(11920,'35A-408A','Saab AB','FRAME MID ASSY','','D522 73397 000 00','','PART ISSUE B',1,'OWED-LTA-001','','A28388','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','helicoil damaged during the assembly process.','Helicoil is inserted improperly.|During the helicoil insertion process, helicoil was not aligned properly to the part but operator continued the process without noticing it.|Usage of damaged tool caused the improper alignment of the helicoil to the part.|At the beginning of operation operator did not noticed the damage in the tool.','|\r<br/>Operators are informed to verify the tool every-time before the beginning of assembly process. ','|\r<br/>Operators are informed to verify the tool every-time before the beginning of assembly process. ','Next batch parts assembled are verified and found okay. ','','2019-08-12','Ramesh(D)','Nithin(S)','','0000-00-00','helicoil damage','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Assembly','','stage 2','no','Misc','Ramesh(D)','no','N02569|35A-408A-KBOI','|\r\nImmediately stopped the process and informed to the supervisor, the damaged tool is replaced with new one and continued the assembly process. ','E3456','ramesh|qas_sez|qas_sez|','2019-09-26|2019-09-27|2019-09-27|','2019-09-27',NULL,NULL,NULL,NULL,NULL,NULL),(11921,'35-292','Saab AB','BEAM FITTING','255720B5','424Z1144-2','','--B',1,'1600203627','','95873','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Base thickness minus 0.3mm.','Fixture not butting on zero point system |chips found on zero point system  |Improper cleaning.','|Clean the chips and load the fixture','|after machining to clean the fixture in every time for every part.','','','2019-08-12','Dinesh kulal()','Ravi(.S.N)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Dinesh kulal()','no','','|after operation completed to check the part,part will be thickens under size because of chips blocked . ','A3456','qas|','2019-08-12|','2019-08-12',NULL,NULL,NULL,NULL,NULL,NULL),(11922,'35A-464','Saab AB','FITTING ASSY','','D522 73408 001 00','','A',3,'OWED-LTA-001','','A22516','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Is condition:Bushing sticks out 1,80 - 1,85 mm.\r\nShould be: Between 1,55-1,68mm according to drawing D5227340800100 and AIPS 01-02-019','Flange projection out of tolerance from the specification limit|More sealant was applied in the flange of the bush, due to which the bush did not assembled properly and the bush protrusion was not measured.|Bush protrusion requirement isn\'t called in the drawing because of which both the operator and inspector didn\'t ensured the projection before the shipment.|Bush protrusion requirement isn\'t called in the drawing because of which both the operator and inspector didn\'t ensured the projection before the shipment.','Bushes are removed and reassembled to meet the requirements.','APS revised and training was given to both inspector and operators.','Effectiveness will be measured by 23_SEP_2019 ','C75372','2019-08-13','Dharani(Shankar)','Dharani(Shankar)','GLB430832','2019-06-11','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER END','yes','Misc','qas_sez(a)','no','','We have inspected our stock parts and are found okay. We also inspected the BOI parts they also and found within limits.','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11923,'35A-464','Saab AB','FITTING ASSY','','D522 73408 001 00','','A',3,'OWED-LTA-001','','A22516','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Is condition:Bushing sticks out 1,80 - 1,85 mm.\r\nShould be: Between 1,55-1,68mm according to drawing D5227340800100 and AIPS 01-02-019','Flange projection out of tolerance from the specification limit.|More sealant was applied in the flange of the bush, due to which the bush did not assembled properly and the bush protrusion was not measured.|Bush protrusion requirement isn\'t called in the drawing because of which both the operator and inspector didn\'t ensured the projection before the shipment.','Bushes are removed and reassembled to meet the requirements.','APS revised and training was given to both inspector and operators.','Effectiveness will be measured by 23_SEP_2019','C75372','2019-08-13','Dharani(Shankar)','Dharani(Shankar)','GLB430832','2019-06-11','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER END','yes','Misc','qas_sez(a)','no','','We have inspected our stock parts and are found okay. We also inspected the BOI parts they also and found within limits.','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11924,'18-385B','Magellan Aerospace Wrexham','NUT RING OUTER ','1616394-2/T3HR','D575 40038 202','','A',1,'162895','','94662','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','PART THICKNESS UNDER SIZE BY -0.07MM','1) Run out occurred in the face of the part.|2) Due to improper butting the face run-out occurred.|3) Improper scrap removal by the operator before loading the part.','|Instructed all the operators to ensure proper removal of scrap from the jaws before loading the part.','|operators are instructed to check the face run out before starting the production.','ca pa found ok','','2019-08-13','Raghavendra Rao(R)','Arun Kumar(R)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','07','no','Misc','Raghavendra Rao(R)','no','','|Immediately removed the part from the machine and cleaned the jaws completely and checked the previously completed parts and found ok.','E3456','qas|qas_sez|','2019-08-16|2019-08-31|','2019-08-31',NULL,NULL,NULL,NULL,NULL,NULL),(11925,'35-599','Saab AB','BEAM','814247','D5227338120400','NA','PART ISSUE C',1,'1600214688','','95668','','0000-00-00',NULL,'yes','yes','yes','','','','','','','running time part vibrated hence base thickness undersized due to applying lenth bolts','Base thickness under-size due to improper clamping|Bolts used to clamp the parts was longer then the required length.|The fixture used was new fixture and operator was not trained enough to select the proper bolt','|Supervisor clamped the part with correct length and continued the production, next part found okay.','|For every new fixture setting will be carried out by the supervisor and operator will be engage to carryout setting for new fixtures only after proper and sufficient training is completed on the same fixture.','Will be measured on 23-SEP-2019','','2019-08-14','pe_sez(a)','        Nagaraju P K ','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','5','','','','','','|Immediately  stopped the production and informed to the supervisor, tool and fixtures are checked, next part found okay','Z3456','pe|qas_sez|','2019-08-16|2019-08-20|','2019-08-20',NULL,NULL,NULL,NULL,NULL,NULL),(11926,'46-037B','Mahindra Aerostructures Pvt.Ltd','STRAP ','M0606A0 27741','D575-40872-200-01','NA','K02, BOM ISS J, ECN NG26090ST1KD02',5,'MAPL Extrusion LTA 2','','95752','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Wrong program run.','Wrong Part Loading|location pin Wrong Located in the Fixture|Due to multiple holes in Fixture','|New Fixture will be Manufactured.','|Dia of the Location pins will be varied',' checked the next part,CAPA FOUND OK','','2019-08-16','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','01','no','Misc','Prashanth Kumar(M)','no','','|Located the pin as per the MPS and then run the Program','E3456','qas|qas|','2019-08-20|2019-08-21|','2019-08-21',NULL,NULL,NULL,NULL,NULL,NULL),(11927,'18-686A','Magellan Aerospace Bournemouth','FORK END OUT BD','772840/271872','D575 41546 202','','B',1,'435247','','96046','','0000-00-00',NULL,'yes','yes','yes','','','','','','','program wrong selection so part reject ','PROGRAM SEARCHED BY WRONG BLOCK|MACHINE  GET RESET\r\n|ALARM FOUND IN MACHINE|ATC TIME OUT PROBLEM','|INDIVIDUAL PROGRAM RUN','|A NEW METHOD OF PROGRAM CALLING (EXT CALL) IS DONE','CA/PA FOUND OK','','2019-08-16','Dhananjaya(N)','        Ravi R','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','7','','','','','','|BY SEARCHING THE CORRECT BLOCK PROGRAM','E3456','pe|qas|qas|','2019-08-17|2019-08-20|2019-08-21|','2019-08-21',NULL,NULL,NULL,NULL,NULL,NULL),(11928,'35-443C','Saab AB','HINGE','YNRQ','D5227338820000','NA','B',1,'OWED-LTA-002','','93158','','0000-00-00',NULL,'yes','no','no','no','yes','yes','no','no','no','HOLE IN LINE MEASURED OUT. PLAIN PLUG GAUGE ANSWERING TIGHT ','Bore under size.|running time reamer got worn out and bore got under sized.|due to hardness of the material the reamer worn out and the operator did not identified the part with proper tag, hence it was identified during final inspection.','|Supervisor instructed all the operators to identify the deviated parts with proper identification tag','|Tool life for the tools used for hard materials will be closely monitored by supervisor.','Effectiveness will be measured on 30-SEP-2019','','2019-08-19','pe_sez(a)','Upendra N ,Ravi Kumar G.B,Nagaraju P K ,Chetan N,Anoop B Divekar,Ananda M,','','0000-00-00','HOLE IN LINE MEASURED OUT. PLAIN PLUG GAUGE ANSWERING TIGHT ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','','FI','yes','a51nx-03','qas_sez(a)','no','','|Immediately changed the reamer and continued the production.','Z3456','qas_sez|','2019-08-29|','2019-08-29',NULL,NULL,NULL,NULL,NULL,NULL),(11929,'56-020A','GKN Aerospace Orangeburg','SUPPORT ANGLE, UPR','662204','119A1440-608','NA','PSDL REV C',1,'LTA GKN ORANGEBURG W','','95471','','0000-00-00',NULL,'yes','no','no','no','yes','yes','no','no','no','profile point out of tolerance','Due to thickness oversize the profile point was measured out of tolerance.|Due to worn out tool the thickness was not achieved properly.|Operator did not ensured the cutting edges of the tool before starting the cycle.','|1) Changed the worn out tool with new tool with sharp cutting edge and continued the production.\r<br/>2) Reworked the part to achieve proper thickness re-measured the part and found the profile point with in the limit.','|Informed the operators to ensure the cutting edges of the re-used tools for every part before starting the cycle.','Similar parts machined verified and found ok.','','2019-08-20','pe_sez(a)','pe_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','','6','yes','Misc','Mahesh(N)','no','','|Immediately checked the previously completed parts and informed the supervisor and checked the cutting edges of the other tools in the machine.','Z3456','qas_sez|qas_sez|','2019-08-23|2019-08-28|','2019-08-28',NULL,NULL,NULL,NULL,NULL,NULL),(11930,'56-112','GKN Aerospace Orangeburg','LH UPPER ARROWHEAD','602679','119A1333-9603','NA','NIL',1,'A000049193','','95765','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','part thickness 0.1 under size and profile mismatch','WRONG UCS Selected While posting in the Program.|Due to Change in Program.|To Improve the Surface Finish Quality.','|New Program with the correct UCS has been given.','|Cross Verification will be donebefore Posting the Program. ','CA/PA FOUND OK.','','2019-08-20','Ramesh(Poojary)','Siddaramappa()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Narayanappa(G)','no','','|Continued the production with earlier Proved program.','E3456','qas|','2019-08-21|','2019-08-21',NULL,NULL,NULL,NULL,NULL,NULL),(11931,'35-681','Saab AB','LATCH FORK','YMS4','D5227348920600','NA','PART ISSUE D',1,'OWED-LTA-003','','93060','','0000-00-00',NULL,'yes','no','no','no','yes','yes','no','no','no','TOOL DIG MARK ON THE PART ','1.DIA 8Ballnose broken while running in roughing program|2.up to 3mm stock distributed on 2nd su roughing |3.while removing in material 3mm stock dia 8Ballnose will be broken ','|\r<br/>1.while running dia 8 ball nose care will be taken ','|1.Re roughing program taken and stabilize the process ','\r\nnext part production found ok ','','2019-08-20','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','TOOL DIG MARK ON THE PART ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','Misc','qas(qas)','no','','|.immediately stop the program and check the previous running part,all parts found OK ','E3456','qas|','2019-08-26|','2019-08-26',NULL,NULL,NULL,NULL,NULL,NULL),(11932,'51-148','THE BOEING COMPANY','UPR SKIN COVER','R6J06/153800','312Z3121-501','NA','NIL',1,'BOEING 001X','','84929','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','yes','The part is incorrectly part marked as 312Z3121-501 S/B 312Z3122-501 per BAC5307 in detail part\r\nrequirements(CODE M).','1) Wrong part marking done on part|2) Identification of similar parts was not done.|3) method used for identifying similar looking parts was not adequate.','|Sent the parts back to supplier and requested to correct the part marking.','|Part marking identification fixtures are designed and put to use to identify similar looking parts.','next batches marked are verified and found ok.','C74649','2019-08-20','Bharath(Kumar)','','CA1565413-00','2019-04-03','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','DN52319','Cust End','yes','Misc','Dharani(Shankar)','no','','|Checked all the similar parts in FG and no similar defects identified.','Z3456','qas_sez|','2019-11-28|','2019-11-28','0000-00-00','0000-00-00','0000-00-00','','',''),(11933,'35-597','Saab AB','CORNER','565567','D5227338620200','NA','PART ISSUE B',1,'OWED-LTA-001','','92009','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Running time tool broken. ','1.DIA 8Ballnose broken while running in roughing program							\r\n|2.up to 3mm stock distributed on 2nd su roughing 							\r\n|3.while removing in material 3mm stock dia 8Ballnose will be broken 							\r\n','|1.while running dia 8 ball nose care will be taken 							\r<br/>','|1.Re roughing program taken and stabilize the process 							\r<br/>','','','2019-08-20','Gurukiran S(M)','Manohara(M)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','05','no','Misc','Gurukiran S(M)','no','','|1.immediately stop the program and check the previous running part,all parts found OK 							\r\n','E3456','pe|qas|','2019-08-21|2019-08-26|','2019-08-26',NULL,NULL,NULL,NULL,NULL,NULL),(11934,'35-598','Saab AB','CORNER','565570','D5227338620300','NA','PART ISSUE B',1,'OWED-LTA-001','','93165','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Running time tool broken ','1.DIA 8Ballnose broken while running in roughing program|2.up to 3mm stock distributed on 2nd su roughing |3.while removing in material 3mm stock dia 8Ballnose will be broken ','|1.while running dia 8 ball nose care will be taken ','|1.Re roughing program taken and stabilize the process','next batch production found ok','','2019-08-20','Gurukiran S(M)','Govindraju(NR)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','5','no','Misc','Gurukiran S(M)','no','','|1.immediately stop the program and check the previous running part,all parts found OK ','E3456','pe|qas|','2019-08-21|2019-08-26|','2019-08-26',NULL,NULL,NULL,NULL,NULL,NULL),(11935,'47-128A','GKN Aerospace Filton','HINGE POST NO. 4','9753201','F5755106220203','NA','PART ISSUE D',1,'GS68-LTA-1-2018','','96859','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','profile unclear and not achieved as per the drawing requirement.','1) Due to Improper loading of part the profile was not achieved properly.|2) Fool proofing of fixture was not done by the engineering team.|3) 8Dia. location pin was provided in both the holes because of which the part got loaded in the in the opposite direction.|4) The process was changed because of customer complaint and the new fixture was issued to production.','|Rejected the part and requested the Engineering team to provide new fixture with proper fool proofing and clear instructions to how to load the part.','|Fool proofing of the fixtures will be verified by senior engineer before using in the production.','CAPC FOUND OK','','2019-08-20','Ramesh(Poojary)','Ramesh(Poojary)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','3','no','Misc','Subramanya L(Naik)','no','','|Delta FAIR part production stopped and informed the production supervisor and engineering team.','E3456','qas|qas|qas|','2019-08-28|2019-08-31|2019-09-04|','2019-09-04',NULL,NULL,NULL,NULL,NULL,NULL),(11936,'51-065','THE BOEING COMPANY','CRANK','72391/01','253W3150-2','NA','PSDL REV A',1,'BOEING 001M','','91826','','0000-00-00',NULL,'yes','no','yes','no','yes','no','no','no','no','PART BORE RUNNING TIME POWER CUT SO PART DIG MARK','dig mark observed on the corner radius.|Part running time power cut, so dig mark formed on the part.','|Power supplied from the backup generator and production continued.','|UPS capacity is increased to withstand power fluctuation.','increase of UPS capacity verified and found okay','','2019-08-21','pe_sez(a)','NataRaj.CV()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','NataRaj.CV()','no','','|Checked all the parts loaded in the machine and found okay.','Z3456','qas_sez|','2019-08-28|','2019-08-28',NULL,NULL,NULL,NULL,NULL,NULL),(11937,'56-008','GKN Aerospace Orangeburg','SPLICE PLATE AFT UPR','8-17-07731/26462','119A1213-608','NA','PSDL REV-',1,'LTA GKN 737 Winglet','','94721','','0000-00-00',NULL,'yes','no','no','no','yes','yes','no','no','no','Thickness u/s & profile out of spec','Profile measured under size due to undersized thickness.|Due to improper clamping of part the thickness measured under size.|Due to bend in the RM the operator did not ensured complete butting of part to the fixture before starting the cycle.|Due to improper storage condition of RM bend observed on the part.','|Informed the operator to ensure proper clamping using feeler gauge before starting the cycle.','|Informed the stores personnel and the RM supplier to ensure proper storage of parts to avoid similar deformation.','Next batches produced verified and found ok.','','2019-08-21','pe_sez(a)','pe_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','6','no','Misc','Mahesh(N)','no','','|Immediately stopped the machine and checked the previously completed parts and remaining RM and segregated the deformed RM.','Z3456','qas_sez|','2019-10-10|','2019-10-10',NULL,NULL,NULL,NULL,NULL,NULL),(11938,'35A-353A','Saab AB','LIFT PIN HOUSING FWD','','423Z1124-5-52','','1',1,'1600204275','','A12054','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Bore Over Size','','','','','','2019-08-22','qas_sez(a)','qas_sez(a)','','0000-00-00','NC Created','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','no','yes','no','Assembly','','FI','no','Misc','qas_sez(a)','no','L05627|BACB28AP20Z253','','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11939,'35-531A','Saab AB','SHAFT LATCH','C91277 SEQC','D5227349020200','NA','PART ISSUE C',1,'OWED-LTA-002','','95154','','0000-00-00',NULL,'yes','no','no','no','yes','yes','no','no','no','OD MEASURED MINUS 0.027 MM . MINIMUM VALUE IS 18.767 MM MEASURED VALUE IS 18.740 ','1)OD Undersized -0.027mm beyond drawing limit.|2)OD undersized during the re-pass operation as the re-pass ran twice.|3)Re-pass ran twice with same 0.027mm wear offset as the operator provided +0.3mm wear offset during the insert change|4)To maintain stock in the ID after the insert change the operator provided -0.2mm in the initial stage and after measuring the diameter he provided -0.15mm to remove the stock and finish to the drawing requirement during this time the re-pass operation was carried out and resulted in diameter was undersized.|5)Operator was unaware that the program for OD runs twice with different stock levels to achieve finish in the final operation.','|Changed the wear offset from +0.2mm to +0.1mm in the next part and after the completion changed the offset to -0.02mm according to the program(after considering both the pass) and found the next part OK. ','|Informed all the operator to check the relevant features after the insert change and provide of the offset accordingly with proper guidance from the supervisor or senior operators. ','CA/PA Found ok. ','','2019-08-23','Dinakar K()','Thaveni D M ,','','0000-00-00','OD MEASURED MINUS 0.027 MM . MINIMUM VALUE IS 18.767 MM MEASURED VALUE IS 18.740 ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','a51nx-02','qas_sez(a)','no','','|Immediately stopped the machine and changed the wear offset and continued the production on the next part. ','Z3456','qas|','2019-08-31|','2019-08-31',NULL,NULL,NULL,NULL,NULL,NULL),(11940,'35-531A','Saab AB','SHAFT LATCH','C93417','D5227349020200','NA','PART ISSUE C',2,'OWED-LTA-002','','95161','','0000-00-00',NULL,'yes','no','no','no','yes','yes','no','no','no','OD Under size by 0.05 to 0.17mm.','1)OD Undersized -0.015mm beyond drawing limit.|2)OD undersized during the re-pass operation as the re-pass ran twice.|3)Re-pass ran twice with same 0.05 to 0.17mm wear offset as the operator provided +0.3mm wear offset during the insert change|4)To maintain stock in the ID after the insert change the operator provided -0.2mm in the initial stage and after measuring the diameter he provided -0.15mm to remove the stock and finish to the drawing requirement during this time the re-pass operation was carried out and resulted in diameter was undersized.|5)Operator was unaware that the program for OD runs twice with different stock levels to achieve finish in the final operation.','|Changed the wear offset from +0.2mm to +0.1mm in the next part and after the completion changed the offset to -0.02mm according to the program(after considering both the pass) and found the next part OK. ','|Informed all the operator to check the relevant features after the insert change and provide of the offset accordingly with proper guidance from the supervisor or senior operators. \r<br/>','CA/PA Found ok','','2019-08-23','Dinakar K()','Vishwanatha M,Thaveni D M ,Shashikumar Y S,Purushothamma C,Purushothama R,Manu K,Manu ,HariPrasad ,Dhanush J.K,Ajith Kumar K ,','','0000-00-00','1. OD UNCLEAR DENT MARK OBSERVED ON THE PART\r\n2. OD MEASURED 0.017 MM MINUS MINIMUM VALUE IS 18.767 MM MEASURED VALUE IS 18.750MM','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','200MY-01','qas_sez(a)','no','','|\r\nImmediately stopped the machine and changed the wear offset and continued the production on the next part. \r\n','Z3456','qas|','2019-08-31|','2019-08-31',NULL,NULL,NULL,NULL,NULL,NULL);
INSERT INTO `nc4qa` VALUES (11941,'18A-434A','Magellan Aerospace Wrexham','STRUT ASSEMBLY','','D321 40203 002 01','','S',5,'190631','API173854','K28913','','0000-00-00',NULL,'no','yes','yes','no','no','no','yes','no','no','During assembly process plunger was got loosened.','1. After application of loctite-270, endcap was not fully tightened |2. Due to that improper tightening of the endcap part assembly was got loosened. |3. Due to low handling time of Loctite-270 the End cap got fixed before completing the assembly operation completely.','|The parts assembly process carry individually, their is no allowable for batch quantity loctite-270 application which performs individual part itself.','|The parts assembly process carry individually, their is no allowable for batch quantity loctite-270 application which performs individual part itself.','CAPA Found ok','','2019-08-23','Phaniraj(G)','Phaniraj(G)','','0000-00-00','Parts rejected from API W/O API173854','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Assembly','','02','no','Misc','Phaniraj(G)','no','93391|D321','|Remaining parts in WIP found OK and the operation to be carry individual parts itself, due to that short time process loctite applied endcap was assembled with part correctly','E3456','qas_sez|qas_sez|','2019-08-26|2019-08-26|','2019-08-26',NULL,NULL,NULL,NULL,NULL,NULL),(11942,'18-685A','Magellan Aerospace Bournemouth','FORK END OUT BD','1710149-1/ZLE9','D575 41546 200','','B',1,'435247','','96056','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','While Thread inspection by using Thread Gauge(0.5-20UNJF-3A) on Final Inspection the gauge was locked during reverse direction.','1. During final inspection process gauge was locked with part|2. While checking the gauge with part go gauge entered freely then removing process which was locked with part |3. Hanging burr was locked with gauge and part due to that locked tightly and can\'t able to remove the gauge with part','|During inspection process the wire cut gauges(relief slots) to be use to avoid the burrs locking in gauge and part','|During machining itself the burrs to be remove','Gauges foumd ok.','','2019-08-23','Nandishkumar(D.K.)','Shivaraj R,Ravi R,Raghavendra P,Mohan Trishul D P,Mallikarjuna D,KRISHNAMURTHY N,Dinakar K,dharshan d,Arun Kumar R,','','0000-00-00','NC CREATION','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','DX200-4','Narasimha Murthy(R)','no','','The remaining parts ensured free of FOD and checked remaining parts via another gauge parts are found OK. ','E3456','qas|qas|','2019-09-18|2019-09-30|','2019-09-30',NULL,NULL,NULL,NULL,NULL,NULL),(11943,'35-196A','Saab AB','AICD CENTERING_SHEAR GUID','51650-3RAA1','423Z1465-2','','--A',1,'Forecast po for B787','','90586','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','WIDTH MEASURED UNDER SIZE AFTER REWORK . MINIMUM VALUE IS 3.48MM MEASURED VALUE IS 3.22 MM TO 3.28MM ','WIDTH MEASURED UNDER SIZE AFTER REWORK.|Step observed on the chamfer land.|Worn out champer tool caused a step formation on the champer land.','|Operators are informed to check the tool for worn out edges while loading the part.','|Informed all operators to ensure sharp edges of the champer tool before loading the part.','Effectiveness will be measured on 30_SEP_2019','','2019-08-24','pe_sez(a)','Pradeep B.D,Manu ,HariPrasad ,Dhanush J.K,','','0000-00-00','WIDTH MEASURED UNDER SIZE AFTER REWORK . MINIMUM VALUE IS 3.48MM MEASURED VALUE IS 3.22 MM TO 3.28MM ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','a51nx-06','qas_sez(a)','no','','|All remaining parts are checked and parts with step problem are reworked.','Z3456','qas_sez|','2019-08-28|','2019-08-28',NULL,NULL,NULL,NULL,NULL,NULL),(11944,'35-600A','Saab AB','FRAME','814232','D5227338520400','NA','PART ISSUE D',1,'OWED-LTA-001','','94942','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','33.353H7 Bore over size by 0.2MM.','Ø33.353 H7 bore found 0.2 oversize|Reamer found run out of 0.08-0.1|found 0.08-0.1 Runout in Reamer shank |Found 0.06-0.07 runout in Tool holder|Found 0.05-0.06 play in machine Spindle','|There was a un consistant play in spindle, \r<br/>spindle dismantled and send to service,  \r<br/>After the spindle bearing replacement, reassembled to machine,  \r<br/>spindle Run-out within 2 micron, Reamer within 4 micron.','|INFORM SERVICE PERSON TO REPLACE SEALED BEARING WITH OPEN BEARING',' CA/PA found okay','','2019-08-24','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','NC Created.','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','Misc','Nagendra(SN)','no','','|Immdiatly stopped , previous part found okay','E3456','qas|','2019-08-29|','2019-08-29',NULL,NULL,NULL,NULL,NULL,NULL),(11945,'35-666','Saab AB','LEVER 2   ','4210601','D5227280620200','NA','PART ISSUE B',1,'1600277523','','95676','','0000-00-00',NULL,'yes','no','no','no','yes','yes','no','no','no','Tool Holder rubbed on the part so dig mark formed','1) Running time tool holder rubbed over the part top face.|2) Tool length selected by the operator was less than the required length.|3) During the production time the previously used tool was causing chatter marks on the part due to which the operator selected the tool with short length.|4) Operator did not cross checked the tool length achieved with the requirement due to which the tool holder rubbed on the part and caused the rejection','|Comment added in the program to instruct operator to ensure proper tool length before starting the production.','|Check list will be implemented for tool change and new setup which will be filled by the operator and validated by Supervisor before starting the production.','CA/PA FOUND OK','','2019-08-26','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','TOOL DIG MARK ON THE PART','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','Misc','qas(qas)','no','','|Immediately stopped the machine and adjusted the tool to achieve proper tool length.','E3456','qas|qas|','2019-09-05|2019-09-18|','2019-09-18',NULL,NULL,NULL,NULL,NULL,NULL),(11946,'35-601A','Saab AB','FRAME','814232','D5227338520600','NA','PART ISSUE D',1,'OWED-LTA-005','','93183','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Tool dig marks observed.','4mm Thickness Over mill near 27H7| Program searched done at wrong Block|\"Z\" axis not lifted to safety limit once machine ON|Power Failure','|After Machine ON , \"Z \" axis to be lifted to safety distance \"','|while power failure occur.  program to be run from starting instead of block search\r<br/>\r<br/> (We are attempting to implement a new method of program calling (EXT CALL) checking with OEM )','NEXT PART FOUND OK','','2019-08-27','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','DN62227','FI','no','Misc','Nagendra(SN)','no','','|Immdiatly machine stopped , ','E3456','qas|','2019-08-30|','2019-08-30',NULL,NULL,NULL,NULL,NULL,NULL),(11947,'51A-076','THE BOEING COMPANY','ASSY - FTG, AFT FAIRING F','','112U7625-11','','PSDL REV-',1,'BOEING 001V','','K23719','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','drilling operation done on the opposite face.(dia 0.2532 to 0.2605 inch)','','','','','','2019-08-27','pe_sez(a)','pe_sez(a)','','0000-00-00','NC RAISED','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','no','yes','no','Assembly','','IN PROCESS','no','Misc','qas_sez(a)','no','87644|112U7625-13','','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11948,'51A-076','THE BOEING COMPANY','ASSY - FTG, AFT FAIRING F','','112U7625-11','','PSDL REV-',6,'BOEING 001V','','K23719','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','drilling operation done on the opposite face.(dia 0.2532 to 0.2605 inch) IN THE DETAIL PARTS SO ASSEMBLED BUSH REJECTED DUE TO MACHINING DONE IN THE BUSH.','','','','','','2019-08-27','pe_sez(a)','pe_sez(a)','','0000-00-00','NC RAISED ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','no','yes','no','Assembly','','IN PROCESS','no','Misc','qas_sez(a)','no','M03718|BACB28AT07B034Z','','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11949,'18-742A','Magellan Aerospace Wrexham','STRIP','63026/02','F57252299204','NA','A',1,'190638','','95467','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Countersunk diameter over size by 3mm. 		','1) Countersink diameter was not measured as per the requirement.							\r\n|2) The diameter of the countersink was .4.45 to 4.65mm greater than the drawing requirement as the tool was stepping down beyond the requirement.			\r\n|3) operator did not left stock for the countersink operation and did not ensured proper dept.			\r\n|4) operator was not aware of the standard method practiced for forming the countersink.			','|1) Supervisor provided sufficient stock for forming the countersink in the next part and found ok.	\r<br/>2) Informed all the operator\'s to provide sufficient stock for the Countersink. 	','|Instruction given to all the operators to perform the formation of the CSK step by step so that the too does not drops over the part and cause oversize. ','CAPA FOUND OK','','2019-08-28','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','1','no','Misc','Dhananjaya(N)','no','','|Immediately stopped the machine and checked the previously completed parts and found ok. 				','E3456','pe|qas_sez|','2019-08-31|2019-08-31|','2019-08-31',NULL,NULL,NULL,NULL,NULL,NULL),(11950,'35A-474A','Saab AB','FRAME ASSY','','D5227338400000','','B',1,'OWED-LTA-001','','A22221','','0000-00-00',NULL,'no','no','no','no','no','yes','yes','yes','no','Deep corrosion pit marks observed on the entire part during anodysing','corrosion pits observed on the part|part were returned from customer for bend rework, after rework the parts were not protected properly with corrosion preventive agents.|less amount of corrosion prevention oil was applied for the part before sending to treatment.|lead time between the operations was less calculated ','|informed all the packing persons to apply sufficient corrosion restrictive oil before shipping the parts','|informed all the packing persons to apply sufficient corrosion restrictive oil before shipping the parts','Next batch shipments are monitored and found okay.','','2019-08-28','pe_sez(a)','pe_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Assembly','','FI','no','Misc','Dharani(Shankar)','no','','|checked all the parts in transit and applied sufficient corrosion restrictive oil to the parts which were under packing ','Z3456','qas_sez|','2019-08-29|','2019-08-29',NULL,NULL,NULL,NULL,NULL,NULL),(11951,'18-090A','Magellan Aerospace(Polska) Sp','BUSH','CD707781/05307A','PID278 50164 200','','A',1,'104569','','96805','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Running time Boring tool insert broken, dig mark formed on the part. ','Dig marks found on the part.|Running time boring tool insert broken.|Insert was worn outed and operator doesn\'t observed it while loading the part.','|Jaws are inspected, insert changed and setting was redone.','|It is informed to the operators to check the inserts while loading the part.','Effectiveness will be measured on 30_SEP_2019','','2019-08-28','Narasimha Murthy (K G)','Vishwanatha M,Sachin N M,Ranjith N D,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','3','no','100MY-02','Narasimha Murthy (K G)','no','','|Immediately stopped the production and informed the supervisor. Checked the other parts and found okay. ','Z3456','qas_sez|','2019-08-28|','2019-08-28',NULL,NULL,NULL,NULL,NULL,NULL),(11952,'35-601A','Saab AB','FRAME','814232','D5227338520600','NA','PART ISSUE D',1,'OWED-LTA-005','','93183','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Tool dig marks observed.','\r\n4mm Thickness Overmill near 27H7\r\n\r\n\r\n|.Program searched done at wrong Block | \"Z\" axis not lifted to safety limit once machine ON| Power Failure','After Machine ON , \"Z \" axis to be lifted to safety distance \"','while power failure occur.  program to be run from starting instead of block search\r<br/>\r<br/> (We are attempting to implement a new method of program calling (EXT CALL) checking with OEM )','Next part found correct. ','','2019-08-30','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','DN62227','FI','no','Misc','Nagendra(SN)','no','','Immediately machine stopped , ','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11953,'51-187','THE BOEING COMPANY','BRACKET - AFT LAIRCM COOL','177730B9','217T4105-762','NA','NIL',1,'BOEING 001Z','','96132','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','0.167 UNF TAP BROKEN WHEN MACHINE RUNNING TIME','Due to excess stock inside the hole the tap broken.|The required stock was not achieved after the drilling was carried out with the use of drilling tool.|The drill bit used was blunt after continuous production.','|Changed the blunt drilling tool with new tool and replaced the tap and continued the production.','|Instructed all the operators to ensure the hole diameter of the part before starting the threading cycle, also instructed to strictly monitor the tool life of the tools and to ensure the cutting edges of the tools once in every part after 20Parts are continuously produced.','Tool life monitoring was verified for the next batches produced and no defects found.','','2019-08-30','Nagaraju P K()','','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','','5','yes','a51nx-01','pe_sez(a)','no','','|Immediately stopped the machine and re-ensured the thread formation of the previously completed tools, also ensured the diameter of the drilling tool used and was according to the requirement.','Z3456','qas_sez|','2019-11-30|','2019-11-30','0000-00-00','0000-00-00','0000-00-00','','',''),(11954,'35-681','Saab AB','LATCH FORK','YMS4','D5227348920600','NA','PART ISSUE D',6,'OWED-LTA-003','','94463','','0000-00-00',NULL,'yes','no','no','no','yes','yes','no','no','no',' TOOL DIG MARKS OBSERVED ON THE PARTS & BORE OVER SIZE MEASURED \r\nNOMINAL IS 18.8 E7 MM MEASURED 18.97 MM TO 19 MM','\r\nWhy 1. Dim 28 found dig Mark\r\nWhy 2. during machining Ø12xR2 Bull cutter broken\r\nWhy 3. New Tool trail under process \r\nWhy 4. old tool life is 15Nos |Why 1. dim 26mm surface dig mark found during Ø8.1H7 hole machining\r\nWhy 2. Ø5 endmill found blunt  \r\nWhy 3. Replace the blunt end mill with new Ø5 End mill \r\nWhy 4. during the replacing the new end mill wrong work offset used|Why 1. Ø18.8 E7 bore oversize by 0.16\r\nWhy 2. during boring insert found Blunt  \r\nWhy 3. Replace the blunt insert with new one \r\nWhy 4. during the replacing the new insert wrong insert used\r\nWhy 5. R0.2 insert used insted of R0.4 |Why 1. Ø18.8 E7 bore oversize\r\nWhy 2. During U-drill Process machine spindle overload \r\nWhy 3. found U-drill broken ( U-drill life only for 3 nos) |\r\nWhy 1. dim 51 thickness undersize\r\nWhy 2. during machining Ø16 cutter ,insert loosen\r\nWhy 3. found M2.5 screw loose\r\nWhy 4. holder insert sitting area worn out and damage\r\n\r\nWhy 1. Ø18.8 E7 bore rough & unclear at one end\r\nWhy 2. During U-drill process one insert fly away \r\nWhy 3. Found insert screw broken\r\nWhy 4. hope screw loosen','|1.Old Ø12xR2 bull cutter used\r<br/>2.Select correct work offset, and take tool height and re-confirm one more time\r<br/>3.before replacing the boring insert cross check what insert used present and what spec to be replaced,\r<br/>4.New U drill used\r<br/>5.Ø16 insert cutter holder replaced with new one\r<br/>','|\r<br/>1)Before Take actual tool Trail Ensure with supplier about tool life and its evidence,  \r<br/>2)a. after tool height , Call same tool in the tool change menu, then obeserve the value in \"z\" axis is to be Zerro, \r<br/>b. Before open the feedrate during machining re confirm  in \"DIST TO GO\" screen in \"X\"Y\"Z axis\r<br/>3)traning provided to employees, after changing the whatever insert need set boring bar as per training .\r<br/>4)Change the U-drill dia from Ø18 to Ø17 and additional hole mill of Ø18 added\r<br/>5)New cutter replaced with old one .  Cutter life under monitoring\r<br/>6)Monitor U-drill screw after completion of every component , if found screw loosen replace with new U-drill  and record down the U-drill life .','CA/PA FOUND OK\r\nafter the training found OK\r\nafter replacing the new cutter. machining found OK.','','2019-08-31','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','TOOL DIG MARKS OBSERVED ON THE PARTS & BORE OVER SIZE MEASURED \r\nNOMINAL IS 18.8 E7 MM MEASURED 18.97 MM TO 19 MM','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','Misc','qas(qas)','no','','|Immdiatly stopped , previous part found okay, informed to continue untill final process','E3456','qas|','2019-10-14|','2019-10-14',NULL,NULL,NULL,NULL,NULL,NULL),(11955,'51A-066A','THE BOEING COMPANY','STRUT SUPPORT ASSY','','113T1958-7','','PSDL REV A',4,'BOEING 001AA','','A28981','','0000-00-00',NULL,'no','yes','yes','no','no','no','yes','no','no','DIA .3750 BUSH COMING OUT SIDE FROM PART WHILE DOING REAMING OPERATION.','The clearance between the bore and the part was high.|The part was machined to the maximum limit of the drawing and the bush was machined to the mean of the requirement.|Assembly requirement was not analyzed during the part processing time.|\r\n','|Checked the bush and bore diameter before assembly.','|Informed the engineering team to process the part bore to the mean value of the drawing dimension to avoid similar rejections.','CA PA found ok.','','2019-08-31','pe_sez(a)','pe_sez(a)','','0000-00-00','NC RAISED','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Assembly','','IN PROCESS','no','Misc','assembly(assembly)','no','M03806|BACB28AT06B011Z','|Checked the bore diameter of all the completed part and the outer diameter of all the bushes and found ok.','E3456','qas|','2019-09-30|','2019-09-30',NULL,NULL,NULL,NULL,NULL,NULL),(11956,'18-284A','Magellan Aerospace Bournemouth',' 	SPINDLE FOR CLACK ALVES','1649863-3/XCQ6','PIA281-40019-200','','A',3,'423253','','90279','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','OD diameter undersized 0.03 to 0.23mm\r\nRequired dimension is 4.63+0.1  but measures 4.4 to 4.6','1) Outer diameter measured undersize to the drawing requirement.|2) Due to run out on the part the diameter got undersized in the finishing operation.|3) Due to improper jaws boring the run out was formed on the part. |4) Operator used worn out insert during the jaws boring operation and dis not checked the run out before starting the production.','|Re bored  the jaws and ensured the run out and continued the production.','|instructed all the operators to use proper insert while boring the jaws and also instructed to ensure run out before starting the cycle.','CA/PA FOUND OK','','2019-08-31','Dinakar(K)','Yogeesha R,Ravi K,Kailash Patil,','','0000-00-00','NC CREATION','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','FI','no','Fitting','Narasimha Murthy(R)','no','','|Immediately stopped the machine and checked the run out of the   Jaws and informed the supervisor.','E3456','qas|qas|','2019-09-05|2019-09-18|','2019-09-18',NULL,NULL,NULL,NULL,NULL,NULL),(11957,'56-005','GKN Aerospace Orangeburg','SPLICE PLATE FWD UPR','8-17-07731/26462','119A1213-603','NA','PSDL REV -',1,'LTA GKN 737 Winglet','','94718','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Rib thickness under size.','Rib thickness under size.|work offset wrong.|while setting the job, new operator does not cross checked the offset and initiated the work cycle without informing the senior operator.','|Inspected tool and spindle, setting is redone by the senior operator and next part found okay.','|In-front of the machine training was given for the new operator on the fixtures 56-104, 56-096, 56-100 and 56-005 for setting and taking tool offset, work offset, straight dialing. after that operator shown all the settings independently to the supervisor. ','Effectiveness will be measured on 23_Sep_2019','','2019-08-31','pe_sez(a)','Rajesha A.R,Pradeep B.D,Maruthi  D R ,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','3','no','Slim3n-5AHT-2','pe_sez(a)','no','','|Immediately stopped the machine and informed the senior operator and supervisor. ','Z3456','qas_sez|','2019-08-31|','2019-08-31',NULL,NULL,NULL,NULL,NULL,NULL),(11958,'18-761A','Magellan Aerospace Wrexham','BRACKET','521506A','D57952066201','NA','A',5,'195321','','96177','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Thickness under size by 0.02 to 0.04',' 1) Thickness of the base got undersized due to excess abrasion.|2) The fitting operator did not ensured the thickness of the part during polishing of the base.|3) Operator was not aware of what rework need to be exactly done to the part and he polished the part without measuring the thickness.|4) Due to miss communication between the operator and the supervisor the operator polished the surface of all the parts instead of reworking the dent in one part.','|Informed all the fitting operators to properly co-ordinate with the supervisors and after getting complete clarification from the supervisor start the fitting work.','|New (or) FAIR parts re work will be carried out only in the presence of supervisor or related process engineer.','CA PA found ok.','','2019-08-31','Suresh Kumar(O)','Suresh Kumar(O)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','5','no','Misc','Suresh Kumar(O)','no','','|Checked all part reworked by the operator and similar part with W/O 96180 was reworked by the same operator and found to be rejected.','Z3456','qas_sez|','2019-11-11|','2019-11-11',NULL,NULL,NULL,NULL,NULL,NULL),(11959,'18-764A','Magellan Aerospace Wrexham','BRACKET','521506A','D57952067201','NA','A',6,'195321','','96180','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Thickness under by 0.02mm to 0.05mm','1)Thickness of the base got undersized due to excess abrasion.|2)The fitting operator did not ensured the thickness of the part during polishing of the base.|3)Operator was not aware of what rework need to be exactly done to the part and he polished the part without measuring the thickness.|4)Due to miss communication between the operator and the supervisor the operator polished the surface of all the parts instead of reworking the dent in one part.','|Informed all the fitting operators to properly co-ordinate with the supervisors and after getting complete clarification from the supervisor start the fitting work.','|New (or) FAIR parts re work will be carried out only in the presence of supervisor or related process engineer.','CA PA found ok.','','2019-08-31','Suresh Kumar(O)','Suresh Kumar(O)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','5','no','Misc','Suresh Kumar(O)','no','','|Checked all part reworked by the operator and similar part with W/O 96180 was reworked by the same operator and found to be rejected.','Z3456','qas_sez|','2019-11-11|','2019-11-11',NULL,NULL,NULL,NULL,NULL,NULL),(11960,'35-149','Saab AB','CED_BS_HINGE_FTG-AFT','272059B7','425Z0311-8','7050 - T7451 ALUMINU','--A',1,'Forecast po for B787','','95716','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','BORE OVERSIZED BY 0.015 MM.','while boring bar setting time 20 microns correction was given but the tool was taken 45 microns cut.  |boring bar shaft was tight. ','|1) checked the boring bar for next part \r<br/>2) cross checked the boring bar with proving on the other material and the part was found ok. ','|1) boring bar will send to service \r<br/>2) will cross check the boring bar after service.',' Boring bar service evidence ok','','2019-08-31','Subramanya L(Naik)','Eranna K,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','3','no','MakinoF5-4','Subramanya L(Naik)','no','','|checked the boring bar & replaced the tool.','E3456','qas|qas|','2019-09-16|2019-09-19|','2019-09-19',NULL,NULL,NULL,NULL,NULL,NULL),(11961,'35-183C','Saab AB','HOUSING, EDGE','739694','423Z1121-6-02','NA','--B',1,'LTA Forecast B787 De','','97103','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Top face dig up to 3mm','Tool overhang length varied|Wrong tool called.|Same tool with different flutes were present.','|Tools loaded will be checked by operator & will be approved by the supervisor along with the data list. ','|\"M00\" will be added within the program saying the required message(Long & short flutes tool) respectively.','NEXT PART CHECKED FOUND PART OK','','2019-09-03','Dinesh kulal()','Vinod.K(V)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','07','no','Misc','Vinod.K(V)','no','','|Immediately stopped machine & informed the supervisor. Tool with correct flute length was called and next parts found ok.','A3456','qas|qas|','2019-09-03|2019-09-18|','2019-09-18',NULL,NULL,NULL,NULL,NULL,NULL),(11962,'51-088A','THE BOEING COMPANY','BEARING PLATE','58594-4RD1','69B12286-2','NA','PSDL REV -',1,'BOEING AC001','','95131','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Bore diameter oversize.','Bore diameter oversize.|wrong entry of D-value in the program.|During setting, operator changed 3 D-values and left another 3 as it is, due to which bore diameter got oversize.','|supervisor corrected the D-values, continued the production and next part found okay.\r<br/>Training is given for the operator In-front of machine regarding D-values, G41 and G42 codes.','|All the operators are instructed to inform seniors/supervisors while changing D-values in the program.','Effectiveness will be measured on next CRC program running by the same operator.','','2019-09-03','Lohith(K)','        Maruthi  D R ','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','03','','','','','','|Immediately  stopped the machine, informed to supervisor.','Z3456','pe|qas_sez|','2019-09-04|2019-09-10|','2019-09-10',NULL,NULL,NULL,NULL,NULL,NULL),(11963,'34-062A','Magellan Aerospace Winnipeg','GUIDE BLK DOOR PIN LATCH','273469','400-12746-1','NA','EM105092 Iss H,EM104765 Iss H',1,'C81597 Rev002','','96113','','0000-00-00',NULL,'yes','yes','yes','','','','','','','hole oblong.','Running time tool shank Rubbed the part top face|Tool length (Fluted) selected by the operator was less then the required length |during the Production time the previously used tool was causing  short tool use on the part due to which the operator selected tool short flute  ','|comment added in the Program to instructed operator to ensure proper Reamer flute length before start the cycle. ','|CRN wise separate box in provide.   ','NEXT PART FOUND OK','','2019-09-03','Dhananjaya(N)','        Dileep Kumar','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','05','','','','','','|immediately stop the mc change the Reamer  ','E3456','pe|pe|qas|qas|','2019-09-04|2019-09-06|2019-09-06|2019-09-10|','2019-09-10',NULL,NULL,NULL,NULL,NULL,NULL),(11964,'35A-518','Saab AB','ROD ASSY','','D522 73510 000 00','','A',1,'OWED-LTA-004','','A26640','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','We have found an issue with the breakaway torque for the spherical bearing in AS81935-1-4K. Today we are suspecting all assemblies including the AS81935-1-4K.\r\n\r\nAccording to M81935/1 Self-Lubricated Rod End Bearings the breakaway torque should be 0.5 – 6.0 in.-lbs (0.06 – 0.68 Nm). Non-conforming Rod Ends have one or two bearings with breakaway torque above 0.68 Nm.\r\n','1) The break away torque measured on the rod ends were not as per the customer requirement.|2) CIM was inspecting the bearings with bolt and nut through bearings and tightening with and and checked the torque.But at SAAB the bolt and nut was torque tightened to 6.3Nm before checking the breakaway torque of the bearing which i not as per the drawing requirement.|3) SAAB selection of Bearing for the assembly was not as per the SAAB higher assembly requirement.','|Informed the bearing supplier about the failure of the bearing during torque test and requested to inspect 100% before shipment.','|SAAB to analyze and revise the drawing according to their higher assembly requirement.','CA PA Found ok.','C80281','2019-09-04','Dharani(Shankar)','Dharani(Shankar)','OF-004027','2019-09-02','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER END','yes','Misc','qas_sez(a)','no','','|Checked the bearings to SAAB specific requirements and change the affected bearings.','Z3456','qas_sez|qas_sez|qas_sez|','2019-10-25|2019-11-12|2019-11-12|','2019-11-12',NULL,NULL,NULL,NULL,NULL,NULL),(11965,'56-006','GKN Aerospace Orangeburg','SPLICE PLATE FWD UPR','8-15-02597-2/27555','119A1213-604','NA','PSDL REV -',3,'LTA GKN 737 Winglet','','94975','','0000-00-00',NULL,'yes','no','no','no','no','yes','no','yes','no','Thickness u/s & profile out of spec','Profile measured under size due to undersized thickness.|Due to improper clamping of part the thickness measured under size.|Due to bend in the RM the operator did not ensured complete butting of part to the fixture before starting the cycle.|Due to improper storage condition of RM bend observed on the part.','|Informed the operator to ensure proper clamping using feeler gauge before starting the cycle.','|Informed the stores personnel and the RM supplier to ensure proper storage of parts to avoid similar deformation.','Next batches produced verified and found ok.','','2019-09-05','pe_sez(a)','Rajesha A.R,Pradeep B.D,Maruthi  D R ,Madhu Kumar N,Lingaraju S,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','','FI','yes','Slim3n-5AHT-2','Mahesh(N)','no','','|Immediately stopped the machine and checked the previously completed parts and remaining RM and segregated the deformed RM.','Z3456','qas_sez|','2019-10-10|','2019-10-10',NULL,NULL,NULL,NULL,NULL,NULL),(11966,'56-070','GKN Aerospace Orangeburg','CARGO NET BEAM','717005B3','475Z3603-187','NA','NIL',1,'A000047052','','97571','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','Holes are drilled in the wrong side of the part.','The position of holes drilled in the part are found to be in the opposite side of the part requirement.|Part loaded by the operator was in the wrong direction of fixture.|The information given in the M.P.S was wrong and due to that operator loaded the part in wrong direction.|While proving the FAIR part it is noticed that lactation pin diameters mentioned in the D00 format are in wrong direction but after that same information was not flow-downed into MPS.','|Next part are loaded in the right direction by using step pins and next produced parts found okay.','|MPS is corrected,ENG and PROD team are informed to ensure the proper information flow-down of any changes occurred/applied while proving the FAI part on priority.','Effectiveness will be measured in next batch production.','','2019-09-07','pe_sez(a)','Umesh B,Diwakar R.B.,Chethan Kumar M,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','9','no','i700-4','pe_sez(a)','no','','|Immediately stopped the production and informed to the supervisor.','Z3456','qas_sez|','2019-10-12|','2019-10-12',NULL,NULL,NULL,NULL,NULL,NULL),(11967,'35-600A','Saab AB','FRAME','521026C1','D5227338520400','NA','PART ISSUE D',1,'OWED-LTA-001','','97659','','0000-00-00',NULL,'yes','no','no','no','yes','yes','no','no','no','THICKNESS MEASURED UNDER SIZE 3.2 MM THICKNESS MEASURED 2.88 MM ','1) Due to excess bend on the part after roughing operation part lifted and resulted in thickness under-size	|2) During the final pass in finishing operation due to residual stress the part is getting lifted up.	|3) During aging time between the roughing and the finishing operation the material was not left in free condition (i.e. the materials were loaded one over the other).		','|Informed all the operators to leave the part in free condition during the aging process. 			','|Training provided to all the operators on site to avoid storage of parts one above the other during the aging operation.','CAPA FOUND OK','','2019-09-09','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','THICKNESS MEASURED UNDER SIZE 3.2 MM THICKNESS MEASURED 2.88 MM ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','Misc','qas(qas)','no','','|Immediately stopped the machine and arranged the material so that the parts are left in free condition. 	','E3456','qas|','2019-09-23|','2019-09-23',NULL,NULL,NULL,NULL,NULL,NULL),(11968,'35-600A','Saab AB','FRAME','521026C1','D5227338520400','NA','PART ISSUE D',1,'OWED-LTA-001','','97659','','0000-00-00',NULL,'yes','no','no','no','yes','yes','no','no','no','TOP RADIUS FILLET PROGRAM RUN WITH DIA8 END-MILL INSISTED OF DIA8 BALLNOSE ','dig mark observed on the part.			\r\n|dia 8 ball nose tool broken.				|material stock in radius.			|dia 8 flat tool was chipped out.			|used the regrinding dia 8 flat tool.		','|instruct to operator for check the tools before load the machine. 				','|stop the using of regrinding tools for pocket roughing & use the new dia 8 flat tool for next batch. 	','CAPA FOUND OK','','2019-09-09','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','TOP RADIUS FILLET PROGRAM RUN WITH DIA8 END-MILL INSISTED OF DIA8 BALLNOSE ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','Misc','qas(qas)','no','','|Immediately change the dia 8 flat tool & run the production. ','E3456','qas|','2019-09-23|','2019-09-23',NULL,NULL,NULL,NULL,NULL,NULL),(11969,'18-697A','Magellan Aerospace(Polska) Sp','BUSH','1693400-1ZEWQ','D278 50164 202','','A',1,'107446','','97450','','0000-00-00',NULL,'yes','no','yes','no','yes','no','no','no','no','OD DIG MARK','air pressure low so od dig mark|power fluctuating','|UPS maintenance team was called and the UPS was inspected and found ok.\r<br/>','|All the machines will be shifted from the power fluctuating source to the non power fluctuating source before 10-Sep-2019','CA/PA FOUND OK','','2019-09-10','Dinakar(K)','Sathish(G)','','0000-00-00','air pressure low so od dig mark   ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Sathish(G)','no','','|Immediately informed the supervisor and the maintenance team about the power failure and identified the rejected part with rejection tag\r\n','E3456','qas|qas|','2019-09-11|2019-09-18|','2019-09-18',NULL,NULL,NULL,NULL,NULL,NULL),(11970,'56-104','GKN Aerospace Orangeburg','CLOSEOUT - RIB, LWR, AFT','238285','119A1441-607','NA','PSDL REV -',1,'A000047470','','97107','','0000-00-00',NULL,'yes','','yes','','yes','','','','','MACHINE C AXIS PROBLEM. RIB THICKENS 1.524 BUT ITS ACHIEVING 1.24 UNDER SIZE BY 0.05   ','1) During running time the C axis of the machine rotation error occurred.|2) Due to vibration the C axis fixing bolt got loose and resulted in rotation problem.|3) Proper tightening of bolt with proper torque was not done during the machine installation by the machine supplier and the same was not ensured by CIM maintenance team.','|Machine supplier and CIM maintenance team verified the tightness of all the axis and gear bolts and tightened the bolts that were not meeting the required torque value.','|Informed the maintenance team to ensure proper tightening of bolts specially to the axis related bolts during new machine installation.','CA PA found ok.','','2019-09-11','Lohith(K)','        Somashekar ','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','3','','','','','','|Immediately stopped the machine and informed the supplier about the issue, checked the previously completed parts and found to be machined within acceptable limits.','Z3456','pe|qas_sez|','2019-09-12|2019-11-11|','2019-11-11',NULL,NULL,NULL,NULL,NULL,NULL),(11971,'18-209B','Magellan Aerospace Wrexham','BODY','M037950/27371','D321 40204 202','','D, ECN NR29999ST1KM15, NR29999ST2KF65, WQN DFB09775',4,'190631','','93355','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Thread flat so nogo answer,','1) Insert locking screw was not tightened.		\r\n|2) Operator hand tightened the screw with hand and went in search of the cutting player after getting the player he just corrected the wear offset and continued the production.	|3) Operator did not practiced to clamp the insert with align key and he did not checked the tightness of the insert.	|4) Operator got distracted and forgot to ensure the tightness if the insert.					','|Informed all the operators to check the tightness of the insert before continuing the production. 		','|informed the supervisors to monitor the operator until he practices to tighten the insert with align key alone. 	','CA PA FOUND OK','','2019-09-12','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','3','no','Misc','Dhananjaya(N)','no','','|Immediately stopped the machine and tightened the insert and re-took the work offset and continued the production. 	','E3456','pe|qas|','2019-09-18|2019-09-18|','2019-09-18',NULL,NULL,NULL,NULL,NULL,NULL),(11972,'55-021','Spirit AeroSystems Incorporated','WEDGE,TRAILING EDGE','716504B6','113A3511-604A','NA','PSDL REV -',1,'4501352392','','97594','','2019-09-13',NULL,'yes','yes','yes','no','no','no','no','no','no','part dig mark found on Side wall.','1) i-machining Running time tool broken and wall open-out. |2)Tool broken because of uncertainty of the tool.|3)Tool uncertainty is caused because of vibration induced by machining parameters.|4) Cutting parameters given during this particular operation was on the upper limit of the tool specification.|5) Factor of safety considered by the engineer was minimal.','|changed the broken tool with new tool retook the offset and continued the production as per senior operator guidance. ','|1) Engineering team need to reduce the cutting parameters and reissue the revised program.\r<br/>2) MPS need to be amended according to the revised program.','CA/PA Verified and found okay.','','2019-09-13','nagaraju(sez)','nagaraju(sez)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Manu()','no','','|Immediately stopped the machining and informed to senior operator and checked the previously completed parts and found okay.','Z3456','qas_sez|qas_sez|','2019-09-13|2019-09-20|','2019-09-20',NULL,NULL,NULL,NULL,NULL,NULL),(11973,'18-373B','Magellan Aerospace Bournemouth','GAMMA FITTINGS','28428487-H','NSA840020-050PF','','L',233,'435253','','94278','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','no','PRESSURE TEST FAILED AT CUSTOMER END','','','','','','2019-09-13','qas_sez(a)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','no','no','yes','Manufacture Only','','ONSITE','no','Misc','Dharani(Shankar)','yes','','','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11974,'51-164','THE BOEING COMPANY','FLANGE','20235105','349T2200-50','NA','PSDL REV J',1,'BOEING 001Z','','97564','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Profile out of requirement.','offset given while setting is wrong.|The program control used is mazatrol and the operator are not familiar with mazatrol control system, In ISO control system, They used to keep \"up\" in the program. this went wrong with mazatrol control system  and removed more material than the requirement.','|The problem is discussed with maztrol co. Instruction are taken from them regarding the working / control of offset in mazatrol control system, next part found okay.','|1) Alert message is displayed in shop floor to create the awareness.\r<br/>2) Training for the programming and control in mazatrol control system is planned.','Next batch parts found okay and effectiveness will be measured on 28-NOV-2019','','2019-09-13','Narasimha Murthy (K G)','Maruthi()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','07','no','Misc','Narasimha Murthy (K G)','no','','|Immediately stopped machining, informed to supervisor.','Z3456','qas_sez|qas_sez|qas_sez|','2019-09-14|2019-10-12|2019-10-12|','2019-10-12',NULL,NULL,NULL,NULL,NULL,NULL),(11975,'18-333B','Magellan Aerospace Bournemouth','PLATE COVER','832073','PID282 50280 200','','A',1,'423255','','96920','','0000-00-00',NULL,'yes','yes','yes','','','','','','','before cut -out m6 bolt not applying','profile dig mark|While part cut out time bolt was not clamped|Operator has missed to put the bolt.  ','| Next part was proved with putting bolts & part found ok','|training will be provided in front of the machine   ','CAPA found ok Operator effectiveness need to be measured. ','','2019-09-14','Subramanya L(Naik)','        Paramaeshappa ','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','3','','','','','','|Immediate M/C stopped check  the Dimension for if the part is accepted ','E3456','pe|qas|qas|','2019-09-14|2019-09-18|2019-09-20|','2019-09-20',NULL,NULL,NULL,NULL,NULL,NULL),(11976,'35-688','Saab AB','BRACKET','800397','D5227283320000','NA','PART ISSUE A',2,'OWED-LTA-004','','96779','','0000-00-00',NULL,'yes','no','no','no','yes','yes','no','no','no','PROFILE OVER MILL','1) Due to wrong tool number called by the operator the part profile got over milled.|2) Operator compared the tool number of the current program with the tool number of the opposite hand part.|3) Operator was not aware of the instructions provided in the data sheet.','|Corrected the tool number in the program and cross checked the details with the data sheet along with supervisor guidance.','|Training provided to the operator to how to interpret the data sheet and enter the tool number in the program.','Next batches done by the operator verified and found ok.','','2019-09-14','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','PROFILE OVER MILL','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','Misc','qas(qas)','no','','|Immediately stopped the machine and informed the supervisor. ','E3456','qas_sez|','2019-11-11|','2019-11-11',NULL,NULL,NULL,NULL,NULL,NULL),(11977,'35-561','Saab AB','VENT HOOK','814253','D522 73530 202 00','','PART ISSUE B',2,'PA1687 LTA-2','','96934','','0000-00-00',NULL,'yes','no','no','no','yes','yes','no','no','no','Profile dig mark','Dig mark found on the outer profile of the part.|During the ramping process tool released from the tool holder due to vibration and caused dig mark on the part.|Due to insufficient clamping of the tool in tool holder tool got released during machining. ','|Changed the collate in tool holder and ensured proper clamping of tool retook the offset under supervisor guidance and continued the production ','|Training given to the operator on ensuring proper clamping of the tool in the  tool holder.','Next produced parts verified and found okay.','','2019-09-14','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','due improper clamping dig mark ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','fi','no','Misc','qas(qas)','no','','|Immediately stopped the production, informed to supervisor and checked proper clamping of tools which are loaded inside the machine.','E3456','qas_sez|','2019-09-20|','2019-09-20',NULL,NULL,NULL,NULL,NULL,NULL),(11978,'35-230A','Saab AB','HINGE BRACKET 3 ','570947','D576 50006 205','','D00',1,'LTA Forecast PO A320','','97868','','0000-00-00',NULL,'yes','yes','yes','','','','','','','run time insert broken ','While part Part Running Insert broken |While tool running Insert screw loose |Operator has not tightened the screw Properly   ','|Changed the Cutter and Run the Remaining Parts & Found ok','|After the Running Program Put the M00 in the Program and check \r<br/>the Insert and Screw. ','next Part found ok','','2019-09-14','Subramanya L(Naik)','        Sundar D.K.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','3','','','','','','|Immediate stop M/C & cheek the previous Finishing Part for any dig Mark observed.  ','E3456','pe|qas|','2019-09-16|2019-09-18|','2019-09-18',NULL,NULL,NULL,NULL,NULL,NULL),(11979,'35A-353A','Saab AB','LIFT PIN HOUSING FWD','','423Z1124-5-52','','1',1,'787 Forecast','','A25139','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Bore under size.','Inner diameter of the assembled bush was under size to the drawing requirement.|The bore was maintained to the bottom limit after assembly during the reaming operation and the bore git undersized due to wear in the tool which was not identified by the operator.|The inspection frequency of the cutting edges was not sufficient to predict the wear before letting the tool to run on the part.','|Reworked the bush till the required diameter is reached.','|1) Informed the Engineering team to revise the process to finish the bore to the mean diameter.\r<br/>2) A shaft to the lower tolerance of the hole is machined and issued to ensure the hole is not tapered during machining.','Next batched supplied are verified and found ok.','C78542','2019-09-16','qas_sez(a)','','MAIL','2019-09-16','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','',' 	CUSTOMER END','yes','Misc','qas_sez(a)','no','','|Checked the inner diameter of all similar parts in  FG and fund to be with in the drawing limit.','Z3456','qas_sez|','2019-11-28|','2019-11-28','0000-00-00','0000-00-00','0000-00-00','','',''),(11980,'35A-351A','Saab AB','Lift Actuator Support Fit','','423Z1223-1-50','','---',1,'LTA SAAB B787 Assemb','','A23364','','0000-00-00',NULL,'no','no','no','no','no','no','yes','yes','yes','PAINT CHIP OUT 10670','Damage in the paint layer was detected by the quality team|Inspection method used to detect the damage was not adequate.|The inspector missed to ensure the complete coverage of paint while doing the touch up on the damaged areas.','|Reworked the part by touching up with paint on the affected areas and shipped to customer.','|check point included in the Final inspection report to ensure no damages on the paint layer.','Next batches supplied verified and found ok.','C76714','2019-09-16','qas_sez(a)','','OF-003033','2018-05-29','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER END','yes','Misc','qas_sez(a)','no','','|checked all the parts in stock and no similar defects identified.','Z3456','qas_sez|','2019-11-28|','2019-11-28','0000-00-00','0000-00-00','0000-00-00','','',''),(11981,'35A-351A','Saab AB','Lift Actuator Support Fit','','423Z1223-1-50','','---',1,'LTA SAAB B787 Assemb','','A24460','','0000-00-00',NULL,'no','no','no','no','yes','no','yes','no','yes','PAINT CHIP OUT.','Damage in the paint layer was detected by the quality team|Inspection method used to detect the damage was not adequate.|The inspector missed to ensure the complete coverage of paint while doing the touch up on the damaged areas.','|Reworked the part by touching up with paint on the affected areas and shipped to customer.','|Check point included in the Final inspection report to ensure no damages on the paint layer.','Next batches supplied verified and found ok.','C78004','2019-09-16','qas_sez(a)','','OF-003033','2018-05-29','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER END','yes','Misc','qas_sez(a)','no','','|Checked all the parts in stock and no similar defects identified.','Z3456','qas_sez|','2019-11-28|','2019-11-28','0000-00-00','0000-00-00','0000-00-00','','',''),(11982,'35-443C','Saab AB','HINGE','D83028 YNRQ','D5227338820000','NA','B',45,'OWED-LTA-002','','88270','','0000-00-00',NULL,'yes','no','no','no','no','no','no','yes','yes','HOLE IN LINE MEASURED OUT OFF TOLERANCE. ','Bore under size.|Running time reamer got worn out and bore got under sized.|Due to hardness of the material the reamer worn out and the operator did not identified the part with proper tag, hence it was identified during final inspection.','|Supervisor instructed all the operators to identify the deviated parts with proper identification tag','|Tool life for the tools used for hard materials will be closely monitored by supervisor.','CA PA found ok.','C77032','2019-09-16','qas_sez(a)','qas_sez(a)','MAIL','2019-09-16','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','DN55058','CUSTOMER END','yes','Misc','qas_sez(a)','no','','|Immediately changed the reamer and continued the production.','Z3456','qas_sez|','2019-11-13|','2019-11-13',NULL,NULL,NULL,NULL,NULL,NULL),(11983,'35A-601A','','','','','','',0,'','','','','0000-00-00',NULL,'no','no','no','no','no','no','no','no','no','','','','','','','2019-09-16','select','','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','','','CUSTOMER END','no','','select','no','','','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11984,'35-415','Saab AB','SHAFT LATCH LINK','M789340','D522 73496 200 00','','A',1,'OWED-LTA-004','','83883','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','yes','DENT MARK IN OD.','Damage in the paint layer was detected by the quality team|Inspection method used to detect the damage was not adequate.|The inspector missed to ensure the complete coverage of paint while doing the touch up on the damaged areas.','|Reworked the part by touching up with paint on the affected areas and shipped to customer.','|Check point included in the Final inspection report to ensure no damages on the paint layer.','Next batches supplied verified and found ok.','C76486','2019-09-16','qas_sez(a)','','MAIL','2019-09-16','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','DN53510','CUSTOMER END','yes','Misc','qas_sez(a)','no','','|Checked all the parts in stock and no similar defects identified.','Z3456','qas_sez|','2019-11-28|','2019-11-28','0000-00-00','0000-00-00','0000-00-00','','',''),(11985,'35-415','Saab AB','SHAFT LATCH LINK','M794860','D522 73496 200 00','','A',3,'OWED-LTA-004','','87190','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','yes','DENT MARK IN OD.','Damaged due to insufficient protection.|intermediate sleeve or foam sheets were not used while packing the parts to avoid damage during transit.|Since no similar issues occurred in the history the packing personnel thought that the current packing method is sufficient.','|reworked the part and shipped to customer.','|intermediate foam sheets are used to avoid damages during transit and to ensure complete protection.','Next batches shipped verified and found ok.','C79049','2019-09-16','qas_sez(a)','','MAIL','2019-09-16','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','DN53705','CUSTOMER END','yes','Misc','qas_sez(a)','no','','|checked all the parts in FG and WIP and found ok.','Z3456','qas_sez|','2019-11-28|','2019-11-28','0000-00-00','0000-00-00','0000-00-00','','',''),(11986,'35-306A','Saab AB','RIB INTER 2 ','0448501 1','F575 54796 201 00','','SCH-ISSUE B, PART ISSUE A',1,'A330 NEO FORECAST-20','','73583','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','yes','PART MARKING INTERCHANGED','These are similar parts so wrong identification in treatment house|F575 54796 201 00 & F575 54797 201 00 similar parts are sent to surface treatment in same day. |As per QAD procedure once parts received to QAD complete the inspection within 2 days & move to surface treatment so parts are inspected same day then same day sent surface treatment.','|1) The deviation part got reworked by CIM & send to customer then request to for replace & return the deviated part. \r<br/>2) Get awareness & provide the CAD sheets to receiving treatment parts inspector how to identify the similar parts. \r<br/>3) We raise the NCR our treatment supplier for CAPA. \r<br/>','|\r<br/>1) Avoid the same day dispatch of similar parts to treatment house. \r<br/>2) Weekly once visit to treatment house for get awareness/training for identify the similar parts/LH & RH Parts, batch Mix up, Documentations issue etc.. \r<br/>3) We are internally discuss for implementation checking JIG. \r<br/>4) Raise the quality alert. \r<br/>5) Include the similar parts identification in PSIS (Parts specific information sheet) by treatment house. \r<br/>\r<br/>','CAPA FOUND OK','C78848','2019-09-16','qas_sez(a)','qas_sez(a)','GLB422116','2019-04-17','NC CREATED','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','DN52223','CUSTOMER END','yes','Misc','qas_sez(a)','no','','|Cross check in our FG all similar parts found ok but 1 part 35-306A (F575 54796 201 00) found deviation. The physically part found 35-308A (F575 54797 201 00) but part marked as 35-306A (F575 54796 201 00) so quarantine the deviated part & inform to supplier. ','Z3456','qas_sez|','2019-09-16|','2019-09-16',NULL,NULL,NULL,NULL,NULL,NULL),(11987,'35A-464','Saab AB','FITTING ASSY','','D522 73408 001 00','','A',3,'OWED-LTA-001','','A25408','','0000-00-00',NULL,'yes','no','no','no','no','no','no','yes','yes','Brief Description of Non Conformance: Is condition:Bushing sticks out 1,80 - 1,85 mm. Should be:\r\nBetween 1,55-1,68mm according to drawing D5227340800100 and AIPS 01-02-019 ','Flange projection out of tolerance from the specification limit.|More sealant was applied in the flange of the bush, due to which the bush did not assembled properly and the bush protrusion was not measured.|Bush protrusion requirement isn\'t called in the drawing because of which both the operator and inspector didn\'t ensured the projection before the shipment.','|Bushes are removed and reassembled to meet the requirements.','|\r<br/>APS revised and training was given to both inspector and operators. ','Effectiveness will be measured by 23_SEP_2019 ','C80239','2019-09-16','qas_sez(a)','qas_sez(a)','GLB430832','2019-07-11','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER END','yes','Misc','qas_sez(a)','no','','|We have inspected our stock parts and are found okay. We also inspected the BOI parts they also and found within limits. ','Z3456','qas_sez|','2019-09-16|','2019-09-16',NULL,NULL,NULL,NULL,NULL,NULL),(11988,'35A-463','Saab AB','FITTING ASSY','','D522 73408 000 00','','A',11,'1600189916','','A25442','','0000-00-00',NULL,'yes','no','no','no','no','no','no','yes','yes','Brief Description of Non Conformance: Is condition:Bushing sticks out 1,80 - 1,85 mm. Should be:\r\nBetween 1,55-1,68mm according to drawing D5227340800100 and AIPS 01-02-019 ','Flange projection out of tolerance from the specification limit.|More sealant was applied in the flange of the bush, due to which the bush did not assembled properly and the bush protrusion was not measured.|\r\nBush protrusion requirement isn\'t called in the drawing because of which both the operator and inspector didn\'t ensured the projection before the shipment.','|Bushes are removed and reassembled to meet the requirements. ','|APS revised and training was given to both inspector and operators. ','Effectiveness will be measured by 23_SEP_2019 ','C80193','2019-09-16','qas_sez(a)','qas_sez(a)','GLB430832','2019-07-11','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER END','yes','Misc','qas_sez(a)','no','','|\r\nWe have inspected our stock parts and are found okay. We also inspected the BOI parts they also and found within limits. ','Z3456','qas_sez|','2019-09-16|','2019-09-16',NULL,NULL,NULL,NULL,NULL,NULL),(11989,'35A-463','Saab AB','FITTING ASSY','','D522 73408 000 00','','A',2,'1600189916','','A25443','','0000-00-00',NULL,'yes','no','no','no','no','no','no','yes','yes','Brief Description of Non Conformance: Is condition:Bushing sticks out 1,80 - 1,85 mm. Should be:\r\nBetween 1,55-1,68mm according to drawing D5227340800100 and AIPS 01-02-019 ','Flange projection out of tolerance from the specification limit.|More sealant was applied in the flange of the bush, due to which the bush did not assembled properly and the bush protrusion was not measured.|Bush protrusion requirement isn\'t called in the drawing because of which both the operator and inspector didn\'t ensured the projection before the shipment.','|Bushes are removed and reassembled to meet the requirements. ','|\r<br/>APS revised and training was given to both inspector and operators. ','Effectiveness will be measured by 23_SEP_2019 ','C80193','2019-09-16','qas_sez(a)','qas_sez(a)','GLB430832','2019-07-11','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER END','yes','Misc','qas_sez(a)','no','','|\r\nWe have inspected our stock parts and are found okay. We also inspected the BOI parts they also and found within limits. ','Z3456','qas_sez|','2019-09-16|','2019-09-16',NULL,NULL,NULL,NULL,NULL,NULL),(11990,'35A-351A','Saab AB','Lift Actuator Support Fit','','423Z1223-1-50','','---',1,'787 Forecast','','A23564','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','yes','PAINT CHIP OUT.','Damage in the paint layer was detected by the quality team|Inspection method used to detect the damage was not adequate.|The inspector missed to ensure the complete coverage of paint while doing the touch up on the damaged areas.','|Reworked the part by touching up with paint on the affected areas and shipped to customer.','|Check point included in the Final inspection report to ensure no damages on the paint layer.','Next batches supplied verified and found ok.','C77236','2019-09-16','qas_sez(a)','','MAIL','2019-09-16','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER END','yes','Misc','qas_sez(a)','no','','|Checked all the parts in stock and no similar defects identified.','Z3456','qas_sez|','2019-11-28|','2019-11-28','0000-00-00','0000-00-00','0000-00-00','','',''),(11991,'56-005','GKN Aerospace Orangeburg','SPLICE PLATE FWD UPR','8-17-07731/26462','119A1213-603','NA','PSDL REV -',1,'LTA GKN 737 Winglet','','94718','','0000-00-00',NULL,'yes','no','no','no','yes','yes','no','no','no','Thickness u/s & profile out of spec','Profile measured under size due to undersized thickness.|Due to improper clamping of part the thickness measured under size.|Due to bend in the RM the operator did not ensured complete butting of part to the fixture before starting the cycle.|Due to improper storage condition of RM bend observed on the part.','|Informed the operator to ensure proper clamping using feeler gauge before starting the cycle.','|Informed the stores personnel and the RM supplier to ensure proper storage of parts to avoid similar deformation.','Next batches produced verified and found ok.','','2019-09-18','pe_sez(a)','Rajesha A.R,Pradeep B.D,Maruthi  D R ,Madhu Kumar N,Kiran Kumar M,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','Slim3n-5AHT-2','Mahesh(N)','no','','|Immediately stopped the machine and checked the previously completed parts and remaining RM and segregated the deformed RM.','Z3456','qas_sez|','2019-10-10|','2019-10-10',NULL,NULL,NULL,NULL,NULL,NULL),(11992,'35-117','Saab AB','ALCD_STRUCT_INTERCOSTAL_L','716504B6','423Z1177-4','7050-T7451 ALUMINUM ','--A',2,'Forecast po for B787','','94679','','0000-00-00',NULL,'no','no','no','no','no','no','yes','yes','no','Requirement: As per Clause 8.6 of AS9100 D,\r\n“8.6 Release of Products and Services \r\nThe organization shall implement planned arrangements, at appropriate stages, to verify that the product and service requirements have been met.\r\n\r\nThe release of products and services to the customer shall not proceed until the planned arrangements have been satisfactorily completed, unless otherwise approved by a relevant authority and, as applicable, by the customer.”\r\n\r\nNonconformity Statement: The organization(ATPL) did not ensured the products and services released to customer has met the requirements.\r\n\r\nObjective Evidence: Verification stages before release of product to customer is not adequate as per BAC5736 in Work order AT51338.\r\n','','','','','','2019-09-18','Mahesh(N)','Dharani(Shankar)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','no','no','yes','With Treatment','DN62400','Onsite','no','Misc','Dharani(Shankar)','yes','','','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11993,'35-717','Saab AB','','W37E','D5227349320600','NA','PART ISSUE E',1,'OWED-LTA-005','','97737','','0000-00-00',NULL,'yes','no','no','no','yes','yes','no','no','no','PART PROFILE MEASURED 1.24MM','1) Chamfer oversize during the rework.|2) Dig mark formed on the chamfer during the de burring operation because of improper handling of de burr tool.|3) The pressure of air supplied to the pneumatic de-burring tool was not controlled by the operator. Therefore because of excess vibration the de burr tool slipped over the chamfer.','|Instruction given to all the operators to not to carry out rework on the chamfer areas without supervisor guidance.','|Training given to all the operators on holding the de burr tool and awareness given to all the operators on the prescribed air pressure to be maintained.','Next batches verified found ok.','','2019-09-18','Krishna(Chowdary.G.P.)','','','0000-00-00','PART PROFILE MEASURED 1.24MM','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','Misc','qas(qas)','no','','|Immediately stopped the de burring operation and reduced the pressure of the air supply.','E3456','qas_sez|','2019-12-13|','2019-12-13','0000-00-00','0000-00-00','0000-00-00','','',''),(11994,'35-443C','Saab AB','HINGE','YNRQ','D5227338820000','NA','B',11,'OWED-LTA-002','','96803','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','THICKNESS UNDERSIZED BY 0.07MM TO 0.20MM','Thickness of the part got undersized at edge area.|Due to process/Fixture issue thickness of some parts(11 out of 120 parts) in a batch found undersized at edge area.|1) The butting surface of the part is 3D but the formation of 3D surface in the fixture is not proper, due to that in some parts thickness got undersized at edge area.|2) On the butting surface area of the part a step mark is found, which is acceptable as per \"Ra\" requirement, but the same step has influence over butting of part to the fixture.','|The task is assigned to develop an improvements in the fixture and new clamping method is also inline. ','|The task is assigned to develop an improvements in the fixture and new clamping method is also inline.','CA/PA FOUND OK','','2019-09-24','Karthineyan(V.S.)','Vijay Kumar H.J,Upendra N ,Thaveni D M ,Manu ,HariPrasad ,Gurukiran R,Chetan N,Ananda M,','','0000-00-00','NC Created','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','a51nx-03','qas(qas)','no','','|Inspected all the parts of the batch for similar issue and same is informed to the respective persons.','E3456','qas_sez|qas|','2019-09-25|2019-10-09|','2019-10-09',NULL,NULL,NULL,NULL,NULL,NULL),(11995,'35A-613','Saab AB','ASSY LEVER 1','','D5227280500100','','PART ISSUE A',7,'OWED-LTA-003','','A16212','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','yes','Zink plating chip out.','Due to Improper packing and handling of parts during transit the platting has chipped off.','|1) Informed the inward inspection team to check all the parts for transit damages before storing to FG.\r<br/>2) Inward inspection check list was amended to instruct inspectors to validate the damages on the paint layer due to transit.','|Supplier has improved the packing of parts to avoid damages to the paint layers during transit.','Next batches shipped to customer and received from supplier are verified and found ok.','C66473','2019-09-26','qas_sez(a)','','MAIL','2019-09-26','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','',' 	CUSTOMER END','yes','Misc','qas_sez(a)','no','','|Immediately checked all the parts in FG and in Inward inspection and separated the defective parts and returned to supplier for rework.','Z3456','qas_sez|','2019-12-23|','2019-12-23','0000-00-00','0000-00-00','0000-00-00','','',''),(11996,'47-169','GKN Aerospace Filton','BRKT MTG','627693A5','F57550259200','NA','PART ISSUE E02',1,'GKN-GS-068 PHASE2- L','','91093','','0000-00-00',NULL,'yes','no','no','no','no','no','no','yes','no','as per drawing base thickness in slot dimension is 6mm  but dimension measured in part is 9mm. ','1) Thickness in the Slot not meeting the customer drawing requirement.|2) Part was machined according to the CIM created model which was not meeting the drawing dimensions. |3) Due to improper interpretation of drawing by the engineering personnel and the model validation process was not done independently.','|1) Results of re validation of models were shared to customer and the models with zero defects were cleared for production.\r<br/>2) Affected models were redesigned by the engineering team with respect to the customer supplied drawing and validated independently.\r<br/>','|Internal procedure revised to include the requirement of carrying our model validation independently.','All the models created are validated independently.','','2019-09-27','CAD(sez)','CAD(sez)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','DN58037','onsite','yes','Misc','Mahesh(N)','yes','','|Immediately stopped the production and validated all the GKN models that are created by CIM.','Z3456','qas_sez|','2019-10-19|','2019-10-19',NULL,NULL,NULL,NULL,NULL,NULL),(11997,'47-169','GKN Aerospace Filton','BRKT MTG','1750032015','F57550259200','NA','PART ISSUE E02',3,'GKN-GS-068 PHASE2- L','','91094','','0000-00-00',NULL,'yes','no','no','no','no','no','no','yes','no','as per drawing base thickness in slot dimension is 6mm  but dimension measured in part is 9mm. ','1) Thickness in the Slot not meeting the customer drawing requirement.|2) Part was machined according to the CIM created model which was not meeting the drawing dimensions. |3) Due to improper interpretation of drawing by the engineering personnel and the model validation process was not done independently.','|1) Results of re validation of models were shared to customer and the models with zero defects were cleared for production.\r<br/>2) Affected models were redesigned by the engineering team with respect to the customer supplied drawing and validated independently.\r<br/>','|Internal procedure revised to include the requirement of carrying our model validation independently.','All the models created are validated independently.','','2019-09-27','CAD(sez)','CAD(sez)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','DN58036','onsite','yes','Misc','Mahesh(N)','yes','','|Immediately stopped the production and validated all the GKN models that are created by CIM.','Z3456','qas_sez|','2019-10-19|','2019-10-19',NULL,NULL,NULL,NULL,NULL,NULL),(11998,'47-169','GKN Aerospace Filton','BRKT MTG','1750032015','F57550259200','NA','PART ISSUE E02',4,'GKN-GS-068 PHASE2- L','','91095','','0000-00-00',NULL,'yes','no','no','no','no','no','no','yes','no','as per drawing base thickness in slot dimension is 6mm  but dimension measured in part is 9mm. ','1) Thickness in the Slot not meeting the customer drawing requirement.|2) Part was machined according to the CIM created model which was not meeting the drawing dimensions. |3) Due to improper interpretation of drawing by the engineering personnel and the model validation process was not done independently.','|1) Results of re validation of models were shared to customer and the models with zero defects were cleared for production.\r<br/>2) Affected models were redesigned by the engineering team with respect to the customer supplied drawing and validated independently.\r<br/>','|Internal procedure revised to include the requirement of carrying our model validation independently.','All the models created are validated independently.','','2019-09-27','CAD(sez)','CAD(sez)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','DN58034','onsite','yes','Misc','Mahesh(N)','yes','','|Immediately stopped the production and validated all the GKN models that are created by CIM.','Z3456','qas_sez|','2019-10-19|','2019-10-19',NULL,NULL,NULL,NULL,NULL,NULL),(11999,'47-169','GKN Aerospace Filton','BRKT MTG','1750032015','F57550259200','NA','PART ISSUE E02',1,'1210042824-2','','91096','','0000-00-00',NULL,'yes','no','no','no','no','no','no','yes','no','as per drawing base thickness in slot dimension is 6mm  but dimension measured in part is 9mm. ','1) Thickness in the Slot not meeting the customer drawing requirement.|2) Part was machined according to the CIM created model which was not meeting the drawing dimensions. |3) Due to improper interpretation of drawing by the engineering personnel and the model validation process was not done independently.','|1) Results of re validation of models were shared to customer and the models with zero defects were cleared for production.\r<br/>2) Affected models were redesigned by the engineering team with respect to the customer supplied drawing and validated independently.\r<br/>','|Internal procedure revised to include the requirement of carrying our model validation independently.','All the models created are validated independently.','','2019-09-27','CAD(sez)','CAD(sez)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','DN58038','onsite','yes','Misc','Mahesh(N)','yes','','|Immediately stopped the production and validated all the GKN models that are created by CIM.','Z3456','qas_sez|','2019-10-19|','2019-10-19',NULL,NULL,NULL,NULL,NULL,NULL),(12000,'47-170','GKN Aerospace Filton','BRKT MTG','3963401 1','F57550259201','NA','PART ISSUE E02',4,'GKN-GS-068 PHASE2- L','','92790','','0000-00-00',NULL,'yes','no','no','no','no','no','no','yes','no','as per drawing base thickness in slot dimension is 6mm  but dimension measured in part is 9mm. ','1) Thickness in the Slot not meeting the customer drawing requirement.|2) Part was machined according to the CIM created model which was not meeting the drawing dimensions. |3) Due to improper interpretation of drawing by the engineering personnel and the model validation process was not done independently.','|1) Results of re validation of models were shared to customer and the models with zero defects were cleared for production.\r<br/>2) Affected models were redesigned by the engineering team with respect to the customer supplied drawing and validated independently.\r<br/>','|Internal procedure revised to include the requirement of carrying our model validation independently.','All the models created are validated independently.','','2019-09-27','CAD(sez)','CAD(sez)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','DN61173','onsite','yes','Misc','Mahesh(N)','yes','','|Immediately stopped the production and validated all the GKN models that are created by CIM.','Z3456','qas_sez|','2019-10-19|','2019-10-19',NULL,NULL,NULL,NULL,NULL,NULL),(12001,'47-170','GKN Aerospace Filton','BRKT MTG','3963401 1','F57550259201','NA','PART ISSUE E02',4,'GKN-GS-068 PHASE2- L','','92791','','0000-00-00',NULL,'yes','no','no','no','no','no','no','yes','no','as per drawing base thickness in slot dimension is 6mm  but dimension measured in part is 9mm. ','1) Thickness in the Slot not meeting the customer drawing requirement.|2) Part was machined according to the CIM created model which was not meeting the drawing dimensions. |3) Due to improper interpretation of drawing by the engineering personnel and the model validation process was not done independently.','|1) Results of re validation of models were shared to customer and the models with zero defects were cleared for production.\r<br/>2) Affected models were redesigned by the engineering team with respect to the customer supplied drawing and validated independently.\r<br/>','|Internal procedure revised to include the requirement of carrying our model validation independently.','All the models created are validated independently.','','2019-09-27','CAD(sez)','CAD(sez)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','DN61175','onsite','yes','Misc','Mahesh(N)','yes','','|Immediately stopped the production and validated all the GKN models that are created by CIM.','Z3456','qas_sez|','2019-10-19|','2019-10-19',NULL,NULL,NULL,NULL,NULL,NULL),(12002,'47-170','GKN Aerospace Filton','BRKT MTG','3963401 1','F57550259201','NA','PART ISSUE E02',3,'GKN-GS-068 PHASE2- L','','92792','','0000-00-00',NULL,'yes','no','no','no','no','no','no','yes','no','as per drawing base thickness in slot dimension is 6mm  but dimension measured in part is 9mm. ','1) Thickness in the Slot not meeting the customer drawing requirement.|2) Part was machined according to the CIM created model which was not meeting the drawing dimensions. |3) Due to improper interpretation of drawing by the engineering personnel and the model validation process was not done independently.','|1) Results of re validation of models were shared to customer and the models with zero defects were cleared for production.\r<br/>2) Affected models were redesigned by the engineering team with respect to the customer supplied drawing and validated independently.\r<br/>','|Internal procedure revised to include the requirement of carrying our model validation independently.','All the models created are validated independently.','','2019-09-27','CAD(sez)','CAD(sez)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','DN61176','onsite','yes','Misc','Mahesh(N)','yes','','|Immediately stopped the production and validated all the GKN models that are created by CIM.','Z3456','qas_sez|','2019-10-19|','2019-10-19',NULL,NULL,NULL,NULL,NULL,NULL),(12003,'51A-066A','THE BOEING COMPANY','STRUT SUPPORT ASSY','','113T1958-7','','PSDL REV A',4,'BOEING 001AA','','A29775','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','After bush Assembled ,the position of the bore is not maintained within 0.001\" while reaming the bush.measures 0.005/0.006\".','','','','','','2019-10-09','Anjinamurthy(H)','Jayarama(M.B.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','no','yes','no','Assembly','','IN PROCESS','no','Misc','Nithin(S)','no','M03807|BACB28AP04Z011','','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(12004,'35-743','Saab AB','HANDLE OUTER','826917','D5227281520200','NA','PART ISSUE B',1,'OWED-LTA-002','','97426','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','CHAMFER OVER SIZE','','','','','','2019-10-10','Dinesh kulal()','prodn_aero(prodn)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','no','yes','no','With Treatment','','2ND','no','Misc','prodn_aero(prodn)','no','','','A3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(12005,'53-010','Triumph Aerostructures','RADIUS WASHER, A330 NEO','64576/01/00','F5725131820000','NA','PART ISSUE A',31,'LTA TRIUMPH 2018','','95025','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','The observed conductivity value is not meeting the requirement.','Conductivity value measured was not meeting the specification requirement.|Due to overheating of the material during machining conductivity value on the measured surface differed from the requirement.|Due to blockage in the coolant filter the flow of coolant was reduced and resulted in overheating.|Frequency for cleaning the coolant filter was high.','|Informed the operator to ensure proper coolant pressure and flow of coolant before starting the production.','|Frequency of the coolant filter maintenance is reduced.','No similar issues observed during the next productions.','','2019-10-10','qas_sez(a)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','DN62578','Post DN','no','Misc','qas_sez(a)','no','','|Informed the maintenance team to check the coolant filters of all the machine and clean the blogs.','Z3456','qas_sez|','2019-10-10|','2019-10-10',NULL,NULL,NULL,NULL,NULL,NULL),(12006,'47-196','GKN Aerospace Filton','M/C HINGE POST 5 I/A','524201','F5755517020103','NA','PART ISSUE A',1,'GKN-GS-068 PHASE2- L','','90993','','0000-00-00',NULL,'yes','no','no','no','no','no','no','yes','no','Due to model error profile not accepted as per drawing.','1) Part profile not meeting the customer drawing requirement.|2) Part was machined according to the CIM created model which was not meeting the drawing dimensions.|3) Due to improper interpretation of drawing by the engineering personnel and the model validation process was not done independently.','|1) Results of re validation of models were shared to customer and the models with zero defects were cleared for production.\r<br/>2) Affected models were redesigned by the engineering team with respect to the customer supplied drawing and validated independently.','|Internal procedure revised to include the requirement of carrying our model validation independently.','All the models created are validated independently.','','2019-10-11','qas_sez(a)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','DN61202','on site','no','Misc','qas_sez(a)','yes','','|Immediately stopped the production and validated all the GKN models that are created by CIM.','Z3456','qas_sez|','2019-10-18|','2019-10-18',NULL,NULL,NULL,NULL,NULL,NULL),(12007,'47-194','GKN Aerospace Filton','M/C HINGE POST 4 I/A','524201','F5755516720103','NA','PART ISSUE A',1,'GKN-GS-068 PHASE2- L','','90980','','0000-00-00',NULL,'yes','no','no','no','no','no','no','yes','no','Due to model error profile not accepted as per drawing.','1) Part profile not meeting the customer drawing requirement.|2) Part was machined according to the CIM created model which was not meeting the drawing dimensions. |3) Due to improper interpretation of drawing by the engineering personnel and the model validation process was not done independently.','|1) Results of re validation of models were shared to customer and the models with zero defects were cleared for production.\r<br/>2) Affected models were redesigned by the engineering team with respect to the customer supplied drawing and validated independently.\r<br/>','|Internal procedure revised to include the requirement of carrying our model validation independently.','All the models created are validated independently.','','2019-10-11','qas_sez(a)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','DN61211','on site','no','Misc','qas_sez(a)','yes','','|Immediately stopped the production and validated all the GKN models that are created by CIM.','Z3456','qas_sez|','2019-10-18|','2019-10-18',NULL,NULL,NULL,NULL,NULL,NULL),(12008,'47-195','GKN Aerospace Filton','M/C HINGE POST 5 I/A','524201','F5755517020003','NA','PART ISSUE A',1,'GKN-GS-068 PHASE2- L','','90990','','0000-00-00',NULL,'yes','no','no','no','no','no','no','yes','no','Due to model error profile not accepted as per drawing.','1) Part profile not meeting the customer drawing requirement.|2) Part was machined according to the CIM created model which was not meeting the drawing dimensions. |3) Due to improper interpretation of drawing by the engineering personnel and the model validation process was not done independently.','|1) Results of re validation of models were shared to customer and the models with zero defects were cleared for production.\r<br/>2) Affected models were redesigned by the engineering team with respect to the customer supplied drawing and validated independently.\r<br/>','|Internal procedure revised to include the requirement of carrying our model validation independently.','All the models created are validated independently.','','2019-10-11','qas_sez(a)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','DN61207','on site','no','Misc','qas_sez(a)','yes','','|Immediately stopped the production and validated all the GKN models that are created by CIM.','Z3456','qas_sez|','2019-10-18|','2019-10-18',NULL,NULL,NULL,NULL,NULL,NULL),(12009,'51-194','THE BOEING COMPANY','TIE ROD BRACKET - LITTER ','288487B2','65B56597-74','NA','NIL',1,'BOEING 001AA','','97365','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','PART TRIMMING TIME, CUTTING TOOLS VIBRATION MARK ON THE PART','The tool vibration marks formed on the part surface are beyond the acceptable limit. |Due to insufficient  flushing chips locked and vibration occurred.|While proving the first part operator used intermediate program stop to check the part.|Visibility through the transparent screen was not so good. ','|Stopped the usage of intermediate program stop during the cycle and next parts found okay.','|Maintenance team is informed to check and change the sheet attached to transparent door to ensure the good visibality of part through it.','Next batch parts found ok.','','2019-10-11','Nagaraju P K()','Vijay Kumar H.J,Manu ,Dhanush J.K,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','5','no','a51nx-05','pe_sez(a)','no','','|Immediately stopped the production and informed to the supervisor.','Z3456','qas_sez|','2019-10-12|','2019-10-12',NULL,NULL,NULL,NULL,NULL,NULL),(12010,'47-196','GKN Aerospace Filton','M/C HINGE POST 5 I/A','524201','F5755517020103','NA','PART ISSUE A',1,'GKN-GS-068 PHASE2- L','','90995','','0000-00-00',NULL,'yes','no','no','no','no','no','no','yes','no','Due to model error profile not accepted as per drawing.','1) Part profile not meeting the customer drawing requirement.|2) Part was machined according to the CIM created model which was not meeting the drawing dimensions. |3) Due to improper interpretation of drawing by the engineering personnel and the model validation process was not done independently.','|1) Results of re validation of models were shared to customer and the models with zero defects were cleared for production.\r<br/>2) Affected models were redesigned by the engineering team with respect to the customer supplied drawing and validated independently.\r<br/>','|Internal procedure revised to include the requirement of carrying our model validation independently.','All the models created are validated independently.','','2019-10-11','qas_sez(a)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','DN61203','on site','no','Misc','qas_sez(a)','yes','','|Immediately stopped the production and validated all the GKN models that are created by CIM.','Z3456','qas_sez|','2019-10-18|','2019-10-18',NULL,NULL,NULL,NULL,NULL,NULL),(12011,'47-195','GKN Aerospace Filton','M/C HINGE POST 5 I/A','524201','F5755517020003','NA','PART ISSUE A',1,'GKN-GS-068 PHASE2- L','','90984','','0000-00-00',NULL,'yes','no','no','no','no','no','no','yes','no','Due to model error profile not accepted as per drawing.','1) Part profile not meeting the customer drawing requirement.|2) Part was machined according to the CIM created model which was not meeting the drawing dimensions. |3) Due to improper interpretation of drawing by the engineering personnel and the model validation process was not done independently.','|1) Results of re validation of models were shared to customer and the models with zero defects were cleared for production.\r<br/>2) Affected models were redesigned by the engineering team with respect to the customer supplied drawing and validated independently.\r<br/>','|Internal procedure revised to include the requirement of carrying our model validation independently.','All the models created are validated independently.','','2019-10-11','qas_sez(a)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','DN61206','on site','no','Misc','qas_sez(a)','yes','','|Immediately stopped the production and validated all the GKN models that are created by CIM.','Z3456','qas_sez|','2019-10-18|','2019-10-18',NULL,NULL,NULL,NULL,NULL,NULL),(12012,'35-526','Saab AB','ROD BODY','2878','D522 73337 200 00','','A',1,'OWED-LTA-004','','81918','','0000-00-00',NULL,'yes','no','no','no','yes','yes','no','no','no','GO THREAD GAUGE NOT ANSWERING','THE BORING OPERATION WILL BE DONE AFTER THE INTERNAL THREAD CUTTING SO BURR GOT FOLDED AFTER THE BORING OPERATION DUE TO WHICH THE THREAD GUAGE WAS NOT ANSWERING.','','','REWORK DONE FOR THE PART AND ALL THE PARTS PRODUCED AFTERWORDS ARE FOUND OK','','2019-10-12','pe_sez(a)','Vijay Kumar H.J,Ravi Kumar G.B,Pradeep B.D,Dinakar K ,','','0000-00-00','5/16-24 UNJF-3B THREAD GAUGE. GO THREAD GAUGE IS NOT ANSWERING ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','','FI','yes','200MY-02','qas_sez(a)','no','','','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(12013,'35-526','Saab AB','ROD BODY','2878','D522 73337 200 00','','A',1,'OWED-LTA-004','','81918','','0000-00-00',NULL,'yes','no','no','no','yes','yes','no','no','no','GO THREAD GAUGE NOT ANSWERING','THE BORING OPERATION WILL BE DONE AFTER THE INTERNAL THREAD CUTTING SO BURR GOT FOLDED AFTER THE BORING OPERATION DUE TO WHICH THE THREAD GUAGE WAS NOT ANSWERING.','','','REWORK DONE FOR THE PART AND ALL THE PARTS PRODUCED AFTERWORDS ARE FOUND OK','','2019-10-12','pe_sez(a)','Vijay Kumar H.J,Ravi Kumar G.B,Pradeep B.D,Dinakar K ,','','0000-00-00','5/16-24 UNJF-3B THREAD GAUGE. GO THREAD GAUGE IS NOT ANSWERING ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','','FI','yes','200MY-02','qas_sez(a)','no','','','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(12014,'35-662','Saab AB','ROD END','802628','D5227334520600','NA','PART ISSUE B',1,'OWED-LTA-005','','98184','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','OD DIG MARK SO PART REJECTED','Insufficient Clamping force. |Breakage of NYLON clamp during in process  ','|New clamping method i.e, clamp made of aluminum with be introduced . ','|new process with the aluminum clamp with be done.','ca/pa found ok','','2019-10-12','Sandhesh D(S)','Manoj Kumar(D)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','09','no','Misc','Raghavendra Rao(R)','no','','|NYLON bush was Replaced with new one of & part found ok','E3456','qas|','2019-10-18|','2019-10-18',NULL,NULL,NULL,NULL,NULL,NULL),(12015,'56-006','GKN Aerospace Orangeburg','SPLICE PLATE FWD UPR','8-17-07731/26462','119A1213-604','NA','PSDL REV -',1,'LTA GKN 737 Winglet','','94717','','0000-00-00',NULL,'yes','no','no','no','yes','yes','no','no','no','TOOL DIG MARK FOUND & PROFILE OUT 20 TO 36 THOU','','','','','','2019-10-13','pe_sez(a)','Rajesha A.R,Pradeep B.D,Maruthi  D R ,Kiran Kumar M,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','no','yes','no','With Treatment','','FI','no','Slim3n-5AHT-2','Mahesh(N)','no','','','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(12016,'51-148A','THE BOEING COMPANY','UPR SKIN COVER ','0-24-15606/29751','312Z3121-501','NA','NIL',1,'BOEING AC001','','95199','','0000-00-00',NULL,'yes','no','yes','no','yes','no','no','no','no','Outer profile marking depth over size.','1) Depth of the relief between the part and the leg is oversize.|2) Tool offset entered wrongly for 10dia end mill.|3) Tool offset taken in the Zoller machine was wrong.|4) The type of tool selected in the Zoller software was wrong by the tooling personnel.|5) The tooling in charge who selected the tool type in the Zoller machine was not fully trained and the trained person responsible for operating the machine was not available.','|Instruction given to all the machine operators to ensure the tooling personnel has picked the proper tooling type and to cross check the tool offset provided by the Zoller machine by manual method.','|Re-training will be provided to the tooling personnel and training effectiveness will be measured by validating the next 100 tools offset measured by him.','Training effectiveness will be monitored for next 100 tools.','','2019-10-14','pe_sez(a)','pe_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','','1','yes','Misc','pe_sez(a)','no','','|1) Immediately stopped the machine and re-checked the tool offset and corrected the offset in the machine.\r\n2) Cross checked the tool offset of all the tools issued by the particular operator and only this tool was issued by him.','Z3456','qas_sez|','2019-10-17|','2019-10-17',NULL,NULL,NULL,NULL,NULL,NULL),(12017,'51-112','THE BOEING COMPANY','FITTING- R3 ,FRONT SPAR B','796230A1','112U7321-5','NA','PSDL REV B',1,'BOEING 001R','','96752','','0000-00-00',NULL,'yes','yes','yes','','','','','','','bore over size 0,14 ','1) Diameter set in the boring bar was not to the requirement.|2) Operator adjusted the boring bar and did not ensured the diameter after adjusting.|3) the boring bar was set to the required dimension when issued to the operator from the tool grip but before loading to the machine the operator re-adjusted the boring bare and did not ensured the diameter before loading to the machine.|4)Due to lack of confidence of the operator on the zoller machine the operator re-adjusted the boring bar thinking to achieve the bore in the minimal side and then we can correct the dimension but after re-adjusting the operator did not ensured to what diameter he has adjusted before loading to machine.','|Informed all the operators to not to re-adjust the boring bar without supervisor knowledge after it is set by the Tool grib using zoller machine.','|Instruction given to all the operators to get the boring bar set from the zoller machine to the lower tolerance band so that even if any variation occurred during the machining due to error in zoller machine the diameter will be either achieved as required or it gets within the re workable limit. ','Next batch settings will be monitored.','','2019-10-14','Karthineyan(V.S.)','        Diwakar R.B.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','3','','','','','','|Immediately stopped the machine and adjusted the boring bar dimension to the requirement under supervisor guidance and continued the production.','Z3456','pe|qas_sez|','2019-10-15|2019-11-06|','2019-11-06',NULL,NULL,NULL,NULL,NULL,NULL),(12018,'51-189','THE BOEING COMPANY','FIXED HINGE - MLG, DRAG S','347601','113W8345-27','NA','PSDL REV A',1,'BOEING 001AA','','95609','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Radius 6.35mm undersized by 3mm.','1) The tool has removed the excessive material than actual profile radius during machining.|2) The Tool path has been made wrong with incorrect Strategy boundary selection.|3) During Dummy part proving, the actual profile radius was not identified as the requirement was not called out in the drawing later it was identified when the FAIR part was compared with the model.','|1) Tool path boundary was verified and corrected.\r<br/>2) Simulation verification was also done and verified.\r<br/>3) New program is generated, verified with simulation and provided to the production team for further process.\r<br/>','|Crosschecking each tool path with G code simulator before releasing the programs to machines will be effectively followed by all the engineers after completion of training from Nov-04-2019.','Verification of Preventive action will be done during the next issue of FAIR programs after 04-Nov-19.','','2019-10-15','CAD(sez)','Vijay Kumar H.J,Upendra N ,Manu ,Madhu Kumar N,Dhanush J.K,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','a51nx-05','qas_sez(a)','no','','|Immediately stopped the production and Part is identified as rejected.','Z3456','qas_sez|','2019-10-21|','2019-10-21',NULL,NULL,NULL,NULL,NULL,NULL),(12019,'34-018C','Magellan Aerospace Winnipeg','BRACKET STRUT LH ','J0702','400-12609-1-905','NA','EM105092 Iss H, EM104302 Iss B, EM104765 Iss H, EM106399 Iss B, EM106400 Iss B, EM106401 Iss B, EM106404 Iss A, EM106522 Iss A, EM106602 Iss A',1,'C96950','','97811','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Hole position out of tolerance by 0.3mm','While part machining time X axis 0.3mm out of tolerance |Multiple Fixture used for bore finishing|Process is Difficult to achieve the Position','|Next Part Machine running time Corrected the X Value, and cross verification Value.','|New Process will be Introduced (Fixture) before next Batch. ','CA/PA FOUND OK','','2019-10-15','Gurukiran S(M)','SIDDESH()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','07','no','Misc','Gurukiran S(M)','no','','|Immediately stop the Machine and informed to Supervisor.   ','E3456','qas|qas|','2019-10-16|2019-10-17|','2019-10-17',NULL,NULL,NULL,NULL,NULL,NULL),(12020,'51-159','THE BOEING COMPANY','FLANGE, SPLIT RING','BC07620','349T2200-443','NA','PSDL REV J',1,'BOEING 001Z','','98666','','0000-00-00',NULL,'yes','yes','yes','','','','','','','DIA 170.18 OVERSIZE BY 1MM SO PART REJECTED  ','1) 12 dia end mill run instead of 10 dia.|2) Tool number entered in the program was wrong.|3) The program has two sub sequences one is for semi finishing and the other is for finishing but the tool used for both the operation was same so the operator changed the tool number for the semi-finishing operation and did not changed for the finishing operation.|4) Usually the programs were run separately but to reduce the cycle time the program was merged and the operator did not cross checked the program before starting the cycle.','|Supervisor verified the tool number of the other tools in the program and changed the wrongly entered values.','|Trial or re-engineering prove outs will be carried out only under the supervisor presence.','Next three batch production will be verified.','','2019-10-16','pe_sez(a)','        Madhu Kumar N','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','3','','','','','','|Immediately stopped the machine and informed the supervisor.','Z3456','pe_sez|qas_sez|','2019-10-16|2019-10-17|','2019-10-17',NULL,NULL,NULL,NULL,NULL,NULL),(12021,'18-318A','Magellan Aerospace Wrexham','HALF CLAMP','M673490/3820B','D574 50551 200','DTD 5014','B01',1,'175170','','98445','','0000-00-00',NULL,'yes','no','yes','no','yes','no','no','no','no','dig mark on profile.','Dig mark occurred on part during machining 		|The program was verified while that time half program was showed in memory.				|The program overlapping occurred		','|The program will be verify in a system to before load into a machine. 						','|The program distribution into a system method will be implement by server method 		','capa found ok','','2019-10-16','Subramanya L(Naik)','Subramanya L(Naik)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Subramanya L(Naik)','no','','|The corrupted program was removed from machine and the correct program was verified in a system then loaded into machine ','E3456','pe|qas|','2019-11-08|2019-11-08|','2019-11-08',NULL,NULL,NULL,NULL,NULL,NULL),(12022,'35-718','Saab AB','','MGJ4','D5227349320700','NA','PART ISSUE E',1,'OWED-LTA-005','','97749','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Profile measure 0.4 mm out tolerance.','1) No clear instruction was available for the operator to ensure the reference point.|2) During the setting operation the part was placed in the mid of the vise due to which the second part loaded was slightly offset from the setting position.|3) Operator did not ensured the reference position before starting the cycle.','|Informed the operators to clamp the part at the corners of the vise and to use butting blocks to ensure the part is butted properly.','|Fixtures will be designed and introduced to clamp the parts in future to avoid similar rejections.','Effectiveness shall be measured once\r\n1. The instructions are provided to operator in the Process Sheet\r\n2. Fixture is put to use.\r\n','','2019-10-16','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','Nc Raised','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','Misc','Nagendra(SN)','no','','|Re-Checked the parts for this particular work order which were already manufactured and found to be in acceptable limits.','E3456','qas_sez|Deshpande|qas_sez|','2019-10-19|2019-10-22|2019-11-18|','2019-11-18',NULL,NULL,NULL,NULL,NULL,NULL),(12023,'47-194','GKN Aerospace Filton','M/C HINGE POST 4 I/A','524201','F5755516720103','NA','PART ISSUE A',1,'GKN-GS-068 PHASE2- L','','90977','','0000-00-00',NULL,'yes','no','no','no','no','no','no','yes','no','Due to model error profile not accepted as per drawing. ','1) Part manufactured to CIM model was not meeting the customer drawing requirement.|2) Part was machined according to the CIM created model which was not meeting the drawing dimensions. |3) Due to improper interpretation of drawing by the engineering personnel and the model validation process was not done independently.','|1) Results of re validation of models were shared to customer and the models with zero defects were cleared for production.\r<br/>2) Affected models were redesigned by the engineering team with respect to the customer supplied drawing and validated independently.\r<br/>','|Internal procedure revised to include the requirement of carrying our model validation independently.','All the models created are validated independently.','','2019-10-19','qas_sez(a)','qas_sez(a)','G8D1157','2019-08-12','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','DN61210','cust end','no','Misc','qas_sez(a)','yes','','|Immediately stopped the production and validated all the GKN models that are created by CIM.','Z3456','qas_sez|','2019-10-21|','2019-10-21',NULL,NULL,NULL,NULL,NULL,NULL),(12024,'47-196','GKN Aerospace Filton','M/C HINGE POST 5 I/A','524201','F5755517020103','NA','PART ISSUE A',1,'GKN-GS-068 PHASE2- L','','90994','','0000-00-00',NULL,'yes','no','no','no','no','no','no','yes','no','Due to model error profile not accepted as per drawing. ','1) Part manufactured to CIM model was not meeting the customer drawing requirement.|2) Part was machined according to the CIM created model which was not meeting the drawing dimensions. |3) Due to improper interpretation of drawing by the engineering personnel and the model validation process was not done independently.','|1) Results of re validation of models were shared to customer and the models with zero defects were cleared for production.\r<br/>2) Affected models were redesigned by the engineering team with respect to the customer supplied drawing and validated independently.\r<br/>','|Internal procedure revised to include the requirement of carrying our model validation independently.','All the models created are validated independently.','','2019-10-19','qas_sez(a)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','DN61204','on site','no','Misc','qas_sez(a)','yes','','|Immediately stopped the production and validated all the GKN models that are created by CIM.','Z3456','qas_sez|','2019-10-21|','2019-10-21',NULL,NULL,NULL,NULL,NULL,NULL),(12025,'47-195','GKN Aerospace Filton','M/C HINGE POST 5 I/A','524201','F5755517020003','NA','PART ISSUE A',1,'GKN-GS-068 PHASE2- L','','90991','','0000-00-00',NULL,'yes','no','no','no','no','no','no','yes','no','Due to model error profile not accepted as per drawing. ','1) Part manufactured to CIM model was not meeting the customer drawing requirement.|2) Part was machined according to the CIM created model which was not meeting the drawing dimensions. |3) Due to improper interpretation of drawing by the engineering personnel and the model validation process was not done independently.','|1) Results of re validation of models were shared to customer and the models with zero defects were cleared for production.\r<br/>2) Affected models were redesigned by the engineering team with respect to the customer supplied drawing and validated independently.\r<br/>','|Internal procedure revised to include the requirement of carrying our model validation independently.','All the models created are validated independently.','','2019-10-19','qas_sez(a)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','DN61205','on site','no','Misc','qas_sez(a)','yes','','|Immediately stopped the production and validated all the GKN models that are created by CIM.','Z3456','qas_sez|','2019-10-21|','2019-10-21',NULL,NULL,NULL,NULL,NULL,NULL),(12026,'47-128A','GKN Aerospace Filton','HINGE POST NO. 4','9753201','F5755106220203','NA','PART ISSUE D',1,'GS68-LTA-1-2018','','74641','','0000-00-00',NULL,'yes','no','no','no','no','no','no','yes','no','Due to model error profile not accepted as per drawing. ','','','','','','2019-10-19','qas_sez(a)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','no','yes','no','With Treatment','DN42048','on site','no','Misc','qas_sez(a)','yes','','','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(12027,'47-194','GKN Aerospace Filton','M/C HINGE POST 4 I/A','524201','F5755516720103','NA','PART ISSUE A',1,'GKN-GS-068 PHASE2- L','','90978','','0000-00-00',NULL,'yes','no','no','no','no','no','no','yes','no','Due to model error profile not accepted as per drawing. ','1) Part manufactured to CIM model was not meeting the customer drawing requirement.|2) Part was machined according to the CIM created model which was not meeting the drawing dimensions. |3) Due to improper interpretation of drawing by the engineering personnel and the model validation process was not done independently.','|1) Results of re validation of models were shared to customer and the models with zero defects were cleared for production.\r<br/>2) Affected models were redesigned by the engineering team with respect to the customer supplied drawing and validated independently.\r<br/>','|Internal procedure revised to include the requirement of carrying our model validation independently.','All the models created are validated independently.','','2019-10-19','qas_sez(a)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','DN61208','on site','no','Misc','qas_sez(a)','yes','','|Immediately stopped the production and validated all the GKN models that are created by CIM.','Z3456','qas_sez|','2019-10-21|','2019-10-21',NULL,NULL,NULL,NULL,NULL,NULL),(12028,'47-194','GKN Aerospace Filton','M/C HINGE POST 4 I/A','524201','F5755516720103','NA','PART ISSUE A',1,'GKN-GS-068 PHASE2- L','','90979','','0000-00-00',NULL,'yes','no','no','no','no','no','no','yes','no','Due to model error profile not accepted as per drawing. ','1) Part manufactured to CIM model was not meeting the customer drawing requirement.|2) Part was machined according to the CIM created model which was not meeting the drawing dimensions. |3) Due to improper interpretation of drawing by the engineering personnel and the model validation process was not done independently.','|1) Results of re validation of models were shared to customer and the models with zero defects were cleared for production.\r<br/>2) Affected models were redesigned by the engineering team with respect to the customer supplied drawing and validated independently.\r<br/>','|Internal procedure revised to include the requirement of carrying our model validation independently.','All the models created are validated independently.','','2019-10-19','qas_sez(a)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','DN61209','on site','no','Misc','qas_sez(a)','yes','','|Immediately stopped the production and validated all the GKN models that are created by CIM.','Z3456','qas_sez|','2019-10-21|','2019-10-21',NULL,NULL,NULL,NULL,NULL,NULL),(12029,'35A-726','Saab AB','ASSY VENT FLAP','','D5227281000601','','PART ISSUE H',1,'OWED-LTA-001','','A30665','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Hole pitch shift by 1MM during Manufacturing.','improper part butting on fixture|fixture is not suitable for the process','|message added in program(check the feeler gauge for all butting parts) and M00 stop given in program.','|opposite side of the fixture extra butting pin added.and jig implemented for the hole checking,to control the escape from quality. ','Fixture verified and found ok.','','2019-10-21','qas_sez(a)','qas_sez(a)','','0000-00-00','Nc Created','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Assembly','','FI','no','Misc','qas_sez(a)','no','92020|D5227281320000','|ensure the part in FG,and treatment house and WIP all are found OK','Z3456','qas|qas|','2019-11-12|2019-11-20|','2019-11-20',NULL,NULL,NULL,NULL,NULL,NULL),(12030,'35-752','Saab AB','LOCK SECTOR','1738802','D5227349920400','NA','PART  ISSUE D',3,'1600283741','','98293','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','Excess material removed in Rib Thickness when re engineering time  ','','','','','','2019-10-21','Nagaraju P K()','Thaveni D M ,Manjunatha  K,HariPrasad ,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','no','yes','no','With Treatment','','3','no','a51nx-01','pe_sez(a)','no','','','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(12031,'18-318A','Magellan Aerospace Wrexham','HALF CLAMP','M038080/27403A','D574 50551 200','DTD 5014','B01',1,'175170','','98765','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','SPOT FACE DEPTH OVERSIZED','DUMMY','|DUMMY','|DUMMY','DUMMY(REFFER NC NO 12032)','','2019-10-23','Anjinamurthy(H)','Suresh(K.R.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','7','no','Misc','Dhananjaya(N)','no','','|DUMMY','E3456','qas|','2019-10-25|','2019-10-25',NULL,NULL,NULL,NULL,NULL,NULL),(12032,'18-318A','Magellan Aerospace Wrexham','HALF CLAMP','M038080/27403A','D574 50551 200','DTD 5014','B01',1,'175170','','98765','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','SPOT FACE DEPTH OVERSIZED 11.0 to 11.3 (Measured at 10.4 Depth)','chips Hold in  Butting Face of the fixture |hole deburr Missed Before starting the next operation . |work instruction  was not sufficient to capture the requirements, the MPS dose not call for Deburring  requirement.|operation sketch in not available to the operator to perform the operation per the during.  ','hole Deurr done for all the Parts And next run the part found ok.','feeler Gauge checking Implementation done in next production Batch, Operation sketch to be provide by Engineering team.  ','CA\\PA FOUND OK','','2019-10-23','Anjinamurthy(H)','Suresh(K.R.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','7','no','Misc','Dhananjaya(N)','no','','Defect found visually on the Part so immediately stop the machine and checked.  ','E3456','qas|','2019-10-25|','2019-10-25',NULL,NULL,NULL,NULL,NULL,NULL),(12033,'47-096B','GKN Aerospace Filton','BRACKET FT5 FWD ','W6409','F57550783000','NA','PART ISSUE E04',1,'LTA GKN GS72 - Forgi','','96903','','0000-00-00',NULL,'yes','no','yes','no','yes','no','no','no','no','Bore ovality up to 0.1mm','Pallet error found  B90°TO B270° of 0.2mm |Due to maintenance error after Machine breakdown recovery   |breakage due to overflow of oil in B axis thumb|breakage of oil seal inside the B axis the thumb','|Axis parameter was cross verified & handover the m\\c to the production by maintenance. ','|after the Maintenance all axis\' shall be verified before running the part.\r<br/>oil leakage will be verified during preventive maintenance. ','CAPA found ok','','2019-10-24','Gurukiran S(M)','Niranjan(Murthy)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','09','no','Misc','Gurukiran S(M)','no','','|Immediately machine stopped & serviced the machined','E3456','qas|qas|','2019-10-30|2019-10-30|','2019-10-30',NULL,NULL,NULL,NULL,NULL,NULL),(12034,'35-176A','Saab AB','LATCH_ACT_PIVOT-FTG ','287975B7','423Z1205-2-02','','--B',1,'LTA SAAB B787 Assemb','','97996','','0000-00-00',NULL,'no','yes','yes','yes','no','no','no','no','no','Outer wall dig up to 1.3mm','','','','','','2019-10-24','Dinesh kulal()','prodn_aero(prodn)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','no','yes','no','With Treatment','','3rd','no','Misc','Dinesh kulal()','no','','','A3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(12035,'57A-001','Maini Precision Products Limited','SPIGOT AFT ASSY WING','','F5725104400001','','PART ISSUE A',1,'4500242150','','A30097','','0000-00-00',NULL,'no','no','no','no','no','no','yes','yes','yes','Sealant used for assy   was not as per the customer Requirement','w1: -MC780C was used instead of MC780B sealant.   |w2: - Engineer designing the process missed to capture the “Fillet or Low Adhesion sealant to                                       ABP 4- 5142” requirement from the “Appendix A” of ABP 2-2082.|w3: - Engineer did not went through the entire specification while defining the process.  ','|Routing was revised as per the requirement and new FAIR part assembled and shipped to customer.','|Routings will be cross verified by the authorized personnel in engineering before releasing for use in the shop floor.','As per customer Requirement Parts Rework to be done and APS Rev 01.','C84075','2019-10-25','Ravindra(Kumar)','Ravindra(Kumar)','Not raised','2019-10-25','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','Cust','yes','Misc','Ravindra(Kumar)','no','','|1) Immediately informed the customer about the escapement and requested to return the part for rework,\r\n   \r\n2) Engineer checked the routing of previous assemblies with similar drawing call out and found them to be correct as per the requirement. ','E3456','qas_sez|','2019-11-07|','2019-11-07',NULL,NULL,NULL,NULL,NULL,NULL),(12036,'57A-002','Maini Precision Products Limited','SPIGOT AFT ASSY WING','','F5725104400101','','PART ISSUE  A',1,'4500242150','','A30098','','0000-00-00',NULL,'no','no','no','no','no','no','yes','yes','yes',' Sealant used for assy   was not as per the customer Requirement','w1: -MC780C was used instead of MC780B sealant.   |w2: - Engineer designing the process missed to capture the “Fillet or Low Adhesion sealant to                                       ABP 4- 5142” requirement from the “Appendix A” of ABP 2-2082.|w3: - Engineer did not went through the entire specification while defining the process.  |  \r\n\r\n','|:- Routing was revised as per the requirement and new FAIR part assembled and shipped to customer.','|Routings will be cross verified by the authorized personnel in engineering before releasing for use in the shop floor.','APS revision verified and FAIR part assembled verified by Customer and found ok.','C84076','2019-10-25','Ravindra(Kumar)','Ravindra(Kumar)','Not raised','2019-10-25','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','Cust','yes','Misc','Ravindra(Kumar)','no','','|1) Immediately informed the customer about the escapement and requested to return the part for rework, \r\n\r\n\r\n2) Engineer checked the routing of previous assemblies with similar drawing call out and found them to be correct as per the requirement. ','E3456','qas_sez|','2019-11-07|','2019-11-07',NULL,NULL,NULL,NULL,NULL,NULL),(12037,'57A-003','Maini Precision Products Limited','SPIGOT FWD ASSY WING','','F5725104500001','','PART ISSUE  A',1,'4500242150','','A30099','','0000-00-00',NULL,'no','no','no','no','no','no','yes','yes','yes','Sealant used for assy   was not as per the customer Requirement','w1: -MC780C was used instead of MC780B sealant.   |w2: - Engineer designing the process missed to capture the “Fillet or Low Adhesion sealant to                                       ABP 4- 5142” requirement from the “Appendix A” of ABP 2-2082.|w3: - Engineer did not went through the entire specification while defining the process.  ','|Routing was revised as per the requirement and new FAIR part assembled and shipped to customer.','|Routings will be cross verified by the authorized personnel in engineering before releasing for use in the shop floor.','APS revision verified and FAIR part assembled verified by Customer and found ok.','C84077','2019-10-25','Ravindra(Kumar)','Ravindra(Kumar)','Not raised','2019-10-25','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','Cust','yes','Misc','Ravindra(Kumar)','no','','|1) Immediately informed the customer about the escapement and requested to return the part for rework,   \r\n\r\n\r\n2) Engineer checked the routing of previous assemblies with similar drawing call out and found them to be correct as per the requirement. ','E3456','qas_sez|','2019-11-07|','2019-11-07',NULL,NULL,NULL,NULL,NULL,NULL),(12038,'57A-004','Maini Precision Products Limited','SPIGOT FWD ASSY WING','','F5725104500101','','PART ISSUE A',1,'4500242150','','A30100','','0000-00-00',NULL,'no','no','no','no','no','no','yes','yes','yes','Sealant used for assy   was not as per the customer Requirement','w1: -MC780C was used instead of MC780B sealant.   |w2: - Engineer designing the process missed to capture the “Fillet or Low Adhesion sealant to                                       ABP 4- 5142” requirement from the “Appendix A” of ABP 2-2082.|w3: - Engineer did not went through the entire specification while defining the process.  | ','|Routing was revised as per the requirement and new FAIR part assembled and shipped to customer.','|Routings will be cross verified by the authorized personnel in engineering before releasing for use in the shop floor.','APS revision verified and FAIR part assembled verified by Customer and found ok.','C84206','2019-10-25','Ravindra(Kumar)','Ravindra(Kumar)','Not raised','2019-10-25','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','Cust','yes','Misc','Ravindra(Kumar)','no','','|1) Immediately informed the customer about the escapement and requested to return the part for rework,   \r\n\r\n2) Engineer checked the routing of previous assemblies with similar drawing call out and found them to be correct as per the requirement.','E3456','qas_sez|','2019-11-07|','2019-11-07',NULL,NULL,NULL,NULL,NULL,NULL),(12039,'35-548','Saab AB','LIFT ARM','814285','D522 73353 201 00','','PART ISSUE A',1,'OWED-LTA-004','','97774','','0000-00-00',NULL,'yes','no','yes','no','yes','no','no','no','no','BORE OVER SIZE','','','','','','2019-10-25','Dinesh kulal()','prodn_aero(prodn)','','0000-00-00','BORE OVER SIZE ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','no','yes','no','With Treatment','','1ST','no','Misc','Dinesh kulal()','no','','','A3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(12040,'47-096B','GKN Aerospace Filton','BRACKET FT5 FWD ','W6409','F57550783000','NA','PART ISSUE E04',1,'LTA GKN GS72 - Forgi','','96903','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Bore dig mark found ','Tool marks formed in the bore of the part due to vibration of the part while experiencing sudden overload|The tool used for forming the countersink in the walls of the part did not had sufficient clearance to pass through the bore of the part.|The bore diameter was not finished to the requirement and was maintained in stock to achieve the hole position and was planned to be done in an alternate machine.|Due to X-axis error in the machine the bore was planned to be finished in an alternative machine.','|Work center and process was changed and parts were proved in alternate machine and the production continued.','|Machine axis errors will be identified and rectified during the preventive maintenance and the same shall be verified by making an artifact part before starting the production after identifying and rectifying the axis errors.','CA PA FOUND OK','','2019-10-25','Gurukiran S(M)','Shivanand(D.B.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','09','no','Misc','Gurukiran S(M)','no','','|Immediately stop the machine checked all the similar parts which were machined and no deviations were identified.','E3456','qas|','2019-11-20|','2019-11-20',NULL,NULL,NULL,NULL,NULL,NULL),(12041,'35A-518','Saab AB','ROD ASSY','','D522 73510 000 00','','A',2,'OWED-LTA-004','','A26589','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','We have found an issue with the breakaway torque for the spherical bearing in AS81935-1-4K. Today we\r\nare suspecting all assemblies including the AS81935-1-4K. According to M81935/1 Self-Lubricated\r\nRod End Bearings the breakaway torque should be 0.5 – 6.0 in.-lbs (0.06 – 0.68 Nm). Non-conforming\r\nRod Ends have one or two bearings with breakaway torque above 0.68 Nm. ','1)The breakaway torque measured on the rod ends were not as per the customer requirement.|2)CIM was inspecting the bearings with bolt and nut through bearings and tightening with and checked the torque. But at SAAB the bolt and nut was torque tightened to 6.3Nm before checking the breakaway torque of the bearing which i not as per the drawing requirement.|3)SAAB selection of Bearing for the assembly was not as per the SAAB higher assembly requirement.','|Informed the bearing supplier about the failure of the bearing during torque test and requested to inspect 100% before shipment.','|SAAB to analyze and revise the drawing according to their higher assembly requirement.','CIM BOM will be changed upon the receipt of revised drawing / instruction from SAAB','C80281','2019-10-26','Dharani(Shankar)','','TR-SAA-89947','2019-10-26','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER END','yes','','Dharani(Shankar)','no','','|Checked the bearings to SAAB specific requirements and change the affected bearings.','Z3456','qas_sez|','2019-12-23|','2019-12-23','0000-00-00','0000-00-00','0000-00-00','','',''),(12042,'35A-518','Saab AB','ROD ASSY','','D522 73510 000 00','','A',4,'OWED-LTA-004','','A26588','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','We have found an issue with the breakaway torque for the spherical bearing in AS81935-1-4K. Today we\r\nare suspecting all assemblies including the AS81935-1-4K. According to M81935/1 Self-Lubricated\r\nRod End Bearings the breakaway torque should be 0.5 – 6.0 in.-lbs (0.06 – 0.68 Nm). Non-conforming\r\nRod Ends have one or two bearings with breakaway torque above 0.68 Nm. ','1)The breakaway torque measured on the rod ends were not as per the customer requirement.|2)CIM was inspecting the bearings with bolt and nut through bearings and tightening with and checked the torque. But at SAAB the bolt and nut was torque tightened to 6.3Nm before checking the breakaway torque of the bearing which i not as per the drawing requirement.|3)SAAB selection of Bearing for the assembly was not as per the SAAB higher assembly requirement.','|Informed the bearing supplier about the failure of the bearing during torque test and requested to inspect 100% before shipment.','|SAAB to analyze and revise the drawing according to their higher assembly requirement.','CA PA Found ok.','C80281','2019-10-26','Dharani(Shankar)','qas_sez(a)','TR-SAAI-89947','2019-10-26','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER END','yes','Misc','qas_sez(a)','no','','|Checked the bearings to SAAB specific requirements and change the affected bearings.','Z3456','qas_sez|','2019-11-12|','2019-11-12',NULL,NULL,NULL,NULL,NULL,NULL),(12043,'35A-501','Saab AB','ROD Assy','','D522 73494 000 00','','A',4,'OWED-LTA-004','','A23554','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','We have found an issue with the breakaway torque for the spherical bearing in AS81935-1-4K. Today we\r\nare suspecting all assemblies including the AS81935-1-4K. According to M81935/1 Self-Lubricated\r\nRod End Bearings the breakaway torque should be 0.5 – 6.0 in.-lbs (0.06 – 0.68 Nm). Non-conforming\r\nRod Ends have one or two bearings with breakaway torque above 0.68 Nm. ','1)The breakaway torque measured on the rod ends were not as per the customer requirement|2)CIM was inspecting the bearings with bolt and nut through bearings and tightening with and checked the torque. But at SAAB the bolt and nut was torque tightened to 6.3Nm before checking the breakaway torque of the bearing which i not as per the drawing requirement.|3)SAAB selection of Bearing for the assembly was not as per the SAAB higher assembly requirement.','|Informed the bearing supplier about the failure of the bearing during torque test and requested to inspect 100% before shipment.','|SAAB to analyze and revise the drawing according to their higher assembly requirement.\r<br/>','CIM BOM will be changed upon the receipt of revised drawing / instruction from SAAB','C76255','2019-10-26','Dharani(Shankar)','qas_sez(a)','TR-SAAI-90515','2019-10-26','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER END','yes','Misc','Dharani(Shankar)','no','','|Checked the bearings to SAAB specific requirements and change the affected bearings.','Z3456','qas_sez|','2019-11-25|','2019-11-25','0000-00-00','0000-00-00','0000-00-00','','',''),(12044,'35A-501','Saab AB','ROD Assy','','D522 73494 000 00','','A',1,'1600217568','','A22406','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','We have found an issue with the breakaway torque for the spherical bearing in AS81935-1-4K. Today we\r\nare suspecting all assemblies including the AS81935-1-4K. According to M81935/1 Self-Lubricated\r\nRod End Bearings the breakaway torque should be 0.5 – 6.0 in.-lbs (0.06 – 0.68 Nm). Non-conforming\r\nRod Ends have one or two bearings with breakaway torque above 0.68 Nm. ','1)The breakaway torque measured on the rod ends were not as per the customer requirement.|2)CIM was inspecting the bearings with bolt and nut through bearings and tightening with and checked the torque. But at SAAB the bolt and nut was torque tightened to 6.3Nm before checking the breakaway torque of the bearing which i not as per the drawing requirement.|3)SAAB selection of Bearing for the assembly was not as per the SAAB higher assembly requirement.','|Informed the bearing supplier about the failure of the bearing during torque test and requested to inspect 100% before shipment.','|SAAB to analyze and revise the drawing according to their higher assembly requirement.','CIM BOM will be changed upon the receipt of revised drawing / instruction from SAAB','C74921','2019-10-26','Dharani(Shankar)','qas_sez(a)','TR-SAAI-90515','2019-10-26','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER END','yes','Misc','Dharani(Shankar)','no','','|Checked the bearings to SAAB specific requirements and change the affected bearings.','Z3456','qas_sez|','2019-11-25|','2019-11-25','0000-00-00','0000-00-00','0000-00-00','','',''),(12045,'35A-501','Saab AB','ROD Assy','','D522 73494 000 00','','A',2,'OWED-LTA-004','','A22404','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','We have found an issue with the breakaway torque for the spherical bearing in AS81935-1-4K. Today we\r\nare suspecting all assemblies including the AS81935-1-4K. According to M81935/1 Self-Lubricated\r\nRod End Bearings the breakaway torque should be 0.5 – 6.0 in.-lbs (0.06 – 0.68 Nm). Non-conforming\r\nRod Ends have one or two bearings with breakaway torque above 0.68 Nm. ','1)The breakaway torque measured on the rod ends were not as per the customer requirement.|2)CIM was inspecting the bearings with bolt and nut through bearings and tightening with and checked the torque. But at SAAB the bolt and nut was torque tightened to 6.3Nm before checking the breakaway torque of the bearing which i not as per the drawing requirement.|3)SAAB selection of Bearing for the assembly was not as per the SAAB higher assembly requirement.','|Informed the bearing supplier about the failure of the bearing during torque test and requested to inspect 100% before shipment.','|SAAB to analyze and revise the drawing according to their higher assembly requirement.','CIM BOM will be changed upon the receipt of revised drawing / instruction from SAAB','C74920','2019-10-26','Dharani(Shankar)','qas_sez(a)','TR-SAAI-90515','2019-10-26','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER END','yes','Misc','Dharani(Shankar)','no','','|Checked the bearings to SAAB specific requirements and change the affected bearings.','Z3456','qas_sez|','2019-11-25|','2019-11-25','0000-00-00','0000-00-00','0000-00-00','','',''),(12046,'35A-501','Saab AB','ROD ASSY','','D522 73494 000 00','','A',4,'1600217568','','A23635','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','We have found an issue with the breakaway torque for the spherical bearing in AS81935-1-4K. Today we\r\nare suspecting all assemblies including the AS81935-1-4K. According to M81935/1 Self-Lubricated\r\nRod End Bearings the breakaway torque should be 0.5 – 6.0 in.-lbs (0.06 – 0.68 Nm). Non-conforming\r\nRod Ends have one or two bearings with breakaway torque above 0.68 Nm. ','1)The breakaway torque measured on the rod ends were not as per the customer requirement.|2)CIM was inspecting the bearings with bolt and nut through bearings and tightening with and checked the torque. But at SAAB the bolt and nut was torque tightened to 6.3Nm before checking the breakaway torque of the bearing which i not as per the drawing requirement.|3)SAAB selection of Bearing for the assembly was not as per the SAAB higher assembly requirement.','|Informed the bearing supplier about the failure of the bearing during torque test and requested to inspect 100% before shipment.','|SAAB to analyze and revise the drawing according to their higher assembly requirement.','CIM BOM will be changed upon the receipt of revised drawing / instruction from SAAB','C76649','2019-10-26','Dharani(Shankar)','qas_sez(a)','TR-SAAI-90515','2019-10-26','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER END','yes','Misc','Dharani(Shankar)','no','','|Checked the bearings to SAAB specific requirements and change the affected bearings.','Z3456','qas_sez|','2019-11-25|','2019-11-25','0000-00-00','0000-00-00','0000-00-00','','',''),(12047,'35A-501','Saab AB','ROD ASSY','','D522 73494 000 00','','A',2,'OWED-LTA-005','','A23964','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','We have found an issue with the breakaway torque for the spherical bearing in AS81935-1-4K. Today we\r\nare suspecting all assemblies including the AS81935-1-4K. According to M81935/1 Self-Lubricated\r\nRod End Bearings the breakaway torque should be 0.5 – 6.0 in.-lbs (0.06 – 0.68 Nm). Non-conforming\r\nRod Ends have one or two bearings with breakaway torque above 0.68 Nm. ','1)The breakaway torque measured on the rod ends were not as per the customer requirement.|2)CIM was inspecting the bearings with bolt and nut through bearings and tightening with and checked the torque. But at SAAB the bolt and nut was torque tightened to 6.3Nm before checking the breakaway torque of the bearing which i not as per the drawing requirement.|3)SAAB selection of Bearing for the assembly was not as per the SAAB higher assembly requirement.','|Informed the bearing supplier about the failure of the bearing during torque test and requested to inspect 100% before shipment.','|SAAB to analyze and revise the drawing according to their higher assembly requirement.','CIM BOM will be changed upon the receipt of revised drawing / instruction from SAAB','C76992','2019-10-26','Dharani(Shankar)','qas_sez(a)','TR-SAAI-90515','2019-10-26','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER END','yes','Misc','Dharani(Shankar)','no','','|Checked the bearings to SAAB specific requirements and change the affected bearings.','Z3456','qas_sez|','2019-11-25|','2019-11-25','0000-00-00','0000-00-00','0000-00-00','','',''),(12048,'35A-501','Saab AB','ROD ASSY','','D522 73494 000 00','','A',1,'OWED-LTA-005','','A23965','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','We have found an issue with the breakaway torque for the spherical bearing in AS81935-1-4K. Today we\r\nare suspecting all assemblies including the AS81935-1-4K. According to M81935/1 Self-Lubricated\r\nRod End Bearings the breakaway torque should be 0.5 – 6.0 in.-lbs (0.06 – 0.68 Nm). Non-conforming\r\nRod Ends have one or two bearings with breakaway torque above 0.68 Nm. ','1)The breakaway torque measured on the rod ends were not as per the customer requirement.|2)CIM was inspecting the bearings with bolt and nut through bearings and tightening with and checked the torque. But at SAAB the bolt and nut was torque tightened to 6.3Nm before checking the breakaway torque of the bearing which i not as per the drawing requirement.|3)SAAB selection of Bearing for the assembly was not as per the SAAB higher assembly requirement.','|Informed the bearing supplier about the failure of the bearing during torque test and requested to inspect 100% before shipment.','|SAAB to analyze and revise the drawing according to their higher assembly requirement.','CIM BOM will be changed upon the receipt of revised drawing / instruction from SAAB','C76992','2019-10-26','Dharani(Shankar)','qas_sez(a)','TR-SAAI-90515','2019-10-26','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER END','yes','Misc','Dharani(Shankar)','no','','|Checked the bearings to SAAB specific requirements and change the affected bearings.','Z3456','qas_sez|','2019-11-25|','2019-11-25','0000-00-00','0000-00-00','0000-00-00','','',''),(12049,'35A-501','Saab AB','ROD ASSY','','D522 73494 000 00','','A',1,'OWED-LTA-005','','A23963','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','We have found an issue with the breakaway torque for the spherical bearing in AS81935-1-4K. Today we\r\nare suspecting all assemblies including the AS81935-1-4K. According to M81935/1 Self-Lubricated\r\nRod End Bearings the breakaway torque should be 0.5 – 6.0 in.-lbs (0.06 – 0.68 Nm). Non-conforming\r\nRod Ends have one or two bearings with breakaway torque above 0.68 Nm. ','1)The breakaway torque measured on the rod ends were not as per the customer requirement.|2)CIM was inspecting the bearings with bolt and nut through bearings and tightening with and checked the torque. But at SAAB the bolt and nut was torque tightened to 6.3Nm before checking the breakaway torque of the bearing which i not as per the drawing requirement.|3)SAAB selection of Bearing for the assembly was not as per the SAAB higher assembly requirement.','|Informed the bearing supplier about the failure of the bearing during torque test and requested to inspect 100% before shipment.','|SAAB to analyze and revise the drawing according to their higher assembly requirement.','CIM BOM will be changed upon the receipt of revised drawing / instruction from SAAB','C76992','2019-10-26','Dharani(Shankar)','qas_sez(a)','TR-SAAI-90515','2019-10-26','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER END','yes','Misc','Dharani(Shankar)','no','','|Checked the bearings to SAAB specific requirements and change the affected bearings.','Z3456','qas_sez|','2019-11-25|','2019-11-25','0000-00-00','0000-00-00','0000-00-00','','',''),(12050,'35A-501','Saab AB','ROD Assy','','D522 73494 000 00','','A',1,'OWED-LTA-004','','A23558','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','We have found an issue with the breakaway torque for the spherical bearing in AS81935-1-4K. Today we\r\nare suspecting all assemblies including the AS81935-1-4K. According to M81935/1 Self-Lubricated\r\nRod End Bearings the breakaway torque should be 0.5 – 6.0 in.-lbs (0.06 – 0.68 Nm). Non-conforming\r\nRod Ends have one or two bearings with breakaway torque above 0.68 Nm. ','1)The breakaway torque measured on the rod ends were not as per the customer requirement.|2)CIM was inspecting the bearings with bolt and nut through bearings and tightening with and checked the torque. But at SAAB the bolt and nut was torque tightened to 6.3Nm before checking the breakaway torque of the bearing which i not as per the drawing requirement.|3)SAAB selection of Bearing for the assembly was not as per the SAAB higher assembly requirement.','|Informed the bearing supplier about the failure of the bearing during torque test and requested to inspect 100% before shipment.','|SAAB to analyze and revise the drawing according to their higher assembly requirement.','CIM BOM will be changed upon the receipt of revised drawing / instruction from SAAB','C76647','2019-10-26','Dharani(Shankar)','qas_sez(a)','TR-SAAI-90515','2019-10-14','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER END','yes','Misc','Dharani(Shankar)','no','','|Checked the bearings to SAAB specific requirements and change the affected bearings.','Z3456','qas_sez|','2019-11-25|','2019-11-25','0000-00-00','0000-00-00','0000-00-00','','',''),(12051,'35A-501','Saab AB','ROD ASSY','','D522 73494 000 00','','A',14,'OWED-LTA-004','','A23634','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','We have found an issue with the breakaway torque for the spherical bearing in AS81935-1-4K. Today we\r\nare suspecting all assemblies including the AS81935-1-4K. According to M81935/1 Self-Lubricated\r\nRod End Bearings the breakaway torque should be 0.5 – 6.0 in.-lbs (0.06 – 0.68 Nm). Non-conforming\r\nRod Ends have one or two bearings with breakaway torque above 0.68 Nm. ','1)The breakaway torque measured on the rod ends were not as per the customer requirement.|2)CIM was inspecting the bearings with bolt and nut through bearings and tightening with and checked the torque. But at SAAB the bolt and nut was torque tightened to 6.3Nm before checking the breakaway torque of the bearing which i not as per the drawing requirement.|3)SAAB selection of Bearing for the assembly was not as per the SAAB higher assembly requirement.','|Informed the bearing supplier about the failure of the bearing during torque test and requested to inspect 100% before shipment.','|SAAB to analyze and revise the drawing according to their higher assembly requirement.','CIM BOM will be changed upon the receipt of revised drawing / instruction from SAAB','C76649','2019-10-26','Dharani(Shankar)','qas_sez(a)','TR-SAAI-90515','2019-10-14','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER END','yes','Misc','Dharani(Shankar)','no','','|Checked the bearings to SAAB specific requirements and change the affected bearings','Z3456','qas_sez|','2019-11-25|','2019-11-25','0000-00-00','0000-00-00','0000-00-00','','',''),(12052,'35A-501','Saab AB','ROD ASSY','','D522 73494 000 00','','A',23,'OWED-LTA-004','','A23632','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','We have found an issue with the breakaway torque for the spherical bearing in AS81935-1-4K. Today we\r\nare suspecting all assemblies including the AS81935-1-4K. According to M81935/1 Self-Lubricated\r\nRod End Bearings the breakaway torque should be 0.5 – 6.0 in.-lbs (0.06 – 0.68 Nm). Non-conforming\r\nRod Ends have one or two bearings with breakaway torque above 0.68 Nm. ','1)The breakaway torque measured on the rod ends were not as per the customer requirement.|2)CIM was inspecting the bearings with bolt and nut through bearings and tightening with and checked the torque. But at SAAB the bolt and nut was torque tightened to 6.3Nm before checking the breakaway torque of the bearing which i not as per the drawing requirement.|3)SAAB selection of Bearing for the assembly was not as per the SAAB higher assembly requirement.','|Informed the bearing supplier about the failure of the bearing during torque test and requested to inspect 100% before shipment.','|SAAB to analyze and revise the drawing according to their higher assembly requirement.','CIM BOM will be changed upon the receipt of revised drawing / instruction from SAAB','C76649','2019-10-26','Dharani(Shankar)','qas_sez(a)','TR-SAAI-90515','2019-10-14','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER END','yes','Misc','Dharani(Shankar)','no','','|Checked the bearings to SAAB specific requirements and change the affected bearings.','Z3456','qas_sez|','2019-11-25|','2019-11-25','0000-00-00','0000-00-00','0000-00-00','','',''),(12053,'35A-501','Saab AB','ROD ASSY','','D522 73494 000 00','','A',37,'OWED-LTA-004','','A23631','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','We have found an issue with the breakaway torque for the spherical bearing in AS81935-1-4K. Today we\r\nare suspecting all assemblies including the AS81935-1-4K. According to M81935/1 Self-Lubricated\r\nRod End Bearings the breakaway torque should be 0.5 – 6.0 in.-lbs (0.06 – 0.68 Nm). Non-conforming\r\nRod Ends have one or two bearings with breakaway torque above 0.68 Nm. ','1)The breakaway torque measured on the rod ends were not as per the customer requirement.|2)CIM was inspecting the bearings with bolt and nut through bearings and tightening with and checked the torque. But at SAAB the bolt and nut was torque tightened to 6.3Nm before checking the breakaway torque of the bearing which i not as per the drawing requirement.|3)SAAB selection of Bearing for the assembly was not as per the SAAB higher assembly requirement.','|Informed the bearing supplier about the failure of the bearing during torque test and requested to inspect 100% before shipment.','|SAAB to analyze and revise the drawing according to their higher assembly requirement.','CIM BOM will be changed upon the receipt of revised drawing / instruction from SAAB','C76647','2019-10-26','Dharani(Shankar)','qas_sez(a)','TR-SAAI-90515','2019-10-14','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER END','yes','Misc','Dharani(Shankar)','no','','|Checked the bearings to SAAB specific requirements and change the affected bearings.','Z3456','qas_sez|','2019-11-25|','2019-11-25','0000-00-00','0000-00-00','0000-00-00','','',''),(12054,'35A-518','Saab AB','ROD ASSY','','D522 73510 000 00','','A',24,'OWED-LTA-005','','A24927','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','We have found an issue with the breakaway torque for the spherical bearing in AS81935-1-4K. Today we\r\nare suspecting all assemblies including the AS81935-1-4K. According to M81935/1 Self-Lubricated\r\nRod End Bearings the breakaway torque should be 0.5 – 6.0 in.-lbs (0.06 – 0.68 Nm). Non-conforming\r\nRod Ends have one or two bearings with breakaway torque above 0.68 Nm. ','1)The breakaway torque measured on the rod ends were not as per the customer requirement.|2)CIM was inspecting the bearings with bolt and nut through bearings and tightening with and checked the torque. But at SAAB the bolt and nut was torque tightened to 6.3Nm before checking the breakaway torque of the bearing which i not as per the drawing requirement.|3)SAAB selection of Bearing for the assembly was not as per the SAAB higher assembly requirement.','|Informed the bearing supplier about the failure of the bearing during torque test and requested to inspect 100% before shipment.','|SAAB to analyze and revise the drawing according to their higher assembly requirement.','CA PA Found ok.','C78774','2019-10-26','Dharani(Shankar)','qas_sez(a)','TR-SAAI-90515','2019-10-14','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER END','yes','Misc','Dharani(Shankar)','no','','|Checked the bearings to SAAB specific requirements and change the affected bearings.','Z3456','qas_sez|','2019-11-12|','2019-11-12',NULL,NULL,NULL,NULL,NULL,NULL),(12055,'35A-518','Saab AB','ROD ASSY','','D522 73510 000 00','','A',27,'OWED-LTA-005','','A24928','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','We have found an issue with the breakaway torque for the spherical bearing in AS81935-1-4K. Today we\r\nare suspecting all assemblies including the AS81935-1-4K. According to M81935/1 Self-Lubricated\r\nRod End Bearings the breakaway torque should be 0.5 – 6.0 in.-lbs (0.06 – 0.68 Nm). Non-conforming\r\nRod Ends have one or two bearings with breakaway torque above 0.68 Nm. ','1)The breakaway torque measured on the rod ends were not as per the customer requirement.|2)CIM was inspecting the bearings with bolt and nut through bearings and tightening with and checked the torque. But at SAAB the bolt and nut was torque tightened to 6.3Nm before checking the breakaway torque of the bearing which i not as per the drawing requirement.|3)SAAB selection of Bearing for the assembly was not as per the SAAB higher assembly requirement.','|Informed the bearing supplier about the failure of the bearing during torque test and requested to inspect 100% before shipment.','|SAAB to analyze and revise the drawing according to their higher assembly requirement.','CA PA Found ok.','C78774','2019-10-26','Dharani(Shankar)','qas_sez(a)','TR-SAAI-90515','2019-10-14','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER END','yes','Misc','Dharani(Shankar)','no','','|Checked the bearings to SAAB specific requirements and change the affected bearings.','Z3456','qas_sez|','2019-11-12|','2019-11-12',NULL,NULL,NULL,NULL,NULL,NULL),(12056,'35A-470','Saab AB','ASSY ROD','','D522 73514 001 00','','A',1,'OWED-LTA-004','','K24602','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','We have found an issue with the breakaway torque for the spherical bearing in AS81935-1-4K. Today we\r\nare suspecting all assemblies including the AS81935-1-4K. According to M81935/1 Self-Lubricated\r\nRod End Bearings the breakaway torque should be 0.5 – 6.0 in.-lbs (0.06 – 0.68 Nm). Non-conforming\r\nRod Ends have one or two bearings with breakaway torque above 0.68 Nm. ','1)The breakaway torque measured on the rod ends were not as per the customer requirement.|2)CIM was inspecting the bearings with bolt and nut through bearings and tightening with and checked the torque. But at SAAB the bolt and nut was torque tightened to 6.3Nm before checking the breakaway torque of the bearing which i not as per the drawing requirement.|3)SAAB selection of Bearing for the assembly was not as per the SAAB higher assembly requirement.','|Informed the bearing supplier about the failure of the bearing during torque test and requested to inspect 100% before shipment.','|SAAB to analyze and revise the drawing according to their higher assembly requirement.','CIM BOM will be changed upon the receipt of revised drawing / instruction from SAAB','C78048','2019-10-26','Dharani(Shankar)','qas_sez(a)','TR-SAAI-90515','2019-10-14','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER END','yes','Misc','Dharani(Shankar)','no','','|Checked the bearings to SAAB specific requirements and change the affected bearings.','Z3456','qas_sez|','2019-11-25|','2019-11-25','0000-00-00','0000-00-00','0000-00-00','','',''),(12057,'35A-470','Saab AB','ASSY ROD','','D522 73514 001 00','','A',2,'OWED-LTA-004','','K24603','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','We have found an issue with the breakaway torque for the spherical bearing in AS81935-1-4K. Today we\r\nare suspecting all assemblies including the AS81935-1-4K. According to M81935/1 Self-Lubricated\r\nRod End Bearings the breakaway torque should be 0.5 – 6.0 in.-lbs (0.06 – 0.68 Nm). Non-conforming\r\nRod Ends have one or two bearings with breakaway torque above 0.68 Nm. ','1)The breakaway torque measured on the rod ends were not as per the customer requirement.|2)CIM was inspecting the bearings with bolt and nut through bearings and tightening with and checked the torque. But at SAAB the bolt and nut was torque tightened to 6.3Nm before checking the breakaway torque of the bearing which i not as per the drawing requirement.|3)SAAB selection of Bearing for the assembly was not as per the SAAB higher assembly requirement.','|Informed the bearing supplier about the failure of the bearing during torque test and requested to inspect 100% before shipment.','|SAAB to analyze and revise the drawing according to their higher assembly requirement.','CIM BOM will be changed upon the receipt of revised drawing / instruction from SAAB','C78049','2019-10-26','Dharani(Shankar)','qas_sez(a)','TR-SAAI-90515','2019-10-14','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER END','yes','Misc','Dharani(Shankar)','no','','|Checked the bearings to SAAB specific requirements and change the affected bearings.','Z3456','qas_sez|','2019-11-25|','2019-11-25','0000-00-00','0000-00-00','0000-00-00','','',''),(12058,'35A-470','Saab AB','ASSY ROD','','D522 73514 001 00','','A',12,'OWED-LTA-004','','K24605','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','We have found an issue with the breakaway torque for the spherical bearing in AS81935-1-4K. Today we\r\nare suspecting all assemblies including the AS81935-1-4K. According to M81935/1 Self-Lubricated\r\nRod End Bearings the breakaway torque should be 0.5 – 6.0 in.-lbs (0.06 – 0.68 Nm). Non-conforming\r\nRod Ends have one or two bearings with breakaway torque above 0.68 Nm. ','1)The breakaway torque measured on the rod ends were not as per the customer requirement.|2)CIM was inspecting the bearings with bolt and nut through bearings and tightening with and checked the torque. But at SAAB the bolt and nut was torque tightened to 6.3Nm before checking the breakaway torque of the bearing which i not as per the drawing requirement.|3)SAAB selection of Bearing for the assembly was not as per the SAAB higher assembly requirement.','|Informed the bearing supplier about the failure of the bearing during torque test and requested to inspect 100% before shipment.','|SAAB to analyze and revise the drawing according to their higher assembly requirement.','CIM BOM will be changed upon the receipt of revised drawing / instruction from SAAB','C78051','2019-10-26','Dharani(Shankar)','qas_sez(a)','TR-SAAI-90515','2019-10-14','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER END','yes','Misc','Dharani(Shankar)','no','','|Checked the bearings to SAAB specific requirements and change the affected bearings.','Z3456','qas_sez|','2019-11-25|','2019-11-25','0000-00-00','0000-00-00','0000-00-00','','',''),(12059,'35A-469','Saab AB','ASSY ROD','','D522 73514 000 00','','A',2,'OWED-LTA-005','','K21700','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','We have found an issue with the breakaway torque for the spherical bearing in AS81935-1-4K. Today we\r\nare suspecting all assemblies including the AS81935-1-4K. According to M81935/1 Self-Lubricated\r\nRod End Bearings the breakaway torque should be 0.5 – 6.0 in.-lbs (0.06 – 0.68 Nm). Non-conforming\r\nRod Ends have one or two bearings with breakaway torque above 0.68 Nm. ','1)The breakaway torque measured on the rod ends were not as per the customer requirement.|2)CIM was inspecting the bearings with bolt and nut through bearings and tightening with and checked the torque. But at SAAB the bolt and nut was torque tightened to 6.3Nm before checking the breakaway torque of the bearing which i not as per the drawing requirement.|3)SAAB selection of Bearing for the assembly was not as per the SAAB higher assembly requirement.','|Informed the bearing supplier about the failure of the bearing during torque test and requested to inspect 100% before shipment.','|SAAB to analyze and revise the drawing according to their higher assembly requirement.','CIM BOM will be changed upon the receipt of revised drawing / instruction from SAAB','C73600','2019-10-26','Dharani(Shankar)','qas_sez(a)','TR-SAAI-90515','2019-10-14','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER END','yes','Misc','Dharani(Shankar)','no','','|Checked the bearings to SAAB specific requirements and change the affected bearings.','Z3456','qas_sez|','2019-11-26|','2019-11-26','0000-00-00','0000-00-00','0000-00-00','','',''),(12060,'35A-469','Saab AB','ASSY ROD','','D522 73514 000 00','','A',1,'OWED-LTA-005','','K21701','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','We have found an issue with the breakaway torque for the spherical bearing in AS81935-1-4K. Today we\r\nare suspecting all assemblies including the AS81935-1-4K. According to M81935/1 Self-Lubricated\r\nRod End Bearings the breakaway torque should be 0.5 – 6.0 in.-lbs (0.06 – 0.68 Nm). Non-conforming\r\nRod Ends have one or two bearings with breakaway torque above 0.68 Nm. ','1)The breakaway torque measured on the rod ends were not as per the customer requirement.|2)CIM was inspecting the bearings with bolt and nut through bearings and tightening with and checked the torque. But at SAAB the bolt and nut was torque tightened to 6.3Nm before checking the breakaway torque of the bearing which i not as per the drawing requirement.|3)SAAB selection of Bearing for the assembly was not as per the SAAB higher assembly requirement.','|Informed the bearing supplier about the failure of the bearing during torque test and requested to inspect 100% before shipment.','|SAAB to analyze and revise the drawing according to their higher assembly requirement.','CIM BOM will be changed upon the receipt of revised drawing / instruction from SAAB','C73600','2019-10-26','Dharani(Shankar)','qas_sez(a)','TR-SAAI-90515','2019-10-14','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER END','yes','Misc','Dharani(Shankar)','no','','|Checked the bearings to SAAB specific requirements and change the affected bearings.','Z3456','qas_sez|','2019-11-26|','2019-11-26','0000-00-00','0000-00-00','0000-00-00','','',''),(12061,'35A-469','Saab AB','ASSY ROD','','D522 73514 000 00','','A',1,'1600217568','','K24615','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','We have found an issue with the breakaway torque for the spherical bearing in AS81935-1-4K. Today we\r\nare suspecting all assemblies including the AS81935-1-4K. According to M81935/1 Self-Lubricated\r\nRod End Bearings the breakaway torque should be 0.5 – 6.0 in.-lbs (0.06 – 0.68 Nm). Non-conforming\r\nRod Ends have one or two bearings with breakaway torque above 0.68 Nm. ','1)The breakaway torque measured on the rod ends were not as per the customer requirement.|2)CIM was inspecting the bearings with bolt and nut through bearings and tightening with and checked the torque. But at SAAB the bolt and nut was torque tightened to 6.3Nm before checking the breakaway torque of the bearing which i not as per the drawing requirement.|3)SAAB selection of Bearing for the assembly was not as per the SAAB higher assembly requirement.','|Informed the bearing supplier about the failure of the bearing during torque test and requested to inspect 100% before shipment.','|SAAB to analyze and revise the drawing according to their higher assembly requirement.','CIM BOM will be changed upon the receipt of revised drawing / instruction from SAAB','C78032','2019-10-26','Dharani(Shankar)','qas_sez(a)','TR-SAAI-90515','2019-10-14','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER END','yes','Misc','Dharani(Shankar)','no','','|Checked the bearings to SAAB specific requirements and change the affected bearings.','Z3456','qas_sez|','2019-11-26|','2019-11-26','0000-00-00','0000-00-00','0000-00-00','','',''),(12062,'35A-469','Saab AB','ASSY ROD','','D522 73514 000 00','','A',1,'OWED-LTA-004','','K24617','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','We have found an issue with the breakaway torque for the spherical bearing in AS81935-1-4K. Today we\r\nare suspecting all assemblies including the AS81935-1-4K. According to M81935/1 Self-Lubricated\r\nRod End Bearings the breakaway torque should be 0.5 – 6.0 in.-lbs (0.06 – 0.68 Nm). Non-conforming\r\nRod Ends have one or two bearings with breakaway torque above 0.68 Nm. ','1)The breakaway torque measured on the rod ends were not as per the customer requirement.|2)CIM was inspecting the bearings with bolt and nut through bearings and tightening with and checked the torque. But at SAAB the bolt and nut was torque tightened to 6.3Nm before checking the breakaway torque of the bearing which i not as per the drawing requirement.|3)SAAB selection of Bearing for the assembly was not as per the SAAB higher assembly requirement.','|Informed the bearing supplier about the failure of the bearing during torque test and requested to inspect 100% before shipment.','|SAAB to analyze and revise the drawing according to their higher assembly requirement.','CIM BOM will be changed upon the receipt of revised drawing / instruction from SAAB','C78034','2019-10-26','Dharani(Shankar)','qas_sez(a)','TR-SAAI-90515','2019-10-14','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER END','yes','Misc','Dharani(Shankar)','no','','|Checked the bearings to SAAB specific requirements and change the affected bearings.','Z3456','qas_sez|','2019-11-26|','2019-11-26','0000-00-00','0000-00-00','0000-00-00','','',''),(12063,'35A-469','Saab AB','ASSY ROD','','D522 73514 000 00','','A',2,'1600192682','','K24607','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','We have found an issue with the breakaway torque for the spherical bearing in AS81935-1-4K. Today we\r\nare suspecting all assemblies including the AS81935-1-4K. According to M81935/1 Self-Lubricated\r\nRod End Bearings the breakaway torque should be 0.5 – 6.0 in.-lbs (0.06 – 0.68 Nm). Non-conforming\r\nRod Ends have one or two bearings with breakaway torque above 0.68 Nm. ','1)The breakaway torque measured on the rod ends were not as per the customer requirement.|2)CIM was inspecting the bearings with bolt and nut through bearings and tightening with and checked the torque. But at SAAB the bolt and nut was torque tightened to 6.3Nm before checking the breakaway torque of the bearing which i not as per the drawing requirement.|3)SAAB selection of Bearing for the assembly was not as per the SAAB higher assembly requirement.','|Informed the bearing supplier about the failure of the bearing during torque test and requested to inspect 100% before shipment.','|Informed the bearing supplier about the failure of the bearing during torque test and requested to inspect 100% before shipment.','CIM BOM will be changed upon the receipt of revised drawing / instruction from SAAB','C78024','2019-10-26','Dharani(Shankar)','Dharani(Shankar)','TR-SAAI-90515','2019-10-14','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER END','yes','Misc','Dharani(Shankar)','no','','|Checked the bearings to SAAB specific requirements and change the affected bearings.','Z3456','qas_sez|','2019-11-26|','2019-11-26','0000-00-00','0000-00-00','0000-00-00','','',''),(12064,'35A-469','Saab AB','ASSY ROD','','D522 73514 000 00','','A',5,'OWED-LTA-004','','K24608','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','We have found an issue with the breakaway torque for the spherical bearing in AS81935-1-4K. Today we\r\nare suspecting all assemblies including the AS81935-1-4K. According to M81935/1 Self-Lubricated\r\nRod End Bearings the breakaway torque should be 0.5 – 6.0 in.-lbs (0.06 – 0.68 Nm). Non-conforming\r\nRod Ends have one or two bearings with breakaway torque above 0.68 Nm. ','1)The breakaway torque measured on the rod ends were not as per the customer requirement.|2)CIM was inspecting the bearings with bolt and nut through bearings and tightening with and checked the torque. But at SAAB the bolt and nut was torque tightened to 6.3Nm before checking the breakaway torque of the bearing which i not as per the drawing requirement.|3)SAAB selection of Bearing for the assembly was not as per the SAAB higher assembly requirement.','|Informed the bearing supplier about the failure of the bearing during torque test and requested to inspect 100% before shipment.','|SAAB to analyze and revise the drawing according to their higher assembly requirement.','CIM BOM will be changed upon the receipt of revised drawing / instruction from SAAB','C78025','2019-10-26','Dharani(Shankar)','qas_sez(a)','TR-SAAI-90515','2019-10-14','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER END','yes','Misc','Dharani(Shankar)','no','','|Checked the bearings to SAAB specific requirements and change the affected bearings.','Z3456','qas_sez|','2019-11-26|','2019-11-26','0000-00-00','0000-00-00','0000-00-00','','',''),(12065,'35A-665','Saab AB','ROD ASSY','','D5227349400400','','PART ISSUE C',6,'OWED-LTA-001','','A23668','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','We have found an issue with the breakaway torque for the spherical bearing in AS81935-1-4K. Today we\r\nare suspecting all assemblies including the AS81935-1-4K. According to M81935/1 Self-Lubricated\r\nRod End Bearings the breakaway torque should be 0.5 – 6.0 in.-lbs (0.06 – 0.68 Nm). Non-conforming\r\nRod Ends have one or two bearings with breakaway torque above 0.68 Nm. ','1)The breakaway torque measured on the rod ends were not as per the customer requirement.|2)CIM was inspecting the bearings with bolt and nut through bearings and tightening with and checked the torque. But at SAAB the bolt and nut was torque tightened to 6.3Nm before checking the breakaway torque of the bearing which i not as per the drawing requirement.|3)SAAB selection of Bearing for the assembly was not as per the SAAB higher assembly requirement.','|Informed the bearing supplier about the failure of the bearing during torque test and requested to inspect 100% before shipment.','|SAAB to analyze and revise the drawing according to their higher assembly requirement.','CIM BOM will be changed upon the receipt of revised drawing / instruction from SAAB','C76705','2019-10-26','Dharani(Shankar)','qas_sez(a)','TR-SAAI-90515','2019-10-14','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER END','yes','Misc','Dharani(Shankar)','no','','|Checked the bearings to SAAB specific requirements and change the affected bearings.','Z3456','qas_sez|','2019-11-26|','2019-11-26','0000-00-00','0000-00-00','0000-00-00','','',''),(12066,'35A-665','Saab AB','ROD ASSY','','D5227349400400','','PART ISSUE C',1,'OWED-LTA-001','','A23666','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','We have found an issue with the breakaway torque for the spherical bearing in AS81935-1-4K. Today we\r\nare suspecting all assemblies including the AS81935-1-4K. According to M81935/1 Self-Lubricated\r\nRod End Bearings the breakaway torque should be 0.5 – 6.0 in.-lbs (0.06 – 0.68 Nm). Non-conforming\r\nRod Ends have one or two bearings with breakaway torque above 0.68 Nm. ','1)The breakaway torque measured on the rod ends were not as per the customer requirement.|2)CIM was inspecting the bearings with bolt and nut through bearings and tightening with and checked the torque. But at SAAB the bolt and nut was torque tightened to 6.3Nm before checking the breakaway torque of the bearing which i not as per the drawing requirement.|3)SAAB selection of Bearing for the assembly was not as per the SAAB higher assembly requirement.','|Informed the bearing supplier about the failure of the bearing during torque test and requested to inspect 100% before shipment.','|SAAB to analyze and revise the drawing according to their higher assembly requirement.','CIM BOM will be changed upon the receipt of revised drawing / instruction from SAAB','C76704','2019-10-26','Dharani(Shankar)','qas_sez(a)','TR-SAAI-90515','2019-10-14','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER END','yes','Misc','Dharani(Shankar)','no','','|Checked the bearings to SAAB specific requirements and change the affected bearings.','Z3456','qas_sez|','2019-11-26|','2019-11-26','0000-00-00','0000-00-00','0000-00-00','','',''),(12067,'35A-665','Saab AB','ROD ASSY','','D5227349400400','','PART ISSUE C',1,'OWED-LTA-001','','A23677','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','We have found an issue with the breakaway torque for the spherical bearing in AS81935-1-4K. Today we\r\nare suspecting all assemblies including the AS81935-1-4K. According to M81935/1 Self-Lubricated\r\nRod End Bearings the breakaway torque should be 0.5 – 6.0 in.-lbs (0.06 – 0.68 Nm). Non-conforming\r\nRod Ends have one or two bearings with breakaway torque above 0.68 Nm. ','1)The breakaway torque measured on the rod ends were not as per the customer requirement.|2)CIM was inspecting the bearings with bolt and nut through bearings and tightening with and checked the torque. But at SAAB the bolt and nut was torque tightened to 6.3Nm before checking the breakaway torque of the bearing which i not as per the drawing requirement.|3)SAAB selection of Bearing for the assembly was not as per the SAAB higher assembly requirement.','|Informed the bearing supplier about the failure of the bearing during torque test and requested to inspect 100% before shipment.','|SAAB to analyze and revise the drawing according to their higher assembly requirement.','CIM BOM will be changed upon the receipt of revised drawing / instruction from SAAB','C76706','2019-10-26','Dharani(Shankar)','qas_sez(a)','TR-SAAI-90515','2019-10-14','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER END','yes','Misc','Dharani(Shankar)','no','','|Checked the bearings to SAAB specific requirements and change the affected bearings.','Z3456','qas_sez|','2019-11-26|','2019-11-26','0000-00-00','0000-00-00','0000-00-00','','',''),(12068,'35A-665','Saab AB','ROD ASSY','','D5227349400400','','PART ISSUE C',1,'OWED-LTA-001','','A23664','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','We have found an issue with the breakaway torque for the spherical bearing in AS81935-1-4K. Today we\r\nare suspecting all assemblies including the AS81935-1-4K. According to M81935/1 Self-Lubricated\r\nRod End Bearings the breakaway torque should be 0.5 – 6.0 in.-lbs (0.06 – 0.68 Nm). Non-conforming\r\nRod Ends have one or two bearings with breakaway torque above 0.68 Nm. ','1)The breakaway torque measured on the rod ends were not as per the customer requirement.|2)CIM was inspecting the bearings with bolt and nut through bearings and tightening with and checked the torque. But at SAAB the bolt and nut was torque tightened to 6.3Nm before checking the breakaway torque of the bearing which i not as per the drawing requirement.|3)SAAB selection of Bearing for the assembly was not as per the SAAB higher assembly requirement.','|Informed the bearing supplier about the failure of the bearing during torque test and requested to inspect 100% before shipment.','|SAAB to analyze and revise the drawing according to their higher assembly requirement.','CIM BOM will be changed upon the receipt of revised drawing / instruction from SAAB','C76704','2019-10-26','Dharani(Shankar)','qas_sez(a)','TR-SAAI-90515','2019-10-14','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER END','yes','Misc','Dharani(Shankar)','no','','|Checked the bearings to SAAB specific requirements and change the affected bearings.','Z3456','qas_sez|','2019-11-26|','2019-11-26','0000-00-00','0000-00-00','0000-00-00','','',''),(12069,'35A-665','Saab AB','ROD ASSY','','D5227349400400','','PART ISSUE C',1,'OWED-LTA-001','','A23678','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','We have found an issue with the breakaway torque for the spherical bearing in AS81935-1-4K. Today we\r\nare suspecting all assemblies including the AS81935-1-4K. According to M81935/1 Self-Lubricated\r\nRod End Bearings the breakaway torque should be 0.5 – 6.0 in.-lbs (0.06 – 0.68 Nm). Non-conforming\r\nRod Ends have one or two bearings with breakaway torque above 0.68 Nm. ','1)The breakaway torque measured on the rod ends were not as per the customer requirement.|2)CIM was inspecting the bearings with bolt and nut through bearings and tightening with and checked the torque. But at SAAB the bolt and nut was torque tightened to 6.3Nm before checking the breakaway torque of the bearing which i not as per the drawing requirement.|3)SAAB selection of Bearing for the assembly was not as per the SAAB higher assembly requirement.','|Informed the bearing supplier about the failure of the bearing during torque test and requested to inspect 100% before shipment.','|SAAB to analyze and revise the drawing according to their higher assembly requirement.','CIM BOM will be changed upon the receipt of revised drawing / instruction from SAAB','C76709','2019-10-26','Dharani(Shankar)','qas_sez(a)','TR-SAAI-90515','2019-10-14','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER END','yes','Misc','Dharani(Shankar)','no','','|Checked the bearings to SAAB specific requirements and change the affected bearings.','Z3456','qas_sez|','2019-11-26|','2019-11-26','0000-00-00','0000-00-00','0000-00-00','','',''),(12070,'35-743','Saab AB','HANDLE OUTER','814252','D5227281520200','NA','PART ISSUE B',4,'OWED-LTA-002','','98281','','0000-00-00',NULL,'no','yes','yes','no','no','no','yes','no','no','5MM RIB CRACK AND BENT.','','','','','','2019-10-26','Dinesh kulal()','prodn_aero(prodn)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','no','yes','no','With Treatment','','03','no','Misc','Dinesh kulal()','no','','','A3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(12071,'51-153','THE BOEING COMPANY','PIVOT STRAP','8-19-01482-2/23540','313Z6310-502','NA','NIL',1,'BOEING 001X','','84719','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Defect No: 1 Defect Count: 2 MBD:313Z6310-502 (501) IS: QTY (2) 313Z6310-502\r\nPIVOT STRAPS IN STOCK HAVE A SURFACE PROFILE THAT IS OUT OF\r\nTOLERANCE IN THE LOCATIONS NOTED BELOW. PIVOT STRAP 1: SURFACE\r\nPROFILE of .118\" AT THE LOCATIONS SHOWN ON THE ATTACHMENT W084719.\r\nPIVOT STRAP 2: SURFACE PROFILE of .080\" AT THE LOCATIONS SHOWN ON THE\r\nATTACHMENT W084967. S/B: SURFACE PROFILE OF THE 313Z6310-502 PIVOT\r\nSTRAP SHOULD BE WITHIN .020\" WITH RESPECT TO DATUMS A, B AND C. NOTE:\r\nPLEASE REFERENCE ATTACHMENTS.','','','','','C75212','2019-10-30','qas_sez(a)','qas_sez(a)','N6400029222','2019-03-05','NC RAISED ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','no','yes','no','With Treatment','DN52314','CUSTOMER END','no','Misc','qas_sez(a)','no','','','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(12072,'51-153','THE BOEING COMPANY','PIVOT STRAP','8-19-01482-2/23540','313Z6310-502','NA','NIL',1,'BOEING 001X','','84967','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Defect No: 1 Defect Count: 2 MBD:313Z6310-502 (501) IS: QTY (2) 313Z6310-502\r\nPIVOT STRAPS IN STOCK HAVE A SURFACE PROFILE THAT IS OUT OF\r\nTOLERANCE IN THE LOCATIONS NOTED BELOW. PIVOT STRAP 1: SURFACE\r\nPROFILE of .118\" AT THE LOCATIONS SHOWN ON THE ATTACHMENT W084719.\r\nPIVOT STRAP 2: SURFACE PROFILE of .080\" AT THE LOCATIONS SHOWN ON THE\r\nATTACHMENT W084967. S/B: SURFACE PROFILE OF THE 313Z6310-502 PIVOT\r\nSTRAP SHOULD BE WITHIN .020\" WITH RESPECT TO DATUMS A, B AND C. NOTE:\r\nPLEASE REFERENCE ATTACHMENTS.','','','','','C75212','2019-10-30','qas_sez(a)','qas_sez(a)','N6400029222','2019-03-05','NC RAISED','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','no','yes','no','With Treatment','DN53307','CUSTOMER END','no','Misc','qas_sez(a)','no','','','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(12073,'51-186','THE BOEING COMPANY','ADAPTER, BULKHEAD - ALUMI','MA20182336','272U0021-6','NA','PSDL REV A',2,'BOEING 001Z','','99491','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','OD undersized by 0.05mm','Outer diameter of the part got undersized by 0.05mm during the finishing of 1st operation.|Re-pass of operation was done by the operator to remove the step formed over the flange surface of the part.|Due to the accommodation of chips over the insert contact surface, a step was formed on the flange surface of the part.','|* Insert was changed and production is restarted, next parts found okay.','|*Operators are instructed to check the insert contact surface while loading every part.\r<br/>*Quality alert is to be displayed near the machining area.\r<br/>','CA PA found ok.','','2019-10-30','Narasimha Murthy (K G)','Ranjith N D,Purushothama R,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','3','no','200MY-02','Narasimha Murthy (K G)','no','','|* Immediately stopped the production,Informed to the supervisor.\r\n* All the previous production parts are checked  and found okay.\r\n','Z3456','qas_sez|qas_sez|','2019-11-04|2019-11-12|','2019-11-12',NULL,NULL,NULL,NULL,NULL,NULL),(12074,'56-112','GKN Aerospace Orangeburg','LH UPPER ARROWHEAD','320998B8','119A1333-9603','NA','NIL',2,'A000049193','','99844','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Tool Dig Mark was evident on the part which was not meeting the required Part configuration','The program given to the machine was rotated using the program generated on the similar part (Two Parts per billet)|The program was rotated by selecting an incorrect hole center hole selected for rotating the program was 7 MM away to the required hole center.','|Program provided for the machine was re-checked and the hole center was corrected','|NC Programs shall be cross verified, by introducing a profile marking program to ensure the rotation is correct.','Next 3 program issued by the engineer will be vitrified. ','','2019-10-30','Ramesh(Poojary)','Ramesh(Poojary)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Narayanappa(G)','no','','|Part identified as rejected.','E3456','cam|qas|','2019-11-07|2019-11-20|','2019-11-20',NULL,NULL,NULL,NULL,NULL,NULL),(12075,'51-141A','THE BOEING COMPANY','CLEVIS - UPPER, RH THREAD','A7J90/184695','112A7112-610','NA','PSDL REV B',1,'BOEING 001AA','','97765','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Flange thickness under size','when doing the machining, the material have some spring back action. |Due to this spring back, excess material was removed while center slot operations finishing time. |The flange thickness have upper limit tolerance one end and the lower limit tolerance at middle of the part.   ','|Process fully observed. the Tapper measured.By tilting the B axis with some degree, part machined and flange found thickness found okay.','|Before proving the first part, all flange thickness will maintain with 1mm stock. after confirm the flange thickness, the remaining stock and operations to be continue. ','','','2019-10-30','Nagaraju P K()','Ananda(M)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','no','yes','no','With Treatment','','9','no','Misc','pe_sez(a)','no','','|Production stopped.checked finished parts and found okay.','Z3456','pe_sez|','2019-11-20|','0000-00-00',NULL,NULL,NULL,NULL,NULL,NULL),(12076,'35A-356A','Saab AB','Pull Lift Actuator Suppor','','423Z1224-4','','---',1,'787 Forecast','','A14728','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Dig mark on bush','','','','','','2019-11-04','qas_sez(a)','qas_sez(a)','','2019-11-11','NC Raised','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','no','yes','no','Assembly','','FI','no','Misc','qas_sez(a)','no','M01682|BACB28AT10B034Z','','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(12077,'35A-356A','Saab AB','Pull Lift Actuator Suppor','','423Z1224-4','','---',1,'787 Forecast','','A14728','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Dig mark on bush','','','','','','2019-11-04','qas_sez(a)','qas_sez(a)','','0000-00-00','Nc Raised','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','no','yes','no','Assembly','','FI','no','Misc','qas_sez(a)','no','L05628|BACB28AP07Z034','','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(12078,'51-150','THE BOEING COMPANY','LWR SKIN COVER','0-24-11167/24147','312Z3122-501','NA','NIL',1,'BOEING 001X','','93005','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','HOLE POSITION MEASURED OUT OF TOLERANCE \r\nS/B 0.0025 INCHES \r\nAS IS 0.01 INCHES ','1) Hole position was measured out of the drawing requirement.|2) After aging the hole position measured out of tolerance to the drawing requirement.|3) During machining time the material got deformed due to residual stress and since the drilling of holes was carried out in the same setup the hole position got shifted. |4) Trial was carried out to check the deference in hole position when drilled before and after aging operation.','|left the remaining parts for aging and then carry out the hole drilling process.','|similar trials will be carried out by drilling pilot holes instead of finished holes.','CA PA found ok.','','2019-11-04','pe_sez(a)','Srinivasa C N,Shivaraj K S,Rajesha A.R,Maruthi  D R ,Kiran Kumar M,Diwakar R.B.,Chethan Kumar M,Basangowda P K,','','0000-00-00','NC RAISED','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','PS105-01','qas_sez(a)','no','','|Informed the supervisor and the engineering department about the deviation and changed the machining to previous proved process.','Z3456','qas_sez|','2019-11-13|','2019-11-13',NULL,NULL,NULL,NULL,NULL,NULL),(12079,'35A-354A','Saab AB','LIFT PIN HOUSING FWD','','423Z1124-6-52','','1',1,'LTA SAAB B787 Assemb','','A27649','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Bore Under size','Due to tapper formation in side the bore the hole diameter is measured to be on the minimum side at the bottom of the bush.','|Reworked the part returned by SAAB and ensured all the parts in line for dispatch are with in the requirement.','|Informed the supervisor and engineering team to change the boring process from using end mill to reamer.','Next batches produced verified and found ok.','C81488','2019-11-04','qas_sez(a)','','D616755','2019-09-18','NC RAISED','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER END','yes','Misc','qas_sez(a)','no','','|Immediately checked all the parts in FG and no parts were in WIP. Informed the operators and supervisors about the issue.','Z3456','qas_sez|','2019-12-23|','2019-12-23','0000-00-00','0000-00-00','0000-00-00','','',''),(12080,'35-597','Saab AB','CORNER','934275 A','D5227338620200','NA','PART ISSUE B',1,'OWED-LTA-001','','91357','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','yes','Minor marks to the paint with bare metal,one impact mark','','','','','C82237','2019-11-04','Dharani(Shankar)','qas_sez(a)','TR-SAAI-91549','2019-09-20','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','no','no','no','With Treatment','DN62281','CUSTOMER END','yes','Misc','Dharani(Shankar)','no','','','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(12081,'35-597','Saab AB','CORNER','934275 A','D5227338620200','NA','PART ISSUE B',2,'OWED-LTA-001','','88120','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','yes','Minor marks to the paint with bare metal,one impact mark','','','','','C82237','2019-11-04','Dharani(Shankar)','qas_sez(a)','TR-SAAI-91549','2019-09-20','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','no','no','no','With Treatment','DN60775','CUSTOMER END','yes','Misc','Dharani(Shankar)','no','','','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(12082,'35-597','Saab AB','CORNER','565567','D5227338620200','NA','PART ISSUE B',1,'OWED-LTA-001','','92007','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','yes','Minor marks to the paint with bare metal,one impact mark','','','','','C82237','2019-11-04','Dharani(Shankar)','qas_sez(a)','TR-SAAI-91549','2019-09-20','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','no','no','no','With Treatment','DN62347','CUSTOMER END','yes','Misc','Dharani(Shankar)','no','','','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(12083,'51A-070A','THE BOEING COMPANY','FITTING ASSY, OUTBD','','112T7057-3','','PSDL REV -',1,'BOEING 001AA','','A29608','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','part damaged at testing time','','','','','','2019-11-05','Ramesh(D)','Ramesh(D)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','no','yes','no','Assembly','','FI','no','Misc','Ramesh(D)','no','','','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(12084,'51A-070A','THE BOEING COMPANY','FITTING ASSY, OUTBD','','112T7057-3','','PSDL REV -',1,'BOEING 001AA','','A29608','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','bearing damaged during load test','','','','','','2019-11-06','Ramesh(D)','Ramesh(D)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','no','yes','no','Assembly','','IN PROCESS','no','Misc','Ramesh(D)','no','N02095|BACB10AB10MZ','','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(12085,'47A-023B','GKN Aerospace Filton','FITTING ASSY','','F57550071000 02','','PART ISSUE G',4,'GKN GS-034 KIT -2018','','A22854','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','CORROSION OBSERVED ON THE BUSHES. ','','','','','','2019-11-07','qas_sez(a)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','no','yes','no','Assembly','','FI','no','Misc','qas_sez(a)','no','M04292|NAS75-11-009','','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(12086,'47A-023B','GKN Aerospace Filton','FITTING ASSY','','F57550071000 02','','PART ISSUE G',4,'GKN GS-034 KIT -2018','','A22854','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','CORROSION OBSERVED ON THE BUSHES.','','','','','','2019-11-07','qas_sez(a)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','no','yes','no','Assembly','','FI','no','Misc','qas_sez(a)','no','M03335|NAS77-8-026','','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(12087,'47A-023B','GKN Aerospace Filton','FITTING ASSY','','F57550071000 02','','PART ISSUE G',4,'GKN GS-034 KIT -2018','','A22856','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','CORROSION OBSERVED ON THE BUSHES.','','','','','','2019-11-07','qas_sez(a)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','no','yes','no','Assembly','','FI','no','Misc','qas_sez(a)','no','M04051|NAS75-11-009','','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(12088,'47A-023B','GKN Aerospace Filton','FITTING ASSY','','F57550071000 02','','PART ISSUE G',4,'GKN GS-034 KIT -2018','','A22856','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','CORROSION OBSERVED ON THE BUSHES.','','','','','','2019-11-07','qas_sez(a)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','no','yes','no','Assembly','','FI','no','Misc','qas_sez(a)','no','M03335|NAS77-8-026','','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(12089,'35-718','Saab AB','','PH2K','D5227349320700','NA','PART ISSUE E',1,'OWED-LTA-005','','97753','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','During machining time tool broken so dig mark on part.','Reamer broken during the machining running time and caused dig mark.|Due to excess depth of cut the tool broke.|The drilling tool used to carry out the pre-drill was blunt and left some stock in the part ID which was greater than the maximum limit for the reamer depth of cut limit.|operator did not checked the sharpness of the tool before loading to the machine.','|Changed the reamer and drilling tool with new one and ensured the machine spindle alignment and continued the production after re-measuring the offsets. ','|Information given to all the operators to only use tools with sharp cutting edges and to ensure the stock left over by the drilling tool for once in 5th part.','CA PA found ok.','','2019-11-08','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','NC CREATED ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','Misc','Nagendra(SN)','no','','|Immediately stopped the machine and informed the supervisor.\r\nThis was the first off part therefore no other parts were rejected.','E3456','qas|','2019-11-15|','2019-11-15',NULL,NULL,NULL,NULL,NULL,NULL),(12090,'35A-518','Saab AB','ROD ASSY','','D522 73510 000 00','','A',1,'OWED-LTA-004','','A26393','','0000-00-00',NULL,'no','no','no','no','no','no','yes','yes','yes','We have found an issue with the breakaway torque for the spherical bearing in AS81935-1-4K. Today we are suspecting all assemblies including the AS81935-1-4K. According to M81935/1 Self-Lubricated Rod End Bearings the breakaway torque should be 0.5 – 6.0 in.-lbs (0.06 – 0.68 Nm). Non-conforming Rod Ends have one or two bearings with breakaway torque above 0.68 Nm','1)The breakaway torque measured on the rod ends were not as per the customer requirement.|2)CIM was inspecting the bearings with bolt and nut through bearings and tightening with and checked the torque. But at SAAB the bolt and nut was torque tightened to 6.3Nm before checking the breakaway torque of the bearing which i not as per the drawing requirement.|3)SAAB selection of Bearing for the assembly was not as per the SAAB higher assembly requirement.','|Informed the bearing supplier about the failure of the bearing during torque test and requested to inspect 100% before shipment.','|SAAB to analyze and revise the drawing according to their higher assembly requirement.','CIM BOM will be changed upon the receipt of revised drawing / instruction from SAAB','C80280','2019-11-09','Dharani(Shankar)','Dharani(Shankar)','OF-004027','2019-09-02','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','Cust','yes','Misc','qas_sez(a)','no','','|Checked the bearings to SAAB specific requirements and change the affected bearings.','Z3456','qas_sez|','2019-11-20|','2019-11-20',NULL,NULL,NULL,NULL,NULL,NULL),(12091,'35A-518','Saab AB','ROD ASSY','','D522 73510 000 00','','A',5,'OWED-LTA-005','','A24927','','0000-00-00',NULL,'no','no','no','no','no','no','yes','yes','yes','We have found an issue with the breakaway torque for the spherical bearing in AS81935-1-4K. Today we are suspecting all assemblies including the AS81935-1-4K. According to M81935/1 Self-Lubricated Rod End Bearings the breakaway torque should be 0.5 – 6.0 in.-lbs (0.06 – 0.68 Nm). Non-conforming Rod Ends have one or two bearings with breakaway torque above 0.68 Nm.','1)The breakaway torque measured on the rod ends were not as per the customer requirement.|2)CIM was inspecting the bearings with bolt and nut through bearings and tightening with and checked the torque. But at SAAB the bolt and nut was torque tightened to 6.3Nm before checking the breakaway torque of the bearing which i not as per the drawing requirement.|3)SAAB selection of Bearing for the assembly was not as per the SAAB higher assembly requirement.','|Informed the bearing supplier about the failure of the bearing during torque test and requested to inspect 100% before shipment.','|SAAB to analyze and revise the drawing according to their higher assembly requirement.','CIM BOM will be changed upon the receipt of revised drawing / instruction from SAAB','C78774','2019-11-09','Dharani(Shankar)','Dharani(Shankar)','OF-004027','2019-09-02','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','Cust','yes','Misc','qas_sez(a)','no','','|Checked the bearings to SAAB specific requirements and change the affected bearings.','Z3456','qas_sez|','2019-11-20|','2019-11-20',NULL,NULL,NULL,NULL,NULL,NULL),(12092,'35A-518','Saab AB','ROD ASSY','','D522 73510 000 00','','A',45,'OWED-LTA-004','','A26392','','0000-00-00',NULL,'no','no','no','no','no','no','yes','yes','yes','We have found an issue with the breakaway torque for the spherical bearing in AS81935-1-4K. Today we are suspecting all assemblies including the AS81935-1-4K. According to M81935/1 Self-Lubricated Rod End Bearings the breakaway torque should be 0.5 – 6.0 in.-lbs (0.06 – 0.68 Nm). Non-conforming Rod Ends have one or two bearings with breakaway torque above 0.68 Nm.','1)The breakaway torque measured on the rod ends were not as per the customer requirement.|2)CIM was inspecting the bearings with bolt and nut through bearings and tightening with and checked the torque. But at SAAB the bolt and nut was torque tightened to 6.3Nm before checking the breakaway torque of the bearing which i not as per the drawing requirement.|3)SAAB selection of Bearing for the assembly was not as per the SAAB higher assembly requirement.','|Informed the bearing supplier about the failure of the bearing during torque test and requested to inspect 100% before shipment.','|SAAB to analyze and revise the drawing according to their higher assembly requirement.','CIM BOM will be changed upon the receipt of revised drawing / instruction from SAAB','C80279','2019-11-09','Dharani(Shankar)','Dharani(Shankar)','OF-004027','2019-09-02','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','Cust','yes','Misc','qas_sez(a)','no','','|Checked the bearings to SAAB specific requirements and change the affected bearings.','Z3456','qas_sez|','2019-11-20|','2019-11-20',NULL,NULL,NULL,NULL,NULL,NULL),(12093,'35A-518','Saab AB','ROD ASSY','','D522 73510 000 00','','A',13,'OWED-LTA-005','','A24928','','0000-00-00',NULL,'no','no','no','no','no','no','yes','yes','yes','We have found an issue with the breakaway torque for the spherical bearing in AS81935-1-4K. Today we are suspecting all assemblies including the AS81935-1-4K. According to M81935/1 Self-Lubricated Rod End Bearings the breakaway torque should be 0.5 – 6.0 in.-lbs (0.06 – 0.68 Nm). Non-conforming Rod Ends have one or two bearings with breakaway torque above 0.68 Nm.','1)The breakaway torque measured on the rod ends were not as per the customer requirement.|2)CIM was inspecting the bearings with bolt and nut through bearings and tightening with and checked the torque. But at SAAB the bolt and nut was torque tightened to 6.3Nm before checking the breakaway torque of the bearing which i not as per the drawing requirement.|3)SAAB selection of Bearing for the assembly was not as per the SAAB higher assembly requirement.','|Informed the bearing supplier about the failure of the bearing during torque test and requested to inspect 100% before shipment.','|SAAB to analyze and revise the drawing according to their higher assembly requirement.','CIM BOM will be changed upon the receipt of revised drawing / instruction from SAAB','C78774','2019-11-09','Dharani(Shankar)','Dharani(Shankar)','OF-004027','2019-09-02','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','Cust','yes','Misc','qas_sez(a)','no','','|Checked the bearings to SAAB specific requirements and change the affected bearings.','Z3456','qas_sez|','2019-11-20|','2019-11-20',NULL,NULL,NULL,NULL,NULL,NULL),(12094,'35A-518','Saab AB','ROD ASSY','','D522 73510 000 00','','A',8,'OWED-LTA-004','','A26588','','0000-00-00',NULL,'no','no','no','no','no','no','yes','yes','yes','We have found an issue with the breakaway torque for the spherical bearing in AS81935-1-4K. Today we are suspecting all assemblies including the AS81935-1-4K. According to M81935/1 Self-Lubricated Rod End Bearings the breakaway torque should be 0.5 – 6.0 in.-lbs (0.06 – 0.68 Nm). Non-conforming Rod Ends have one or two bearings with breakaway torque above 0.68 Nm.','1)The breakaway torque measured on the rod ends were not as per the customer requirement.|2)CIM was inspecting the bearings with bolt and nut through bearings and tightening with and checked the torque. But at SAAB the bolt and nut was torque tightened to 6.3Nm before checking the breakaway torque of the bearing which i not as per the drawing requirement.|3)SAAB selection of Bearing for the assembly was not as per the SAAB higher assembly requirement.','|Informed the bearing supplier about the failure of the bearing during torque test and requested to inspect 100% before shipment.','|SAAB to analyze and revise the drawing according to their higher assembly requirement.','CIM BOM will be changed upon the receipt of revised drawing / instruction from SAAB','C80281','2019-11-09','Dharani(Shankar)','Dharani(Shankar)','OF-004027','2019-09-02','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','Cust','yes','Misc','qas_sez(a)','no','','|Checked the bearings to SAAB specific requirements and change the affected bearings.','Z3456','qas_sez|','2019-11-20|','2019-11-20',NULL,NULL,NULL,NULL,NULL,NULL),(12095,'35A-518','Saab AB','ROD ASSY','','D522 73510 000 00','','A',94,'OWED-LTA-004','','A28276','','0000-00-00',NULL,'no','no','no','no','no','no','yes','yes','yes','We have found an issue with the breakaway torque for the spherical bearing in AS81935-1-4K. Today we are suspecting all assemblies including the AS81935-1-4K. According to M81935/1 Self-Lubricated Rod End Bearings the breakaway torque should be 0.5 – 6.0 in.-lbs (0.06 – 0.68 Nm). Non-conforming Rod Ends have one or two bearings with breakaway torque above 0.68 Nm.','1)The breakaway torque measured on the rod ends were not as per the customer requirement.|2)CIM was inspecting the bearings with bolt and nut through bearings and tightening with and checked the torque. But at SAAB the bolt and nut was torque tightened to 6.3Nm before checking the breakaway torque of the bearing which i not as per the drawing requirement.|3)SAAB selection of Bearing for the assembly was not as per the SAAB higher assembly requirement.','|Informed the bearing supplier about the failure of the bearing during torque test and requested to inspect 100% before shipment.','|SAAB to analyze and revise the drawing according to their higher assembly requirement.','CIM BOM will be changed upon the receipt of revised drawing / instruction from SAAB','C82163','2019-11-09','Dharani(Shankar)','Dharani(Shankar)','OF-004027','2019-09-02','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','Cust','yes','Misc','qas_sez(a)','no','','|Checked the bearings to SAAB specific requirements and change the affected bearings.','Z3456','qas_sez|','2019-11-20|','2019-11-20',NULL,NULL,NULL,NULL,NULL,NULL),(12096,'35A-518','Saab AB','ROD ASSY','','D522 73510 000 00','','A',2,'OWED-LTA-004','','A28318','','0000-00-00',NULL,'no','no','no','no','no','no','yes','yes','yes','We have found an issue with the breakaway torque for the spherical bearing in AS81935-1-4K. Today we are suspecting all assemblies including the AS81935-1-4K. According to M81935/1 Self-Lubricated Rod End Bearings the breakaway torque should be 0.5 – 6.0 in.-lbs (0.06 – 0.68 Nm). Non-conforming Rod Ends have one or two bearings with breakaway torque above 0.68 Nm.','1)The breakaway torque measured on the rod ends were not as per the customer requirement.|2)CIM was inspecting the bearings with bolt and nut through bearings and tightening with and checked the torque. But at SAAB the bolt and nut was torque tightened to 6.3Nm before checking the breakaway torque of the bearing which i not as per the drawing requirement.|3)SAAB selection of Bearing for the assembly was not as per the SAAB higher assembly requirement.','|Informed the bearing supplier about the failure of the bearing during torque test and requested to inspect 100% before shipment.','|SAAB to analyze and revise the drawing according to their higher assembly requirement.','CIM BOM will be changed upon the receipt of revised drawing / instruction from SAAB','C82163','2019-11-09','Dharani(Shankar)','Dharani(Shankar)','OF-004027','2019-09-02','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','Cust','yes','Misc','qas_sez(a)','no','','|Checked the bearings to SAAB specific requirements and change the affected bearings.','Z3456','qas_sez|','2019-11-20|','2019-11-20',NULL,NULL,NULL,NULL,NULL,NULL),(12097,'35A-518','Saab AB','ROD ASSY','','D522 73510 000 00','','A',21,'OWED-LTA-004','','A26640','','0000-00-00',NULL,'no','no','no','no','no','no','yes','yes','yes','We have found an issue with the breakaway torque for the spherical bearing in AS81935-1-4K. Today we are suspecting all assemblies including the AS81935-1-4K. According to M81935/1 Self-Lubricated Rod End Bearings the breakaway torque should be 0.5 – 6.0 in.-lbs (0.06 – 0.68 Nm). Non-conforming Rod Ends have one or two bearings with breakaway torque above 0.68 Nm.','1)The breakaway torque measured on the rod ends were not as per the customer requirement.|2)CIM was inspecting the bearings with bolt and nut through bearings and tightening with and checked the torque. But at SAAB the bolt and nut was torque tightened to 6.3Nm before checking the breakaway torque of the bearing which i not as per the drawing requirement.|3)SAAB selection of Bearing for the assembly was not as per the SAAB higher assembly requirement.','|Informed the bearing supplier about the failure of the bearing during torque test and requested to inspect 100% before shipment.','|SAAB to analyze and revise the drawing according to their higher assembly requirement.','CIM BOM will be changed upon the receipt of revised drawing / instruction from SAAB','C80281','2019-11-09','Dharani(Shankar)','Dharani(Shankar)','OF-004027','2019-09-02','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','Cust','yes','Misc','qas_sez(a)','no','','|Checked the bearings to SAAB specific requirements and change the affected bearings.','Z3456','qas_sez|','2019-11-20|','2019-11-20',NULL,NULL,NULL,NULL,NULL,NULL),(12098,'35A-518','Saab AB','ROD ASSY','','D522 73510 000 00','','A',5,'OWED-LTA-004','','A29107','','0000-00-00',NULL,'no','no','no','no','no','no','yes','yes','yes','We have found an issue with the breakaway torque for the spherical bearing in AS81935-1-4K. Today we are suspecting all assemblies including the AS81935-1-4K. According to M81935/1 Self-Lubricated Rod End Bearings the breakaway torque should be 0.5 – 6.0 in.-lbs (0.06 – 0.68 Nm). Non-conforming Rod Ends have one or two bearings with breakaway torque above 0.68 Nm.','1)The breakaway torque measured on the rod ends were not as per the customer requirement.|2)CIM was inspecting the bearings with bolt and nut through bearings and tightening with and checked the torque. But at SAAB the bolt and nut was torque tightened to 6.3Nm before checking the breakaway torque of the bearing which i not as per the drawing requirement.|3)SAAB selection of Bearing for the assembly was not as per the SAAB higher assembly requirement.','|Informed the bearing supplier about the failure of the bearing during torque test and requested to inspect 100% before shipment.','|SAAB to analyze and revise the drawing according to their higher assembly requirement.','CIM BOM will be changed upon the receipt of revised drawing / instruction from SAAB','C83946','2019-11-09','Dharani(Shankar)','Dharani(Shankar)','OF-004027','2019-09-02','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','Cust','yes','Misc','qas_sez(a)','no','','|Checked the bearings to SAAB specific requirements and change the affected bearings.','Z3456','qas_sez|','2019-11-20|','2019-11-20',NULL,NULL,NULL,NULL,NULL,NULL),(12099,'35A-518','Saab AB','ROD ASSY','','D522 73510 000 00','','A',3,'OWED-LTA-004','','A28319','','0000-00-00',NULL,'no','no','no','no','no','no','yes','yes','yes','We have found an issue with the breakaway torque for the spherical bearing in AS81935-1-4K. Today we are suspecting all assemblies including the AS81935-1-4K. According to M81935/1 Self-Lubricated Rod End Bearings the breakaway torque should be 0.5 – 6.0 in.-lbs (0.06 – 0.68 Nm). Non-conforming Rod Ends have one or two bearings with breakaway torque above 0.68 Nm.','1)The breakaway torque measured on the rod ends were not as per the customer requirement.|2)CIM was inspecting the bearings with bolt and nut through bearings and tightening with and checked the torque. But at SAAB the bolt and nut was torque tightened to 6.3Nm before checking the breakaway torque of the bearing which i not as per the drawing requirement.|3)SAAB selection of Bearing for the assembly was not as per the SAAB higher assembly requirement.','|Informed the bearing supplier about the failure of the bearing during torque test and requested to inspect 100% before shipment.','|SAAB to analyze and revise the drawing according to their higher assembly requirement.','CIM BOM will be changed upon the receipt of revised drawing / instruction from SAAB','C82163','2019-11-09','Dharani(Shankar)','Dharani(Shankar)','OF-004027','2019-09-02','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','Cust','yes','Misc','qas_sez(a)','no','','|Checked the bearings to SAAB specific requirements and change the affected bearings.','Z3456','qas_sez|','2019-11-20|','2019-11-20',NULL,NULL,NULL,NULL,NULL,NULL),(12100,'35A-518','Saab AB','ROD ASSY','','D522 73510 000 00','','A',6,'OWED-LTA-005','','A29108','','0000-00-00',NULL,'no','no','no','no','no','no','yes','yes','yes','We have found an issue with the breakaway torque for the spherical bearing in AS81935-1-4K. Today we are suspecting all assemblies including the AS81935-1-4K. According to M81935/1 Self-Lubricated Rod End Bearings the breakaway torque should be 0.5 – 6.0 in.-lbs (0.06 – 0.68 Nm). Non-conforming Rod Ends have one or two bearings with breakaway torque above 0.68 Nm.','1)The breakaway torque measured on the rod ends were not as per the customer requirement.|2)CIM was inspecting the bearings with bolt and nut through bearings and tightening with and checked the torque. But at SAAB the bolt and nut was torque tightened to 6.3Nm before checking the breakaway torque of the bearing which i not as per the drawing requirement.|3)SAAB selection of Bearing for the assembly was not as per the SAAB higher assembly requirement.','|Informed the bearing supplier about the failure of the bearing during torque test and requested to inspect 100% before shipment.','|SAAB to analyze and revise the drawing according to their higher assembly requirement.','CIM BOM will be changed upon the receipt of revised drawing / instruction from SAAB','C83946','2019-11-09','Dharani(Shankar)','Dharani(Shankar)','OF-004027','2019-09-02','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','Cust','yes','Misc','qas_sez(a)','no','','|Checked the bearings to SAAB specific requirements and change the affected bearings.','Z3456','qas_sez|','2019-11-20|','2019-11-20',NULL,NULL,NULL,NULL,NULL,NULL),(12101,'35A-518','Saab AB','ROD ASSY','','D522 73510 000 00','','A',2,'OWED-LTA-004','','A26394','','0000-00-00',NULL,'no','no','no','no','no','no','yes','yes','yes','We have found an issue with the breakaway torque for the spherical bearing in AS81935-1-4K. Today we are suspecting all assemblies including the AS81935-1-4K. According to M81935/1 Self-Lubricated Rod End Bearings the breakaway torque should be 0.5 – 6.0 in.-lbs (0.06 – 0.68 Nm). Non-conforming Rod Ends have one or two bearings with breakaway torque above 0.68 Nm.','1)The breakaway torque measured on the rod ends were not as per the customer requirement.|2)CIM was inspecting the bearings with bolt and nut through bearings and tightening with and checked the torque. But at SAAB the bolt and nut was torque tightened to 6.3Nm before checking the breakaway torque of the bearing which i not as per the drawing requirement.|3)SAAB selection of Bearing for the assembly was not as per the SAAB higher assembly requirement.','|Informed the bearing supplier about the failure of the bearing during torque test and requested to inspect 100% before shipment.','|SAAB to analyze and revise the drawing according to their higher assembly requirement.','CIM BOM will be changed upon the receipt of revised drawing / instruction from SAAB','C80280','2019-11-09','Dharani(Shankar)','Dharani(Shankar)','OF-004027','2019-09-02','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','Cust','yes','Misc','qas_sez(a)','no','','|Checked the bearings to SAAB specific requirements and change the affected bearings.','Z3456','qas_sez|','2019-11-20|','2019-11-20',NULL,NULL,NULL,NULL,NULL,NULL),(12102,'47-097B','GKN Aerospace Filton','BRACKET FT5 FWD','W8305','F57550783001','NA','PART ISSUE E04',3,'LTA GKN GS72 - Forgi','','86330','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','yes','Bore To be free from Painting,but in parts CCC application was done which is not meeting the drawing requriment','','','','','C79743','2019-11-09','Dharani(Shankar)','qas_sez(a)','G0208B993','2019-09-18','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','no','no','no','With Treatment','DN58162','CUSTOMER END','yes','Misc','Dharani(Shankar)','no','','','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(12103,'47-097B','GKN Aerospace Filton','BRACKET FT5 FWD','W8305','F57550783001','NA','PART ISSUE E04',1,'LTA GKN GS72 - Forgi','','86330','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','yes','Bore to be free from paint,but in part CCC application was done which is not meeting the drawing requriment.','','','','','C80458','2019-11-09','Dharani(Shankar)','qas_sez(a)','G0208B993','2019-09-18','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','no','no','no','With Treatment','DN58162','CUSTOMER END','yes','Misc','Dharani(Shankar)','no','','','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(12104,'56-011','GKN Aerospace Orangeburg','SPLICE PLATE AFT LWR','H31415','119A1214-607','NA','PSDL REV-',1,'LTA GKN 737 Winglet','','100578','','0000-00-00',NULL,'no','','yes','','yes','','yes','','','Machine malfunction during 5 axis running time.','','','','','','2019-11-12','pe_sez(a)','        Kiran Kumar M','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','','yes','','','','3','','','','','','','Z3456','pe_sez|','2019-11-12|','0000-00-00',NULL,NULL,NULL,NULL,NULL,NULL),(12105,'56-004','GKN Aerospace Orangeburg','GAS DUMPER FITTING','1850044651','475Z3604-19','NA','NIL',1,'A000044745','','100261','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','BORE OVERSIZE BORE DIA required 12.7mm AND 17.463mm but measures oversize by 0.1mm TO 0.12mm respectively.','1) Ovality formed during the boring operation due to which the diameter measured oversize in one direction.|2) Due to run out of the tool the ovality formation of the bore has occurred.|3) The operator used the collate tool holder for holding the tool but he did not measured and reduced the collate run out before starting the production.','|1) Checked the run out of all the other tools and changed the tool holder for the tool with high run out (i.e. for tools which has run out greater than 6micron).\r<br/>2) On job training provided to all the operators on the type of tool holders and what are the parameters to be ensured for those specific tool holders.','|Instructions will be displayed near the machines containing the details of the tool holders used for production and the parameters to be ensured on the holders before starting the production near the machines on or before 03-Dec-2019.','Effectiveness of training for all three shift operators will be verified and the display of instructions near the machines will be verified and confirmed.','','2019-11-14','pe_sez(a)','','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','3','no','Slim3n-4AHS-4','pe_sez(a)','no','','|Immediately stopped the production and checked the part in process and the boring operation was not started. Moved the rejected part to Quality clinic with rejection tag.','Z3456','qas_sez|qas_sez|','2019-11-22|2019-11-26|','2019-11-26','0000-00-00','0000-00-00','0000-00-00','','',''),(12106,'51A-072','THE BOEING COMPANY','BEARING ASSY','','113T1204-1','','NIL',1,'BOEING 001S','','A30974','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','bearing damaged  while swagging operation  time. ','','','','','','2019-11-15','Ramesh(D)','Ramesh(D)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','no','yes','no','Assembly','','procesing','no','Misc','Ramesh(D)','no','M03805|MS14103-6','','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(12107,'35-480B','Saab AB','LOCK LEVER','MGJ4','D5227349820000','NA','PART ISSUE C',1,'OWED-LTA-003','','99166','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Required Diameter is 12.65 d9 (12.557 TO 12.6)but Measured Diameter is 12.527mm resulting the outer diameter to be undersized by 0.027mm.','Excess material removed during rework of dent on the OD|Dent on the OD formed due to improper handling during machining.|Part fell on the conveyor while the operator was unloading the finished part from fixture.','|On- Job training given to all the operators by the supervisor on precautions to be taken while handling of parts during loading and unloading parts in the fixture inside the machine.','|1) Quality Alert will be displayed.\r<br/>2) Special trays are designed and used while unloading the parts from fixtures to avoid damages during handling.','1) Training effectiveness of all the three shift operators before the next part production.\r\n2) Display of Quality Alert will be verified on 22-Nov-19.','','2019-11-15','Raghavendra Rao(R)','','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','09','no','Misc','Raghavendra Rao(R)','no','','|Similar parts under machining verified and found ok. Rejected part was identified with rejection tag and moved to Quality Clinic.','E3456','qas|qas_sez|qas_sez|qas|qas|','2019-11-15|2019-11-16|2019-11-18|2019-11-18|2019-11-25|','2019-11-25','0000-00-00','0000-00-00','0000-00-00','','',''),(12108,'47-165','GKN Aerospace Filton','PLATE SPREADER UPPER','2593601 3','F57455017200','NA','PART ISSUE B01',1,'GKN-GS-068 PHASE2- L','','100841','','0000-00-00',NULL,'yes','no','no','no','no','yes','no','yes','no','1) thickness undersize 4.8+/- 0.15mm.                        measured 4.33 to 4.73 mm.\r\n2)  thickness undersize 9.30+/- 0.15mm.                           measured 8.80 to 8.94 mm.\r\n3) step observed on radius.','1) Fixture and the program used for the production of the part was not as per the requirement.|2) Engineer revised the model and NC program and issued the D00 format to the production team but did not changed the clamping fixture according to the revised model.|3) Engineer did not completely analyzed the change requirements after revising the model.','|Removed the new program and revised model from the production server and moved to the obsolete folder.','|Engineering team need to validate the changes and requirements for the changes to be implemented along with the senior engineers before flowing down them to the shop floor for use.','Verification of engineering flow down to the shop floor for next batches will be verified.','','2019-11-16','pe_sez(a)','','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','',' 02 final','no','Misc','Mahesh(N)','no','','|Immediately informed the engineering team after identifying the deviation during the first off inspection and continued the production according to the old process','Z3456','qas_sez|qas_sez|','2019-11-22|2019-11-26|','2019-11-26','0000-00-00','0000-00-00','0000-00-00','','',''),(12109,'51-190','THE BOEING COMPANY','FIXED HINGE - MLG, DRAG S','347601','113W8345-28','NA','PSDL REV A',1,'BOEING 001AA','','95618','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','DENT OBSERVED ON THE SERRATIONS','1) Serration damaged during miss-handling.|2) Part was not sufficiently protected from damage during internal transit.|3) Part was only protected by using sleeve and was moved from department to department without any partitions.|Please ignore the above root cause.|1) Damage in serration area (partly) occurred due to mishandling.\r\n2) Protection from damage during inter department transit was not adequate.\r\n3) Use of bins / trays for less qty. (1 no, 2 No’s) was not followed by concern department personnel.\r\n','|Awareness training given to all the operators, fitting personnel and Quality personnel.|Please ignore the above Corrective Action\r<br/>\r<br/>Short Term: Intermediate partitions (GAMMA Partitions) implemented in the bins for storage and movement of parts to avoid part contact and damages. ','|1) Intermediate partitions will be implemented (GAMMA Partitions) during the storage and movement of parts to avoid part to part contact and damages.|Please ignore the above Preventive Action\r<br/>\r<br/>Long Term: Alert Notes will be displayed with instructions to use trays/ bins with partitions and sleeves for each and every part during transit from department to department.','Implementation of partition verified for the parts and display of alert notes will be verified on 22-Nov-2019.','','2019-11-18','pe_sez(a)','Upendra N ,Thaveni D M ,Rajesha A.R,Prashanth B,Maruthi  D R ,Manu ,Kiran Kumar M,Dhanush J.K,Chetan N,Ananda M,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','no','yes','no','With Treatment','','FI','no','Fitting','qas_sez(a)','no','','|Checked all the other parts which were moved with the affected parts and no damages were observed on the other parts. The damaged part was identified with rejection tag and moved to Quality Clinic.|Please ignore the above Containment action.\r\n\r\nChecked all similar parts from W/O 95618 for damage and identified none. The damaged par was moved to Quality Clinic with rejection tag.','Z3456','qas_sez|qas_sez|','2019-11-18|2019-11-18|','0000-00-00',NULL,NULL,NULL,NULL,NULL,NULL),(12110,'56-115','GKN Aerospace Orangeburg','RH LOWER ARROWHEAD','581551','119A1433-9604','NA','NIL',6,'A000049193','','89292','','0000-00-00',NULL,'yes','no','no','no','no','no','no','yes','yes','Profile of arrow head not meeting the MBD requirement when compared to model there is a mis-match of 1.5 to 2 mm. ','','','','','C76757','2019-11-18','Dharani(Shankar)','Mahesh(N)','R18391','2019-08-02','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','no','no','no','With Treatment','DN54391','CUSTOMER END','yes','Misc','Dharani(Shankar)','no','','','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(12111,'56-115','GKN Aerospace Orangeburg','RH LOWER ARROWHEAD','750131','119A1433-9604','NA','NIL',4,'A000049193','','89293','','0000-00-00',NULL,'yes','no','no','no','no','no','no','yes','yes','Profile of arrow head not meeting the MBD requirement when compared to model there is a mis-match of 1.5 to 2 mm. ','','','','','C78255','2019-11-18','Dharani(Shankar)','Mahesh(N)','R18391','2019-08-02','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','no','no','no','With Treatment','DN54392','CUSTOMER END','yes','Misc','Dharani(Shankar)','no','','','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(12112,'56-115','GKN Aerospace Orangeburg','RH LOWER ARROWHEAD','581551','119A1433-9604','NA','NIL',9,'A000049193','','89291','','0000-00-00',NULL,'yes','no','no','no','no','no','no','yes','yes','Profile of arrow head not meeting the MBD requirement when compared to model there is a mis-match of 1.5 to 2 mm. ','','','','','C76757','2019-11-18','Dharani(Shankar)','Mahesh(N)','R18391','2019-08-02','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','no','no','no','With Treatment','DN54390','CUSTOMER END','yes','Misc','Dharani(Shankar)','no','','','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(12113,'56-115','GKN Aerospace Orangeburg','RH LOWER ARROWHEAD','750131','119A1433-9604','NA','NIL',10,'A000049193','','89360','','0000-00-00',NULL,'yes','no','no','no','no','no','no','yes','yes','Profile of arrow head not meeting the MBD requirement when compared to model there is a mis-match of 1.5 to 2 mm. ','','','','','C78255','2019-11-18','Dharani(Shankar)','Mahesh(N)','R18391','2019-08-02','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','no','no','no','With Treatment','DN54220','CUSTOMER END','yes','Misc','Dharani(Shankar)','no','','','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(12114,'56-115','GKN Aerospace Orangeburg','RH LOWER ARROWHEAD','750131','119A1433-9604','NA','NIL',8,'A000049193','','90330','','0000-00-00',NULL,'yes','no','no','no','no','no','no','yes','yes','Profile of arrow head not meeting the MBD requirement when compared to model there is a mis-match of 1.5 to 2 mm. ','','','','','C83624','2019-11-18','Dharani(Shankar)','Mahesh(N)','R18391','2019-08-02','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','no','no','no','With Treatment','DN56313','CUSTOMER END','yes','Misc','Dharani(Shankar)','no','','','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(12115,'56-115','GKN Aerospace Orangeburg','RH LOWER ARROWHEAD','750131','119A1433-9604','NA','NIL',1,'A000049193','','89361','','0000-00-00',NULL,'yes','no','no','no','no','no','no','yes','yes','Profile of arrow head not meeting the MBD requirement when compared to model there is a mis-match of 1.5 to 2 mm. ','','','','','C78255','2019-11-18','Dharani(Shankar)','Mahesh(N)','R18391','2019-08-02','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','no','no','no','With Treatment','DN54212','CUSTOMER END','yes','Misc','Dharani(Shankar)','no','','','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(12116,'56-115','GKN Aerospace Orangeburg','RH LOWER ARROWHEAD','0664201-1','119A1433-9604','NA','NIL',1,'A000049193','','89231','','0000-00-00',NULL,'yes','no','no','no','no','no','no','yes','yes','Pilot holes mis-located,the part was not matching the mating part during assembly. ','','','','','C76756','2019-11-18','Dharani(Shankar)','Mahesh(N)','R18391','2019-08-02','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','no','yes','no','With Treatment','DN54464','CUSTOMER END','no','Misc','Dharani(Shankar)','no','','','Z3456','qas_sez|','2019-11-21|','0000-00-00',NULL,NULL,NULL,NULL,NULL,NULL),(12117,'56-114','GKN Aerospace Orangeburg','LH LOWER ARROWHEAD','581551','119A1433-9603','NA','NIL',6,'A000049193','','89289','','0000-00-00',NULL,'yes','no','no','no','no','no','no','yes','yes','Profile of arrow head not meeting the MBD requirement when compared to model there is a mis-match of 1.5 to 2 mm. ','','','','','C76758','2019-11-18','Dharani(Shankar)','Mahesh(N)','R18391','2019-08-02','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','no','no','no','With Treatment','DN54389','CUSTOMER END','yes','Misc','Dharani(Shankar)','no','','','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(12118,'56-114','GKN Aerospace Orangeburg','LH LOWER ARROWHEAD','581551','119A1433-9603','NA','NIL',2,'A000049193','','89290','','0000-00-00',NULL,'yes','no','no','no','no','no','no','yes','yes','Profile of arrow head not meeting the MBD requirement when compared to model there is a mis-match of 1.5 to 2 mm. ','','','','','C78253','2019-11-18','Dharani(Shankar)','Mahesh(N)','R18391','2019-08-02','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','no','no','no','With Treatment','DN54466','CUSTOMER END','yes','Misc','Dharani(Shankar)','no','','','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(12119,'56-114','GKN Aerospace Orangeburg','LH LOWER ARROWHEAD','581551','119A1433-9603','NA','NIL',1,'A000049193','','89357','','0000-00-00',NULL,'yes','no','no','no','no','no','no','yes','yes','Profile of arrow head not meeting the MBD requirement when compared to model there is a mis-match of 1.5 to 2 mm. ','','','','','C78253','2019-11-18','Dharani(Shankar)','Mahesh(N)','R18391','2019-08-02','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','no','no','no','With Treatment','DN54214','CUSTOMER END','yes','Misc','Dharani(Shankar)','no','','','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(12120,'56-114','GKN Aerospace Orangeburg','LH LOWER ARROWHEAD','581551','119A1433-9603','NA','NIL',1,'A000049193','','89359','','0000-00-00',NULL,'yes','no','no','no','no','no','no','yes','yes','Profile of arrow head not meeting the MBD requirement when compared to model there is a mis-match of 1.5 to 2 mm. ','','','','','C78254','2019-11-18','Dharani(Shankar)','Mahesh(N)','R18391','2019-08-02','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','no','no','no','With Treatment','DN54216','CUSTOMER END','yes','Misc','Dharani(Shankar)','no','','','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(12121,'56-112','GKN Aerospace Orangeburg','LH UPPER ARROWHEAD','75985/02','119A1333-9603','NA','NIL',3,'A000049193','','89285','','0000-00-00',NULL,'yes','no','no','no','no','no','no','yes','yes','Pilot holes mis-located,the part was not matching the mating part during assembly. ','','','','','C78250','2019-11-18','Dharani(Shankar)','Mahesh(N)','R18391','2019-08-02','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','no','yes','no','With Treatment','DN54455','CUSTOMER END','no','Misc','Dharani(Shankar)','no','','','Z3456','qas_sez|','2019-11-21|','0000-00-00',NULL,NULL,NULL,NULL,NULL,NULL),(12122,'56-113','GKN Aerospace Orangeburg','RH UPPER ARROWHEAD','75985/02','119A1333-9604','NA','NIL',1,'A000049193','','89286','','0000-00-00',NULL,'yes','no','no','no','no','no','no','yes','yes','Pilot holes mis-located,the part was not matching the mating part during assembly. ','','','','','C76989','2019-11-18','Dharani(Shankar)','Mahesh(N)','R18391','2019-08-02','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','no','yes','no','With Treatment','DN55151','CUSTOMER END','no','Misc','Dharani(Shankar)','no','','','Z3456','qas_sez|','2019-11-21|','0000-00-00',NULL,NULL,NULL,NULL,NULL,NULL),(12123,'35-750','Saab AB','LOCK LEVER','C78729','D5227349820200','NA','PART ISSUE D',2,'1600283741','','99411','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Required size of dia 8+/-0.15 mm measured value 8.25 mm','during rework time bore over size up to 0.1mm|step observed in the bore|during machining time drill flute was brokened|improper coolant flow ','|change the new drill bit and adjust the coolant flow.','|instruction given to operator before run run the part adjust the coolant flow and check the finished part. ','CA and PA FOUND OK.','','2019-11-18','Krishna(Chowdary.G.P.)','','','0000-00-00','NC Created','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','Misc','Nagendra(SN)','no','','|immediately stop the machine and checked all previous finished parts ,one part is found with same issue, reaming parts are found OK   ','E3456','qas|','2019-12-04|','2019-12-04','0000-00-00','0000-00-00','0000-00-00','','',''),(12124,'56-024A','GKN Aerospace Orangeburg','CLOSEOUT FAIRING - AFT, U','715232B5','119A1522-604','NA','PSDL REV A',3,'LTA GKN ORANGEBURG W','','100668','','0000-00-00',NULL,'yes','no','no','no','yes','yes','no','no','no','1) OBSERVED DIG MARK ON THE PART.\r\n','','','','','','2019-11-18','pe_sez(a)','pe_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','With Treatment','','2ND','no','Misc','qas_sez(a)','no','','','Z3456','qas_sez|','2019-11-21|','2019-11-21',NULL,NULL,NULL,NULL,NULL,NULL),(12125,'55A-008','Spirit Aero Systems Inc. Tulsa','ANGLE ASSY - SEAL BULKHEA','','115A2981-605','','NIL',3,'LTA PO spirit ','','A31479','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','GROMMET CROSS SEATED AFTER ASSEMBLY.','','','','','','2019-11-19','Ramesh(D)','Varadaraju(D)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','no','yes','no','Assembly','','procesing','no','Misc','Ramesh(D)','no','N05092|BACG20Z-P000612B','','E3456','bmandyam|bmandyam|bmandyam|bmandyam|bmandyam|bmandyam|bmandyam|','2019-11-27|2019-11-27|2019-11-27|2019-11-27|2019-11-27|2019-11-27|2019-11-27|','0000-00-00','0000-00-00','0000-00-00','0000-00-00','','',''),(12126,'35A-354A','Saab AB','LIFT PIN HOUSING FWD','','423Z1124-6-52','','1',1,'LTA SAAB B787 Assemb','','A22783','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','BORE OVER SIZE','','','','','','2019-11-20','qas_sez(a)','qas_sez(a)','','0000-00-00','NC RAISED','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','no','yes','no','Assembly','','FI','no','Misc','qas_sez(a)','no','M06354|BACB28AP20Z253','','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(12127,'35-443C','Saab AB','HINGE','YNRQ','D5227338820000','NA','B',1,'OWED-LTA-002','','98806','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Hole position Distance 0.1mm under size from datum Face','','','','','','2019-11-20','Nagaraju P K()','Thaveni D M ,Manu ,Manjunatha  K,HariPrasad ,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','no','no','yes','With Treatment','','5','no','a51nx-01','pe_sez(a)','no','','','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(12128,'35-445','Saab AB','INTERCOSTAL','570875','D522 73398 201 00','','A',1,'OWED-LTA-001','','99070','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Dig mark on part.','','','','','','2019-11-20','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','NC raised','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','no','yes','no','With Treatment','','FI','no','Misc','Nagendra(SN)','no','','','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(12129,'56-039B','GKN Aerospace Orangeburg','ROOT FITTING','9453370','119A1210-603','NA','PSDL REV C',1,'LTA GKN ORANGEBURG 2','','99868','','0000-00-00',NULL,'yes','no','yes','no','yes','no','no','no','no','Machine C Axis Mal Function. Part Thickness shape out ','','','','','','2019-11-21','pe_sez(a)','pe_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','no','yes','no','With Treatment','','03','no','Misc','pe_sez(a)','no','','','Z3456','pe_sez|','2019-11-21|','0000-00-00',NULL,NULL,NULL,NULL,NULL,NULL),(12130,'35A-501A','Saab AB','ROD ASSY','','D5227349400000','','PART ISSUE D',26,'OWED-LTA-004','','A28415','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Break Torque of the rod end bearing is over the tolerance of 0.68 Nm,Should be less than 0.68 Nm ','1)The breakaway torque measured on the rod ends were not as per the customer requirement.|2)CIM was inspecting the bearings with bolt and nut through bearings and tightening with and checked the torque. But at SAAB the bolt and nut was torque tightened to 6.3Nm before checking the breakaway torque of the bearing which i not as per the drawing requirement.|3)SAAB selection of Bearing for the assembly was not as per the SAAB higher assembly requirement.','|Informed the bearing supplier about the failure of the bearing during torque test and requested to inspect 100% before shipment.','|SAAB to analyze and revise the drawing according to their higher assembly requirement.','CIM BOM will be changed upon the receipt of revised drawing / instruction from SAAB','C82241','2019-11-21','Dharani(Shankar)','qas_sez(a)','100368','2019-10-28','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER END','yes','Misc','Dharani(Shankar)','no','','|Checked the bearings to SAAB specific requirements and change the affected bearings.','Z3456','qas_sez|','2019-11-25|','2019-11-25','0000-00-00','0000-00-00','0000-00-00','','',''),(12131,'35A-501A','Saab AB','ROD ASSY','','D5227349400000','','PART ISSUE D',3,'OWED-LTA-004','','A27127','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Break Torque of the rod end bearing is over the tolerance of 0.68 Nm,Should be less than 0.68 Nm ','1)The breakaway torque measured on the rod ends were not as per the customer requirement.|2)CIM was inspecting the bearings with bolt and nut through bearings and tightening with and checked the torque. But at SAAB the bolt and nut was torque tightened to 6.3Nm before checking the breakaway torque of the bearing which i not as per the drawing requirement.|3)SAAB selection of Bearing for the assembly was not as per the SAAB higher assembly requirement.','|Informed the bearing supplier about the failure of the bearing during torque test and requested to inspect 100% before shipment.','|SAAB to analyze and revise the drawing according to their higher assembly requirement.','CIM BOM will be changed upon the receipt of revised drawing / instruction from SAAB','C82241','2019-11-21','Dharani(Shankar)','qas_sez(a)','100368','2019-10-28','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER END','yes','Misc','Dharani(Shankar)','no','','|Checked the bearings to SAAB specific requirements and change the affected bearings.','Z3456','qas_sez|','2019-11-25|','2019-11-25','0000-00-00','0000-00-00','0000-00-00','','',''),(12132,'35A-501A','Saab AB','ROD ASSY','','D5227349400000','','PART ISSUE D',6,'OWED-LTA-004','','A27124','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Break Torque of the rod end bearing is over the tolerance of 0.68 Nm,Should be less than 0.68 Nm ','1)The breakaway torque measured on the rod ends were not as per the customer requirement.|2)CIM was inspecting the bearings with bolt and nut through bearings and tightening with and checked the torque. But at SAAB the bolt and nut was torque tightened to 6.3Nm before checking the breakaway torque of the bearing which i not as per the drawing requirement.|3)SAAB selection of Bearing for the assembly was not as per the SAAB higher assembly requirement.','|Informed the bearing supplier about the failure of the bearing during torque test and requested to inspect 100% before shipment.','|SAAB to analyze and revise the drawing according to their higher assembly requirement.','CIM BOM will be changed upon the receipt of revised drawing / instruction from SAAB','C80723','2019-11-21','Dharani(Shankar)','qas_sez(a)','100368','2019-10-28','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER END','yes','Misc','Dharani(Shankar)','no','','|Checked the bearings to SAAB specific requirements and change the affected bearings.','Z3456','qas_sez|','2019-11-25|','2019-11-25','0000-00-00','0000-00-00','0000-00-00','','',''),(12133,'35A-501A','Saab AB','ROD ASSY','','D5227349400000','','PART ISSUE D',6,'OWED-LTA-004','','A27122','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Break Torque of the rod end bearing is over the tolerance of 0.68 Nm,Should be less than 0.68 Nm ','1)The breakaway torque measured on the rod ends were not as per the customer requirement.|2)CIM was inspecting the bearings with bolt and nut through bearings and tightening with and checked the torque. But at SAAB the bolt and nut was torque tightened to 6.3Nm before checking the breakaway torque of the bearing which i not as per the drawing requirement.|3)SAAB selection of Bearing for the assembly was not as per the SAAB higher assembly requirement.','|Informed the bearing supplier about the failure of the bearing during torque test and requested to inspect 100% before shipment.','|SAAB to analyze and revise the drawing according to their higher assembly requirement.','CIM BOM will be changed upon the receipt of revised drawing / instruction from SAAB','C80723','2019-11-21','Dharani(Shankar)','qas_sez(a)','100368','2019-10-28','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER END','yes','Misc','Dharani(Shankar)','no','','|Checked the bearings to SAAB specific requirements and change the affected bearings.','Z3456','qas_sez|','2019-11-25|','2019-11-25','0000-00-00','0000-00-00','0000-00-00','','',''),(12134,'35A-501A','Saab AB','ROD ASSY','','D5227349400000','','PART ISSUE D',10,'OWED-LTA-004','','A28443','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Break Torque of the rod end bearing is over the tolerance of 0.68 Nm,Should be less than 0.68 Nm ','1)The breakaway torque measured on the rod ends were not as per the customer requirement.|2)CIM was inspecting the bearings with bolt and nut through bearings and tightening with and checked the torque. But at SAAB the bolt and nut was torque tightened to 6.3Nm before checking the breakaway torque of the bearing which i not as per the drawing requirement.|3)SAAB selection of Bearing for the assembly was not as per the SAAB higher assembly requirement.','|Informed the bearing supplier about the failure of the bearing during torque test and requested to inspect 100% before shipment.','|SAAB to analyze and revise the drawing according to their higher assembly requirement.','CIM BOM will be changed upon the receipt of revised drawing / instruction from SAAB','C82241','2019-11-21','Dharani(Shankar)','qas_sez(a)','100368','2019-10-28','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER END','yes','Misc','Dharani(Shankar)','no','','|Checked the bearings to SAAB specific requirements and change the affected bearings.','Z3456','qas_sez|','2019-11-25|','2019-11-25','0000-00-00','0000-00-00','0000-00-00','','',''),(12135,'35A-501A','Saab AB','ROD ASSY','','D5227349400000','','PART ISSUE D',2,'OWED-LTA-004','','A28416','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Break Torque of the rod end bearing is over the tolerance of 0.68 Nm,Should be less than 0.68 Nm ','1)The breakaway torque measured on the rod ends were not as per the customer requirement.|2)CIM was inspecting the bearings with bolt and nut through bearings and tightening with and checked the torque. But at SAAB the bolt and nut was torque tightened to 6.3Nm before checking the breakaway torque of the bearing which i not as per the drawing requirement.|3)SAAB selection of Bearing for the assembly was not as per the SAAB higher assembly requirement.','|Informed the bearing supplier about the failure of the bearing during torque test and requested to inspect 100% before shipment.','|SAAB to analyze and revise the drawing according to their higher assembly requirement.','CIM BOM will be changed upon the receipt of revised drawing / instruction from SAAB','C82241','2019-11-21','Dharani(Shankar)','qas_sez(a)','100368','2019-10-28','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','Customer End','yes','Misc','Dharani(Shankar)','no','','|Checked the bearings to SAAB specific requirements and change the affected bearings.','Z3456','qas_sez|','2019-11-25|','2019-11-25','0000-00-00','0000-00-00','0000-00-00','','',''),(12136,'35A-501A','Saab AB','ROD ASSY','','D5227349400000','','PART ISSUE D',4,'OWED-LTA-004','','A27125','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Break Torque of the rod end bearing is over the tolerance of 0.68 Nm,Should be less than 0.68 Nm ','1)The breakaway torque measured on the rod ends were not as per the customer requirement.|2)CIM was inspecting the bearings with bolt and nut through bearings and tightening with and checked the torque. But at SAAB the bolt and nut was torque tightened to 6.3Nm before checking the breakaway torque of the bearing which i not as per the drawing requirement.|3)SAAB selection of Bearing for the assembly was not as per the SAAB higher assembly requirement.','|Informed the bearing supplier about the failure of the bearing during torque test and requested to inspect 100% before shipment.','|SAAB to analyze and revise the drawing according to their higher assembly requirement.','CIM BOM will be changed upon the receipt of revised drawing / instruction from SAAB','C80723','2019-11-21','Dharani(Shankar)','qas_sez(a)','100368','2019-10-28','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','Customer End','yes','Misc','Dharani(Shankar)','no','','|Checked the bearings to SAAB specific requirements and change the affected bearings.','Z3456','qas_sez|','2019-11-25|','2019-11-25','0000-00-00','0000-00-00','0000-00-00','','',''),(12137,'35A-501A','Saab AB','ROD ASSY','','D5227349400000','','PART ISSUE D',1,'OWED-LTA-004','','A28445','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Break Torque of the rod end bearing is over the tolerance of 0.68 Nm,Should be less than 0.68 Nm ','1)The breakaway torque measured on the rod ends were not as per the customer requirement.|2)CIM was inspecting the bearings with bolt and nut through bearings and tightening with and checked the torque. But at SAAB the bolt and nut was torque tightened to 6.3Nm before checking the breakaway torque of the bearing which i not as per the drawing requirement.|3)SAAB selection of Bearing for the assembly was not as per the SAAB higher assembly requirement.','|Informed the bearing supplier about the failure of the bearing during torque test and requested to inspect 100% before shipment.','|SAAB to analyze and revise the drawing according to their higher assembly requirement.','CIM BOM will be changed upon the receipt of revised drawing / instruction from SAAB','C82242','2019-11-21','Dharani(Shankar)','qas_sez(a)','100368','2019-10-28','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','Customer End','yes','Misc','Dharani(Shankar)','no','','|Checked the bearings to SAAB specific requirements and change the affected bearings.','Z3456','qas_sez|','2019-11-25|','2019-11-25','0000-00-00','0000-00-00','0000-00-00','','',''),(12138,'35A-501A','Saab AB','ROD ASSY','','D5227349400000','','PART ISSUE D',1,'OWED-LTA-004','','A28446','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Break Torque of the rod end bearing is over the tolerance of 0.68 Nm,Should be less than 0.68 Nm ','1)The breakaway torque measured on the rod ends were not as per the customer requirement.|2)CIM was inspecting the bearings with bolt and nut through bearings and tightening with and checked the torque. But at SAAB the bolt and nut was torque tightened to 6.3Nm before checking the breakaway torque of the bearing which i not as per the drawing requirement.|3)SAAB selection of Bearing for the assembly was not as per the SAAB higher assembly requirement.','|Informed the bearing supplier about the failure of the bearing during torque test and requested to inspect 100% before shipment.','|SAAB to analyze and revise the drawing according to their higher assembly requirement.','CIM BOM will be changed upon the receipt of revised drawing / instruction from SAAB','C82242','2019-11-21','Dharani(Shankar)','qas_sez(a)','100368','2019-10-28','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','Customer End','yes','Misc','Dharani(Shankar)','no','','|Checked the bearings to SAAB specific requirements and change the affected bearings.','Z3456','qas_sez|','2019-11-25|','2019-11-25','0000-00-00','0000-00-00','0000-00-00','','',''),(12139,'35A-469','Saab AB','ASSY ROD','','D522 73514 000 00','','A',4,'OWED-LTA-004','','K24608','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Break Torque of the rod end bearing is over the tolerance of 0.68 Nm,Should be less than 0.68 Nm ','1)The breakaway torque measured on the rod ends were not as per the customer requirement.|2)CIM was inspecting the bearings with bolt and nut through bearings and tightening with and checked the torque. But at SAAB the bolt and nut was torque tightened to 6.3Nm before checking the breakaway torque of the bearing which i not as per the drawing requirement.|3)SAAB selection of Bearing for the assembly was not as per the SAAB higher assembly requirement.','|Informed the bearing supplier about the failure of the bearing during torque test and requested to inspect 100% before shipment.','|SAAB to analyze and revise the drawing according to their higher assembly requirement.','CIM BOM will be changed upon the receipt of revised drawing / instruction from SAAB','C78025','2019-11-21','Dharani(Shankar)','qas_sez(a)','100324','2019-10-28','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','Customer End','yes','Misc','Dharani(Shankar)','no','','|Checked the bearings to SAAB specific requirements and change the affected bearings.','Z3456','qas_sez|','2019-11-26|','2019-11-26','0000-00-00','0000-00-00','0000-00-00','','',''),(12140,'35A-469','Saab AB','ASSY ROD','','D522 73514 000 00','','A',4,'1600192682','','K24607','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Break Torque of the rod end bearing is over the tolerance of 0.68 Nm,Should be less than 0.68 Nm ','1)The breakaway torque measured on the rod ends were not as per the customer requirement.|2)CIM was inspecting the bearings with bolt and nut through bearings and tightening with and checked the torque. But at SAAB the bolt and nut was torque tightened to 6.3Nm before checking the breakaway torque of the bearing which i not as per the drawing requirement.|3)SAAB selection of Bearing for the assembly was not as per the SAAB higher assembly requirement.','|Informed the bearing supplier about the failure of the bearing during torque test and requested to inspect 100% before shipment.','|SAAB to analyze and revise the drawing according to their higher assembly requirement.','CIM BOM will be changed upon the receipt of revised drawing / instruction from SAAB','C78024','2019-11-21','Dharani(Shankar)','qas_sez(a)','100324','2019-10-28','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','Customer End','yes','Misc','Dharani(Shankar)','no','','|Checked the bearings to SAAB specific requirements and change the affected bearings.','Z3456','qas_sez|','2019-11-26|','2019-11-26','0000-00-00','0000-00-00','0000-00-00','','',''),(12141,'35A-469','Saab AB','ASSY ROD','','D522 73514 000 00','','A',2,'OWED-LTA-004','','K24614','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Break Torque of the rod end bearing is over the tolerance of 0.68 Nm,Should be less than 0.68 Nm ','1)The breakaway torque measured on the rod ends were not as per the customer requirement.|2)CIM was inspecting the bearings with bolt and nut through bearings and tightening with and checked the torque. But at SAAB the bolt and nut was torque tightened to 6.3Nm before checking the breakaway torque of the bearing which i not as per the drawing requirement.|3)SAAB selection of Bearing for the assembly was not as per the SAAB higher assembly requirement.','|Informed the bearing supplier about the failure of the bearing during torque test and requested to inspect 100% before shipment.','|SAAB to analyze and revise the drawing according to their higher assembly requirement.','CIM BOM will be changed upon the receipt of revised drawing / instruction from SAAB','C78031','2019-11-21','Dharani(Shankar)','qas_sez(a)','100324','2019-10-28','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','Customer End','yes','Misc','Dharani(Shankar)','no','','|Checked the bearings to SAAB specific requirements and change the affected bearings.','Z3456','qas_sez|','2019-11-26|','2019-11-26','0000-00-00','0000-00-00','0000-00-00','','',''),(12142,'35A-469','Saab AB','ASSY ROD','','D522 73514 000 00','','A',2,'OWED-LTA-004','','K26980','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Break Torque of the rod end bearing is over the tolerance of 0.68 Nm,Should be less than 0.68 Nm ','1)The breakaway torque measured on the rod ends were not as per the customer requirement.|2)CIM was inspecting the bearings with bolt and nut through bearings and tightening with and checked the torque. But at SAAB the bolt and nut was torque tightened to 6.3Nm before checking the breakaway torque of the bearing which i not as per the drawing requirement.|3)SAAB selection of Bearing for the assembly was not as per the SAAB higher assembly requirement.','|Informed the bearing supplier about the failure of the bearing during torque test and requested to inspect 100% before shipment.','|SAAB to analyze and revise the drawing according to their higher assembly requirement.','CIM BOM will be changed upon the receipt of revised drawing / instruction from SAAB','C80705','2019-11-21','Dharani(Shankar)','qas_sez(a)','100324','2019-10-28','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','Customer End','yes','Misc','Dharani(Shankar)','no','','|Checked the bearings to SAAB specific requirements and change the affected bearings.','Z3456','qas_sez|','2019-11-26|','2019-11-26','0000-00-00','0000-00-00','0000-00-00','','',''),(12143,'35A-469','Saab AB','ASSY ROD','','D522 73514 000 00','','A',1,'1600192682','','K24612','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Break Torque of the rod end bearing is over the tolerance of 0.68 Nm,Should be less than 0.68 Nm ','1)The breakaway torque measured on the rod ends were not as per the customer requirement.|2)CIM was inspecting the bearings with bolt and nut through bearings and tightening with and checked the torque. But at SAAB the bolt and nut was torque tightened to 6.3Nm before checking the breakaway torque of the bearing which i not as per the drawing requirement.|3)SAAB selection of Bearing for the assembly was not as per the SAAB higher assembly requirement.','|Informed the bearing supplier about the failure of the bearing during torque test and requested to inspect 100% before shipment.','|SAAB to analyze and revise the drawing according to their higher assembly requirement.','CIM BOM will be changed upon the receipt of revised drawing / instruction from SAAB','C78029','2019-11-21','Dharani(Shankar)','qas_sez(a)','100324','2019-10-28','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','Customer End','yes','Misc','Dharani(Shankar)','no','','|Checked the bearings to SAAB specific requirements and change the affected bearings.','Z3456','qas_sez|','2019-11-26|','2019-11-26','0000-00-00','0000-00-00','0000-00-00','','',''),(12144,'35A-469','Saab AB','ASSY ROD','','D522 73514 000 00','','A',1,'OWED-LTA-004','','K26980','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Break Torque of the rod end bearing is over the tolerance of 0.68 Nm,Should be less than 0.68 Nm ','1)The breakaway torque measured on the rod ends were not as per the customer requirement.|2)CIM was inspecting the bearings with bolt and nut through bearings and tightening with and checked the torque. But at SAAB the bolt and nut was torque tightened to 6.3Nm before checking the breakaway torque of the bearing which i not as per the drawing requirement.|3)SAAB selection of Bearing for the assembly was not as per the SAAB higher assembly requirement.','|Informed the bearing supplier about the failure of the bearing during torque test and requested to inspect 100% before shipment.','|SAAB to analyze and revise the drawing according to their higher assembly requirement.','CIM BOM will be changed upon the receipt of revised drawing / instruction from SAAB','C80705','2019-11-21','Dharani(Shankar)','qas_sez(a)','100324','2019-10-28','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','Customer End','yes','Misc','Dharani(Shankar)','no','','|Checked the bearings to SAAB specific requirements and change the affected bearings.','Z3456','qas_sez|','2019-11-26|','2019-11-26','0000-00-00','0000-00-00','0000-00-00','','',''),(12145,'35A-469','Saab AB','ASSY ROD','','D522 73514 000 00','','A',1,'OWED-LTA-004','','K24613','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Break Torque of the rod end bearing is over the tolerance of 0.68 Nm,Should be less than 0.68 Nm ','1)The breakaway torque measured on the rod ends were not as per the customer requirement.|2)CIM was inspecting the bearings with bolt and nut through bearings and tightening with and checked the torque. But at SAAB the bolt and nut was torque tightened to 6.3Nm before checking the breakaway torque of the bearing which i not as per the drawing requirement.|3)SAAB selection of Bearing for the assembly was not as per the SAAB higher assembly requirement.','|Informed the bearing supplier about the failure of the bearing during torque test and requested to inspect 100% before shipment.','|SAAB to analyze and revise the drawing according to their higher assembly requirement.','CIM BOM will be changed upon the receipt of revised drawing / instruction from SAAB','C78030','2019-11-21','Dharani(Shankar)','qas_sez(a)','100324','2019-10-28','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','Customer End','yes','Misc','Dharani(Shankar)','no','','|Checked the bearings to SAAB specific requirements and change the affected bearings.','Z3456','qas_sez|','2019-11-26|','2019-11-26','0000-00-00','0000-00-00','0000-00-00','','',''),(12146,'35A-469','Saab AB','ASSY ROD','','D522 73514 000 00','','A',1,'OWED-LTA-004','','A28849','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Break Torque of the rod end bearing is over the tolerance of 0.68 Nm,Should be less than 0.68 Nm ','1)The breakaway torque measured on the rod ends were not as per the customer requirement.|2)CIM was inspecting the bearings with bolt and nut through bearings and tightening with and checked the torque. But at SAAB the bolt and nut was torque tightened to 6.3Nm before checking the breakaway torque of the bearing which i not as per the drawing requirement.|3)SAAB selection of Bearing for the assembly was not as per the SAAB higher assembly requirement.','|Informed the bearing supplier about the failure of the bearing during torque test and requested to inspect 100% before shipment.','|SAAB to analyze and revise the drawing according to their higher assembly requirement.','CIM BOM will be changed upon the receipt of revised drawing / instruction from SAAB','C83084','2019-11-21','Dharani(Shankar)','qas_sez(a)','100324','2019-10-28','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','Customer End','yes','Misc','Dharani(Shankar)','no','','|Checked the bearings to SAAB specific requirements and change the affected bearings.','Z3456','qas_sez|','2019-11-26|','2019-11-26','0000-00-00','0000-00-00','0000-00-00','','',''),(12147,'35A-469','Saab AB','ASSY ROD','','D522 73514 000 00','','A',1,'1600192682','','K24609','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Break Torque of the rod end bearing is over the tolerance of 0.68 Nm,Should be less than 0.68 Nm ','1)The breakaway torque measured on the rod ends were not as per the customer requirement.|2)CIM was inspecting the bearings with bolt and nut through bearings and tightening with and checked the torque. But at SAAB the bolt and nut was torque tightened to 6.3Nm before checking the breakaway torque of the bearing which i not as per the drawing requirement.|3)SAAB selection of Bearing for the assembly was not as per the SAAB higher assembly requirement.','|Informed the bearing supplier about the failure of the bearing during torque test and requested to inspect 100% before shipment.','|SAAB to analyze and revise the drawing according to their higher assembly requirement.','CIM BOM will be changed upon the receipt of revised drawing / instruction from SAAB','C78026','2019-11-21','Dharani(Shankar)','qas_sez(a)','100324','2019-10-28','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','Customer End','yes','Misc','Dharani(Shankar)','no','','|Checked the bearings to SAAB specific requirements and change the affected bearings.','Z3456','qas_sez|','2019-11-26|','2019-11-26','0000-00-00','0000-00-00','0000-00-00','','',''),(12148,'35A-469','Saab AB','ASSY ROD','','D522 73514 000 00','','A',1,'1600217568','','K24615','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Break Torque of the rod end bearing is over the tolerance of 0.68 Nm,Should be less than 0.68 Nm ','1)The breakaway torque measured on the rod ends were not as per the customer requirement.|2)CIM was inspecting the bearings with bolt and nut through bearings and tightening with and checked the torque. But at SAAB the bolt and nut was torque tightened to 6.3Nm before checking the breakaway torque of the bearing which i not as per the drawing requirement.|3)SAAB selection of Bearing for the assembly was not as per the SAAB higher assembly requirement.','|Informed the bearing supplier about the failure of the bearing during torque test and requested to inspect 100% before shipment.','|SAAB to analyze and revise the drawing according to their higher assembly requirement.','CIM BOM will be changed upon the receipt of revised drawing / instruction from SAAB','C78032','2019-11-21','Dharani(Shankar)','qas_sez(a)','100324','2019-10-28','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','Customer End','yes','Misc','Dharani(Shankar)','no','','|Checked the bearings to SAAB specific requirements and change the affected bearings.','Z3456','qas_sez|','2019-11-26|','2019-11-26','0000-00-00','0000-00-00','0000-00-00','','',''),(12149,'35A-470','Saab AB','ASSY ROD','','D522 73514 001 00','','A',2,'OWED-LTA-004','','K27069','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Break Torque of the rod end bearing is over the tolerance of 0.68 Nm,Should be less than 0.68 Nm ','1)The breakaway torque measured on the rod ends were not as per the customer requirement.|2)CIM was inspecting the bearings with bolt and nut through bearings and tightening with and checked the torque. But at SAAB the bolt and nut was torque tightened to 6.3Nm before checking the breakaway torque of the bearing which i not as per the drawing requirement.|3)SAAB selection of Bearing for the assembly was not as per the SAAB higher assembly requirement.','|Informed the bearing supplier about the failure of the bearing during torque test and requested to inspect 100% before shipment.','|SAAB to analyze and revise the drawing according to their higher assembly requirement.','CIM BOM will be changed upon the receipt of revised drawing / instruction from SAAB','C81992','2019-11-21','Dharani(Shankar)','qas_sez(a)','100366','2019-10-28','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','Customer End','yes','Misc','Dharani(Shankar)','no','','|Checked the bearings to SAAB specific requirements and change the affected bearings.','Z3456','qas_sez|','2019-11-25|','2019-11-25','0000-00-00','0000-00-00','0000-00-00','','',''),(12150,'35A-470','Saab AB','ASSY ROD','','D522 73514 001 00','','A',5,'OWED-LTA-004','','K24603','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Break Torque of the rod end bearing is over the tolerance of 0.68 Nm,Should be less than 0.68 Nm ','1)The breakaway torque measured on the rod ends were not as per the customer requirement.|2)CIM was inspecting the bearings with bolt and nut through bearings and tightening with and checked the torque. But at SAAB the bolt and nut was torque tightened to 6.3Nm before checking the breakaway torque of the bearing which i not as per the drawing requirement.|3)SAAB selection of Bearing for the assembly was not as per the SAAB higher assembly requirement.','|Informed the bearing supplier about the failure of the bearing during torque test and requested to inspect 100% before shipment.','|SAAB to analyze and revise the drawing according to their higher assembly requirement.','CIM BOM will be changed upon the receipt of revised drawing / instruction from SAAB','C78049','2019-11-21','Dharani(Shankar)','qas_sez(a)','100366','2019-10-28','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','Customer End','yes','Misc','Dharani(Shankar)','no','','|Checked the bearings to SAAB specific requirements and change the affected bearings.','Z3456','qas_sez|','2019-11-25|','2019-11-25','0000-00-00','0000-00-00','0000-00-00','','',''),(12151,'35A-470','Saab AB','ASSY ROD','','D522 73514 001 00','','A',5,'OWED-LTA-004','','K24994','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Break Torque of the rod end bearing is over the tolerance of 0.68 Nm,Should be less than 0.68 Nm ','1)The breakaway torque measured on the rod ends were not as per the customer requirement.|2)CIM was inspecting the bearings with bolt and nut through bearings and tightening with and checked the torque. But at SAAB the bolt and nut was torque tightened to 6.3Nm before checking the breakaway torque of the bearing which i not as per the drawing requirement.|3)SAAB selection of Bearing for the assembly was not as per the SAAB higher assembly requirement.','|Informed the bearing supplier about the failure of the bearing during torque test and requested to inspect 100% before shipment.','|SAAB to analyze and revise the drawing according to their higher assembly requirement.','CIM BOM will be changed upon the receipt of revised drawing / instruction from SAAB','C80698','2019-11-21','Dharani(Shankar)','qas_sez(a)','100366','2019-10-28','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','Customer End','yes','Misc','Dharani(Shankar)','no','','|Checked the bearings to SAAB specific requirements and change the affected bearings.','Z3456','qas_sez|','2019-11-25|','2019-11-25','0000-00-00','0000-00-00','0000-00-00','','',''),(12152,'35A-470','Saab AB','ASSY ROD','','D522 73514 001 00','','A',1,'1600217568','','K24995','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Break Torque of the rod end bearing is over the tolerance of 0.68 Nm,Should be less than 0.68 Nm ','1)The breakaway torque measured on the rod ends were not as per the customer requirement.|2)CIM was inspecting the bearings with bolt and nut through bearings and tightening with and checked the torque. But at SAAB the bolt and nut was torque tightened to 6.3Nm before checking the breakaway torque of the bearing which i not as per the drawing requirement.|3)SAAB selection of Bearing for the assembly was not as per the SAAB higher assembly requirement.','|Informed the bearing supplier about the failure of the bearing during torque test and requested to inspect 100% before shipment.','|SAAB to analyze and revise the drawing according to their higher assembly requirement.','CIM BOM will be changed upon the receipt of revised drawing / instruction from SAAB','C80699','2019-11-21','Dharani(Shankar)','qas_sez(a)','100366','2019-10-28','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','Customer End','yes','Misc','Dharani(Shankar)','no','','|Checked the bearings to SAAB specific requirements and change the affected bearings.','Z3456','qas_sez|','2019-11-25|','2019-11-25','0000-00-00','0000-00-00','0000-00-00','','',''),(12153,'35A-518','Saab AB','ROD ASSY','','D522 73510 000 00','','A',3,'OWED-LTA-004','','A26392','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Break Torque of the rod end bearing is over the tolerance of 0.68 Nm,Should be less than 0.68 Nm ','1)The breakaway torque measured on the rod ends were not as per the customer requirement.|2)CIM was inspecting the bearings with bolt and nut through bearings and tightening with and checked the torque. But at SAAB the bolt and nut was torque tightened to 6.3Nm before checking the breakaway torque of the bearing which i not as per the drawing requirement.|3)SAAB selection of Bearing for the assembly was not as per the SAAB higher assembly requirement.','|Informed the bearing supplier about the failure of the bearing during torque test and requested to inspect 100% before shipment.','|SAAB to analyze and revise the drawing according to their higher assembly requirement.','CIM BOM will be changed upon the receipt of revised drawing / instruction from SAAB','C80280','2019-11-21','Dharani(Shankar)','qas_sez(a)','GLB442528','2019-10-28','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','Customer End','yes','Misc','Dharani(Shankar)','no','','|Checked the bearings to SAAB specific requirements and change the affected bearings.','Z3456','qas_sez|','2019-11-25|','2019-11-25','0000-00-00','0000-00-00','0000-00-00','','',''),(12154,'35A-518','Saab AB','ROD ASSY','','D522 73510 000 00','','A',4,'OWED-LTA-004','','A26394','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Break Torque of the rod end bearing is over the tolerance of 0.68 Nm,Should be less than 0.68 Nm ','1)The breakaway torque measured on the rod ends were not as per the customer requirement.|2)CIM was inspecting the bearings with bolt and nut through bearings and tightening with and checked the torque. But at SAAB the bolt and nut was torque tightened to 6.3Nm before checking the breakaway torque of the bearing which i not as per the drawing requirement.|3)SAAB selection of Bearing for the assembly was not as per the SAAB higher assembly requirement.','|Informed the bearing supplier about the failure of the bearing during torque test and requested to inspect 100% before shipment.','|SAAB to analyze and revise the drawing according to their higher assembly requirement.','CIM BOM will be changed upon the receipt of revised drawing / instruction from SAAB','C80280','2019-11-21','Dharani(Shankar)','qas_sez(a)','GLB442528','2019-10-28','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','Customer End','yes','Misc','Dharani(Shankar)','no','','|Checked the bearings to SAAB specific requirements and change the affected bearings.','Z3456','qas_sez|','2019-11-25|','2019-11-25','0000-00-00','0000-00-00','0000-00-00','','',''),(12155,'35A-665','Saab AB','ROD ASSY','','D5227349400400','','PART ISSUE C',3,'OWED-LTA-001','','A23666','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Break Torque of the rod end bearing is over the tolerance of 0.68 Nm,Should be less than 0.68 Nm ','1)The breakaway torque measured on the rod ends were not as per the customer requirement.|2)CIM was inspecting the bearings with bolt and nut through bearings and tightening with and checked the torque. But at SAAB the bolt and nut was torque tightened to 6.3Nm before checking the breakaway torque of the bearing which i not as per the drawing requirement.|3)SAAB selection of Bearing for the assembly was not as per the SAAB higher assembly requirement.','|Informed the bearing supplier about the failure of the bearing during torque test and requested to inspect 100% before shipment.','|SAAB to analyze and revise the drawing according to their higher assembly requirement.','CIM BOM will be changed upon the receipt of revised drawing / instruction from SAAB','C76704','2019-11-21','Dharani(Shankar)','qas_sez(a)','100373','2019-10-28','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','Customer End','yes','Misc','Dharani(Shankar)','no','','|Checked the bearings to SAAB specific requirements and change the affected bearings.','Z3456','qas_sez|','2019-11-26|','2019-11-26','0000-00-00','0000-00-00','0000-00-00','','',''),(12156,'35A-665','Saab AB','ROD ASSY','','D5227349400400','','PART ISSUE C',2,'OWED-LTA-001','','A23671','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Break Torque of the rod end bearing is over the tolerance of 0.68 Nm,Should be less than 0.68 Nm ','1)The breakaway torque measured on the rod ends were not as per the customer requirement.|2)CIM was inspecting the bearings with bolt and nut through bearings and tightening with and checked the torque. But at SAAB the bolt and nut was torque tightened to 6.3Nm before checking the breakaway torque of the bearing which i not as per the drawing requirement.|3)SAAB selection of Bearing for the assembly was not as per the SAAB higher assembly requirement.','|Informed the bearing supplier about the failure of the bearing during torque test and requested to inspect 100% before shipment.','|SAAB to analyze and revise the drawing according to their higher assembly requirement.','CIM BOM will be changed upon the receipt of revised drawing / instruction from SAAB','C76705','2019-11-21','Dharani(Shankar)','qas_sez(a)','100373','2019-10-28','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','Customer End','yes','Misc','Dharani(Shankar)','no','','|Checked the bearings to SAAB specific requirements and change the affected bearings.','Z3456','qas_sez|','2019-11-26|','2019-11-26','0000-00-00','0000-00-00','0000-00-00','','',''),(12157,'35A-665','Saab AB','ROD ASSY','','D5227349400400','','PART ISSUE C',3,'OWED-LTA-001','','A23668','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Break Torque of the rod end bearing is over the tolerance of 0.68 Nm,Should be less than 0.68 Nm ','1)The breakaway torque measured on the rod ends were not as per the customer requirement.|2)CIM was inspecting the bearings with bolt and nut through bearings and tightening with and checked the torque. But at SAAB the bolt and nut was torque tightened to 6.3Nm before checking the breakaway torque of the bearing which i not as per the drawing requirement.|3)SAAB selection of Bearing for the assembly was not as per the SAAB higher assembly requirement.','|Informed the bearing supplier about the failure of the bearing during torque test and requested to inspect 100% before shipment.','|SAAB to analyze and revise the drawing according to their higher assembly requirement.','CIM BOM will be changed upon the receipt of revised drawing / instruction from SAAB','C76705','2019-11-21','Dharani(Shankar)','qas_sez(a)','100373','2019-10-28','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','Customer End','yes','Misc','Dharani(Shankar)','no','','|Checked the bearings to SAAB specific requirements and change the affected bearings.','Z3456','qas_sez|','2019-11-26|','2019-11-26','0000-00-00','0000-00-00','0000-00-00','','',''),(12158,'35A-665','Saab AB','ROD ASSY','','D5227349400400','','PART ISSUE C',2,'OWED-LTA-001','','A23664','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Break Torque of the rod end bearing is over the tolerance of 0.68 Nm,Should be less than 0.68 Nm ','1)The breakaway torque measured on the rod ends were not as per the customer requirement.|2)CIM was inspecting the bearings with bolt and nut through bearings and tightening with and checked the torque. But at SAAB the bolt and nut was torque tightened to 6.3Nm before checking the breakaway torque of the bearing which i not as per the drawing requirement.|3)SAAB selection of Bearing for the assembly was not as per the SAAB higher assembly requirement.','|Informed the bearing supplier about the failure of the bearing during torque test and requested to inspect 100% before shipment.','|SAAB to analyze and revise the drawing according to their higher assembly requirement.','CIM BOM will be changed upon the receipt of revised drawing / instruction from SAAB','C76704','2019-11-21','Dharani(Shankar)','qas_sez(a)','100373','2019-10-28','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','Customer End','yes','Misc','Dharani(Shankar)','no','','|Checked the bearings to SAAB specific requirements and change the affected bearings.','Z3456','qas_sez|','2019-11-26|','2019-11-26','0000-00-00','0000-00-00','0000-00-00','','',''),(12159,'35A-665','Saab AB','ROD ASSY','','D5227349400400','','PART ISSUE C',1,'OWED-LTA-001','','A21438','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Break Torque of the rod end bearing is over the tolerance of 0.68 Nm,Should be less than 0.68 Nm ','1)The breakaway torque measured on the rod ends were not as per the customer requirement.|2)CIM was inspecting the bearings with bolt and nut through bearings and tightening with and checked the torque. But at SAAB the bolt and nut was torque tightened to 6.3Nm before checking the breakaway torque of the bearing which i not as per the drawing requirement.|3)SAAB selection of Bearing for the assembly was not as per the SAAB higher assembly requirement.','|Informed the bearing supplier about the failure of the bearing during torque test and requested to inspect 100% before shipment.','|SAAB to analyze and revise the drawing according to their higher assembly requirement.','CIM BOM will be changed upon the receipt of revised drawing / instruction from SAAB','C73405','2019-11-21','Dharani(Shankar)','qas_sez(a)','100373','2019-10-28','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','Customer End','yes','Misc','Dharani(Shankar)','no','','|Checked the bearings to SAAB specific requirements and change the affected bearings.','Z3456','qas_sez|','2019-11-26|','2019-11-26','0000-00-00','0000-00-00','0000-00-00','','',''),(12160,'35A-665','Saab AB','ROD ASSY','','D5227349400400','','PART ISSUE C',1,'OWED-LTA-001','','A21038','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Break Torque of the rod end bearing is over the tolerance of 0.68 Nm,Should be less than 0.68 Nm ','1)The breakaway torque measured on the rod ends were not as per the customer requirement.|2)CIM was inspecting the bearings with bolt and nut through bearings and tightening with and checked the torque. But at SAAB the bolt and nut was torque tightened to 6.3Nm before checking the breakaway torque of the bearing which i not as per the drawing requirement.|3)SAAB selection of Bearing for the assembly was not as per the SAAB higher assembly requirement.','|Informed the bearing supplier about the failure of the bearing during torque test and requested to inspect 100% before shipment.','|SAAB to analyze and revise the drawing according to their higher assembly requirement.','CIM BOM will be changed upon the receipt of revised drawing / instruction from SAAB','C73296','2019-11-21','Dharani(Shankar)','qas_sez(a)','100373','2019-10-28','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','Customer End','yes','Misc','Dharani(Shankar)','no','','|Checked the bearings to SAAB specific requirements and change the affected bearings.','Z3456','qas_sez|','2019-11-26|','2019-11-26','0000-00-00','0000-00-00','0000-00-00','','',''),(12161,'35A-665','Saab AB','ROD ASSY','','D5227349400400','','PART ISSUE C',1,'OWED-LTA-001','','A23670','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Break Torque of the rod end bearing is over the tolerance of 0.68 Nm,Should be less than 0.68 Nm ','1)The breakaway torque measured on the rod ends were not as per the customer requirement.|2)CIM was inspecting the bearings with bolt and nut through bearings and tightening with and checked the torque. But at SAAB the bolt and nut was torque tightened to 6.3Nm before checking the breakaway torque of the bearing which i not as per the drawing requirement.|3)SAAB selection of Bearing for the assembly was not as per the SAAB higher assembly requirement.','|Informed the bearing supplier about the failure of the bearing during torque test and requested to inspect 100% before shipment.','|SAAB to analyze and revise the drawing according to their higher assembly requirement.','CIM BOM will be changed upon the receipt of revised drawing / instruction from SAAB','C76705','2019-11-21','Dharani(Shankar)','qas_sez(a)','100373','2019-10-28','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','Customer End','yes','Misc','Dharani(Shankar)','no','','|Checked the bearings to SAAB specific requirements and change the affected bearings.','Z3456','qas_sez|','2019-11-26|','2019-11-26','0000-00-00','0000-00-00','0000-00-00','','',''),(12162,'35A-665','Saab AB','ROD ASSY','','D5227349400400','','PART ISSUE C',1,'OWED-LTA-001','','A23665','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Break Torque of the rod end bearing is over the tolerance of 0.68 Nm,Should be less than 0.68 Nm ','1)The breakaway torque measured on the rod ends were not as per the customer requirement.|2)CIM was inspecting the bearings with bolt and nut through bearings and tightening with and checked the torque. But at SAAB the bolt and nut was torque tightened to 6.3Nm before checking the breakaway torque of the bearing which i not as per the drawing requirement.|3)SAAB selection of Bearing for the assembly was not as per the SAAB higher assembly requirement.','|Informed the bearing supplier about the failure of the bearing during torque test and requested to inspect 100% before shipment.','|SAAB to analyze and revise the drawing according to their higher assembly requirement.','CIM BOM will be changed upon the receipt of revised drawing / instruction from SAAB','C76704','2019-11-21','Dharani(Shankar)','qas_sez(a)','100373','2019-10-28','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','Customer End','yes','Misc','Dharani(Shankar)','no','','|Checked the bearings to SAAB specific requirements and change the affected bearings.','Z3456','qas_sez|','2019-11-26|','2019-11-26','0000-00-00','0000-00-00','0000-00-00','','',''),(12163,'35A-665','Saab AB','ROD ASSY','','D5227349400400','','PART ISSUE C',1,'OWED-LTA-001','','A23674','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Break Torque of the rod end bearing is over the tolerance of 0.68 Nm,Should be less than 0.68 Nm ','1)The breakaway torque measured on the rod ends were not as per the customer requirement.|2)CIM was inspecting the bearings with bolt and nut through bearings and tightening with and checked the torque. But at SAAB the bolt and nut was torque tightened to 6.3Nm before checking the breakaway torque of the bearing which i not as per the drawing requirement.|3)SAAB selection of Bearing for the assembly was not as per the SAAB higher assembly requirement.','|Informed the bearing supplier about the failure of the bearing during torque test and requested to inspect 100% before shipment.','|SAAB to analyze and revise the drawing according to their higher assembly requirement.','CIM BOM will be changed upon the receipt of revised drawing / instruction from SAAB','C76706','2019-11-21','Dharani(Shankar)','qas_sez(a)','100373','2019-10-28','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','Customer End','yes','Misc','Dharani(Shankar)','no','','|Checked the bearings to SAAB specific requirements and change the affected bearings.','Z3456','qas_sez|','2019-11-26|','2019-11-26','0000-00-00','0000-00-00','0000-00-00','','',''),(12164,'35A-665A','Saab AB','ROD ASSY','','D5227349400400','','PART ISSUE D',3,'OWED-LTA-005','','A27819','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Break Torque of the rod end bearing is over the tolerance of 0.68 Nm,Should be less than 0.68 Nm ','1)The breakaway torque measured on the rod ends were not as per the customer requirement.|2)CIM was inspecting the bearings with bolt and nut through bearings and tightening with and checked the torque. But at SAAB the bolt and nut was torque tightened to 6.3Nm before checking the breakaway torque of the bearing which i not as per the drawing requirement.|3)SAAB selection of Bearing for the assembly was not as per the SAAB higher assembly requirement.','|Informed the bearing supplier about the failure of the bearing during torque test and requested to inspect 100% before shipment.','|SAAB to analyze and revise the drawing according to their higher assembly requirement.','CIM BOM will be changed upon the receipt of revised drawing / instruction from SAAB','C81498','2019-11-21','Dharani(Shankar)','qas_sez(a)','100373','2019-10-28','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','Customer End','yes','Misc','Dharani(Shankar)','no','','|Checked the bearings to SAAB specific requirements and change the affected bearings.','Z3456','qas_sez|','2019-11-26|','2019-11-26','0000-00-00','0000-00-00','0000-00-00','','',''),(12165,'51A-191','THE BOEING COMPANY','FIXED HINGE ASSEMBLY - ML','','113W8345-21','','PSDL REV A',1,'BOEING 001AD','','A31980','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','bearing rework','','','','','','2019-11-22','Ramesh(D)','Phaniraj(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','no','no','no','Assembly','','in process','yes','Misc','Ramesh(D)','no','N04137|BACB10FH06GZ','','E3456',NULL,NULL,NULL,'0000-00-00','0000-00-00','0000-00-00','','',''),(12166,'18-344A','Magellan Aerospace Wrexham','LANDING TOP PANNEL','R 229015','F574 50968 203','','E, ECN PG49998ST1TV31, PG49999ST1TF77',1,'175166','','100221','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Profile unclear up to 0.5 mm','part shifted while running time|improper clamping|while inter changing toggle clamp time ,unclamp the all clamp,before clamp part.  ','|option stop added in program(Before unclamp the toggle clamp of semi finished parts,clamp the opposite side toggle clamp)','| Ø6mm pin will be introduce in fixture,for ensure part butting. ','','','2019-11-23','Dhananjaya(N)','','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','1','no','BMV 60-1','Dhananjaya(N)','no','','|immediately stop the machine and ensure the all previous completed parts, all are found OK.','E3456','qas|qas|','2019-11-27|2019-12-18|','2019-12-18','0000-00-00','0000-00-00','0000-00-00','','',''),(12167,'51-191','THE BOEING COMPANY','FIXED HINGE - MLG, DRAG S','347601','113W8345-23','NA','PSDL REV A',1,'BOEING 001AD','','101074','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Base thickness under size due to wrong butting the Part on the Fixture','The first facing  operation removed the 0.3mm excess material.\r\n|The Part not Seated on the fixture top surface properly.  |The operator not able to cross check the part butting area by using feeler gauge|The clamping method of the part so critical','|The part is seated on the fixture properly. the opposite surface of the seated side was  dialed. top level ensured. ','|one plunger dial indicator added.  After loading the part, the operator will cross check and ensure the top level. ','CAPA verified and found ok.','','2019-11-24','Nagaraju P K()','','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','','','','','|Production stopped. All machined parts checked. Found ok.','Z3456','pe_sez|pe_sez|pe_sez|qas_sez|','2019-11-25|2019-11-26|2019-11-26|2019-12-05|','2019-12-05','0000-00-00','0000-00-00','0000-00-00','','',''),(12168,'56A-104','GKN Aerospace Orangeburg','CLOSEOUT - RIB, LWR, AFT','','119A1441-605','','PSDL REV -',1,'A000047471','','A30744','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','no','CSK OVERSIZE AND HENCE GAP FOUND AFTER NUT PLATE ASSEMBLY. ','','','','','','2019-11-27','Ramesh(D)','Ramesh(D)','','0000-00-00','Assembly done at ATPL.','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','no','yes','no','Assembly','','IN PROCESS','no','Misc','Dharani(Shankar)','yes','','','Z3456',NULL,NULL,NULL,'0000-00-00','2019-12-06','0000-00-00','','',''),(12169,'56A-103','GKN Aerospace Orangeburg','CLOSEOUT RIB ASSY - AFT, ','','119A1383-606','','PSDL REV -',1,'A000047470','','A29651','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','no','CSK OVERSIZE AND HENCE GAP FOUND AFTER NUT PLATE ASSEMBLY.','','','','','','2019-11-27','Ramesh(D)','Ramesh(D)','','0000-00-00','ASSEMBLY DONE AT ATPL.','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','no','yes','no','Assembly','','IN PROCESS','no','Misc','Dharani(Shankar)','yes','','','Z3456',NULL,NULL,NULL,'0000-00-00','2019-12-06','0000-00-00','','',''),(12170,'35-418','Saab AB','BRACKET TARGET','533924C','D522 73538 200 00','','A',1,'OWED-LTA-004','','98002','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Part damaged during leg cut-out operation.','1) The reference taken for the leg cutout tool was wrong.|2) Operator took wrong Z-offset.|3) Z-offset was supposed to be taken on the top face of the fixture but the offset was taken on the part butting face of the fixture.|4) operator did not referred to the MPS properly before taking the reference.','|Re-took the reference under supervisor guidance and continued the production.','|On job training given to the operator on how to interpret the reference points defined in MPS.','Training effectiveness of the operator will be verified during the next batch productions.','','2019-11-27','Krishna(Chowdary.G.P.)','','','0000-00-00','NC raised','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','Misc','Nagendra(SN)','no','','|Immediately stopped the machine and cross verified the references of all the other tools loaded in the machine.','E3456','qas_sez|qas_sez|','2019-12-02|2019-12-05|','2019-12-05','0000-00-00','0000-00-00','0000-00-00','','',''),(12171,'35-702','Saab AB','LEVER 1','827928','D5227281620300','NA','PART ISSUE D',1,'OWED-LTA-001','','98040','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Tool dig mark on 8.995 H7 bore.','1) Damage inside the bore caused due to improper handling of de-burr tool.|2) During the de-burring of outer profile of the part using the pneumatic de-burring tool the operator touched the ID of the bore due to hand slip.|3) Hole de burring was not done by the operator in the designated area because of which the operator did not had sufficient space to handle the parts.','|Instructed the operator to carry out the de burring operation only in the designated areas with sufficient handling space.','|De-burring zones are designated in the shop floor and awareness given to the operators to carry out de-burring operations only on the designated area. ','De-burring operation of the next batches will be verified.','','2019-11-27','Krishna(Chowdary.G.P.)','','','0000-00-00','NC raised','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','Misc','Nagendra(SN)','no','','|checked the previously completed parts and no similar defects identified.','E3456','qas_sez|qas_sez|qas_sez|','2019-12-02|2019-12-05|2019-12-05|','2019-12-05','0000-00-00','0000-00-00','0000-00-00','','',''),(12172,'18-780A','Magellan Aerospace Wrexham','STUD AFT HINGE','A1041Z','F57551861200','NA','PART ISSUE A',1,'190638','','98406','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','REQUIRED VALUE IS Ø3+0.1 MM MEASURED VALUE Ø3.2 MM.','Hole oblong 0.1 mm|cutting angle of the drill bit was not equal. |due to improper tool grinding,the cutting angle was varied and the operator did not the ensure the cutting angle of drill bit','|ensure the cutting angle of the new drill bit,before loading to machine.','|instruction given to the operators,to ensure the cutting tool parameter after regrinding.','CA AND PA FOUND OK','','2019-11-27','Anjinamurthy(H)','','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','7','no','Misc','Dhananjaya(N)','no','','|immediately stop the machine and inspected the previous completed parts ,all parts are found OK.  ','E3456','pe|qas|','2019-12-02|2019-12-02|','2019-12-02','0000-00-00','0000-00-00','0000-00-00','','',''),(12173,'56-029A','GKN Aerospace Orangeburg','CLOSEOUT FAIRING - WINGTI','290324B3','119A1532-604','NA','PSDL REV A',2,'LTA GKN ORANGEBURG W','','99185','','2019-11-30',NULL,'no','no','yes','no','no','no','yes','yes','no','PROGRAM FAULT TOOL DIG ON 3D FACE SO PART REJECTED.','1) The G code provided in the program was not read by the machine.|2) G68.2 code is blocked in the machine but this was not communicated to the engineer by the Software developer.|3) Common format is used by the engineering to generate the programs for 5 axis machines and this specific requirement was not communicated to the programmers in engineering dept. therefore they followed the standard template and generated the program.','|Information given to all the engineers to not to provide G68.2 code to these specific machines and instructed to use the alternative coding.','|Requested the machining application engineer to activate the G68.2 code and the software developer to change the parameters accordingly in the post.','Activation of the code and the changes of the post will be monitored for the new programs.','','2019-11-30','CAD(sez)','','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','3','no','Makino PS105-3','pe_sez(a)','no','','|Immediately informed the engineering team and the machine application engineer and checked all similar programs for G68.2 code and replaces the same with the alternate code which is readable by the machine. ','Z3456','qas_sez|','2019-12-10|','2019-12-10','0000-00-00','0000-00-00','0000-00-00','','',''),(12174,'35A-545','Saab AB','BEAM ASSY','','D522 73335 000 00','','PART ISSUE A',1,'OWED-LTA-001','','A31993','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','VISUAL APPEARANCE NOT OK,AS PER AIPS 02-04-006 (ZINC NICKEL PLATING CHIP OUT) ','','','','','','2019-12-03','qas_sez(a)','qas_sez(a)','','0000-00-00','NC CREATED','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','no','yes','no','Assembly','','FI','no','Misc','qas_sez(a)','no','93611|D5227347420200','','Z3456',NULL,NULL,NULL,'0000-00-00','0000-00-00','2019-12-04','','NA','NA'),(12175,'35-407','Saab AB','BEAM 3','1738802','D522 73396 200 00','','A',1,'OWED-LTA-001','','101107','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','','','','','','','2019-12-04','Nagaraju P K()','Nagaraju P K ,','','0000-00-00','Side wall thickness u/s up to 2MM ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','no','yes','no','With Treatment','','3','no','a51nx-01','pe_sez(a)','no','','','Z3456',NULL,NULL,NULL,'0000-00-00','0000-00-00','2019-12-04','','',''),(12176,'35-622','Saab AB','FLAP, VENT','513520 A','D5227280420000','NA','PART ISSUE A',1,'1600217549','','85767','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Operations Incomplete','','','','','','2019-12-05','pe_sez(a)','op_sez(s)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','no','no','no','With Treatment','','3','yes','Misc','pe_sez(a)','no','','','Z3456',NULL,NULL,NULL,'0000-00-00','0000-00-00','2019-12-31','','',''),(12177,'35A-354A','Saab AB','LIFT PIN HOUSING AFT','','423Z1124-6-52','','1',2,'LTA Forecast PO B787','','A32136','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Zinc Nickel plating chip off','','','','','','2019-12-05','qas_sez(a)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','no','yes','no','Assembly','','FI','no','Misc','qas_sez(a)','no','N07757|BACB28AP20Z253','','Z3456',NULL,NULL,NULL,'0000-00-00','0000-00-00','2019-12-05','','NA','NA'),(12178,'35A-354A','Saab AB','LIFT PIN HOUSING AFT','','423Z1124-6-52','','1',2,'LTA Forecast PO B787','','A32143','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Zinc Nickel plating chip off','','','','','','2019-12-05','qas_sez(a)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','no','yes','no','Assembly','','04','no','Misc','qas_sez(a)','no','N07757|BACB28AP20Z253','','Z3456',NULL,NULL,NULL,'0000-00-00','0000-00-00','2019-12-06','','NA','NA'),(12179,'35-609A','Saab AB','LEVER','568689','D5227335220300','NA','PART ISSUE B,SCH ISSUE C',1,'OWED-LTA-004','','99286','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Dia 17.995 +0.018MM over size by 0.06MM','','','','','','2019-12-06','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','NC created','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','no','yes','no','With Treatment','','FI','no','Misc','Nagendra(SN)','no','','','E3456',NULL,NULL,NULL,'0000-00-00','0000-00-00','2019-12-07','','NA','NA'),(12180,'35-699','Saab AB','LEVER 3 ','814285','D5227280920400','NA','PART ISSUE C',4,'OWED-LTA-001','','100499','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Total hight undersized by 1.00 MM ','work offset wrong.|while taking of tool offset, work \'Z\' off set was not ensured.','|\'Z\' work offset corrected and run the machine.remaining parts are found OK .','|1) awareness given to operator.\r<br/>2)profile marking will be introduced in program.  ','','','2019-12-06','Krishna(Chowdary.G.P.)','','','0000-00-00','NC Created','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','no','yes','no','With Treatment','','FI','no','Misc','Nagendra(SN)','no','','|immediately stop the machine and informed to supervisor and rejected part moved to quality clinic.','E3456','qas|','2019-12-19|','0000-00-00','0000-00-00','0000-00-00','0000-00-00','','',''),(12181,'51-144','THE BOEING COMPANY','STRUT, AFT','H29604','112A7111-602','NA',' PSDL REV -',2,'BOEING 001AA','','97757','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','1 part thread Effective diameter undersized, therefore thread go gauge not answering second part threading operation not done.','1)a) Due to wear of the threading insert the effective diameter of the thread got undersized.\r\nb) The operator removed the part from the machine before the completion of threading cycle.|2)a) The life time of the insert used was less than the defined life time of the tool.\r\nb) The machine stopped for a warning raised due to external error for which the operator thought that the part was completed and removed the part. |3)a) According to the insert life monitoring the insert used was supposed to be worn out after 20 parts but this insert got worn before the completion of 20 parts.\r\nb) The machine was stopped for low air pressure because of loss of air in the supply line.','|1) Changed the insert and the air hose and continued the production after releasing the error message and retaking the offset.\r<br/>2) Re verified the life of the insert and reduced the insert life from 30No\'s to 25No\'s.','|1) Training and awareness given to all the operators about the reduction in insert life.\r<br/>2) Informed all the operators to ensure any loss of air in the supply due to leakage once a day.','Reduction in the insert life and training of the operators will be verified in the next batch production.','','2019-12-06','Narasimha Murthy (K G)','','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','no','no','no','With Treatment','','7','yes','Misc','Narasimha Murthy (K G)','no','','|Immediately stopped the production and checked the previously completed parts and no similar defects identified.','Z3456','|','2019-12-06|','0000-00-00','0000-00-00','0000-00-00','0000-00-00','','',''),(12182,'55-013','Spirit Aero Systems Inc. Tulsa','BRACKET','180307-1','276A9127-6','NA','NIL',1,'LTA PO spirit ','','101167','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Hole Diameter 2.50MM Measures 6.00MM','Dia 6.00 Ball nose run in lieu of Dis 2.5 Drill|Improper Tool Indexing (Incomplete Tool Indexing)due to Low Air pressure|BMV machine do not stop automatically when Air pressure is Low  (Limitation of the BMV Machine.)|No specific checklist for the BMV Machine operator\'s to ensure the Tool Indexing after Air pressure Low.','|All tools removed from the Magazine and Tool offset taken.','|1. All Machine operators appraised about the NC.\r<br/>2. All machine operators trained about the limitation of BMV Machine.\r<br/>3. Check list updated to incorporate Proper Tool Indexing.','','','2019-12-07','Subramanya L(Naik)','','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','','yes','','','','1','','','','','','|Machine Stopped and Informed to Supervisor and Maintenance department.','E3456','pe|qas|','2019-12-09|2019-12-09|','0000-00-00','0000-00-00','0000-00-00','0000-00-00','','',''),(12183,'47-122A','GKN Aerospace Filton','CROSS MEMBER FWD M/C','628653','F57550106200','NA','PART ISSUE A',1,'GS68-LTA-1-2018','','101877','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Profile Dig mark','RH program run in lieu of LH|Improper Program Selection|Multiple CRN\'s program\'s stored in DNC Mode','|RH program removed and LH program run and found OK','|Production Supervisors to ensure only the current part program is available for the operator in DNC Mode.','','','2019-12-07','Subramanya L(Naik)','','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','','yes','','','','3','','','','','','|Machine Stopped and Informed the Supervisor.\r\nPart moved to Quality clinic.','E3456','pe|qas|','2019-12-09|2019-12-09|','0000-00-00','0000-00-00','0000-00-00','0000-00-00','','',''),(12184,'35-720','Saab AB','ROD BODY','8241','D5227333720200','NA','PART ISSUE B',1,'OWED-LTA-005','','102091','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Tooling marks on OD and Slot length oversize.','1) Tooling marks are formed on the OD of the part due to rotation of the part inside fixture during machining running time.|2) Clamping force was not uniformly distributed on all the parts.|3) 4 parts are loaded per setup and according to the fixture design all the four parts are clamped by using a clamp made of single material (Refer MPS for more details) because of which if the variation of the OD between four parts are greater than .01mm the clamping force will not be equal on all the parts.','|Information given to all the operators to load the parts which falls between the .01mm variation limit.','|Quality alert will be displayed near the machine for all similar part numbers to create awareness to the operators on the specific requirements and the same shall be included in the MPS of the respective Part numbers during the next revision in routing.','','','2019-12-10','Nagaraju P K()','','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','no','yes','no','With Treatment','','7','no','Misc','pe_sez(a)','no','','|1) Immediately stopped the machine and checked the separated the parts as a group of four with OD variations less than .01mm\r\n2) Checked the tools for any damage and replaced the damaged tools and re-took the offset.','Z3456','qas_sez|','2019-12-11|','0000-00-00','0000-00-00','0000-00-00','0000-00-00','','',''),(12185,'35-598','Saab AB','CORNER','565568','D5227338620300','NA','PART ISSUE B',2,'PA1687 LTA-1','','101112','','0000-00-00',NULL,'yes','no','yes','no','yes','no','no','no','no','1 nos Mazak i700 profile dig in SEZ.1nos Face dig Makino slim-AHS Machine.','','','','','','2019-12-10','Ravi nayak()','','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','no','yes','no','With Treatment','','4','no','Misc','prodn_aero(prodn)','no','','','A3456','qas_aero|','2019-12-17|','0000-00-00','0000-00-00','0000-00-00','0000-00-00','','',''),(12186,'35-598','Saab AB','CORNER','565570','D5227338620300','NA','PART ISSUE B',1,'OWED-LTA-001','','99144','','0000-00-00',NULL,'yes','no','yes','no','yes','no','no','no','no','Part dig in Mazak i700 SEZ  ','','','','','','2019-12-10','Ravi nayak()','prodn_aero(prodn)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','no','yes','no','With Treatment','','3rd','no','Misc','prodn_aero(prodn)','no','','','A3456',NULL,NULL,NULL,'0000-00-00','0000-00-00','2019-12-13','','',''),(12187,'35-166C','Saab AB','HOUSING, PIN ','560746','423Z1124-6-01','NA','--C',1,'LTA Forecast PO B787','','99260','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Spot face depth 3mm instead of 1mm. ','Wrong tool length compensation taken|During re setting tool length not ensured','|New tool offset taken and run the remaining parts all are found OK','|1)operator taken tool and work offset re ensured with shift in-charge.                                                   2) quality displayed and instruction given to  all operator.  ','','','2019-12-11','Dinesh kulal()','','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','no','yes','no','With Treatment','','15','no','Misc','Dinesh kulal()','no','','|immediately stop the machine and informed to shift in-charge.  ','A3456','qas|','2019-12-18|','0000-00-00','0000-00-00','0000-00-00','0000-00-00','','',''),(12188,'35-186','Saab AB','CED_LATCH_FITTING-FWD','711512B4','425Z0610-18','','---',1,'LTA Forecast B787 De','','101323','','0000-00-00',NULL,'yes','no','yes','no','yes','no','no','no','no','Required diameter is 25.41mm +0.017mm measured diameter is 25.47mm.','Boring bar run out|chips struck on BT-40 holder   |chips not cleaned in holder|insufficient air pressure through spindle nozzle','|clean the magazine and holder with manually then run the part.','|every Monday clean the magazine and tool holder and maintain the checklist .\r<br/>set the required air pressure. ','','','2019-12-11','Dinesh kulal()','','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','no','yes','no','With Treatment','','05','no','Misc','Dinesh kulal()','no','','|stop the machine and segregate part with identification tag and informed to shift in-charge. ','A3456','qas|','2019-12-19|','0000-00-00','0000-00-00','0000-00-00','0000-00-00','','',''),(12189,'58-087','Saab AB','TOW BRAKE MANIFOLD BRKT','724371B0','326P3S2341-203-M001','NA','PART ISSUE 001',2,'LTA FORECAST FOR TX ','','102198','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','1.required diameter is 3.81 mm +0.05/-0.025,measured diameter is 4.25mm     \r\n\r\n2.dig mark found on part .      \r\n                              ','1.wrong tool selected .\r\n2.while cut out part was lifted.|1.in program required diameter is 3.81 mm but added in program    4.25mm.\r\n2.less stock for cut out.|1.typing error.\r\n','|1.Delete the old program and given to new program.\r<br/>2.added stock for cut out program.and run parts all parts are found OK.','|Before start the fair part cross check the inspection plan and tool list.prescience of operator and supervisor in front of machine.   ','','','2019-12-11','Ramesh(Poojary)','','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','no','yes','no','With Treatment','','03','no','Misc','Subramanya L(Naik)','no','','|stop the machine and move the part to quality clinic with identification tag.\r\n','E3456','cam|qas|qas|','2019-12-11|2019-12-18|2019-12-18|','0000-00-00','0000-00-00','0000-00-00','0000-00-00','','',''),(12190,'56-110','GKN Aerospace Orangeburg','FAIRING SUPPORT - T.E.','76538/01','119A1560-603','NA','PSDL REV -',1,'A000047470','','100735','','0000-00-00',NULL,'yes','no','no','no','yes','yes','no','no','no','HOLE POSITION IN CMM','','','','','','2019-12-11','pe_sez(a)','Srinivasa C N,Somashekar ,Shivaraj K S,Madhu Kumar N,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','no','yes','no','With Treatment','','FI','no','Slim3n-5AHS-2','Mahesh(N)','no','','','Z3456',NULL,NULL,NULL,'0000-00-00','0000-00-00','2019-12-10','','',''),(12191,'35-758','Saab AB','LEVER CAM','YMS7','D5227353720400','NA','PART  ISSUE D',2,'1600283741','','101203','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','DIA 22.15H7 BORE SHIFTED UP TO 0.2 MM',' RUNNING PART WAS DISTURBED|PART FACE WAS IMPROPER FITTING|WHILE CLAMPING PART WAS LIFTED |BURR NOT REMOVED ON BUTTING FACE.','|REMOVE THE BURR ON BUTTING FACE,','|ENSURE THE BUTTING FACE BY USING FEELER GAUGE.','CA AND PA FOUND OK.','','2019-12-12','Krishna(Chowdary.G.P.)','','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','Misc','Nagendra(SN)','no','','|AFTER MACHINING  IDENTIFIED THE PROBLEM AND CHECK THE PREVIOUS MACHINED PARTS,ONE PART WAS FOUND WITH SAME PROBLEM ,REMAINING PARTS ARE FOUND OK.','E3456','qas|qas|','2019-12-13|2019-12-13|','2019-12-13','0000-00-00','0000-00-00','0000-00-00','','',''),(12192,'35A-474A','Saab AB','FRAME ASSY','','D5227338400000','','B',1,'OWED-LTA-001','','A31293','','0000-00-00',NULL,'no','no','no','no','no','yes','yes','yes','no','1 Part sent to LAB testing the purpose of dis-colorization occurs on Alochrome touch-up  ','','','','','','2019-12-12','qas_sez(a)','qas_sez(a)','','0000-00-00','NC CREATION (1 PART SENT TO LAB TESTING)','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','no','no','yes','Assembly','','FI','no','Misc','qas_sez(a)','no','95358|D5227338420000','','Z3456',NULL,NULL,NULL,'0000-00-00','0000-00-00','2019-12-13','','',''),(12193,'18-697A','Magellan Aerospace(Polska) Sp','BUSH','1693400-1/ZEWQ','D278 50164 202','','A',2,'107446','','101127','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Required diameter is 45.964mm to 45.980mm. measured diameter is 45.955mm to 45.960mm  ','UNEVEN STOCK FOR FINISHING TOOLS|ROUGHING INSERT WAS BLUNT|IMPROPER COOLANT FLOW FOR ROUGHING TOOL |CHIPS CLOGGED ON THE PART','|BEFORE RUN THE FINISHING TOOL REMOVE THE CLOGGED CHIPS AND ENSURE THE COOLANT FLOW.','|BEFORE RUN THE FINISHING TOOL ACTIVATE THE OPTIONAL STOP.','CA AND PA FOUND OK.','','2019-12-13','Dinakar(K)','','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Dinakar(K)','no','','|PARTS IDENTIFIED AND SEGREGATE WITH REJECT CARD','E3456','qas|','2019-12-13|','2019-12-13','0000-00-00','0000-00-00','0000-00-00','','',''),(12194,'35A-671','','','','','','',0,'','','','','0000-00-00',NULL,'no','no','no','no','no','no','no','no','no','','','','','','','2019-12-13','select','','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','','no','no','no','','','','no','','select','no','','','Z3456',NULL,NULL,NULL,'0000-00-00','0000-00-00','0000-00-00','','',''),(12196,'35A-671','Saab AB','SHAFT LEVER ASSY','','D5227346201800','','PART ISSUE D',1,'OWED-LTA-001','','A32590','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','while plain bush pressing part got bend by over load','','','','','','2019-12-13','Ramesh(D)','Ramesh(D)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','no','yes','no','Assembly','','procesing','no','Misc','Ramesh(D)','no','100901|D5227346221800','','Z3456',NULL,NULL,NULL,'0000-00-00','0000-00-00','2019-12-13','','',''),(12197,'56-007','GKN Aerospace Orangeburg','SPLICE PLATE AFT UPR','8-17-07731/26462','119A1213-607','NA','PSDL REV-',1,'LTA GKN 737 Winglet','','99517','','2019-12-09',NULL,'no','no','yes','yes','yes','no','no','no','no','BECAUSE OFF RAW MATERIAL BEND 5TH AXIS HOLE POSITIONS OUT FOR 0.5 MM TO 1MM WILL BE SHIFTED  SO PART WILL REJECTED   ','1) During the first setup operation the RM bend was not identified.|2) The bend of the RM was checked by the operator after loading to the fixture where the bend was unable to identified.|3) After loading  to the fixture the butting can be identified only on the two side of the material but the bend of the of the material was on the other two faces which was not detected.','|1) Instructed all the operators to ensure the bend on the RM to be less than 0.03mm by inspecting them for flatness on the surface table before loading to the fixture.\r<br/>2) Informed all the operators to check the flatness of all the part to be less than 0.03mm after completely clamping the part in the fixture.','|Informed the stores personnel to communicate the issue to the supplier and to not to inward the parts with bend grater than .03mm','','','2019-12-13','op_sez(s)','','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','no','yes','no','With Treatment','','1','no','Makino PS105-3','pe_sez(a)','no','','|1) Immediately stopped the machine and checked all the previously machined parts and found ok.\r\n2) Checked the other parts in the RM condition for bend by placing the part on the surface table.','Z3456','qas_sez|','2019-12-13|','0000-00-00','0000-00-00','0000-00-00','0000-00-00','','',''),(12198,'18A-740','Magellan Aerospace Wrexham','A/NUT STRIP ASSY','','F57252299000','','A',4,'190638','','A28130','','0000-00-00',NULL,'yes','no','no','no','yes','yes','no','no','no','Pilot hole out of position  of 2.8mm compare to drawing specification - pitch of 35.25mm','Process: Tool offset correction was wrongly entered by the operator.\r\nQuality: Inspection of the pilot hole pitch was inadequate.','|Process: Re-training was carried out to all concern operators on how to ensure the tool correction before starting the cycle. (Refer Attachment-1)\r<br/>Quality: A checking fixture for the hole positions will be implemented by 11-Nov-19 to ensure the hole position during the machining and Inspection.','|Process: Re-training was carried out to all concern operators on how to ensure the tool correction before starting the cycle. (Refer Attachment-1)\r<br/>Quality: A checking fixture for the hole positions will be implemented by 11-Nov-19 to ensure the hole position during the machining and Inspection.','Next batches are verified and found ok.','','2019-12-14','qas(qas)','','','0000-00-00','NC CREATION','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Assembly','','FI','no','Misc','qas(qas)','no','','|All the parts in FG, & WIP are verified and the affected batches are rejected and scrapped.','E3456','qas_sez|','2019-12-14|','2019-12-14','0000-00-00','0000-00-00','0000-00-00','','',''),(12199,'18A-740','Magellan Aerospace Wrexham','A/NUT STRIP ASSY','','F57252299000','','A',2,'190638','','A27912','','0000-00-00',NULL,'yes','no','no','no','yes','yes','no','no','no','Pilot hole out of position  of 2.8mm compare to drawing specification - pitch of 35.25mm','Process: Tool offset correction was wrongly entered by the operator.\r\nQuality: Inspection of the pilot hole pitch was inadequate.\r\n','|Process: Re-training was carried out to all concern operators on how to ensure the tool correction before starting the cycle. (Refer Attachment-1)\r<br/>Quality: A checking fixture for the hole positions will be implemented by 11-Nov-19 to ensure the hole position during the machining and Inspection.','|Process: Re-training was carried out to all concern operators on how to ensure the tool correction before starting the cycle. (Refer Attachment-1)\r<br/>Quality: A checking fixture for the hole positions will be implemented by 11-Nov-19 to ensure the hole position during the machining and Inspection.','Next batches are verified and found ok.','','2019-12-14','qas(qas)','','','0000-00-00','NC CREATION','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Assembly','','FI','no','Misc','qas(qas)','no','','|All the parts in FG, & WIP are verified and the affected batches are rejected and scrapped.','E3456','qas_sez|','2019-12-14|','2019-12-14','0000-00-00','0000-00-00','0000-00-00','','',''),(12200,'18A-740','Magellan Aerospace Wrexham','A/NUT STRIP ASSY','','F57252299000','','A',1,'190638','','A28129','','0000-00-00',NULL,'yes','no','no','no','yes','yes','no','no','no','Pilot hole out of position  of 2.8mm compare to drawing specification - pitch of 35.25mm','Process: Tool offset correction was wrongly entered by the operator.\r\nQuality: Inspection of the pilot hole pitch was inadequate.\r\n','|Process: Re-training was carried out to all concern operators on how to ensure the tool correction before starting the cycle. (Refer Attachment-1)\r<br/>Quality: A checking fixture for the hole positions will be implemented by 11-Nov-19 to ensure the hole position during the machining and Inspection.','|Process: Re-training was carried out to all concern operators on how to ensure the tool correction before starting the cycle. (Refer Attachment-1)\r<br/>Quality: A checking fixture for the hole positions will be implemented by 11-Nov-19 to ensure the hole position during the machining and Inspection.','Next batches are verified and found ok.','','2019-12-14','qas(qas)','','','0000-00-00','NC CREATION','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Assembly','','FI','no','Misc','qas(qas)','no','','|All the parts in FG, & WIP are verified and the affected batches are rejected and scrapped.','E3456','qas_sez|','2019-12-14|','2019-12-14','0000-00-00','0000-00-00','0000-00-00','','',''),(12201,'18A-740','Magellan Aerospace Wrexham','A/NUT STRIP ASSY','','F57252299000','','A',3,'190638','','A28131','','0000-00-00',NULL,'yes','no','no','no','yes','yes','no','no','no','Pilot hole out of position  of 2.8mm compare to drawing specification - pitch of 35.25mm','Process: Tool offset correction was wrongly entered by the operator.\r\nQuality: Inspection of the pilot hole pitch was inadequate.\r\n','|Process: Re-training was carried out to all concern operators on how to ensure the tool correction before starting the cycle. (Refer Attachment-1)\r<br/>Quality: A checking fixture for the hole positions will be implemented by 11-Nov-19 to ensure the hole position during the machining and Inspection.\r<br/>','|Process: Re-training was carried out to all concern operators on how to ensure the tool correction before starting the cycle. (Refer Attachment-1)\r<br/>Quality: A checking fixture for the hole positions will be implemented by 11-Nov-19 to ensure the hole position during the machining and Inspection.','Next batches are verified and found ok.','','2019-12-14','qas(qas)','','','0000-00-00','NV CREATION','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Assembly','','FI','no','Misc','qas(qas)','no','','|All the parts in FG, & WIP are verified and the affected batches are rejected and scrapped.','E3456','qas_sez|','2019-12-14|','2019-12-14','0000-00-00','0000-00-00','0000-00-00','','',''),(12202,'18A-740','Magellan Aerospace Wrexham','A/NUT STRIP ASSY','','F57252299000','','A',2,'190638','','A27911','','0000-00-00',NULL,'yes','no','no','no','yes','no','no','no','yes','Pilot hole out of position  of 2.8mm compare to drawing specification - pitch of 35.25mm','Process: Tool offset correction was wrongly entered by the operator.\r\nQuality: Inspection of the pilot hole pitch was inadequate.\r\n','|Process: Re-training was carried out to all concern operators on how to ensure the tool correction before starting the cycle. (Refer Attachment-1)\r<br/>Quality: A checking fixture for the hole positions will be implemented by 11-Nov-19 to ensure the hole position during the machining and Inspection.\r<br/>','|Process: Re-training was carried out to all concern operators on how to ensure the tool correction before starting the cycle. (Refer Attachment-1)\r<br/>Quality: A checking fixture for the hole positions will be implemented by 11-Nov-19 to ensure the hole position during the machining and Inspection.\r<br/>','Next batches are verified and found ok.','C82021','2019-12-14','qas(qas)','','RDN2666','2019-09-19','NC CREATION','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Assembly','','CUST END','no','Misc','qas(qas)','no','','|All the parts in FG, & WIP are verified and the affected batches are rejected and scrapped.','E3456','qas_sez|','2019-12-14|','2019-12-14','0000-00-00','0000-00-00','0000-00-00','','',''),(12203,'18A-740','Magellan Aerospace Wrexham','A/NUT STRIP ASSY','','F57252299000','','A',3,'190638','','A27910','','0000-00-00',NULL,'yes','no','no','no','yes','no','no','no','yes','Pilot hole out of position  of 2.8mm compare to drawing specification - pitch of 35.25mm','Process: Tool offset correction was wrongly entered by the operator.\r\nQuality: Inspection of the pilot hole pitch was inadequate.','|Process: Re-training was carried out to all concern operators on how to ensure the tool correction before starting the cycle. (Refer Attachment-1)\r<br/>Quality: A checking fixture for the hole positions will be implemented by 11-Nov-19 to ensure the hole position during the machining and Inspection.\r<br/>','|Process: Re-training was carried out to all concern operators on how to ensure the tool correction before starting the cycle. (Refer Attachment-1)\r<br/>Quality: A checking fixture for the hole positions will be implemented by 11-Nov-19 to ensure the hole position during the machining and Inspection.\r<br/>','Next batches are verified and found ok.','C81540','2019-12-14','qas(qas)','','RDN2666','2019-09-19','NC CREATION','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Assembly','','CUST END','no','Misc','qas(qas)','no','','|All the parts in FG, & WIP are verified and the affected batches are rejected and scrapped.','E3456','qas_sez|','2019-12-14|','2019-12-14','0000-00-00','0000-00-00','0000-00-00','','',''),(12204,'18A-740','Magellan Aerospace Wrexham','A/NUT STRIP ASSY','','F57252299000','','A',1,'190638','','A27910','','0000-00-00',NULL,'yes','no','no','no','yes','no','no','no','yes','Pilot hole out of position  of 2.8mm compare to drawing specification - pitch of 35.25mm','Process: Tool offset correction was wrongly entered by the operator.\r\nQuality: Inspection of the pilot hole pitch was inadequate.','|Process: Re-training was carried out to all concern operators on how to ensure the tool correction before starting the cycle. (Refer Attachment-1)\r<br/>Quality: A checking fixture for the hole positions will be implemented by 11-Nov-19 to ensure the hole position during the machining and Inspection.\r<br/>','|Process: Re-training was carried out to all concern operators on how to ensure the tool correction before starting the cycle. (Refer Attachment-1)\r<br/>Quality: A checking fixture for the hole positions will be implemented by 11-Nov-19 to ensure the hole position during the machining and Inspection.\r<br/>','Next batches are verified and found ok.','C82021','2019-12-14','qas(qas)','','RDN2666','2019-09-19','NC CREATION','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Assembly','','CUST END','no','Misc','qas(qas)','no','','|All the parts in FG, & WIP are verified and the affected batches are rejected and scrapped.','E3456','qas_sez|','2019-12-14|','2019-12-14','0000-00-00','0000-00-00','0000-00-00','','',''),(12205,'18-119B','Magellan Aerospace Bournemouth',' 	HOUSING OUT B DRG 3 ','1649701-2/WSGW','PID275 40011 200','','D01',1,'428868','','81764','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','yes',' 137 OFF  Bearing Housings PID27540011200 Steel parts have been fettled prior to PFD which is not permitted. These parts are shipped in CIM COC\'s C73688,C72486, C71874 \r\n','To overcome dent marks, fettling was carried out.|Chips gets clogged in between part and fixture during machining, resulting in dents.|The existing fixture itself had preexisting dents on the butting surface.|Since it was Aluminum fixture while in contact with steel part, dent was occurring on both fixture and part.','|Process: The hardened steel material with blackening fixture to be implement to avoid dent damages on fixture and parts\r<br/>Quality: The training conducted thru brain storming, to all the concerned inspectors, we have also planned to carry out the training formally.\r<br/>','|Process: Fixture will be implemented \r<br/>Quality: Training will be carried out to all the concerned inspectors formally','Fixture re-deigned, next batches verified and found ok.','C73688','2019-12-14','qas_sez(a)','','RDN02058','2019-03-04','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Manufacture Only','','Cust','yes','Misc','qas_sez(a)','no','','|Checked the Parts in FG and transit.','Z3456','qas_sez|','2019-12-14|','2019-12-14','0000-00-00','0000-00-00','0000-00-00','','',''),(12206,'18-121A','Magellan Aerospace Bournemouth','BARREL - STRUT','CD703435/06400A','PID572 50463 201','','F',1,'428863','','79578','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','yes','19 OFF Parts shipped on COC C69503, C70631 were identified to be non conforming because of low hardness.','Possible of hardness variation during machining.','|Trial carried out on parts by checking the hardness at different stages of process but the hardness did not varied during machining.','|Root cause not identified and the hardness value reported by the customer did not fell into the category of materials processed by CIM. ','No similar issues reported from customer.','C69503','2019-12-14','qas_sez(a)','','RDN02051','2019-07-05','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','Cust','no','Misc','qas_sez(a)','no','','|All the parts in FG, WIP, & in RM stage are verified and found ok.','Z3456','qas_sez|','2019-12-14|','2019-12-14','0000-00-00','0000-00-00','0000-00-00','','',''),(12207,'18-098B','Magellan Aerospace Bournemouth','VALVE- SEAT','231171B0','D282 50060 204','','D',1,'428870','','92535','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','yes','Burrs envident on the slots and radieuses of the aperture on the D28250060204 seat valve – in result causing paint damage on the complete assembly parts.    \r\nVarious QTYs of various batches affected: API163269, API168968, API168966, API168965, API168967, API113121, API113124','Process: Due to improper / inadequate de-burring.\r\nQuality: Parts are visually inspected for removal of sharp edges through naked eye without magnification could be the possible cause for escape.','|Process: Requirements of break sharp edges are displayed near the machine and the operators are instructed to ensure parts are finished as per the requirement.\r<br/>Quality: 100% inspection of the break sharp edge in the slots & controlled surface will be done under 8X magnifying lamp and sample parts will be inspected in VMS(Vision Measuring System) with magnification of 67X.','|Process: Requirements of break sharp edges are displayed near the machine and the operators are instructed to ensure parts are finished as per the requirement.\r<br/>Quality: 100% inspection of the break sharp edge in the slots & controlled surface will be done under 8X magnifying lamp and sample parts will be inspected in VMS(Vision Measuring System) with magnification of 67X.','Next Batches shipped are verified and found ok.','C80781','2019-12-14','qas_sez(a)','','RDN02107','2019-08-30','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','DN59232','Cust','yes','Misc','qas_sez(a)','no','','|All the parts in FG, WIP and treatment are verified and found ok.','Z3456','qas_sez|','2019-12-14|','2019-12-14','0000-00-00','0000-00-00','0000-00-00','','',''),(12208,'18-101A','Magellan Aerospace Bournemouth','TUBE -STRUT','B 18/067','PID572 50464 202','','F',1,'428863','','91194','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','yes','Qty 152 off, tube strut P/N : PID57250464202 supplied was rejected for Rust and Scratches. This NC also includes RDN\'s 2145, 2147 & 2157.','Corrosion identified on the parts supplied to customer|Protection of part from corrosion was inadequate.|Temporary protection applied during the final packing was inadequate.','|1) Temporary protection oil shall be applied on the part in all the directions before packing for dispatch.\r<br/>2) Part shall be protected with sleeves / foam sheet during storage to avoid scratches.','|1) Quality Alert shall be displayed in all applicable areas to instruct the personnel to apply rust preventive oil during every stage until dispatch.\r<br/>2) Quality Alert shall be displayed in all applicable locations to instruct individuals to use protective sleeves / foam sheets to protect the parts from damages during storage.','Next batch  shipments are monitored and no similar defects are identified.','C83776','2019-12-14','qas_sez(a)','','RDN02144','2019-11-08','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','yes','Manufacture Only','','Cust','no','Misc','qas_sez(a)','no','','|All the parts in FG, WIP are inspected and the details of the parts in transit is communicated to the customer.','Z3456','qas_sez|','2019-12-14|','2019-12-14','0000-00-00','0000-00-00','0000-00-00','','',''),(12209,'18-711A','Magellan Aerospace Wrexham','STUD ','1657633-3/XPMA','D278 50006 206','','D',1,'167896','','94338','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','yes','Machine abuse identified on 13 off parts.','Process: Rubbing of string type chips along the part during machining might have caused machine abuse.Quality: Possibility of identifying machine abuse on the part after machining is minimal.','|Process: Insert cutter raduis is reduced from R.4mm insert to R.2mm insert inorder to reduce the formation of string type of chips from the machine.\r<br/>Quality: Alert of machine abuse defect is displayed near the machine and inspection area and given awareness to the operators and Inspectors.','|Process: Insert cutter raduis is reduced from R.4mm insert to R.2mm insert inorder to reduce the formation of string type of chips from the machine.\r<br/>Quality: Alert of machine abuse defect is displayed near the machine and inspection area and given awareness to the operators and Inspectors.','Next batches produced are verified and the issue is not repeated.','C81268','2019-12-14','qas_sez(a)','','RDN02150','2019-11-20','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','Cust','no','Misc','qas_sez(a)','no','','|All the parts in FG & WIP are inspected and found ok.','Z3456','qas_sez|','2019-12-14|','2019-12-14','0000-00-00','0000-00-00','0000-00-00','','',''),(12210,'18-684A','Magellan Aerospace Bournemouth','FORKEND ASSEMBLY ','CD711594/00816A','D572 50462 201','','J01',1,'425753','','100511','','0000-00-00',NULL,'yes','yes','yes','','','','','','','OD 1/2-20UNJ L H  Threading NO GO  answered','','','','','','2019-12-15','Raghavendra Rao(R)','','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','','yes','','','','05','','','','','','','E3456','pe|pe|','2019-12-16|2019-12-16|','0000-00-00','0000-00-00','0000-00-00','0000-00-00','','',''),(12211,'35-669A','Saab AB','BRACKET ','530222C2','D5227342920600 ','NA','PART ISSUE F',1,'OWED-LTA-002','','101079','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Thickness undersized by 0.5MM','','','','','','2019-12-18','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','NC Created','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','no','yes','no','With Treatment','','FI','no','Misc','qas(qas)','no','','','E3456',NULL,NULL,NULL,'2019-12-18','0000-00-00','2019-12-19','','NA','NA'),(12212,'35-445','Saab AB','INTERCOSTAL','570875','D522 73398 201 00','','A',1,'OWED-LTA-001','','100816','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Part lifted during machining so dig mark observed on part.','','','','','','2019-12-19','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','NC CREATED','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','no','yes','no','With Treatment','','FI','no','Misc','Nagendra(SN)','no','','','E3456',NULL,NULL,NULL,'0000-00-00','0000-00-00','2019-12-20','','NA','NA'),(12213,'35A-599','Saab AB','BEAM ASSY','','D5227338100400','','PART ISSUE C',5,'OWED-LTA-001','','A24328','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','no','Inkjet part-marking not done','','','','','C77657','2019-12-24','qas_sez(a)','qas_sez(a)','GLB428429','2019-12-24','NC RAISED','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','no','no','no','Assembly','','FI','yes','Misc','qas_sez(a)','no','','','Z3456',NULL,NULL,NULL,'0000-00-00','0000-00-00','2019-12-24','','NA','NA'),(12214,'PRN-1','Aerostructures Assemblies India Pvt. Ltd','Partname1','BAT1','part1','RMS','A',1,'Custpo-001','','103513','','0000-00-00',NULL,'yes','no','no','no','yes','yes','no','no','no','','','','','','','2020-01-09','abc(abc)','abc(abc)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','no','no','no','Manufacture Only','','FI','yes','Misc','abc(abc)','no','','','E3456',NULL,NULL,NULL,'0000-00-00','2020-01-09','2020-01-09','','',''),(12215,'PRN-6','Aerostructures Assemblies India Pvt. Ltd','partname6','Bat','part6','RMS','A',1,'Custpo-006','','103515','','0000-00-00',NULL,'yes','no','no','no','no','yes','no','yes','no','','','','','','','2020-01-10','abc(abc)','abc(abc)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','no','no','no','Manufacture Only','','FI','yes','Misc','abc(abc)','no','','','E3456',NULL,NULL,NULL,'0000-00-00','0000-00-00','2020-01-10','','','');

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