085 202','L164 T4','A',1,'RP400844','','35127','','0000-00-00',NULL,'no','yes','no','yes','no','yes','no','no','no','Corrosion observed on the part','Due to polishing or tool rubbing marks machine abuse was found in treatment house','Polishing should be avoided, speed and depth of cutting and tool marks should be avoided. Instructed CAD and Production to modify the program and run with low RPM & parts should be cleaned with PX-24 solvent on regular intervals','Polishing should be avoided, speed and depth of cutting and tool marks should be avoided. Instructed CAD and Production to modify the program and run with low RPM & parts should be cleaned with PX-24 solvent on regular intervals','Next batches found okay','','2014-09-18','Avinash(R.J.)','Muniyappa(N)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','POST DN','no','Misc','Muniyappa(N)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7715,'18-414B','Magellan Aerospace Bournemouth','ACTUATOR HOUSING','M534810/92191A','D278 50163 200','','D',4,'RP401021_Amnd No. 1','','34543','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','chips mark observed on the taper OD & insideside 6.0mm thickness Machine abuse. ','Due to polishing or tool rubbing marks machine abuse was found in treatment house','Polishing should be avoided, speed and depth of cutting and tool marks should be avoided. Instructed CAD and Production to modify the program and run with low RPM','Polishing should be avoided, speed and depth of cutting and tool marks should be avoided. Instructed CAD and Production to modify the program and run with low RPM','Machine abuse FAIR done and next batch found okay','','2014-09-18','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','14327','POSTDN','no','Misc','Muniyappa(N)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7716,'40-015','Universal Engineering Limited','STIFFENER BUTT STRAP','4403102','D575 41603 201','','C01, ECN HG29999ST1TE12',1,'318176','','36901','','0000-00-00',NULL,'yes','yes','yes','','','','','','','While Cut out Part Rotate.','While running production due to clamping strength is less part rotates when final cutout program running.','Checked the final Z value in program and altered the Z value for more strength to avoid movement.\r\nChecked the parameters and found ok.','Checked the final Z value in program and altered the Z value for more strength to avoid movement.\r\nChecked the parameters and found ok.\r\n\r\nAfter PA taken, next all the parts found ok.','Next part found okay','','2014-09-19','Narayanappa(G)','        Gajendra Singh C.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7717,'18-394A','Magellan Aerospace Bournemouth','VALVE BODY','456336','A284 40009 200','','A',1,'RP400947','','35611','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dia 4.35 pin nogo answerd.','1)4.40 drill running time nogo answer.','dia 4.35 drill running part checked found ok. ','dia 4.35 drill running part checked found ok using next every bacth same drill. ','Next batch found okay','','2014-09-19','Dinakar(K)','Manjunatha N,Dinakar K,Bharath R,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','1','no','QT100S-2','Narasimhamurthy(K.G.)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7718,'18-087B','Magellan Aerospace Wrexham','Plate Sealing','420582','D572 52914 200','ABM3 1029','B',2,'RP127045','','35501','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Low conductivity found on these parts','After machining RAW Material conductivity found low to required spec.','Conductivity and Material certificates should be checked by stores quality person and should put seal for the document. Instructions given to RM supplier to check the conductivity twice and send the parts.\r\n','Conductivity and Material certificates should be checked by stores quality person and should put seal for the document. Instructions given to RM supplier to check the conductivity twice and send the parts.\r\n','Next RM found okay with the conductivity','','2014-09-19','Avinash(R.J.)','Muniyappa(N)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','','POST DN','yes','Misc','Muniyappa(N)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7719,'18-214A','Magellan Aerospace(Chalfont) Limited','SPECIAL WASHER ','472203','D321 40210 202','','E01, ECN NR29999ST1JB79',11,'P/074114','','35506','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Broching problem 2mm width under size.','As the broaching operation is doing manually, this problem is getting repeated from long time','New fixture was manufactured and part found okay','New fixture was manufactured and part found okay','Next batch found satisfactory','','2014-09-20','Anjinamurthy(H)','S. Shiva Kumar,Ningaraj A N,Nandeesha N,Manjunatha N.R.,Kalakappa T H,Dinakar K,Anjinamurthy H,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','FI','no','BMV 60-1','Narasimha Murthy(R)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7720,'18-414B','Magellan Aerospace Bournemouth','ACTUATOR HOUSING','20005','D278 50163 200','','D',3,'RP401021_Amnd No. 1','','36612','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Machine abuse found in 3 nos','Due to polishing or tool rubbing marks machine abuse was found in treatment house','Polishing should be avoided, speed and depth of cutting and tool marks should be avoided. Instructed CAD and Production to modify the program and run with low RPM','Polishing should be avoided, speed and depth of cutting and tool marks should be avoided. Instructed CAD and Production to modify the program and run with low RPM','Machine abuse FAIR done and next batch found okay','','2014-09-20','Avinash(R.J.)','Muniyappa(N)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','POST DN','no','Misc','Muniyappa(N)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7721,'35-242','Saab AB','BUSHING','1465374','423Z1416-2','','---',1,'PA 1510 STEEL','','37411','','0000-00-00',NULL,'yes','no','no','no','no','yes','no','yes','no',' chamfer done instead of radius at the hole','This has happen due to misinterpretation of specs and not saw the flag notes properly','Checklists have been made so that none of the specs and flag notes will not miss in future, Instructions have been given to all CAD Engineers and this will be Validated by Head CAD','Checklists have been made so that none of the specs and flag notes will not miss in future, Instructions have been given to all CAD Engineers and this will be Validated by Head CAD','Next batch found okay','','2014-09-20','Ramesh(Poojary)','Sameer Kumar(Pradhan)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','02','no','Misc','Avinash(R.J.)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7722,'34-012B','Magellan Aerospace Winnipeg','STAND-OFF RH CENTRE ','52302-2','400-12602-2-905','','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','','37503','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Wall thickens under size by -0.2','Fixture 5 deg  angle wear out so part running time part lifted\r\n  \r\n','New Fixture already manufacturing done. Fixture used in next batch production.','New Fixture already manufacturing done. Fixture used in next batch production.','Next batch will be monitored for effectiveness','','2014-09-20','Lohith(K)','Hari(Prasad)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','07','no','Misc','Hari(Prasad)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7723,'18-211B','Magellan Aerospace(Chalfont) Limited','PLUNGER','238302','D321 40205 200','','H01, ECN NR29998ST1JB80',1,'P/074114','','37554','','0000-00-00',NULL,'yes','yes','yes','','','','','','','o d re work time -','Chips clogged during operation and caused the deviation.\r\n','Instructed Operator to clean the chips clogging onto the tool tip periodically.\r\n','Instructed Operator to clean the chips clogging onto the tool tip periodically.\r\n','Next Batches found okay','','2014-09-20','Dinakar(K)','        Ningaraj A N','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7724,'18-106A','Magellan Aerospace Bournemouth','EYE END INBOARD','512111','D575 41542 200','S98 FHT','D',1,'RP400841','','37633','','0000-00-00',NULL,'yes','yes','yes','','','','','','no','bore +sede  running time','Machine Problem while machining, bore becomes plus side, reason for that is under investigation','Machine Problem while machining, bore becomes plus side, reason for that is under investigation','Machine Problem while machining, bore becomes plus side, reason for that is under investigation','Machine Problem while machining, bore becomes plus side, reason for that is under investigation','','2014-09-21','Anjinamurthy(H)','        Mohan Kumar C.M.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7725,'18-382A','Magellan Aerospace(Chalfont) Limited','SLEEVE BEARING ','226100','D575 40037 200','','A',2,'P/074123','','36599','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','OD ovality.','Due to while OD operation running time insert brokened\r\nso OD under size. ','New insert added and tool offset takened run the part and checked the od dimension is ok continuve the production.\r\n','Instructed operator to every 50 nos will be completed checked the insert. ','Next batch found okay','','2014-09-22','Dinakar(K)','Subramanya L Naik,Shivarajakumar T M,Ningaraj A N,Manjunatha N,Dinakar K,Bharath R,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','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,NULL),(7726,'18-382A','Magellan Aerospace(Chalfont) Limited','SLEEVE BEARING ','226100','D575 40037 200','','A',2,'P/074123','','36599','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Thread tight.','Thread gauge was not butting.','Next time thread gauge kept to be free. ','Any threaded parts after machining checked in machine before removing. ','Next batch found okay','','2014-09-22','Dinakar(K)','Subramanya L Naik,Shivarajakumar T M,Ningaraj A N,Manjunatha N,Dinakar K,Bharath R,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Manufacture Only','','FI','yes','QT100S-2','Narasimha Murthy(R)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7727,'34-010B','Magellan Aerospace Winnipeg','STAND-OFF R/H UPPER','52311-2','400-12601-2-905','','EM104302 Iss A, EM104765 Iss G, EM105092 Iss F, EM106399 Iss B, EM106400 Iss B, EM106401 Iss A, EM106404 Iss A, EM106522 Iss A, EM106602 Iss A',2,'B91379 Rev-024','','35418','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Hole position 0.007\" measures 0.012\"','For this batch production while doing hole finish operation due to run out in free drill hole position not achieved.','After checking the part find the problem and new carbide drill placed and after hole mill done.Then checked the hole position as per drg is OK.','Inform to operator to check the drill tip while doing setting to avoid such problems in next batches.','Next batch found okay with this problem','','2014-09-22','Lohith(K)','Theerthappa K.N.,Shivaraj K S,Punith G S,Lohith K,Hari Prasad,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','FI','no','HAASVF2SS','Sudhagar(V)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7728,'34-009B','Magellan Aerospace Winnipeg','STAND-OFF L/H UPPER','G17965','400-12601-1-905','','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-024','','35434','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1)Dig mark observed on part & thickness undersized.','While doing production, part lifts from fixture then dig mark observed.','1.Informed to operator to clamp the part correctly and also ensure once before running the program.','After clamping the part ,every part will be checked using feeler for air gaps between part and fixture.','Next batch found okay','','2014-09-22','Lohith(K)','Theerthappa K.N.,Shivaraj K S,Punith G S,Lohith K,Hari Prasad,Dhananjaya N,Anjinamurthy H,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','0','FI','no','HAASVF2SS','Sudhagar(V)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7729,'34-009B','Magellan Aerospace Winnipeg','STAND-OFF L/H UPPER','50126-2','400-12601-1-905','','EM104302 Iss A, EM104765 Iss G, EM105092 Iss F, EM106399 Iss B, EM106400 Iss B, EM106401 Iss A, EM106404 Iss A, EM106522 Iss A, EM106602 Iss A',1,'B91379 Rev-024','','35435','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1)Thickness under size by 0.10MM.','The part was not butted in the fixture properly which was slightly lifted while finishing the base thickness.','1.The part was kept separately for further investigation and NC was raised .\r\n2.The program was studied in brief so as to avoid the escapes 3.All the tool offset was reseted .','After loading the part into the fixture,it will be checked for air gaps between the part and the fixture using the feeler gauge and then start the machining.','Next batch found okay','','2014-09-22','Lohith(K)','Theerthappa K.N.,Shivaraj K S,Punith G S,Lohith K,Hari Prasad,Dhananjaya N,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','0','FI','no','HAASVF2SS','Sudhagar(V)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7730,'18-225A','Magellan Aerospace Bournemouth','CLAMP BLOCK','4552263','D282 50123 204','NYLON 66','A',6,'RP400846','','36698','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dia 5.5 hole formed to radius  ','Coolant was not flown to the hole so that the hole diameter not formed properly.','Ensure that the coolant is flowing properly while machining.','Ensure that the coolant is flowing properly while machining.','Next part found okay.','','2014-09-22','Girish(Prasad P)','Girish(Prasad P)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','00','no','Misc','Anjinamurthy(H)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7731,'18-416A','Magellan Aerospace(Blackpool) Limited','BRACKET','M362250/72801','PI55-2119004-00','','NIL',1,'P/501835','','37761','','0000-00-00',NULL,'yes','no','no','no','no','yes','no','yes','no','Sl no 25 in Bubble drawing,  Actual Dimension 11.543 +/- 0.25 measures 11.28. ','Model which we prepared was wrong, so dimension deviation occured','Validation of the model will be done by other CAD Engineers , for every FAI part model validation will be done','Validation of the model will be done by other CAD Engineers , for every FAI part model validation will be done','Next batch found okay','','2014-09-22','Ramesh(Poojary)','Sameer Kumar(Pradhan)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','FI','no','Misc','Avinash(R.J.)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7732,'18-417A','Magellan Aerospace(Blackpool) Limited','BRACKET','M362250/72801','PI55-2120004-00','','NIL',1,'P/501902','','37760','','0000-00-00',NULL,'yes','no','no','no','no','yes','no','yes','no','Sl no 25 in Bubble drawing, Actual Dimension 11.543 +/- 0.25 measures 11.28.','Model which we prepared was wrong, so dimension deviation occured','Validation of the model will be done by Head CAD, for every FAI part model validation will be done','Validation of the model will be done by Head CAD, for every FAI part model validation will be done','Next batch found okay','','2014-09-22','Ramesh(Poojary)','Sameer Kumar(Pradhan)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','FI','no','Misc','Avinash(R.J.)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7733,'18-413B','Magellan Aerospace Bournemouth','ACTUATOR HOUSING','3440','D278 50162 200','','A',14,'RP401021_Amnd No. 1','','34553','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','It was observed during source inspection that part marking was done on the wrong place in all the 14nos','As the operator was new due to misinterpretation part marking was done on wrong side','Operator replaced and necessary training provided not to repeat these mistakes, First off for part marking introduced and 100% Visual inspection will be done Final inspection','Operator replaced and necessary training provided not to repeat these mistakes, First off for part marking introduced and 100% Visual inspection will be done Final inspection','Next batches found okay','','2014-09-22','Avinash(R.J.)','Muniyappa(N)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','','CUST END','yes','Misc','Muniyappa(N)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7734,'18A-001','Magellan Aerospace Wrexham','BRACKET - ASSY','','D361 50110 000','','A',1,'RP125887','','A03561','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','It was observed during source inspection that part marking(W O No.) was marked as A3561 instead of  A03561 in 01nos','It was happen by the new part marking operator, by visual misinterpretation he did this mistake ','Assembly part marking first off will be done and reference photo graphs will be available for the partmarking . New operator replaced by old operator who was well trained.','Assembly part marking first off will be done and reference photo graphs will be available for the partmarking . New operator replaced by old operator who was well trained.','Next part found okay','','2014-09-22','Avinash(R.J.)','Muniyappa(N)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUST END','yes','Misc','Muniyappa(N)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7735,'18-263C','Magellan Aerospace Bournemouth','BUTTSTRAP UPP RS4X2390 ','5298501-3','L575 54101 200','','B00',1,'RP391492_Amnd 3','','32252','','2014-08-21',NULL,'yes','yes','no','no','no','no','no','no','yes','Deep Tool Gauge of Buttstrap which runs through an earthing point ( As Marked)','This was happen due to part not butting properly to the fixture,chips might have clogged to the fixture, operator might have missed and even same in Final inspection','Training has been given to operator to butt the part properly and ensure with feeler gauge.\r\n100% visual inspection will be done in future batches','Training has been given to operator to butt the part properly and ensure with feeler gauge.\r\n100% visual inspection will be done in future batches','Next part found okay','C31057','2014-09-22','Avinash(R.J.)','Muniyappa(N)','RDN 01517','2014-08-21','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','DN12828','CUST END','no','Misc','Muniyappa(N)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7736,'34-012B','Magellan Aerospace Winnipeg','STAND-OFF RH CENTRE ','50508-2','400-12602-2-905','','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-024','','35428','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1)Thickness under size by 0.10MM.','Fixture 5 deg  angle wear out so part running time part lifted \r\n  \r\n','New Fixture already manufacturing done. Fixture used in next batch production.','New Fixture already manufacturing done. Fixture used in next batch production.','Next batch will be monitored for effectiveness','','2014-09-23','Lohith(K)','Theerthappa K.N.,Shivaraj K S,Punith G S,Lohith K,Hari Prasad,Dhananjaya N,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','0','FI','no','HAASVF2SS','Sudhagar(V)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7737,'28-016','Magellan Aerospace New York  Inc.','STOP FITTING','G20388K08','161A6119-1','15-5PH Per AMS 5659 ','N/C',1,'123151','','35132','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1)Chemfer over size by 0.10MM.','Chamfer tool was not in proper cone shape , because of this problem chamfer got oversize','Instructions given to tool head that to procure proper cone head chamfer tool','Instructions given to tool head that to procure proper cone head chamfer tool','Next batch found okay','','2014-09-23','Lohith(K)','Punith G S,Dhananjaya N,Anjinamurthy H,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','0','FI','no','VM2-1','Sudhagar(V)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7738,'18-305A','Magellan Aerospace(Chalfont) Limited','HINGE ','425391','D572 59245 202','ABM3 1029','B, ECN NG29999ST2TY72',1,'P/074120','','37697','','0000-00-00',NULL,'yes','yes','yes','','','','','','','1nos wall thickness 0.1 -side so part rejected...','1) Thickness was reduced due to vibration while machining. 2) Fixture plate was not centerlised to base plate that loaded end to the base plate. \r\n','1) For next part fixture was centerlised to base plate and machining performed. ','1)Fixture to be replaced with new and to be made in steel plate. ','Next batch found satisfactory','','2014-09-23','Anjinamurthy(H)','        Manjunatha N.R.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7739,'28-004A','Magellan Aerospace New York  Inc.','PIN','G20551K01','161A2332-1','15-5PH Steel Bar per','NA',1,'120243-3172','','37553','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Part accepted.','','','','','','2014-09-23','Dinakar(K)','        Devaraj K.C.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7740,'28-005','Magellan Aerospace New York  Inc.','SHOULDER BOLT','G19876K01','162A3109-1','15-5PH Steel bar per','A',6,'120162_R0_C1','','35451','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','OD under size by 0.005 to 0.015.\r\n','It is happened due to insert problem.New insert loaded but operator was not cross checked whether insert properly\r\nseatted or not.','loaded the insert properly & cross checked dimension for\r\nseveral components and found within tolerance.  ','1) Proper training given to the operators\r\nregarding the above NC.\r\n2) Training planned on Six Sigma and mainly concentrating on quality tools like SPC and Gauge R and R.','Next batch found okay','','2014-09-23','Dinakar(K)','Seetharamu D,Ravi M,Rajesh B D,Punith G S,Lohith K,KRISHNAMURTHY N,Girish V M,Dhananjaya N,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','0','FI','no','DX 200-2 ','Sudhagar(V)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7741,'35-144A','Saab AB','BCD_LATCH_PROBE__FTG_HOUS','574402A4','424Z6115-4-01','','--C',5,'1600073861','','34491','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','pocket inside step under size. (1.0 mm)','Actually this was happened in night shift, As the operator was new for work and he misunderstood the drawing spec and cleared out the step in the part which was required','1. As this parameter should be cross checked by CATIA Model only requested to CAD department to add a photocopy of the Model in process sheet.\r\n2. Separate file is getting prepared which consists of the CATIA Model in which these parameters attached.','1. As this parameter should be cross checked by CATIA Model only requested to CAD department to add a photocopy of the Model in process sheet.\r\n2. Separate file is getting prepared which consists of the CATIA Model in which these parameters attached.','Next batch found okay','','2014-09-23','Nagaraju(T)','Yogesha(K)','','0000-00-00','* pocket inside step under size. (1.0mm)','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','06','no','Misc','Girish(Prasad P)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7742,'18-110A','Magellan Aerospace Bournemouth','FORK END INTERMEDIATE','A0860N','D575 40494 202','S80 FHT','J',1,'RP400840','','37658','','0000-00-00',NULL,'yes','yes','yes','','','','','','no','spindle chips  hold so bore(+)5micron','small chips clogged to tool from ATC while machining due to this bore got oversize ','ATC will be cleaned before machining and ensure no chips clogged to tool','ATC will be cleaned before machining and ensure no chips clogged to tool','Next batch found okay','','2014-09-24','Anjinamurthy(H)','        Manohara M','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7743,'28-003A','Magellan Aerospace New York  Inc.','PIN-ATTACHMENT WALKING BE','G20527K07','161A7305-1','','PL-Rev-NC, DL Rev-B',1,'120240_R0_C0','','36932','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1)Thread tieght.','Thread gauge was not butting.','Next time thread gauge kept to be free.','Any threaded parts after machining checked in machine before removing. ','Next batch found okay','','2014-09-24','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Manufacture Only','0','FI','yes','Misc','Sudhagar(V)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7744,'35-226','Saab AB','HINGE BRACKET 1','580220A2','D576 50004 207','','D00',1,'1600076514','','34604','','0000-00-00',NULL,'yes','no','yes','no','yes','no','no','no','no','Dig mark on bore.','While running boring tool, Machine alarm coming related to spindle contractor.\r\nAfter alarm machine spindle was stooped and small mark observed on bore.','Immediately machine was stopped and informed to machine supplier regarding the problem.\r\nService engineer came and changed the machine parameter to avoid the alarm. After ensuring the machine condition machining stared.','As per service provider this alarm will not come in future and we need ensure the contractor voltage at every Preventive maintenance.','Next parts were okay','','2014-09-24','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','04','no','Misc','Krishna(Chowdary.G.P.)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7745,'35-066A','Saab AB','7605450-200 ','560753','L574 55450 200','','B00, PG74415001JA02',2,'1600082589','','36008','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','2nos Base thickness problem, measures 1.43, actual dimension required 1.8 to 2.20 in base finish.','vacuum not holding properly  part in the fixture ,not used proper lenth bolts.(used more then required lenth bolts)  ','* used correct lenth bolts, \r\n* check vacuum holding in properly,  ','* check vacuum holding in properly,\r\n* we segregate correct proper bolts used this CRN only.','CA/PA found satisfactory.','','2014-09-24','Narayanappa(G)','Siddaramappa ,Paramesh K,Gajendra Singh C.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','3','no','VR11','Narayanappa(G)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7746,'18-295A','Magellan Aerospace Bournemouth','BOLT','A0484U','D577 56145 200','S80','A',1,'RP400846','','37193','','0000-00-00',NULL,'yes','yes','yes','','','','','','no','35.80mm width under size','Wrong butting of the part lead to width undersize','Instructed to operator that ensure every part for clamping before machining and ensure any chips or screws are loose and then start machining','Instructed to operator that ensure every part for clamping before machining and ensure any chips or screws are loose and then start machining','Next parts found okay','','2014-09-24','Girish(Prasad P)','        Sundar D.K.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7747,'18-295A','Magellan Aerospace Bournemouth','BOLT','A0484U','D577 56145 200','S80','A',67,'RP400846','','33128','','0000-00-00',NULL,'no','no','no','yes','yes','no','no','no','yes','Parts are ETCH inspection rejected in 12 dia bore at customer end.','Due to polishing or tool rubbing marks etch inspection failed ','Polishing should be avoided, speed and depth of cutting and tool marks should be avoided. Instructed CAD and Production to modify the program and run with low RPM','Polishing should be avoided, speed and depth of cutting and tool marks should be avoided. Instructed CAD and Production to modify the program and run with low RPM','Next batches found okay','C29437','2014-09-25','Avinash(R.J.)','Muniyappa(N)','CIM WO No-33128','2014-08-27','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Manufacture Only','0','CUST END','yes','Misc','Muniyappa(N)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7748,'18-295A','Magellan Aerospace Bournemouth','BOLT','A0484U','D577 56145 200','S80','A',9,'RP400846','','34476','','0000-00-00',NULL,'no','no','no','yes','yes','no','no','no','yes','Parts are ETCH inspection rejected in 12 dia bore at customer end.','Due to polishing or tool rubbing marks etch inspection failed ','Polishing should be avoided, speed and depth of cutting and tool marks should be avoided. Instructed CAD and Production to modify the program and run with low RPM','Polishing should be avoided, speed and depth of cutting and tool marks should be avoided. Instructed CAD and Production to modify the program and run with low RPM','Next batches found okay','C30230','2014-09-25','Avinash(R.J.)','Muniyappa(N)','CIM WO No:34476','2014-08-27','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Manufacture Only','0','CUST END','yes','Misc','Muniyappa(N)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7749,'18-295A','Magellan Aerospace Bournemouth','BOLT','A0484U','D577 56145 200','S80','A',26,'RP400846','','34478','','0000-00-00',NULL,'no','no','no','yes','yes','no','no','no','yes','Parts are ETCH inspection rejected in 12 dia bore at customer end.','Due to polishing or tool rubbing marks etch inspection failed ','Polishing should be avoided, speed and depth of cutting and tool marks should be avoided. Instructed CAD and Production to modify the program and run with low RPM','Polishing should be avoided, speed and depth of cutting and tool marks should be avoided. Instructed CAD and Production to modify the program and run with low RPM','Next batches found okay','C30535','2014-09-25','Avinash(R.J.)','Muniyappa(N)','CIM WO No:34478','2014-08-27','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Manufacture Only','0','CUST END','yes','Misc','Muniyappa(N)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7750,'30-012A','Gardner Aerospace-Derby Limited','SPAR FWD - RH','480938','L575 51827 201','ABM3-1029 T7651','A00, ECN:PG60049U01LC52',1,'LPR0000576','','37580','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','material cutting problem requard thickness 30.00mm, finishing thickness 25.00, material size 23.5 so part not machined.','crass cutting due to cutting blade wobbling & twist ','bearing & blade changed ','frequent checked to be done for blade wobbling prior to cutting','CA/PA Satisfaction ok. ','','2014-09-25','Nagaraja (G)','Sunil Kumar(K.R.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','1','no','Misc','Narayanappa(G)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7751,'18-414B','Magellan Aerospace Bournemouth','ACTUATOR HOUSING','20005','D278 50163 200','','D',1,'RP401021_Amnd No. 1','','36614','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','ID Bore ovear size 0.012mm.','Insert was worn out so this problem occurred','Check insert status regularly and know the life of inserts and change inserts according instructions ','Check insert status regularly and know the life of inserts and change inserts according instructions','Next Batches found okay','','2014-09-25','Dinakar(K)','Shivashankar H.G.,SHIVAKUMAR ,Rangaswamy ,Ningaraj A N,Dinakar K,Ashith B,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','ST20Y1','Narasimha Murthy(R)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7752,'18-380B','Magellan Aerospace Bournemouth','GAMMA FITTINGS ','M510620','NSA840020-350','','L',1,'RP401481_Amend No.-1','','34195','','0000-00-00',NULL,'yes','','yes','','yes','','','','','GJ dimension (-0.05)','1) dial stand not setting properly.\r\n2) high pressure given in dial stand.\r\n3)taper in flat probe.\r\n4) he dont know about adjust the taper in dial stand. ','give the instruction and set the stand and run the part.','given the guidence for operator for how to set the stand and how to check the part. ','Next batch found okay','','2014-09-25','Dinakar(K)','        Kalakappa T H','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7753,'18-414B','Magellan Aerospace Bournemouth','ACTUATOR HOUSING','20005','D278 50163 200','','D',1,'RP401021_Amnd No. 1','','37214','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Tickness under size 0.04mm.','1)rough tool running time thickness undersize 2)single tool running 3)tool shortage.\r\n','new tool orderd\r\n\r\n\r\n\r\n\r\n','additon tool adedd  this process mention in data sheet.\r\n\r\n\r\n\r\n\r\n','Process sheet not updated!Next part found okay.','','2014-09-25','Dinakar(K)','Shivashankar H.G.,SHIVAKUMAR ,Ravi M,Rangaswamy ,Ningaraj A N,Nataraja C V,Mahesh N,Dinakar K,Ashith B,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','ST20','Narasimha Murthy(R)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7754,'18-414B','Magellan Aerospace Bournemouth','ACTUATOR HOUSING','20005','D278 50163 200','','D',2,'RP401021_Amnd No. 1','','37214','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','I.d WAS OVER SIZE BY(+0.10MM)','while offset taken time, he give a cut for finished bore. so part will over sized.','give the  instruction for operator and run the part.','training give the operator. before setting check the process sheet and then do the setting.  ','Next Batches found okay','','2014-09-25','Dinakar(K)','Nataraja C(V)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Sandhesh D(S)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7755,'18-414B','Magellan Aerospace Bournemouth','ACTUATOR HOUSING','20005','D278 50163 200','','D',3,'RP401021_Amnd No. 1','','37214','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','BORE UNDER SIZE BY (-0.12MM).','Insert was worn out operator failed to notice that and machined the part and found bore undersize','Warned operators strictly to change the inserts after some quantity which is displayed in boards, and work order should entered regarding change of insert and first off should be done by quality person and get signed ','Warned operators strictly to change the inserts after some quantity which is displayed in boards, and work order should entered regarding change of insert and first off should be done by quality person and get signed','Next parts found okay','','2014-09-25','Dinakar(K)','Shivanand(D.B.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','','01','yes','Misc','Sandhesh D(S)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7756,'18-391B','Magellan Aerospace Bournemouth','END COVER','M511480 89971A','D278 50166 200','','A',6,'RP401022_Amend No 1','','37287','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dia 6.426 to 6.446 Dia ovear size.','1) 6.42 drill running so pin tight\r\n2) 6.43 drill not available\r\n3) so 6.42 drill using and rework done \r\n4) using hand drill so drillout and part rejected\r\n','6.43 drill using & running parts.','drill any time stock in 5nos.\r\n\r\n\r\n\r\n\r\n','Next batch found okay','','2014-09-25','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Dinakar(K)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7757,'18-392B','Magellan Aerospace Bournemouth','END COVER','M510610','D278 50167 200','','D',4,'RP401023_Amend No.-1','','37290','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Diam 6.426 to 6.446 dia ovear size.','1) 6.42 drill running so pin tight\r\n2) 6.43 drill not available\r\n3) rework time step occurred\r\n4) again rewok this part so dia will over sized.\r\n','6.43 drill using & running parts.','drill any time stock in 5nos.\r\n\r\n\r\n\r\n\r\n','Next batch found okay','','2014-09-25','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Dinakar(K)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7758,'18-106A','Magellan Aerospace Bournemouth','EYE END INBOARD','512111','D575 41542 200','S98 FHT','D',1,'RP400841','','37638','','0000-00-00',NULL,'yes','yes','yes','','','','','','','OD Thread NO GO Answered....','1) offset problem.\r\n2) after changing the insert not taken in plus (+) side.\r\n3) He taken plus in other tool \r\n4) operator problem\r\n','instruction given to the operator\r\n\r\n\r\n\r\n\r\n','before setting give the instruction about part and setting to the operator \r\n\r\n\r\n\r\n\r\n','Next Batches found okay','','2014-09-25','Dinakar(K)','        Seetharamu D','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7759,'28-006','Ellanef Manufacturing Corporation','SHOULDER BOLT','G19876K01','162A3109 2','15-5PH Bar,Per AMS56','NA',1,'117105_R0_C1','','37239','','0000-00-00',NULL,'yes','yes','yes','','','','','','','OD measures undersize by 0.1mm.','It is happened due to insert problem.New insert loaded but operator was not cross checked whether insert properly seatted or not. ','For next piece supervisor loaded the insert properly & cross checked dimension for several components and found within tolerance. ','Proper training given to the operators regarding the above NC.','Next batch found satisfactory','','2014-09-25','Dinakar(K)','        GUNDEGOWDA H.G.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7760,'18-295A','Magellan Aerospace Bournemouth','BOLT','A0484U','D577 56145 200','S80','A',1,'RP400846','','37534','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Air pressure low so OD Thread dig mark.','running time air pressure that time o.d thread was digmark.','We are inform to the maintenence for the proper air connection','We are inform to the maintenence for the proper air connection','Maintenance done immediately  and next parts found okay ','','2014-09-26','Dinakar(K)','        Ravi M','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7761,'28-006','Ellanef Manufacturing Corporation','SHOULDER BOLT','G19876K01','162A3109 2','15-5PH Bar,Per AMS56','NA',1,'117105_R0_C1','','37239','','0000-00-00',NULL,'yes','yes','yes','','','','','','','O.D (-) side 1.NO S  0.01','1) chips rubbing.2) single tool running 3) in data sheet have single tool so single tool running.\r\n','additional tool added and run the part\r\n\r\n\r\n\r\n\r\n','additional tool added in datd sheet and run the the part for next every batch.\r\n\r\n\r\n\r\n\r\n','Next batch found satisfactory','','2014-09-26','Dinakar(K)','        KRISHNAMURTHY N','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7762,'40-020','Universal Engineering Limited','BUTT STRAP T.E TOP SKIN ','412130','D575 41101 200- 01','','H01, ECN NG29999ST2XC85',4,'318176','','36983','','0000-00-00',NULL,'no','yes','yes','yes','no','no','no','no','no','R/M Thickness Under Size, Required Size 40mm But issued 37.5mm. ','While swapping the RM for this CRN, RM physically not verified and also approved by CAD and Purchase.Due to this manual error RM booked in ERP causes rejection.','Procedure are in place to swap the Raw material and taken care to avoid manual errors in ERP.','Procedure are in place to swap the Raw material and taken care to avoid manual errors in ERP.','Next parts found okay','','2014-09-26','Sunil Kumar(K.R.)','Sunil Kumar(K.R.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','01','no','Misc','Rangaswamy()',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7763,'28-039','Magellan Aerospace New York  Inc.','SPACER WASHER, BUSHING - ','13-163/5 D10','161A2303-1','','PL _A, PSDL_ N/C',1,'120242_R0_C1','','35091','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','raw material length shortage.','While cutting the material in cutting machine, due to cutting blade bend material cutted tapered.\r\nDue to this problem one no. total length measures minus side.','After checking the part immediately Cutting blade changed and checked the tightness and then continued production. Next all the parts found ok.','Informed to cutting machine operator to check the cutting machine blade tightness regularly while doing cutting operation.','Next parts found okay','','2014-09-26','Nagaraja (G)','Sunil Kumar(K.R.)','','0000-00-00','raw material length shortage.','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','01','no','Misc','Dinakar(K)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7764,'18-114A','Magellan Aerospace Bournemouth','NUT','456336','D575 40499 200','S80 FHT','D01',2,'RP400841','','34156','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1nosThread nogo answeard. 1nos dent mark.','1)running time gauge tight so thread re-pass running. 2)threading insert changed. 3)threading insert wear out 4)running time chips rubbing\r\n','after running the every part check the insert and load the next part.\r\n\r\n\r\n\r\n\r\n','change the insert for every 40 parts.\r\n\r\n\r\n\r\n\r\n','Next batch found okay','','2014-09-26','Dinakar(K)','SHIVAKUMAR ,Rajesh B D,Nataraja C V,KRISHNAMURTHY N,Dinakar K,Ashith B,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','DX 200-3','Narasimha Murthy(R)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7765,'18-415B','Magellan Aerospace Bournemouth','ACTUATOR HOUSING','M534810/92191A','D278 50163 201','','D',2,'RP401022_Amend No 1','','34545','','0000-00-00',NULL,'no','no','no','yes','yes','yes','no','no','no','Machine abuse rejected at API.','Due to polishing or tool rubbing marks machine abuse was found in treatment house','Polishing should be avoided, speed and depth of cutting and tool marks should be avoided. Instructed CAD and Production to modify the program and run with low RPM','Polishing should be avoided, speed and depth of cutting and tool marks should be avoided. Instructed CAD and Production to modify the program and run with low RPM','Machine abuse FAIR done and next batch found okay','','2014-09-26','Muniyappa(N)','Nandishkumar(D.K.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','14891','POSTDN','no','Misc','Muniyappa(N)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7766,'18-182A','Magellan Aerospace Bournemouth','SCREWED BUSH','L21684','A284 40011 200','DTD 197','A',1,'RP400845','','36746','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Part not received from treatment house.','Certain parts will get stick into the big tanks for anodizing hence the part is very small part was missed from Treatment supplier ','Instructions has been given to Treatment house not to happen this type of incidences.','Instructions has been given to Treatment house not to happen this type of incidences.','Next incidences part missed was not from past several months','','2014-09-26','Dayananda(K.G.)','Veerandra(H.R.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','14741','POSTDN','no','Misc','Muniyappa(N)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7767,'18-376B','Magellan Aerospace Bournemouth','GAMMA FITTINGS ','M510600 89235A','NSA840020-150','','L',1,'RP401478_Amend No.-1','','37425','','0000-00-00',NULL,'yes','yes','yes','','','','','','','id ovality.','1) not boring the jaws properly. 2) small diameter ring used for boring the jaws. 3)with out boring the step in jaws and given the bush and boring the jaws.4) big dia boring tool not entering in step bore so without boring, given the ring. ','using small dia boring tool and boring the step bore and give the ring and jaws boring.','given the training about setting to the operator.','Next batch found okay','','2014-09-27','Dinakar(K)','        Chandre  Gowda','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7768,'35-104','Saab AB','ALCD_STRUCT_BUSHING-LATCH','L20997','423Z1141-1','Al-Ni-Bronze (UNS C6','--A',2,'1600080762','','37346','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Hole Operation pending or hole not performed.','Thickness was oversize after reworking the thickness hole operation will be done so left pending','Rework done and part found okay','Rework done and part found okay','Rework done and part found okay','','2014-09-27','Girish(Prasad P)','Subramanya L Naik,Shivarajakumar T M,Ningaraj A N,Nataraja C V,Manjunath  M,Krishna Chowdary.G.P.,Dinakar K,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Manufacture Only','','FI','yes','BMV 45-1','Manjunath(G)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7769,'18-317A','Magellan Aerospace(Chalfont) Limited','PIN SIDE ROLLER','B4570A','F579 53066 200','S145','C',7,'P/074118','','37059','','0000-00-00',NULL,'yes','no','no','no','yes','yes','no','no','no','Od accepted.','Accepted','Accepted','Accepted','Accepted','','2014-09-27','Dinakar(K)','Manjunatha N,KRISHNAMURTHY N,Dinakar K,Bharath R,Ashith B,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','With Treatment','0','FI','no','QT100S-2','Nandishkumar(D.K.)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7770,'35-299','Saab AB','SERRATED PLATE','581148A4','425Z0312-4','','--A',1,'PA 1510 AL','','36706','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','Finishing Part Flatness Not Achieved (0.05 Flatness) ','Flatness as per drawing is 0.05mm and due to bend and also twist in part. 0.05mm flatness not achieved.\r\n(FAI part)','After checking the flatness, New process planned.\r\nTo avoid bend aging done for both the operations and checked the flatness. After this process change flatness achieved below drawing tolerance.','Process was proved and same as implemented in MPS.\r\nWe need to check the consistency in first production batch.','Next parts found okay','','2014-09-27','Rangaswamy()','Rangaswamy()','','0000-00-00','Finishing Part Flatness Not Achieved (0.05 Flatness) ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Rangaswamy()',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7771,'35-083','Saab AB','PIN-SIDE ROLLER','B4570A','F579 53066 200','S145 FHT','C',40,'PA 1226-Roller Housi','','37025','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','o.d under size.','1)chips rubbing. 2)single tool running 3)in data sheet have single tool so single tool running.\r\n','additional tool added and run the part.\r\n\r\n\r\n\r\n\r\n','additional tool added in datd sheet and run the the part for next every batch.\r\n\r\n\r\n\r\n\r\n','Process sheet to be updated. Next batch found okay.','','2014-09-27','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','01','no','Misc','Dinakar(K)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7772,'35-083','Saab AB','PIN-SIDE ROLLER','B3288A','F579 53066 200','S145 FHT','C',101,'PA 1226-Roller Housi','','32618','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','old batch o.d under size.','1)chips rubbing. 2)single tool running 3)in data sheet have single tool so single tool running.\r\n','additional tool added and run the part.\r\n\r\n\r\n\r\n\r\n','additional tool added in datd sheet and run the the part for next every batch.\r\n\r\n\r\n\r\n\r\n','Process sheet to be updated!!!Next batch found good','','2014-09-27','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','01','no','Misc','Dinakar(K)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7773,'18-279A','Magellan Aerospace(Chalfont) Limited','DOOR OUTER TYPE 23','217769 001','L572 53721 200','ABS5032A055','B00',1,'P/074117','','37108','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','* bass thickness under size. (2.5 +/-0.08) \r\n* measured 2.30 to 2.35mm. ','In 1setup running time dimension 269.1 +/- 0.2 this dimension properly not checked .so in 2nd setup\r\nouter profile stock minus side ,so part rejected.  \r\n\r\n','Instruct to operator check every dimension & train to use checking instruments. then using profile\r\nchecking gauge.  \r\n','In 2setup running time to use outer profile checking gauge add in process sheet. \"GO\" pin & \"NOGO\"\r\npin check in every part.  \r\n  \r\n','Next batches found good  \r\n','','2014-09-27','Girish(Prasad P)','Girish(Prasad P)','','0000-00-00','* bass thickness under size. (2.5 +/-0.08) \r\n* measured 2.30 to 2.35mm.   ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','04','no','Misc','Girish(Prasad P)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7774,'18-157A','Magellan Aerospace Wrexham','Strap Crackstopper','4621702 2','D572 50203 204','ABM3 1029','L',1,'RP125886','','37263','','0000-00-00',NULL,'no','no','no','yes','yes','yes','no','no','no','Corrosion fits observed on the part surface.','Due to polishing or tool rubbing marks corrosion fits found in the part','Polishing should be avoided, speed and depth of cutting and tool marks should be avoided. Instructed CAD and Production to modify the program and run with low RPM & parts should be cleaned with PX-24 solvent on regular intervals','Polishing should be avoided, speed and depth of cutting and tool marks should be avoided. Instructed CAD and Production to modify the program and run with low RPM & parts should be cleaned with PX-24 solvent on regular intervals','Next batch found okay','','2014-09-28','Narayanappa(G)','Narayanappa(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','14824','POSTDN','no','Misc','Muniyappa(N)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7775,'18-380B','Magellan Aerospace Bournemouth','GAMMA FITTINGS ','M510610','NSA840020-350','','L',6,'RP396195','','30569','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','G dimension undersize 0.04/0.100 mm.','not setted the dial zero properly.','setted the dial zero using slip gauge & run the production.','instructions given to operator to cross check the instruments whether it is zero or not before start\r\nthe production . ','Next batch found okay','','2014-09-28','Dinakar(K)','Vishvanath K,Nandeesha N,Krishnanaik J N,Kalakappa T H,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','FI','no','QT100S-5','Narasimha Murthy(R)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7776,'18-315A','Magellan Aerospace Bournemouth','THROAT  PLATE','365428','L572 51943 200','ABM3 1029','B00',1,'RP400946','','36533','','0000-00-00',NULL,'yes','no','no','no','yes','yes','no','no','no','Linear indication observed on the part.','Due to polishing or tool rubbing marks this indication found in the parts','Polishing should be avoided, speed and depth of cutting and tool marks should be avoided. Instructed CAD and Production to modify the program and run with low RPM','Polishing should be avoided, speed and depth of cutting and tool marks should be avoided. Instructed CAD and Production to modify the program and run with low RPM','Next batches found good','','2014-09-28','Avinash(R.J.)','Anjinamurthy(H)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','14721','POSTDN','yes','Misc','Muniyappa(N)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7777,'18-413B','Magellan Aerospace Bournemouth','ACTUATOR HOUSING','M563520/94551A','D278 50162 200','','A',1,'RP401021_Amnd No. 1','','37212','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Thickness under size 0.06mm.','Due to butting face not cleaned properly .So part thickness under size. ','Before load the part of the butting face cleaned by air per sure then load the part..','Before load the part of the butting face cleaned by air per sure then load the part..','Next Batches found okay','','2014-09-28','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Dinakar(K)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7778,'18-380B','Magellan Aerospace Bournemouth','GAMMA FITTINGS ','M510620','NSA840020-350','','L',4,'RP399319','','32961','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','OD undersize.','The Following route cause analyzed for the parts rejected, 1. Ovality in RM. 2. Total Length Minus\r\nin RM. 3. Improper Butting in Jaws. 4. Jaws Boring is not good( Flatness is not achieved. 5. RM\r\nunclear on OD and ID. 6. Ovality More than 0.05mm in billet stage. 7. Chips clocking at the Jaws ,\r\nIn 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. ','Very next parts found okay','','2014-09-28','Dinakar(K)','Sathish G,Nandeesha N,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','0','FI','no','QT100S-5','Nandishkumar(D.K.)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7779,'18-209B','Magellan Aerospace(Chalfont) Limited','BODY','R2628','D321 40204 202','','D, ECN NR29999ST1KM15, NR29999ST2KF65, WQN DFB09775',1,'P/074113','','37692','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Total length under size.','Due to part butting problem so total length under size.','Next part butting properly and run the part the total length found OK.','Inform to operator every part butting properly and cross checked \"Z\" reference and run the part.','Next Batches found okay','','2014-09-28','Dinakar(K)','        Kalakappa T H','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7780,'18-378B','Magellan Aerospace Bournemouth','GAMMA FITTINGS ','91396','NSA840020-250','','L',2,'RP401480_Amend No.-1','','37044','','0000-00-00',NULL,'yes','no','no','no','yes','yes','no','no','no','OD undersize.','Due to operator checking eroor in micrometer not zero reading','Next micrometer set zero reading and master pin cross checked and run the part the OD found OK','Inform to operator first instrument cross checked master gauge then after part checked','Next batch found okay','','2014-10-06','Dinakar(K)','Sathish G,Dinakar K,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','0','FI','no','QT100S-3','Muniyappa(N)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7781,'35-030A','Saab AB','7600169-200 ','421932','L574 50169 200','','B00, PG74415001JA01',1,'1600076911','','35134','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Paint chip up.','After sending the parts to customer, paint chip up in some areas were found, due to packing methods','As these parts will be sent directly to customer from treatment house, one person has been appointed for visual inspection of treated parts only. And training provided for both visual and packing inspections','As these parts will be sent directly to customer from treatment house, one person has been appointed for visual inspection of treated parts only. And training provided for both visual and packing inspections','Next batches found good ','C31464','2014-10-06','Avinash(R.J.)','Manjunath(G)','Through mail dated 19th Aug 2014from Marcus','2014-08-19','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','DN14030','cust end','yes','Misc','Manjunath(G)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7782,'35-067A','Saab AB','7605450-201 ','3952601 1','L574 55450 201','','B00, PG74415001JA02',1,'1600076911','','34134','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Paint chip up.','After sending the parts to customer, paint chip up in some areas were found, due to packing methods','one person has been appointed for visual inspection of treated parts only. And training provided for both visual and packing inspections, instructions has been given to treatment house to check for paint chip up 100%.','one person has been appointed for visual inspection of treated parts only. And training provided for both visual and packing inspections, instructions has been given to treatment house to check for paint chip up 100%.','Next batches found okay','C30253','2014-10-06','Avinash(R.J.)','Manjunath(G)','Through mail dated 19th Aug 2014from Marcus','2014-08-19','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','DN13313','cust end','yes','Misc','Manjunath(G)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7783,'18-378B','Magellan Aerospace Bournemouth','GAMMA FITTINGS ','91396','NSA840020-250','','L',2,'RP401480_Amend No.-1','','37044','','0000-00-00',NULL,'yes','no','no','no','yes','yes','no','no','no','OD undersize.','Due to operator dail gauge setting not properly','Next dail gauge zero reading and master pin cross checked and run the part the OD found OK.','Inform to operator first instrument cross checked master gauge then after part checked.','Next batch found okay','','2014-10-06','Dinakar(K)','Sathish G,Dinakar K,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','0','FI','no','QT100S-3','Muniyappa(N)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7784,'18-380B','Magellan Aerospace Bournemouth','GAMMA FITTINGS ','M510620','NSA840020-350','','L',4,'RP399319','','32961','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','OD ovality problem.','due to bore ovality problem this deviation occur.','changed the boring tool to avoid ovality & run the production.','instructions given to operator to select the tools properly before running the production.','Next batch found okay','','2014-10-06','Dinakar(K)','Sathish G,Nandeesha N,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','0','FI','no','QT100S-5','Nandishkumar(D.K.)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7785,'18-376B','Magellan Aerospace Bournemouth','GAMMA FITTINGS ','M510600 89235A','NSA840020-150','','L',1,'RP401478_Amend No.-1','','37425','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Total length -0.2','Due to part butting problem so total length under size.','Next part butting properly and run the part the total length found OK.','Inform to operator every part butting properly and cross checked \"Z\" reference and run the part.','Next batch found okay','','2014-10-06','Dinakar(K)','        Chandre  Gowda','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7786,'18-030A','Magellan Aerospace Bournemouth','PIN','220831','D278 50156 200','S130 FHT','A',41,'RP391467','','28491','','0000-00-00',NULL,'no','no','no','yes','yes','yes','no','no','no','Face digmark noticed.','In this fixture operator loaded multiple of parts so while machining of parts some parts not\r\nseated properly in fixture so dig mark found on part. ','Instructed to operator for machining of parts in higher tolerance and then check the parts\r\nhaving dig mark on face if any parts found do it once again machine that parts for lower tolerance.\r\n','New fixture was designed for avoiding this type of error in further batches.','CA/PA found satisfactory. ','','2014-10-06','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','13032','POSTDN','no','Misc','Muniyappa(N)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7787,'18-295A','Magellan Aerospace Bournemouth','BOLT','A0484U','D577 56145 200','S80','A',1,'RP400846','','37534','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Air pressure low so OD Thread dig mark.','running time air pressure that time o.d thread was digmark. ','We are inform to the maintenence for the proper air connection.','We are inform to the maintenence for the proper air connection.','Next batch found okay','','2014-10-07','Dinakar(K)','Manjunath (M)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','09','no','Misc','Narasimhamurthy(K.G.)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7788,'18-376B','Magellan Aerospace Bournemouth','GAMMA FITTINGS ','94294','NSA840020-150','','L',1,'RP401478_Amend No.-1','','37434','','0000-00-00',NULL,'yes','yes','yes','','','','','','','PART TOTAL LENGTH -0.2','1) running time part rotating.(comeout)2) low clamping pressure given 3) becouse runout come above 0.05.\r\n4) improper jaws boring.\r\n','mention the chuck pressure and same pressure used for every batch \r\n\r\n\r\n\r\n\r\n','this proces updated in data sheet.\r\n\r\n\r\n\r\n\r\n','Next batch found okay','','2014-10-07','Dinakar(K)','        Dinakar K','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7789,'34-013B','Magellan Aerospace Winnipeg','STAND-OFF, LH LOWER ','54331-2','400-12603-1-905','','EM104302 Iss A, EM104765 Iss G, EM105092 Iss F, EM106399 Iss B, EM106400 Iss B, EM106401 Iss A, EM106404 Iss A, EM106522 Iss A, EM106602 Iss A',1,'B91379 Rev.026','','37523','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Running time part loose','While part running clamping not properly.So part running time part loose. ','Clamping process change ( instead of 1 now using 2 clamps for clamping).Analyzed the problem and minor changes done in Fixture to improve the rigid clamping. Process is under monitoring.','Instructed to operator before run the part check the clamp and butting area.   ','Next batch found okay','','2014-10-07','Lohith(K)','        Lohith K','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7790,'28-002A','Magellan Aerospace New York  Inc.','LOWER LINK','G19815K06D','161A6104-4','','PL Rev_B, DL Rev_N/C',2,'123667_R0_C0','','37153','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1)Total thickness under size by 0.05 to 0.07MM.','1.RM thickness taper (Center point).\r\n2.After completion of 1st operation total thickness measures taper on flat surface due to recived raw material was taper.   ','1.Immediatelly checking the remaining raw materials size taper and bend.\r\n2)same was instructed to the operators and explained to check the R/M before start the machine.','1.Before run the part check the Rm size,bend and taper.','Next batch found okay','','2014-10-08','Lohith(K)','Lohith(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','0','DN','no','Misc','Sudhagar(V)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7791,'18-386A','Magellan Aerospace(Chalfont) Limited','NUT RING INNER','239340','D575 40039 200','','B',1,'P/074123','','37686','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','1.3 Drill bit cut during drilling.','1.This was happened during drilling of parts, After several parts machining drill bit got blunt.\r\n2. When the grinding of the drill bit after blunting is not proper means chances of drill getting cut may occur','1.Drill bit should be changed for every 50 to 60 no\'s once even its not worn out.\r\n2.Ensuring proper grinding of drill bit after blunting.','1.Drill bit should be changed for every 50 to 60 no\'s once even its not worn out.\r\n2.Ensuring proper grinding of drill bit after blunting.','Next batch found okay','','2014-10-08','Nagaraju(T)','Nagaraju(T)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','09','no','Misc','Narasimha Murthy(R)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7792,'35-034','Saab AB','7600298-200','521550','L574 50298 200','ABM3 1029','B00',1,'1600066889','','34557','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','rib thick ness under size','Part was not butted to the fixtures properly.','Before clamping the part , clean the surface with air properly and check the part with feeler gauge.','Before clamping the part , clean the surface with air properly and check the part with feeler gauge.','Next batch found okay','','2014-10-08','Girish(Prasad P)','Girish(Prasad P)','','0000-00-00','rib thick ness under size','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Prashanth Kumar(M)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7793,'35-034','Saab AB','7600298-200','521550','L574 50298 200','ABM3 1029','B00',1,'1600066889','','34557','','0000-00-00',NULL,'yes','yes','yes','','','','','','no','DUMMY NCR,\r\nORIGINAL NCR NO 7792','DUMMY NCR,\r\nORIGINAL NCR NO 7792','DUMMY NCR,\r\nORIGINAL NCR NO 7792','','DUMMY NCR,\r\nORIGINAL NCR NO 7792','','2014-10-08','Girish(Prasad P)','        Girish Prasad P','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7794,'18-295A','Magellan Aerospace Bournemouth','BOLT','A0484U','D577 56145 200','S80','A',1,'RP400846','','37939','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','While running time power was trip so drill bit broken.','11.5mm drill running time power tripped that time drill bit broken.','We are inform to the maintenence for the proper UPS connection. ','We are inform to the maintenence for the proper UPS connection.','Next Batches found okay','','2014-10-08','Dinakar(K)','Shivanand(D.B.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','01','no','Misc','NIRANJAN(N  )',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7795,'18-220A','Magellan Aerospace(Chalfont) Limited','BUSH SLIDING CON N/DRIVEN','B2425A','L579 51161 200','S145 FHT','B00',1,'P/074115','','37242','','0000-00-00',NULL,'yes','no','no','no','yes','yes','no','no','no','OD undersize0.010mm.','1)new insert  changing\r\n2)insert not butting proper \r\n3)turning tool problem\r\n4)insert  locking screw wear out\r\n','change the tool & run the part. ','While setting time cross check the all tool cim & screw.','Next batch found okay','','2014-10-08','Dinakar(K)','SHIVAKUMAR ,Seetharamu D,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','0','FI','no','DX 200-2 ','Nandishkumar(D.K.)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7796,'18-110A','Magellan Aerospace Bournemouth','FORK END INTERMEDIATE','482737','D575 40494 202','S80 FHT','J',1,'RP400840','','37655','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Thread effect dia ovear size 0.01 to 0.02mm.','theard gauge was problem,so thread effect dia over size then parts are rework done.','parts are ok.','parts are ok.','Rework done and part found okay','','2014-10-09','Dinakar(K)','Ravi M,Mohan Kumar C.M.,Ashith B,Anjinamurthy H,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Manufacture Only','','FI','yes','DX 200-2 ','Dinakar(K)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7797,'35-160','Saab AB','STOP SUPPORT','G20109K01','423Z6188-5','','---',1,'600088847','','38038','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Dig mark noticed on the part.','While running production this deviation coming due to part not butted properly to pins or Part moving while running the program due to clamping error.','After checking the deviation next part butting checked with feller gauge and also clamps tightness checked and found ok.\r\nChecking all the above and production continued.','One more location done to avoid part moving and also part straightness will achieve after loading the part automatically.\r\nThis new fixture introduced and checked the all the PA points and all are found OK.','Next parts found okay','','2014-10-09','Lohith(K)','Lohith(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','Misc','Manjunath(G)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7798,'18-117B','Magellan Aerospace Bournemouth','HOUSING-OUT BD BRG','W72275','D275 40004 200','','C01',4,'RP400841','','37783','','0000-00-00',NULL,'yes','yes','yes','','','','','','','4no- air pressure low,\r\n\r\n','running time air pressure that time o.d thread was digmark.','We are inform to the maintenence for the proper air connection.','We are inform to the maintenence for the proper air connection.','Maintenance done and part found okay ','','2014-10-09','Dinakar(K)','        Manjunath  M','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7799,'18-152A','Magellan Aerospace Wrexham','CLEAT ','427960 2 C1','F572 54597 202 01','','E',2,'RP125889','','37132','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','dia 4.0 hole NO GO (2nos no go Gauge 4.12 answered )','158nos part complete after drill chip off,\r\nWhile running time drill chip off due to wear out of drill.\r\n','change the new drill, & continue production, Instructed to operator for checking drill wear & size regularly, and drill life was calculated, and same will\r\nbe updated for next batches.\r\n','* Drill life frequency was fixed and same will be updated.\r\n* over after 150 part once a new drill will be change.\r\n* caret coolant flow   ','Next production parts found satisfactory.','','2014-10-09','Narayanappa(G)','Siddaramappa()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','03','no','Misc','Narayanappa(G)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7800,'18-120C','Magellan Aerospace Bournemouth','HOUSING OUT B D BRG 3','230699','D275 56121 200','','E01,  ECN NG27011ST1KA83',1,'RP400843','','36669','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','O.D under size by (71.951 to 71.966)measure 71.942 so part was rejected.','1)running time part rotating.\r\n2) improper tightening.\r\n3) if over tight ovality will occure\r\n4) closed tollerance part (15 micron)\r\n','Given the guidence about tightning.','same 35-104 clamping method used for this CRN  \r\n\r\n\r\n\r\n\r\n','Next Batches found okay','','2014-10-09','Ravi(M)','Manjunatha N,Bharath R,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','11','no','QT100S-2','Ravi(M)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7801,'18-120C','Magellan Aerospace Bournemouth','HOUSING OUT B D BRG 3','230699','D275 56121 200','','E01,  ECN NG27011ST1KA83',1,'RP400843','','36675','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','O.D damage in fitting pollishing time o.d under size by(-0.01mm).','Due to operator air gauge setting not properly. ','Next air gauge zero reading and master pin cross checked\r\nand run the part the OD found OK. ','Inform to operator first instrument cross checked master air gauge then after part checked. ','Next batches found good\r\n','','2014-10-09','Nagaraju(T)','Nagaraju(T)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','15','no','Misc','Ravi(M)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7802,'18-078A','Magellan Aerospace Wrexham','ADAPTOR ','R3671','A282 50081 200','','A',1,'RP125890','','37286','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Thickness under size 0.05 to 0.06mm.','1) tool changing\r\n2) tool sim brocken\r\n3) job total length over size.\r\n4) in first set up total length not maintaining properly.\r\n','total length check before loading.\r\n\r\n\r\n\r\n\r\n','all parts same length maintain in first set up.\r\n\r\n\r\n\r\n\r\n','Next batch found okay','','2014-10-10','Dinakar(K)','SHIVAKUMAR ,Seetharamu D,Ravi M,Punith G S,Lohith K,Girish V M,Dinakar K,Dhananjaya N,Ashith B,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','FI','no','ST20Y1','Narasimha Murthy(R)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7803,'18-306A','Magellan Aerospace(Chalfont) Limited','HINGE ','658967A5','D572 59245 203','ABM3 1029','B, ECN NG29999ST2TY72',1,'P/074120','','37703','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','4mm Thickness under size mesured 3.97','1) Thickness was reduced due to vibration while machining.\r\n2) Fixture plate was not centerlised to base plate that loaded end to the base plate.\r\n     ','1) For next part fixture was centerlised to base plate and machining performed.\r\n','1)Fixture to be replaced with new and to be made in steel   plate.','Next batch found satisfactory','','2014-10-10','Anjinamurthy(H)','Anjinamurthy(H)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Anjinamurthy(H)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7804,'18-118B','Magellan Aerospace Bournemouth','BEARING HOUSING','240346','D275 40005 200','','C01',1,'RP400842','','37889','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','While running time part rotate OD ovality(+0.015mm/-0.03mm).','1) grooving tool running time part rotating.\r\n2) chuck pressure low \r\n3) if high pressure given ovality will occure\r\n4) becouse itz have a closed tollerance.\r\n','set the proper pressure and run the parts. ','mention the chuck pressure and same pressure used for every batch \r\n\r\n\r\n\r\n\r\n\r\n\r\n\r\n\r\n\r\n','Next batch found okay','','2014-10-10','Dinakar(K)','Devaraj(K.C.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','09','no','Misc','Narasimhamurthy(K.G.)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7805,'18-211B','Magellan Aerospace(Chalfont) Limited','PLUNGER','238302','D321 40205 200','','H01, ECN NR29998ST1JB80',1,'P/074114','','36512','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dia 1.6 hole damage.','1.This was happened during drilling of parts, After several parts machining drill bit got blunt.				\r\n2. When the grinding of the drill bit after blunting is not proper means chances of drill getting cut may occur	\r\n3.As the coolant flow is manual in these drilling operation the improper flow may cause drill cut			\r\n			','1.Drill bit should be changed for every 50 to 60 no\'s once even its not worn out.		\r\n2.Ensuring proper grinding of drill bit after blunting	\r\n3.While drilling , we have planned for often blowing of air and proper channelize of coolant to the hole so that the drill may not worn out easily','1.Drill bit should be changed for every 50 to 60 no\'s once even its not worn out.		\r\n2.Ensuring proper grinding of drill bit after blunting	\r\n3.While drilling , we have planned for often blowing of air and proper channelize of coolant to the hole so that the drill may not worn out easily','Next batch found okay','','2014-10-11','Nagaraju(T)','Hanumantha(Rao)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','14','no','Misc','Irappa(Badiger)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7806,'35-242','Saab AB','BUSHING','1465374','423Z1416-2','','---',1,'PA 1510 STEEL','','37820','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','100degree angle undersize.','This deviation while doing FAI part.\r\nDue to Wrong Interpretation of 100Degree angle, wrong program done. (Instead of A230 deg in program supervisor entered A220 deg)','After checking the parts, this deviation noticed and then analyzed the problem and found error in program.\r\nProgram corrected and machined FAI part.Same part 100deg found ok.\r\nProgram proved and saved in proved program folder.','Informed to CAD/CAM to check the program while doing the FAI part.\r\nSupervisor is to cross check once before doing the proving.\r\n ','Next parts found okay','','2014-10-11','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','1','no','Misc','Narasimhamurthy(K.G.)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7807,'18-340A','Magellan Aerospace Bournemouth','LANDING TOP PANNEL','A595274','F574 50961 200 01','','E, ECN PG49998ST1TV45',21,'RP400947','','36703','','0000-00-00',NULL,'no','no','no','yes','no','yes','no','yes','no','Corrosion fits observed on the surface.','Due to polishing or tool rubbing marks corrosion fits observed in treatment house','Polishing should be avoided, speed and depth of cutting and tool marks should be avoided. Instructed CAD and Production to modify the program and run with low RPM & parts should be cleaned with PX-24 solvent on regular intervals','Polishing should be avoided, speed and depth of cutting and tool marks should be avoided. Instructed CAD and Production to modify the program and run with low RPM & parts should be cleaned with PX-24 solvent on regular intervals','Next batches found okay','','2014-10-11','Avinash(R.J.)','Muniyappa(N)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','14484','POSTDN','yes','Misc','Muniyappa(N)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7808,'18-414B','Magellan Aerospace Bournemouth','ACTUATOR HOUSING','M563530','D278 50163 200','','D',1,'RP401021_Amnd No. 1','','37661','','0000-00-00',NULL,'yes','yes','yes','','','','','','','offset problem','insert screw not tightning properly.','all inserts screw and tools check and run the part. ','before setting check the tool lenght, inserts and tightning the toots and then run the part.','Next Batches found okay','','2014-10-12','NIRANJAN(N )','        SHIVAKUMAR ','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7809,'18-295A','Magellan Aerospace Bournemouth','BOLT','A0484U','D577 56145 200','S80','A',2,'RP400846','','37193','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Thraed tight.','Thread gauge was not butting.','Next time thread gauge kept to be free.','Any threaded parts after machining checked in machine before removing. ','Next batch found okay','','2014-10-13','Dinakar(K)','Ningaraj A N,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Manufacture Only','','9','yes','QT100S-1','Narasimhamurthy(K.G.)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7810,'18-295A','Magellan Aerospace Bournemouth','BOLT','A0484U','D577 56145 200','S80','A',1,'RP400846','','37534','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Thraed tight.','Thread gauge was not butting.','Next time thread gauge kept to be free.','Any threaded parts after machining checked in machine before removing. ','Next batch found okay','','2014-10-13','Dinakar(K)','Ravi M,Ningaraj A N,Nataraja C V,Manjunath  M,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Manufacture Only','','9','yes','QT100S-1','Ravi(M)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7811,'35-138','Saab AB','FLCD_DS_SUPPORT_DEFLECT_S','500738','423Z6189-3','BAC1534-62C','---',3,'600088847','','37333','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Material chip out.','The Following Route causes analyzed for material chip off after outer profile machining.\r\n1. Due to RM deviations material will chip off.\r\n2. While running production, the finishing tool wear out causes light chip off in material.\r\n3. Steel Butting sheet for part is not Flat. ','The following Corrective Action/Preventive Action taken to avoid Materiel chip off.\r\n1. Raw Material will inspect visually before issuing to production. If found any problem visually RM will be quarantined.\r\n2. Dia 8 end mill life calculated, informed to operators to monitor the tool life.and change the tool after as mentioned.\r\n3. Steel butting plates flatness inspection done before production starts.','The following Corrective Action/Preventive Action taken to avoid Materiel chip off.\r\n1. Raw Material will inspect visually before issuing to production. If found any problem visually RM will be quarantined.\r\n2. Dia 8 end mill life calculated, informed to operators to monitor the tool life.and change the tool after as mentioned.\r\n3. Steel butting plates flatness inspection done before production starts.\r\nTaking all the above PA, rejections happened in material chip off. Out of 100nos production 5 to 6nos getting rejection. Due to customer requirement parts are manufactures with considering rejections.','Next batch found okay','','2014-10-13','Lohith(K)','Theerthappa K.N.,Shivaraj K S,Lohith K,Hari Prasad,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','HAASVF2SS-2','Narasimha Murthy(R)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7812,'35-138','Saab AB','FLCD_DS_SUPPORT_DEFLECT_S','J0J3','423Z6189-3','BAC1534-62C','---',9,'600088847','','37334','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','material chipout 9nos.','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 quarantined.\r\n2. Dia 8 end mill life calculated, informed to operators to monitor the tool life.and change the tool after as mentioned.\r\n3. Steel butting plates flatness inspection done before production starts.','The following Corrective Action/Preventive Action taken to avoid Materiel chip off.\r\n1. Raw Material will inspect visually before issuing to production. If found any problem visually RM will be quarantined.\r\n2. Dia 8 end mill life calculated, informed to operators to monitor the tool life.and change the tool after as mentioned.\r\n3. Steel butting plates flatness inspection done before production starts.\r\nTaking 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.','Next batch found okay','','2014-10-13','Lohith(K)','Theerthappa K.N.,Shivaraj K S,Hari Prasad,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','HAASVF2SS-2','Narasimha Murthy(R)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7813,'35-138','Saab AB','FLCD_DS_SUPPORT_DEFLECT_S','J0J3','423Z6189-3','BAC1534-62C','---',2,'1600071420','','37338','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Material chipout 2nos.','The Following Route causes analyzed for material chip off after outer profile machining.\r\n1. Due to RM deviations material will chip off.\r\n2. While running production, the finishing tool wear out causes light chip off in material.\r\n3. Steel Butting sheet for part is not Flat. \r\n','The following Corrective Action/Preventive Action taken to avoid Materiel chip off.\r\n1. Raw Material will inspect visually before issuing to production. If found any problem visually RM will be quarantined.\r\n2. Dia 8 end mill life calculated, informed to operators to monitor the tool life.and change the tool after as mentioned.\r\n3. Steel butting plates flatness inspection done before production starts.','The following Corrective Action/Preventive Action taken to avoid Materiel chip off.\r\n1. Raw Material will inspect visually before issuing to production. If found any problem visually RM will be quarantined.\r\n2. Dia 8 end mill life calculated, informed to operators to monitor the tool life.and change the tool after as mentioned.\r\n3. Steel butting plates flatness inspection done before production starts.\r\nTaking all the above PA, rejections happened in material chip off. Out of 100nos production 5 to 6nos getting rejection. Due to customer requirement parts are manufactures with considering rejections.','Next batch found okay','','2014-10-13','Lohith(K)','Shivaraj K S,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','HAASVF2SS-2','Narasimha Murthy(R)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7814,'34-014B','Magellan Aerospace Winnipeg','STAND-OFF, RH LOWER ','52311-2','400-12603-2-905','','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','','37526','','0000-00-00',NULL,'yes','yes','yes','','','','','','','running time 3 drill cut 3.35 no go enter. ','While drilling program running time dia 3mm drill chip off . ','Drawing dimension required dia 3.25mm to dia 3.4mm. \r\nBut 3.4mm pin nogo pin not enter. \r\n ','Drawing dimension required dia 3.25mm to dia 3.4mm. \r\nBut 3.4mm pin nogo pin not enter. \r\n ','Waiting for next batch to measure effectivenss','','2014-10-13','Lohith(K)','        Lohith K','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7815,'18-314A','Magellan Aerospace Wrexham','STUD','238172','D278 50006 206 01','','D',3,'RP125889','','36858','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','O.D undersize by 0.01mm.','1) chips rubbing.2) single tool running 3) in data sheet have single tool so single tool running.\r\n','additional tool added and run the part\r\n\r\n\r\n\r\n\r\n','additional tool added in datd sheet and run the the part for next every batch.\r\n\r\n\r\n\r\n\r\n','Next Batches found okay','','2014-10-13','Dinakar(K)','Rajesh B(D)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','03','no','Misc','Narasimhamurthy(K.G.)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7816,'18-309B','Magellan Aerospace(Chalfont) Limited','SPIGOT','B4599A','F 575 51290 200','S80','B, ECN PG49999SMAKH49',1,'P/074122','','38147','','0000-00-00',NULL,'yes','yes','yes','','','','','','','O.D under size.','fixture bolt problem so runinng time part reject o.d ovality problem.','Bolt was changed.','After finishing job bolt & fixture will be keeping saperately.','Next batch found okay','','2014-10-14','Ravi(M)','        GUNDEGOWDA H.G.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7817,'18-415B','Magellan Aerospace Bournemouth','ACTUATOR HOUSING','20005','D278 50163 201','','D',3,'RP401022_Amend No 1','','37216','','0000-00-00',NULL,'no','no','no','yes','yes','yes','no','no','no','Mchine abuse rejected on tappered diameter.','Due to polishing or tool rubbing marks machine abuse was found in treatment house','Polishing should be avoided, speed and depth of cutting and tool marks should be avoided. Instructed CAD and Production to modify the program and run with low RPM','Polishing should be avoided, speed and depth of cutting and tool marks should be avoided. Instructed CAD and Production to modify the program and run with low RPM','Machine abuse FAIR done and next batch found okay','','2014-10-14','Avinash(R.J.)','Muniyappa(N)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','15033','POSTDN','yes','Misc','Muniyappa(N)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7818,'18-229B','Magellan Aerospace Bournemouth','CLAMP STRIP TOP OUTBD','420789','L572 52377 200','ABM3 1029','B00',3,'RP401009','','36242','','0000-00-00',NULL,'no','no','no','yes','yes','yes','no','no','no','Corrosion fits observed on the part surface.','Due to polishing or tool rubbing marks corrosion fits observed in treatment house','Polishing should be avoided, speed and depth of cutting and tool marks should be avoided. Instructed CAD and Production to modify the program and run with low RPM & parts should be cleaned with PX-24 solvent on regular intervals','Polishing should be avoided, speed and depth of cutting and tool marks should be avoided. Instructed CAD and Production to modify the program and run with low RPM & parts should be cleaned with PX-24 solvent on regular intervals','Next batches found satisfactory','','2014-10-15','Muniyappa(N)','Nandishkumar(D.K.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','15036','POSTDN','yes','Misc','Muniyappa(N)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7819,'35-298','Saab AB','SERRATED PLATE','581148A4','425Z0312-3','','--A',1,'PA 1510 AL','','36705','','0000-00-00',NULL,'no','yes','no','yes','no','yes','no','no','no','Material thickness is more than Rulling dimension 0.001 inches.\r\nRulling dimension is 0.249 inches but used material is 0.25 inches.','The standard size available for this part is more we have asked for SAAB for the change the ruling dimension of the part but the part got accepted and dispatched to customer with DR(Deviation Report)','The standard size available for this part is more we have asked for SAAB for the change the ruling dimension of the part but the part got accepted and dispatched to customer with DR(Deviation Report)','The standard size available for this part is more we have asked for SAAB for the change the ruling dimension of the part but the part got accepted and dispatched to customer with DR(Deviation Report)','The standard size available for this part is more we have asked for SAAB for the change the ruling dimension of the part but the part got accepted and dispatched to customer with DR(Deviation Report)','','2014-10-15','Avinash(R.J.)','Manjunath(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','With Treatment','','FI','no','Misc','Manjunath(G)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7820,'18-372B','Magellan Aerospace Bournemouth','GAMMA FITTINGS ','94906','NSA840007-250 ','','N',1,'RP401477_Amend No.-1','','38128','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','THREAD \'GO\' NOT ANSWERING...','','','','','','2014-10-15','Dinakar(K)','Nandeesha(N)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Manufacture Only','','03','yes','Misc','Sandhesh D(S)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7821,'18-378B','Magellan Aerospace Bournemouth','GAMMA FITTINGS ','91395','NSA840020-250','','L',1,'RP401480_Amend No.-1','','37027','','0000-00-00',NULL,'yes','yes','yes','','','','','','','setting time k dimention(-0.3)-side','1) offset problem.2) after changing the insert not taken in plus (+) side.3) He taken plus in other tool 4)operator problem\r\n','instruction given to the operator about tool and setting.\r\n\r\n\r\n\r\n\r\n','before setting give the instruction about part and setting to the operator \r\n\r\n\r\n\r\n\r\n','Next batch found okay','','2014-10-15','Sandhesh D(S)','        Krishnanaik J N','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7822,'18-378B','Magellan Aerospace Bournemouth','GAMMA FITTINGS ','91395','NSA840020-250','','L',1,'RP401480_Amend No.-1','','37027','','0000-00-00',NULL,'yes','yes','yes','','','','','','','G.J dia under size.','1)running time part rotating. 2)improper tightening. 3)if over tight ovality will occure\r\n\r\n',' dialing the fixture and medium tightning the part.  ','while setting time  dialing the fixture and medium tightning the part','Next batch found okay','','2014-10-15','Dinakar(K)','        Dinakar K','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7823,'30-016A','Gardner Aerospace-Derby Limited','FRAME MID RIB IFS - RH ','6793701','L575 51892 201','7010 T7651 ABM3-1029','A, ECN:PG60049M01JA74',1,'LPR0000511','','37799','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','negative area base thickness required dimension 2.0mm, but  masseur value 0.9mm ','while machining part got lifted, in sequence process problem.','1)inform to CAD CAM department & all program sequence changed,   \r\n2)all 5axis program trail checking & running, \r\n3)all 5axis program feed & speed monitoring proving & production time, \r\n4)before doing fair part or any program change production people & CAD team will plane the process & programing sequence, by that there will be no chance  of part problem. ','1)inform to CAD CAM department & all program sequence changed,  \r\n2)all 5axis program trail checking & running,  \r\n3)all 5axis program feed & speed monitoring proving & production time,  4)before doing fair part or any program change production people & CAD team will plane the process & programing sequence, by that there will be no chance  of part problem. ','ca/pa Satisfaction ok.','','2014-10-15','Narayanappa(G)','Siddaramappa ,Paramesh K,Narayanappa G,Gajendra Singh C.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','7','no','VR11','Narayanappa(G)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7824,'30-112','Gardner Aerospace-Derby Limited','RIB 1 OFW ','8080701','L575 57325 200 - PF','','A00',1,'LPR0000612','','38044','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','pocket wall broken ','wrong program selected from USB','instructed to operator  After separate folder mode  for all program run in  USB only , ','instructed to operator  After separate folder mode  for all program run in  USB only , ','CA/PA Satisfaction ok.','','2014-10-15','Narayanappa(G)','Sathish Y.R.,PAVAN KUMAR  S.K.,Narayanappa G,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','3','no','HAAS','Narayanappa(G)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7825,'34-022B','Magellan Aerospace Winnipeg','BUSHING','54585','400-12614-1-905','','EM104302 Iss A, EM104765 Iss G, EM105092 Iss F, EM106399 Iss B, EM106400 Iss B, EM106401 Iss A, EM106404 Iss A, EM106522 Iss A, EM106602 Iss A ',5,'B91379 Rev-024','','35758','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','1)Raw material certificate  missing.','The material was received on March-2012, at that time relevant documents was not received with material. Raw material booking done with out Documents.','All material certificates to be verified by Stores,and also approved by QAD before Book in the material.','Informed to supplier to provide all the documents before material dispatch. ','Next parts found okay','','2014-10-16','Nagaraja (G)','Nagaraja (G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','0','FI','no','Misc','Sudhagar(V)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7826,'34-022','BRISTOL AEROSPACE LIMITED','BUSHING','54585','400-12614-1-905','17-4PH Stainless Ste','EM 104302 Iss. A, EM 105092 Iss. E',2,'B91379 Rev-002','','18006','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','1)Raw material certificate  missing.','The material was received on March-2012, at that time relevant documents was not received with material. Raw material booking done with out Documents.','All material certificates to be verified by Stores,and also approved by QAD before Book in the material.','Informed to supplier to provide all the documents before material dispatch. ','Next parts found okay','','2014-10-16','Nagaraja (G)','GUNDEGOWDA H.G.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','0','FI','no','DX 200-3','Sudhagar(V)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7827,'35-138','Saab AB','FLCD_DS_SUPPORT_DEFLECT_S','J0J3','423Z6189-3','BAC1534-62C','---',1,'600088847','','37334','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Material layer chipout in treatment house.\r\n','The Following Route causes analyzed for material chip off after outer profile machining.\r\n1. Due to RM deviations material will chip off.\r\n2. While running production, the finishing tool wear out causes light chip off in material.\r\n3. Steel Butting sheet for part is not Flat. \r\n','The following Corrective Action/Preventive Action taken to avoid Materiel chip off.\r\n1. Raw Material will inspect visually before issuing to production. If found any problem visually RM will be quarantined.\r\n2. Dia 8 end mill life calculated, informed to operators to monitor the tool life.and change the tool after as mentioned.\r\n3. Steel butting plates flatness inspection done before production starts.','The following Corrective Action/Preventive Action taken to avoid Materiel chip off.\r\n1. Raw Material will inspect visually before issuing to production. If found any problem visually RM will be quarantined.\r\n2. Dia 8 end mill life calculated, informed to operators to monitor the tool life.and change the tool after as mentioned.\r\n3. Steel butting plates flatness inspection done before production starts.\r\nTaking all the above PA, rejections happened in material chip off. Out of 100nos production 5 to 6nos getting rejection. Due to customer requirement parts are manufactures with considering rejections.','Next batch found okay','','2014-10-16','Avinash(R.J.)','Manjunath(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','15139','post DN','no','Misc','Manjunath(G)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7828,'35-138','Saab AB','FLCD_DS_SUPPORT_DEFLECT_S','500738','423Z6189-3','BAC1534-62C','---',1,'600088847','','37333','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Material layer chipout in treatment house.','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 quarantined.\r\n2. Dia 8 end mill life calculated, informed to operators to monitor the tool life.and change the tool after as mentioned.\r\n3. Steel butting plates flatness inspection done before production starts.','The following Corrective Action/Preventive Action taken to avoid Materiel chip off.\r\n1. Raw Material will inspect visually before issuing to production. If found any problem visually RM will be quarantined.\r\n2. Dia 8 end mill life calculated, informed to operators to monitor the tool life.and change the tool after as mentioned.\r\n3. Steel butting plates flatness inspection done before production starts.\r\nTaking 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.','Next batch found okay','','2014-10-16','Avinash(R.J.)','Manjunath(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','15138','post DN','no','Misc','Manjunath(G)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7829,'28-004A','Ellanef Manufacturing Corporation','PIN','G16433R05','161A2332-1','15-5PH Steel Bar per','NA',1,'115976_Rel-0_Ch-01','','37818','','0000-00-00',NULL,'yes','yes','yes','','','','','','','bore over size (0.05)','since it is a blind bore while maching the bore the chips was blocked inside the bore which took extra material by\r\nrubbing to the bore at the end.','1.coolant nozzle was set along with the tools so as to remove the chips from the bore.','a station was provided in the programm to clean the chips.\r\n','Next batch found okay','','2014-10-16','NIRANJAN(N )','        Rajesh B D','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7830,'28-004A','Ellanef Manufacturing Corporation','PIN','G16433R05','161A2332-1','15-5PH Steel Bar per','NA',1,'115976_Rel-0_Ch-01','','37818','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','od undersize by 0.05 to 0.02 mm','While doing OD turning chips clocking on part and chattering coming then to avoid chattering again re pass done for this part,then deviation coming.  ','For next part OD turning operation done with stock,then inspected the part.After checking then  run the finishing pass.','Program changed to cut with stock for first pass.Then after\r\nroughing operation finishing pass running to avoid such\r\nproblem.','Next batch found okay','','2014-10-16','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','03','no','Misc','Dinakar(K)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7831,'18-098B','Magellan Aerospace Bournemouth','VALVE- SEAT','90415','D282 50060 204','','D',1,'RP400844','','38204','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Dig mark noticed on part Top.( Near the 100 deg countersink area, 03 places)','1. Diameter 10 x 100 deg Counter sink tool interchanging in Two machines due to unavailability of tool. \r\n2. Instructed to operator to interchange the tool in Two machines due to urgent in dispatches for both the parts.\r\n','1.Dedicated Tools kept for both the parts(Special Tools only).\r\n2.Spare tools to be kept in stock for unexpected breakages.\r\n3.Tools life and stock will monitored by Tools supervisor.\r\n    ','1.Dedicated Tools kept for both the parts(Special Tools only).\r\n2.Spare tools to be kept in stock for unexpected breakages.\r\n3.Tools life and stock will monitored by Tools supervisor.\r\n    ','Next batch found okay','','2014-10-17','Lohith(K)','        Punith G S','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7832,'18-274D','Magellan Aerospace Bournemouth','BUTTSTRAP UPP RS4X2110 ','429125','L575 54394 201','','C00',1,'RP400948_Amnd-01','','38369','','0000-00-00',NULL,'yes','yes','yes','','','','','','no','center thickness 0.1(-) side so part reject','1.As this process is carried in 2nd setup, the first setup bend may cause this type of problems\r\n2.Fixture is worn out \r\n3.By not Dialing the fixture properly\r\n','1.Requested CAD department to change the process and do the both setups in one time\r\n2.Informed Management that New Fixture is need for the butt straps\r\n3.Zero clamping system should be introduced for dialing problems\r\n','1.Requested CAD department to change the process and do the both setups in one time\r\n2.Informed Management that New Fixture is need for the butt straps\r\n3.Zero clamping system should be introduced for dialing problems','Next batch found satisfactory','','2014-10-17','Anjinamurthy(H)','        Anjinamurthy H','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7833,'18-111A','Magellan Aerospace Bournemouth','BODY TURNBUCKLE INTMD','A0484U','D575 41544 200','S80 FHT','A',1,'RP400840','','37943','','0000-00-00',NULL,'yes','yes','yes','','','','','','','id grove width oversize by 0.5mm.','part running time grove insert broken.','next changed the i.d grove insert then part was ok.','next changed the i.d grove insert then part was ok.','Next batch found okay','','2014-10-17','Dinakar(K)','        Girish V M','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7834,'18-078A','Magellan Aerospace Wrexham','ADAPTOR ','R3671','A282 50081 200','','A',1,'RP125890','','37285','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Thread gauge not answered.','Thread gauge was not butting. ','Next time thread gauge kept to be free.','Any threaded parts after machining checked in machine before removing. ','Next batch found okay','','2014-10-18','Dinakar(K)','Shivaraj K S,Shivanand D.B.,SHIVAKUMAR ,Ravi M,Raghavendra Rao R,Lohith K,Hari Prasad,Dinakar K,Ashith B,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Manufacture Only','','FI','yes','ST20Y1','Narasimha Murthy(R)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7835,'18-211B','Magellan Aerospace(Chalfont) Limited','PLUNGER','238302','D321 40205 200','','H01, ECN NR29998ST1JB80',1,'P/074114','','37555','','0000-00-00',NULL,'yes','yes','yes','','','','','','','running time chips rub so od (-)side 0.02mm','','','','','','2014-10-18','Dinakar(K)','        Nataraja C V','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7836,'05-088','HAL-Aircraft','TRAVERSE BEAM - RH','XP156311/1E-14-A320','D521-10353-201-00-E0','7175  T 7351','NA',1,'ES14AB-C/271/ES/COMP','','38072','','0000-00-00',NULL,'yes','yes','yes','','','no','','','','* Bass thickness under size (0.5 to 0.8mm).','* I-machine program running 16r2 broken so part dig. Base thickness under size.','* Stop the production and inform to the CAD/CAM department.','* I-mach program change in the 16r2 tool.\r\n* Take care 16r2 cutter helix angle.\r\n','CA/PA Satisfaction ok.','','2014-10-19','Girish(Prasad P)','                Prashanth Kumar M','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7837,'18-211B','Magellan Aerospace(Chalfont) Limited','PLUNGER','238302','D321 40205 200','','H01, ECN NR29998ST1JB80',2,'P/074114','','37555','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Running time chips rub so OD (-).02 & .04','','','','','','2014-10-20','Dinakar(K)','        Ningaraj A N','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7838,'18-330A','Magellan Aerospace Wrexham','FLANGE MACHINED ','97653','F282 50098 200','','A',1,'RP125889','','38222','','0000-00-00',NULL,'yes','yes','yes','','','','','','','OD [-0.5MM] U/S X-AXIS WAS DOWN','Sunday manchine was idle so monday day running turret x axis was shift.','Wear Offset take (+ side) and running part was ok.\r\n','When machince was off take the offset all tool & running.','Next production parts found satisfactory.','','2014-10-20','Dinakar(K)','        Shivanand D.B.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7839,'28-004A','Magellan Aerospace New York  Inc.','PIN','G16433R05','161A2332-1','15-5PH Steel Bar per','NA',1,'120243-3172','','37815','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1)Bore over size by 0.10MM.','since it is a blind bore while maching the bore the chips was blocked inside the bore which took extra material by\r\nrubbing to the bore at the end.','1.coolant nozzle was set along with the tools so as to remove the chips from the bore.','a station was provided in the programm to clean the chips.\r\n','Program updated and parts found okay','','2014-10-20','Dinakar(K)','Rajesh T,Rajesh B D,Mohan Kumar C.M.,KRISHNAMURTHY N,GUNDEGOWDA H.G.,Devaraj K.C.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','0','FI','no','DX 200-1','Sudhagar(V)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7840,'35-176A','Saab AB','LATCH_ACT_PIVOT-FTG ','562176','423Z1205-2-02','','--B',1,'NOV 2014 ','','37335','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Hole Position not Achived.\r\n','Fixture Wrong Loading hole Position not Achived in Using Zero Point System, for Fast Loading & Unloading. ','Inform to operoter Before running the progrem cross check fixture loading .progrem inside insert msg.','Next batch using double pin Avide fixture Wrong loading.','Very Next batch found okay','','2014-10-20','Rangaswamy()','Gurukiran S(M)','','0000-00-00','Fixture Wrong Loading so Part Reject.\r\n','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Rangaswamy()',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7841,'35-149','Saab AB','CED_BS_HINGE_FTG-AFT','540268','425Z0311-8','7050 - T7451 ALUMINU','--A',1,'NOV 2014 ','','37350','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Dent mark noticed on serrations.','Dent mark noticed on serrations.','Fitting department we are instructed  to take care of in this issues.','We are give the training in  Fitting department.','Next batch found ok.','','2014-10-20','Rangaswamy(H A)','Rangaswamy(H A)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','DN','no','Misc','Manjunath(G)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7842,'18-413B','Magellan Aerospace Bournemouth','ACTUATOR HOUSING','M563520/94551A','D278 50162 200','','A',1,'RP401021_Amnd No. 1','','38309','','0000-00-00',NULL,'yes','yes','yes','','','','','','','running time part come out 6MM thick ness under size','1) rough tool running time thickness undersize\r\n2) single tool running\r\n3) tool shortage\r\n','new tool orderd\r\n\r\n\r\n\r\n\r\n','additon tool adeddthis process mention in data sheet.\r\n','Next Batches found okay','','2014-10-20','Dinakar(K)','        SHIVAKUMAR ','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7843,'35-193','Saab AB','INTERCOSTAL CAM HOUSING','428527A','423Z1190-1-01','','---',1,'NOV 2014 ','','37730','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Dia 3.18 to 3.27 measures oversize. ','While proving the first off in operation-01, dia 3.2 drill offset not taken correctly. This error causes dig mark on hole.','Tool offset taken correctly and all the tool which is running are cross checked and continued production.\r\nNext part checked and all the dimensions found ok.','Supervisor need to monitor the operator and Train them to avoid such manual errors.\r\nOperator should concentrate on work, Informed him to cross check once before running the program and tool wear value to be written moderately till further notice. \r\n\r\nAfter checking the data of operator written in reference book and cross checking the tool offset after setting is found ok.','Next batch found okay','','2014-10-20','Rangaswamy(H A)','Rangaswamy(H A)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','DN','no','Misc','Manjunath(G)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7844,'18-211B','Magellan Aerospace(Chalfont) Limited','PLUNGER','238302','D321 40205 200','','H01, ECN NR29998ST1JB80',3,'P/074114','','37554','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','OD Under size 0.01mm 2nos 1nos dia 1.6 drill bit cut.','1) chips rubbing.\r\n2) single tool running\r\n3) in data sheet have single tool so single tool running.\r\n','additional tool added and run the part\r\n\r\n\r\n\r\n\r\n','additional tool added in datd sheet and run the the part for next every batch.\r\n\r\n\r\n\r\n\r\n','Next Batches found okay','','2014-10-21','Dinakar(K)','Dinakar(K)','','0000-00-00','nagaraju T.','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','03','no','Misc','Ravi(M)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7845,'35-193','Saab AB','INTERCOSTAL CAM HOUSING','428527B','423Z1190-1-01','','---',1,'1600081742 Rev 2','','37890','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Rib thickness measures plus side out of tolerance 0.1mm.','While running the operation-02, wall finish cutter dia 16r3 was blunted, causes variations in wall thickness.','After checking the part new tool placed and continued production.\r\nFirst off done for all the dimensions after changing the tool and all dimensions are ok.','Informed to operators and concern supervisor to check the tool condition at regular intervals.\r\nDedicated tool to be kept to avoid such problems.\r\n\r\nRework done for 01 no. and part accepted.','Next parts found okay','','2014-10-21','Rangaswamy(H A)','Rangaswamy(H A)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','','DN','yes','Misc','Manjunath(G)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7846,'35-017','Saab AB','9901503-075','95856','D576 50011 200','L167','A',3,'PA 1217 2014','','37915','','0000-00-00',NULL,'yes','yes','yes','','','','','','','radius problem in 3parts','vacuum not holding properly , so part lifting during part running so radius Digg mark appeared. ','inform to maintenance team, clean the vacuum value,& put the pressure reader for checking vacuum, ',' vacuum pump & vacuum value are cleaning weekly one time ','CA/PA found satisfactory.','','2014-10-21','Narayanappa(G)','        Siddaramappa ','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7847,'30-016A','Gardner Aerospace-Derby Limited','FRAME MID RIB IFS - RH ','6793701','L575 51892 201','7010 T7651 ABM3-1029','A, ECN:PG60049M01JA74',1,'LPR0000511','','37799','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','negative area base thickness required dimension 2.0mm, but  masseur value 0.9mm ','while machining part got lifted, in sequence process problem.','1)inform to CAD CAM department & all program sequence changed,   \r\n2)all 5axis program trail checking & running, \r\n3)all 5axis program feed & speed monitoring proving & production time, \r\n4)before doing fair part or any program change production people & CAD team will plane the process & programing sequence, by that there will be no chance  of part problem. ','1)inform to CAD CAM department & all program sequence changed,  \r\n2)all 5axis program trail checking & running,  \r\n3)all 5axis program feed & speed monitoring proving & production time,  4)before doing fair part or any program change production people & CAD team will plane the process & programing sequence, by that there will be no chance  of part problem. ','CA/PA Satisfaction ok. ','','2014-10-21','Narayanappa(G)','Siddaramappa ,Paramesh K,Narayanappa G,Gajendra Singh C.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','7','no','VR11','Narayanappa(G)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7848,'18-098B','Magellan Aerospace Bournemouth','VALVE- SEAT','90415','D282 50060 204','','D',2,'RP400844','','35911','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Vacuum  fixture trial for bend removing so part lifted so part dig mark.','Trail operation did for vacuum fixture and found part bend ','Changed to old process and part found okay','Changed to old process and part found okay','Changed to old process and part found okay','','2014-10-21','Lohith(K)','Lohith(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','00','no','Misc','Anjinamurthy(H)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7849,'18-032A','Magellan Aerospace Bournemouth','BUSH','W72421','D278 50165 200','S80 FHT','A',3,'RP400838','','37711','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','OD under size 0.01mm.','1)chips rubbing.2)single tool running 3)in data sheet have single tool so single tool running.\r\n','additional tool added and run the part\r\n\r\n\r\n\r\n\r\n','additional tool added in datd sheet and run the the part for next every batch.\r\n\r\n\r\n\r\n\r\n','Next batch found okay','','2014-10-22','Dinakar(K)','Seetharamu D,Rajesh B D,KRISHNAMURTHY N,GUNDEGOWDA H.G.,Girish V M,Ashith B,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','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,NULL),(7850,'18-186A','Magellan Aerospace Bournemouth','BUSH','P1631','L575 50336 200','B23','B00',7,'RP401024','','33969','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Thickness under size 0.02mm.','1) improper work offset given\r\n2) total length not meassuring properly.\r\n3) micrometer error\r\n4) micrometer zero not checking.\r\n','while checking every part using slip gauge & cross check the micrometer.  ','befor checking the every part check the slip and cross check the micrometer.\r\n\r\n\r\n\r\n\r\n','Next Batches found okay','','2014-10-22','Dinakar(K)','GUNDEGOWDA H.G.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','FI','no','DX 200-3','Narasimha Murthy(R)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7851,'18-211B','Magellan Aerospace(Chalfont) Limited','PLUNGER','238302','D321 40205 200','','H01, ECN NR29998ST1JB80',2,'P/074114','','37554','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','OD Under size 0.01mm.','1) chips rubbing.\r\n2) single tool running\r\n3) in data sheet have single tool so single tool running.\r\n','additional tool added and run the part\r\n\r\n\r\n\r\n\r\n','additional tool added in datd sheet and run the the part for next every batch.\r\n\r\n\r\n\r\n\r\n','Next batch found okay','','2014-10-22','Dinakar(K)','Theerthappa K.N.,Shivaraj K S,Ningaraj A N,Nataraja C V,Lohith K,KRISHNAMURTHY N,Hari Prasad,GUNDEGOWDA H.G.,Girish V M,Girish L N,Dinakar K,Devaraj K.C.,Ashith B,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','FI','no','QT100S-1','Narasimha Murthy(R)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7852,'35-017','Saab AB','9901503-075','95856','D576 50011 200','L167','A',18,'PA 1217 2014','','37913','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','all parts broken, 18nos  ','while machining parts got lifted, in vacuum holding problem.','inform to maintenance team, clean the vacuum value,& put the pressure reader for checking vacuum,\r\n ','vacuum pump & vacuum value are cleaning weekly one time. ','CA/PA found satisfactory.','','2014-10-23','Narayanappa(G)','Paramesh(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','3','no','Misc','Narayanappa(G)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7853,'18-407A','Magellan Aerospace Bournemouth','STIFFENER EDGE BEAM','404744','L575 53248 200','','A00',1,'RP401021_Amnd No. 1','','38162','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Dig mark on part.','The root cause is as follows,\r\n\r\n1.Mis interpretation of process in cad. Part UCS and fixture locating pin distances are not matching.\r\n2.process not followed when setting done in production.While doing setting for FAI part cross checking parameters not checked like XO YO to locating pin distances.','After part got deviation production and Programer set and discussed the process and checked the errors and changed the UCS in CAD and regenerated the program. Also cross checked the distances between X0 to Locating pins.\r\n\r\nNext part produced and accepted.\r\n','MPS done as per above changes done.\r\nFAI part was accepted.\r\n\r\nInformed operator to check the basic values while doing a FAI and co-ordinate with CAD engineer and understand the process before running the part on machine. ','MPS to be uploaded still. CAPA to be verified .','','2014-10-24','Ramesh(Poojary)','        Girish Prasad P','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7854,'35-183A','Saab AB','EDGE HOUSING','653650A2','423Z1121-6-02','','--A',1,'1600082632','','36721','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Dig mark noticed on the part.','Dig mark due to tool down while running 3D base finishing.','Tool holder scrap and tool holded in new tool holder, offset taken and continued production.','All the holders condition checked and informed to operators and supervisor to monitor the collects, holders at regular, if found any deviations inform to concern person.','Next parts found okay','','2014-10-24','Rangaswamy()','Rangaswamy()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','DN','no','Misc','Manjunath(G)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7855,'35-183A','Saab AB','EDGE HOUSING','675763A7','423Z1121-6-02','','--A',1,'1600082632','','36722','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Wall thickness measures 0.5mm undersize.','Due to put the center bolts not properly so wall thickness undesize\r\n','Put the center bolts properly and bolt tightness also checked then run the production. \r\n','Instructed operator to every part put the center bolts properly and bolt tightness also checked then run the production.  \r\n','Next batch found satisfactory','','2014-10-24','Rangaswamy()','Rangaswamy()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','DN','no','Misc','Manjunath(G)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7856,'18-382A','Magellan Aerospace(Chalfont) Limited','SLEEVE BEARING ','230330','D575 40037 200','','A',1,'P/074123','','38310','','0000-00-00',NULL,'yes','yes','yes','','','','','','','setting time grove length change.','new tool loading then not taken the offset so groove lenght over sized.','offset taken and run the part.  ','after change the tool taken the x and z offset before running the part. ','Next parts found okay','','2014-10-24','Dinakar(K)','        Manjunath  M','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7857,'18-430A','Magellan Aerospace Bournemouth','CLEAT','0709701A','L575 52435 201','','A00',1,'RP404750','','38320','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Tool dig mark.','Due to put the center bolts not properly so part outer profile dig mark. \r\n\r\n   ','Put the center bolts properly and bolt tightness also checked then run the production. \r\n','Put the center bolts properly and bolt tightness also checked then run the production. \r\n','Next part found okay','','2014-10-25','Rangaswamy()','Umesh(B)','','0000-00-00','Tool dig mark.','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Rangaswamy()',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7858,'18-116B','Magellan Aerospace Bournemouth','ASSEMBLY FORKEND','5565','F575 51377 200','','A',1,'RP400841','','38274','','0000-00-00',NULL,'yes','yes','yes','','','','','','','thread no go answer. ','1) offset problem. 2)after changing the insert not taken in plus (+) side. 3)He taken plus in other tool 4)operator problem.\r\n','instruction given to the operator.\r\n\r\n\r\n\r\n\r\n','before setting give the instruction about part and setting to the operator.\r\n\r\n\r\n\r\n\r\n','Next part found okay','','2014-10-26','Dinakar(K)','        KRISHNAMURTHY N','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7859,'35-297','Saab AB','HINGE FITTING','426692 B','425Z0311-12','','---',1,'PA 1510 AL','','38081','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Base thickness measures undersize.','This FAIR part 2nd setup running time base thick under size,because process problem & 2nd setup fixture problem. ','Re-work 2nd setup fixture,then ok.','Machining another steel fixture for 2nd setup.','Next parts found okay','','2014-10-26','Rangaswamy()','Rangaswamy()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','DN','no','Misc','Manjunath(G)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7860,'18-382A','Magellan Aerospace(Chalfont) Limited','SLEEVE BEARING ','230330','D575 40037 200','','A',1,'P/074123','','38310','','0000-00-00',NULL,'yes','yes','yes','','','','','','','OD under size in 0.0010 to 0.015MM.','Due to operator checking dial setting not properly.','Checking dial setting  properly and part checked the dimension is ok.','Instructed operator to Checking dial setting properly and\r\npart checked the dimension is ok.','Next batch found okay','','2014-10-27','Dinakar(K)','        Nataraja C V','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7861,'18-430A','Magellan Aerospace Bournemouth','CLEAT','0709701A','L575 52435 201','','A00',1,'RP404750','','38320','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Qty 2nos manufacturing  in one billet ,FAI proving  time one part rejected, So one number already NC raised . Another one number 03 operation not completed  but we need another two parts to do the new FAIR, since we put a Rework for this one number,after completion of FAIR parts will be finished.  ','Under work','Under Work','Under work','Under rework','','2014-10-27','Rangaswamy()','        Umesh(B)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','','03','yes','Misc','Rangaswamy()',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7862,'18-379B','Magellan Aerospace Bournemouth','GAMMA FITTINGS ','6586','NSA840020-300','','L',1,'RP401480_Amend No.-1','','38323','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Running Time 2mm Parting Insert Breake & Tool Dig marke','1) running time parting insert brocken 2) that time parting tool will be blented 3) parting insert not locking properly 4) that time part dig mark occure.\r\n\r\n','new parting tool loading and run the part.','after every 800 numbers change the parting  insert and run the part...','Next batch found okay','','2014-10-27','Dinakar(K)','        Chandre  Gowda','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7863,'35-263','Saab AB','EXTENSION ROD','G20551K01','424Z3414-1','','--A',1,'PA 1510 STEEL','','37806','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1)ID Over size by 0.23MM.\r\n2)120 Degree under size by 20 Degree ','1)While doing FAI part due to mis interpretation of threading dimensions, 20UNJ 6IR insert used instead of 2IR 1.5mm pitch insert.\r\nPart checked with thread gauge and found ok but, ID measures 0.23mm over size.\r\n2.This is also due to misinterpretation of drawing, CAD/CAM not given correct angle as per drawing.  \r\n','1.After checking the part find deviations and then again new insert placed 2IR 1.5mm pitch and machined the part, ID and thread gauge found as per drawing requirement.\r\nProgram proved and also insert specification mentioned in MPS.\r\n2.Model imported to CAM software and checked the dimensions ans and new program done. ','1.After checking the part again new insert placed 2IR 1.5mm pitch and machined the part, ID and thread gauge found as per drawing requirement.\r\nProgram proved and also insert specification mentioned in MPS.\r\n2.Model imported to CAM software and checked the dimensions ans and new program done. ','Next parts found okay','','2014-10-27','Ravi(M)','Ravi(M)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','0','FI','no','Misc','Sudhagar(V)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7864,'18-214A','Magellan Aerospace(Chalfont) Limited','SPECIAL WASHER ','245160','D321 40210 202','','E01, ECN NR29999ST1JB79',1,'P/074114','','37540','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Thickness under size drawing dimension 3.5 mesure 3.11.','running time parting insert broken that time parting tool will be blunted parting insert not locking properly that time taper will occur.\r\n','change the insert for every 150 parts.\r\n\r\n\r\n\r\n\r\n\r\n','change the insert for every 150 parts.\r\n\r\n\r\n\r\n\r\n','Next batch found satisfactory','','2014-10-27','Dinakar(K)','Seetharamu D,S. Shiva Kumar,Manjunatha N.R.,Girish V M,Anjinamurthy H,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','FI','no','DX 200-2 ','Narasimha Murthy(R)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7865,'18-225A','Magellan Aerospace Bournemouth','CLAMP BLOCK','4552263','D282 50123 204','NYLON 66','A',1,'RP400846','','38447','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Thickness undersize in 0.5mm.','supporting block for the butting in the conventional machining went wrong extra 0.5 mm block has been placed ','Ensure the butting block surface while machining and check the thickness regularly while machining the part','Make one block for the butting support instead of placing more blocks.And check regularly the thickness also','Next part found okay and future batches will be keenly watched ','','2014-10-28','Anjinamurthy(H)','Ravindra(Singh R)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','03','no','Misc','Muniyappa(N)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7866,'18-381B','Magellan Aerospace Bournemouth','GAMMA FITTINGS ','4728','NSA840020-400','','L',1,'RP401481_Amend No.-1','','34221','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','OD under size.','The Following route cause analyzed for the parts rejected, 1. Ovality in RM. 2. Total Length Minus\r\nin RM. 3. Improper Butting in Jaws. 4. Jaws Boring is not good( Flatness is not achieved. 5. RM\r\nunclear on OD and ID. 6. Ovality More than 0.05mm in billet stage. 7. Chips clocking at the Jaws ,\r\nIn 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. ','Very next parts found okay','','2014-10-28','Dinakar(K)','Vishvanath K,Nandeesha N,Krishnanaik J N,Kalakappa T H,Girish S,Girish L N,Dinakar K,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','FI','no','QT100S-5','Nandishkumar(D.K.)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7867,'18-382A','Magellan Aerospace(Chalfont) Limited','SLEEVE BEARING ','230330','D575 40037 200','','A',1,'P/074123','','37911','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Thread gauge not answeard.','Thread gauge was not butting.','Next time thread gauge kept to be free','Any threaded parts after machining checked in machine before removing. ','Next batch found okay','','2014-10-28','Dinakar(K)','Ningaraj A N,Nataraja C V,Dinakar K,Bharath R,Anjinamurthy H,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Manufacture Only','','FI','yes','QT100S-1','Narasimha Murthy(R)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7868,'18-225A','Magellan Aerospace Bournemouth','CLAMP BLOCK','4552263','D282 50123 204','NYLON 66','A',239,'RP400846','','38548','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Thickness under size Drawing dimension 14.oomm mesure 13.5 t0 13.6','supporting block for the butting in the conventional machining went wrong extra 0.5 mm block has been placed ','Ensure the butting block surface while machining and check the thickness regularly while machining the part','Make one block for the butting support instead of placing more blocks.And check regularly the thickness also','Next part found okay and future batches will be keenly watched ','','2014-10-29','Ravindra(Singh R)','Ravindra(Singh R)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','FI','no','Misc','Narasimha Murthy(R)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7869,'28-044','Ellanef Manufacturing Corporation','LINK ASSEMBLY UPPER UPLOC','A13368 ( WO # 139199','161A6122-6','','PL_Rev-A, PSDL-Rev-N/C',1,'118817_R0_C6','','36995','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1)Chamfer oversize by 0.5mm in the controlled bore.','1)This was happened during 1st setting due to wrong work offset.','1)During 1st off part, operator instructed to check the work offset dummy material.\r\n2)Countersunk depth measuring gauge will be procured to check the diameter during machining itself.\r\n','1)During 1st off part, operator instructed to check the work offset dummy material.\r\n2)Countersunk depth measuring gauge will be procured to check the diameter during machining itself.\r\n','1)Next batch will be closely monitoring by the supervisor.','','2014-10-29','Rangaswamy()','Umesh B,Theerthappa K.N.,Shivaraj K S,Manohara B.C.,Lohith K,Hari Prasad,Gurukiran S M,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','FI','no','MakinoF5','Avinash(R.J.)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7870,'35-176A','Saab AB','LATCH_ACT_PIVOT-FTG ','624690A4','423Z1205-2-02','','--B',1,'NOV 2014 ','','37337','','2014-10-29',NULL,'yes','yes','no','no','no','yes','no','no','no','BORE + 6 MICRONS IN LARGER BORE 25.403.','Dia 10fl using for Dia 25.4+/-.007 bore finish.10fl finishing repass running,every time rotary rotate so bore ovality.','Program changed to only single pass for finish the Bore. ','Now we are introuduced new reamer for bore finishing.','CA/PA found satisfactory.','','2014-10-29','Girish(Prasad P)','Girish(Prasad P)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','DN','no','Misc','Manjunath(G)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7871,'18-091A','Magellan Aerospace Bournemouth','BUSH','Y12196','D278 50164 202','S80 FHT','A',1,'RP400843','','38138','','0000-00-00',NULL,'yes','yes','yes','','','','','','','O.d .14 (-)side','micrometer problem o.d -0.14 (-)side.','Micrometer master and slip gauge checking and run.','befor checking the every part check the slip and cross check the micrometer.\r\n\r\n\r\n\r\n\r\n','Next Batches found okay','','2014-10-29','Dinakar(K)','        Manjunatha N','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7872,'18-090A','Magellan Aerospace Bournemouth','BUSH','235508','D278 50164 200','S80 FHT','A',1,'RP400843','','38527','','0000-00-00',NULL,'yes','yes','yes','','','','','','','power trip becous o.d. dig mark','running time power tripped that time o.d was digmark. ','We are inform to the maintenence for the proper UPS connection.','We are inform to the maintenence for the proper UPS connection.','UPS problem solved .','','2014-10-29','Dinakar(K)','        Shivappa M B','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7873,'18-090A','Magellan Aerospace Bournemouth','BUSH','235508','D278 50164 200','S80 FHT','A',1,'RP400843','','38527','','0000-00-00',NULL,'yes','yes','yes','','','','','','no','Running Time Power Trip So Part OD is Dig mark...','running time power tripped that time o.d was digmark. ','We have informed to the maintenance for the proper UPS connection.','We have informed to the maintenance for the proper UPS connection.','UPS problem solved .','','2014-10-29','Dinakar(K)','        Seetharamu D','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7874,'18-090A','Magellan Aerospace Bournemouth','BUSH','235508','D278 50164 200','S80 FHT','A',1,'RP400843','','38527','','0000-00-00',NULL,'yes','yes','yes','','','','','','','power trip','running time power tripped that time o.d was digmark. ','We are inform to the maintenence for the proper UPS connection.','We are inform to the maintenence for the proper UPS connection.','UPS problem solved .','','2014-10-30','Dinakar(K)','        Devaraj K.C.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7875,'18-210B','Magellan Aerospace(Chalfont) Limited','BODY','R2497','D321 40204 204','','D, ECN NR29999ST1KM15, NR29999ST2KF65, WQN DFB09775',1,'P/074113','','37192','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','76.mm depth under size mesure 75.75mm.','Due to problem in tool holder these occurs. 							\r\n','Holder was changed and scrapped the old holder and instructed to operator for checking holder every batch and if any errors will come change the holder. 							\r\n','Holder was changed and scrapped the old holder and instructed to operator for checking holder every batch and if any errors will come change the holder. 							\r\n','Rework parts are okay','','2014-10-30','Narasimha Murthy(R)','Subramanya L Naik,Shivarajakumar T M,Shivappa M B,Rajesh T,Krishna Chowdary.G.P.,Devaraj K.C.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','','FI','yes','DX 200-1','Narasimha Murthy(R)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7876,'35-030A','Saab AB','7600169-200 ','421933','L574 50169 200','','B00, PG74415001JA01',1,'1600082589','','35525','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Paint chipup.','','','','','C32356','2014-10-31','Manjunath(G)','Manjunath(G)','Troug mail.','2014-09-19','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','14249','CUST END','yes','Misc','Avinash(R.J.)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7877,'35-030A','Saab AB','7600169-200 ','3419701 3','L574 50169 200','','B00, PG74415001JA01',1,'1600082589','','35890','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Paint chipup.','After sending the parts to customer, paint chip up in some areas were found, due to packing methods','As these parts will be sent directly to customer from treatment house, one person has been appointed for visual inspection of treated parts only. And training provided for both visual and packing inspections','As these parts will be sent directly to customer from treatment house, one person has been appointed for visual inspection of treated parts only. And training provided for both visual and packing inspections','Next batches found good ','C32357','2014-10-31','Manjunath(G)','Manjunath(G)','Through mail.','2014-09-19','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','14247','CUST END','yes','Misc','Avinash(R.J.)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7878,'35-031A','Saab AB','7600169-201 ','421934','L574 50169 201','','B00, PG74415001JA01',1,'1600082589','','35527','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Paint chipup.','Refer tour report for rectification of above problem.','Refer tour report for rectification of above problem.','Refer tour report for rectification of above problem.','Next batch found satisfactory.','C32361','2014-10-31','Manjunath(G)','Manjunath(G)','Through Mail.','2014-09-19','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','14242','CUST END','yes','Misc','Avinash(R.J.)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7879,'35-031A','Saab AB','7600169-201 ','3445701 3','L574 50169 201','','B00, PG74415001JA01',1,'1600082589','','35892','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Part chipup.','Refer tour report for rectification of above problem.','Refer tour report for rectification of above problem.','Refer tour report for rectification of above problem.','Next batch found satisfactory.','C32363','2014-10-31','Manjunath(G)','Manjunath(G)','Through Mail.','2014-09-19','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','14244','CUST END','yes','Misc','Avinash(R.J.)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7880,'35-084','Saab AB','WASHER-SIDE ROLLER ','222','F579 53067 200','S535','A',12,'PA 1226-Roller Housi','','31949','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1)OD Undersize,camfer uneven and part damage.','2) chips rubbing. 3) single tool running 4) in data sheet have single tool so single tool running.\r\n','additional tool added and run the part\r\n\r\n\r\n\r\n\r\n','additional tool added in datd sheet and run the the part for next every batch.\r\n\r\n\r\n\r\n\r\n','Next batch found satisfactory','','2014-10-31','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','DN','no','Misc','Manjunath(G)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7881,'35-236','Saab AB','JACK BRACKET 1','133891','D576 50009 207','','D00',1,'1600090548','','38033','','0000-00-00',NULL,'no','yes','yes','yes','no','no','no','no','no','RM unclear.','Required RM 105mm, but recived rm size 105 to 103mm measured,2mm taper.so part rm not clear. dimession 3.8mm measured 3.4mm.','Stop the production, inform to supervisor,& store person,then next another fixture manufacturing maintine 3mm pluse side. then start production.','In RM sizeing in 1st settup ,maintain rm size,in 3mm stock in  2nd setup.no issues.  ','CA/PA found satisfactory.','','2014-10-31','Rangaswamy()','Shivashankar(H.G.)','','0000-00-00','RM unclear.','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','03','no','Misc','Rangaswamy()',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7882,'40-011','Universal Engineering Limited','BRACKET- TEE ','321908','D574 55153 200','','A, ECN NG29999ST2TV19',1,'318176','','36892','','0000-00-00',NULL,'yes','no','no','no','yes','yes','no','no','no','Thickness under size by 0.30mm.(Nominal 4 +0.30/-0.20 Measured 3.50mm)','Dig mark observed on part due to tool cut in roughing operation.\r\nRework done to remove the dig mark on part, but drawing dimension measures 0.3mm minus side.','New tool placed and reduced the Feed and Speed with in allowable limit and continued production.\r\nAfter changing the parameter all the parts found ok.','Program proved and saved in proved program folder.','Next parts found okay','','2014-10-31','Rangaswamy()','Umesh B,Manohara B.C.,Gurukiran S M,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','MakinoF3','Avinash(R.J.)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7883,'18-310A','Magellan Aerospace(Chalfont) Limited','STOP - U/C HINGED DOOR ','417437','F575 51392 200','','A, ECN PG49999SMAKG01',1,'P/074122','','38485','','0000-00-00',NULL,'yes','yes','yes','','','','','','no','serration tool dig mark so part reject','Wrong Y offset taken by the operator','Certain value for the Y axis will be included in both program and Process sheet so that sudden tool down to serration will be avoided .','Certain value for the Y axis will be included in both program and Process sheet so that sudden tool down to serration will be avoided .','NC under review till next batch.','','2014-10-31','Anjinamurthy(H)','        ','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7884,'35-140','Saab AB','BCD_DR_BEAM_FTG_UPR_FWD_4','426691 A','424Z1130-14-01','7050 - T7451 ALUMINU','--B',1,'NOV 2014 ','','37361','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Total RIb Height measured under size out of tolerance(35.52)','Due to error in tool offset this deviation coming.Tool down while running roughing operation.','Tool holder scrap and tool holded in new tool holder, offset taken and continued production.','All the holders condition checked and informed to operators and supervisor to monitor the collects, holders at regular, if found any deviations inform to concern person.','Next parts found okay','','2014-11-03','Rangaswamy()','Rangaswamy()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','DN','no','Misc','Manjunath(G)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7885,'18-407A','Magellan Aerospace Bournemouth','STIFFENER EDGE BEAM','404744','L575 53248 200','','A00',1,'RP401021_Amnd No. 1','','38264','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','WEB Thickness undersize 6.00+0.13/-0.08 mm measure 5.70mm. ','Due to process problem this deviation coming.\r\n\r\nWhile running the base finish program base thickness varies due to more length.\r\n\r\nProcess analyzed and planned to clamp the base with vacuum to get the thickness.','New Vacuum fixture done and proved FAI part.\r\n\r\nBase thickness measure with in tolerance and also flatness with in 0.08mm.','New process was proved and MPS to be done as per process.\r\n\r\nConsistency to be monitor in first batch production.','MPS to be uploaded still. CAPA to be verified .','','2014-11-03','Girish(Prasad P)','Girish(Prasad P)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','0','FI','no','Misc','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7886,'18-414B','Magellan Aerospace Bournemouth','ACTUATOR HOUSING','M563530','D278 50163 200','','D',1,'RP401021_Amnd No. 1','','37661','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Hole chamfer over size.','This deviation due to chamfer diameter setting in machine by altering the tool offset value. While doing a alter operator done a mistake.','Chamfer adjusted by editing the tool value and checked in slip gauge and also cross checked with profile projector and found ok.\r\nProduction continued and checked the parts 100%.','Dedicated tool arranged and separate tool box made to avoid such minor alteration in further batches.\r\nWhile doing next batch production because of dedicated tool chamfer dimension will not vary.','Next parts found okay','','2014-11-03','Girish(Prasad P)','        Basavaraja S. Jr.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7887,'18-117B','Magellan Aerospace Bournemouth','HOUSING-OUT BD BRG','W72275','D275 40004 200','','C01',1,'RP400841','','37787','','0000-00-00',NULL,'yes','yes','yes','','','','','','','1)O.D Thread Nogo answeard.','1)running time gauge tight so thread re-pass running. 2)threading insert changed. 3)threading insert wear out 4)running time chips rubbing\r\n','after running the every part check the insert and load the next part\r\n\r\n\r\n\r\n\r\n','change the insert for every 40 parts.\r\n\r\n\r\n\r\n\r\n','Next batch found okay','','2014-11-03','Ravi(M)','        Dinakar K','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7888,'35-249','Saab AB','STANDOFF','G20388K05','423Z1916-3','','---',1,'PA 1510 STEEL','','37418','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Thickness 1.27 was bend.','process not setted while running time 1.27 thickness  was bend.','Next part 3rd setup  1.27 thickness profile will be running in milling.','We are not running the 3rd setup.(Milling Machine will undergo 3rd setup)','Under Review next batch will be taken care','','2014-11-03','NIRANJAN(N  )','NIRANJAN(N  )','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','NIRANJAN(N  )',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7889,'35-261','Saab AB','RODEND','G19618K13','424Z3411-2','','--B',1,'PA 1510 STEEL','','37809','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','I.D thread diameter over size 12.37 to 12.65 measured diameter 12.90. ','Not given proper threading insert. ','Proper thread insert using.','We order insert any time 5nos stock. ','Under Review next batch will be taken care','','2014-11-03','Ravi(M)','Ravi(M)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','01','no','Misc','Ravi(M)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7890,'35-023','Saab AB','7605120-201','417706','L574 55120 201','ABM3 1029','C00',1,'1600091592','','38508','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','*Wall thickness under size (2+/_0.2) measures 1.60mm to 1.70mm.','Deviation due to locating hole problem, While doing operation-01, locating hole measures 8.1mm.( Locating pin should be 8 H7), This deviation not observed when doing operation-02 and part not located perfectly as per process.','All the parts 8H7 checked and step pin made to locate the part as per process and continued production by cross checking the straightness for every part.','Locating pins should be H7 tolerance and also operators should check the holes by pins 100% in all the parts to avoid such problems.\r\nDedicated tool planned to monitor the control dimensions in production process.','Next parts found okay','','2014-11-04','Girish(Prasad P)','Prashanth Kumar(M)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Girish(Prasad P)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7891,'18-152A','Magellan Aerospace Wrexham','CLEAT ','425413','F572 54597 202 01','','E',1,'RP125889','','37922','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Thickness under size 0.05 mm drawing dimension 2.5 mm measures 2.25 mm.','Because of T slot cutter bend, this deviation occured','offset will be taken to all tooth of the T slot cutter and ensure it twice','1.offset will be taken to all tooth of the T slot cutter and ensure it twice\r\n2.By dialing the cutter face out and ensuring the Z offset','Next part found okay','','2014-11-04','Girish(Prasad P)','Siddaramappa ,Paramesh K,Narayanappa G,Gajendra Singh C.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','FI','no','VMC 70L','Narasimha Murthy(R)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7892,'35-299','Saab AB','SERRATED PLATE','581148A4','425Z0312-4','','--A',1,'PA 1510 AL','','37995','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','Serration flatness 0.05mm not achieved.','Flatness as per drawing is 0.05mm and due to bend and also twist in part. 0.05mm flatness not achieved.\r\n(FAI part)','After checking the flatness, New process planned.\r\nTo avoid bend aging done for both the operations and checked the flatness. After this process change flatness achieved below drawing tolerance.','Process was proved and same as implemented in MPS.\r\nWe need to check the consistency in first production batch.','Next parts found okay','','2014-11-04','Rangaswamy()','Rangaswamy()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Rangaswamy()',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7893,'35-118','Saab AB','ALCD_STRUCT_INTERCOSTAL_L','614185A7','423Z1178-3','7050-T7451 ALUMINUM ','--A',1,'1600082632','','36587','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Profile dig.','While doing final cutout program, part rotates and dig mark observed on outer profile. ','Cut out stock increased by putting TRANS in cutout program and checked the tightness of clamp.','In WO no. 36587 9nos checked with above CA and all the parts found ok.','After rework dimensions are found ok.','','2014-11-05','Rangaswamy()','Rangaswamy()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','With Treatment','','DN','no','Misc','Manjunath(G)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7894,'35-231A','Saab AB','HINGE BRACKET 4 ','547769','D576 50007 208','','E00',1,'1600093863 Rev-2','','38673','','0000-00-00',NULL,'yes','no','no','no','yes','yes','no','no','no','DIG MARK IN BORE','While running boring tool, Machine alarm coming related to spindle contractor.\r\nAfter alarm machine spindle was stooped and small mark observed on bore.','Immediately machine was stopped and informed to machine supplier regarding the problem.\r\nService engineer came and changed the machine parameter to avoid the alarm. After ensuring the machine condition machining stared.','As per service provider this alarm will not come in future and we need ensure the contractor voltage at every Preventive maintenance.','Next parts found okay','','2014-11-05','Rangaswamy()','Rangaswamy()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','DN','no','Misc','Manjunath(G)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7895,'35-232A','Saab AB','HINGE BRACKET 4','420588','D576 50007 209','','E00',1,'1600093863 Rev-2','','38674','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','DIG MARK IN BORE','While running boring tool, Machine alarm coming related to spindle contractor.\r\nAfter alarm machine spindle was stooped and small mark observed on bore.','Immediately machine was stopped and informed to machine supplier regarding the problem.\r\nService engineer came and changed the machine parameter to avoid the alarm. After ensuring the machine condition machining stared.  ','As per service provider this alarm will not come in future and we need ensure the contractor voltage at every Preventive maintenance.','Next parts found okay','','2014-11-05','Rangaswamy()','Rangaswamy()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','DN','no','Misc','Manjunath(G)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7896,'18-284A','Magellan Aerospace Bournemouth','SPINDLE FOR CLACK ALVES O','Y10819','A281-40019-200','S80 FHT','A',34,'RP400846','','38037','','0000-00-00',NULL,'yes','yes','no','no','no','yes','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 problems in the future','After finishing of the part , part will be covered with paper so that contact of the parts will no be there and dent marks can be avoided','Next batch found okay','','2014-11-06','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','FI','no','Misc','Govind H(Onkar)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7897,'18-372B','Magellan Aerospace Bournemouth','GAMMA FITTINGS ','94906','NSA840007-250 ','','N',1,'RP401477_Amend No.-1','','38128','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Thickness under size 0.25mm','1) running time part rotating.(comeout) 2) low clamping pressure given 3) becouse runout come above 0.05.4) improper jaws boring.\r\n','mention the chuck pressure and same pressure used for every batch \r\n\r\n\r\n\r\n\r\n','this proces updated in data sheet.\r\n\r\n\r\n\r\n\r\n','Very next parts found okay','','2014-11-06','Dinakar(K)','Nandeesha N,Lohith K,Krishnanaik J N,Kalakappa T H,Girish S,Dinakar K,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','FI','no','QT100S-4','Narasimha Murthy(R)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7898,'18-372B','Magellan Aerospace Bournemouth','GAMMA FITTINGS ','94906','NSA840007-250 ','','N',1,'RP401477_Amend No.-1','','38130','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Thickness under size 0.07mm.','1) running time part rotating.(comeout) 2)low clamping pressure given 3) becouse runout come above 0.05.4) improper jaws boring.\r\n\r\n','mention the chuck pressure and same pressure used for every batch. \r\n\r\n\r\n\r\n\r\n\r\n\r\n\r\n\r\n','this proces updated in data sheet.\r\n\r\n\r\n\r\n\r\n\r\n\r\n\r\n\r\n','Next batch found okay','','2014-11-06','Dinakar(K)','Punith G S,Kalakappa T H,Dinakar K,Chandre  Gowda,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','FI','no','QT100S-4','Narasimha Murthy(R)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7899,'18-379B','Magellan Aerospace Bournemouth','GAMMA FITTINGS ','M510600 89235A','NSA840020-300','','L',52,'RP401480_Amend No.-1','','34619','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','I.D ovality problem.','1)single bore gauge setting.\r\n2)single bore gauge used for 2 id dimensions.\r\n3)bore gauge shortage.\r\n4)given currection in boring tool, but set the bore gauge for +0.1 toleranced dimension. ','set the bore gauge for closed toleranced dimension and run the part.  ','set the bore gauge for closed toleranced dimension and run the part.  ','Next batch found okay','','2014-11-06','Sandhesh D(S)','Nandeesha N,Krishnanaik J N,Dinakar K,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','1','no','QT100S-5','Sandhesh D(S)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7900,'18-377B','Magellan Aerospace Bournemouth','GAMMA FITTINGS ','M510590','NSA840020-200','','L',9,'RP399317','','30733','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','j dimension -0.02 to -0.025','Due to wear out of insert these error was occurred','Instructed to operator for checking insert wear regularly and changing insert frequency as mention\r\nin the board. ','Training given for the operator for CRN vise.','Next batch found okay','','2014-11-07','Dinakar(K)','Vikram(E)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','3','no','Misc','Dinakar(K)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7901,'28-004A','Magellan Aerospace New York  Inc.','PIN','G16433R05','161A2332-1','15-5PH Steel Bar per','NA',1,'120243-3172','','38399','','0000-00-00',NULL,'yes','yes','yes','','','','','','','running time insert brocken OD under size 0.03mm .','while setting time after o.d roughing more stock given to the finishing tool that time finishing insert will be brocken.\r\n','adjusting stock for finishing tool and run the part. ','setting time after running the o.d or i.d,set the stock for finishing tool then run the part.this same instruction inform to the operator.','Next batch found okay','','2014-11-07','Narasimhamurthy(K.G.)','        GUNDEGOWDA H.G.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7902,'18-381B','Magellan Aerospace Bournemouth','GAMMA FITTINGS ','94451A','NSA840020-400','','L',1,'RP401481_Amend No.-1','','37869','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Running time chips rotateing in part od J dimension(-0.025)','insert changing. more stock given to the finished tool so this problem will occure.','proper stock given and run the part.after insert changing check the stock properly.','when insert will change, that time ensure the finishing stock and run the part. ','Next batch found okay','','2014-11-08','Sandhesh D(S)','        Girish S','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7903,'18-107B','Magellan Aerospace Bournemouth','LINK BODY','20652','D574 50553 200','','A',3,'RP400839','','38665','','0000-00-00',NULL,'yes','yes','yes','','','no','','','no','RUNNING TIME BORE .05 OVELLTY','Machine Problem while machining, bore becomes plus side, reason for that is under investigation','Machine Problem while machining, bore becomes plus side, reason for that is under investigation','Machine Problem while machining, bore becomes plus side, reason for that is under investigation','Machine Problem while machining, bore becomes plus side, reason for that is under investigation','','2014-11-08','Anjinamurthy(H)','        Mohan Kumar C.M.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7904,'35-053','Saab AB','7605163-201','571009A0','L574 55163 201','ABM3 1029','A00',1,'1600091592','','38537','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Base thickness 2.5 mm measures 2.02 to 2.05mm.','While running dia 12r3 cutter, tool touches the outer profile extra material and due to jerk tool was broken.Due to tool breakage dig mark found and after removing the dig manually total thickness measures 2.02mm.','Minor tool travel added and removed the extra material which is touching the tool while running base finish program.\r\nNew program path added in existing program and proven program given back to cad/Cam.','After changing the program all the other parts are found ok and there is no load for any tool. Now after ensuring this continued production.','Next parts found okay','','2014-11-10','Girish(Prasad P)','        Prashanth Kumar M','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7905,'34-011B','Magellan Aerospace Winnipeg','STAND-OFF LH CENTRE ','52305-2','400-12602-1-905','','EM104302 Iss A, EM104765 Iss G, EM105092 Iss F, EM106399 Iss B, EM106400 Iss B, EM106401 Iss A, EM106404 Iss A, EM106522 Iss A, EM106602 Iss A',1,'B91379 Rev.026','','37519','','0000-00-00',NULL,'yes','','yes','','yes','yes','','','no','Z AXIS 3.11MM DOWNE OS PARI TOTAL HEIGHT 3.11MM(-SIDE)','1) Programmer has not good knowledge on 4-AXIS continuous program.','1) Called the application engineer and taken the assistance from him.','1) planned to take 4-axis NC-program.','Provided the training class for required personals then thereafter batches found satisfactory.','','2014-11-10','Lohith(K)','                Chiranjeevi S','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7906,'28-007A','Magellan Aerospace New York  Inc.','Shaft Support Lever','0-25-06718','251A1747-1','Ti-6AL-4V Per Mil-T-','N/C',1,'123424-3186_R0_C0','','37160','','0000-00-00',NULL,'yes','yes','yes','','','','','','','od diameter minus by 4 micron.','Operator did not take the offset correctly. ','Instructed operator to take the offset correctly.','Instructed operator to take the offset correctly.','Next batch found okay','','2014-11-10','Ravi(M)','        Manjunatha N','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7907,'34-011B','Magellan Aerospace Winnipeg','STAND-OFF LH CENTRE ','53286-3','400-12602-1-905','','EM104302 Iss A, EM104765 Iss G, EM105092 Iss F, EM106399 Iss B, EM106400 Iss B, EM106401 Iss A, EM106404 Iss A, EM106522 Iss A, EM106602 Iss A',1,'B91379 Rev.026','','37516','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Dig mark observed on the part.','Due to unproper of clamping part lifts then dig mark observed on part.','New Steel clamps made to arrest the part properly and continued production.','New Steel clamps made to arrest the part properly and continued production.','Waiting for next batch to measure effectiveness','','2014-11-11','Lohith(K)','        Dhananjaya N','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7908,'18-117B','Magellan Aerospace Bournemouth','HOUSING-OUT BD BRG','W72275','D275 40004 200','','C01',1,'RP400841','','37787','','0000-00-00',NULL,'yes','yes','yes','','','','','','','1)OD ovality(+0.015mm/-0.03mm).\r\n','1)grooving tool running time part rotating. 2)chuck pressure low  3)if high pressure given ovality will occure\r\n4)becouse itz have a closed tollerance.\r\n','mention the chuck pressure and same pressure used for every batch.\r\n\r\n','mention the chuck pressure and same pressure used for every batch.\r\n\r\n\r\n\r\n\r\n','Next batch found okay','','2014-11-11','Dinakar(K)','        Ningaraj A N','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7909,'18-414B','Magellan Aerospace Bournemouth','ACTUATOR HOUSING','20005','D278 50163 200','','D',1,'RP401021_Amnd No. 1','','36614','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','ID Bore ovear size 0.012mm.','Insert was worn out so this problem occurred ','Check insert status regularly and know the life of inserts and change inserts according instructions','Check insert status regularly and know the life of inserts and change inserts according instructions','Next batch found okay','','2014-11-11','Dinakar(K)','Shivashankar H.G.,SHIVAKUMAR ,Rangaswamy ,Ningaraj A N,Dinakar K,Ashith B,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','ST20Y1','Narasimha Murthy(R)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7910,'18-381B','Magellan Aerospace Bournemouth','GAMMA FITTINGS ','94451A','NSA840020-400','','L',1,'RP401481_Amend No.-1','','37866','','0000-00-00',NULL,'yes','yes','yes','','','','','','','OVALITY PROBLEM PART REWORK ( J ) DIMENSION ( -0.025 )\r\n','The Following route cause analyzed for the parts rejected, 1. Ovality in RM. 2. Total Length Minus\r\nin RM. 3. Improper Butting in Jaws. 4. Jaws Boring is not good( Flatness is not achieved. 5. RM\r\nunclear on OD and ID. 6. Ovality More than 0.05mm in billet stage. 7. Chips clocking at the Jaws ,\r\nIn 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. ','Very next parts found okay','','2014-11-11','Dinakar(K)','        Dinakar K','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7911,'35-138','Saab AB','FLCD_DS_SUPPORT_DEFLECT_S','7530455','423Z6189-3','BAC1534-62C','---',1,'NOV 2014 ','','38761','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Material layer chip out. ','The Following Route causes analyzed for material chip off after outer profile machining.\r\n1. Due to RM deviations material will chip off.\r\n2. While running production, the finishing tool wear out causes light chip off in material.\r\n3. Steel Butting sheet for part is not Flat. \r\n','The following Corrective Action/Preventive Action taken to avoid Materiel chip off.\r\n1. Raw Material will inspect visually before issuing to production. If found any problem visually RM will be quarantined.\r\n2. Dia 8 end mill life calculated, informed to operators to monitor the tool life.and change the tool after as mentioned.\r\n3. Steel butting plates flatness inspection done before production starts.','The following Corrective Action/Preventive Action taken to avoid Materiel chip off.\r\n1. Raw Material will inspect visually before issuing to production. If found any problem visually RM will be quarantined.\r\n2. Dia 8 end mill life calculated, informed to operators to monitor the tool life.and change the tool after as mentioned.\r\n3. Steel butting plates flatness inspection done before production starts.\r\nTaking all the above PA, rejections happened in material chip off. Out of 100nos production 5 to 6nos getting rejection. Due to customer requirement parts are manufactures with considering rejections.','Next batch found okay','','2014-11-11','Rangaswamy()','Theerthappa K.N.,Shivaraj K S,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','HAASVF2SS-2','Manjunath(G)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7912,'18-117B','Magellan Aerospace Bournemouth','HOUSING-OUT BD BRG','W72275','D275 40004 200','','C01',1,'RP400841','','37786','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','O.d thread no go answer.','1) running time gauge tight so thread re-pass running.\r\n2) threading insert changed. \r\n3) threading insert wear out \r\n4) running time chips rubbing\r\n','after running the every part check the insert and load the next part.\r\n\r\n\r\n\r\n\r\n','change the insert for every 40 parts.\r\n\r\n\r\n\r\n\r\n','Next Batches found okay','','2014-11-11','Ravi(M)','Ningaraj A N,Nataraja C V,Manjunath  M,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','3','no','QT100S-1','Ravi(M)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7913,'18-113A','Magellan Aerospace Bournemouth','ADJUSTER','424402','D575 40496 200','S80 FHT','G',1,'RP400840','','37999','','0000-00-00',NULL,'yes','yes','yes','','','','','','','1)ID Thread Nogo answeard.\r\n','1)running time gauge tight so thread re-pass running. 2)threading insert changed. 3)threading insert wear out 4)running time chips rubbing\r\n','after running the every part check the insert and load the next part.\r\n\r\n\r\n\r\n\r\n','change the insert for every 40 parts.\r\n\r\n\r\n\r\n\r\n','Next batch found okay','','2014-11-12','Dinakar(K)','        Seetharamu D','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7914,'18-414B','Magellan Aerospace Bournemouth','ACTUATOR HOUSING','M563530','D278 50163 200','','D',1,'RP401021_Amnd No. 1','','37661','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Bore over size 0.015.','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','Next Batches found okay','','2014-11-12','Dinakar(K)','Yogesha K,Shivanand D.B.,SHIVAKUMAR ,Raghavendra Rao R,Prashanth Kumar M,Basavaraja S. Jr.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','ST20','Govind H(Onkar)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7915,'35-186','Saab AB','CED_LATCH_FITTING-FWD','619678A6','425Z0610-18','','---',1,'1600093935','','38613','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Dig mark on part sue to offset problem.','While doing firstoff part operator not taken correct offset due to negligence.\r\nChecked the MPS and operator understanding, operator is experience and have capable of doing first offs.','X offset corrected and cross checked by supervisor and continued production.\r\nFor a concern supervisor cross checked all the tool offset and work offset.Then production continued and proved.','Training conducted for operator practically in front of machine to take the WO offsets.\r\nInformed him to concentrate on setting and cross check once when doing first-offs.','Next parts found okay','','2014-11-12','Girish(Prasad P)','        Basavaraja S. Jr.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7916,'18-317A','Magellan Aerospace(Chalfont) Limited','PIN SIDE ROLLER','A0587U','F579 53066 200','S145','C',1,'P/074118','','37597','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Id Thread Nogo answer.','while running time carbide threading tool broken.  ','after running the every part check the carbide threading tool and load the next part.\r\n\r\n\r\n\r\n\r\n','change the carbide threading tool for every 100nos parts.\r\n\r\n\r\n\r\n\r\n','Next batch found okay','','2014-11-14','Dinakar(K)','Nataraja C V,Manjunatha N,Manjunath  M,Dinakar K,Bharath R,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','QT100S-1','Narasimha Murthy(R)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7917,'18-157A','Magellan Aerospace Wrexham','Strap Crackstopper','4621704 2','D572 50203 204','ABM3 1029','L',1,'RP125886','','37266','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Thickness under size 0.08mm.','Raw material flatness is twisted, so part not holding in vacuum, part found minus in thickness at one end.\r\n(identify  to operator)   ','stopped the production, \r\nsort-out the bend raw material then Continue the production with flat raw material,\r\nif part not holding in vacuum due to bend inform to supervisor immediately,\r\ninform to store persons about part bend problem.       ','check the flatness of raw material when we receiving from the store,\r\nnot receiving bend raw material from store.\r\ninform to store persons about part bend problem. ','Next parts found good.','','2014-11-14','Narayanappa(G)','Sathish Y.R.,PAVAN KUMAR  S.K.,Narayanappa G,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','HAAS','Narasimha Murthy(R)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7918,'35-232A','Saab AB','HINGE BRACKET 4','425130','D576 50007 209','','E00',1,'1600095733','','38823','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Dig mark on part.','Wrong part loading in operation-01.\r\nOperator not checked the MPS while loading the part in Zero point fixture.','Training conducted for Operator( Mr. Manu kumar Employee no.300028)to load the part in fixture.\r\nAfter training operator understanding the process and production done as per MPS.','Training conducted for Operator( Mr. Manu kumar Employee no.300028)to load the part in fixture.\r\nAfter training operator understanding the process and production done as per MPS.','Next part found okay','','2014-11-14','Girish(Prasad P)','        ERANNA KAYAKAD','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7919,'18-383A','Magellan Aerospace(Chalfont) Limited','SLEEVE BEARING ','Y11518','D575 40037 202','','A',1,'P/074123','','38845','','0000-00-00',NULL,'yes','yes','yes','','','','','','','OD threading chattering problem...  ','Due to operator checking eroor in micrometer not zero reading. ','Next micrometer set zero reading and master pin cross checked and run the part the OD found OK.','Inform to operator first instrument cross checked master gauge then after part checked. ','Next batch found okay','','2014-11-14','Dinakar(K)','        Manjunath  M','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7920,'28-006','Magellan Aerospace New York  Inc.','SHOULDER BOLT','G19876K01','162A3109 2','15-5PH Bar,Per AMS56','NA',17,'120168_R0_C0','','35966','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','center drill over depth over size.','with out checking the center drill run the part.so center depth will over size.','we are add the depth of center drill will be added in the  process sheet.','we are add the depth of center drill will be added in the  process sheet.and given the instruction to the operator.','Next batch found satisfactory','','2014-11-15','Narasimhamurthy(K.G.)','Rajesh B(D)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','6','no','Misc','Narasimhamurthy(K.G.)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7921,'28-006','Ellanef Manufacturing Corporation','SHOULDER BOLT','G19876K01','162A3109 2','15-5PH Bar,Per AMS56','NA',1,'117105_R0_C1','','37239','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','od under size (-0.003)','1) chips rubbing.2) single tool running3)in data sheet have single tool so single tool running.\r\n','additional tool added and run the part\r\n\r\n\r\n\r\n\r\n','additional tool added in datd sheet and run the the part for next every batch.\r\n\r\n\r\n\r\n\r\n','Next batch found satisfactory','','2014-11-15','Narasimhamurthy(K.G.)','GUNDEGOWDA(H.G.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','6','no','Misc','Narasimhamurthy(K.G.)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7922,'18-123A','Magellan Aerospace Bournemouth','FORK END OUT BD','W71530','D575 41546 202','S80 FHT','B',1,'RP400840','','38143','','0000-00-00',NULL,'yes','yes','yes','','','','','','no','runinng time bore (+) side,','Tool was worn out without noticing it operator ran the part and found oversize.','Tool life will be monitored and tool will be changed for some number of parts. ','Tool life will be monitored and tool will be changed for some number of parts. ','Next part found okay. Tool life is getting monitored','','2014-11-15','Anjinamurthy(H)','        Manohara M','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7923,'18-211B','Magellan Aerospace(Chalfont) Limited','PLUNGER','238302','D321 40205 200','','H01, ECN NR29998ST1JB80',1,'P/074114','','36524','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Id Thread tight.','Thread gauge was not butting.','Next time thread gauge kept to be free. ','Any threaded parts after machining checked in machine before removing. ','Rework under progress ','','2014-11-16','Dinakar(K)','Theerthappa K.N.,Shivaraj K S,SHIVAKUMAR ,Ningaraj A N,Nataraja C V,Manjunatha N,Lohith K,Kalakappa T H,Dinakar K,Bharath R,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Manufacture Only','','FI','yes','QT100S-2','Narasimha Murthy(R)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7924,'28-002A','Magellan Aerospace New York  Inc.','LOWER LINK','G19441K01BX','161A6104-4','','PL Rev_B, DL Rev_N/C',1,'123667_R0_C0','','37154','','0000-00-00',NULL,'no','no','no','yes','no','yes','no','yes','no','1)Dent mark on the part.','After treatment dent marks found on the part','Informed both CIM team and Treatment house teams to handle the part carefully while packing. Instructions board has been displayed in Packing department regarding care to be taken while packing the part.','Informed both CIM team and Treatment house teams to handle the part carefully while packing. Instructions board has been displayed in Packing department regarding care to be taken while packing the part.','Next batch found okay','','2014-11-17','Avinash(R.J.)','Sudhagar(V)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','0','Post DN','no','Misc','Sudhagar(V)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7925,'18-123A','Magellan Aerospace Bournemouth','FORK END OUT BD','W71530','D575 41546 202','S80 FHT','B',1,'RP400840','','38143','','0000-00-00',NULL,'yes','yes','yes','','','','','','no','running time rotate so part dig mark','In this setup clamping of the part is on threaded side. i.e. threaded side made to clamp, while clamping operator missed to tight the bolts.','Instructed to operator that bolts should be tighten fully before running the part.','Instructed to operator that bolts should be tighten fully before running the part.','Next part found okay.','','2014-11-17','Anjinamurthy(H)','        Mohan Kumar C.M.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7926,'35-178','Saab AB','SUPPORT-SEAL-RETAINER','748191A4','423Z1833-3-02','','---',1,'1600093935','','38599','','0000-00-00',NULL,'yes','yes','yes','','','','','','','part running time dia 6ballnose broken so part dig .','Dia 6 ballnose running time tool broken,so part dig.  ','Next change the tool check stock, to change or avid stock in 6 ballnose. then ok.','All wall & base finish in dia 10 ballnose, 6 ballnose only for R3 radius finishing , so no stock in 6 ball.','Next batch found satisfactory','','2014-11-17','Rangaswamy()','        Gurukiran S M','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7927,'28-006','Ellanef Manufacturing Corporation','SHOULDER BOLT','G19876K01','162A3109 2','15-5PH Bar,Per AMS56','NA',2,'117105_R0_C1','','37239','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1)Thread Gauge not answer.','Thread gauge was not butting.  \r\n\r\n','Next time thread gauge kept to be free.','Any threaded parts after machining checked in machine before removing. ','CAPA unsufficient','','2014-11-17','Dinakar(K)','Theerthappa K.N.,Shivaraj K S,Rajesh B D,KRISHNAMURTHY N,Hari Prasad,GUNDEGOWDA H.G.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Manufacture Only','0','FI','yes','DX 200-3','Sudhagar(V)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7928,'28-006','Magellan Aerospace New York  Inc.','SHOULDER BOLT','G19876K01','162A3109 2','15-5PH Bar,Per AMS56','NA',1,'120168_R0_C0','','35966','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1)Thread dent.','part handling problem. ','parts are puted in wooden pallets. ','parts are puted in wooden pallets. ','Next batch found satisfactory','','2014-11-17','Dinakar(K)','Theerthappa K.N.,Shivappa M B,Rajesh B D,KRISHNAMURTHY N,Hari Prasad,GUNDEGOWDA H.G.,Girish V M,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','0','FI','no','DX 200-2 ','Sudhagar(V)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7929,'28-006','Ellanef Manufacturing Corporation','SHOULDER BOLT','G13088','162A3109 2','15-5PH Bar,Per AMS56','NA',3,'117105_R0_C1','','38520','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1)Thread chattering.','while running time revolving center not rotate properly.','proper pressure adjusted to revolving center and the run the part.','proper pressure adjusted to revolving center and the run the part.','Next batch found satisfactory','','2014-11-17','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','0','FI','no','Misc','Sudhagar(V)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7930,'28-041','Magellan Aerospace New York  Inc.','LEVER ASSY-SECONDARY SPOI','158326','65-46358-16','','PL_E, DL_N/C, Sketch # 1',6,'122693','','35843','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1)Bore over size by 0.010 to 0.012MM.','Insert was worn out so this problem occurred ','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','Next batch found okay','','2014-11-17','Avinash(R.J.)','Theerthappa K.N.,Shivaraj K S,Shivappa M B,S. Shiva Kumar,Rajesh T,Punith G S,Mohan Kumar C.M.,Manjunatha N.R.,Manjunatha N,Lohith K,Hari Prasad,Diwakar R.B.,Dinakar K,Dhananjaya N,Devaraj K.C.,Bharath R,Anjinamurthy H,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','DX 200-1','Sudhagar(V)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7931,'28-006','Ellanef Manufacturing Corporation','SHOULDER BOLT','G19876K01','162A3109 2','15-5PH Bar,Per AMS56','NA',2,'117105_R0_C1','','37239','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1)Thread Gauge not answer.','Thread gauge was not butting.','Next time thread gauge kept to be free.','Any threaded parts after machining checked in machine before removing.','Next batch found okay','','2014-11-17','Dinakar(K)','Theerthappa K.N.,Shivaraj K S,Rajesh B D,KRISHNAMURTHY N,Hari Prasad,GUNDEGOWDA H.G.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Manufacture Only','0','FI','yes','DX 200-3','Sudhagar(V)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7932,'35-188','Saab AB','INTERCOSTAL_MIDSPAN_NO_2 ','426691 A','423Z1170-1-05','','---',1,'NOV 2014 ','','37381','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','*Dimension 2.54mm tool dig mark.* ','While running operation -02 part not butted properly due to clamping screw is not sufficient for part.\r\nPart thickness measures minus side in all pockets.  ','Due to process problem this deviation coming.\r\nProcess changed to avoid such problems,Clamping method changed instead of using screws from top side Allen screws placed from bottom to strengthened the clamping. ','Process changed to avoid such problems,Clamping method changed instead of using screws from top side Allen screws placed from bottom to strengthened the clamping.  \r\nAfter changing the clamping method 70nos production completed and all parts found OK.','Next part found okay','','2014-11-17','Rangaswamy()','Rangaswamy()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Rangaswamy()',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7933,'28-007A','Magellan Aerospace New York  Inc.','Shaft Support Lever','0-25-06718','251A1747-1','Ti-6AL-4V Per Mil-T-','N/C',1,'123424-3186_R0_C0','','37160','','0000-00-00',NULL,'yes','yes','yes','','','','','','','taper problam OD (-) 0.003mm','1) chips rubbing.2) single tool running3)in data sheet have single tool so single tool running.','additional tool added and run the part','additional tool added in datd sheet and run the the part for next every batch.','Next batch found okay','','2014-11-17','Ravi(M)','        Manjunatha N','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7934,'28-006','Ellanef Manufacturing Corporation','SHOULDER BOLT','G19876K01','162A3109 2','15-5PH Bar,Per AMS56','NA',2,'117105_R0_C1','','37239','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1)Thread Gauge not answer.','Thread gauge was not butting.','Next time thread gauge kept to be free.','Any threaded parts after machining checked in machine before removing.','Next batch found okay','','2014-11-17','Dinakar(K)','Theerthappa K.N.,Shivaraj K S,Rajesh B D,KRISHNAMURTHY N,Hari Prasad,GUNDEGOWDA H.G.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Manufacture Only','0','FI','yes','DX 200-3','Sudhagar(V)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7935,'18-090A','Magellan Aerospace Bournemouth','BUSH','235508','D278 50164 200','S80 FHT','A',1,'RP400843','','38527','','0000-00-00',NULL,'yes','yes','yes','','','','','','','power trip','running time power tripped that time o.d was digmark. ','We are inform to the maintenence for the proper UPS connection.','We are inform to the maintenence for the proper UPS connection.','','','2014-11-17','Dinakar(K)','        Devaraj K.C.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7936,'18-090A','Magellan Aerospace Bournemouth','BUSH','235508','D278 50164 200','S80 FHT','A',1,'RP400843','','38527','','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. ','We are inform to the maintenence for the proper UPS connection.','We are inform to the maintenence for the proper UPS connection.','','','2014-11-17','Dinakar(K)','        Seetharamu D','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7937,'18-392B','Magellan Aerospace Bournemouth','END COVER','M510610','D278 50167 200','','D',3,'RP401023_Amend No.-1','','37290','','0000-00-00',NULL,'yes','no','yes','no','yes','no','no','no','no','C-axis problem,so profile shift.','C-axis position not locked in properly.','inform to the maintenence and haas maintenence team.','inform to the maintenence and haas maintenence team.','Maintenance done and next parts found okay','','2014-11-17','Dinakar(K)','SHIVAKUMAR ,Dinakar K,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','3','no','ST20','Narasimhamurthy(K.G.)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7938,'35-177','Saab AB','ALCD_STRUCT_BEAM-LOWER_OU','540268','423Z1404-5-02','','---',2,'NOV 2014 ','','37364','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Base Thickness measures minus side.','While running operation -02 part not butted properly due to clamping screw is not sufficient for part.\r\nPart thickness measures minus side in all pockets.  ','Due to process problem this deviation coming.\r\nProcess changed to avoid such problems,Clamping method changed instead of using screws from top side Allen screws placed from bottom to strengthened the clamping.  ','Process changed to avoid such problems,Clamping method changed instead of using screws from top side Allen screws placed from bottom to strengthened the clamping.  \r\nAfter changing the clamping method 70nos production completed and all parts found OK.\r\n\r\n','Next part found okay','','2014-11-18','Rangaswamy()','Rangaswamy()','','0000-00-00','Base thick Under size.','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Rangaswamy()',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7939,'18-113A','Magellan Aerospace Bournemouth','ADJUSTER','424402','D575 40496 200','S80 FHT','G',1,'RP400840','','37998','','0000-00-00',NULL,'yes','yes','yes','','','','','','','running time air pressure low machine emergency stop so od thread damege..','running time  air pressure  that time o.d was digmark\r\n','We are inform to the maintenence for the proper air connection. ','We are inform to the maintenence for the proper air connection. ','Next batch found okay','','2014-11-19','Dinakar(K)','        Nataraja C V','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7940,'35-165A','Saab AB','HOUSING PIN','541025','423Z1124-5-01','','--A',1,'1600086478','','35800','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','RIB thickness measures 0.7mm oversize.','This problem is due to dia 8 flat long cutter vibration because of tool overhang.\r\nDue to vibration more material removed in wall.','Tool holder changed and checked the tool run out and found 0.012 to 0.016mm.\r\nAfter checking the run out machining started and next part found ok.','Planned to change the process, due to lug in outer surface at 4 places bigger diameter not entering. therefore dia 8 cutter cued to rough and finish the wall.\r\nNew process discussed and implemented with no outer lugs, this will allow to use bigger diameter cutter to finish the wall.','Next parts found okay','','2014-11-19','Avinash(R.J.)','Manjunath(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','14656','post DN','no','Misc','Manjunath(G)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7941,'18-293C','Magellan Aerospace Bournemouth','BAFFLE ADAPTOR ','5719','L281 50313 200','','D00',1,'RP400946','','38265','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dia 4.83 drill  drawing   required 1 side but drill was 2 side.','The difference 2 side holes is nearly 0.1 mm due to misinterpretation of the visual effect 2 side drill has been done','suitable pin will be inserted for the drill hole and it will be taken as reference point for the next drill operation','suitable pin will be inserted for the drill hole and it will be taken as reference point for the next drill operation','Next parts found okay','','2014-11-19','Nagaraju(T)','Nagaraju(T)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','00','no','Misc','Nagaraju(T)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7942,'35-116','Saab AB','ALCD_STRUCT_INTERCOSTAL_L','564338','423Z1177-3','7050-T7451 ALUMINUM ','--A',1,'1600097307','','39013','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Tool dig mark in part base face.','Dia 16R3 running  time tool dig in base, because  makino m/c proved   program edit & run in jyoti m/c, in center of the program G18 generated,  change  \"XY\" plane  so tool dig.','Stop the machine ,inform to supervisor ,next  program taken in CAD/CAM  then run ,next part found ok.','No edit in any program, any changes in program inform to supervisor & CAD/CAM department.','Next batches found good\r\n','','2014-11-19','Rangaswamy()','Siddaramappa()','','0000-00-00','Tool dig mark in part base face.','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','01','no','Misc','Rangaswamy()',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7943,'35-184','Saab AB','CED_LATCH_FITTING-AFT','642318A0','425Z0610-16','','---',1,'1600093935','','38615','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Dig mark on part.','While running serration operation in operation-04, While running dia 10 ball nose part lifts from fixture this caused dig mark.\r\nThe route cause for this is due to clamping not done correctly.','Part clamped in Fixture and process was proved and parts manufactured after FAI completion with the same process.(191 nos manufactured till date)\r\nWe analyzed the problem and not find any process related problems. Therefore again machining done with same process by checking the clamping and remaining 25nos found ok in this batch.','Message entered in beginning of program to ensure the clamping once again before running the program.\r\n','Next parts found okay','','2014-11-20','Girish(Prasad P)','        Girish Prasad P','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7944,'18-058A','Magellan Aerospace Bournemouth','Top Skin Stiffener','534740-2A1','L575 53250 200','ABM3 1029 7010','A00',2,'RP400837','','36993','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Base Thickness 3 mm +0.13, -0.08 mm measured 2.87 mm to 2.89 mm.','While machining time Part has lifted, due to insufficient clamping.','Provide sufficient clamps to butting the part properly.','Instructed operator to ensure the part butting with the help of feeler gauge before run the part.','Next batch will be taken care and effectiveness will be measured','','2014-11-20','Lohith(K)','Punith G(S)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','04','no','Misc','Lohith(K)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7945,'35-189','Saab AB','INTERCOSTAL_MIDSPAN_NO_2 ','426691 C','423Z1170-1-06','','---',1,'NOV 2014 ','','37374','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Rib milled and dig mark on part.','While running roughing operation part lifts from fixture due to in sufficient clamping.','Production stooped and analyzed the problem and found clamping screws not at good condition and also clamping force is not sufficient.\r\nClamping method changed to Allen bolts to strengthened the clamping from back side. \r\n ','After changing the clamping method production continued and not find any deviations.\r\nProcess proved and checked the clamping force foe all the parts and MPS changed as per new method.','Next batch found okay','','2014-11-20','Rangaswamy()','Rangaswamy()','','0000-00-00','Dimension 4.03 rib milled. ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Rangaswamy()',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7946,'28-004A','Magellan Aerospace New York  Inc.','PIN','G16433R05','161A2332-1','15-5PH Steel Bar per','NA',6,'120243-3172','','37816','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1)Boore over size by 0.12MM.','while running tool come outside the holder or parts not butted properly.','instruction given to operator before giving cut check part\r\nbutted or not by usinf filler set.','instruction given to operator before giving cut check part\r\nbutted or not by usinf filler set.','Next batch found okay','','2014-11-20','Dinakar(K)','S. Shiva Kumar,Rajesh B D,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,'$','Closed','no','yes','no','Manufacture Only','0','FI','no','DX 200-3','Sudhagar(V)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7947,'28-004A','Magellan Aerospace New York  Inc.','PIN','G16433R05','161A2332-1','15-5PH Steel Bar per','NA',4,'120243-3172','','37816','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','ID over size by 0.04 micron.','since it is a blind bore while maching the bore the chips was blocked inside the bore which took extra material by\r\nrubbing to the bore at the end.','1.coolant nozzle was set along with the tools so as to remove the chips from the bore.','a station was provided in the programm to clean the chips.','Next batch found okay','','2014-11-20','Dinakar(K)','Rajesh B D,GUNDEGOWDA H.G.,Ashith B,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','11','no','DX 200-3','Ravi(M)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7948,'28-004A','Magellan Aerospace New York  Inc.','PIN','G16433R05','161A2332-1','15-5PH Steel Bar per','NA',1,'120243-3172','','38400','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','opn no 1 drill out so bore plus side.','Hole got oversize because of drill run out. \r\n','After drilling operation the drill dia will be checked before boring and after boring also the dia will be checked.  \r\n','Drilling operation will be done with short distance after ensuring the runout, whole drilling\r\noperation will be done.  \r\n','Next batch found satisfactory','','2014-11-20','Dinakar(K)','Rajesh B D,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','11','no','DX 200-3','Ravi(M)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7949,'28-004A','Magellan Aerospace New York  Inc.','PIN','G16433R05','161A2332-1','15-5PH Steel Bar per','NA',2,'120243-3172','','38399','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','ID over size by 0.04 micron.','since it is a blind bore while maching the bore the chips was blocked inside the bore which took extra material by\r\nrubbing to the bore at the end.','1.coolant nozzle was set along with the tools so as to remove the chips from the bore.','a station was provided in the programm to clean the chips.','Next batch found okay','','2014-11-20','Dinakar(K)','Rajesh B D,GUNDEGOWDA H.G.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','11','no','DX 200-3','Ravi(M)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7950,'35-190','Saab AB','INTERCOSTAL_MIDSPAN_NO_4','564309','423Z1171-2-03','','---',1,'1600093935','','38607','','0000-00-00',NULL,'yes','yes','yes','','','','','','','part running time dia 12r3 broken so part dig mark.','Dia 12r3 running time broken because tool wear-out or stock in ruffing program.   ','Change dia 12r3 then change the re-ruff progrem then run.  ','In every 10nos runned check all the tool.','Next batch found satisfactory','','2014-11-20','Rangaswamy()','        Umesh B','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7951,'18-079B','Magellan Aerospace Bournemouth','TOP SKIN STIFFNER 3','556796A1','L575 53251 201','','A00',4,'RP400837','','38743','','0000-00-00',NULL,'yes','yes','yes','','','','','','no','dia 32 f/m running time insart brakage t-3 thickness 0.05 - side ','Under discussion with customer whether to accept or Reject','Under discussion with customer whether to accept or Reject','Under discussion with customer whether to accept or Reject','Under discussion with customer whether to accept or Reject','','2014-11-20','Lohith(K)','        Chiranjeevi S','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','no','yes','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7952,'18-211B','Magellan Aerospace(Chalfont) Limited','PLUNGER','238302','D321 40205 200','','H01, ECN NR29998ST1JB80',1,'P/074114','','38419','','0000-00-00',NULL,'yes','yes','yes','','','','','','','While running time part chips rub (-) 0.007 ','Insert was worn out so this problem occurred\r\n\r\n\r\n\r\n\r\n','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.','Next batch found okay','','2014-11-20','Dinakar(K)','        Ningaraj A N','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7953,'18-386A','Magellan Aerospace(Chalfont) Limited','NUT RING INNER','487664','D575 40039 200','','B',2,'P/074123','','37621','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','ID Slot width over size 0.5 to 0.7mm.','While doing slotting operation this deviation coming due to slotting tool wear out.\r\nSlotting width not checked for 02nos while running production due to process stability.\r\n','After finding a deviation in slot width, all the parts checked and found OK.\r\nAfter checking the all the parts production continued with new slotting tool and found ok.','Informed to operator to check the tool wear regularly. and also check the slot width 100% by slip gauge.','Next parts found okay','','2014-11-21','Krishna(Chowdary.G.P.)','Ningaraj A N,Nataraja C V,Manjunath  M,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','QT100S-1','Narasimha Murthy(R)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7954,'35-231A','Saab AB','HINGE BRACKET 4 ','425130','D576 50007 208','','E00',2,'1600095733','','39038','','0000-00-00',NULL,'yes','yes','yes','','','','','','','94mm total width measures 93.5mm.','While doing first off proving Dia 80 face mill Tool wear edited by operators and 0.2mm part width measures minus side on both the sides.','After inspecting the parts by operator in production, changed the tool wear and continued production.\r\nAfter approving dimension by QAD production continued.','1.Training conducted for operator (MR. Sundar Employee no.   400198)for checking the tool wear and editing the tool wear in machine.\r\n','Next batches found good\r\n','','2014-11-21','Girish(Prasad P)','        Sundar D.K.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7955,'18-211B','Magellan Aerospace(Chalfont) Limited','PLUNGER','238302','D321 40205 200','','H01, ECN NR29998ST1JB80',1,'P/074114','','38419','','0000-00-00',NULL,'yes','yes','yes','','','','','','','While running time part chips rub (-) 0.007 							\r\n','Insert was worn out so this problem occurred 							\r\n','Check insert status regularly and know the life of inserts and change inserts according instructions.							\r\n 							\r\n','Check insert status regularly and know the life of inserts and change inserts according instructions. 							\r\n','Next batch found okay','','2014-11-21','Dinakar(K)','        Ningaraj A N','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7956,'18-382A','Magellan Aerospace(Chalfont) Limited','SLEEVE BEARING ','230330','D575 40037 200','','A',1,'P/074123','','38310','','0000-00-00',NULL,'yes','yes','yes','','','','','','','tnmg tool given to mazak-2, not taken minus tool offset. part run so id (+) side..  ','while setting time after i.d roughing more stock given to the finishing tool that time finishing\r\ninsert will be brocken. ','adjusting stock for finishing tool and run the part. ','setting time after running the o.d or i.d,set the stock for finishing tool then run the part.this\r\nsame instruction inform to the operator. ','Next batch found okay','','2014-11-21','Dinakar(K)','        Nataraja C V','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7957,'35-234A','Saab AB','HINGE BRACKET 5 ','425129','D576 50008 209','','D00',1,'1600093863 Rev-2','','38763','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Dig mark in Bore.','As the tool was blunt while machining at bore side , bore got  dig marks ','Ensure the life of the tool for both aluminium and Steel parts.Planned to prepare the register for the life of the tools and before machining the tool will be checked','Ensure the life of the tool for both aluminium and Steel parts.Planned to prepare the register for the life of the tools and before machining the tool will be checked','Next batch found okay','','2014-11-22','Rangaswamy()','Rangaswamy()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','Misc','Avinash(R.J.)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7958,'18-382A','Magellan Aerospace(Chalfont) Limited','SLEEVE BEARING ','230330','D575 40037 200','','A',1,'P/074123','','38310','','0000-00-00',NULL,'yes','yes','yes','','','','','','','tnmg tool given to mazak-2 not taken minus tool offset part run so o.d (-) side..  ','while setting time after o.d roughing more stock given to the finishing tool that time finishing\r\ninsert will be brocken. ','adjusting stock for finishing tool and run the part. ','setting time after running the o.d or i.d,set the stock for finishing tool then run the part.this\r\nsame instruction inform to the operator. ','Next batch found okay','','2014-11-22','Dinakar(K)','        Nataraja C V','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7959,'18-215C','Magellan Aerospace(Chalfont) Limited','ROD END ASSMY - MALE ','245160','D321 53012 200','','F01, ECN NR29998ST1KH40',2,'P/074113','','38121','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Thread Nogo answared. thread effect dia under size 0.03mm.','1)offset problem. 2)after changing the insert not taken in plus (+) side. 3)He taken plus in other tool  4)operator problem\r\n','before setting give the instruction about part and setting to the operator.\r\n\r\n\r\n\r\n','before setting give the instruction about part and setting to the operator.\r\n\r\n\r\n\r\n\r\n','Next batch found okay','','2014-11-22','Narasimhamurthy(K.G.)','Seetharamu D,Girish V M,Dinakar K,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','7','no','DX 200-2 ','Narasimhamurthy(K.G.)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7960,'18-295A','Magellan Aerospace Bournemouth','BOLT','A0484U','D577 56145 200','S80','A',1,'RP400846','','37534','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Air pressure low so OD Thread dig mark.','running time air pressure that time o.d thread was digmark','We are inform to the maintenence for the proper air connection.','We are inform to the maintenence for the proper air connection.','Next batch found okay','','2014-11-22','Dinakar(K)','        Ravi M','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7961,'35-082','Saab AB','HOUSING-SIDE ROLLER','425389','F579 53065 202','ABM3-1029 T7651','B, PG52307ST4KA80',1,'1600082589','','38833','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Thread damage due to tap broken','While machining tap broken, because of chips clogging in hole causes thread got damaged.','1.Informed to operator to blow the air after pre drilling to avoid chips clocking in hole.\r\n2.Optional stop given after tool change(TAP,to ensure chips clogging in tap.\r\n3.Future batches Standard Tap life will be measured for certain numbers and after that Taps will be changed.','1.Future batches Standard Tap life will be measured for certain numbers and after that Taps will be changed. This will be continued for the future batches also.\r\n2. Dedicated tools set done to monitor tool life. ','Next batch found okay','','2014-11-22','Lohith(K)','        Dhananjaya N','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7962,'18-211B','Magellan Aerospace(Chalfont) Limited','PLUNGER','238302','D321 40205 200','','H01, ECN NR29998ST1JB80',1,'P/074114','','38420','','0000-00-00',NULL,'yes','yes','yes','','','','','','','While running time part chips rub (-) 0.007. 							\r\n','Insert was worn out so this problem occurred.							\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. ','Next batch found okay','','2014-11-22','Dinakar(K)','        Ningaraj A N','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7963,'18-293C','Magellan Aerospace Bournemouth','BAFFLE ADAPTOR ','5719','L281 50313 200','','D00',1,'RP400946','','38265','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Width under size 0.2mm','Wrong Z offset taken by the new operator','Hence the operator was new the supervisors instructed him to take proper offsets live in machines and trained the personal. ','For setting and taking offsets supervisors will ensure it first after that parts will be taken for manufacture.','Next batch found okay','','2014-11-23','Anjinamurthy(H)','Shivappa M B,Ravi R,Mohan Kumar C.M.,Manohara M,GUNDEGOWDA H.G.,Devaraj K.C.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','FI','no','BMV 45-2','Narasimha Murthy(R)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7964,'18-214A','Magellan Aerospace(Chalfont) Limited','SPECIAL WASHER ','245160','D321 40210 202','','E01, ECN NR29999ST1JB79',1,'P/074114','','38708','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Face dig mark.','New manufacturing method was implemented by manufacturing new fixture first part got dig mark','Fixture got ok and part found okay','Fixture got ok and part found okay','Batch found very good and satisfactory','','2014-11-23','Ashith(B)','S. Shiva Kumar,Manjunatha N.R.,KRISHNAMURTHY N,GUNDEGOWDA H.G.,','','0000-00-00','Basavaraju.sB','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','FI','no','BMV 60-1','Narasimha Murthy(R)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7965,'35-057','Saab AB','7605197-201','27326-1','L574 55197 201','ABS 5125 A 016 N','C, ECN - PG69999001',1,'1600094539','','38993','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','2mm  pocket depth side profile length over size by +2mm.','Wrong correction given by the operator in 2nd setup while marking','Necessary training will be given by both supervisors Anjina Murthy and Lohith. ','Necessary training will be given by both supervisors Anjina Murthy and Lohith. ','Next parts found good.','','2014-11-24','Lohith(K)','Hari(Prasad)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','00','no','Misc','Anjinamurthy(H)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7966,'35-237A','Saab AB','JACK BRACKET 2 ','133891','D576 50010 206','','D00',1,'1600093863 Rev-2','','38758','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Thickness minus at web area (0.2)','While machining pocket roughing in operation -02 part vibrates and chatter mark observed on wall causes thickness minus side by 0.2mm.\r\nRoute cause for part vibration is, butting surface is not flat in operation -02.(in RM stage Taper cutting surface part are coming from RM supplier)\r\n\r\n','For all the JACK BRACKETS, while doing Tapping and drilling operation in operation-01, Facing tool added and maintained flatness to strengthening the clamping for operation-02.\r\nThe above operation added and checked the clamping strength by running 10 nos and found OK. \r\n','After taking the above Corrective action we are not find any deviation on parts.\r\nFacing operation added in MPS and also informed to QAD to do a Internal Delta FAI.','Next batch found okay','','2014-11-25','Rangaswamy()','Rangaswamy()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','DN','no','Misc','Manjunath(G)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7967,'18-211B','Magellan Aerospace(Chalfont) Limited','PLUNGER','238302','D321 40205 200','','H01, ECN NR29998ST1JB80',8,'P/074114','','38584','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','1)OD dentmark.','Dent on the parts while holding in the vise. ','Advised to use Aluminum Jaws for vise.   ','Advised to use Aluminum Jaws for vise.   ','Next batch found ok.','','2014-11-25','Nagaraju(T)','Nagaraju(T)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','0','09','no','Misc','Nagaraju(T)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7968,'28-007A','Magellan Aerospace New York  Inc.','Shaft Support Lever','0-25-06718','251A1747-1','Ti-6AL-4V Per Mil-T-','N/C',3,'123424-3186_R0_C0','','37160','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','OD under size 0.003 to 0.004 micron.','1) chips rubbing.2) single tool running3)in data sheet have single tool so single tool running.','additional tool added and run the part','additional tool added in datd sheet and run the the part for next every batch.','Next batch found okay','','2014-11-26','Dinakar(K)','Shantala Devi V,Rajesh B D,Manjunatha N,KRISHNAMURTHY N,GUNDEGOWDA H.G.,Dinakar K,Bharath R,Ashith B,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','QT100S-2','Narasimha Murthy(R)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7969,'35-119','Saab AB','ALCD_STRUCT_INTERCOSTAL_L','632530A2','423Z1178-4','7050-T7451 ALUMINUM ','--A',1,'PA-1300 2014-2','','36658','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Rib length is mines.','Re-work time total length minis, because dia 12R3 running place dia 12R4 runned in 2nd setup ,so this part re-work. ','This CRN tools detected, so No wrong tool selected. program inside insert massage check tool radius. ','This CRN tools detected, so No wrong tool selected. program inside insert massage check tool radius.','Next batch found okay','','2014-11-26','Rangaswamy()','Rangaswamy()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','DN','no','Misc','Manjunath(G)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7970,'35-162','Saab AB','BEAM-LOWER_INNER_AFT','541688','423Z1403-2-02','','---',1,'1600086478','','35540','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Extra material stock in wall.','While running wall finishing operation,machine tripped due to power problem and step in wall program is not runned and continued remaining programs by mistake.','All the parts wall thickness checked and found ok. one no. can rework by taking dia 3.02 hole reference.\r\n','Power fail is regular because all the machines are under UPS. this error will not repeat in future.\r\nAlso informed to operators to check the program sequence once, if any destruction in between machining cycle. ','Next parts found okay','','2014-11-26','Rangaswamy()','Rangaswamy()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','','DN','yes','Misc','Manjunath(G)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7971,'35-237A','Saab AB','JACK BRACKET 2 ','133891','D576 50010 206','','D00',1,'1600095733','','39132','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Dig mark on part.','While running boring operation operator wrongly edited the CRC value for bore finish program.\r\nThis error in editing causes dig mark.','CRC value corrected and continued production.\r\nThis is the proven process and need not to take any CA for this.Need close monitoring of operators to concentrate on work.','This is the proven process and need not to take any CA/PA for this.Need close monitoring of operators to concentrate on work.','Next batches found good\r\n','','2014-11-26','Girish(Prasad P)','        Sundar D.K.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7972,'18-322A','Magellan Aerospace Bournemouth','BRACKET','565504','L575 52483 200','ABM3 1030','A00',1,'RP400946_Amnd_No.1','','38504','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dia 4.0 mm Hole oblong (dia 4.00 mm +0.12 measure 4.25 mm) ','While drilling the bit got tilted and part found oversize','After clamping the job, tight the drill bit properly and then drill will be done','After clamping the job, tight the drill bit properly and then drill will be done','Next part found okay','','2014-11-28','Nagaraju(T)','Nagaraju(T)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','00','no','Misc','Nagaraju(T)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7973,'18-323A','Magellan Aerospace Bournemouth','BRACKET','565504','L575 52483 201','ABM3 1030','A00',1,'RP400946','','38362','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dia 4.0mm Hole ambling (dia 4.00mm +0.12 measure 4.25mm)','While drilling the bit got tilted and part found oversize','After clamping the job, tight the drill bit properly and then drill will be done','After clamping the job, tight the drill bit properly and then drill will be done','Next batch found okay','','2014-11-28','Nagaraju(T)','Nagaraju(T)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','00','no','Misc','Nagaraju(T)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7974,'35-058','Saab AB','7605198-200','26910-1','L574 55198 200','ABS 5125 A 016','C',3,'1600090315','','37641','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','yes','1)1 have paint release on primer. Protective material was stuck on the part when received. Affected area 13 x 6mm, metal not affected. See pictures paint release and protective material.\r\n2)1 is discolored on primer. See picture Discolored.\r\n3)1 has FOD in primer, affected area 4x4mm. See picture FOD.\r\n','After sending the parts to customer, paint chip up in some areas were found, due to packing methods','As these parts will be sent directly to customer from treatment house, one person has been appointed for visual inspection of treated parts only. And training provided for both visual and packing inspections','As these parts will be sent directly to customer from treatment house, one person has been appointed for visual inspection of treated parts only. And training provided for both visual and packing inspections','Next batches found good ','C33368','2014-11-28','Avinash(R.J.)','Manjunath(G)','Through mail dated 28th Nov2014 from Marcus','2014-11-28','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','15178','cust end','yes','Misc','Manjunath(G)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7975,'35-082','Saab AB','HOUSING-SIDE ROLLER','3966601 2','F579 53065 202','ABM3-1029 T7651','B, PG52307ST4KA80',1,'1600073867','','34264','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','NDT Failed.','Due to polishing or tool rubbing marks NDT got failed in treatment house','Polishing should be avoided, speed and depth of cutting and tool marks should be avoided. Instructed CAD and Production to modify the program and run with low RPM\r\n','Polishing should be avoided, speed and depth of cutting and tool marks should be avoided. Instructed CAD and Production to modify the program and run with low RPM\r\n','Next batches found satisfactory','','2014-11-28','Avinash(R.J.)','Manjunath(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','14812','post Dn','no','Misc','Manjunath(G)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7976,'18-056B','Magellan Aerospace Bournemouth','Top Skin Stiffener ','402690 A2','L575 53249 200','','A00',1,'RP400837','','39186','','0000-00-00',NULL,'yes','yes','yes','','','','','','','3.25 drill holder rabing in rib so part dig mark and reject','Due to short in length of drill holder part found dig mark','A register has been maintained for the length. Holders will be given to operator according to CRN\'s','A register has been maintained for the length. Holders will be given to operator according to CRN\'s','Next part found okay','','2014-11-28','Anjinamurthy(H)','        Girish HP','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7977,'35-236A','Saab AB','JACK BRACKET 1','133891','D576 50009 207','','D00',1,'1600095733','','39118','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Rib dig mark & thickness minus. ','In the Part dig Mark happened, When I machining is running,  Dia 20*R5 Bull Nose cutting tool Pull out from the Tool holder due to Hydraluic clamping failure in the Tool holder.','Stop the production, to change the progrem in dia 25r2 cutter using for ruffing, then countinu the production.','Using dia 25r2 for ruffing. Stop I machining progrem.','Next batch found okay','','2014-11-29','Rangaswamy()','                Karthineyan V.S.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7978,'35-030A','Saab AB','7600169-200 ','3419701 4','L574 50169 200','','B00, PG74415001JA01',1,'1600087247 Rev 1','','36422','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Digmark noticed on outer profile.','outer wall program running time power failed, UPS also not working,part not holding in vacuum , but\r\nspindle was running so part is dig.','inform to maintenance team,check the UPS system. inform to operator stop the spindle manual.','inform to maintenance team,check the UPS system. inform to operator stop the spindle manual.','Next parts found okay','','2014-11-29','Narayanappa(G)','Narayanappa(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','yes','With Treatment','','DN','no','Misc','Manjunath(G)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7979,'18-056B','Magellan Aerospace Bournemouth','Top Skin Stiffener ','402690 A2','L575 53249 200','','A00',3,'RP400837','','39185','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dia 10B/N Broken So 3.25 wall thickness under size.','Chips clogged to ball nose while machining so, wall thickness undersize','Asked for Re Engineering for CAD department. Until re engineering done part will not be machined.','Asked for Re Engineering for CAD department. Until re engineering done part will not be machined.','Next batch found okay','','2014-11-29','Anjinamurthy(H)','Girish(HP)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','00','no','Misc','Anjinamurthy(H)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7980,'18-110A','Magellan Aerospace Bournemouth','FORK END INTERMEDIATE','242096','D575 40494 202','S80 FHT','J',79,'RP400840','','33664','','0000-00-00',NULL,'yes','no','no','no','yes','yes','no','no','no','1/2 20 UNJF 3A OD Thread Gauge go not answer.','theard gauge was problem,so thread effect dia over size then parts are rework done. 							\r\n','parts are ok. 							\r\n','parts are ok. 							\r\n','parts are okay. 							','','2014-12-01','Dinakar(K)','Shivappa M B,Rajesh T,Punith G S,Mohan Kumar C.M.,Manohara M,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Manufacture Only','0','FI','yes','DX 200-1','Nandishkumar(D.K.)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7981,'18-414B','Magellan Aerospace Bournemouth','ACTUATOR HOUSING','M563530','D278 50163 200','','D',1,'RP401021_Amnd No. 1','','38898','','0000-00-00',NULL,'yes','yes','yes','','','','','','','operator mistak so part 0.4 - side thicknas','Due to butting face not cleaned properly .So part thickness under size. 							\r\n','Before load the part of the butting face cleaned by air per sure then load the part.							\r\n','Before load the part of the butting face cleaned by air per sure then load the part. 							\r\n','Next batch found okay','','2014-12-01','Dinakar(K)','        Devaraj K.C.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7982,'35-030A','Saab AB','7600169-200 ','3419701 4','L574 50169 200','','B00, PG74415001JA01',1,'1600087247 Rev 1','','36422','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Digmark noticed on outer profile.','outer wall program running time power failed, UPS also not working,part not holding in vacuum , but spindle was running so part is dig. ','inform to maintenance team,check the UPS system.\r\ninform to operator stop the spindle manual.  ','inform to maintenance team,check the UPS system weekly one time,\r\ninform to operator stop the spindle manual.  ','Next parts found good. UPS problem solved','','2014-12-02','Narayanappa(G)','Narayanappa(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','yes','With Treatment','','DN','no','Misc','Manjunath(G)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7983,'18-159C','Magellan Aerospace Bournemouth','STRUT FWD INNER','A615348','F574 50155 200','','B01, ECN PG49998ST1TW20, PG40011ST1KK20',1,'RP400845','','39267','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','part profile dig mark ','program running time part lifted, due to improper clamping.','we will check the clamp & bolt before loading the part,   \r\nmade a new clamp then part clamped proper,\r\n ','we will check the clamp & bolt before loading the part,   \r\nmade a new clamp then part clamped proper,\r\nwe will ensure that clamping is proper before program running. ','Next parts found good.','','2014-12-03','Narayanappa(G)','Manjunath(K.N.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','01','no','Misc','Narayanappa(G)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7984,'18-101A','Magellan Aerospace Bournemouth','TUBE-STRUT','G9438','D572 50464 202','T45','F',1,'RP400839','','38444','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Hole over size 0.04mm','While drilling the part was not fully clamped to jig.','Instructed operator to ensure the part before drilling whether the part is fully clamped and also ensure the condition of the drill.','Instructed operator to ensure the part before drilling whether the part is fully clamped and also ensure the condition of the drill.','Next part found okay','','2014-12-04','Nagaraju(T)','Shivanand D.B.,SHIVAKUMAR ,Raghavendra Rao R,','','0000-00-00','Irappa badiger.','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','FI','no','ST20','Narasimha Murthy(R)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7985,'18-279A','Magellan Aerospace(Chalfont) Limited','DOOR OUTER TYPE 23','217769 001','L572 53721 200','ABS5032A055','B00',1,'P/074117','','37108','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','280.60 +/-0.50 Total width undersize 279.92 measured.','In 1setup running time dimension 269.1 +/- 0.2 this dimension properly not checked .so in 2nd setup outer profile stock minus side ,so  part rejected.','Instruct to operator  check every dimension & train to use checking  instruments. then using profile checking gauge.','In 2setup running time to use outer profile checking gauge add in process sheet.  \"GO\" pin & \"NOGO\" pin check in every part.','Next batches found good\r\n','','2014-12-04','Rangaswamy()','Rangaswamy()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','0','FI','no','Misc','Nandishkumar(D.K.)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7986,'35-237A','Saab AB','JACK BRACKET 2 ','133891','D576 50010 206','','D00',1,'1600095733','','38829','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Dim 144.00mm Measured 141.82mm.','After changing 80 face mill insert operator not checked the tool offset. due to insert not seated properly and tool height varies and total thickness measures minus side.','Insert seating corrected and tool offset taken then production continued.','Informed to operator to check the insert seating and mandatory offset to be check after any insert changes.\r\nThis procedures to be monitored in every machine.','Next parts found okay','','2014-12-05','Krishna(Chowdary.G.P.)','        Krishna Chowdary.G.P.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7987,'18-121A','Magellan Aerospace Bournemouth','BARREL - STRUT','247348','D572 50463 201','S98 FHT','F',1,'RP400839','','38270','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Dia 1.55mm drill broken, dig mark observed on hole.','This problem is due to Un-availability of Carbide (     ) drill when plan to start production.\r\nDue to urgency instead of Carbide drill(      ) HSS drill (    )used with proving the correct parameters.\r\nChanging of tool is approved by CAD/CAM.','After finding deviations in Two parts, Parameter adjusted and monitored the tool lip and continued production.\r\n203 nos of Parts continuously machined with 02 nos drills(HSS-     )\r\nInformed to buy Carbide drill(      ) for next batch production and also informed to tool supplier to maintain the stock at any given point of time.','1.Dedicated tools kept for this CRN and also informed to Tool manager to monitor the tool stock. \r\n2.Planned to prove multiple make tools for tools flexibility.\r\n3.Training to be impart to all the operators to calculate the Feed/Speed and monitoring the tool life.','Machine Problem while machining, bore becomes plus side, reason for that is under investigation','','2014-12-05','Anjinamurthy(H)','Rajesh T,Girish V M,Girish HP,Dinakar K,Devaraj K.C.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','FI','no','BMV 60-2','Narasimha Murthy(R)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7988,'35-138','Saab AB','FLCD_DS_SUPPORT_DEFLECT_S','7530455','423Z6189-3','BAC1534-62C','---',2,'1600096186','','39027','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Material chip out thickness minus minmum 1.4 measured1.3(.1minus)','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. \r\n','The following Corrective Action/Preventive Action taken to avoid Materiel chip off.\r\n1. Raw Material will inspect visually before issuing to production. If found any problem visually RM will be quarantined.\r\n2. Dia 8 end mill life calculated, informed to operators to monitor the tool life.and change the tool after as mentioned.','The following Corrective Action/Preventive Action taken to avoid Materiel chip off.\r\n1. Raw Material will inspect visually before issuing to production. If found any problem visually RM will be quarantined.\r\n2. Dia 8 end mill life calculated, informed to operators to monitor the tool life.and change the tool after as mentioned.\r\n3. Steel butting plates flatness inspection done before production starts.\r\nTaking 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.','Next batch found okay','','2014-12-05','Rangaswamy()','Rangaswamy()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','DN','no','Misc','Manjunath(G)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7989,'35-138','Saab AB','FLCD_DS_SUPPORT_DEFLECT_S','501721','423Z6189-3','BAC1534-62C','---',4,'1600097307','','39195','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Material chip out.','The Following Route causes analyzed for material chip off after outer profile machining.\r\n1. Due to RM deviations material will chip off.\r\n2. While running production, the finishing tool wear out causes light chip off in material.\r\n3. Steel Butting sheet for part is not Flat. \r\n','The following Corrective Action/Preventive Action taken to avoid Materiel chip off.\r\n1. Raw Material will inspect visually before issuing to production. If found any problem visually RM will be quarantined.\r\n2. Dia 8 end mill life calculated, informed to operators to monitor the tool life.and change the tool after as mentioned.\r\n3. Steel butting plates flatness inspection done before production starts.','The following Corrective Action/Preventive Action taken to avoid Materiel chip off.\r\n1. Raw Material will inspect visually before issuing to production. If found any problem visually RM will be quarantined.\r\n2. Dia 8 end mill life calculated, informed to operators to monitor the tool life.and change the tool after as mentioned.\r\n3. Steel butting plates flatness inspection done before production starts.\r\nTaking all the above PA, rejections happened in material chip off. Out of 100nos production 5 to 6nos getting rejection. Due to customer requirement parts are manufactures with considering rejections.','Next batch found okay','','2014-12-05','Rangaswamy()','Rangaswamy()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','DN','no','Misc','Manjunath(G)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7990,'35-166A','Saab AB','HOUSING PIN','657639A1','423Z1124-6-01','','--A',1,'1600078597','','38526','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Thickness measures undersize.','In 2 setup ruffing tool running time tool down, so part thickness under size,','Check tool & holder ,increase tool & holding length, scrape tool holder. ','Dedicated tool list in this CRN, & mandatory tool life & holder life.every 10 nos runned check tool & holder.  ','Next batch found okay','','2014-12-06','Rangaswamy()','Yogesha K,Prashanth Kumar M,Manohara B.C.,Gurukiran S M,Basavaraja S. Jr.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','MakinoF5-3','Manjunath(G)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7991,'35-165A','Saab AB','HOUSING PIN','541028','423Z1124-5-01','','--A',1,'1600078597','','38133','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Thickness measures undersize.','Part running time part rotate so dimension 5.08 thickness under size& part bend is one-off reason.','Next  annualize  the  problem addiction extra clamp in part cutout time, next part found ok.','Next batch change process, change programs for avid bend and avid rejection.','Next batches found good\r\n','','2014-12-06','Rangaswamy()','Umesh B,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','MakinoF5','Manjunath(G)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7992,'18-341A','Magellan Aerospace Bournemouth','LANDING TOP PANNEL','A605640','F574 50966 200 01','','E, ECN PG49998ST1TV38',1,'RP400947','','39051','','0000-00-00',NULL,'no','no','no','yes','no','yes','no','yes','no','Corrosion pits observed on the part surface','Due to polishing or tool rubbing marks corrosion fits observed in treatment house','Polishing should be avoided, speed and depth of cutting and tool marks should be avoided. Instructed CAD and Production to modify the program and run with low RPM & parts should be cleaned with PX-24 solvent on regular intervals','Polishing should be avoided, speed and depth of cutting and tool marks should be avoided. Instructed CAD and Production to modify the program and run with low RPM & parts should be cleaned with PX-24 solvent on regular intervals','Next batch found okay','','2014-12-07','Muniyappa(N)','Nandishkumar(D.K.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','15657','POSTDN','no','Misc','Muniyappa(N)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7993,'18-341A','Magellan Aerospace Bournemouth','LANDING TOP PANNEL','A605640','F574 50966 200 01','','E, ECN PG49998ST1TV38',3,'RP400947','','39048','','0000-00-00',NULL,'no','no','no','yes','no','yes','no','yes','no','Corrosion pits observed on the part surface','Due to polishing or tool rubbing marks corrosion fits observed in treatment house','Polishing should be avoided, speed and depth of cutting and tool marks should be avoided. Instructed CAD and Production to modify the program and run with low RPM & parts should be cleaned with PX-24 solvent on regular intervals','Polishing should be avoided, speed and depth of cutting and tool marks should be avoided. Instructed CAD and Production to modify the program and run with low RPM & parts should be cleaned with PX-24 solvent on regular intervals','Next batches found okay','','2014-12-07','Muniyappa(N)','Nandishkumar(D.K.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','15658','POSTDN','no','Misc','Muniyappa(N)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7994,'18-378B','Magellan Aerospace Bournemouth','GAMMA FITTINGS ','M426780 / 80100','NSA840020-250','','L',226,'RP394902','','32089','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dimension\r\nG,J,K OD\r\n','The Following route cause analyzed for the parts rejected,\r\n1. Ovality in RM.\r\n2. Total Length Minus in RM.\r\n3. Improper Butting in Jaws.\r\n4. Jaws Boring is not good( Flatness is not achieved.\r\n5. RM unclear on OD and ID.\r\n6. Ovality More than 0.05mm in billet stage.\r\n7. Chips clocking at the Jaws , In Part butting faces.\r\n8. Roughing and Finishing inserts wear out.','The Following CA/PA taken to avoid the rejections,\r\n1.Sizes and Tolerance for Roughing stage.(Sample parts made to check the parts visually also for reference)\r\n2. Compulsorily use 6-Jaw chuck for  all the Gamma for both roughing and Finishing operations.\r\n3.Plan for Parts to be inspect for Face out and Ovelity before loading for finishing operations.\r\n4.Methods of tightening the part on to the Mandril in operation-02.\r\n5.create the rough surface on OD in roughing operation to strengthening the clamping.\r\n\r\n','The Following CA/PA taken to avoid the rejections,\r\n1.Sizes and Tolerance for Roughing stage.(Sample parts made to check the parts visually also for reference)\r\n2. Compulsorily use 6-Jaw chuck for  all the Gamma for both roughing and Finishing operations.\r\n3.Plan for Parts to be inspect for Face out and Ovelity before loading for finishing operations.\r\n4.Methods of tightening the part on to the Mandril in operation-02.\r\n5.create the rough surface on OD in roughing operation to strengthening the clamping.\r\n','Very next parts found okay','','2014-12-08','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','3','no','Misc','Dinakar(K)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7995,'18-378B','Magellan Aerospace Bournemouth','GAMMA FITTINGS ','M465540 85428','NSA840020-250','','L',227,'RP401480_Amend No.-1','','35387','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dimension\r\nG,J,K OD\r\n','The Following route cause analyzed for the parts rejected, 1. Ovality in RM. 2. Total Length Minus\r\nin RM. 3. Improper Butting in Jaws. 4. Jaws Boring is not good( Flatness is not achieved. 5. RM\r\nunclear on OD and ID. 6. Ovality More than 0.05mm in billet stage. 7. Chips clocking at the Jaws ,\r\nIn Part butting faces. 8. Roughing and Finishing inserts wear out. ','The Following CA/PA taken to avoid the rejections, 1.Sizes and Tolerance for Roughing stage.(Sample\r\nparts made to check the parts visually also for reference) 2. Compulsorily use 6-Jaw chuck for all\r\nthe Gamma for both roughing and Finishing operations. 3.Plan for Parts to be inspect for Face out\r\nand Ovelity before loading for finishing operations. 4.Methods of tightening the part on to the\r\nMandril in operation-02. 5.create the rough surface on OD in roughing operation to strengthening\r\nthe clamping. ','The Following CA/PA taken to avoid the rejections, 1.Sizes and Tolerance for Roughing stage.(Sample\r\nparts made to check the parts visually also for reference) 2. Compulsorily use 6-Jaw chuck for all\r\nthe Gamma for both roughing and Finishing operations. 3.Plan for Parts to be inspect for Face out\r\nand Ovelity before loading for finishing operations. 4.Methods of tightening the part on to the\r\nMandril in operation-02. 5.create the rough surface on OD in roughing operation to strengthening\r\nthe clamping. ','Very next parts found okay','','2014-12-08','Dinakar(K)','Vishvanath K,Girish L N,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','3','no','QT100S-5','Dinakar(K)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7996,'18-378B','Magellan Aerospace Bournemouth','GAMMA FITTINGS ','M489450 87744','NSA840020-250','','L',35,'RP401480','','33557','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dimension\r\nG,J,K OD\r\n','The Following route cause analyzed for the parts rejected, 1. Ovality in RM. 2. Total Length Minus\r\nin RM. 3. Improper Butting in Jaws. 4. Jaws Boring is not good( Flatness is not achieved. 5. RM\r\nunclear on OD and ID. 6. Ovality More than 0.05mm in billet stage. 7. Chips clocking at the Jaws ,\r\nIn 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. ','Very next parts found okay','','2014-12-08','Dinakar(K)','Kalakappa T H,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','3','no','QT100S-4','Dinakar(K)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7997,'18-378B','Magellan Aerospace Bournemouth','GAMMA FITTINGS ','0989','NSA840020-250','','L',42,'RP401480_Amend No.-1','','34189','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dimension\r\nG,J,K OD\r\n','The Following route cause analyzed for the parts rejected, 1. Ovality in RM. 2. Total Length Minus\r\nin RM. 3. Improper Butting in Jaws. 4. Jaws Boring is not good( Flatness is not achieved. 5. RM\r\nunclear on OD and ID. 6. Ovality More than 0.05mm in billet stage. 7. Chips clocking at the Jaws ,\r\nIn Part butting faces. 8. Roughing and Finishing inserts wear out. ','The Following CA/PA taken to avoid the rejections, 1.Sizes and Tolerance for Roughing stage.(Sample\r\nparts made to check the parts visually also for reference) 2. Compulsorily use 6-Jaw chuck for all\r\nthe Gamma for both roughing and Finishing operations. 3.Plan for Parts to be inspect for Face out\r\nand Ovelity before loading for finishing operations. 4.Methods of tightening the part on to the\r\nMandril in operation-02. 5.create the rough surface on OD in roughing operation to strengthening\r\nthe clamping. ','The Following CA/PA taken to avoid the rejections, 1.Sizes and Tolerance for Roughing stage.(Sample\r\nparts made to check the parts visually also for reference) 2. Compulsorily use 6-Jaw chuck for all\r\nthe Gamma for both roughing and Finishing operations. 3.Plan for Parts to be inspect for Face out\r\nand Ovelity before loading for finishing operations. 4.Methods of tightening the part on to the\r\nMandril in operation-02. 5.create the rough surface on OD in roughing operation to strengthening\r\nthe clamping. ','Very next parts found okay','','2014-12-08','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','3','no','Misc','Dinakar(K)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7998,'18-378B','Magellan Aerospace Bournemouth','GAMMA FITTINGS ','2150','NSA840020-250','','L',76,'RP394902','','32090','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dimension\r\nG,J,K OD\r\nrework.','The Following route cause analyzed for the parts rejected, 1. Ovality in RM. 2. Total Length Minus\r\nin RM. 3. Improper Butting in Jaws. 4. Jaws Boring is not good( Flatness is not achieved. 5. RM\r\nunclear on OD and ID. 6. Ovality More than 0.05mm in billet stage. 7. Chips clocking at the Jaws ,\r\nIn 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. ','Very next parts found okay','','2014-12-08','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','3','no','Misc','Dinakar(K)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7999,'18-090A','Magellan Aerospace Bournemouth','BUSH','B4599A','D278 50164 200','S80 FHT','A',156,'RP400843','','36919','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','13.40/13.60 length undersize by -0.2mm(13.18to13.20).','This was happened in 1st set up due to wrong work offset took by the operator. 							\r\n','Operator trained infornt of the machine about work offset. 							\r\n','Dimension will be introduced in 1st set up which effects to 2nd set up ( overall thickness ). 							\r\n','Process sheet to be updated.Next parts are okay','','2014-12-08','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','03','no','Misc','Narasimhamurthy(K.G.)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8000,'18-377B','Magellan Aerospace Bournemouth','GAMMA FITTINGS ','M435940 81523','NSA840020-200','','L',206,'RP397605','','29754','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','K,G,J& H\r\ndimension all\r\nare undersize\r\nin 0.010 to\r\n0.030.','The Following route cause analyzed for the parts rejected, 1. Ovality in RM. 2. Total Length Minus\r\nin RM. 3. Improper Butting in Jaws. 4. Jaws Boring is not good( Flatness is not achieved. 5. RM\r\nunclear on OD and ID. 6. Ovality More than 0.05mm in billet stage. 7. Chips clocking at the Jaws ,\r\nIn 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. ','Very next parts found okay','','2014-12-08','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','1','no','Misc','Dinakar(K)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8001,'18-377B','Magellan Aerospace Bournemouth','GAMMA FITTINGS ','M428200 80333','NSA840020-200','','L',143,'RP396194','','31092','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','K,G,J& H\r\ndimension all\r\nare undersize\r\nin 0.010 to\r\n0.030.','The Following route cause analyzed for the parts rejected, 1. Ovality in RM. 2. Total Length Minus\r\nin RM. 3. Improper Butting in Jaws. 4. Jaws Boring is not good( Flatness is not achieved. 5. RM\r\nunclear on OD and ID. 6. Ovality More than 0.05mm in billet stage. 7. Chips clocking at the Jaws ,\r\nIn Part butting faces. 8. Roughing and Finishing inserts wear out. ','The Following CA/PA taken to avoid the rejections, 1.Sizes and Tolerance for Roughing stage.(Sample\r\nparts made to check the parts visually also for reference) 2. Compulsorily use 6-Jaw chuck for all\r\nthe Gamma for both roughing and Finishing operations. 3.Plan for Parts to be inspect for Face out\r\nand Ovelity before loading for finishing operations. 4.Methods of tightening the part on to the\r\nMandril in operation-02. 5.create the rough surface on OD in roughing operation to strengthening\r\nthe clamping. ','The Following CA/PA taken to avoid the rejections, 1.Sizes and Tolerance for Roughing stage.(Sample\r\nparts made to check the parts visually also for reference) 2. Compulsorily use 6-Jaw chuck for all\r\nthe Gamma for both roughing and Finishing operations. 3.Plan for Parts to be inspect for Face out\r\nand Ovelity before loading for finishing operations. 4.Methods of tightening the part on to the\r\nMandril in operation-02. 5.create the rough surface on OD in roughing operation to strengthening\r\nthe clamping. ','Very next parts found okay','','2014-12-08','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','1','no','Misc','Dinakar(K)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8002,'18-104A','Magellan Aerospace Bournemouth','BODY TURNBUCKLE','239338','D575 40490 200','S80 FHT','E',1,'RP400840','','38880','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','OD Dent mark.','Dent on the parts while holding in the vise. 							\r\n','Advised to use Aluminum Jaws for vise. 							\r\n','Advised to use Aluminum Jaws for vise. 							\r\n','Next parts found okay							','','2014-12-08','Narasimhamurthy(K.G.)','Ravi R,Rajesh B D,Mohan Kumar C.M.,Manohara M,KRISHNAMURTHY N,GUNDEGOWDA H.G.,Devaraj K.C.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','FI','no','DX 200-3','Narasimha Murthy(R)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8003,'18-377B','Magellan Aerospace Bournemouth','GAMMA FITTINGS ','M510590','NSA840020-200','','L',226,'RP397973','','30511','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','K,G,J& H\r\ndimension all\r\nare undersize\r\nin 0.010 to\r\n0.030.','The Following route cause analyzed for the parts rejected, 1. Ovality in RM. 2. Total Length Minus\r\nin RM. 3. Improper Butting in Jaws. 4. Jaws Boring is not good( Flatness is not achieved. 5. RM\r\nunclear on OD and ID. 6. Ovality More than 0.05mm in billet stage. 7. Chips clocking at the Jaws ,\r\nIn Part butting faces. 8. Roughing and Finishing inserts wear out. ','The Following CA/PA taken to avoid the rejections, 1.Sizes and Tolerance for Roughing stage.(Sample\r\nparts made to check the parts visually also for reference) 2. Compulsorily use 6-Jaw chuck for all\r\nthe Gamma for both roughing and Finishing operations. 3.Plan for Parts to be inspect for Face out\r\nand Ovelity before loading for finishing operations. 4.Methods of tightening the part on to the\r\nMandril in operation-02. 5.create the rough surface on OD in roughing operation to strengthening\r\nthe clamping. ','The Following CA/PA taken to avoid the rejections, 1.Sizes and Tolerance for Roughing stage.(Sample\r\nparts made to check the parts visually also for reference) 2. Compulsorily use 6-Jaw chuck for all\r\nthe Gamma for both roughing and Finishing operations. 3.Plan for Parts to be inspect for Face out\r\nand Ovelity before loading for finishing operations. 4.Methods of tightening the part on to the\r\nMandril in operation-02. 5.create the rough surface on OD in roughing operation to strengthening\r\nthe clamping. ','Very next parts found okay','','2014-12-08','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','1','no','Misc','Dinakar(K)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8004,'18-378B','Magellan Aerospace Bournemouth','GAMMA FITTINGS ','2150','NSA840020-250','','L',1,'RP394902','','32090','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','G J K DIMENTION OVALITY','The Following route cause analyzed for the parts rejected, 1. Ovality in RM. 2. Total Length Minus\r\nin RM. 3. Improper Butting in Jaws. 4. Jaws Boring is not good( Flatness is not achieved. 5. RM\r\nunclear on OD and ID. 6. Ovality More than 0.05mm in billet stage. 7. Chips clocking at the Jaws ,\r\nIn 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. ','Very next parts found okay','','2014-12-09','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','3','no','Misc','Dinakar(K)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8005,'18-413B','Magellan Aerospace Bournemouth','ACTUATOR HOUSING','6957','D278 50162 200','','A',1,'RP401021_Amnd No. 1','','39245','','0000-00-00',NULL,'yes','yes','yes','','','','','','','6mm thick ness [-] side 0.03 5mm groving inserts chip break inserts no stock so part face out','Due to butting face not cleaned properly .So part thickness under size. 							\r\n','Before load the part of the butting face cleaned by air per sure then load the part. 							\r\n','Before load the part of the butting face cleaned by air per sure then load the part. 							\r\n','CAPA not sufficient.But next parts found good','','2014-12-09','NIRANJAN(N )','        SHIVAKUMAR ','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8006,'18-368A','Magellan Aerospace Bournemouth','CATCHER ACTUATOR SPI ','0719701','L575 52396 200','','C00',1,'RP400947','','39482','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Program fault rib dig mark observed. ','While doing continual improvement to reduce cycle time reduction, While posting the program in CAM, clearance plane is selected below the part top.\r\nBecause of pocket machining after final depth completes tool approaches to next pocket below the part top, caused dig mark on part. ','The following CA taken to avoid this type of error in future,\r\n1. Mandatory program will generate above the clearance plane.\r\n2. All the programers are understanding the procedure and follow the same in future for all the programs.','The following CA/PA taken to avoid this type of error in future,\r\n1. Mandatory program will generate above the clearance plane.\r\n2. All the programers are understanding the procedure and follow the same in future for all the programs.','Next parts found okay','','2014-12-09','Ramesh(Poojary)','D.K.Pavan (Kumar)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','1','no','Misc','Lohith(K)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8007,'18-373B','Magellan Aerospace Bournemouth','GAMMA FITTINGS ','8185','NSA840020-050','','L',6,'RP401477','','33829','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','G AND J DIMENTION UNDER SIZE','G and J rework doing time o.d under size.','before doing rework check the dimension of every part and give sufficient amount of pressure for polishing to achieve the drawing dimension.','instructions given to operator to check the  dimension of every part before  polishing .','Next batches found good\r\n','','2014-12-09','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','3','no','Misc','Dinakar(K)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8008,'18-374B','Magellan Aerospace Bournemouth','GAMMA FITTINGS ','5580','NSA840020-075','','L',4,'RP401477','','33825','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','G AND J DIMENTION UNDER SIZE.','The Following route cause analyzed for the parts rejected, 1. Ovality in RM. 2. Total Length Minus\r\nin RM. 3. Improper Butting in Jaws. 4. Jaws Boring is not good( Flatness is not achieved. 5. RM\r\nunclear on OD and ID. 6. Ovality More than 0.05mm in billet stage. 7. Chips clocking at the Jaws ,\r\nIn 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. ','Very next parts found okay','','2014-12-09','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','3','no','Misc','Dinakar(K)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8009,'18-379B','Magellan Aerospace Bournemouth','GAMMA FITTINGS ','6586','NSA840020-300','','L',29,'RP401480_Amend No.-1','','38323','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','K,J,G,H & N\r\nDimensions all\r\nare undersize\r\nin 0.01 to\r\n0.06.','The Following route cause analyzed for the parts rejected, 1. Ovality in RM. 2. Total Length Minus\r\nin RM. 3. Improper Butting in Jaws. 4. Jaws Boring is not good( Flatness is not achieved. 5. RM\r\nunclear on OD and ID. 6. Ovality More than 0.05mm in billet stage. 7. Chips clocking at the Jaws ,\r\nIn Part butting faces. 8. Roughing and Finishing inserts wear out. ','The Following CA/PA taken to avoid the rejections, 1.Sizes and Tolerance for Roughing stage.(Sample\r\nparts made to check the parts visually also for reference) 2. Compulsorily use 6-Jaw chuck for all\r\nthe Gamma for both roughing and Finishing operations. 3.Plan for Parts to be inspect for Face out\r\nand Ovelity before loading for finishing operations. 4.Methods of tightening the part on to the\r\nMandril in operation-02. 5.create the rough surface on OD in roughing operation to strengthening\r\nthe clamping. ','The Following CA/PA taken to avoid the rejections, 1.Sizes and Tolerance for Roughing stage.(Sample\r\nparts made to check the parts visually also for reference) 2. Compulsorily use 6-Jaw chuck for all\r\nthe Gamma for both roughing and Finishing operations. 3.Plan for Parts to be inspect for Face out\r\nand Ovelity before loading for finishing operations. 4.Methods of tightening the part on to the\r\nMandril in operation-02. 5.create the rough surface on OD in roughing operation to strengthening\r\nthe clamping. ','Very next parts found okay','','2014-12-09','Dinakar(K)','Kalakappa T H,Chandre  Gowda,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','3','no','QT100S-4','Dinakar(K)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8010,'35-193','Saab AB','INTERCOSTAL CAM HOUSING','569849','423Z1190-1-01','','---',1,'NOV 2014 ','','37732','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dia 27.00 +/- 12 micron, but measured 27.02 ,8micron out of tolorance. ','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','','2014-12-09','Rangaswamy()','Rangaswamy()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','05','no','Misc','Rangaswamy()',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8011,'18-280A','Magellan Aerospace(Chalfont) Limited','DOOR OUTER TYPE 15','508103','L572 53722 200','ABS5032A055','B00',1,'P/074117','','39333','','0000-00-00',NULL,'yes','','yes','','yes','','','','','vacum m/c problem running time part left so part dig....','Part running time vacum pump problemed, vacum presser autometicly down so part lefted. tool dig in outer profile.','Next every 3month in maintenens, check vacum presser & insert vacum presser switch in every collaction.','Next every 3month in maintenens repot, check vacum presser & insert vacum presser switch in every collaction.','Next batches found good\r\n','','2014-12-09','Rangaswamy()','        Umesh B','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8012,'18-381B','Magellan Aerospace Bournemouth','GAMMA FITTINGS ','4729','NSA840020-400','','L',1,'RP401481_Amend No.-1','','37198','','0000-00-00',NULL,'yes','yes','yes','','','','','','','setting time K Dia (-0.06 -side)','The Following route cause analyzed for the parts rejected, 1. Ovality in RM. 2. Total Length\r\nMinus in RM. 3. Improper Butting in Jaws. 4. Jaws Boring is not good( Flatness is not achieved. 5.\r\nRM unclear on OD and ID. 6. Ovality More than 0.05mm in billet stage. 7. Chips clocking at the Jaws\r\n, In Part butting faces. 8. Roughing and Finishing inserts wear out.  \r\n','The Following CA/PA taken to avoid the rejections, 1.Sizes and Tolerance for Roughing\r\nstage.(Sample parts made to check the parts visually also for reference) 2. Compulsorily use 6-Jaw\r\nchuck for all the Gamma for both roughing and Finishing operations. 3.Plan for Parts to be inspect\r\nfor 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\r\nstrengthening the clamping. ','The Following CA/PA taken to avoid the rejections, 1.Sizes and Tolerance for Roughing\r\nstage.(Sample parts made to check the parts visually also for reference) 2. Compulsorily use 6-Jaw\r\nchuck for all the Gamma for both roughing and Finishing operations. 3.Plan for Parts to be inspect\r\nfor 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\r\nstrengthening the clamping.  \r\n','Next batches found good\r\n','','2014-12-09','Dinakar(K)','        Krishnanaik J N','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8013,'18-326A','Magellan Aerospace Bournemouth','ATTACHMENT ANGLE','4718401','L572 53314 200','ABM3 1029','A00',3,'RP400946','','38357','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','wrong Part marking in WO No.','Due to misinterpretation one number from the work order interchanged','Warning NC, part has been accepted but to warn the part marking operator this NC has been raised.','First off will be done for every part marking of the part and signed by Quality Inspector. Planning to train one more part marking operator so that load will be less and part marking issues can be solved','Parts accepted','','2014-12-10','Anjinamurthy(H)','Santhosh(RH)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','With Treatment','','05','no','Misc','Narasimha Murthy(R)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8014,'35-228A','Saab AB','HINGE BRACKET 2 ','7600601','D576 50005 205','','D00',28,'1600093863 Rev-2','','38670','','0000-00-00',NULL,'no','yes','no','yes','no','yes','no','no','no','Ndt Fail.','Due to polishing or tool rubbing marks NDT failed in treatment house','Polishing should be avoided, speed and depth of cutting and tool marks should be avoided. Instructed CAD and Production to modify the program and run with low RPM','Polishing should be avoided, speed and depth of cutting and tool marks should be avoided. Instructed CAD and Production to modify the program and run with low RPM','Part reworked and NDT tests passed','','2014-12-10','Krishna(Chowdary.G.P.)','Rangaswamy()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','15496','post Dn','yes','Misc','Manjunath(G)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8015,'18-392B','Magellan Aerospace Bournemouth','END COVER','94466','D278 50167 200','','D',1,'RP401023_Amend No.-1','','38890','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Bore over size 0.007mm','while offset taken time, he give a cut for finished bore.\r\nso part will over sized. ','give the instruction for operator and run the part.','training give the operator. before setting check the\r\nprocess sheet and then do the setting.','Next batches found good\r\n','','2014-12-10','Dinakar(K)','Shivanand D.B.,SHIVAKUMAR ,Rajesh T,Raghavendra Rao R,KRISHNAMURTHY N,Devaraj K.C.,Ashith B,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','ST20Y1','Narasimha Murthy(R)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8016,'34-032C','Magellan Aerospace Winnipeg','BASE FITTING, F/D HINGE L','54331-2','400-12780-1-905','','EM104302 Iss A, EM105092 Iss F, EM104765 Iss G, EM106399 Iss B, EM106400 Iss B, EM106401 Iss A, EM106404 Iss A, EM106522 Iss A, EM106602 Iss A',1,'B91379 Rev.026','','39353','','0000-00-00',NULL,'yes','yes','yes','','','','','','no','Dia 5.08 measures 5.3mm( 03 holes)','Due to drill blunt this deviation coming.\r\nImmediately new drill placed and continued production.','New Drill placed and informed to operator to monitor the drill blunt at regular interval.','New Drill placed and informed to operator to monitor the drill blunt at regular interval.\r\nDrill size reduced and hole mill introduced to avoid hole diameter oversize.\r\n\r\n','Next parts found okay','','2014-12-10','Lohith(K)','        Shivaraj K S','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8017,'18-102A','Magellan Aerospace Bournemouth','BARREL-STRUT','247348','D572 50463 200','S98 FHT','F',2,'RP400839','','38961','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dia 1.55mm drill broken, dig mark observed on hole.','This problem is due to Un-availability of Carbide (     ) drill when plan to start production.\r\nDue to urgency instead of Carbide drill(      ) HSS drill (    )used with proving the correct parameters.\r\nChanging of tool is approved by CAD/CAM.','After finding deviations in Two parts, Parameter adjusted and monitored the tool lip and continued production.\r\n203 nos of Parts continuously machined with 02 nos drills(HSS-     )\r\nInformed to buy Carbide drill(      ) for next batch production and also informed to tool supplier to maintain the stock at any given point of time.','1.Dedicated tools kept for this CRN and also informed to Tool manager to monitor the tool stock. \r\n2.Planned to prove multiple make tools for tools flexibility.\r\n3.Training to be impart to all the operators to calculate the Feed/Speed and monitoring the tool life.','Next part found okay','','2014-12-10','Anjinamurthy(H)','Ravi R,Mohan Kumar C.M.,Manohara M,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','7','no','BMV 45-2','Anjinamurthy(H)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8018,'18-293C','Magellan Aerospace Bournemouth','BAFFLE ADAPTOR ','5719','L281 50313 200','','D00',1,'RP400946','','38267','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Running time part rotates so on 3mm thickness dig mark observed.','Because of more material removal, cutter load on part while removing material and also clamping strength is less for this operation.\r\nDue to this part moves from jaws around 10mm. This causes dig mark observed on OD.\r\n\r\n\r\n\r\n \r\n','The following actions taken to prevent this deviations,\r\n1.Rough surface on OD created to strengthened the clamping.\r\n2.Chuck pressure increased and updated in MPS.\r\n3.Part Butting to be ensuring for every part.','The following actions taken to prevent this deviations,\r\n1.Rough surface on OD created to strengthened the clamping.\r\n2.Chuck pressure increased and updated in MPS.\r\n3.Part Butting to be ensuring for every part.','Next batch found okay','','2014-12-11','Dinakar(K)','        Devaraj K.C.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8019,'35-230A','Saab AB','HINGE BRACKET 3 ','688931A5','D576 50006 205','','D00',1,'1600099854','','39496','','0000-00-00',NULL,'yes','yes','yes','','','','','','no','Dim 94 *-0.05 measuerd 93.75 mm when changed the cutting tool insert','While doing operationn-04, Dia 80 face mill insert changed and offset taken and runned the program, But insert seating not noticed by operator and 0.1mm varies in z offset for 02 inserts out of 06 inserts.\r\nThis causes total Thickness measures 0.2mm minus side.','As per drawing 94 +/- 0.25mm, due to process control and butting face for next setup we mentioned 94 +/- 0.05mm in MPS.\r\n\r\nAfter inspection the part Tool insert seating checked with dial and adjusted and then continued production.\r\nNext part found 94.02/94.05mm.\r\n \r\nThis part is accepted After checking all the parameters in CMM.\r\n','Informed to operator to check the insert seating while changing the insert in face mills.\r\nThis information passed to all the operators who is using 80 face mill or Multiple insert cutters.\r\n','Part accepted','','2014-12-11','Girish(Prasad P)','        Girish Prasad P','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8020,'35-228A','Saab AB','HINGE BRACKET 2 ','688931A5','D576 50005 205','','D00',1,'PA 1217 2014-2015','','39407','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Dimension 23.09 +/-0.03 is reached to out of tolerance to 23.22/.27','Due to urgency slotting operation planned in HMC 440HP machine to meet the customer requirement.\r\nWhile proving the parts in HMC 440HP Manual error happened while editing the program.\r\nWhile doing operation-03 Slotting operation, Critical wall machining operator wrong TRANS value entered for dia 22 cutter.\r\nThis manual  error causes deviation in 23.09 dimension.','Program corrected and TRANS value entered in program.\r\nProgram proved and backup given to CAD/CAM and if part loaded to HMC again same program will use.\r\nMessage checked in all the brackets program and TRANS values and all are found OK.','Program corrected and TRANS value entered in program.\r\nProgram proved and backup given to CAD/CAM and if part loaded to HMC again same program will use.\r\nMessage checked in all the brackets program and TRANS values and all are found OK.','Next batch found okay','','2014-12-12','Rangaswamy()','Rangaswamy()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','DN','no','Misc','Manjunath(G)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8021,'18-106A','Magellan Aerospace Bournemouth','EYE END INBOARD','245160','D575 41542 200','S98 FHT','D',1,'RP400841','','39249','','0000-00-00',NULL,'yes','yes','yes','','','','','','no','Deburing time ID digmarke so part 0.008 micron bore over size','While deburring part got dig marks','Instructed strictly to fitting department not to happen these types of simple mistakes that lead to rejection of the part.','Instructed strictly to fitting department not to happen these types of simple mistakes that lead to rejection of the part.','Next batches found okay','','2014-12-12','Anjinamurthy(H)','        Ravi R','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8022,'18-209B','Magellan Aerospace(Chalfont) Limited','BODY','4842','D321 40204 202','','D, ECN NR29999ST1KM15, NR29999ST2KF65, WQN DFB09775',1,'P/074113','','39470','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Both side center drill program running.','Offset mistaken by operator. 							\r\n','Instructions given to operator to take the offset and run the production. ','Instructions given to operator to take the offset and run the production. 							\r\n','Next batch found okay','','2014-12-12','Narasimhamurthy(K.G.)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','01','no','Misc','Seetharamu(D)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8023,'18-372B','Magellan Aerospace Bournemouth','GAMMA FITTINGS ','M368680','NSA840007-250 ','','N',4,'RP394895','','32255','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','thread NOGO answered.','Due to wear out of insert these error was occurred.','Insert was changed and instructed to operator for changing insert as mentioned in board for tool life.','Instructed to operator for follow the instructions for as mentioned in board.','Very next parts found okay','','2014-12-12','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','3','no','Misc','Dinakar(K)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8024,'18-086B','Magellan Aerospace Wrexham','PLATE SEALING','419747','D572 52913 200','ABM3 1029','B',1,'RP125884','','39047','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Outer profile -side (daring  dimension 119 + -0.3  mesa rad dimension 118.3  )','Due to put the center bolts not properly so part outer profile dig mark.','Put the center bolts properly and bolt tightness also checked then run the production.','Instructed operator to every part put the center bolts properly and bolt tightness also checked\r\nthen run the production.','Next batch found okay','','2014-12-14','Anjinamurthy(H)','Anjinamurthy(H)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','00','no','Misc','Anjinamurthy(H)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8025,'18-376B','Magellan Aerospace Bournemouth','GAMMA FITTINGS ','M420400 78745','NSA840020-150','','L',132,'RP401478_Amend No.-1','','34789','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','G J K DIMENTION OVALITY.','The Following route cause analyzed for the parts rejected, 1. Ovality in RM. 2. Total Length Minus in RM. 3. Improper Butting in Jaws. 4. Jaws Boring is not good( Flatness is not achieved. 5. RM unclear on OD and ID. 6. Ovality More than 0.05mm in billet stage. 7. Chips clocking at the Jaws , In Part butting faces. 8. Roughing and Finishing inserts wear out. \r\n','The Following CA/PA taken to avoid the rejections, 1.Sizes and Tolerance for Roughing stage.(Sample parts made to check the parts visually also for reference) 2. Compulsorily use 6-Jaw chuck for all the Gamma for both roughing and Finishing operations. 3.Plan for Parts to be inspect for Face out and Ovelity before loading for finishing operations. 4.Methods of tightening the part on to the Mandril in operation-02. 5.create the rough surface on OD in roughing operation to strengthening the clamping. \r\n','Compulsorily use 6-Jaw chuck for all the Gamma for both roughing and Finishing operations. 3.Plan for Parts to be inspect for Face out and Ovelity before loading for finishing operations. 4.Methods of tightening the part on to the Mandril in operation-02. 5.create the rough surface on OD in roughing operation to strengthening the clamping. \r\n','Next batches found good\r\n','','2014-12-15','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','01','no','Misc','Krishna(Chowdary.G.P.)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8026,'18-392B','Magellan Aerospace Bournemouth','END COVER','94466','D278 50167 200','','D',1,'RP401023_Amend No.-1','','38890','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Bore over size 0.007mm','while offset taken time, he give a cut for finished bore. so part will over sized. ','give the instruction for operator and run the part.','training give the operator. before setting check the process sheet and then do the setting.','Instructions given to operator to take the offset and run the production. ','','2014-12-15','Dinakar(K)','Shivanand D.B.,SHIVAKUMAR ,Rajesh T,Raghavendra Rao R,KRISHNAMURTHY N,Devaraj K.C.,Ashith B,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','ST20Y1','Narasimha Murthy(R)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8027,'18-376B','Magellan Aerospace Bournemouth','GAMMA FITTINGS ','M420400 78745','NSA840020-150','','L',132,'RP401478_Amend No.-1','','34789','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','G K and J dimension ovality','Dummy NC original NC no: 8025','Dummy NC original NC no: 8025','Dummy NC original NC no: 8025','Dummy NC original NC no: 8025					','','2014-12-15','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','01','no','Misc','Krishna(Chowdary.G.P.)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8028,'28-006','Ellanef Manufacturing Corporation','SHOULDER BOLT','G19876K01','162A3109 2','15-5PH Bar,Per AMS56','NA',2,'117105_R0_C1','','37239','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1)Thread Gauge not answer.','Thread gauge was not butting. ','Next time thread gauge kept to be free. \r\n','Any threaded parts after machining checked in machine before removing.','Parts yet to be taken for Rework.','','2014-12-15','Dinakar(K)','Theerthappa K.N.,Shivaraj K S,Rajesh B D,KRISHNAMURTHY N,Hari Prasad,GUNDEGOWDA H.G.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Manufacture Only','0','FI','yes','DX 200-3','Sudhagar(V)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8029,'18-214A','Magellan Aerospace(Chalfont) Limited','SPECIAL WASHER ','245160','D321 40210 202','','E01, ECN NR29999ST1JB79',1,'P/074114','','38331','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Broching problem 2mm width under size. ','As the broaching operation is doing manually, this problem is getting repeated from long time ','New fixture was manufactured and part found okay ','New fixture was manufactured and part found oka','Next batches found good\r\n','','2014-12-15','Anjinamurthy(H)','Diwakar R.B.,Dinakar K,Anjinamurthy H,','','0000-00-00','Basavaraju sb','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','FI','no','BMV 60-2','Narasimha Murthy(R)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8030,'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','','','','','','','O.D under size by (71.951 to 71.966)measure 71.942 so part was rejected. 							\r\n','1)running time part rotating. 2) improper tightening. 3) if over tight ovality will occure.4)closed tollerance part (15 micron) 							\r\n							\r\n','Given the guidence about tightning. 							\r\n','same 35-104 clamping method used for this CRN .							\r\n','Next parts are okay','','2014-12-15','Ravi(M)','        Dinakar K','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8031,'18-090A','Magellan Aerospace Bournemouth','BUSH','B4599A','D278 50164 200','S80 FHT','A',4,'RP400843','','36919','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Thikness under size 0.1mm Total length under size 0.15mm.','This was happened in 1st set up due to wrong work offset took by the operator.  \r\n\r\n\r\n \r\n','Operator trained infornt of the machine about work offset.','Dimension will be introduced in 1st set up which effects to 2nd set up ( overall thickness ).','Dimension should be updated in Process sheet.Very next parts found satisfactory','','2014-12-16','Narasimhamurthy(K.G.)','NIRANJAN(N  )','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','FI','no','Misc','Narasimha Murthy(R)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8032,'42-003','RAFAEL','Clamp-1','746349','BA1E2002B','','38-576104_Rev-E, TILDOCS#172373_Rev-13,111.21_Rev 6,  PR603-2-3_Rev-16, ECN 57176 2014/08/05',1,'347592024','','39397','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','1)1-no Thread gauge NOGO answered.\r\n','While proving a FAI part this deviation coming.\r\nWhen proving the Thread mill, by trialing the tool this deviation accord.','Thread mill proved and 09nos production completed and checked all the parts with gauge and found ok.','While proving the new tool this errors will happen. and approval given to supervisor to do trial and errors for new technologies.\r\n\r\nNow understand the thread mill program and terminology of using the tools.','Next parts found okay','','2014-12-18','Rangaswamy()','Prashanth Kumar M,Girish Prasad P,Basavaraja S. Jr.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','3','no','MakinoF5-4','Rangaswamy()','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8033,'30-011A','Gardner Aerospace-Derby Limited','SPAR FWD - LH','430416-B','L575 51827 200','ABM3-1029 T7651','A00, ECN:PG60049U01LC52',1,'LPR0000612','','39535','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','RM size variation.\r\nThe required RM size is 13mm in outer, but measures 10mm.','After machining found that RM was undersized\r\n','Instructed to RM cutter to have the process sheet and exact required dimension and then cut the RM\r\n','Instructed to RM cutter to have the process sheet and exact required dimension and then cut the RM\r\n','RM will be checked 100% and stamps will be done after cutting ','','2014-12-18','Nagaraja (G)','Devaraja (M S)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','01','no','Misc','Krishna(Chowdary.G.P.)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8034,'42-004','RAFAEL','Clamp-2','D4043','BA1E2003B','','38-576104_Rev-E, PR603-2-3_Rev-16, TILDOCS#172373_Rev-13, 111.21_Rev 6, ECN57176 2014/08/05',1,'347592024','','38946','','0000-00-00',NULL,'yes','no','no','no','no','yes','no','yes','no','Outer profile radius one side not achiveed.','Misinterpretation of program sequence caused Radius problem and part got reject','Instructed to cad department to program according to sequence and checklists have been prepared to correct according to sequence\r\n','Instructed to cad department to program according to sequence and checklists have been prepared to correct according to sequence\r\n','Next part found ok','','2014-12-18','Lohith(K)','Lohith(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','00','no','Misc','Avinash(R.J.)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8035,'18-381B','Magellan Aerospace Bournemouth','GAMMA FITTINGS ','M332020 69275A','NSA840020-400','','L',1,'RP401481_Amend No.-1','','37875','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','0.5 grooving insert break down so part od groove dig mark.','The Following route cause analyzed for the parts rejected, 1. Ovality in RM. 2. Total Length Minus\r\nin RM. 3. Improper Butting in Jaws. 4. Jaws Boring is not good( Flatness is not achieved. 5. RM\r\nunclear on OD and ID. 6. Ovality More than 0.05mm in billet stage. 7. Chips clocking at the Jaws ,\r\nIn Part butting faces. 8. Roughing and Finishing inserts wear out.  \r\n','The Following CA/PA taken to avoid the rejections, 1.Sizes and Tolerance for Roughing stage.(Sample\r\nparts made to check the parts visually also for reference) 2. Compulsorily use 6-Jaw chuck for all\r\nthe Gamma for both roughing and Finishing operations. 3.Plan for Parts to be inspect for Face out\r\nand Ovelity before loading for finishing operations. 4.Methods of tightening the part on to the\r\nMandril in operation-02. 5.create the rough surface on OD in roughing operation to strengthening\r\nthe clamping.  \r\n','The Following CA/PA taken to avoid the rejections, 1.Sizes and Tolerance for Roughing stage.(Sample\r\nparts made to check the parts visually also for reference) 2. Compulsorily use 6-Jaw chuck for all\r\nthe Gamma for both roughing and Finishing operations. 3.Plan for Parts to be inspect for Face out\r\nand Ovelity before loading for finishing operations. 4.Methods of tightening the part on to the\r\nMandril in operation-02. 5.create the rough surface on OD in roughing operation to strengthening\r\nthe clamping.  \r\n','Next batches found good\r\n','','2014-12-19','Dinakar(K)','Krishnanaik J N,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','3','no','QT100S-4','Sandhesh D(S)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8036,'18-381B','Magellan Aerospace Bournemouth','GAMMA FITTINGS ','M510650 89213A','NSA840020-400','','L',8,'RP401481_Amend No.-1','','37203','','0000-00-00',NULL,'no','yes','yes','yes','no','no','no','no','no','R/M problem total lenght undersize.','The Following route cause analyzed for the parts rejected, 1. Ovality in RM. 2. Total Length\r\nMinus in RM. 3. Improper Butting in Jaws. 4. Jaws Boring is not good( Flatness is not achieved. 5.\r\nRM unclear on OD and ID. 6. Ovality More than 0.05mm in billet stage. 7. Chips clocking at the Jaws\r\n, 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.  \r\n','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.  \r\n','Next batches found good\r\n','','2014-12-19','Sandhesh D(S)','Girish S,Girish L N,Dinakar K,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','1','no','QT100S-5','Sandhesh D(S)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8037,'18-211B','Magellan Aerospace(Chalfont) Limited','PLUNGER','238302','D321 40205 200','','H01, ECN NR29998ST1JB80',3,'P/074114','','38420','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','dia 9.65 to 9.75 undersize. (0.006 to 0.008)','Insert was worn out so this problem occurred.  \r\n','Check insert status regularly and know the life of inserts and change inserts according\r\ninstructions.  \r\n','Check insert status regularly and know the life of inserts and change inserts according\r\ninstructions.  \r\n','Next batches found good\r\n','','2014-12-19','Ravi(M)','Ningaraj A N,Nataraja C V,Manjunath  M,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','3','no','QT100S-1','Sandhesh D(S)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8038,'18-317A','Magellan Aerospace(Chalfont) Limited','PIN SIDE ROLLER','A0587U','F579 53066 200','S145','C',20,'P/074118','','37599','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','o.d under size by (-0.006 t0 -0.010).','1) chips rubbing.2)single tool running 3)in data sheet have single tool so single tool running.\r\n \r\n \r\n','additional tool added and run the part','additional tool added in datd sheet and run the the part for next every batch.  ','Next batches found good\r\n','','2014-12-20','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','01','no','Misc','Narasimhamurthy(K.G.)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8039,'18-317A','Magellan Aerospace(Chalfont) Limited','PIN SIDE ROLLER','A0587U','F579 53066 200','S145','C',53,'P/074118','','38503','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','o.d under size by (-0.010 to -0.015) & dent marks in o.d, i.d grove chatting problem.','chips rubbing.2)single tool running 3)in data sheet have single tool so single tool running. \r\n','additional tool added and run the part. ','additional tool added in datd sheet and run the the part for next every batch.','Next batches found good\r\n','','2014-12-20','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','01','no','Misc','Narasimhamurthy(K.G.)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8040,'35-169','Saab AB','ALCD_STRUCT_SUPPORT-FTG_L','569847','423Z1200-12-01','','---',1,'PA-1300 2014','','38470','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dimension 5.08 wall thickness minus.*','While running production this deviation coming due to part not butted properly to pins or Part moving while running the program due to clamping error.','After checking the deviation next part butting checked with feller gauge and also clamps tightness checked and found ok.\r\nChecking all the above and production continued.','One more location done to avoid part moving and also part straightness will achieve after loading the part automatically.\r\nThis new fixture introduced and checked the all the PA points and all are found OK.','Next parts found okay','','2014-12-20','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','07','no','Misc','Rangaswamy()',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8041,'35-169','Saab AB','ALCD_STRUCT_SUPPORT-FTG_L','569848','423Z1200-12-01','','---',1,'PA-1300 2014','','38469','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dimension 157.43 +/- 0.25 measured 157.02 *','While running production this deviation coming due to part not butted properly to pins or Part moving while running the program due to clamping error.','After checking the deviation next part butting checked with feller gauge and also clamps tightness checked and found ok.\r\nChecking all the above and production continued.','One more location done to avoid part moving and also part straightness will achieve after loading the part automatically.\r\nThis new fixture introduced and checked the all the PA points and all are found OK.','Next parts found okay','','2014-12-20','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','Dimension 157.43 +/- 0.25 measured 157.02 .','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','05','no','Misc','Rangaswamy()',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8042,'35-227A','Saab AB','HINGE BRACKET 2','9865601','D576 50005 204','','D00',9,'1600093863 Rev-2','','38669','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','NDT FAIL.','Due to polishing or tool rubbing marks NDT failed in treatment house','Polishing should be avoided, speed and depth of cutting and tool marks should be avoided. Instructed CAD and Production to modify the program and run with low RPM','Polishing should be avoided, speed and depth of cutting and tool marks should be avoided. Instructed CAD and Production to modify the program and run with low RPM','Next batches passed NDT tests','','2014-12-20','Avinash(R.J.)','Manjunath(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','15489','post Dn','yes','Misc','Manjunath(G)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8043,'35-170','Saab AB','ALCD_STRUCT_SUPPORT-FTG_L','569848','423Z1200-11-01','','---',1,'PA-1300 2014','','38471','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Tool dig mark in top face.*','While doing first off part tool overhang not setted as per MPS.\r\nThis manual error caused dig mark on part.','Tool over hang corrected and continued production.\r\n','Informed to operator to check the tool overhang as per datasheet while loading the part and also cross check with machine reference book for tool length.\r\nSupervisor to be monitor the PA for all the machine to avoid such manual errors\r\n','Next parts found okay','','2014-12-20','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Rangaswamy()',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8044,'18-215C','Magellan Aerospace(Chalfont) Limited','ROD END ASSMY - MALE ','245160','D321 53012 200','','F01, ECN NR29998ST1KH40',32,'P/074113','','34570','','0000-00-00',NULL,'yes','no','no','no','yes','no','no','no','yes','Some of the .375\"-24 U.N.F-3 A threads oversize ','Thread features was checked with Thread Pitch Micrometer to ensure the thread effective diameter and might be the chances of hanging burrs that detected in Pitch Micrometer','We will procure thread gauge to solve current problems facing from thread pitch micrometer, From production side we will use die for removing burrs and PO released expecting mid Dec 2014','We will procure thread gauge to solve current problems facing from thread pitch micrometer, From production side we will use die for removing burrs and PO released expecting mid Dec 2014','Next batches found good and die are being used from production side','C31246','2014-12-21','Avinash(R.J.)','Muniyappa(N)','CAR S-000382','2014-11-11','CHALFONT CUSTOMER NC','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','CUST END','no','Misc','Muniyappa(N)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8045,'35-077','Saab AB','BUSH','1112509740','D575 40147 200','DTD-197','B ECN NG29999ST2TT59',27,'PA 1217-Bushes (A320','','39420','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','OD&ID undersize.','It is happened due to insert problem.New insert loaded but operator was not cross checked whether\r\ninsert properly seatted or not.  \r\n','For next piece supervisor loaded the insert properly & cross checked dimension for several components and found within tolerance.  \r\n','Proper training given to the operators regarding the above NC.  \r\n','Next batches found good\r\n','','2014-12-21','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Narasimhamurthy(K.G.)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8046,'30-011A','Gardner Aerospace-Derby Limited','SPAR FWD - LH','430416-B','L575 51827 200','ABM3-1029 T7651','A00, ECN:PG60049U01LC52',1,'LPR0000612','','39534','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Flange thickness 25.0 +0.2 -0.1 measures 23.0mm in rm stage ','While cutting the material as per layout, due to Machine blade was slack & wobbling due to bearing broken cross cutted the material.','Cutting  process stopped and machine manufacturer was visited and verified the machine and informed to change the bearing.','Complete machine servicing are planned and hence forth regular machine maintenance will be planning and maintained.\r\n','Next parts found okay','','2014-12-22','Nagaraja (G)','Devaraja (M S)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','01','no','Misc','Narayanappa(G)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8047,'35-234A','Saab AB','HINGE BRACKET 5 ','425129','D576 50008 209','','D00',1,'PA 1217 2014-2015','','39379','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Dig mark on 100 deg counter sink.','Running time dia 2,5 drill broken so dig mark on part csk dia 4.5.\r\nDue to drill blunt this deviation occurred.','New Drill placed and diameter checked and continued production.\r\nInformed to operator and Supervisor to monitor the drill blunt and change the drill if found any deviation.','Informed to operator and Supervisor to monitor the drill blunt and change the drill if found any deviation.\r\nTool life to be calculate and change the drills after tool life completes.\r\nThis will avoid tool breakages.','Next parts found okay','','2014-12-22','Girish(Prasad P)','        Subramanya L Naik','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','no','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8048,'18-373B','Magellan Aerospace Bournemouth','GAMMA FITTINGS ','8185','NSA840020-050','','L',6,'RP401477','','33829','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','G J K DIMENTION OVALITY. ','The Following route cause analyzed for the parts rejected, 1. Ovality in RM. 2. Total Length Minus\r\nin RM. 3. Improper Butting in Jaws. 4. Jaws Boring is not good( Flatness is not achieved. 5. RM\r\nunclear on OD and ID. 6. Ovality More than 0.05mm in billet stage. 7. Chips clocking at the Jaws ,\r\nIn 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 the\r\n','Compulsorily use 6-Jaw chuck for all the Gamma for both roughing and Finishing operations. 3.Plan\r\nfor Parts to be inspect for Face out and Ovelity before loading for finishing operations. 4.Methods\r\nof tightening the part on to the Mandril in operation-02. 5.create the rough surface on OD in\r\nroughing operation to strengthening the clamping. ','Next part found good','','2014-12-22','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','3','no','Misc','Dinakar(K)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8049,'35-170','Saab AB','ALCD_STRUCT_SUPPORT-FTG_L','569848','423Z1200-11-01','','---',1,'PA-1300 2014','','38471','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','* Part butting problem so ACYL DIM 166.45+/-0.25 MUSED 165.85 to 165.80. ','While running production this deviation coming due to part not butted properly to pins or Part moving while running the program due to clamping error.','After checking the deviation next part butting checked with feller gauge and also clamps tightness checked and found ok.\r\nChecking all the above and production continued.','One more location done to avoid part moving and also part straightness will achieve after loading the part automatically.\r\nThis new fixture introduced and checked the all the PA points and all are found OK.','Next parts found okay','','2014-12-22','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','2014-12-23','* ACYL DIM 166.45+/-0.25 MUSED 165.85 to 165.80.','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','05','no','Misc','Gurukiran S(M)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8050,'28-045','Magellan Aerospace New York  Inc.','LEVER','158524','65-51632-6','','PL_Rev - A + ADCN # 2 ; DL_Rev - N/C',4,'125339-2520_R0_C0','','38214','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1)Hole pitch under size by 0.05 to 0.06MM.','This is first batch production and parts machined as per process done in FAI, but boring operation and step OD not done due to misinterpretation of MPS.  \r\nAfter all the parts machining for next operation not located in fixture.\r\nThen while doing rework hole pitch shifted and not inspected 100% in production.','Process studied and through bore, Step bore and OD are machined in single setup.\r\nProcess proved and Feed back given to CAD/CAM to MPS.','Process studied and through bore, Step bore and OD are machined in single setup.\r\nProcess proved and Feed back given to CAD/CAM to MPS.\r\nTo check the parts 100%, checking jig done and parts will inspect at production.','Next parts found okay','','2014-12-23','Ravi(M)','Shivappa M B,S. Shiva Kumar,Ravi R,Rajesh T,Nataraja C V,Mohan Kumar C.M.,Manohara M,Manjunath  M,Girish HP,Devaraj K.C.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','0','FI','no','DX 200-1','Sudhagar(V)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8051,'28-045','Magellan Aerospace New York  Inc.','LEVER','158524','65-51632-6','','PL_Rev - A + ADCN # 2 ; DL_Rev - N/C',4,'125339-2520_R0_C0','','38217','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1)Hole pitch under size by 0.05 to 0.06MM.','This is first batch production and parts machined as per process done in FAI, but boring operation and step OD not done due to misinterpretation of MPS.  \r\nAfter all the parts machining for next operation not located in fixture.\r\nThen while doing rework hole pitch shifted and not inspected 100% in production.','Process studied and through bore, Step bore and OD are machined in single setup.\r\nProcess proved and Feed back given to CAD/CAM to MPS.','Process studied and through bore, Step bore and OD are machined in single setup.\r\nProcess proved and Feed back given to CAD/CAM to MPS.\r\nTo check the parts 100%, checking jig done and parts will inspect at production.','Next parts found okay','','2014-12-23','Ravi(M)','Ravi R,Rajesh B D,Ningaraj A N,Nataraja C V,Mohan Kumar C.M.,Manohara M,Manjunatha N.R.,Manjunath  M,KRISHNAMURTHY N,GUNDEGOWDA H.G.,Girish V M,Diwakar R.B.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','0','FI','no','QT100S-1','Sudhagar(V)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8052,'18-105A','Magellan Aerospace Bournemouth','FORKEND ASSEMBLY','512111','D572 50462 200','S98 FHT','J01',1,'RP400839','','39692','','0000-00-00',NULL,'yes','yes','yes','','no','','','','no','dummy NC created by ERP, original NC no 08058','dummy NC created by ERP, original NC no 08058','dummy NC created by ERP, original NC no 08058','dummy NC created by ERP, original NC no 08058','dummy NC created by ERP, original NC no 08058','','2014-12-23','Narasimhamurthy(K.G.)','        Rajesh B D','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8053,'18-168A','Magellan Aerospace Bournemouth','PLATE WEAR AFT','1111506671','L575 53156 200','BSB 23','A00',1,'RP400845','','39272','','0000-00-00',NULL,'yes','yes','yes','','','','','','no','1nos reject 10.65 nogo pin entry','Discussion with QAD is going on may the part get accepted','Discussion with QAD is going on may the part get accepted','Discussion with QAD is going on may the part get accepted','Discussion with QAD is going on may the part get accepted','','2014-12-23','Anjinamurthy(H)','        Diwakar R.B.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8054,'35-170','Saab AB','ALCD_STRUCT_SUPPORT-FTG_L','569848','423Z1200-11-01','','---',1,'PA-1300 2014','','38471','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Tool dig mark in top face.*','While doing setting for first off tool overhang not setted as per MPS.\r\nThis error causes dig mark on part.','Tool length corrected as mentioned in MPS and production continued.','Informed to operator to check the MPS and also production reference book for tool over hang while doing first off.\r\nSupervisor will monitor the setting for all the machines and he will guide the operators to avoid manual errors. ','Next parts found okay','','2014-12-24','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Rangaswamy()',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8055,'35-146','Saab AB','CED_HINGE_FTG_FWD','614048A7','425Z0301-6','7050 - T7451 ALUMINU','--A',1,'1600097307','','39024','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Rib thickness measuring over size of 0.8 mm','Due to power trip fluctuations operator didnt ran the final sequence of the part which will finish the RIB thickness','Instructed to Maintenance department to provide continuous power supply and part will be re worked  ','Instructed to Maintenance department to provide continuous power supply and part will be re worked','Under rework stage','','2014-12-24','Rangaswamy()','Rangaswamy()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','','DN','yes','Misc','Manjunath(G)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8056,'18-215C','Magellan Aerospace(Chalfont) Limited','ROD END ASSMY - MALE ','245160','D321 53012 200','','F01, ECN NR29998ST1KH40',1,'P/074113','','38518','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Thread gauge NO GO answering.(24 UNJ )','After threading operation in turning, In operation 07 Key way will complete, After key way thread gauge is not answering due to burr is folding in threads.\r\nBefore Key way operation all the parts is checking with gauge and found ok.  \r\nDue to problem facing in gauge entry after the key way, we planned to rework with OD thread Die and this operation is manually done. This is a first batch with new process and out of 247 nos. 01 no. rejected due to NOGO answering.','Corrective action is not taken now because this operation is done by manually and out of 247nos. 01 got deviation due to Die entry problem.\r\nDue to manually operation this will stabilize by experience and we need to conduct practical training to the operator. ','Preventive action is as same as Corrective Action.','Next parts found okay','','2014-12-24','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','03','no','Misc','Narasimhamurthy(K.G.)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8057,'18-368A','Magellan Aerospace Bournemouth','CATCHER ACTUATOR SPI ','0719701','L575 52396 200','','C00',1,'RP400947','','39324','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Y offset rung so hole pitch 6mm shift.  ','Operator took offset for 6 mm instead of 0.6 mm.','Warning has been given and fined the operator for one day salary and one extra Sunday duty which is commencing from 1st of Jan. \r\n','New fixture has been introduced so that taking offset for every part is avoided and part ran and part found okay ','Next part found okay','','2014-12-24','Lohith(K)','Chiranjeevi(S)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','05','no','Misc','Anjinamurthy(H)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8058,'18-105A','Magellan Aerospace Bournemouth','FORKEND ASSEMBLY','512111','D572 50462 200','S98 FHT','J01',1,'RP400839','','39692','','0000-00-00',NULL,'yes','yes','yes','','no','','','','no','Thread dimensions 41.24mm measures 42.02mm.','After completion of First off part, the dimension achieved 41.3mm. Operator is to maintain the dimension in mean.Then he altered the Z value in tool wear.\r\n','Warning letter has been issued to the operator and necessary training has been given for him. For next few batches one the supervisor will monitor the effectiveness of the operator by standing near the machine before he taking the offsets.','Warning letter has been issued to the operator and necessary training has been given for him. For next few batches one the supervisor will monitor the effectiveness of the operator by standing near the machine before he taking the offsets.','Next parts found okay by the same operator.','','2014-12-24','Narasimhamurthy(K.G.)','        Rajesh B D','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8059,'35-144A','Saab AB','BCD_LATCH_PROBE__FTG_HOUS','556564','424Z6115-4-01','','--C',1,'1600096186','','38878','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','* wrong part loading so dia 6.35mm hole shift. ','As the 2 sides of the part looks same operator got confused and loaded wrong side of the part','Warning has been given and fined the operator for one day salary and one extra Sunday duty which is commencing from 1st of Jan. \r\n','New fixture has been created and pin will be located to identify the side of the part, fixture used and found okay with the parts','Next parts found good','','2014-12-24','Rangaswamy()','Manohara(B.C.)','','0000-00-00','* wrong part loading so dia 6.35mm hole shift. ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','07','no','Misc','Girish(Prasad P)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8060,'30-113','Gardner Aerospace-Derby Limited','RIB 1 OFW','5440601','L575 57325 201 - PF','','A00',2,'LPR0000410','','33440','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','21 Holes of diameter 5.6 mm  missing in 2 parts. ','The operation of 21 holes of diameter 5.6 mm will happen in 1st setup itself. Due to power trip the operator missed that sequence of program itself while machining','Checked all the stock parts and quarantined the parts which was affected and immediately sent replacement parts for that batch to the customer','Changes have been made such a way that if program misses next program will not be able to run until and unless previous sequence of program running.','Next batches found good ','C30007','2014-12-24','Avinash(R.J.)','Muniyappa(N)','GARDNER-001','2014-10-29','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','CUST END','no','Misc','Avinash(R.J.)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8061,'30-081','Gardner Aerospace-Derby Limited','FITTING FWD','584238A0','L575 52120 201','','A00',4,'LPR0000410','','32219','','0000-00-00',NULL,'yes','no','no','no','yes','no','no','no','yes','14.654 Bore diameter over size by 0.5 mm.','Since its a controlled bore and datum bore also, 100% inspection of bore is carried out in all the parts by either Bore gauge or CMM, Discussion is going on with customer regarding the problems and CAPA.','Since its a controlled bore and datum bore also, 100% inspection of bore is carried out in all the parts by either Bore gauge or CMM, Discussion is going on with customer regarding the problems and CAPA.','Since its a controlled bore and datum bore also, 100% inspection of bore is carried out in all the parts by either Bore gauge or CMM, Discussion is going on with customer regarding the problems and CAPA.','Since its a controlled bore and datum bore also, 100% inspection of bore is carried out in all the parts by either Bore gauge or CMM, Discussion is going on with customer regarding the problems and CAPA.','C29464','2014-12-24','Avinash(R.J.)','Narayanappa(G)','GARDNER-002','2014-10-29','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','CUST END','no','Misc','Avinash(R.J.)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8062,'35-183A','Saab AB','EDGE HOUSING','675763A7','423Z1121-6-02','','--A',1,'1600082632','','36722','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Wall thickness measures 0.5mm undersize.','Due to put the center bolts not properly so wall thickness undersize\r\n','Put the center bolts properly and bolt tightness also checked then run the production. \r\n','Instructed operator to every part put the center bolts properly and bolt tightness also checked then run the production.  \r\n','Next Part found satisfactory','','2014-12-24','Rangaswamy()','Rangaswamy()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','DN','no','Misc','Manjunath(G)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8063,'18-368A','Magellan Aerospace Bournemouth','CATCHER ACTUATOR SPI ','0719701','L575 52396 200','','C00',1,'RP400947','','39324','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Y offset wrong so hole pitch 6 mm shift.  ','Operator took wrong offset( taken offset for 6 mm instead of .06 mm)\r\n','Warning has been given and fined the operator for one day salary and one extra Sunday duty which is commencing from 1st of Jan. New fixture has been introduced for avoid taking offset.after butting the part check with feeler gauge and run according to progaram','New fixture has been introduced for avoid taking offset.after butting the part check with feeler gauge and run according to progaram','Next Part found ok','','2014-12-25','Lohith(K)','Chiranjeevi(S)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','05','no','Misc','Anjinamurthy(H)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8064,'18-380B','Magellan Aerospace Bournemouth','GAMMA FITTINGS ','4193','NSA840020-350','','L',126,'RP397607','','31462','','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.','Root Cause:\r\nThe Following route cause analyzed for the parts rejected, 1. Ovality in RM. 2. Total Length Minus\r\nin RM. 3. Improper Butting in Jaws. 4. Jaws Boring is not good( Flatness is not achieved. 5. RM\r\nunclear on OD and ID. 6. Ovality More than 0.05mm in billet stage. 7. Chips clocking at the Jaws ,\r\nIn Part butting faces. 8. Roughing and Finishing inserts wear out.  \r\n','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 the\r\nclamping.  \r\n','Compulsorily use 6-Jaw chuck for all the Gamma for both roughing and Finishing operations. 3.Plan\r\nfor Parts to be inspect for Face out and Ovelity before loading for finishing operations. 4.Methods\r\nof tightening the part on to the Mandril in operation-02. 5.create the rough surface on OD in\r\nroughing operation to strengthening the clamping. ','Old batches parts, Next parts found okay','','2014-12-25','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','3','no','Misc','Dinakar(K)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8065,'18-380B','Magellan Aerospace Bournemouth','GAMMA FITTINGS ','M510620','NSA840020-350','','L',2,'RP393647','','30428','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','K,G,J& H\r\ndimension all\r\nare undersize\r\nin 0.010 to\r\n0.030.','The Following route cause analyzed for the parts rejected, 1. Ovality in RM. 2. Total Length\r\nMinus in RM. 3. Improper Butting in Jaws. 4. Jaws Boring is not good( Flatness is not achieved. 5.\r\nRM unclear on OD and ID. 6. Ovality More than 0.05mm in billet stage. 7. Chips clocking at the Jaws\r\n, In Part butting faces. 8. Roughing and Finishing inserts wear out. ','The Following CA/PA taken to avoid the rejections, 1.Sizes and Tolerance for Roughing\r\nstage.(Sample parts made to check the parts visually also for reference) 2. Compulsorily use 6-Jaw\r\nchuck for all the Gamma for both roughing and Finishing operations. 3.Plan for Parts to be inspect\r\nfor Face out and Ovelity before loading for finishing operations. 4.Methods of tightening the part\r\non to the Mandril in operation-02. 5.create the rough surface on OD in roughing operation to\r\nstrengthening the clamping. ','The Following CA/PA taken to avoid the rejections, 1.Sizes and Tolerance for Roughing\r\nstage.(Sample parts made to check the parts visually also for reference) 2. Compulsorily use 6-Jaw\r\nchuck for all the Gamma for both roughing and Finishing operations. 3.Plan for Parts to be inspect\r\nfor Face out and Ovelity before loading for finishing operations. 4.Methods of tightening the part\r\non to the Mandril in operation-02. 5.create the rough surface on OD in roughing operation to\r\nstrengthening the clamping. ','Next parts found okay','','2014-12-25','Dinakar(K)','Krishnanaik J N,Kalakappa T H,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','3','no','QT100S-4','Dinakar(K)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8066,'18-381B','Magellan Aerospace Wrexham','GAMMA FITTINGS ','M498570','NSA840020-400','','L',84,'RP114762','','30559','','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\r\nMinus in RM. 3. Improper Butting in Jaws. 4. Jaws Boring is not good( Flatness is not achieved. 5.\r\nRM unclear on OD and ID. 6. Ovality More than 0.05mm in billet stage. 7. Chips clocking at the Jaws\r\n, 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\r\nstage.(Sample parts made to check the parts visually also for reference) 2. Compulsorily use 6-Jaw\r\nchuck for all the Gamma for both roughing and Finishing operations. 3.Plan for Parts to be inspect\r\nfor 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\r\nstrengthening the clamping. ','The Following CA/PA taken to avoid the rejections, 1.Sizes and Tolerance for Roughing\r\nstage.(Sample parts made to check the parts visually also for reference) 2. Compulsorily use 6-Jaw\r\nchuck for all the Gamma for both roughing and Finishing operations. 3.Plan for Parts to be inspect\r\nfor 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\r\nstrengthening the clamping. ','Next parts found okay','','2014-12-25','Dinakar(K)','Nandeesha N,Girish S,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','Manufacture Only','','3','no','QT100S-5','Dinakar(K)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8067,'18-381B','Magellan Aerospace Bournemouth','GAMMA FITTINGS ','M498570','NSA840020-400','','L',107,'RP397608','','30172','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','K,G,J& H dimension all are undersize in 0.010 to 0.030. ','The Following route cause analyzed for the parts rejected, 1. Ovality in RM. 2. Total Length\r\nMinus in RM. 3. Improper Butting in Jaws. 4. Jaws Boring is not good( Flatness is not achieved. 5.\r\nRM unclear on OD and ID. 6. Ovality More than 0.05mm in billet stage. 7. Chips clocking at the Jaws\r\n, In Part butting faces. 8. Roughing and Finishing inserts wear out. ','The Following CA/PA taken to avoid the rejections, 1.Sizes and Tolerance for Roughing\r\nstage.(Sample parts made to check the parts visually also for reference) 2. Compulsorily use 6-Jaw\r\nchuck for all the Gamma for both roughing and Finishing operations. 3.Plan for Parts to be inspect\r\nfor Face out and Ovelity before loading for finishing operations. 4.Methods of tightening the part\r\non to the Mandril in operation-02. 5.create the rough surface on OD in roughing operation to\r\nstrengthening the clamping. ','The Following CA/PA taken to avoid the rejections, 1.Sizes and Tolerance for Roughing\r\nstage.(Sample parts made to check the parts visually also for reference) 2. Compulsorily use 6-Jaw\r\nchuck for all the Gamma for both roughing and Finishing operations. 3.Plan for Parts to be inspect\r\nfor Face out and Ovelity before loading for finishing operations. 4.Methods of tightening the part\r\non to the Mandril in operation-02. 5.create the rough surface on OD in roughing operation to\r\nstrengthening the clamping. ','Next parts found okay','','2014-12-25','Dinakar(K)','Nandeesha N,Kalakappa T H,Dinakar K,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','Manufacture Only','','3','no','QT100S-4','Dinakar(K)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8068,'07-019','HAL-NASIK','SPAR','AS-14952','11.3120.3.800.001-1','','Technical Sheets',1,'NK/M/2513 (4440) ?MP','','38483','','0000-00-00',NULL,'yes','','yes','','','no','','yes','','Part right side small pocket base thickness - side.\r\nre-engineering program running time after 2nd part bend  observe.Part got minus side','Right side part get more bend after 16 flat program running then 12R3 program running time part inside pocket base thickness 0.5 minus side after tolerance','Change the 16 Flat program with 2mm more stock in bottom and adding one more clamp that side.','Re engineering part get more bend after 1st SU, there for next batches run the old proved process program and any changes required for continuous improvement, in same process only program will be changes required. ','Old Program ran, There is no MPS revision done for re engineering.Waiting for next batch for production to evaluate effectiveness','','2014-12-25','Narayanappa(G)','        Sathish Y.R.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8069,'35-192','Saab AB','SUPPORT-FTG','581308','423Z1202-14','','---',1,'1600096186','','38871','','0000-00-00',NULL,'yes','no','yes','','','','','yes','','Dig Mark on R5 radius on Pocket.','This deviation due to load taken by Dia 10 ball nose in Base radius.\r\nTool broken and dig mark observed on part.','Due to Scallop height in radius is more when we checked in CAD,May this deviation coming.\r\nScallop reduced to 0.5mm and regenerated the program and checked the tool load while Dia 10 ball nose program running.\r\nSmoothly program was running now and continued production.','The following PA action discussed with CAD/CAM and actions will follow as follows.\r\n1.While doing a FAI part programming radius stock will considered as minimum to avoid any load to finishing cutters.\r\n2.If required Semi-finish program will run to avoid load on finishing cutters.\r\n3.Cutters condition will check before loading the tools to machine while doing setting.\r\n4. Dedicated tools will kept to monitor the tool condition for each CRN.','Waiting for next batch production and next parts found okay also','','2014-12-25','Rangaswamy()','        Manohara B.C.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8070,'18-342A','Magellan Aerospace Bournemouth','LANDING TOP PANNEL','A595321','F574 50967 200 01','','E, ECN PG49998ST1TV23',2,'RP400947','','38777','','0000-00-00',NULL,'no','no','no','yes','no','yes','no','yes','no','Linear indication found on the part surface.','RM received from the supplier having feed lines on the surface and this surface was not machined so\r\ninformed to Procurement for this issue. ','Informed to procurement for taking actions for supplier. ','Informed to procurement for taking actions for supplier. ','CA/PA found satisfactory. ','','2014-12-25','Muniyappa(N)','Nandishkumar(D.K.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','15822','POST DN','no','Misc','Muniyappa(N)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8071,'35-157A','Saab AB','INTERCOSTAL_VENT','564338','423Z1172-3-01','','---',1,'1600086478','','38905','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Running time part left so 7.2 hole shift.','While machining operation-01, part lift from Vice and dia 7.2mm hole shifted.\r\nDue to less clamping force in vice part lifts and this deviation coming.\r\nMay be operator not tightened the vice at required force.\r\nDue to RM not flat at butting face causes vibration to lift part while running roughing program.\r\n','Kurt Vices are used from years and clamping force is enough to clamp the aluminum billets.\r\nClamping force checked for every part and continued production.\r\nRM flatness and butting face checked for every part.\r\n','Informed to all the operators to clamp the Vices at required force.( Checking by hand felling).\r\nHardened Jaws ordered with serration to increase the clamping force to avoid such problems.','CAPA found satisfactory. Next parts found okay','','2014-12-26','Girish(Prasad P)','        Prashanth Kumar M','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8072,'18-376B','Magellan Aerospace Bournemouth','GAMMA FITTINGS ','3822 ','NSA840020-150','','L',226,'RP397604','','28720','','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\r\nin RM. 3. Improper Butting in Jaws. 4. Jaws Boring is not good( Flatness is not achieved. 5. RM\r\nunclear on OD and ID. 6. Ovality More than 0.05mm in billet stage. 7. Chips clocking at the Jaws ,\r\nIn 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. ','Next batches found ok.','','2014-12-29','Dinakar(K)','Dinakar K,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','3','no','QT100S-3','Dinakar(K)',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8073,'35-191','Saab AB','SUPPORT-FTG','581308','423Z1202-13','','---',1,'1600096186','','40015','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Dia 18R5 tool offset wrong taken.','Dia 18R5 tool offset wrong taken. so part base tool dig mark.','check wrong tool offset and identify , stop the  m/c Again taken tool offset correctly, and run the machine.Instruct  to value of operator work, responsibility of operator.','Instruct to operator every tool offset taken cross check two times.','Effectiveness needed to be measured because hence its a repeated reason for rejection(Taking offset).','','2014-12-30','Rangaswamy()','        Manohara B.C.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8074,'07-008B','HAL-NASIK','Web 3 Route Portion ','BS-17679','11.2000.2.125.904-LH','','221.02141.00688',1,'NK/M/2513(4520)/MP/O','','39721','','0000-00-00',NULL,'no','yes','yes','yes','no','no','no','no','no','Right End U Type  profile area, required 6.0mm wall thickness mines,measure value is 5.0mm so 1mm mines ','Refer NCR no.08075','Refer NCR no.08075','Refer NCR no.08075','Dummy NCR created refer NC no 8075','','2014-12-31','Narayanappa(G)','PAVAN KUMAR (S.K.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','Manufacture Only','','03','no','Misc','Narayanappa(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8075,'07-008B','HAL-NASIK','Web 3 Route Portion ','BS-17679','11.2000.2.125.904-LH','','221.02141.00688',1,'NK/M/2513(4520)/MP/O','','39721','','0000-00-00',NULL,'no','yes','yes','yes','no','no','no','no','no','Right End U Type  profile area, required 6.0mm wall thickness mines,measure value is 5.0mm so 1mm mines ','RM size variation.After machining found that RM was over size, The required RM size is 170mm to 180mm in outer, but measures 200mm RM width over, program run only 180mm width in pocket,tool hit the wall and the part was removed from location pin part disturbed due to excess of RM size.   ','1.Instructed to operator put proper clamps while run program, \r\n2.inform to  store, The process sheet and exact required dimension and then cut the RM,\r\n3.Immediately inform to cad & requested to give the currect program. ','1.Strictly inform to operators if any deviation from RM not received in production.\r\n2.Instructed to operator put proper clamps while run program,\r\n3.Immediately inform to cad & requested to give the correct program. ','CAPA found satisfactory and next batch productions will be taken care','','2014-12-31','Narayanappa(G)','PAVAN KUMAR (S.K.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','Manufacture Only','','03','no','Misc','Narayanappa(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8076,'18-386A','Magellan Aerospace(Chalfont) Limited','NUT RING INNER','487664','D575 40039 200','','B',1,'P/074123','','37620','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Slot width over size by 1.1mm mesured.','While doing slotting operation this deviation coming due to slotting tool wear out. Slotting width\r\nnot checked for 02nos while running production due to process stability. \r\n','After finding a deviation in slot width, all the parts checked and found OK. After checking the all\r\nthe parts production continued with new slotting tool and found ok. \r\n','Informed to operator to check the tool wear regularly. and also check the slot width 100% by slip\r\ngauge. \r\n','After wear out of tool, Previous part and next part should be ensured by Quality. ','','2014-12-31','Rakeshbabu(V)','Manjunath  M,Dinakar K,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','QT100S-1','Narasimha Murthy(R)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8077,'18-121A','Magellan Aerospace Bournemouth','BARREL - STRUT','247348','D572 50463 201','S98 FHT','F',1,'RP400839','','39666','','0000-00-00',NULL,'yes','yes','yes','','','','','','','part butting probelm so total length (- 0.5). ','The Following route cause analyzed for the parts rejected, Jaws Boring is not good,part not butted properiy to the jaws because of small chips are in Part butting faces.Roughing and Finishing inserts wear out. 							\r\n','The Following CA/PA taken to avoid the rejections.Sizes and Tolerance for Roughing stage clean the jaws with the help of air and before loading the part.after clamping the every part check the part it was butted in the jaws face properly.																	\r\n							\r\n','The Following CA/PA taken to avoid the rejections.Sizes and Tolerance for Roughing stage clean the jaws with the help of air and before loading the part.after clamping the every part check the part it was butted in the jaws face properly.','Warned operator because 3 numbers of same work order rejected in 2 consecutive days and next parts found okay.','','2014-12-31','Dinakar(K)','        Girish V M','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8078,'28-006A','Magellan Aerospace New York  Inc.','SHOULDER BOLT ','G21123','162A3109 -2','',' 	PL Iss A, PSDL Iss A, ECN C141079',1,'128183_R0_C1','','39488','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','It was observed during source inspection that Dimension .1300/.1400 inch measures .1213/.1222 and .4800/.4900 measures 0.4720 in one part out of 37 parts.','1)Insert was changed and the first part was not checked.\r\n2)The above dimensions were overlooked by the inspector in the particular part.','1)Instructed to the operator take correct offset.\r\n2)Instructed to inspector to concentrate thoroughly while inspecting the parts.\r\n','1) When the tool is changed part to be Offered to inspection.\r\n2)A checking gauge is designed to check linear dimension.\r\n','Warned both Inspector and Operator not to commit these types of mistakes. After changing the tool before part and after part should be checked either by supervisor or Quality person.','','2014-12-31','Avinash(R.J.)','Sudhagar(V)','','0000-00-00','Source Inspector IRR','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','CUST END','no','Misc','Muniyappa(N)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8079,'35-138','20d5Saab AB','FLCD_DS_SUPPORT_DEFLECT_S','7530455','423Z6189-3','BAC1534-62C','---',1,'1600097307','','39194','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Material layer chip out.Part thickness reached out of tolerance.','The Following Route causes analyzed for material chip off after outer profile machining. 1. Due to RM deviations material will chip off. 2. While running production, the finishing tool wear out causes light chip off in material. 3. Steel Butting sheet for part is not Flat.','The following Corrective Action/Preventive Action taken to avoid Materiel chip off. 1. Raw Material will inspect visually before issuing to production. If found any problem visually RM will be quarantined. 2. Dia 8 end mill life calculated, informed to operators to monitor the tool life.and change the tool after as mentioned. 3. Steel butting plates flatness inspection done before production starts.','The following Corrective Action/Preventive Action taken to avoid Materiel chip off. 1. Raw Material will inspect visually before issuing to production. If found any problem visually RM will be quarantined. 2. Dia 8 end mill life calculated, informed to operators to monitor the tool life.and\r\nchange the tool after as mentioned. 3. Steel butting plates flatness inspection done before production starts. Taking all the above PA, rejections happened in material chip off. Out of 100nos production 5 to 6nos getting rejection. Due to customer requirement parts are manufactures with considering rejections.','**Theoretical Explanation**. Practically should be implemented.Next batch will be observed for effectiveness. ','','2015-01-01','Lohith(K)','','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','\r\n198','yes','no','With Treatment','','DN','no','Misc','Manjunath(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8080,'18-090A','Magellan Aerospace Bournemouth','BUSH','A0484U','D278 50164 200','S80 FHT','A',1,'RP400843','','39903','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','R/M length under size by (-0.50mm).','After machining found that RM was undersized, While cutting the RM he misinterpreted the dimension and made it wrong.\r\n','Instructed to RM cutter to have the process sheet and exact required dimension and then cut the RM\r\n','Instructed to RM cutter to have the process sheet and exact required dimension and then cut the RM\r\n','Next batch found okay\r\n','','2015-01-01','Nagaraja (G)','Sunil Kumar(K.R.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','01','no','Misc','NIRANJAN(N  )','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8081,'18-121A','Magellan Aerospace Bournemouth','BARREL - STRUT','247348','D572 50463 201','S98 FHT','F',1,'RP400839','','39666','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Total length undersize(-0.04mm).','Root Cause:\r\nThe Following route cause analyzed for the parts rejected, Jaws Boring is not good,part not butted\r\nproperiy to the jaws because of small chips are in Part butting faces.Roughing and Finishing inserts\r\nwear out.  \r\n','The Following CA/PA taken to avoid the rejections.Sizes and Tolerance for Roughing stage clean the\r\njaws with the help of air and before loading the part.after clamping the every part check the part\r\nit was butted in the jaws face properly.  \r\n','The Following CA/PA taken to avoid the rejections.Sizes and Tolerance for Roughing stage clean the\r\njaws with the help of air and before loading the part.after clamping the every part check the part\r\nit was butted in the jaws face properly.  \r\n','As per customer Instruction Parts accepted.','','2015-01-01','Dinakar(K)','Girish V(M)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','Manufacture Only','','05','no','Misc','Narasimhamurthy(K.G.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8082,'18-121A','Magellan Aerospace Bournemouth','BARREL - STRUT','247348','D572 50463 201','S98 FHT','F',1,'RP400839','','39666','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Total length undersize(-0.06mm).','Root Cause: The Following route cause analyzed for the parts rejected, Jaws Boring is not good,part\r\nnot butted properiy to the jaws because of small chips are in Part butting faces.Roughing and\r\nFinishing inserts wear out. ','The Following CA/PA taken to avoid the rejections.Sizes and Tolerance for Roughing stage clean the\r\njaws with the help of air and before loading the part.after clamping the every part check the part\r\nit was butted in the jaws face properly.  \r\n','The Following CA/PA taken to avoid the rejections.Sizes and Tolerance for Roughing stage clean the\r\njaws with the help of air and before loading the part.after clamping the every part check the part\r\nit was butted in the jaws face properly.  \r\n','As per customer Instruction Parts accepted.','','2015-01-01','Dinakar(K)','Girish V(M)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','Manufacture Only','','05','no','Misc','Narasimhamurthy(K.G.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8083,'35-160','Saab AB','STOP SUPPORT','G21183K07','423Z6188-5','','---',1,'1600097307','','39030','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Due to running time tool broken.so Dia 22.86 bore over  size (0.1 mm)','Due to running time tool broken.so Dia 22.86 bore over  size (0.1 mm)','1) New tool changed and further part found OK.\r\n2) Instruction given to operator cross check the end mill condition.\r\n3) Instructed to operator first refer in tool overhang in the process sheet and after tool loaded then run the production.','1) New tool changed and further part found OK.\r\n2) Instruction given to operator cross check the end mill condition.\r\n3) Instructed to operator first refer in tool overhang in the process sheet and after tool loaded then run the production.','No proper Root cause. Repeated reason for rejection.Instructed to operator to ensure the tool life in register.','','2015-01-01','Lohith(K)','Lohith(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','3','no','Misc','Lohith(K)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8084,'18-209B','Magellan Aerospace(Chalfont) Limited','BODY','4842','D321 40204 202','','D, ECN NR29999ST1KM15, NR29999ST2KF65, WQN DFB09775',1,'P/074113','','39471','','0000-00-00',NULL,'yes','no','no','no','yes','yes','no','no','no','19.00 +0.021 Bore oversize 0.010 mm.','All stage operation will be completed part bore over size not noticed in milling, turning and fitting department, but noticed in inspection 1no.','Next batch production will be take care.\r\nInstructed to operators and fitters check the stage-vice any deviation report in concern supervisor and written in the rejection board.     ','Next batch production will be take care.\r\nInstructed to operators and fitters check the stage-vice any deviation report in concern supervisor and written in the rejection board. ','Waiting for next batch to evaluate effectiveness.','','2015-01-02','Lohith(K)','Theerthappa K.N.,Shivaraj K S,Shivappa M B,Seetharamu D,Nandeesha N,Krishnanaik J N,Hari Prasad,Girish V M,Dinakar K,Devaraj K.C.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','0','FI','no','HAASVF2SS-2','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8085,'35-031A','Saab AB','7600169-201 ','3437701','L574 50169 201','','B00, PG74415001JA01',1,'1600091592','','39466','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Dia 4.83 Hole Chamfer Plus Side.','Refer NCR no.08091 ','Refer NCR no.08091 ','Refer NCR no.08091 ','For effectiveness refer NC no 8091','','2015-01-04','Narayanappa(G)','        Gajendra Singh C.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','','yes','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8086,'35-145','Saab AB','BCD_LATCH-PROBE_FTG_BRACK','755085A8','424Z6116-2-01','7050 - T7451 ALUMINU','--B',1,'1600101109','','40163','','0000-00-00',NULL,'yes','yes','yes','','','','','','','part wall broken','while program running time unexpected Tool Hit on the Part, so part wall broken, part was rejected. ','Problem analyzed and find problem in Tool D value.D-value not calculated by machine.This problem not continuously coming,at some time this was noticed.\r\nPlanned to enter the D-value in all the programs and this was monitoring.\r\nInformed to operators to check the D-value activation in machine after every tool change.    ','Planned to enter the D-value in all the programs to monitor.\r\nInformed to operators to check the D-value activation in machine after every tool change.    ','Next part found okay.','','2015-01-04','Narayanappa(G)','        Gajendra Singh C.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8087,'18-331A','Magellan Aerospace Bournemouth','LANDING STRIP FWD','66894/01/00','L575 53255 200','L109','A00',2,'RP400947','','37322','','0000-00-00',NULL,'no','no','no','no','no','yes','yes','yes','no','Corrosion fits abserved on the surface.','Due to scratches in parts and feed lines and behavior of RM corrosion fits found  ','Part should be cleansed with PX-24 at regular intervals, excessive feed lines and fitting work should be avoided.','Part should be cleansed with PX-24 at regular intervals, excessive feed lines and fitting work should be avoided.','Part reworked and sent for Treatment house','','2015-01-05','Narayanappa(G)','Narayanappa(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','','postdn','yes','Misc','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8088,'18-331A','Magellan Aerospace Bournemouth','LANDING STRIP FWD','66894/01/00','L575 53255 200','L109','A00',2,'RP400947','','38781','','0000-00-00',NULL,'no','no','no','no','no','yes','yes','yes','no','Corrosion fits abserved on the surface.','Due to scratches in parts and feed lines and behavior of RM corrosion fits found  ','Part should be cleansed with PX-24 at regular intervals, excessive feed lines and fitting work should be avoided.','Part should be cleansed with PX-24 at regular intervals, excessive feed lines and fitting work should be avoided.','Part reworked and sent for Treatment house','','2015-01-05','Narayanappa(G)','Narayanappa(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','','POSTDN','yes','Misc','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8089,'18-331A','Magellan Aerospace Bournemouth','LANDING STRIP FWD','66894/01/00','L575 53255 200','L109','A00',2,'RP400947','','38792','','0000-00-00',NULL,'no','no','no','no','no','yes','yes','yes','no','Corrosion fits abserved on the surface.','Due to scratches in parts and feed lines and behavior of RM corrosion fits found  ','Part should be cleansed with PX-24 at regular intervals, excessive feed lines and fitting work should be avoided.','Part should be cleansed with PX-24 at regular intervals, excessive feed lines and fitting work should be avoided.','Part reworked and sent for Treatment house','','2015-01-05','Narayanappa(G)','Narayanappa(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','','POSTDN','yes','Misc','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8090,'18-332A','Magellan Aerospace Bournemouth','LANDING STRIP FWD','66894/01/00','L575 53255 201','L109','A00',3,'RP400947','','38793','','0000-00-00',NULL,'no','no','no','no','no','yes','yes','yes','no','Corrosion fits abserved on the surface.','Due to scratches in parts and feed lines and behavior of RM corrosion fits found  ','Part should be cleansed with PX-24 at regular intervals, excessive feed lines and fitting work should be avoided.','Part should be cleansed with PX-24 at regular intervals, excessive feed lines and fitting work should be avoided.','Part reworked and sent for Treatment house','','2015-01-05','Narayanappa(G)','Narayanappa(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','','POSTDN','yes','Misc','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8091,'35-031A','Saab AB','7600169-201 ','3437701','L574 50169 201','','B00, PG74415001JA01',1,'1600091592','','39466','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Dia 4.83 Holes Plus Side(3holes) measure value dia 6.0mm','While adjusting the Chamfer, operator wrong wear value entered and dig mark observed on hole.\r\nPart thickness varies in different pockets and single program created causes dig mark on one pocket.\r\n\r\n','1.Wear value corrected and continued production.\r\n2.Program spited and individual programs done for all the pockets, this will avoid error in adjusting in tool wear or program.\r\n3.Dedicated tools ordered to eliminate the editing of program in every batch. ','1.Program spited and individual programs done for all the pockets, this will avoid error in adjusting in tool wear or program.\r\n2.Dedicated tools ordered to eliminate the editing of program in every batch. ','If program has been edited,split, changed where is the Revision?? Until and unless procedure followed NC will be closed.','','2015-01-05','Narayanappa(G)','        Gajendra Singh C.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','no','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8092,'28-006A','Magellan Aerospace New York  Inc.','SHOULDER BOLT ','G21123','162A3109 -2','',' 	PL Iss A, PSDL Iss A, ECN C141079',1,'128183_R0_C1','','39488','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Dummy NC','Dummy NC','Dummy NC','Dummy NC','Dummy NC','','2015-01-06','Avinash(R.J.)','Sudhagar(V)','','0000-00-00','Source Inspector IRR','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','CUST END','no','Misc','Muniyappa(N)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8093,'18-104A','Magellan Aerospace Bournemouth','BODY TURNBUCKLE','239338','D575 40490 200','S80 FHT','E',1,'RP400840','','39670','','0000-00-00',NULL,'yes','yes','yes','','','','','','','ID Thread NO GO Anwsered..','After 25nos running threading insert will be wear out.for next part threading insert will be changed and 0.4 plus(+)taken in wear offset and run the part but thread gauge was not answered then 0.2 minous(-) taken to wear offset and run the part that time thread gauge was nogo answered.','For next part x-offset taken and taking 0.3 mm up in toolwear offset and run the part gauge not answerd,in x-offset give 0.1mm down and run the part and gauge not answered then in x-offset down 0.05mm and run the part and then gauge answered and next part run in same reading & the part found okay.','Instruction given to operator to take x-offset & z-offset whenever the inserts are changed.','CAPA found okay, but instructions should be either in Process sheet as a flag note or prepare a board for it and hang over it near by machines.','','2015-01-06','','        Seetharamu D','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8094,'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','','39802','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Total length -0.5mm','The Following route cause analyzed for the parts rejected, Jaws Boring is not\r\ngood,part not butted properiy to the jaws because of small chips are in Part butting faces.Roughing\r\nand Finishing inserts wear out.  \r\n','Sizes and Tolerance for Roughing stage clean\r\nthe jaws with the help of air and before loading the part.after clamping the every part check the\r\npart it was butted in the jaws face properly.','Sizes and Tolerance for Roughing stage clean\r\nthe jaws with the help of air and before loading the part.after clamping the every part check the\r\npart it was butted in the jaws face properly.','Next parts found okay. Please take care of this simple basic rules of machining like butting the part, do the jaws boring correctly.','','2015-01-07','','        Shivappa M B','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8095,'28-045','Magellan Aerospace New York  Inc.','LEVER','158524','65-51632-6','','PL_Rev - A + ADCN # 2 ; DL_Rev - N/C',1,'125339-2520_R0_C0','','39879','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Dig mark observed on part.','Part wrongly loaded in operation-07. Operator not noticed the loading of part and dig mark observed after running roughing\r\ntool because part was wrongly loaded.','1) Immediately checked and marked the front face for all the remaining parts.\r\n2) Changing the clamping bolt and washers.\r\n3) Instructed to operator, every part loading time check the front and back face.    ','1) Changing of washer in fixture for clamp identification.\r\n2) Give in \"M0\" and message in the program.\r\n3) Machining impossible wrong loading of part by changing the  clamps and  bolts.\r\n     ','Next parts found okay','','2015-01-07','Anjinamurthy(H)','        Manohara M','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8096,'35-257','Saab AB','BRACKET, DEFLECTION STOP','G19002K03','423Z6187-5','','---',1,'PA 1510 NEW PARTS-1','','40223','','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.\r\nOperator 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\nProduction continued and supervisor is monitoring. \r\n\r\n  ','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.\r\n\r\n','Next parts found okay','','2015-01-07','Lohith(K)','        Dhananjaya N','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8097,'35-140','Saab AB','BCD_DR_BEAM_FTG_UPR_FWD_4','582082','424Z1130-14-01','7050 - T7451 ALUMINU','--B',2,'1600097307','','38996','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1.Side wall thickness is minus side.\r\n2.Base thickness measures minus side.                                         ','1. While running production batch, when final cutout program running part moved due to less clamping.( There is no locating pins in operation-02)this moving of part causes wall thickness measures minus side.\r\n2.When doing first off part operator not checked the tool offset.Previous part Z-offset considered and running this part and dig mark observed in base.','1.Clamping bolts and Washers checked and also threads in hole cross checked and found ok. Production continued with extra care and all other parts found ok.\r\n2.Tool offset taken and continued production. Next part found ok.','1.Planned to introduce locating pins while cutout program running. or New Fixture to be made with rigid clamping with washers for 06 holes to avoid part moving.\r\n2.This error is due to not follow the procedure while doing setting in machines.Operator should check the Work offset and written done the value in reference book.Therefore informed to operators to follow the procedure. Supervisor to be monitor the same.','Next parts found okay.','','2015-01-07','Rangaswamy()','Rangaswamy()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','Misc','Manjunath(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8098,'18-284A','Magellan Aerospace Bournemouth','SPINDLE FOR CLACK ALVES O','Y10819','A281-40019-200','S80 FHT','A',5,'RP400846','','39979','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','dia 1.6mm drill broken, Distance 1.6mm is measure 1.8mm.','','','','Closed','','2015-01-07','Nagaraju(T)','Nagaraju(T)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','05','no','Misc','Nagaraju(T)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8099,'18-387A','Magellan Aerospace(Chalfont) Limited','NUT RING INNER','229234','D575 40039 202','','B',1,'P/074123','','40196','','0000-00-00',NULL,'yes','yes','yes','','','','','','no','parting insert bronken thickness (-) sid o.1','after running the key way setup we are done the parting for next setup so after 20 to 25 parts parting insert will be brocken or blented. In this setup after running a 15 parts parting insert edge chiped out and insert will rubbing the part so 0.1 taper occure in the next part so that part will be rejected.\r\n','next batch after every 20 nos one time parting insert will be checked thoroughly and before loading the next part parting insert checking after running.','next batch after every 20 nos one time parting insert will be checked thoroughly and before loading the next part parting insert checking after running','CAPA found okay. CAPA will be monitored.','','2015-01-08','','        Manjunatha N','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8100,'18-350A','Magellan Aerospace(Chalfont) Limited','PLATE','28294','F574 51166 200','ABM3 1029','B01, ECN PG40011ST1KG85, PG40011ST1TB03',1,'P/074120_Amnd-04','','39937','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','Dig mark observed on part (1mm). ','Due to process problem.Clamping method not properly. While part running time part was roteted.','When cutout program running time \"Z\" offset 0.2mm up after run the program.Production continued and supervisor is monitoring. ','The following PA action planned and implemented,\r\n1)Put the angle holes and apply the M5 taps and added some bolts.\r\nInform to CAD department change the  process sheet in next batch. ','If we have problem in process, let it be corrected by CAD. Until the process is standardized NC will not be closed. (Raghuveer)','','2015-01-08','Anjinamurthy(H)','Girish(HP)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Lohith(K)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8101,'28-044','Magellan Aerospace New York  Inc.','LINK ASSEMBLY UPPER UPLOC','A13434 ( WO NO 14175','161A6122-6','','PL_Rev-A, PSDL-Rev-N/C',1,'128069-3170','','38148','','0000-00-00',NULL,'yes','','yes','','','','','yes','no','PART RUNNING TIME REAMER FAILURE,,,','Part Accepted','Part Accepted','Part Accepted','Part Accepted','','2015-01-08','Rangaswamy()','        Gurukiran S M','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8102,'35-139','Saab AB','BCD_DR_BEAM_FTG-LWR_FWD-4','582083','424Z1130-13-01','7050 - T7451 ALUMINU','--B',1,'1600071424','','39701','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','* Dia 7.0mm Holes Plus Side(1hole) measure value dia 8.0mm.','While doing first off part, due to operator mistake this deviation coming.\r\nHole mill Program running before pre drill program. This causes hole oblong and hole size not achieved.','After checking the first part, operator noticed the error and program sequence checked and corrected and next part manufactured and found ok.','Regular practice is to call all the sub-programs in main program and Program sequence is to be checked while doing first off.\r\nNeed training to operator to ensure and understand the program sequences.  ','Next parts found good','','2015-01-08','Rangaswamy()','Rangaswamy()','','0000-00-00','* Dia 7.0mm Holes Plus Side(1hole) measure value dia 8.0mm.','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Girish(Prasad P)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8103,'18-104A','Magellan Aerospace Bournemouth','BODY TURNBUCKLE','239338','D575 40490 200','S80 FHT','E',1,'RP400840','','39671','','0000-00-00',NULL,'yes','yes','yes','','','','','','','thread NO GO answering 01nos','Thread was damaged due to wear out of inserts. The operator intended to rework the damaged\r\nthread resulting in non conformance of ID. ','Insert was worn out at that stage which was replaced for the next job. ','The block holding the tool shall be set by the Supervisor for every batch which is expected\r\nto extend the tool life and reduce these type of non conformances. ','Next part found okay. Training will be given for operators also for holding the block','','2015-01-09','Dinakar(K)','        Dinakar K','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8104,'35-145','Saab AB','BCD_LATCH-PROBE_FTG_BRACK','755085A8','424Z6116-2-01','7050 - T7451 ALUMINU','--B',1,'1600101109','','40163','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Base thickness under size at one point (-0.05)','tool radius problem so due to chartering part under size.\r\nwhile running re-pass at that time due chartering part under size...','when radius found not Ok, immediately tool changed.\r\nbefore loading the tool radius will be checked from the inspection and will be taken clearance. ','before loading the tool radius will be checked at inspection.\r\nbefore loading part at the machine tools will be arranged from the supervisor and it will be checked by the operator for every setting..','CAPA found satisfactory.....','','2015-01-09','Narayanappa(G)','Paramesh(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','01','no','Misc','Paramesh(K)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8105,'18-295A','Magellan Aerospace Bournemouth','BOLT','238302','D577 56145 200','S80','A',1,'RP400846','','40103','','0000-00-00',NULL,'yes','yes','yes','','','','','','','wrong offset entery threading nogo answarde.......','after changing the threading insert we are taking every time  +0.3 in wear offset but  this part after changing the threading insert taking only +.1 in wear offset so thraed effective diameter under sized and NOGO answered.\r\n','for next part +0.3 taken in wear offset & run the threading programe  but go gauge not answered then adjust the wear offset & running  the threading programme GOgauge was answered part checked\r\nfound ok.\r\n','while next batch threading insert changing  +0.3 \r\ntaken in wear offset & run the part  & checking thread\r\neffective dia meter using thread pitch micrometer & adjust wear offset &  run threading programme & checking effective dia & also thread gauge part \r\nfound ok.\r\n','CAPA found okay. But implementation should be done next batches will be monitored.','','2015-01-10','Dinakar(K)','        Manjunatha N','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8106,'18-309B','Magellan Aerospace(Chalfont) Limited','SPIGOT','Y12196','F 575 51290 200','S80','B, ECN PG49999SMAKH49',3,'P/074122','','39909','','0000-00-00',NULL,'yes','yes','yes','','','','','','','TNMG tool probelm so running time part - side (0.01)','after running 5ns TNMG tool sim was brocken so insert \r\nwill not seated properly so running time insert tip will be\r\nbrocken  and insert was rubbing  the part and vibation\r\nstarted in the insert that time it   will removing the extra material in outer diameter  so outer diameter will be undersized.\r\n','change the brocken sim, insert and screw and newely offset taken and 0.2 (+) plus taken in the tool wear offset and run the part and then check the outer diameter and give the correction in wear offset and run the part and checked \r\nfound 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',' CAPA found okay but Implementation is needed.','','2015-01-10','Dinakar(K)','                Girish V M','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8107,'18-386A','Magellan Aerospace(Chalfont) Limited','NUT RING INNER','487664','D575 40039 200','','B',1,'P/074123','','37620','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Slot width over size by 1.1mm mesured.','2nd NCR raised due to ERP problem,\r\n\r\nOriginal NCR no.8076','2nd NCR raised due to ERP problem,\r\n\r\nOriginal NCR no.8076','2nd NCR raised due to ERP problem,\r\n\r\nOriginal NCR no.8076','Dummy NC refer NC no 8076','','2015-01-12','Rakeshbabu(V)','Manjunath  M,Dinakar K,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','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),(8108,'18-113A','Magellan Aerospace Bournemouth','ADJUSTER','424402','D575 40496 200','S80 FHT','G',11,'RP400840','','37999','','0000-00-00',NULL,'yes','no','no','no','yes','yes','no','no','no','Thread nogo answered.','Wrong gauge issued by QAD, Instead of giving truncated gauge normal gauge issued.','Next production parts checked and found okay.Effective diameter will be maintained in middle values so that chances of getting these problems will be less','Gauges with proper identification numbers will be done so that any operator in night or general shifts can easily identify the required gauges. And every time after the first part check the effective diameter by thread pitch micrometer. ','Next parts found okay. Identification numbers under implementation. ','','2015-01-12','Avinash(R.J.)','Shivaraj K S,Seetharamu D,Ningaraj A N,Nataraja C V,Manjunath  M,Hari Prasad,Girish V M,Dinakar K,Chiranjeevi S,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','0','FI','no','DX 200-2 ','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8109,'18-295A','Magellan Aerospace Bournemouth','BOLT','238302','D577 56145 200','S80','A',1,'RP400846','','40104','','0000-00-00',NULL,'yes','','yes','','yes','','','','','1 number thread dig mark.','Running time air pressure low so od thread dig mark .','We are inform to the maintenence for the proper air connection.','We are inform to the maintenence for the proper air connection.','Maintenance team informed sudden loss of pressure avoided and next parts found okay ','','2015-01-12','Ravi(M)','        Bharath R','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8110,'18-309B','Magellan Aerospace(Chalfont) Limited','SPIGOT','Y12196','F 575 51290 200','S80','B, ECN PG49999SMAKH49',1,'P/074122','','39909','','0000-00-00',NULL,'yes','yes','yes','','no','','','','','Od Under Size by .008mm','after running 5ns TNMG tool sim was brocken so insert will not seated properly so running time insert tip will be\r\nbrocken  and insert was rubbing  the part and vibation\r\nstarted in the insert that time it will removing the extra\r\nmaterial in outer diameter so outer diameter will be \r\nundersized\r\n','change the brocken sim,insert and screw  and newely offset \r\ntaken 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 \r\nfound 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',' CAPA found okay but Implementation is needed.','','2015-01-12','Dinakar(K)','        Seetharamu D','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8111,'18-284A','Magellan Aerospace Bournemouth','SPINDLE FOR CLACK ALVES O','Y10819','A281-40019-200','S80 FHT','A',4,'RP400846','','39979','','0000-00-00',NULL,'yes','no','no','no','yes','yes','no','no','no','OD feed lines found.','','','','','','2015-01-13','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','0','FI','no','Misc','Nandishkumar(D.K.)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8112,'35A-239','Saab AB','L/H KIT FOR ARD HINGE / J','','9901503-993','','Exhibit-B',27,'1600091593','','K03714','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','The bushing (drawing no D575403862) installed in D5765000400201 and D5765000400301 should have a chamfer of 0,5 X 45 &#778;with a tolerance of +/- 0,3mm according to document S104 but it measures 1.00mm.','Due to mis drawing interpretaion','We have requested to customer to rework the parts.','Re-arranged the working level and designated separate inspector for checking the BOI.','Next batch found satisfactory.','C33586','2015-01-13','Avinash(R.J.)','Manjunath(G)','Through mail dated 12th Jan2014 from Marcus','2015-01-12','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','cust end','yes','Misc','Manjunath(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8113,'35A-240','Saab AB','R/H KIT FOR ARD HINGE / J','','9901503-994','','Exhibit-B',19,'1600091593','','K03715','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','The bushing (drawing no D575403862) installed in D5765000400201 and D5765000400301 should have a chamfer of 0,5 X 45 &#778;with a tolerance of +/- 0,3mm according to document S104 but it measures 1.00mm.','We have requested to customer to rework the parts.','Re-arranged the working level and designated separate inspector for checking the BOI.','Re-arranged the working level and designated separate inspector for checking the BOI.','Next batch found satisfactory.','C33587','2015-01-13','Avinash(R.J.)','Manjunath(G)','Through mail dated 12th Jan-2015 from Marcus','2015-01-12','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','cust end','yes','Misc','Manjunath(G)','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),