(10417,'18-092A','Magellan Aerospace Bournemouth','PRESSURE RING','68115/01','D301 50085 200','L164 T4','A',2,'415456','','62691','','0000-00-00',NULL,'no','no','no','yes','yes','yes','no','no','no','Corrosion observed.','Part has undergone secondary process along with the corrosion pits.|Corrosion was not identified at the initial stage.|Poor visual Inspection.|Sufficient light source was not used by the inspector.','|Information given to supplier on the corrosion observation on the part and informed them to send back the suspected parts before processing.','|1) Information given to all the packing personnel to apply PX-24 sufficiently during every shipment of parts.\r<br/>2) Dedicated tables with sufficient light source is provided to carry out visual inspection. ','Next Batches found ok.','','2018-02-06','Nandishkumar(D.K.)','Bhuvanesh(P)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','DN32383','POST DN','no','Misc','Bhuvanesh(P)','no','','|ALL the parts in FG was rechecked to confirm the parts are free from corrosion. ','E3456','qas|qas|','2018-07-24|2018-07-24|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10418,'18-394A','Magellan Aerospace Bournemouth','VALVE BODY','1573446-2/QA8D','PIA284 40009 200','','A',2,'423253','','69226','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no',' hole over size 0.12mm.','Running time drill was blunt so 4.37mm pin dia 0.12mm oversized. for reason of hanging burr part was not identify the operator so part was found in FI. ','For the next batches we are ensure 4.37 drill cutting edge before start the operation & The dia 4.37 pin checking in both 01 and 03 operation. ','Inform to the operator to ensure the pin size in both 01 and 03 operation and avoid this type of mistakes.','CAPA Found ok','','2018-02-06','Dinakar(K)','Yogeesha R,Vasu SN,Sunil Gowda B N,Sudhakar C.M,Sathish G,Ningaraj A N,Kailash Patil,Dinakar K,Bhuvaneshwar K,Ashoka R,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','FI','no','QT100S-1','Narasimha Murthy(R)','','','Change the 4.37mm drill and run the production.','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10419,'28-027','Magellan Aerospace New York  Inc.','GUIDE ','20190181','141T6274-4','','PL_A + ADCN # 3 & 4, DL_N/C',1,'141859-3002','','68721','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','OD under size up to .5mm.','Due to wrong jaw selected, OD Undersized.','1) jaws re-bored for this particular part.\r\n2) Instructed to Operator to check the MDI mode for every parts & check the run out.','Guidance given to the operator about jaws boring and part run out, and operator check the every part run out before runing the program. ','Next Part Found OK.','','2018-02-06','Dinakar(K)','Seetharamu D,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','3','no','DX 200-2 ','Sandhesh D(S)','','','Re-jaws boring and check the part run out and run the part.','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10420,'35-630','Saab AB','SUPPORT SEAL RETAINER ','203993B1','423Z1834-1-03','NA','---',2,'1600218100','','68900','','0000-00-00',NULL,'yes','no','yes','no','yes','no','no','no','no','Profile dig mark.','5 Axis Machine problem','Machine maintenance done by Jyoti Machine Service Engineer','Machine maintenance frequency increased','CAPA FOUND OK','','2018-02-06','Rangaswamy()','Basavaraju(S. Sr.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','05','no','Misc','Rangaswamy()','','','Immediately machine stopped and informed to Maintenance department  ','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10421,'28-003A','Magellan Aerospace New York  Inc.','PIN-ATTACHMENT WALKING BE','SG2432A2-H30','161A7305-1','','PL-Rev-NC, DL Rev-B',1,'A000148638','','68700','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','OD UNDER SIZE -0.2MM','In OD roughing setup running time insert will be breakage and part will OD oversize and that part not checking the operator and part not maintain in proper stock for finishing tool. So in the finishing setup that part loading time finishing tool get the more stock and coolant flows not\r\ncorrectly and chips will be over lapped in the outer diameter and part will be -0.02mm under sized.','After roughing check the diameter and maintain the proper stock for the finishing tool and run the part and adjust the coolant in insert edge coolant will be avoided the chips over lapping and every 15 to 20 NS change the finished insert tip and run the part so this problem not repeated again . ','After roughing check the diameter and maintain the proper stock for the finishing tool and run the part and adjust the coolant in insert edge coolant will be avoided the chips over lapping and every 15 to 20 ns change the finished insert tip and run the part so this problem not repeated again . ','CAPA Found ok ','','2018-02-07','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','09','no','Misc','Raghavendra Rao(R)','','','Change the insert and Re-offset taken and run the part.','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10422,'43-031','Composite Industrie','BRACKET','6004202 2','V251 15027 201 00','','B00, ECN PV101306ST1AL08',1,'LTA PO-1','','70197','','0000-00-00',NULL,'yes','yes','yes','','','','','','','part profile unclear.','RM wrong loaded by operator.','1)Cross check the RM size in MPS and loaded the RM as per process sheet.\r\n2)Massage given in machine  as \"cross check the RM loading\" before machining. ','1)RM side butting given in fixture.\r\n2)Massage given in machine  as \"cross check the RM loading\" before machining.\r\n','EFFECTIVENESS FOUND OK.','','2018-02-08','Subramanya L(Naik)','        CHETANA K','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','1','','','','','','stop the machine and inform to supervises.','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10423,'51-075','THE BOEING COMPANY','BELLCRANK','F2445-1','252T1271-2','NA','PSDL REV -',1,'486998 MPP','','69714','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Surface mismatch Due to Cutting tool mark','','','','Not observed the like mismatches in next parts.','','2018-02-08','pe_sez(a)','Umesh B,Nataraja C V,Diwakar R.B.,','','0000-00-00','Surface Mismatch','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','yes','With Treatment','','3','no','i700-2','pe_sez(a)','','','for every first part proving time must check the all tool offset in machine. ','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10424,'51-105','THE BOEING COMPANY','RADIUS FILLER ','32377490 45124A','112T7057-9','NA','PSDL REV -',1,'BOEING 001R','','70633','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Tool dig mark.','Clamping was not done properly','Clamping method was arranged in a fool proof method. ','Clamping method was arranged in a fool proof method. ','CAPA FOUND OK','','2018-02-08','Dhananjaya(N)','Dhananjaya(N)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','1','no','Misc','Dhananjaya(N)','','','clamping method was changed and ensured correct one.','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10425,'51-106','THE BOEING COMPANY','RADIUS FILLER','32377490 45124A','112T7057-10','NA','PSDL REV -',1,'BOEING 001R','','70634','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dimensions deviations ','Part was rotated during the machining as the clamping surface of the part was painted and finished surface.','The usage of this type of packing material was made compulsory on this part to ensure that the part does not rotate while machining.','The parts with such surfaces will always be provided with a packing material, and will be made as a standard instructions to the team.','Next batch found ok.','','2018-02-08','Ramesh(Poojary)','Ramesh(Poojary)','','0000-00-00','Avinash Kashyap  (cad cam )','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','1','no','Misc','Dhananjaya(N)','no','','Clamping was aided with a packing material (soft Material) which helped us in tightening the part further more.','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10426,'35A-609','Saab AB','LEVER ASSY','','D5227335200300','','PART ISSUE B',1,'1600217568','','A13261','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Parts damage.','Operator did not ensured the proper pressure of the hydraulic press due to which excess load was applied on the part and resulted in part dig.','|Trained the operator on how to set the pressure and how to calculate the pressure needed based on the tool used.','|Assembly supervisor to ensure the proper pressure of the hydraulic machine before starting the assembly.','Next batches found ok.','','2018-02-09','nagaraju(sez)','nagaraju(sez)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Assembly','','FI','no','Misc','qas_sez(a)','no','','|Immediately stopped the hydraulic machine and corrected the pressure accordingly and continued the assembly process.','Z3456','qas|','2018-08-10|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10428,'35-510','Saab AB','HINGE FAIRING','359864 D','D522 73390 201 00','','A',1,'OWED-LTA-002','','69378','','0000-00-00',NULL,'no','yes','yes','no','no','no','yes','no','no','Part radius dig up to 0.5.','Whenever extra material cut out time screw driver slipped.','Next extra material remove time use the aluminium piece.','Whenever cut out time use the alluminium instrument.','CAPA FOUND OK','','2018-02-09','prodn_aero(prodn)','Kiran.K.S(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Kiran.K.S(K)','','','Change the cut out method & instrument','A3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10429,'35-139','Saab AB','BCD_DR_BEAM_FTG-LWR_FWD-4','722293','424Z1130-13-01','7050 - T7451 ALUMINU','--B',1,'1600218100','','68743','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Outer profile less than requirement(minus 0.3).','Cutter insert broken when positive wall running time & dig mark on part.','Give the optional stop for cutter program to see the cutter insert edges.','Give the optional stop for cutter program to see the cutter insert edges.','CAPA FOUND OK','','2018-02-09','prodn_aero(prodn)','Kiran.K.S(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Dinesh kulal()','','','Change the cutter insert and run the part.','A3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10430,'51-060','THE BOEING COMPANY','BRACKET','789080A9','149A7371-9728','','PSDL REV A',2,'BOEING 001G','','66903','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Program problem part found dig mark','while drilling operation part vibrated so hole ob-longed. ','changed the operation sequence and run the new part and found ok. ','Review all the operation sequence before running the part. ','Next part found within acceptable limit.','','2018-02-10','pe_sez(a)','pe_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','Misc','qas_sez(a)','no','','Checked program sequence and found defective.','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10431,'35-648','Saab AB','BRACKET','515371C','D5227342920300','NA','C',1,'PA1687 LTA-2','','69162','','0000-00-00',NULL,'yes','yes','yes','','','','','','','profile damaged.','wrong program loaded to machine .','Loaded the correct program to machine and run next part found OK .','we have cross check the program before load to machine.','CA/PA FOUND OK.','','2018-02-10','Subramanya L(Naik)','                Subramanya L Naik','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','3','','','','','','stop the machine and check program.','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10432,'35A-353A','Saab AB','LIFT PIN HOUSING FWD','','423Z1124-5-52','','1',1,'1600203627','','A13238','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','BORE OVER SIZE BY 0.015MM','During the reaming operation operator did not ensured the diameter of the bore.','|Informed the operator to ensure the bore diameter  before each and every pass.','|Operator to ensure the bore diameter before every pass of the reamer.','Next Batches found ok.','','2018-02-11','Nagaraju(T)','Nagaraju(T)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Assembly','36607','05','no','Misc','Phaniraj(G)','no','M00915','|Immediately stopped the reaming operation and rechecked all the completed parts and found ok.','E3456','qas|','2018-08-10|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10433,'51-125','THE BOEING COMPANY','BRACKET DETAIL','659121','332A2930-89','NA','PSDL REV B',8,'486998 MPP','','70090','','0000-00-00',NULL,'yes','yes','yes','','','','','','no','Hole position shifted  by 1mm.','1)Fixture wrong loaded by operator. \r<br/>2)8no\'s rejected since 8 no\'s of RM can be loaded in a fixture at a time.','Immediate location bolt added to fixture bottom side. ','In future operator can not wrong load the fixture because  location bolt added to fixture bottom side. ','effectiveness found ok.','','2018-02-12','Subramanya L(Naik)','        Subramanya L Naik\r\nFor Sumil G S','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','3','','','','','','Stop the machine and inform to supervisor.','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10434,'51-083','THE BOEING COMPANY','BRACKET DETAIL','659121','332A2930-8','NA','PSDL REV B',1,'BOEING 001M','','70133','','0000-00-00',NULL,'yes','yes','yes','','','','','','no','Dia 9.525 hole over sized by 0.1mm.','Less than required flute length used hence hole diameter oversize.','Change the new tool required flute length 25mm.','Instruction given to operator that check the tool length , flute length before run the program.\r\n2)Tool flute length given in program. ','Effectiveness Found OK.','','2018-02-13','Subramanya L(Naik)','        CHETANA K','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','3','','','','','','Stop the machine change the new tool.','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10435,'18-003A','Magellan Aerospace Wrexham','BRACKET SUPPORT','628652','D361 50111 200','ABM3 1029 T7651','A',2,'162890','','70368','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Tool offset problem occurred so dig mark occurred in part','Tool offset problem so Dig mark was observed in first set up then dig mark was cleared.','Work instructions given to the operator.','Work instructions given to the operator.','CAPA FOUND OK','','2018-02-13','Dhananjaya(N)','        dharshan d','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','','','','5','','','','','','Tool offset was properly taken.','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10436,'18-354C','Magellan Aerospace Wrexham','SADDLE C / R STRAKE ','A0144U','F575 51398 200 PF','','C',1,'162895','','68667','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Total length under size (0.2mm)','During milling operation insert was weard out and got broken.','1) Insert life was monitored and measured during milling operation.\r\n2) Based on the previous life of insert insert was changed periodically.','1) Depending upon the life time of the insert taken. The supervisors and operators are instructed to change the insert accordingly and to monitor the same for Wear during every cycle.','CA PA found ok','','2018-02-13','Dhananjaya(N)','Narasimhamurthy C,Hari Prasad,Dhananjaya N,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','3','no','VM2-3','Dhananjaya(N)','','','Insert was changed and machining was carried out','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10437,'51-125','THE BOEING COMPANY','BRACKET DETAIL','659121','332A2930-89','NA','PSDL REV B',1,'486998 MPP','','70077','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','','Due Wrong tool loaded.|Due to refereeing the data sheet.|Due to manual editing of the tool name.|Program cannot be read by the machine without manual editing.|CAM Software doesn’t output the program name as machine required.','|Program was changed and program proved part found OK, Obsolete the old program and new proved program saved in to data base.','|When giving the program the program name will be four eye checked.','CA PA found ok.','','2018-02-14','Ramesh(Poojary)','Subramanya L Naik,','','0000-00-00','tool dig mark.','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','3','no','MakinoF5-2','Subramanya L(Naik)','no','','|Program was changed and program proved part found OK','E3456','cam|qas|','2018-08-06|2018-08-10|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10438,'44-008','Saab AB','FRAME INT 2 ','4199102 2','E5347562720101','','A',1,'1600190066','','70837','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Profile dig mark occurred','During milling operation part was loaded in opposite face due to that profile dig mark occurred.','Part was loaded as per the part instructions ensured in process sheet','Fixture to be re ensure the Fool Proof method','CAPA FOUND OK','','2018-02-14','Anjinamurthy(H)','        Paramaeshappa ','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','3','','','','','','Stop the machine and check fixture location.','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10439,'35-142A','Saab AB','BCD_HINGE_SUPPORT_FITTING','494689A2','424Z3111-5','','--B',1,'1600218100','','68726','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Outer wall dig up to 1mm.','25R4 cutter broken at a time of outer wall running time because operator not remove the side two clamps.','again give message after tool changing.','Guide the operator about message of clamp removing.','CAPA FOUND OK','','2018-02-14','prodn_aero(prodn)','Anil(kumar)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Anil(kumar)','','','Change the the cutter and run the part.','A3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10440,'35-150','Saab AB','CED_BS_HINGE_BUMPER_FITTI','9310429','425Z0311-9','7050 - T7451 ALUMINU','--A',1,'PA 1510 FORECAST','','69407','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','wrong correction given so part total height minus side.','wrong correction given actual correction is 0.1mm given value is 1.0mm','Given the correct correction and run next part found ok.','Training to operator in case of correction, inform to seiner shift operator and given the correction.','EFFECTIVENESS FOUND OK.','','2018-02-16','Rangaswamy()','DILIP G C()','','0000-00-00','Total height -ve side 1mm.','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','01','no','Misc','Rangaswamy()','','','stop the machine and check the part dimension .','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10441,'35-165B','Saab AB','HOUSING PIN','330661','423Z1124-5-01','','--B',1,'PA 1510 FORECAST','','63061','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','chamfer over size ','wrong CRC given so chamfer over size,','Every time crc program running time check the D value.',' To prevent the specified chamfer tool on separate kit.','Next batch produced found ok.','','2018-02-17','Rangaswamy()','Rangaswamy()','','0000-00-00','Part Rejected to over size chamfer. ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','07','no','Misc','Gurukiran S(M)','no','','machine stop and give the correct CRC vallue .','E3456','qas|','2018-07-10|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10442,'43-032','Composite Industrie','LOWER LINING BRACKET','72774/01','V251 14022 202 00','','C00, ECN PV104201ST1AA01',2,'LTA- PO-1','','68694','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Dig Formed in hole during holding the parts while painting.','Dig Formed in hole during holding the parts while painting.','atpl corective action pending.','atpl preventive action pending.','Effectiveness will be reviewed.','','2018-02-17','qas_sez(a)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','DN37035','POST DN','no','Misc','qas_sez(a)','no','','atpl containment action pending.','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10443,'35-648','Saab AB','BRACKET','515371C','D5227342920300','NA','C',1,'PA1687 LTA-2','','69162','','0000-00-00',NULL,'yes','yes','yes','','','','','','no','Refer NC#10431','Refer NC#10431','Refer NC#10431','Refer NC#10431','Refer NC#10431','','2018-02-17','Subramanya L(Naik)','        Subramanya L Naik','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','','','','3','','','','','','Stop the machine and check program. ','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10444,'51-041','THE BOEING COMPANY','BRACKET','180534B0','149A7371-9603','','PSDL REV A',2,'BOEING 001F','','70226','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Thickness 2.54mm Measured as 2.4mm to 2.3mm','While part running time tool was broken. ','Inform to CAD CAM department change the program level after continue the production. ','Inform and training given to operator check the feed and speed every program. ','Next part found within acceptable limit.','','2018-02-17','pe_sez(a)','op_sez(s)','','0000-00-00','Part under the Quarantine Status','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','1','no','Misc','pe_sez(a)','no','','New tool added and continue the production. ','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10445,'51-086','THE BOEING COMPANY','KICK LINK','G24256K05','251W3122-4','NA','PSDL REV -',1,'BOEING 001M','','69710','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','no','Part found with the machining step in supplier site.','Part found with the machining step in supplier site.','NC program was changed to remove the extra material(step). ','NC program was changed to remove the extra material(step). ','Step not observed from next run part. ','','2018-02-17','qas_sez(a)','qas_sez(a)','','0000-00-00','Step observed in Treatment house and informed production department for Rework.\r\n\r\nNote: Rework WO to be raised','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','DN37519','POST DN','yes','Misc','qas_sez(a)','yes','','Checked in WIP and ensured.','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10446,'18-780A','Magellan Aerospace Wrexham','STUD AFT HINGE','CD719119','F57551861200','NA','PART ISSUE A',1,'166522','','68695','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','THREAD PITCH PROBLEM','IMPROPER INSERT SELECTION SO THREAD PITCH PROBLEM \r\n(USING 32-UNJ 3ER INSERT INSTEAD OF 20-UNJ 3ER INSERT)','INFORM TO THE OPERATOR ABOUT AFTER FINISH THE ANY THREADING PARTS REMOVE THE THREADING INSERT FROM THE TOOL','INFORM TO THE OPERATOR ABOUT AFTER FINISH THE ANY THREADING PARTS REMOVE THE THREADING INSERT FROM THE TOOL','CAPA FOUND OK','','2018-02-17','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Raghavendra Rao(R)','','','PROPER INSERT SELECTION  AND RE-OFFSET TAKEN AND RUN THE PART','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10447,'35-648','Saab AB','BRACKET','515371C','D5227342920300','NA','C',1,'PA1687 LTA-2','','69162','','0000-00-00',NULL,'yes','yes','yes','','','no','','','no','Refer NC#10431 	','Refer NC#10431','Refer NC#10431','Refer NC#10431','Refer NC#10431','','2018-02-20','Subramanya L(Naik)','        Subramanya L Naik','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','3','','','','','','Refer NC#10431','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10448,'35-118','Saab AB','ALCD_STRUCT_INTERCOSTAL_L','177852B1','423Z1178-3','7050-T7451 ALUMINUM ','--A',1,'1600218100','','68468','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Outer profile radius dig UP TO 0.5.','While filing the extra material in fitting radius filed.','Guide the operator about radius. ','Inform the cadd engg for change the cut out program for remove that stock in machine.','CAPA FOUND OK','','2018-02-20','prodn_aero(prodn)','prodn_aero(prodn)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Dinesh kulal()','','','Change the filing method.','A3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10449,'51-109','THE BOEING COMPANY','IDLER CRANK ','687314','251T2663-2','NA','PSDL REV -',1,'BOEING 001Q','','70715','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','ID OVERSIZE BY +0.3MM.','TOOL SHANK WAS DISTURBED ON PART DIA 15.49MM DIAMETER .DUE TO THAT DIAMETER WAS GETTING OVERSIZE.','THE ADDITIONAL TOOL RELIEF TOOL ARE STORED IN TOOL GRIB FOR THE PARTICULAR PART.','DURING PRODUCTION THE CLEARANCE BETWEEN TOOL SHANK AND PARTS MINIMUM DIAMETER TO BE ENSURE AS PER THAT THE TOOL SHANK TO BE SELECT AND INSTRUCTIONS GIVEN TO OPERATORS.','CAPA FOUND OK','','2018-02-21','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','09','no','Misc','Ravi(M)','','','THE RELIEF  WAS CREATED IN TOOL SHANK DUE TO CLEARANCE BETWEEN DIA 15.49MM AND TOOL SHANK,','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10450,'35-429A','Saab AB','BRACKET ','693822 2B1','D5227341520100','NA','PART ISSUE A',5,'OWED-LTA-001','','69902','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Back side wall thickness less than requirement.','Batting taper in 2nd set up.','Fix the butting block to vice and guide the operator about chips blocking in butting surface.','Fix the butting block to vice.','CAPA FOUND OK','','2018-02-21','prodn_aero(prodn)','Anil(kumar)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Dinesh kulal()','','','Clean the chips in the block butting surface.','A3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10451,'35-426','Saab AB','BRACKET','739630','D522 73394 200 00','','A',1,'OWED-LTA-001','','69406','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Side wall thickness less than requirement.','X Butting wrong done by operator.','Create the new block for butting the part with help of CADD Engineer.','Create the new block for butting the part with help of CADD Engineer. ','CAPA FOUND OK','','2018-02-21','prodn_aero(prodn)','Anil(kumar)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Dinesh kulal()','','','Correct the x butting and then run the part.','A3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10452,'35-426','Saab AB','BRACKET','739630','D522 73394 200 00','','A',2,'OWED-LTA-001','','68272','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Side wall thickness less than requirement.','X butting wrong.','Prepare the new butting block.','Guide the operator about part cross cutting and make the new fixture like butting block.','CAPA FOUND OK','','2018-02-21','prodn_aero(prodn)','Manjunatha.S.T(M)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','01','no','Misc','Dinesh kulal()','','','Correct the x butting and run the part.','A3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10453,'35-560','Saab AB','BRACKET','5124801 1','D522 73418 202 00','','PART ISSUE B',1,'OWED-LTA-001','','68945','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Base thickness less than requirement.','Part lifted in 2nd operation.','In cut out program give the message to observe the cut out stock in setting time.','In cut out program give the message to observe the cut out stock in setting time.','CAPA FOUND OK','','2018-02-23','prodn_aero(prodn)','Dinesh kulal()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Dinesh kulal()','','','Give the cut out stock up to 0.2','A3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10455,'35-266','Saab AB','LATCH PROBE','SF2711B1-H10','424Z6101-1','','--A',2,'PA 1510 FORECAST-2','','69297','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Pocket length shifted 5 mm. ','Work offset wrong taken by operator. ','Cross check the work offset and run. ','Every setting time cross check the work offset before run the part. ','CAPA FOUND OK','','2018-02-24','Dinesh kulal()','Anil(kumar)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','07','no','Misc','Dinesh kulal()','','','Correct the work offset and run the part. ','A3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10456,'35-294','Saab AB','BRACKET','130994B7','424Z1209-3-01','','---',2,'Forecast po for B787','','71166','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Tool dig mark on outer wall.','Fixture direction reversed and work offset wrong.','Engrave the fixture front side.','Put the location hole to fixture clamping block .','CAPA FOUND OK','','2018-02-26','prodn_aero(prodn)','Manjunatha.S.T(M)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Manjunatha.S.T(M)','','','Correct the fixture direction and work offset.','A3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10457,'35-406','Saab AB','BRACKET ','701946 1D1','D522 73395 200 00','','A',2,'OWED-LTA-001','','69403','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Outer wall dig up to 0.3.','Part butting wrong in fixture.','Guide the operator about part butting.','Before tightening the clamp check the part butting with the help of feeler gauge.','CAPA FOUND OK','','2018-02-26','prodn_aero(prodn)','Manjunatha.D()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Manjunatha.D()','','','Correct the butting and run the part.','A3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10458,'35-510A','Saab AB','HINGE FAIRING','359864 D','D5227339020100','NA','PART ISSUE B',1,'OWED-LTA-002','','71366','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Part radius dig up to 0.5MM. 							\r\n','Whenever extra material cut out time screw driver slipped. 							\r\n','Next extra material remove time use the aluminium piece. 							\r\n','Whenever cut out time use the alluminium instrument. 							\r\n','CAPA FOUND OK','','2018-02-27','Ravi nayak()','Kiran.K.S(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Ravi nayak()','','','Change the cut out method & instrument 							\r\n','A3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10459,'18-546A','Magellan Aerospace Wrexham','FITTING INBD FWD','506809C','L575 51830 200','','A00',2,'RM132921 Amnd 1','','68549','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Thickness over size by 0.02mm.','1) Tool running time because of part bend material was not removed completely.\r\n2) Operator did not checked the part in all places to ensure 100% achievement of dimension.','The thickness will be checked in the machine itself before unloading from the machine and if deviation found in thickness program will be re-run to achieve correct thickness.','Instruction given to operator to rerun program for thickness maintain.and check the thickness in machine before unload part from machine.','Part found acceptable after re-work. effectiveness to be measured in the next batch.','','2018-02-27','Subramanya(S)','Eranna K,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','','FI','yes','MakinoF5-4','Narasimha Murthy(R)','','','program rerun for thickness maintain.','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10460,'35-486','Saab AB','BRACKET','515369A','D522 73416 200 00','','A',1,'OWED-LTA-002','','69393','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dig mark on bore.','CRC correction wrong done by operator.','Give the message in program with M00.','Guide the operator about bore CRC .','CAPA FOUND OK','','2018-02-27','prodn_aero(prodn)','Lakshmi(Narasimha)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Dinesh kulal()','','','Adjust the CRC value and run the program.','A3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10461,'35-630','Saab AB','SUPPORT SEAL RETAINER ','203993B1','423Z1834-1-03','NA','---',1,'Forecast po for B787','','70028','','0000-00-00',NULL,'yes','yes','yes','','','','','','','10 Ball nose broken so part dig,','Roughing stock more than actual stock ,actual stock0.5mm,part stock on that time 1.0mm so tool broken.','Next batch production to control the thickness constant on 1 setup','Take the program backup and save to correct folder ','CAPA found ok.','','2018-02-28','Rangaswamy()','        Manohara M','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','05','','','','','','check the all parts stock and change the program ','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10462,'28-002A','Magellan Aerospace New York  Inc.','LOWER LINK','58507-4RB3','161A6104-4','','PL Rev_B, DL Rev_N/C',30,'A000143459','','61309','','2017-05-11',NULL,'no','no','no','no','no','yes','yes','yes','no','Etching of part marking not to drawing requirement.','Refer API Root Cause on Supplier Nc No.198.','Refer API Corrective Action Plan on Supplier Nc No.198.','Refer API Preventive Action Plan on Supplier Nc No.198. ','Next Batch Found Ok','','2018-02-28','Manu(P)','Manu(P)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','With Treatment','DN30988','Final Inspection','no','Misc','Manu(HB)','','','NC Raised for Supplier. NC No. 198 ','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10463,'18-374B','Magellan Aerospace Bournemouth','GAMMA FITTINGS','30318*4629','NSA840020-075PF','','L',9,'423231','','70315','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Out of inspection of 100No\'s of part no NSA840020-075 a Qty. of 9 No\'s is rejected due to observation of Improper coverage of Solid film lubricant, improper masking and unapproved rework.','This is happen during the transportation as there was no safety in the inner layer of the box in which the parts were shipped','Parts were done manual touch up as per the specification and found ok','Instruction was given to the treatment house on packaging to put extra kushan type of material surronding the inner layer of the box to avoid such paint damages during the transportation.','Next Lot Received from the treatment supplier ,parts were checked and found visually acceptable to the requirement','','2018-03-01','qas_sez(a)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','DN37451','POST DN','no','Misc','qas_sez(a)','no','','parts were identified and segregated and the same was communicated to the treatment house','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10464,'18-373B','Magellan Aerospace Bournemouth','GAMMA FITTINGS','28428472-D','NSA840020-050PF','','L',13,'423231','','67303','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Out of inspection of 100No\'s of part no NSA840020-050 a Qty. of 13 No\'s is rejected due to observation of Improper coverage, Poor Marking,& Scratches on OD.','','','','','','2018-03-01','qas_sez(a)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','DN37450','POST DN','no','Misc','qas_sez(a)','no','','','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10465,'18-377B','Magellan Aerospace Bournemouth','GAMMA FITTINGS','30318*4601','NSA840020-200PF','','L',13,'423232','','69454','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Out of inspection of 100No\'s of part no NSA840020-200 a Qty. of 13 No\'s is rejected due to observation of Part marking Invisibility, unclear rear surface, scratches and dimensional deviation.','','','','','','2018-03-01','qas_sez(a)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','DN37453','POST DN','no','Misc','qas_sez(a)','no','','','Z3456','nandishkumardk|','2018-07-14|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10466,'18-375B','Magellan Aerospace Bournemouth','GAMMA FITTINGS','8651','NSA840020-100PF','','L',3,'423231','','70059','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Out of inspection of 100No\'s of part no NSA840020-100 a Qty. of 3 No\'s is rejected due to observation of Part marking Invisibility, scratches, unapproved rework, unclear rear face, unclear front face, & Improper masking.','','','','','','2018-03-01','qas_sez(a)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','DN37452','POST DN','no','Misc','qas_sez(a)','no','','','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10467,'18-375B','Magellan Aerospace Bournemouth','GAMMA FITTINGS','8651','NSA840020-100PF','','L',7,'423231','','70059','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Out of inspection of 100No\'s of part no NSA840020-100 a Qty. of 7 No\'s is rejected due to observation of Part marking Invisibility, scratches, unapproved rework, unclear rear face, unclear front face, & Improper masking.','','','','','','2018-03-01','qas_sez(a)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','DN37452','POST DN','no','Misc','qas_sez(a)','no','','','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10468,'35-245','Saab AB','WASHER SMALL','850836-16','423Z1457-1','','--C',1,'Forecast po for B787','','70414','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Part chamfer oversized.','While setting time tool nose radius was not considered, so ID chamfer getting oversize.','Instruction given to the operator about tool nose radius and tool directions.','Instruction given to the operator about tool nose radius and tool directions during Machining.','cA PA FOUND OK','','2018-03-02','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','05','no','Misc','Sandhesh D(S)','','','Check the tool data and given the proper tool nose radius.','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10469,'18-314A','Magellan Aerospace Bournemouth','STUD','504356','D278 50006 206 01','','D',1,'423233','','69485','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Thread flat so gauge not answered. ','DURING INSERT CHANGE WRONG OFFSET GIVEN . DUE TO THAT MINOR DIA AND EFFECTIVE DIA WAS NOT FINISHED','TRAINING IS GIVING TO THE OPERATOR FOR OFFSET DIMENSIONS DURING INSERT CHANGE','TRAINING IS GIVING TO THE OPERATOR FOR OFFSET DIMENSIONS DURING INSERT CHANGE','cA PA FOUND OK','','2018-03-03','Dinakar(K)','Sunil Gowda B N,Sudhakar C.M,SHIVAKUMAR ,Ravi M,Punith G S,Ningaraj A N,Girish HP,BHUVANAPRAKASH  J.S,Ashoka R,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','FI','no','QT100S-2','Narasimha Murthy(R)','','','NEXT PART OFFSET WAS CORRECTED EFFECTIVE DIA WAS ACHIEVED','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10470,'18-314A','Magellan Aerospace Bournemouth','STUD','504356','D278 50006 206 01','','D',3,'423233','','69485','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Thickness over size from 0.010mm to 0.030mm.','During part inspection by the operator Micrometer Zero setting was did wrong. So part had over size.','During part inspection from operator in production they were educated how to make zero on Micrometer with the usage of Tissue paper cleaning in both anvils.','Operators are aware of how to handle Micrometer during inspection.','cA PA FOUND OK','','2018-03-03','Dinakar(K)','Sunil Gowda B N,Sudhakar C.M,SHIVAKUMAR ,Ravi M,Punith G S,Ningaraj A N,Girish HP,BHUVANAPRAKASH  J.S,Ashoka R,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Manufacture Only','','fi','yes','QT100S-2','Narasimha Murthy(R)','','','ZERO SET THE MICROMETER AND PART CHECKED FOUND OK.','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10471,'51-082','THE BOEING COMPANY','BRACKET DETAIL','659761','332A2930-2','NA','PSDL REV B',1,'BOEING 001M','','70759','','0000-00-00',NULL,'yes','yes','yes','','','','','','no','Bore oversize by 0.2mm.','wrong CRC correction entered(0.2mm instead of 0.002mm).','1.Tool replaced from end mill to reamer tool.\r\n2.Informed operators to avoid these kind of manual errors. ','Tool replaced from end mill to reamer tool.','CA/PA found OK.','','2018-03-03','Subramanya L(Naik)','        Subramanya L Naik','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','3','','','','','','stop the machine and check given correction. ','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10472,'35-232A','Saab AB','HINGE BRACKET 4 ','233915B8','D576 50007 209','','E00',3,'1600223433/Forecast ','','71167','','0000-00-00',NULL,'yes','yes','yes','','','no','','','no','M/C FMS SHUDULE PROBLEM SO PART REJECT[ PALLET NOMBER CHANGEING]','M/C FMS SHUDULE PROBLEM SO PART REJECT[ PALLET NOMBER CHANGEING]','Given to training on particular operator to check the schedule details of the FMS m/c.','Informed to operator to every batch check the FMS Schedule And run the program','CA/PA found acceptable.','','2018-03-04','Lohith(K)','                        Diwakar R.B.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','03','','','','','','stop the machine and check the schedule quantity','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10473,'18-032A','Magellan Aerospace Bournemouth','BUSH','CD700162/05878A','PID278 50165 200','','A',8,'423255','','70153','','0000-00-00',NULL,'yes','no','no','no','no','yes','no','yes','no','OD OVERSIZE BY 0.006 TO 0.008 MM','Parts was processed to dull finish cadmium platting which resulted in improper coverage all over the part surface.|','Instruction given to all the process owners to inspect the part at every stage of operations.|','process changed to dull to Bright finish.|','FAIR proved and parts found ok after the process change. ','','2018-03-04','Nandishkumar(D.K.)','Bhuvanesh(P)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','DN37489','POST DN','no','Misc','Bhuvanesh(P)','no','','All the parts in-house and WIP are re-inspected and the deviated parts are reprocessed.|','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10474,'18-032A','Magellan Aerospace Bournemouth','BUSH ','CD748432/00277B','PID278 50165 200','','A',61,'415448','','63076','','0000-00-00',NULL,'yes','no','no','no','no','yes','no','yes','no','OD UNDERSIZED BY 0.005/0.008 MM ','Parts was processed to dull finish cadmium platting which resulted in improper coverage all over the part surface.|','Instruction given to all the process owners to inspect the part at every stage of operations.|','process changed to dull to Bright finish.|','FAIR proved and parts found ok after the process change. ','','2018-03-04','Nandishkumar(D.K.)','Bhuvanesh(P)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','POST DN','no','Misc','Bhuvanesh(P)','no','','All the parts in-house and WIP are re-inspected and the deviated parts are reprocessed.|','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10475,'18-679A','Magellan Aerospace Bournemouth','BUSH','CD749591/05892A','D278 50165 200','','A',6,'417546','','68748','','0000-00-00',NULL,'yes','no','no','no','no','yes','no','yes','no','OD OVERSIZED BY 0.004/0.007 MM ','Part OD got oversize after treatment that was ensured|Untreated condition that was not ensured|The untreated parts were check by trainees due that manual error occurred','|The training given to the trainees','|Training record to be created','CAPA found ok','','2018-03-05','Nandishkumar(D.K.)','Bhuvanesh(P)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','DN36276','POST DN','no','Misc','Bhuvanesh(P)','no','','|The remaining parts in Inspection and ready to treatment are ensure found ok','E3456','qas|','2018-08-07|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10476,'18-032A','Magellan Aerospace Bournemouth','BUSH ','CD748432/00277B','PID278 50165 200','','A',61,'415448','','63076-1','','0000-00-00',NULL,'yes','no','no','no','yes','yes','no','no','no','ID Diameter oversize 0.005/0.013 mm.','Parts was processed to dull finish cadmium platting which resulted in improper coverage all over the part surface.||','Instruction given to all the process owners to inspect the part at every stage of operations.||','process changed to dull to Bright finish.||','FAIR proved and parts found ok after the process change.','','2018-03-05','Nandishkumar(D.K.)','Bhuvanesh(P)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','DN34264','POST DN','no','Misc','Nandishkumar(D.K.)','no','','All the parts in-house and WIP are re-inspected and the deviated parts are reprocessed.||','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10477,'18-090A','Magellan Aerospace Bournemouth','BUSH','1517166-3/M5AZ','D278 50164 200','S80 FHT','A',2,'415455','','62947','','0000-00-00',NULL,'yes','no','no','no','no','yes','no','yes','no','CD PLATING CHIPPED OUT(CHROMATE NOT DONE)','Improper handling of parts during inspection.','Parts will be stored in proper trays during transit and inspection.','inspection will be carried out with sufficiant space to handle the parts and care will be taken during holding the parts.','CA PA Found ok.','','2018-03-05','Nandishkumar(D.K.)','Bhuvanesh(P)','','0000-00-00','CD PLATING CHIPPED OUT(CHROMATE NOT DONE)','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','DN37465','POST DN','no','Misc','Bhuvanesh(P)','no','','Care taken to handle the parts during inspection.','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10478,'35A-354A','Saab AB','LIFT PIN HOUSING FWD','','423Z1124-6-52','','1',4,'1600218100','','A13652','','0000-00-00',NULL,'yes','no','yes','no','yes','no','no','no','no','bore oversize','During the reaming operation operator did not ensured the diameter of the bore.','|Informed the operator to ensure the bore diameter before each and every pass.','|Operator to ensure the bore diameter before every pass of the reamer.','Next Batches found ok. ','','2018-03-06','Lohith(K)','Lohith(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Assembly','','03','no','Misc','Nagaraju(T)','no','M01478','|Immediately stopped the reaming operation and rechecked all the completed parts and found ok. ','E3456','qas|','2018-08-10|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10479,'35A-353A','Saab AB','LIFT PIN HOUSING FWD','','423Z1124-5-52','','1',1,'1600203627','','A13650','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','bore over size','During the reaming operation operator did not ensured the diameter of the bore.','|Informed the operator to ensure the bore diameter before each and every pass.','|Operator to ensure the bore diameter before every pass of the reamer.','Next Batches found ok.','','2018-03-06','Lohith(K)','Lohith(K)','','0000-00-00','bore over size','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Assembly','','03','no','Misc','Nagaraju(T)','no','M01478','|Immediately stopped the reaming operation and rechecked all the completed parts and found ok.','E3456','qas|qas|','2018-08-07|2018-08-10|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10480,'35-303A','Saab AB','RIB INTER 1 ','703726B0','F575 54795 200 00','','SCH-ISSUE B, PART ISSUE A',1,'A330 NEO FORECAST -2','','70036','','0000-00-00',NULL,'yes','yes','yes','','','','','','','12R4 bull nose wall finishing program running time tool broken so dig mark found at base . \r\n\r\n','Tool holding length was 31mm.','New HANITA make dia 12R4 tool loaded with holding length of minimum 40mm.message added in the program about holding length of 40mm.','Message added in the program about holding length of 40mm.','NC Not closed as the CAPA is under investigation.','','2018-03-06','Narayanappa(G)','        Sathish Y.R.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','7','','','','','','New hanita make dia 12R4 tool loaded & continue the production','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10481,'28-003A','Magellan Aerospace New York  Inc.','PIN-ATTACHMENT WALKING BE','SG2432A3-H10','161A7305-1','','PL-Rev-NC, DL Rev-B',2,'A000148638','','68703','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Internal Dia is Under size by up to 0.6mm.\r\nNominal Required 28.346/28.397mm.\r\nMeasuring 27.740mm.\r\n','Operator Mistake.','From Next batch parts will be kept in separate trays.','','Waiting for next Batch.','','2018-03-06','Dinakar(K)','SHIVAKUMAR ,Seetharamu D,Santhosh Kumar N,S. Shiva Kumar,Raghavendra P,Punith G S,Madhu ,Girish HP,Dinakar K,Chandrashekara V K,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','Manufacture Only','','FI','no','DX 200-2 ','Manu(P)','','','Parts Segregated in to two Separate Trays Finished & Semi finished. ','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10482,'35-624','Saab AB','SHAFT 3','B76568','D5227281320000','NA','PART ISSUE A',2,'OWED-LTA-004','','69763','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','OD UNDER SIZE BY -0.02MM','Production running and in between 02nos OD variation coming.This deviation due to insert problem.\r\nInsert wear out and chips clocking in tip and tool holder.Because of this dimensions varies. ','Insert changed and check the OD diameter and continued production. ','1)Insert life calculated and informed to operator to change the insert at standard quantities.\r\n2)Planned to introduce chip braking insert to get insert life more and chips will not clock in\r\nholder. ','CAPA OK','','2018-03-06','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Raghavendra Rao(R)','','','Insert changed take offset run the part dimension ok.','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10483,'51-075','THE BOEING COMPANY','BELLCRANK','F2445-1','252T1271-2','NA','PSDL REV -',1,'486998 MPP','','69714','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Surface mismatch Due to Cutting tool mark','While running the production batch,dia 10 ball nose cutter broken, and causes the dig mark on the part.\r\n\r\nwhile matching the part in fitting, surface mismatch observed and mismatch is out of tolerance.','Checked the stock for dia 10 ball nose. found ok\r\nChecked the cutter flute angle. found ok as per tool drg.\r\nChecked the RPM & feed rate. (Parameter reduced by 5%)\r\n\r\n\r\n\r\n','All the above corrective actions monitoring and found ok for next 2 batches.\r\n','Not observed the like mismatches in next parts.','','2018-03-08','pe_sez(a)','Umesh B,Nataraja C V,Diwakar R.B.,','','0000-00-00','Surface Mismatch','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','yes','With Treatment','','3','no','i700-2','pe_sez(a)','','','for every first part proving time must check the all tool offset in machine. ','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10484,'18-688A','Magellan Aerospace Bournemouth','FORK END INTERMEDIATE ','CD701876/02368A','D575 40494 202','','J',1,'417546','','70617','','0000-00-00',NULL,'yes','no','no','no','no','yes','no','yes','no','Thread go gauge not answer(thread tight) ','Thread GO gauge not answering on treated part|During inspection one part GO gauge fully tightly answered|After passivation that gauge not answering ','|During thread inspection the GO gauge to be answer smoothly not to be tight','|During thread inspection the GO gauge to be answer smoothly not to be tight','CAPA FOUND OK','','2018-03-09','Nandishkumar(D.K.)','Bhuvanesh(P)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','DN37546','POST DN','no','Misc','Bhuvanesh(P)','no','','|The parts which are all in shipping to treatment and under inspection that was ensured ok','E3456','qas|','2018-08-07|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10485,'35-479','Saab AB','SHAFT','B76568','D522 73365 200 00','','A',1,'OWED-LTA-004','','70248','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','OD Undersized by up to 0.15mm','WE ARE GIVEN THE OPTIONAL STOP IN THE PROGRAM FOR REMOVE THE CHIPS, BUT THE OPERATOR DE-CLAMP THE PART AND AGAIN SEE THE PROGRAM AND CLAMP THE SAME PART AGAIN AND RUN THE PART, FOR THAT PART RUN OUT WILL BE OCCURRED AND PART WILL BE 0.2MM OD UNDERSIZED. ','INSTRUCTION GIVEN TO THE OPERATOR FOR CHECK THE EVERY PARTS IN MACHINE BEFORE DE-CLAMPING. AND INSTRUCTION GIVEN ABOUT PROGRAM CODES AND COMMENTS. ','AFTER THE INSTRUCTION HE WILL RUN 15 PARTS AND FOLLOW THE INSTRUCTION PROGRAM CODES AND COMMENTS. ','CAPA OK','','2018-03-10','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','05','no','Misc','Raghavendra Rao(R)','','','COMMENTS ADDED IN THE PROGRAM AND RUN THE PRODUCTION.','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10486,'51-049','THE BOEING COMPANY','BRACKET ','741191','149A7371-9623','NA','PSDL REV A',1,'BOEING 001P','','70385','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','CUTTING TOOL DIG MARK ON THE BASE THICKNESS OF THE PART','Running time tool was broken.','1) Loaded new tool and run the program.','1) Tool life will be monitored.','CA PA found ok.','','2018-03-11','pe_sez(a)','Diwakar R.B.,','','0000-00-00','TOOL DIG MARK','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','1','no','i700-3','pe_sez(a)','no','','checked the spindle and loaded new tool.','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10487,'18-314A','Magellan Aerospace Bournemouth','STUD','504356','D278 50006 206 01','','D',1,'423233','','69485','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Thread effective diameter undersized.\r\n','Thread length under size so taken the part and use the die to do the rework, that time thread effective diameter was under sized. ','After run the part check the thread rotation before unloading the part.','Inform to the operator and comment added in the program about thread rotation and pitch micrometer reading.','CAPA OK','','2018-03-12','Dinakar(K)','SHIVAKUMAR()','','0000-00-00','ENTER THE ROOT CAUSE,CA AND PA.','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','01','no','Misc','Sandhesh D(S)','','','Change the thread length and run the production.    ','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10488,'35-547','Saab AB','LIFT ARM','701946 2C1','D522 73353 200 00','','PART ISSUE A',2,'OWED-LTA-004','','69375','','0000-00-00',NULL,'yes','no','yes','no','yes','no','no','no','no','Wall dig up to 1mm.','Z axis drop 100 mm.','Tool offset taken again.','So related to above subject suggesting from HASS service engineer guide and solve the problems.','CAPA FOUND OK','','2018-03-13','prodn_aero(prodn)','prodn_aero(prodn)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Dinesh kulal()','','','Inform to service engg.','A3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10489,'51A-083','THE BOEING COMPANY','BRACKET ASSY','','332A2930-7','','PSDL REV B',7,'BOEING 001M','','A12747','','0000-00-00',NULL,'yes','no','no','no','no','no','no','yes','yes','There are QTY (22) 332A2930-7 BRKTS ASSY\r\nreceived from vendors with undersized holes. the\r\nflange opposite the bushing s/b per DWG. 332a2930\r\nSHT1 VW b5 .3750\"/ .3756\". The holes are measuring\r\nbetween .3710 and .3725\". Undersized between .004\"\r\nto .0025\". these parts are unusable for\r\ninstallation.','1) OUT OF THESE 22 NO\'S ONLY 7 NO\'S WAS DEVIATED FROM OUR SUPPLY.\r<br/>2) AFTER GOING THROUGH THE 5 WHY ANALYSIS IT WAS FOUND THAT THE MASKING REQUIREMENT DURING PRIMER APPLICATION IN THE CONTROLLED BORE OF DIA .3750\"/ .3756\" WAS NOT MENTIONED IN THE CUSTOMER ISSUED DRAWING.','1) UPON INVESTIGATION ON THE N.C.N. IT WAS FOUND THAT THE CONTROLLED BORE OF DIA .3750\"/ .3756\" HAS TO BE MASKED BEFORE PRIMER APPLICATION, BUT THESE INFORMATION WAS NOT FLOWED DOWN THROUGH CUSTOMER DRAWING.\r<br/>2)AFTER DISCUSSION AND CONFORMATION WITH THE CUSTOMER ON THIS ISSUE IT WAS AGREED THAT THE CONTROLLED BORE OF DIA .3750\"/ .3756\" HAS TO BE MASKED BEFORE PRIMER APPLICATION. THE SAME INFORMATION WAS THEN FLOWED DOWN TO THE TREATMENT SUPPLIER (ATPL).\r<br/>3) THE MASKING REQUIREMENT WAS THEN FLOWED DOWN TO THE TREATMENT HOUSE(ATPL) AND INSTRUCTED THEM TO CARRY OUT THE PROCESS BY MASKING THE CONTROLLED BORE OF DIA .3750\"/ .3756\" BEFORE CARRYING OUT THE PRIMER APPLICATION.\r<br/>4) ALL THE SUPPLY OF PART NO. 332A2930-7 WAS CARRIED OUT WITH MRB NOTIFICATION UNTIL THE CUSTOMER DRAWING IS CHANGED TO INCLUDE THE MASKING REQUIREMENT.','1)PRIOR INTIMATION IS REQUESTED FROM THE CUSTOMER FOR SUCH ISSUES IN FUTURE.','EFFECTIVENESS WILL BE MEASURED IN THE NEXT PRODUCT AUDIT SCHEDULED ON APRIL-2018.','C60821','2018-03-13','qas_sez(a)','qas_sez(a)','CA1224688-00_N1810051087','2018-03-14','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','Assembly','','CUST END','no','Misc','qas_sez(a)','no','','IMMEDIATELY ON THE ISSUE N.C.N. THE COMMUNICATION WAS FLOWED DOWN TO THE TREATMENT SUPPLIER(ATPL) AND CHECKED FOR WIP AND FOUND THAT THE PARTS WHERE SENT FOR TREATMENT AND THE PROCESS WAS NOT STARTED HENCE WE MADE THE TREATMENT HOUSE TO HOLD THE PROCESS UNTIL CONFIRMATION.','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10490,'51-110','THE BOEING COMPANY','RIBPOST FRONT SPAR RIB 12','AJ16','112T2216-5','NA','PSDL REV -',2,'486998 MPP','','68779','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','ALL CONNECTING CURVED SURFACES OR CURVED AND PLANE SURFACES SHOWN.\r\nAS TANGENT NOT BLENDED SMOOTHLY (Refer Attachment).\r\n(Should Be): AS PER PL-112T2216-5, PART SPECIFIC NOTE, ALL CONNECTING CURVED\r\nSURFACES OR CURVED AND PLANE SURFACES SHOWN AS TANGENT MUST BE BLENDED\r\nSMOOTHLY AND MISMATCH MUST NOT EXCEED .005 EXCEPT AS NOTED.\r\n','It was observed that  after treatment there was sharp edge at the area near intersection which was missed during fitting ','Instruction was given to the fitter on the break sharp edges requirement on the shot peening parts','List of shot peening parts and non shot peening parts and there break sharp edges requirements with photo is displayed in the fitting department for better understanding to the fitters','Next batch Production done and parts where checked Visually for break sharp edges found ok','','2018-03-14','qas_sez(a)','Nataraja C V,Kiran KM,Diwakar R.B.,','CA1206676-01_000000576044','2018-01-29','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','yes','With Treatment','DN36474','FI','no','i700-1','qas_sez(a)','no','','The part was moved to quarantine area','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10491,'28-043','Magellan Aerospace New York  Inc.','SHAFT  SUPPORT LEVER SPOI','U6A26/101596','69-38910-2','','PL _A +ADCN # 1,PSDL_N/C',1,'A000148600','','68771','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','OD undersized by 0.012mm.','Improper part butting so running time run-out occurred, so part OD 0.012mm undersized. ','Every part before running the program check the run-out in a MDI mode then run the parts.','Instruction given to the operator about to check the part run-out and jaws boring. ','CAPA OK','','2018-03-14','Dinakar(K)','Ashoka(R)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','011','no','Misc','Sandhesh D(S)','','','Clean the jaws and check the part run-out before run the part.','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10492,'51A-083','THE BOEING COMPANY','BRACKET ASSY','','332A2930-7','','PSDL REV B',5,'BOEING 001M','','A12785','','0000-00-00',NULL,'yes','no','no','no','no','no','no','yes','yes','THERE ARE QTY (5) 332A2930-7 BRKTS ASSY\r\nRECEIVED FROM VENDOR WITH UNDERSIZED HOLES. THE\r\nFLANGE OPPOSITE THE BUSHING S/B PER DWG 332A2930\r\nSHT1 VW B5 .3750\"/ .3756\". THE HOLES ARE MEASURING\r\nBETWEEN .3710 AND .3725\". UNDERSIZED BETWEEN .004\" TO .0025\". THESE PARTS ARE UNUSABLE FOR INSTALLATION.','1) AFTER GOING THROUGH THE 5 WHY ANALYSIS IT WAS FOUND THAT THE MASKING REQUIREMENT DURING PRIMER APPLICATION IN THE CONTROLLED BORE OF DIA .3750\"/ .3756\" WAS NOT MENTIONED IN THE CUSTOMER ISSUED DRAWING.','1) UPON INVESTIGATION ON THE N.C.N. IT WAS FOUND THAT THE CONTROLLED BORE OF DIA .3750\"/ .3756\" HAS TO BE MASKED BEFORE PRIMER APPLICATION, BUT THESE INFORMATION WAS NOT FLOWED DOWN THROUGH CUSTOMER DRAWING.\r<br/>2)AFTER DISCUSSION AND CONFORMATION WITH THE CUSTOMER ON THIS ISSUE IT WAS AGREED THAT THE CONTROLLED BORE OF DIA .3750\"/ .3756\" HAS TO BE MASKED BEFORE PRIMER APPLICATION. THE SAME INFORMATION WAS THEN FLOWED DOWN TO THE TREATMENT SUPPLIER (ATPL).\r<br/>3) THE MASKING REQUIREMENT WAS THEN FLOWED DOWN TO THE TREATMENT HOUSE(ATPL) AND INSTRUCTED THEM TO CARRY OUT THE PROCESS BY MASKING THE CONTROLLED BORE OF DIA .3750\"/ .3756\" BEFORE CARRYING OUT THE PRIMER APPLICATION.\r<br/>4) ALL THE SUPPLY OF PART NO. 332A2930-7 WAS CARRIED OUT WITH MRB NOTIFICATION UNTIL THE CUSTOMER DRAWING IS CHANGED TO INCLUDE THE MASKING REQUIREMENT.\r<br/>','1)PRIOR INTIMATION IS REQUESTED FROM THE CUSTOMER FOR SUCH ISSUES IN FUTURE.','EFFECTIVENESS WILL BE MEASURED IN THE NEXT PRODUCT AUDIT SCHEDULED ON APRIL-2018.','C61061','2018-03-14','qas_sez(a)','qas_sez(a)','CA1227879-00_N1810051116','2018-01-29','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','Assembly','','CUST END','no','Misc','qas_sez(a)','no','','IMMEDIATELY ON THE ISSUE N.C.N. THE COMMUNICATION WAS FLOWED DOWN TO THE TREATMENT SUPPLIER(ATPL) AND CHECKED FOR WIP AND FOUND THAT THE PARTS WHERE SENT FOR TREATMENT AND THE PROCESS WAS NOT STARTED HENCE WE MADE THE TREATMENT HOUSE TO HOLD THE PROCESS UNTIL CONFIRMATION.','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10493,'51A-086','THE BOEING COMPANY','KICK LINK ASSY','','251W3122-3','','PSDL REV -',3,'BOEING 001M','','A13546','','0000-00-00',NULL,'no','no','no','no','yes','no','yes','no','yes','Machining mismatch measuring between 0.0014 -\r\n0.0049 inch (see attachment 1) that has not been\r\nblended out. Considering tactile detection,\r\nmachining mismatch on the parts doesn\'t meet root\r\nradius to mismatch height requirements.','1) THE TOOL PATH GENERATED WAS NOT SUFFICE TO COVER THE MISMATCH. HOWEVER THE STEP OVER WAS BLENDED IN THE FITTING SECTION BY DE-BURRING OPERATION.','1) THE NC PROGRAM WAS REVISED TO EXTEND THE STEP OVER AND THE REVISION DETAILS WHERE UPDATED TO THE MANUFACTURING PROCESS SHEET(MPS).\r<br/>2) DELTA-FAI WAS DONE TO PROVE THE PROGRAM AND FOUND THAT THE PARTS ARE MANUFACTURED WITHOUT MISMATCH.','1) EVERY PROGRAMS GENERATED WILL BE SIMULATED TO ENSURE THE TOOL PATH AND MISMATCHES BEFORE FORWARDING TO PRODUCTION.\r<br/>2) ALL THE ENGINEER\'S ARE INSTRUCTED TO MAKE NECESSARY CHANGES IN THE PROGRAM TO PREVENT MISMATCHES AT THE FAIR STAGE ITSELF.','EFFECTIVENESS WILL BE MEASURED IN THE NEXT PRODUCT AUDIT WHICH IS SCHEDULED ON APRIL-2018.','C62142','2018-03-14','qas_sez(a)','qas_sez(a)','CA1246790-00_N1610102653','2018-02-22','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUST END','yes','Misc','qas_sez(a)','','','ALL THE IN-HOUSE PARTS ARE CHECKED FOR THE MISMATCH AND FOUND POSITIVE.','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10494,'51A-086','THE BOEING COMPANY','KICK LINK ASSY','','251W3122-3','','PSDL REV -',2,'BOEING 001M','','A13547','','0000-00-00',NULL,'no','no','no','no','yes','no','yes','no','yes','Machining mismatch measuring between 0.0014 -\r\n0.0049 inch (see attachment 1) that has not been\r\nblended out. Considering tactile detection,\r\nmachining mismatch on the parts doesn\'t meet root\r\nradius to mismatch height requirements.','THE TOOL PATH GENERATED WAS NOT SUFFICE TO COVER THE MISMATCH. HOWEVER, THE STEP OVER WAS BLENDED IN THE FITTING SECTION BY DE-BURRING OPERATION.','1) THE NC PROGRAM WAS REVISED TO EXTEND THE STEP OVER AND THE REVISION DETAILS WHERE UPDATED TO THE MANUFACTURING PROCESS SHEET(MPS).\r<br/>2) DELTA-FAI WAS DONE TO PROVE THE PROGRAM AND FOUND THAT THE PARTS ARE MANUFACTURED WITHOUT MISMATCH.\r<br/>','1) EVERY PROGRAMS GENERATED WILL BE SIMULATED TO ENSURE THE TOOL PATH AND MISMATCHES BEFORE FORWARDING TO PRODUCTION.\r<br/>2) ALL THE ENGINEER\'S ARE INSTRUCTED TO MAKE NECESSARY CHANGES IN THE PROGRAM TO PREVENT MISMATCHES AT THE FAIR STAGE ITSELF.\r<br/>','EFFECTIVENESS WILL BE MEASURED IN THE NEXT PRODUCT AUDIT WHICH IS SCHEDULED ON APRIL-2018.','C62143','2018-03-14','qas_sez(a)','qas_sez(a)','CA1246811-00_N1610102652','2018-02-22','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUST END','yes','Misc','qas_sez(a)','','','ALL THE IN-HOUSE PARTS ARE CHECKED FOR THE MISMATCH AND FOUND POSITIVE.','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10495,'51A-086','THE BOEING COMPANY','KICK LINK ASSY','','251W3122-3','','PSDL REV -',1,'BOEING 001M','','A13548','','0000-00-00',NULL,'no','no','no','no','yes','no','yes','no','yes','Machining mismatch measuring between 0.0014 -\r\n0.0049 inch (see attachment 1) that has not been\r\nblended out. Considering tactile detection,\r\nmachining mismatch on the parts doesn\'t meet root\r\nradius to mismatch height requirements.','Machining mismatch measuring between 0.0014 -\r<br/>0.0049 inch (see attachment 1) that has not been\r<br/>blended out. Considering tactile detection,\r<br/>machining mismatch on the parts doesn\'t meet root\r<br/>radius to mismatch height requirements.','Machining(CNC) program was changed to remove the step.','Machining(CNC) program was changed to remove the step.','CA/PA found acceptable.','C62143','2018-03-14','qas_sez(a)','qas_sez(a)','CA1246811-00_N1610102652','2018-02-22','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUST END','yes','Misc','qas_sez(a)','no','','Check the part with the above issue in WIP,at supplier site and FG and rework work order was raised for step observed quantities and fitting work done.','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10496,'35-580','Saab AB','LEVER','LL0109408','D5227346720400','NA','PART ISSUE B',10,'OWED-LTA-003','','69209','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','yes','PART NO: D5227346720500 OF WORK ORDER NO 69209(10) & 69210910) IS INTERCHANGED WITH THE PART NO: D5227346720400 OF WORK ORDER NO 69214(18).','Interchange of parts due to lack of proper identification and traceability.','1) Indeividual parts will be identified wih Bag and lable by the Quality Inspector after the completion of receiving inspection.\r<br/>2) All the parts will be moved to the FG Stores in separate bin\'s after the completion of receiving inspection.','An authorized person from the FG stores will verify the parts with respect to the Release COC and the Bag and lable before carrying out the packing and will sign and stamp the Packlist before dispatch. This will be effective from June 18, 2018.','NC Accepted by customer and next batches found ok.','C62441','2018-03-14','qas_sez(a)','qas_sez(a)','OF-002855','2018-03-09','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','yes','With Treatment','DN37948','CUST END','no','Misc','qas_sez(a)','','','All the Parts in FG are inspected and the interchanged parts are identified with the correct label.','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10497,'35-577','Saab AB','SHAFT','B76568','D5227344120000','NA','PART ISSUE A',36,'OWED-LTA-004','','68570','','0000-00-00',NULL,'no','no','no','no','no','no','yes','yes','yes','Corrosion observed on the part.','All the parts were found ok during the final inspection as there where no suspect of corrosion symptoms on the part after the receipt of part from sub-supplier.|','1) All the Quality inspectors inspecting the parts after secondary process are instructed to carry out Final inspection (FI) under the dedicated tables with proper light source.\r<br/>2) Supplier NC is raised for the corrosion symptoms observed on parts during the inspection and forwarded the Non Conformance Report to the supplier.|','1) All the Parts undergone passivation will be inspected under 20X magnifying lens to ensure no symptoms of corrosion on parts.\r<br/>2) All the inspectors involved in receiving inspection are instructed to wear clean and dry hand gloves to inspect the parts that have under gone passivation process in order to avoid possibilities of contamination.\r<br/>3) Supplier has implemented extra water cleaning (DIP and spray rinse) method instead of water spray rinse method to prevent corrosion due to residuals refer attached supplier response NCR-221.|','Next batches found OK.','C61781','2018-03-14','qas_sez(a)','qas_sez(a)','OF-002890','2018-03-14','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','yes','With Treatment','DN37027','CUST END','no','Misc','qas_sez(a)','no','','All the Parts in FG and inspection are inspected for the suspect of corrosion and the suspected parts are sent back to the supplier for reprocessing.|','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10498,'18-295A','Magellan Aerospace Bournemouth','BOLT','CD700163/06279A','PID577 56145 200','','A',1,'423258','','67091','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','ID 12mm dent mark was observed. ','Running time drill was broken, so dent mark occurred in the part ID. ','If running time noise observed or drill edge change in to a black colour that case we change the drill and run the production.','Inform to the operator to If running time noise observed or drill edge change in to a black colour that case change the drill and run the production.','CAPA OK','','2018-03-14','Dinakar(K)','SHIVAKUMAR ,Chandrashekara V K,','','0000-00-00','ENTER THE ROOT CAUSE CA AND PA.','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','1','no','ST20Y1','Sandhesh D(S)','','','Change the drill and new offset taken and run the part.','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10499,'35-254','Saab AB','DRAIN CONNECTOR','789426A4','425Z0640-2','','--C',1,'Forecast po for B787','','70023','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Running time Tool broken , ','Tool broken, while running in wall finishing program  ','check the wall stock and change the RPM and feed rate for particular program .','program backup taken and waiting for next batch production .','CAPA FOUND OK','','2018-03-15','Shivashankar(H.G.)','SIDDESH ,MANJE GOWDA S,KIRAN  M V,DILIP G C ,','','0000-00-00','Tool broken so part rejected ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','3','no','MakinoF3-1','Shivashankar(H.G.)','no','','stop the machine and check the part and informed to supervisor,','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10500,'51A-072','THE BOEING COMPANY','BEARING ASSY','','113T1204-1','','NIL',1,'BOEING 001S','','A13646','','0000-00-00',NULL,'no','no','no','yes','no','no','no','yes','yes','Parts have been manufactured using stock 3.0 x 1.2\r\nx 1.00 CRES 15-5 PH Plate per BMS7-240.\r\n\r\nAs per part list requirement ST shall be 0.70inches.','Thickness of the raw material was taken 1.00inch instead of 0.70 inches.','Per the Everett models substitution drawing, 012W6100, Sheet 1, Section 4.2.c.1.b, this practice is allowed.','Per the Everett models substitution drawing, 012W6100, Sheet 1, Section 4.2.c.1.b, this practice is allowed.','CA/PA acceptable.','C62338','2018-03-15','qas_sez(a)','qas_sez(a)','CA1252649-00_N1610102747','2018-03-01','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','Assembly','','CUST END','no','Misc','qas_sez(a)','no','','Per the Everett models substitution drawing, 012W6100, Sheet 1, Section 4.2.c.1.b, this practice is allowed.','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10501,'51A-072','THE BOEING COMPANY','BEARING ASSY','','113T1204-1','','NIL',15,'BOEING 001S','','A13647','','0000-00-00',NULL,'no','no','no','yes','no','no','no','yes','yes','Parts have been manufactured using stock 3.0 x 1.2\r\nx 1.00 CRES 15-5 PH Plate per BMS7-240.','Refer NCR NO 10500','Refer NCR NO 10500','Refer NCR NO 10500','Refer NCR NO 10500','C62338','2018-03-15','qas_sez(a)','qas_sez(a)','CA1252649-00_N1610102747','2018-03-01','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','Assembly','','CUST END','no','Misc','qas_sez(a)','no','','Refer NCR NO 10500','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10502,'51-005','THE BOEING COMPANY','Upper Beam AFT Splice','772513','315Z1303-501','','NIL',9,'BOEING 001J','','68035','','0000-00-00',NULL,'yes','no','no','no','yes','no','no','no','yes','Oversize of the pilot hole has observed in the part\r\nwhich is having deviation from (0.0001 to 0.0006)\r\ninches.','WHILE DOING THE CMM PROGRAMMING THE TOLERANCE OF THE HOLE WAS NOT DEFINED AS PER THE DRG REQUIREMENT.BY DEFAULT THE OPEN TOLERANCE HAS BEEN SELECTED IN THE PROGRAM WHICH IS.0039\'.','MRB was raised and submitted to the customer for review, acceptance and disposition','CMM programm was validated as per the drawing and the correct tolerance was given the programm.','MRB Disposition received from the customer parts were accepcted.','C61980','2018-03-15','qas_sez(a)','qas_sez(a)','CA1236153-00_N6400022938','2018-03-14','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','With Treatment','DN36686','CUST END','no','Misc','qas_sez(a)','no','','1.All the parts was checked as per the drawing requirement and found that hole is oversize in all the parts\r\n2.Parts were moved to the Qurantine area until for customer approval\r\n','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10503,'30-017A','Gardner Aerospace-Derby Limited','FRAME OUT BD RIB IFS - LH','5865801 6-10','L575 51896 200','7010 T7651 ABM3-1029','A00, ECN:PG60621001JA01Routing sheets page 1 & 2',1,'LPR0000629','','44088','','0000-00-00',NULL,'no','no','yes','no','no','no','yes','yes','no','Semi -Finished part of qty-1 No belonging to CRN 30-017A of Work Order No-44088 was found in the production floor unfinished till 2018 ','Order for parts on work order no 44088 was stopped by Customer. ','Verified that there are no components with deviations are available on the shop floor.','Retraining is scheduled for the production supervisors Components have been scrapped as the company in UK has closed down\r\n','CA PA Effectiveness will be measured during the next Internal Quality Audit.','','2018-03-16','Narayanappa(G)','Narayanappa(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','1','no','Misc','Narayanappa(G)','','','1)NC is raised in the ERP and the Part is marked as rejected due to no customer demand.\r\n2)The part is moved to the Rejection area and disposition is requested from the QA department.\r\n','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10504,'51-131','THE BOEING COMPANY','CLIP','8-22-04977/24123','476Z2912-15','NA','NIL',1,'BOEING 001N','','69800','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','no','mismatch on the part surface. ','Due to the tool wear this mismatched was not meeting the drawing requirement.','Instructed the operator to check for every production run part ensure all the required tools are not damaged. ','Instructed the operator to check for every production run part ensure all the required tools are not damaged. ','Next run parts found with zero mismatch and all are within acceptable limit. ','','2018-03-16','pe_sez(a)','pe_sez(a)','','0000-00-00','TOOL MISMATCH/STEP OVER ON SURFAC.','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','DN37508','customer end','no','Misc','qas_sez(a)','yes','','Checked all parts available in WIP and ensure that no above issue for the remaining produced quantities. ','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10505,'18-436A','Magellan Aerospace(Blackpool) Limited','MANIFOLD','6278','PI201274624','','NIL',1,'BPP-529619 amed-1','','71989','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Tool dig mark.','Operator not holding on required length, so tool holder rub in part. ','change the tool length and run the program.','Operator fair or production running time see the tool length in program inside and data sheet.','Part Accepted and NC closed.','','2018-03-19','Rangaswamy()','Rangaswamy()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','Manufacture Only','','05','no','Misc','Rangaswamy()','','','Stop the fair part and inform to supervisor.','E3456','qas|','2018-07-10|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10506,'18-694A','Magellan Aerospace Bournemouth','HOUSING OUT BD BRG 3','1573705-1/QD84','D275 40011 200','','D01',1,'417546','','71090','','0000-00-00',NULL,'yes','yes','yes','','','','','','','PART DIG MARK FOUND.','PART IS LOAD ON FIXTURE NOT PROPERLY,','LOADING AND UN LOADING THE PART TRAINING GIVEN TO NEW OPERATOR   AS PER MPS, INFRONT OF MACHINE.','ESPECIALLY, NEW OPERATORS TRAINING CONDUCTED ON EVERY END OF THE WEEK FOR PART LOADING,UNLOADING AND ETC....  ','Effectiveness will be measured in the next batch after the training.','','2018-03-20','Dhananjaya(N)','        dharshan d','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','13','','','','','','STOP THE MACHINE.','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10507,'18A-107','Magellan Aerospace Wrexham','LINK BODY ASSY','','D574 50553 000','','A',1,'165478','','A13010','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Part Failed in torque test. Measured torque is in negative side(Too loose to measure).','During torque test part rejection was ensured|During assembly Lactite overflow occurred inside|Due to that bearing shifted in negative side during torque test','|Lactite application to do as per the Process Sheet','|Lactite application to do as per the Process Sheet','CAPA FOUND OK','','2018-03-21','Nagaraju(T)','Phaniraj(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Assembly','','FI','no','Misc','Bhuvanesh(P)','no','','|The remaining parts in WIP is ensured for lactite application ensured ok','E3456','qas|','2018-08-07|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10508,'51-003','THE BOEING COMPANY','LWR BEAM FWD INBD SPLICE','790731A4','315Z1302-501','','NIL',3,'BOEING 001K','','70855','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Base Thickness under size','Running time part bend.','Additional clamping provided to avoid part bend.','Additional clamping method is included in the MPS.','CA PA Found OK.','','2018-03-21','pe_sez(a)','op_sez(s)','','0000-00-00','Part Pend','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','1','no','Misc','pe_sez(a)','no','','checked all the parts.','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10509,'35-404','Saab AB','BEAM 2','721607 1D1','D522 73392 200 01','','A',2,'OWED-LTA-001','','69770','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Part got Dig mark on the wall.','WRONG PROGRAM CALL AND RUN IN DNC MODE|The NC program loaded second time and the cycle restarted automatically and the part got dig marked on the wall during the cutout stage.','|Informed all the supervisors to re-check the program before stating the production.','|Informed the Mazak Maintenance team to address this issue in the next preventive maintenance.','CA PA found effective. Mazak team visited the plant and resolved the issue and the problem was not repeated.','','2018-03-22','pe_sez(a)','Umesh B,Nataraja C V,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','5','no','i700-2','pe_sez(a)','no','','|Stopped the machine immediately and deleted the previously copied files and reloaded the correct program once again and continued the production.','Z3456','qas|qas|','2018-07-27|2018-07-27|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10510,'35-192','Saab AB','SUPPORT-FTG','9386187','423Z1202-14','','---',1,'Forecast po for B787','','71396','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Bore over size 0.025.','CRC correction error done by operator.','Guide the operator about CRC correction.','Guide the operator about CRC correction for bore.','CAPA FOUND OK','','2018-03-22','prodn_aero(prodn)','Anil(kumar)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','05','no','Misc','Dinesh kulal()','','','Correct the CRC value and run the production.','A3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10511,'35-141A','Saab AB','BCD_HINGE_SUPPORT_FITTING','722293','424Z3111-4','','--B',1,'Forecast po for B787','','71624','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Total height -1mm.','wrong prediction of Z axis over travel of machine','Fixed the z value for rotary table machine.','Fixed the z value for rotary table machine.','CAPA FOUND OK','','2018-03-22','prodn_aero(prodn)','Anil(kumar)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Dinesh kulal()','','','Correct the value of z.','A3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10512,'35A-601','Saab AB','FRAME ASSY','','D5227338501000','','PART ISSUE C',1,'OWED-LTA-001','','A12537','','0000-00-00',NULL,'no','no','no','no','no','no','yes','yes','yes','Electrical bonding between point A and point F is measured 19,93m&#8486;. See SH02 Zone L04 Anchor Nut Detail G ','Initially the parts were shipped using the DR for electrical bonding. Later as a trial requested by SAAB it was assembled with sealant which resulted in non conformity of bonding due to resistivity of the sealant.','|Discussed with the SAAB team on how the assembly needs to be made and revised the assembly procedure.','|Delta FAI for the revised procedure has to be submitted to customer.','Delta FAI done and part accepted at customer end.','C60424','2018-03-22','qas_sez(a)','qas_sez(a)','OF-002905','2018-03-14','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','yes','Assembly','','CUST END','no','Misc','qas_sez(a)','no','','|Immediately informed the assembly team to stop assembling the parts until further confirmation on process.','Z3456','qas|','2018-08-07|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10513,'18-189A','Magellan Aerospace Bournemouth','BUSH HINGE BRKT FWD','L07584','L575 52328 200','BS 23','A00',1,'415456','','60216','','0000-00-00',NULL,'yes','no','no','no','no','yes','no','yes','no','External diameter undersized by 0.010 to 0.020mm','Part OD got oversize after treatment that was ensured|Untreated condition that was not ensured|The untreated parts were check by trainees due that manual error occurred','|The training given to the trainees','|Training record to be created','CAPA FOUND OK','','2018-03-23','Nandishkumar(D.K.)','Bhuvanesh(P)','','0000-00-00','External diameter undersized by 0.010 to 0.020mm','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','DN34636','POST TREATMENT','no','Misc','Bhuvanesh(P)','no','','|The remaining parts in Inspection and ready to treatment are ensure found ok','E3456','qas|','2018-08-07|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10514,'35-588','Saab AB','LOCK SECTOR','701946 1D1','D5227349920200','NA','PART ISSUE C',1,'OWED-LTA-003','','71676','','0000-00-00',NULL,'yes','yes','yes','','','no','','','no','fixture wrong loading so part rejected..','fixture wrong loading so part rejected.','FIXTURE M6 BOLTING IN BOTTOM FACE AND ENSURE THE FRONT MARKING .','FIXTURE M6 BOLTING IN BOTTOM FACE AND ENSURE THE FRONT MARKING ','CA/PA Acceptable.','','2018-03-23','pe_sez(a)','                Diwakar R.B.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','3','','','','','','FIXTURE M6 BOLTING IN BOTTOM FACE..','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10515,'35-142A','Saab AB','BCD_HINGE_SUPPORT_FITTING','72306/02/00','424Z3111-5','','--B',1,'1600218100','','71630','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Side wall thickness minus 1mm.','Incorrect clamping done by operator.\r\n','Give the multi message on that program.','Give the M0 & message on that program.','CAPA FOUND OK','','2018-03-24','prodn_aero(prodn)','Manjunatha.S.T(M)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Manjunatha.S.T(M)','','','Correct the clamping and run the production.','A3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10516,'51-001','THE BOEING COMPANY','Upper Beam FWD Splice','789431A4','315Z1301-501','','NIL',1,'BOEING 001K','','70557','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Un Wanted Machining due to Post Processor Wrong Selection','Post processor wrong selection','|As per the analysis selected corrected post processor and generated new program.|As per the analysis selected corrected post processor and generated new program.','|senior person is nominated to review the programs before running on machine.|senior person is nominated to review the programs before running on machine.','Root Cause not addressed properly and the information is not flowed down to the concern personnel by the person who raised the NC. Moreover the work order is closed without director approval. This Nc is closed for releasing the work orders and the effectiveness will be measured during the next production.','','2018-03-24','pe_sez(a)','nagaraju(sez)','','0000-00-00','post processor error','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','3','no','Misc','pe_sez(a)','no','','|Done brainstorming with engineering team to analyze the problem and found the cause for problem \r\n|Done brainstorming with engineering team to analyze the problem and found the cause for problem \r\n','Z3456','||cam|qas|','2018-07-06|2018-07-06|2018-07-06|2018-07-06|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10517,'35-407','Saab AB','BEAM 3','521026B2','D522 73396 200 00','','A',1,'OWED-LTA-001','','71290','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Mirror Part also Added in the Billet when Designing by the Engineer  ','','','','','','2018-03-24','pe_sez(a)','op_sez(s)','','0000-00-00','Mirror Part Also Run','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','yes','With Treatment','','3','no','Misc','pe_sez(a)','no','','','Z3456','qas_sez|','2018-08-06|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10518,'35-588','Saab AB','LOCK SECTOR','704718','D5227349920200','NA','PART ISSUE C',1,'OWED-LTA-003','','71677','','0000-00-00',NULL,'yes','yes','yes','','','no','','','no','Tool dig into the part','During roughing m6 bolt broke,\r<br/>hence Part rotated,\r<br/>\r<br/>Root cause being - tap depth in the previous operation found less','Bolt length Increased,\r<br/>Operator to check proper tightening of bolts','Bolt length Increased,\r<br/>Operator to check proper tightening of bolts','CA/PA found satisfactory and next part within the acceptable limit.','','2018-03-25','pe_sez(a)','        Nataraja C V','','0000-00-00','BOLT BROKEN DIG MARK ON THE PART','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','3','','','','','','changing the bolt and run','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10519,'35-525','Saab AB','ROD BODY','M973530','D522 73336 200 00','','A',1,'OWED-LTA-004','','70295','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Running time part rotated and dig mark formed on part. ','Outside diameter is maintained between 11.9 to 12.2 in turning  operation and hence 11.9 diameter maintained parts not holds properly in milling fixture of 12mm diameter.So this made the part rotated while milling operation','Information given to turning team to  maintain the diameter constant within 12.0mm+/- 0.05.\r\n','1.After turning operation we will ensure all the parts and run the program .\r\n2.The O.D of 12 mm is added as a Key charectristics in MPS. -It will done before May 30th 2018.','Effectiveness will be verified after adding Key charecteristics for that dimension','','2018-03-27','Gurukiran S(M)','NIRANJAN(N  )','','0000-00-00','Part OD dig mark observed','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','07','no','Misc','Gurukiran S(M)','','','stop the machine and check the all parts and run the program','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10520,'47-128','GKN Aerospace Filton','HINGE POST NO. 4','9753201','F5755106220203','NA','PART ISSUE D',1,'1210041296','','70792','','0000-00-00',NULL,'yes','yes','yes','','','','','','','In manually editing Drilling program co ordinates wrong.','manually editing in program','Take program from programmer and then run program part is ok. ','don\'t edit the program in manual.','1) Supervisors needed training on Configuration control and control of changes.\r\n2) Effectiveness will be measured after the completion of training during the process audit.','','2018-03-27','Dhananjaya(N)','        Mallikarjuna D','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','3','','','','','','stop the machine, immediate inform to programmer and take a new correct program.','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10521,'47-113','GKN Aerospace Filton','BRACKET','6358201','D57952066200','NA','PART ISSUE A',1,'1210041296','','70776','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','DIA. 6mm BALL NOSE CUTTING TOOL BROKEN AND DIG MARK IDENTIFICATION IN PART. ','Tool was overhanging and as the length of the tool was less than the requirement.','|Informed all the operator to select the proper tool length and holder to avoid overhanging of the tool.','|Tool presetter is used for all the tools offset.','CA PA Found ok.','','2018-03-28','pe_sez(a)','op_sez(s)','','0000-00-00','DIG MARK','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','3','no','Misc','pe_sez(a)','no','','|Changed the correct tool and continued the production.','Z3456','qas|qas|','2018-07-27|2018-07-27|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10522,'47-119','GKN Aerospace Filton','TOP SPREADER PLT M/C','6358201','F57451570200','NA','PART ISSUE B',2,'1210041296','','70786','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','part thickness under sized by 1mm.','Program was edited to reduce the cycle but the edited program was not validated before running the program in machine because of which stock was present in one face later when butting the same face thickness got undersized.','1) Dumped the edited program in the obsolete folder and received the validated program from the engineering department and loaded to the machine.\r\n2) Instructed all the supervisors to make a note on getting the program validated before loading the same to the machine.','1) Training program is scheduled for the supervisors on control of changes.\r\n2) Instructed all the supervisors to not to load the program to machine without proper validation.','CA PA found OK since it is a repeated NC Effectiveness will be measured during the next process audit.','','2018-03-29','Subramanya L(Naik)','Dhananjaya N,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','3','no','VM2-3','Subramanya L(Naik)','','','Stop the machine ,Immediate inform to programmer and take a new correct program.','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10523,'35A-491','Saab AB','LINK Assy','','D522 73527 000 00','','A',1,'OWED-LTA-004','','A13068','','0000-00-00',NULL,'yes','no','no','no','no','no','no','yes','yes','IS CONDITION: Bearing, Plain MS14101-3K need too big breakaway torque. Ranging to up to 2 IN-LB. FAI states “Conforms”. Full re-inspection of Saab stock required. CIM to quarantine current lots in work, until method to ensure breakaway-torque is verified and guaranteed. Delta FAI on form 3 character 18 and 30. \r\nSHOULD BE: No-load rotational breakaway torque IN-LB “K” Type 0-0.5 IN-LB. Force and breakaway load measured and verified if not statistically proofed to be in no need of measurement.\r\n','Miss-interpretation of standard requirements.','1) Stacking process of all the WIP was carried out in such a way to achieve the torque specified as per the standard requirement.','1) APS is amended to capture the torque requirement as per the standard.\r<br/>2) Delta FAIR will be produced and submitted to customer during the next shipment capturing the torque values required as per the spec and the value measured on the part.\r<br/>3) Training program is scheduled for both the QAD personnel involved in FAIR documentation and for the Engineering department personnel, subjected on how to interpret and understand the drawing requirements.','Customer verified the NC on Site and closed the NC.','C62438','2018-03-29','qas_sez(a)','qas_sez(a)','OF-002919','2018-03-28','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','yes','Assembly','','CUST END','no','Misc','qas_sez(a)','','','All the in-house parts are quarantined and re-inspected.','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10524,'35-570','Saab AB','RUBBING PLATE','WO-A-007961','F575 54807 203 01','','SCH-ISSUE E, PART ISSUE E',1,'A330 NEO FORECAST -3','','72085','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Wrong fixture loading .','while part proving the wrong fixture name shown on MPS.','change the fixture name and load the MPS details on cim soft,','while fair proving time to ensure the fixture name correctly .And engraving the name 100%. ','CA PA Found Ok.','','2018-03-29','Shivashankar(H.G.)','DILIP G C()','','0000-00-00','Part thickness minus side ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Shivashankar(H.G.)','no','','Stop the m/c and informed to engineering department ','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10525,'35-631','Saab AB','SUPPORT SEAL RETAINER ','203993B1','423Z1834-2-03','NA','---',1,'Forecast po for B787','','70029','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','part wall negative side -0.5mm','part not holding properly ,','Check the bolt length and give the training for operator .','On this particular CRN bolts and program depth will adjusted .','Next Batch Found ok.','','2018-03-29','Shivashankar(H.G.)','MANJE(GOWDA S)','','0000-00-00','part wall dig','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','07','no','Misc','Shivashankar(H.G.)','no','','stop the machine and check the all parts counter depth checking .','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10526,'18-392B','Magellan Aerospace Bournemouth','END COVER','19278','D278 50167 200','','D',1,'423241','','71085','','0000-00-00',NULL,'no','no','no','no','no','yes','yes','yes','no','Dent mark observed top of chamfer and bore','Improper handling at supplier end.','|Reject and debit note raised the supplier','|separate bin are used in supplier end','Next batches found ok.','','2018-03-30','Nandishkumar(D.K.)','Bhuvanesh(P)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','DN38765','post treatment','no','Misc','Bhuvanesh(P)','no','','|Information passed to supplier','E3456','bhuvanesh|','2018-07-31|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10527,'35-158','Saab AB','FLCD_DS_SUPPORT_DEFLECT-S','850303-04','423Z6187-7','','---',1,'Forecast po for B787','','70337','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','wrong work offset entered,','new operator entered wrong offset  ','To give the training for new operator on sez site .','while setting done by new operator, cross verify the offset by senior operator ','CA PA found ok Effectiveness to be measured in the next process audit.','','2018-03-30','pe_sez(a)','Kiran Kumar M,Kiran KM,','','0000-00-00','wrong wpc','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','3','no','PS105-01','op_sez(s)','','','cross check the work offset and correct the offset and run the program .','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10528,'18-694A','Magellan Aerospace Bournemouth','HOUSING OUT BD BRG 3','1573705-1/QD84','D275 40011 200','','D01',1,'417546','','71090','','0000-00-00',NULL,'yes','yes','yes','','','','','','no','Repeated Dummy NC','Repeated Dummy NC','Repeated Dummy NC.','Repeated Dummy NC','Repeated Dummy NC','','2018-04-05','Dhananjaya(N)','        dharshan d','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','13','','','','','','STOP THE MACHINE.','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10529,'47-128','GKN Aerospace Filton','HINGE POST NO. 4','9753201','F5755106220203','NA','PART ISSUE D',1,'1210041296','','70792','','0000-00-00',NULL,'yes','yes','yes','','','','','','no','Repeated Dummy NC','Repeated Dummy NC','Repeated Dummy NC','Repeated Dummy NC','Repeated Dummy NC','','2018-04-05','Dhananjaya(N)','        Mallikarjuna D','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','3','','','','','','stop the machine, immediate inform to programmer and take a new correct program.','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10530,'35-332A','Saab AB','RUBBING PLATE FWD','40763','F575 54805 20101','','D',3,'A330 Neo Forecast 20','','62963','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Corrosion Pits observed ','Due to rubbing of tool or material behavior Corrosion Pits has been observed in Treatment house ','Apply PX-24 after machining, and polishing and rubbing of tool should be avoid. ','Apply of PX-24 is mandatory before sending the parts to treatment house  ','Next parts and batches found okay ','','2018-04-05','qas_sez(a)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','DN32369','On site','no','Misc','qas_sez(a)','','','In formed to operators.  ','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10531,'47-124','GKN Aerospace Filton','LUG AFT M/C','560504A3','F57550116200','NA','PART ISSUE C',1,'1210041296','','70788','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','part loaded in wrong orientation.','part dimension in L*W*H not checked before loading.','1,Before loading the part to the m/c operator is instructed to verify the L/W/T As per process sheet \r\n\r\n2,instructed all the operators to ensure proper loading of the parts before continue the production .','1.Fixture will be done before May 10th and will be used in next batch of production.\r\n2.M00 will be added in the program to state \"before running the part check for proper orientation of part\".\r\n3. fixture detaile will be captured in mps and delta fair will be carriedout  ','Effectiveness will be measured during the next production.','','2018-04-06','Gurukiran S(M)','MANJE(GOWDA S)','','0000-00-00','part rejected','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','01','no','Misc','Gurukiran S(M)','','','Ensure the part dimension L*W* H Write the RM Surface and inform all 3 shift operators .','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10532,'18-296B','Magellan Aerospace Bournemouth','PIN GUIDE ','B000077382','PIL575 52882 200','','B00',2,'423258','','72070','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Total length 0.2mm undersized.','For the work offset 3.0mm moving place 2.5mm moved so total length maintain time center depth was not cleared.  ','For the program top comment added and inform to the operator about the comment.','For the program top comment added and inform to the operator about the comment.\r\nImformed operators to check the center depth of 3.0mm.','Effectiveness found ok','','2018-04-06','Dinakar(K)','Sudhakar(C.M)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','03','no','Misc','Sandhesh D(S)','','','3.00mm moved in the work offset and run the production.','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10533,'51-082','THE BOEING COMPANY','BRACKET DETAIL','659761','332A2930-2','NA','PSDL REV B',1,'BOEING 001M','','71984','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','PART TOP SURFACE NOT MACHINED','Part butting problem in first setup.No stock for second setup','Parts are properly butting done.Verified by the feeler Gauge.\r<br/>|','operators are requested to verify the butting by double cross check before cycle start. |','CA/PA Accepted','','2018-04-07','pe_sez(a)','pe_sez(a)','','0000-00-00','PART TOP SURFACE NOT MACHINED','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','1','no','Misc','pe_sez(a)','no','','Production stopped. 1st setup all parts are checked.|','Z3456','qas_sez|','2018-07-03|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10534,'35-602','Saab AB','SHAFT 1','C90570','D5227280720000','NA','PART ISSUE A',1,'OWED-LTA-004','','69754','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Corrosion Pits observed ','Due to rubbing of tool or material behavior Corrosion Pits has been observed in Treatment house ','Apply PX-24 after machining, and polishing and rubbing of tool should be avoid','Apply of PX-24 is mandatory before sending the parts to treatment house ','Next parts and batches found okay ','','2018-04-07','qas_sez(a)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','DN38168','POST DN','no','Misc','qas_sez(a)','','','In formed to operators. ','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10535,'18-679A','Magellan Aerospace Bournemouth','BUSH','CD700162/05878A','D278 50165 200','','A',1,'417546','','71424','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','no','Outer Diameter 9.452/9.467 measures 9.607/9.610 in o1no, out of 48 nos.','1)After the insert change the operator removed the part from the machine with-out measuring the part dimension, after identifying the oversize in the part the operator separated the part from the good ones without identifying with proper identification tag. Due to the lack of communication during the shift change the deviated part got mixed up with the good ones.</br>2)During the Final Inspection (FI) operation the quality inspector inspecting the part missed to ensure the proper dimension as the total batch quantity was 2,500 no\'s and the entire batch was inspected by a single quality inspector using the micrometer because the air gauge set was sent for calibration.','1) Operators are instructed to identify the deviated parts with proper identification tape and separate it from the correct parts.<br/> 2) The part dimension will be ensured inside the machine itself to avoid mix-up and to carry out the rework immediately if any deviation is found. <br/>3) All the quality Inspectors are instructed to get an additional support for checking the parts with controlled features if the batch qty is more than 500 no\'s.','1) Training is conducted to all the turning operators on Pre and Post setting requirements to be ensured before continuing the production.<br/>2) Pre and Post setting check list is introduced to all the turning centers to ensure no deviation due to setting change.<br/>3) Additional set of air gauge is ordered to use as an alternate to each other during the time of calibration.','Next batches found ok.','','2018-04-08','Bhuvanesh(P)','Narasimha Murthy(R)','RDN 00216','2018-04-09','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','CUST END','no','Misc','Nandishkumar(D.K.)','yes','','Checked all the parts in WIP and Stock to ensure similar deviation and found all parts to be good.','E3456','qas|','2018-09-18|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10536,'18-106A','Magellan Aerospace Bournemouth','EYE END INBOARD','05029B','PID575 41542 200','','D',1,'423256','','72094','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Thread effect dia under size by 0.3mm.','DUMMY NC ','DUMMY NC ','DUMMY NC ','DUMMY NC','','2018-04-09','Dinakar(K)','Seetharamu D,Ravi R,Mallikarjuna D,Kammar Nagaraj,Dinakar K,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','FI','no','DX 200-3','Narasimha Murthy(R)','','','DUMMY NC ','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10537,'44-010','Saab AB','FRAME INT 4','172937','E5347562920101','','A',1,'AAI-DP-LTA-15SS','','72249','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Base thickness - side.  (0.15mm)','Second setup ruining time base thickness - side because  part bend, ','1.provide sufficient clamp to butting the part properly .\r\n','1 Instructed operator to ensure the part butting with the help of feeler gauge before run the part.\r\n\r\n2 Instructed to operator before loading job material bend is to be chuck,','cap/a found ok','','2018-04-09','Dhananjaya(N)','Dhananjaya N,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','5','no','VM2-3','Dhananjaya(N)','','','m/c stop and checking the part , ','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10538,'18-106A','Magellan Aerospace Bournemouth','EYE END INBOARD','05029B','PID575 41542 200','','D',2,'423256','','72094','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','sphere diameter undersized.','During the second setup operation the total length became oversize in two numbers. In-order to achieve the total length operator loaded the part again and provided the offset for the required length and ran the program without the knowledge of supervisor this resulted in under size of the sphere.  ','1) Informed the operator about the rework procedure and instructed all the operators to not to perform any rework in the absence of the supervisor.\r\n2) Instruction given to supervisors to perform rework of parts only with the senior operators.','1) Instructed operators to identify and handover the rework parts separately to the concern supervisors.\r\n2) Instruction given to all the supervisors and operators to monitor the offset taken and tool correction periodically.','EFFECTIVENESS FOUND OK','','2018-04-09','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','05','no','Misc','Ravi(M)','','','Immediately changed the offset and checked all the parts machined and found ok.','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10539,'18-106A','Magellan Aerospace Bournemouth','EYE END INBOARD','05029B','PID575 41542 200','','D',1,'423256','','72094','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Thread effect dia under size by 0.3mm.','Due to while thread running time thread insert brokened and broken insert is taking over cut and therad major dia will be undersize so thread NOGO answered. ','Next part thread insert changed and takened tool X-&Z-offset and maintained the thraed offsete effective dia and soot the thread gauge,Gauge is answered and run the part. ','1.Inform to operator every 50 nos will be completed changed the insert and takened tool X-offset&Z-offset and maintained the thraed effective dia and soot the thread gauge,Gauge is\r\nanswered and run the part.\r\n2.Message added in the program to change the Inserts after every 50 no\'s. \r\n3.Informed operators to check thread gauges after every part.','Effectiveness Found OK.','','2018-04-10','Dinakar(K)','Seetharamu D,Ravi R,Mallikarjuna D,Kammar Nagaraj,Dinakar K,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','FI','no','DX 200-3','Narasimha Murthy(R)','','','change the insert re-offset taken and run the part.','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10540,'43-019','Composite Industrie','BRACKET','750288 2B1','V251 11749 200','','A00, ECN PV100298ST1AG07',1,'LTA PO-2','','71207','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','program problem so part profile under size.','program problem from  CAD/CAM.','Program Modified and Executed On machine part found OK ','Double Cross the check by Engineer Before Executing Program on Machine ','Next batch produced found ok.','','2018-04-10','Ramesh(Poojary)','Sundar D.K.,Shivappa M B,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','3','no','BMV 45-1','Subramanya L(Naik)','no','','Program Modified and Executed On machine part found OK ','E3456','qas|','2018-07-10|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10541,'49-001','CIRCOR Aerospace, Inc.','MANIFOLD','8-17-3451','30C00001-817-2','','ECO 25492A',1,'4047910-000 OP','','61133','','0000-00-00',NULL,'yes','no','yes','no','yes','no','no','no','no','Eccentric Bore pitch was shifted.','Eccentric bore pitch problem due to fixture problem.',' fixture to change in all machines for turning process.','Changed fixture in all machine for turning process.','CAPA FOUND OK','','2018-04-11','Dinakar(K)','Raghavendra Rao(R)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Raghavendra Rao(R)','','','Trail part 01 no.\r\nStopped production.','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10542,'18-116B','Magellan Aerospace Bournemouth','ASSEMBLY FORKEND','163118*7433','F575 51377 200','','A',1,'423246','','71260','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Dia 14.288 Bore Over size ','Chips were locked in holder due to that tool to spindle Runout  not achieved. So the Bore over size occurred.','All tools are removed from ATC then ATC all pockets and spindle cleaning doing. At final all tools are loading in ATC. That is doing in every week.','The remaining ATC pockets to be filled with dummy holders.','CAPA FOUND OK','','2018-04-11','Anjinamurthy(H)','        Ravi R','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','5','','','','','','Chips was removed from holder and ensured the tool Runout.','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10543,'35-592','Saab AB','BRACKET','5124801 1','D5227342220200','NA','PART ISSUE B',4,'OWED-LTA-001','','71787','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Base thickness Minus -.40 MM .','Wrong tool wear offset edited by operator.','Guide the operator about tool wear editing.','whenever setting time we are work and tool wear offset cross check and run the programs.','CAPA FOUND OK','','2018-04-11','prodn_aero(prodn)','Lakshmi(Narasimha)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Dinesh kulal()','','','Correct the tool wear offset value and run the production.','A3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10544,'18-386B','Magellan Aerospace Wrexham','NUT RING INNER ','1563816-2/QCD9','D575 40039 200','','B',1,'162895','','72444','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Bore Dia. under-size by -0.3mm.','Bur folded in the Id due to which the under size measured on the part.','1) Removed the bur from the ID and measured the part and found OK.','1) Instructed all the fitting and production operators to remove the bur properly before handing over to the next operation.','CA PA found Ok.','','2018-04-17','Dinakar(K)','Sudhakar C.M,Dinakar K,Ashoka R,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','With Treatment','','FI','no','QT100S-1','Narasimha Murthy(R)','no','','Checked all the completed parts to ensure no bur is folded in the part.','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10545,'18-684A','Magellan Aerospace Bournemouth','FORKEND ASSEMBLY ','1572815-3/QD6H','D572 50462 201','','J01',4,'417546','','70823','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Fork end assembly treated part D57250462200 (LH) API121651- 4 No’s .Each two numbers from this API work order mixed up with two API work order in D57250462201(RH) part.','After the completion of Final Inspection (FI) both the LH and RH parts are kept close to each other and the parts was not identified either by ink marking or bag and label after cad platting.','1) After the completion of FI by quality inspector All the CAD Platting parts will be identified with bag and label before handing over to Finished Goods(FG) if the parts are not marked with ink part marking. <br/> 2) LH and RH parts will not be taken for FI together. Once the LH (or) RH part is completed the parts will be handed over to the FG immediately before taking the RH (or) LH parts for inspection.','1) Comment is included in the Supplier Purchase Order (SPPO) to include part identification by Bag & Label to each parts before shipping to CIM Tools. <br/> 2) checking Jig is introduced to verify the LH & RH parts during the final inspection.','Next batches found ok.','','2018-04-17','Nandishkumar(D.K.)','Bhuvanesh(P)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','With Treatment','DN38060','CUST END','no','Misc','Nandishkumar(D.K.)','','','All the parts in FG was inspected to ensure there is no similar mix-up of parts and found OK.','E3456','qas|','2018-07-31|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10546,'47-103','GKN Aerospace Filton','BRACKET FT4 FWD','W2948','F57550777002','NA','PART ISSUE E',1,'1210038562 Amnd 3','','72095','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','part rejected due to process proving time wrong program given ','Due to NC Program Problem ','Updated NC program and Executed on Machine and Part Found OK ','Before Execution the program on Machine Programmer has to double cross check program. ','CAPA Found ok.','','2018-04-18','Gurukiran S(M)','        Ramesh(Poojary)','','0000-00-00','part total hight under size (1.5mm)','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Gurukiran S(M)','no','','Updated NC program and Executed on Machine and Part Found OK. Obsolete old program and New updated\r\nprogram moved to Program Data Storage ','E3456','qas|','2018-09-05|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10547,'18-382B','Magellan Aerospace Wrexham','SLEEVE BEARING','1466763-2/JEQD','D575 40037 200 PF','','A',1,'RP143022','','71820','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','TOTAL LENGTH UNDER-SIZE 1.5MM','CHECK PRESSURE WAS LOW SO RUNNING TIME PART GOT REMOVED FROM THE JAWS ; TOTAL LENGTH GOT UNDER SIZE. ','INSTRUCTION GIVEN TO THE OPERATOR,BEFORE SETTING CHECK THE PRESSURE OF THE CHUCK AND LATER RUN THE PARTS AND ALSO MENTION IN THE PROGRAM .','INSTRUCTION GIVEN TO THE OPERATOR,BEFORE SETTING CHECK THE PRESSURE OF THE CHUCK AND LATER RUN THE PARTS AND ALSO MENTION IN THE PROGRAM .','Effectiveness found ok.','','2018-04-18','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','03','no','Misc','Raghavendra Rao(R)','','','CHECK PRESSURE DONE HIGH AND PART RUN. LATER PART WAS OK','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10548,'35-169','Saab AB','ALCD_STRUCT_SUPPORT-FTG_L','223359B1','423Z1200-12-01','','---',1,'Forecast po for B787','','72030','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Chamfer oversize up to 2 mm.','Tool was not edited properly','Edited the tool properly according to the tool number.','Check the tool positions and tool number properly.','CAPA FOUND OK','','2018-04-18','prodn_aero(prodn)','Santhosh Kumar.R()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','05','no','Misc','Santhosh Kumar.R()','no','','Edited the tool position','A3456','qas_aero|','2018-07-17|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10549,'18-382B','Magellan Aerospace Wrexham','SLEEVE BEARING','1466763-2/JEQD','D575 40037 200 PF','','A',2,'RP143022','','71819','','0000-00-00',NULL,'yes','no','yes','no','yes','no','no','no','no','Dent mark observed in the part OD','while power was tripped so air pressure down so dig mark occurred in the part OD. ','If any power trip issues stop the machine and wait for the air pressure.','Information given to the operator about power trip issues ','CAPA FOUND OK','','2018-04-18','Dinakar(K)','Dinakar K,Ashoka R,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','11','no','QT100S-1','Sandhesh D(S)','','','Stop the machine and waiting for the air pressure. ','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10550,'18-030A','Magellan Aerospace Bournemouth','PIN','1518553-2/M4LM','D278 50156 200','S130 FHT','A',1,'423233','','66922','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','part missing treatment house,','During treatment process part was getting missed|The treatment parts were tiny in size and large number of quantities |So after treatment process completion the parts accountability was not carried out','|Before treatment process the parts quantity to be ensure correctly and after that also that to be re-verify by using job cards','|After treatment completion parts quantity to be take into accountability','NEXT BATCH FOUND OK','','2018-04-19','Bhuvanesh(P)','Narasimha Murthy(R)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','DN35440','post DN','no','Misc','Bhuvanesh(P)','no','','|The parts which were all in treatment process that accountability was taken and ensured full quantity','E3456','nandishkumardk|nandishkumardk|qas|','2018-08-06|2018-08-06|2018-08-07|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10551,'18-030A','Magellan Aerospace Bournemouth','PIN','1518553-2/M4LM','D278 50156 200','S130 FHT','A',3,'423233','','65315','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','part missing in treatment house,','During treatment process part was getting missed|The treatment parts were tiny in size and large number of quantities |So after treatment process completion the parts accountability was not carried out','|Before treatment process the parts quantity to be ensure correctly and after that also that to be re-verify by using job cards','|After treatment completion parts quantity to be take into accountability','CAPA FOUND OK','','2018-04-19','Bhuvanesh(P)','Narasimha Murthy(R)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','DN34358','post DN','no','Misc','Bhuvanesh(P)','no','','|The parts which were all in treatment process that accountability was taken and ensured full quantity','E3456','nandishkumardk|nandishkumardk|qas|qas|','2018-08-06|2018-08-06|2018-08-07|2018-08-07|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10552,'51-065','THE BOEING COMPANY','CRANK','148225B6','253W3150-2','NA','PSDL REV A',1,'BOEING 001M','','70763','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','8 flat long tool running time tool broken so part dig mark and bore finish chattering...[ process problem] ','8 flat long tool running time tool broken so part dig mark and bore finish chattering... ..[ process problem] ','8 flat long tool slow running so next part ok.. ','8 flat long tool slow running so next part ok.. ','','','2018-04-19','pe_sez(a)','pe_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','pe_sez(a)','no','','m/c stop ','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10553,'43-002','Composite Industrie','BRACKET','6868201 2','V251 11617 200','','A00, ECN PV100298ST1AC92',1,'LTA PO-2','','70953','','0000-00-00',NULL,'yes','yes','yes','','','','','','no','PART PROFILE DIG MARK  ','While  rotary referencing for Machine after power trip part got collided with rotary bottom plate.','1.Instructions given to operators to take the machine reference without part loaded on the machine.','1.M0 & message added in the program to not to rotate /take the reference with part loaded on the machine.','Effectiveness found ok.','','2018-04-19','Subramanya L(Naik)','        CHETANA K','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','07','','','','','','1.Removed the part and took the rotary reference,Next part found ok.','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10554,'18A-007A','Magellan Aerospace Wrexham','ASSY PLATE COVER','','D572 52517 000','','A, ECN HG29999ST1TP78',2,'162892','','A14546','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Wrong part marking work order is raised on APR 30, 2018, but part marked to date code 41617 which means 4th day of 16th week year2017. It has to be written as 41618 means 4th day of 16th week year2018.','human error|','after part marking completed it is checked before lacquering|','we planned in future part marking is done using part marking machine(for approval)|','Next batch produced found ok.','','2018-04-20','Phaniraj(G)','Varadaraju(D)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','FI','yes','Misc','Bhuvanesh(P)','','','correction has been done|','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10555,'35A-613','Saab AB','ASSY LEVER 1','','D5227280500100','','PART ISSUE A',1,'OWED-LTA-003','','A14477','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Operation missing. Bush not pressed.','1.During Assembly process bush pressing was not done|2.In assembly process due to work pressure bush pressing was not identified','|The assembly process is carrying by as per operation sketch','|The training to be given to the operator','CAPA found ok','','2018-04-20','Phaniraj(G)','Venkatesh(BI)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','FI','yes','Misc','Yashawantha(NH)','no','','|The remaining parts are all identified and found ok','E3456','qas|','2018-12-20|','2018-12-20',NULL,NULL,NULL,NULL,NULL,NULL),(10556,'35-510A','Saab AB','HINGE FAIRING','493099 D','D5227339020100','NA','PART ISSUE B',1,'OWED-LTA-002','','71364','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Total length minus-0.20mm','Whenever filing time fitting operator done mistake.','We will fully opened in machine when cutout running time.','We will fully opened that portion in machine when cutout running time.','CAPA FOUND PK','','2018-04-20','Ravi nayak()','prodn_aero(prodn)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','Misc','Ravi nayak()','no','','That portion we will change the debbur method.','A3456','qas_aero|','2018-07-17|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10557,'18A-007A','Magellan Aerospace Wrexham','ASSY PLATE COVER','','D572 52517 000','','A, ECN HG29999ST1TP78',1,'162892','','A13748','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Operation Skipped, Lacquering not done.','human error|','after lacquering is done each part is checked before offer is done|','after lacquering is done each part is checked before offer is done |','Next batch Production found ok.','','2018-04-20','Phaniraj(G)','Venkatesh(BI)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','FI','yes','Misc','Bhuvanesh(P)','','','lacquering has been done|','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10558,'18A-107','Magellan Aerospace Wrexham','LINK BODY ASSY','','D574 50553 000','','A',1,'165478','','A14536','','2018-04-21',NULL,'no','yes','yes','no','no','no','yes','no','no','while doing staking operation one side dent done hence part has been rejected.assay w/o no A14536 ','During stacking operation dent mark observed on part|During stacking process the bottom bush was slipped from the fixture|Due to that dent stacking toll hit on top of the part then dent mark occurred','|The Fixture was re modified due to avoiding bush slippage','|The Fixture was re modified due to avoiding bush slippage','CAPA FOUND OK','','2018-04-21','Phaniraj(G)','Vasanth (Kumar N)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Assembly','','3','no','Misc','Ramesh(D)','no','','|The bush was located in fixture correctly then the remaining parts work is done as well','E3456','qas|','2018-08-07|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10559,'35-623','Saab AB','SHAFT 2','515372A','D5227280820000','NA','PART ISSUE A',1,'OWED-LTA-004','','71761','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','OD UNDER SIZE 0.012MM','RUNNING TIME PART WAS IN OVER SIZE , AS WELL AS TAPPER.LATER WHILE DOING RE-WORK PART GOT UNDER SIZE 0.012MM ','1) All the Operators are instructed to inform the Supervisor before doing rework.\r<br/>2) Instruction given to operators to carry out rework with proper supervisor guidance or in the presence of Senior operator.','Instruction given to operators not to carry out rework operation without the presence of senior operator or supervisor.','CA PA found OK.','','2018-04-23','Dinakar(K)','Ugraiah()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Raghavendra Rao(R)','','','LATER  TAPPER ADJUSTED IN PROGRAM AND PART FOUND OK','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10560,'18-692A','Magellan Aerospace Bournemouth','HOUSING-OUT BD BRG','1576361-2/QPGF','D275 40004 200','','C01',1,'417546','','70684','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','THICKNESS UNDER SIZE 0.3MM','BUTTING PROBLEM PART THICKNESS FACE-OUT -0.3MM SO PART GOT REJECTED ','BEFORE LOADING THE PART I AM GOING TO CLEAN THE PART AS WELL AS JAWS BEFORE LOADING THE PART  FOR EVERY PART   ','AS SOON AS I COME TO SHIFT I AM GOING TO CLEAN EVERY PART AND KEEP READY FOR LOADING AND INFORM MY RE LEAVER TO CLEAN THE PART BEFORE LOADING TO JAWS ','CA/PA Found satisfactory.','','2018-04-23','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','05','no','Misc','Raghavendra Rao(R)','','','BEFORE LOADING THE PART CLEANING THE JAWS AND PART.PART FOUND OK  ','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10561,'18-295A','Magellan Aerospace Bournemouth','BOLT','CD703067/W87849','PID577 56145 200','','A',1,'423258','','72382','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','od dig mark.','running time air pipe got disconnected because of house keeping member by unknowing she as touched the pipe , air pressure got low , machine stopped part got dig on od ','we have trained the house keeping members not to touch wires and air pipes ','we have trained the house keeping members not to touch wires and air pipes ','','','2018-04-23','Dinakar(K)','Sunil Gowda(B N)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','Manufacture Only','','09','no','Misc','Ravi(M)','','','called maintenance team to change the connector  , run the part , part found ok ','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10562,'51-023','THE BOEING COMPANY','BRACKET','180534B0','149A7371-931','','PSDL REV A',3,'BOEING 001D','','71599','','0000-00-00',NULL,'yes','no','no','no','no','yes','no','yes','no','Hole diameter 0.06 inches measured out of tolerance to the drawing requirement.\r\n','Wrong NC program was generated from the engineering team and same was given to production to run the part.','Required hole diameter size was included in the NC program and run the next part.','Required hole diameter size was included in the NC program and run the next part.','Next part found within acceptable limit.','','2018-04-24','pe_sez(a)','Shivaraj K S,Diwakar R.B.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','i700-4','qas_sez(a)','no','','Stop the next production run and immediately inform the engineering to the above issue.','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10563,'51-024','THE BOEING COMPANY','BRACKET','180534B0','149A7371-932','','PSDL REV A',3,'BOEING 001D','','71600','','0000-00-00',NULL,'yes','no','no','no','no','yes','no','yes','no','Hole diameter 0.06 inches measured out of tolerance to the drawing requirement. ','Refer NC Number 10562.','Refer NC Number 10562.','Refer NC Number 10562.','Refer NC Number 10562.','','2018-04-24','pe_sez(a)','Shivaraj K S,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','i700-3','qas_sez(a)','no','','Refer NC Number 10562.','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10564,'51-023','THE BOEING COMPANY','BRACKET','789223A5','149A7371-931','','PSDL REV A',3,'BOEING 001D','','64601','','0000-00-00',NULL,'yes','no','no','no','no','yes','no','yes','no','Hole diameter 0.06 inches measured out of tolerance to the drawing requirement. ','Refer NC Number 10562.','Refer NC Number 10562.','Refer NC Number 10562.','Refer NC Number 10562.','','2018-04-24','pe_sez(a)','op_sez(s)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','Misc','qas_sez(a)','no','','Refer NC Number 10562.','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10565,'51-024','THE BOEING COMPANY','BRACKET','789223A5','149A7371-932','','PSDL REV A',3,'BOEING 001D','','64602','','0000-00-00',NULL,'yes','no','no','no','no','yes','no','yes','no','Hole diameter 0.06 inches measured out of tolerance to the drawing requirement. ','Refer NC Number 10562.','Refer NC Number 10562.','Refer NC Number 10562.','Refer NC Number 10562.','','2018-04-24','qas_sez(a)','op_sez(s)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','Misc','qas_sez(a)','no','','Refer NC Number 10562.','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10566,'18-295A','Magellan Aerospace Bournemouth','BOLT','CD703067/W87849','PID577 56145 200','','A',1,'423258','','72383','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','2.84 drill broken','Drill broken while power tripped. ','1) Drill changed and continued the production.\r<br/>2) Re-drilled through the hole to remove the broken drill from the part and rechecked the dimension and found Ok.','1) The drill life will be monitored in the next production batches.\r<br/>2) UPS back up will be used during power tripping.','CAPA found ok.','','2018-04-24','Anjinamurthy(H)','S. Shiva Kumar,Punith G S,Girish HP,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Manufacture Only','','5','yes','BMV 60-2','Anjinamurthy(H)','','','verified all the parts for any chattering marks and dimensional deviation and found OK.','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10567,'18-118B','Magellan Aerospace Bournemouth','BEARING HOUSING ','1613719-2/T7SH','PID275 40005 200','','C01',1,'423253','','72505','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','OD 0.2mm undersized.','Face grooving running time part rotating so OD 0.2mm undersized. ','Chuck pressure comment added in the program top and this information passed to the operator.','Chuck pressure comment added in the program top and this information passed to the operator.','CA PA Found Ok.','','2018-04-24','Dinakar(K)','Ravi(M)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','11','no','Misc','Sandhesh D(S)','no','','Increase the chuck pressure value and run the part.','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10568,'35-182B','Saab AB','EDGE HOUSING','203993B1','423Z1121-5-02','','--B',4,'Forecast po for B787','','71414','','0000-00-00',NULL,'yes','no','yes','no','yes','no','no','no','no','Outer profile dig up to 0.3mm.','Whenever outer wall program running time tool dig mark on profile.','Inform the HASS service engineer and clear that problem & inform the CADD engineer to check the outer wall program.','Finally we change tool to that program dia 16 E/M instead of 16R3 B/N.','CAPA FOUND OK','','2018-04-25','prodn_aero(prodn)','prodn_aero(prodn)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','09','no','Misc','Dinesh kulal()','no','','Change the setting to other CRN .','A3456','qas_aero|qas_aero|','2018-07-17|2018-07-17|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10569,'51-048','THE BOEING COMPANY','BRACKET','741181','149A7371-9616','NA','PSDL REV A',3,'BOEING 001P','','72281','','0000-00-00',NULL,'yes','no','yes','no','yes','no','no','no','no','while running condition fms communication error,due to same programme taken to mc-3(mazak).','on that time fms programmed modified.','inform to mazak team same problem shoud having due to correct the problem','inform to mazak team same problem having while running condition next the programe we r maintained optional stop.','','','2018-04-26','pe_sez(a)','pe_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','01','no','Misc','pe_sez(a)','no','','on that time fms programmed modified.','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10570,'35-258','Saab AB','BRACKET, DEFLECTION STOP','846961-04','423Z6187-6','','---',1,'Forecast po for B787','','72514','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','while setting condition wrong direction loaded','fixture was loaded in the reverse direction .\r<br/>','for the next part fixture was loaded in the correct direction and new offset was taken.','Identification on the fixture is done so that operator can easily identify which side fixture is to be loaded on the machine','CA/PA Found OK.','','2018-04-26','pe_sez(a)','pe_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','pe_sez(a)','no','','then next change the fixture as per operation module','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10571,'51-027','THE BOEING COMPANY','BRACKET','741161','149A7371-945','','PSDL REV A',1,'BOEING 001E','','73324','','0000-00-00',NULL,'yes','no','yes','no','yes','no','no','no','no','running time 12xr3 tool broken so part base dig mark 1nos reject.','running time 12xr3 tool broken so part base dig mark','new tool change and running ','new tool change and running ','','','2018-04-26','pe_sez(a)','pe_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','01','no','Misc','pe_sez(a)','no','','new tool change and running','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10572,'35-169','Saab AB','ALCD_STRUCT_SUPPORT-FTG_L','9366958','423Z1200-12-01','','---',1,'PA 1510 FORECAST','','66682','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Corrosion Pits observed','Due to rubbing of tool or material behavior Corrosion Pits has been observed in Treatment house','|Apply PX-24 after machining, and polishing and rubbing of tool should be avoided  ','|Apply of PX-24 is mandatory before sending the parts to treatment house. ','CAPA FOUND OK','','2018-04-27','qas_sez(a)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','DN36590','POST DN','yes','Misc','qas_sez(a)','no','','|PARTS NOT FOUND IN FI OR WIP','Z3456','nagendra|','2018-08-07|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10573,'18-391B','Magellan Aerospace Bournemouth','END COVER','28163030-B','D278 50166 200','','A',1,'423234','','72808','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Hole position problem out-off tolerance  (0.20mm) ','The older fixture was loaded without zero point clamping technique. therefore in order to reduce the cycle time zero point clamping system was introduced to the fixture and the fixture was not validated after the implementation of the zero point technique, due to which the taper on the top face of the fixture was not identified and this resulted to the deviation in the hole position.','1) The new fixture made with zero point system is scraped and the older fixture is used to continue the production.\r\n2) All the parts made with new fixture was rechecked with the Checking gauge for hole position.','1)If any new fixture is made or if any alteration carried out in the fixture the fixture will be validated before using for production.\r\n2) Fixture validation record will be maintained.','CA found ok, PA effectiveness will be evaluated in the next process audit.','','2018-04-27','Anjinamurthy(H)','Prashanth Kumar M,Paramaeshappa ,Girish MS,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','5','no','MAKINO SLIM-2','Dhananjaya(N)','','','The milling operation was stopped. Then the new implemented fixture was removed and the next operation was carried out in old process only.','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10574,'18-696A','Magellan Aerospace Bournemouth','BUSH ','1517166-3/M5AZ','D278 50164 200','','A',4,'417546','','68746','','0000-00-00',NULL,'no','no','no','no','no','yes','yes','yes','no',' MPI REJECTION DUE TO CORROSION OBSERVED IN PART ','Corrosion observed on parts during treatment process that was observed |During final Inspection process that was observed and cleared |But corrosion resistant oil was not used during part shipment to treatment house|The persons who were packed are new persons|Due to that parts was failed in MPI','|Training to be given to the packing persons and ensure the application of corrosion resistant oil application','|That was contentiously monitor and review','CAPA FOUND OK','','2018-04-27','qas_sez(a)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','DN36277','POST DN','no','Misc','qas_sez(a)','no','','|The parts which are in shipment that was ensured to apply Corrosion resistant oil ','Z3456','qas|qas|','2018-08-07|2018-08-07|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10575,'46-030A','Mahindra Aerostructures Pvt.Ltd','PACKER','4259401','D574 50543 221 MH','','C',2,'MAPL Forecast ','','68358','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Buffing not Properly & HOLE DEBURR NOT DONE. ','after debarring part not checked by fitting person. ','after deburring fitting person will ensure all parts are deburred before moving to inspection. ','after deburring fitting supervisor will ensure 1st two batches all parts are deburred before moving\r\nto inspection.','CAPA FOUND OK','','2018-04-28','Irappa(Badiger)','Prashanth Kumar M,Manukumar H M,Girish MS,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','With Treatment','','FI','no','MAKINO SLIM-1','Nandishkumar(D.K.)','','','checked all the Parts. ','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10576,'18-415B','Magellan Aerospace Bournemouth','ACTUATOR HOUSING','9309','D278 50163 201','','D',2,'423234','','72857','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Hole position  problem','Due to improper butting method during the stage inspection there was a deviation on the hole position, for which the operator provided correction and after changing the clamping method part found ok.','1) Changed the butting method for inspection and changed the measuring method.\r<br/>2) Instructed stage inspector to consult with the senior project leader before providing correction.\r<br/>3) All the operators are instructed to communicate with the supervisors before providing correction to the part.','1) Inspection method changed and on-spot training provided to the stage inspector in how to inspect the part and provide clearance.\r<br/>2) Part will be ensured with the checking jig before providing correction in the machine.','Next batch inspection method checked and found OK.','','2018-04-28','Anjinamurthy(H)','Paramaeshappa ,Anjinamurthy H,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','5','no','MAKINO SLIM-1','Dhananjaya(N)','no','','Immediately stopped the production and ensured all the finished parts are not defected.','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10577,'51-053','THE BOEING COMPANY','BRACKET','741181','149A7371-9631','','PSDL REV A',1,'BOEING 001G','','72268','','0000-00-00',NULL,'no','no','yes','no','yes','no','yes','no','no','Part running time part edge cut.','When Part Cutout time part was got vibration. ','Holding Wall thickness increased to avoid the Vibration.In Part cutout program cutting tool\'s Feed rate reduced 50%.','part holding to be increase. Cutting tool\'s holding Shank to be increase to avoid and stabilize the Vibration ','CA PA found effective.','','2018-04-28','pe_sez(a)','Umesh B,Diwakar R.B.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','1','no','i700-3','pe_sez(a)','no','','Production Stopped.All parts checked.Found correct.','Z3456','qas|','2018-07-24|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10579,'35-142A','Saab AB','BCD_HINGE_SUPPORT_FITTING','722293','424Z3111-5','','--B',1,'1600218100','','71628','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Outer wall thickness less than requirement.','Part running time part will be vibrated so wall thickness -0.1mm.','Give message before running the programe cross check the clamp tightening.','Give message before running the programe cross check the clamp tightening.','CAPA FOUND OK','','2018-05-01','prodn_aero(prodn)','Manjunatha.S.T(M)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Manjunatha.S.T(M)','no','','Correct the clamp tightening.','A3456','qas_aero|qas_aero|','2018-07-17|2018-07-17|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10580,'35A-563','Saab AB','LEVER ASSY','','D522 73536 002 00','','PART ISSUE B',1,'PA1687 LTA-2','','A13898','','0000-00-00',NULL,'no','no','no','no','no','no','yes','yes','yes','D5227353600200 CIM W/O A13898, A13899, A13900 and A13922, total qty 33 pcs\r\nD5227353600300 CIM W/O A13881, A13882 total qty 19 pcs\r\nD5227349920200 CIM W/O 69879 total qty 20 pcs\r\n\r\nRequirement on drawing D52273536 and D52273499 is TV which according to ABD0003 is Part marking with ink or pen and clear coat. All parts are marked with a label in the plastic bag.\r\n','1) Lack of awareness on the interpretation of drawing needs.\r<br/>2) For Part No. D5227349920200 Part marking Identification mentioned in the drawing denotes for part marking to be done after assembly.','1) For Part No. D5227353600300 & D5227353600200 we have displayed a quality alert in assembly and inspection area to identify the marking requirement refer the attached QA-19.\r<br/>2) For Part No. D5227349920200 communication is forwarded to customer regarding the drawing requirement on identifying the part after assembly which is not applicable for CIM Tools as the parts are not assembled in CIM.','1) For Part No. D5227353600300 & D5227353600200 we have displayed a quality alert in assembly and inspection area to identify the marking requirement.\r<br/>2) Training program is scheduled for the Quality Inspector and the Assembly personnel on interpretation of the drawing needs.\r<br/>','Next batch found ok and customer accepted the CA & PA and mail conformation received for the part marking in assembly location.','C62932','2018-05-01','qas_sez(a)','qas_sez(a)','OF-002955','2018-04-17','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','yes','Assembly','','CUST END','no','Misc','qas_sez(a)','','','1) All the parts in FG and WIP are inspected for missing of part marking and the deviated parts are part marked and clear coated as per the drawing requirements.','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10581,'35-650','Saab AB','SHAFT','B76568','D5227346820200','NA','B',1,'PA1687 LTA-2','','69060','','0000-00-00',NULL,'no','no','no','no','no','no','yes','yes','yes','Dry film lubricant release found on total 13 pcs. According to AIPS/AIPI 0204-009 there should be no adhesion failure.\r\n\r\nLinked Work Order: 69061.','The parts subjected to the release of the dry film lubrication was processed without undergoing passivation after the completion of Zi/Ni as per the Type-1 process. this resulted in improper adhesion of the dry film.','Treatment process was changed from Type-1 to Type-2 (i.e. with passivation after the Zi/Ni platting.','Both the Zi/Ni and dry film lubrication process are carried out in same treatment house as per the Type-2 process.Refer CIM FAIR Document F35650A002.','NC Accepted by customer and next batches found ok.','C61262','2018-05-02','qas_sez(a)','qas_sez(a)','OF-002896','2018-03-15','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','yes','With Treatment','DN36895','CUST END','no','Misc','qas_sez(a)','no','','Intimated the supplier on the issue and verified all the in-house parts for the defect.','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10582,'35-630','Saab AB','SUPPORT SEAL RETAINER ','203993B1','423Z1834-1-03','NA','---',1,'1600218100','','68380','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','yes','During receiving inspection the following nick mark was found on 423Z1834-1-03, Support Seal Retainer. The packaging had no damage.','Improper handling of parts during transit.||','1) All the parts are sufficiently packed with bubble wrap and foam sheets during transit.\r<br/>2) Sufficient partitions are made with foam sheets to avoid part to part contact. ||','Parts will be stored in proper trays with adequate partition to avoid part to part contact.||','Next batch packing methods are verified and found ok.','C62230','2018-05-02','qas_sez(a)','qas_sez(a)','OF-002956','2018-04-18','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','yes','With Treatment','DN36763','CUST END','no','Misc','qas_sez(a)','no','','All the parts stored and in process are inspected for similar defect and found nil.||','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10583,'47-119','GKN Aerospace Filton','TOP SPREADER PLT M/C','6360203','F57451570200','NA','PART ISSUE B',1,'1210041001','','67191','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Incorrect profile.\r\n\r\nSimilar defect is observed in W/O\'s 70784(20), 70786(20) also.','CAD model generated by the engineering department is not properly validated with respected to the customer supplied drawing.','1) The CAD Model generated is re validated and the NC program is re generated to meet the revised drawing requirements. Refer Attachment-1.\r<br/>2) All similar models will be re-checked to ensure no deviation from the customer supplied drawing requirement and the action will be completed on or before Jun 1, 2018.','1) Model validation reference no will be included in the Master Process Sheet(MPS).\r<br/>2) Quality Engineer shall trace the model validation details from the engineering department from MPS during the FAIR documentation.\r<br/>3) Checking Jig will be introduced both in production and Final inspection to avoid similar deviations on or before May 31, 2018.','Next FAIR found ok.','C59778','2018-05-02','qas_sez(a)','qas_sez(a)','201129451','2018-04-27','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','DN35181','CUST END','no','Misc','qas_sez(a)','','','All the parts in process are quarantined and found to be defective and the parts are rejected.','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10584,'18-122A','Magellan Aerospace Bournemouth',' 	FORKEND ASSEMBLY ','CD703874/08354A','PID572 50462 201','','J01',1,'423255','','72315','','0000-00-00',NULL,'yes','no','yes','no','yes','no','no','no','no','POWER TRIP.','POWER TRIP OFF OCCURRED DURING THAT TIME ALARM BUSS ER NOT HIGHLIGHTED SO MACHINE WAS NOT STOPPED MANUALLY . MACHINE WAS STOPPED AUTOMATICALLY SO TOOL DIG MARK OCCURRED IN PART. ','THE ALARM BUSS ER TO BE CHECK DAILY AND MAINTENANCE TO BE CARRY OUT EVERY WEEK','MAINTENANCE TEAM TO BE MAINTAIN  FOR THE ALARM BUSS ER ','CA PA found Ok.','','2018-05-03','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','05','no','Misc','Ravi(M)','no','','THE ALARM BUSS ER WAS CHECKED AND REPAIRED TO HIGHLIGHT THE POWER OFF','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10585,'51A-082','THE BOEING COMPANY','BRACKET ASSY','','332A2930-1','','PSDL REV B',2,'BOEING 001M','','A14767','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','OVER SIZED SLOT WIDTH OF THE PART WHILE DOING THE BUSH PRESSING OPERATION DUE TO THE OVER FORCE APPLIED.','wile doing the bush pressing operation we have ensure that butting block has given in-between the slot. ','|training given to the operators,that butting block is mandatory while pressing the bush |training given to the operators,that butting block is mandatory while pressing the bush |training given to the operators,that butting block is mandatory while pressing the bush |training given to the operators,that butting block is mandatory while pressing the bush ','|given to well training for the operator|given to well training for the operator|given to well training for the operator|given to well training for the operator','Operator effectiveness to be measured.','','2018-05-03','pe_sez(a)','pe_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Assembly','','FI','no','Misc','pe_sez(a)','no','','|wile doing the bush pressing operation we have ensure that butting block has given in-between the slot.|wile doing the bush pressing operation we have ensure that butting block has given in-between the slot.|wile doing the bush pressing operation we have ensure that butting block has given in-between the slot.|wile doing the bush pressing operation we have ensure that butting block has given in-between the slot.','Z3456','||||qas|','2018-08-10|2018-08-10|2018-08-10|2018-08-10|2018-08-10|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10586,'18-438A','Magellan Aerospace(Blackpool) Limited','MANIFOLD','2800','PI55-1213031-00','','NIL',1,'BPP-529619 amed-1','','70409','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Spot-faces omitted x 4 places,[Ref Detail Y] Req. before treatment.','Improper interpretation of drawing.','1) Query raised to the customer on the spot face depth. \r<br/>2) Re-processing of the parts initiated based on the revised drawing supplied by the customer.\r<br/>3) All the NC program for the subjected part is revised as per the revised drawing.','In case of any missing details in the customer supplied drawing immediate query will be raised to the customer before initiating the FAIR production.','NC Accepted by customer and MPS amended.','C62167','2018-05-03','qas_sez(a)','qas_sez(a)','RDN 4666','2018-04-26','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','CUST END','no','Misc','qas_sez(a)','no','','All the similar parts under process was quarantined and immediate query was raised to the customer on the spot face depth.','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10587,'18-435A','Magellan Aerospace(Blackpool) Limited','MANIFOLD','29098139','PI201274609','','NIL',1,'BPP-529619','','69145','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Spot-faces omitted, Ref Detail U.','Improper interpretation of drawing.','1) Query raised to the customer on the spot face depth.\r<br/>1) Re-processing of the parts initiated based on the revised drawing supplied by the customer.\r<br/>2) All the NC program for the subjected part is revised as per the revised drawing.','In case of any missing details in the customer supplied drawing immediate query will be raised to the customer before initiating the FAIR production.','NC accepted by customer and MPS amended.','C62276','2018-05-03','qas_sez(a)','qas_sez(a)','RDN 4667','2018-04-26','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','CUST END','no','Misc','qas_sez(a)','no','','All the similar parts under process was quarantined and immediate query was raised to the customer on the spot face depth.','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10588,'18-118B','Magellan Aerospace Bournemouth','BEARING HOUSING ','1613719-2/T7SH','PID275 40005 200','','C01',1,'423253','','72844','','0000-00-00',NULL,'yes','yes','yes','','','','','','','ID diameter over size by 0.02 mm.','X axis was shifted DUE TO X AXIS SHIFTED BREAK CIRCUIT  MAL FUNCTION                    ',' \r<br/>1)Inform to the maintenance team and adjust the x axis.                                                        2)IN THE NEXT PREVENTIVE MAINTENANCE THE X AXIS BREAK CIRCUIT WAS CHANGED BY JYOTI PREVENTIVE MAINTENANCE TEAM                ','THE X AXIS BREAK CIRCUIT WELL BE INSPECTED FOR PROPER FUNCTION DURING EVERY PREVENTIVE MAINTENANCE','CAPA found Ok.','','2018-05-03','Dinakar(K)','        Seetharamu D','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','05','','','','','','Correct the X axis and run the part.','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10589,'47-113A','GKN Aerospace Filton','BRACKET','6358202','D57952066200','NA','PART ISSUE A',1,'GS68-LTA-2018','','73146','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Deep Tool dig mark observed on top surface.','while program running time tool broken.|During Outer wall finishing program,the lug rotated and tool dig mark occurred.\r\n\r\n|The bolt length selected was equal to thread length in the lug|operator not select the correct length bolt.\r\n|operator was not aware about the proper bolt length to be used','|proper bolts changed and continue the production.','|informed all the operators to use bolt of length 10mm greater then the part thickness.','Next batch found ok.','','2018-05-03','Krishna(Chowdary.G.P.)','Dhananjaya(N)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','3','no','Misc','Dhananjaya(N)','no','','|all proves part cross cheeked and all the parts are ok.','E3456','pe|qas|','2018-07-31|2018-07-31|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10590,'47-113A','GKN Aerospace Filton','BRACKET','6358202','D57952066200','NA','PART ISSUE A',1,'GS68-LTA-2018','','73155','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Countersunk diameter over size by 0.3mm.','1) Countersink diameter was not measured as per the requirement.|2) The diameter of the countersink was .3mm greater than the drawing requirement as the tool was stepping down beyond the requirement.|3) operator did not left stock for the countersink operation and did not ensured proper dept.|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.','CA PA found ok.','','2018-05-03','Krishna(Chowdary.G.P.)','Dhananjaya(N)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','3','no','Misc','Dhananjaya(N)','no','','|Immediately stopped the machine and checked the previously completed parts and found ok.','E3456','qas|qas|','2018-07-26|2018-07-26|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10591,'51-074','THE BOEING COMPANY','BRACKET DETAIL','508348','322U8810-9','NA','NIL',1,'BOEING 001N','','72183','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','When I maching running time dia 16 flat pull down from the holder due to over cutting load.','Due to More Depth of cut and Cutting Speed in NC program','New NC program collected From the Engg Department with Low Depth cut and high Cutting Speed. The cutting holding shank also incresed from 16mm to 20 mm. ','Cutting tools Holding area to be increase and Depth of cut to be reduced where ever cutting tool\'s more overhang.','CA PA is found effective in next batches.','','2018-05-04','pe_sez(a)','op_sez(s)','','0000-00-00','DIG MARK','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','1','no','Misc','pe_sez(a)','no','','production Stopped. informed to Eng Dept','Z3456','qas|','2018-07-24|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10592,'51-072','THE BOEING COMPANY','BANJO FITTING','G23551K01','113T1204-2','NA','NIL',1,'BOEING 001S','','73100','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Thread Damage occurred','While checking the threads,thread gauge jammed on the part.\r\n<br/>\r\n<br/>Due to threads burr not debarred properly, this may cause for jamming the thread gauge.\r\n<br/>\r\n<br/>  ','Effectiveness checked with fitters and found ok.\r<br/>1. Erappa Badiger\r<br/>2. Raghu','Effectiveness checked with fitters and found ok.\r<br/>1. Erappa Badiger\r<br/>2. Raghu','Training is given to all the fitters and the next batches found ok.','','2018-05-05','Ravikumar(L)','Rakesh (KC)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','13','no','Misc','Ravikumar(L)','no','','Training conducted for fitters, How to remove the burr in the threads.\r\n','E3456','qas|','2018-08-01|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10593,'47-119A','GKN Aerospace Filton','TOP SPREADER PLT M/C ','6358202','F57451570200','NA','PART ISSUE B',36,'GS68-LTA-1-2018','','73278','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','INCORRECT PROFILE','Due to NC Program Problem','Updated NC program and Executed on Machine and Part Found OK \r<br/>','Before Execution the program on Machine Programmer has to double cross check program.  ','Next batches found ok.','','2018-05-06','Nandishkumar(D.K.)','Nandishkumar(D.K.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','INSPECTION','no','Misc','Nandishkumar(D.K.)','no','','Updated NC program and Executed on Machine and Part Found OK.\r\nObsolete old program and New updated program moved to Program Data Storage','E3456','qas|','2018-07-24|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10594,'51-049','THE BOEING COMPANY','BRACKET ','741161','149A7371-9623','NA','PSDL REV A',2,'BOEING 001P','','73518','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Unwanted Operations due to Fixture Disturb','The Parts Machined with Side Clamped fixture. Due to Over Cutting Speed and 5 Axis Bed Tilting the Fixture disturbed from its original Position','Side Clamped removed. Holes are Made in Fixture and directly mounted on the Bed along with Location Pins and Allen Screws','Side clamps to be avoid and Top clamp to be added where ever more cutting Speed and Bed Tilting','Next part found within acceptable limit.','','2018-05-08','pe_sez(a)','op_sez(s)','','0000-00-00','Unwanted Operations due to Fixture Disturb','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','1','no','Misc','pe_sez(a)','no','','Production stopped. previous machined Parts are 100% checked','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10595,'51A-003','THE BOEING COMPANY','LOWER BEAM FWD INBD SPLIC','','315Z1302-1501','','NIL',1,'BOEING 001K','','A14808','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Pilot hole diameter was oversized due to drill Broken when Machine Running Time.','Dia 2.5mm Drill is broken when assembly Drilling Operations carried Out.','New drill replaced with Sufficient length with 6mm rigid shank','when assembly parts drilling time heavy duty drills are to be taken. Operators are requested to monitor the cutting tools Life..','Next part found within acceptable limit.','','2018-05-08','pe_sez(a)','op_sez(s)','','0000-00-00','Drill Broken when Machine Running Time','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Assembly','','03','no','Misc','pe_sez(a)','no','','Production Stopped. Machined Parts are verified.','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10596,'18-117B','Magellan Aerospace Bournemouth',' 	HOUSING-OUT BD BRG','1552479-2/NLWL','PID275 40004 200','','C01',1,'423253','','71854','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','OD Dig mark on top face,  ','','','','capa found ok.','','2018-05-08','Anjinamurthy(H)','Punith G S,Girish HP,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','7','no','BMV 60-2','Dhananjaya(N)','no','','','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10597,'35-564','Saab AB','LEVER','509667C','D522 73536 203 00','','PART ISSUE B',4,'PA1687 LTA-2','','72474','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Tool dig mark on part surface .','Running time tool broken.','|Informed the operator to monitor the tool life and to ensure the cutting edges before starting cycle.','|Life of the tool will be monitored regularly.','Next batches found ok.','','2018-05-09','Krishna(Chowdary.G.P.)','Rakeshbabu(V)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Gurukiran S(M)','no','','|Immediately stopped the machine and changed the tool.','E3456','qas|','2018-08-09|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10598,'35-475A','Saab AB','FRAME ','528986D1','D5227338420100','NA','A',1,'OWED-LTA-001','','71188','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Part thickness under size -0.2mm,','Operator did not ensured the proper butting of part.','|Informed all the operator to ensure proper butting of the part before starting the cycle.','|Informed all the operator to ensure proper butting of part by using feeler gauge before starting the cycle.','Next batches found ok.','','2018-05-09','Krishna(Chowdary.G.P.)','Rakeshbabu(V)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','10','no','Misc','Gurukiran S(M)','no','','|Immediately informed the operator to stop the machine and ensure proper butting of the part.','E3456','qas|','2018-08-09|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10599,'47-113A','GKN Aerospace Filton','BRACKET','503459D','D57952066200','NA','PART ISSUE A',1,'GS68-LTA-2018','','73644','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Hole size over size,','CRC value entered wrongly by the operator.','|Informed all the operator to check the CRC value before starting the production.','|All the Operators are informed not to run the machine until supervisor confirms the CRC value entered.','Next Batches found ok.','','2018-05-09','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','3','no','Misc','Dhananjaya(N)','no','','|Immediately stopped the machine and changed the CRC value.','E3456','qas|qas|','2018-08-09|2018-08-09|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10600,'47-115A','GKN Aerospace Filton','BRACKET','3243302','D57952067200','NA','PART ISSUE A',4,'GS68-LTA-2018','','73627','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Tool dig mark on outer profile,','Program running time tool broken. |Insufficient coolant flow. |Coolant filter clog.','|Preventive maintenance done once in 3 months.','|Preventive maintenance done once in 3 months.\r<br/>Operator will ensure Coolant flow before shift start.','CA/PA found satisfactory. ','','2018-05-09','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','3','no','Misc','Dhananjaya(N)','no','','|Cleaned the coolant filter.\r\nTool changed.','E3456','pe|nandishkumardk|','2018-11-27|2018-11-27|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10601,'18-118B','Magellan Aerospace Bournemouth','BEARING HOUSING ','1613719-2/T7SH','PID275 40005 200','','C01',1,'423253','','72844','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','OD DIG MARK , SO PART REJECTED ',' POWER TRIP ,UPS PROBLEM ','SUPERVISOR ENSURED  PROPER FUNCTIONING OF MACHINE AFTER THE RECOVER FORM POWER FAILURE.                  ','MAINTENANCE TEAM REPLACED THE UPS UNIT ','CA PA found OK.','','2018-05-10','Dinakar(K)','Seetharamu(D)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','11','no','Misc','Raghavendra Rao(R)','no','','MACHINE STOPPED , UPS GOT FIRED AND WENT OUTSIDE TO OFF THE FIRE ','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10602,'51-062','THE BOEING COMPANY','HINGE FITTING PANEL SUPPO','546791','115W3665-12','NA','PSDL REV -',1,'BOEING 001M','','71904','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Bore over size','Reamers are added instead of Boring bar. Due to Over length and Parts rib thickness less the bore was oversize up to 10 microns from the upper limit value ','Cutting tool\'s parameter Speed and feed are changed.','New Reamers size to be ensured in Dummy Part before to Start in original part.','Next batches found ok.','','2018-05-10','pe_sez(a)','Nataraja C V,Diwakar R.B.,','','0000-00-00','Bore over size','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','3','no','i700-1','pe_sez(a)','no','','Production Stopped. Informed to cutting tool manufacture. ','Z3456','qas|','2018-07-27|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10603,'35A-353A','Saab AB','LIFT PIN HOUSING FWD','','423Z1124-5-52','','1',1,'787 Forecast','','A14813','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','ASSEMBLY BORE REJECTED   ','While bore proving time position will be shifted so bush bore over size 0.1mm.','While check the CMM after give the correction then continue the production.','Inform to operator first part proving time maintain the bore will under size after checking CMM then after maintain in the bore diameter.','Next Batches found ok.','','2018-05-11','pe_sez(a)','pe_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Assembly','','05','no','Misc','pe_sez(a)','no','M03441','While check the CMM after give the correction then continue the production.','Z3456','qas|','2018-08-09|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10604,'35-474A','Saab AB','FRAME ','704718','D5227338420000','NA','A',1,'PA1687 LTA-2','','73174','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','Thread mill double formation','trail part proving|For Tool Trials program given|To reduce the Cycle time.|For continuous improvement|To achieve the target cycle time.','|Program was changed and program proved part found OK, Obsolete the old program and new proved program saved in to data base.','|When giving the program the program will be four eye checked.','New program found effective.','','2018-05-11','Ramesh(Poojary)','Mahesh(N)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','05','no','Misc','Narayanappa(G)','no','','take the new program and run the another one part proving.|Program was changed and program proved part found OK','E3456','cam|qas|','2018-08-06|2018-08-09|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10605,'35A-353A','Saab AB','LIFT PIN HOUSING FWD','','423Z1124-5-52','','1',1,'787 Forecast','','A14811','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','ASSEMBLY BORE REJECTED ','While bore proving time position will be shifted so bush bore over size 0.05mm.','While check the CMM after give the correction then continue the production. ','Inform to operator first part proving time maintain the bore will under size after checking CMM then after maintain in the bore diameter. ','Next Batches found ok.','','2018-05-14','Lohith(K)','Kiran(KM)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Assembly','','5','no','Misc','Lohith(K)','no','M00915','While check the CMM after give the correction then continue the production. ','E3456','qas|','2018-08-09|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10606,'18-119B','Magellan Aerospace Bournemouth',' 	HOUSING OUT B DRG 3 ','1573705-1/QD84','PID275 40011 200','','D01',1,'423253','','72211','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','ID OVER SIZE by 0.02MM SO PART REJECTED','Parts were already Finished, Unknowingly same part loaded again for finishing.','1.Operator is Given Training Again on House keeping and Part tractability.  \r<br/>2.Segregation of Finished and semi finished parts with separate trays with display boards on it.','1.All the Operators in the in the group are given similar training and awareness is created','Effectiveness found ok.','','2018-05-14','Dinakar(K)','Sudhakar C.M,Dinakar K,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','11','no','QT100S-1','Raghavendra Rao(R)','no','','PART AS BEEN INCEPTION WHICH I HAVE RUN BEFORE ','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10607,'35-676','Saab AB','HANDLE BLOCKAGE ','701945 4A1','D5227343820400','NA','PART ISSUE C',16,'OWED-LTA-004','','74274','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Outer profile over size so part dig mark,','Due outer Profile cut out program problem. part get reject.','New program given and executed on machine part got OK and removed the old program and new program moved to data storage. ','Before execution on machine, program has to 4-Eyes cross check then execute the program on machine.','Next batches found ok.','','2018-05-14','Ramesh(Poojary)','Paramaeshappa ,Girish MS,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','3','no','MAKINO SLIM-1','Dhananjaya(N)','no','','New program given and executed on machine part got OK','E3456','qas|','2018-08-04|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10608,'47-109A','GKN Aerospace Filton','BLOCK COVER LH','7689501-1','D5725097420801','NA','PART ISSUE N',1,'GS68-LTA-2018','','74098','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dig mark observed on face.','While part 1st operation running time part was lifted.','Inform to operator before running the programs check part clamping properly.','Inform to operator each and every part check the RM size after load the part and continue the production.','Next batch found ok.','','2018-05-15','pe_sez(a)','pe_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','1','no','Misc','pe_sez(a)','no','','Inform to operator before running the programs check part clamping properly.','Z3456','qas|','2018-07-24|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10609,'47-110A','GKN Aerospace Filton','BLOCK COVER RH','7689504-1','D5725097420901','NA','PART ISSUE N',1,'GS68-LTA-2018','','74100','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Thickness under size.','While part 2nd operation running time roughing tool broken.','Inform to operator, before start the programs cross check the roughing tool edges.','Inform to operator, every time before start the programs cross check the roughing tool edges.','Next batch found ok.','','2018-05-15','pe_sez(a)','pe_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','pe_sez(a)','no','','Immediately stop the machine, new tool added after continue the production. ','Z3456','qas|','2018-07-24|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10610,'51-013','THE BOEING COMPANY','SPACER','192311B9','673Z3480-19','','NIL',1,'BOEING 001J','','73308','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dig mark observed on face.','Part not clamping properly, roughing program running time\r<br/>part was lifted.','Inform to operator before running the programs check part clamping properly. ','Inform to operator each and every part check the RM size after load the part and continue the production. ','CA/PA acceptable.','','2018-05-15','pe_sez(a)','pe_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','3','no','Misc','pe_sez(a)','no','','Inform to operator before running the programs check part clamping properly. ','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10611,'35-226A','Saab AB','HINGE BRACKET 1','4761501 1','D576 50004 207','','D00',1,'1600223433/Forecast ','','74017','','0000-00-00',NULL,'no','yes','yes','yes','no','no','no','no','no','Due to RM size incorrect the part profile was measured under size.','Due to RM size incorrect the part profile was measured under size.','Informed and training given to the operator before loading the part ensure the correct RM size was taken as mentioned in the Manufacturing process sheet.','Informed and training given to the operator before loading the part ensure the correct RM size was taken as mentioned in the Manufacturing process sheet.','CA/PA acceptable and next part found within acceptable limit.','','2018-05-15','pe_sez(a)','op_sez(s)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','01','no','Misc','pe_sez(a)','no','','RM SIZE CHECKING AND RUN','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10612,'35-456A','Saab AB','LATCH BRACKET','LL0102097','D522 73484 200 00','','PART ISSUE A',1,'OWED-LTA-002','','72763','1','2018-05-16',NULL,'no','yes','yes','yes','no','no','no','no','no','Part thickness undersized.','CLAMP WILL NOT PERPETUALLY CLAMPING  |Clamping of the part was not done properly to avoid to avoid the bend in the part.','TO CHECK PART AT RUNNING TIME MUST AND SHOULD |Informed the operator to ensure proper clamping of the part using feeler gauge before starting the cycle.','TO INFORM THE SUPERVISOR |Instructed the operators to maintain the thickness of the part in the maximum side in the First setup(OP-01)to avoid the deviation of the dimension when completing the machining on the other side(Op-03).','CAPA Found ok.','','2018-05-16','pe_sez(a)','pe_sez(a)','','2018-05-16','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','pe_sez(a)','no','','TO CHECK PART AT RUNNING TIME MUST AND SHOULD   |Stopped the machine and rechecked all the previously completed parts and found ok.','Z3456','qas|qas|','2018-07-27|2018-07-27|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10613,'35-456A','Saab AB','LATCH BRACKET','LL0090938','D522 73484 200 00','','PART ISSUE A',10,'OWED-LTA-002','','69199','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','no','Part Missed in ATPL.','Part missed at supplier end.|Supplier did not ensured the qty of the parts.|Supplier did not ensured the batch qty at each and every operation.','|Reject and debit note raised to the supplier.','|Supplier to ensure the batch qty after the completion of each and every operation.','Next batches found ok.','','2018-05-17','qas_sez(a)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','DN38625','POST DN','no','Misc','qas_sez(a)','yes','','|Information given to the supplier.','Z3456','qas|qas|','2018-07-24|2018-07-24|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10614,'18-423A','Magellan Aerospace(Blackpool) Limited','BRACKET','9768','PI201484604','','NIL',1,'BPP-533299','','72341','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Part hole ablong size by o.1mm ','part running time chips present in spindle so tool run out occur .','Every day 1st shift clean the ATC Arm and spindle ,','1.once a week clean the ATC Shutter and information pass the all 3 shift operator,\r<br/>2.TO every part setting time to check and ensure the m/c ATC arm and shutter door .','CA PA found Ok.','','2018-05-17','Gurukiran S(M)','ABHISHEK(M G)','','0000-00-00','Part hole over size ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','05','no','Misc','Gurukiran S(M)','no','','Clean the tool holder and spindle,ATC ARM ','E3456','Deshpande|','2018-07-25|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10615,'35-262','Saab AB','ROD-END','G24288K03','424Z3413-1','','--A',6,'1600218100','','72523','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Bore over size 0.02mm so part rejected ','Running time tool blunt so parts bore diameter (22.223 H7 ) Over size by 0.02mm ','To check the tool cutting edge and supply the Coolant properly by manually adjusting the coolant force and supply angle at setting time .','1.To give the proper training for operator ,\r<br/>2.Monitor to check the tool life for bore finish tool ','CA PA found ok.','','2018-05-17','Gurukiran S(M)','        SIDDESH()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','05','no','Misc','Gurukiran S(M)','no','','Change the bore finishing tool and run the program.','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10616,'51-050','THE BOEING COMPANY','BRACKET ','741191','149A7371-9624','NA','PSDL REV A',1,'BOEING 001P','','71098','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','during receiving inspection it was found that 51-046 was mixed along with 51-050.','While doing bench work the part work order was mixed.|The new fitters mixed up the work order unknowingly. As both the parts were similar to each other.','|Informed to all the fitting department to get approve individual CRN at a time. ','|Informed to all the fitting department to get approve individual CRN at a time.','CAPA found ok.','','2018-05-18','qas_sez(a)','qas_sez(a)','','0000-00-00','part mixup','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','yes','With Treatment','DN40025','POST TREATMENT','no','Misc','qas_sez(a)','no','','|Educate the fitter to make sure the identification of the part work order correctly. ','Z3456','pe_sez|qas|','2018-09-24|2018-09-27|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10617,'51-042','THE BOEING COMPANY','BRACKET','180534B0','149A7371-9604','','PSDL REV A',1,'BOEING 001C','','71369','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','While receiving inspection it was found that 51-044 mixed with 51-042','While doing bench work the part work order was mixed.|The new fitters mixed up the work order unknowingly. As both the parts were similar to each other.  ','|Informed to all the fitting department to get approve individual CRN at a time.','|Informed to all the fitting department to get approve individual CRN at a time.','CAPA found ok.','','2018-05-18','qas_sez(a)','qas_sez(a)','','0000-00-00','PART MIXUP','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','yes','With Treatment','DN39928','POST TREATMENT','no','Misc','qas_sez(a)','no','','|Educate the fitter to make sure the identification of the part work order correctly.','Z3456','pe_sez|qas|','2018-09-24|2018-09-27|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10618,'35-491','Saab AB','LINK','530221B1','D522 73527 200 00','','A',24,'PA1687 LTA-2','','73798','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Required 18.29H7 but Measured 18.265mm (0.025mm under size).','Due to part proving time not checking properly .|Next part check and correction given so part found ok|some instrumentation error is occur |correct training given to shift operator|Before removing the part cross check and remove component ','|CRC value constant for particular part given in 5.00','|we order to reamer on bore size found ok on next batch ','CAPA OK','','2018-05-18','Gurukiran S(M)','SIDDESH ,MANJE GOWDA S,DILIP G C ,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','','FI','yes','MakinoF5-1','Yashawantha(NH)','no','','|given training to operator','E3456','pe|nagendra|','2018-07-25|2018-07-30|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10619,'35-671','Saab AB','SHAFT LEVER ','443305 B','D5227346221800','NA','PART ISSUE D',1,'OWED-LTA-001','','74251','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','CHAMFER OVERSIZE.','For the proving purpose taken the CRN 35-672, 03 operation length undersized reject part and offset taken and prove out the bore diameter. next load the OK part in this CRN and not taken the Z offset so part chamfer was oversized. ','For the next part Re-offset taken and run the part.','For next any proving purpose we are not taking the NC part.','CA/PA Found satisfactory.','','2018-05-18','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','07','no','Misc','Ravi(M)','no','','For the next part Re-offset taken and run the part.','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10620,'35-672','Saab AB','SHAFT LEVER ','468065 B','D5227346221900','NA','PART ISSUE D',1,'OWED-LTA-001','','74253','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','total length undersize.','Total length not measuring correctly, so 0.7mm length extra moved in the work offset so total length was 0.7mm undersized.   ','Ensure the total length twice before move the length in work offset. ','Deburing the part and butting the part face by using the slip gauge and check the length in the height gauge then move the length in work offset.  ','CA/PA Found satisfactory.  ','','2018-05-18','Dinakar(K)','Ravi(M)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Ravi(M)','no','','0.7mm plus taken in the work offset and run the part.','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10621,'35-672','Saab AB','SHAFT LEVER ','468065 B','D5227346221900','NA','PART ISSUE D',1,'OWED-LTA-001','','74253','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','process problem.','This part contains many critical features.|There was 2 process for same part due to many critical features.|One process failed.|Process failed due to Critical dimension not achieved|Another process succeeded.','|Plan B process achieved Critical dimensions, So Plan A process was done Obsolete','|Continued Plan B process for Fair as well as for Production parts. ','CA PA Found ok.','','2018-05-18','Ramesh(Poojary)','Ramesh(Poojary)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','05','no','Misc','Gurukiran S(M)','no','','|Plan A process was replaced by Plan B process. ','E3456','cam|qas|','2018-08-06|2018-08-22|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10622,'44A-033','Saab AB','X- FIXATION ASSY','','E5347560300000','','A',2,'1600190066','','A15165','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','DUMMY','DUMMY','DUMMY','DUMMY','DUMMY','','2018-05-18','Ramesh(D)','Phaniraj(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','Assembly','','ASSY','no','Misc','Phaniraj(G)','no','72421','DUMMY','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10623,'44A-034','Saab AB','X- FIXATION ASSY','','E5347560400000','','A',2,'1600190066','','A15168','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','DUMMY','DUMMY','DUMMY','DUMMY','DUMMY','','2018-05-18','Phaniraj(G)','Ramesh(D)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','Assembly','','ASSY','no','Misc','Phaniraj(G)','no','72421','DUMMY','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10624,'35-118','Saab AB','ALCD_STRUCT_INTERCOSTAL_L','589751','423Z1178-3','7050-T7451 ALUMINUM ','--A',1,'Forecast po for B787','','71618','','0000-00-00',NULL,'yes','no','yes','no','yes','no','no','no','no','Base dig up to 1 mm.','When running time Z axis drop due to ground data fault alarm.','Clear that problem of rotary cable damage.','Haas service engineer give clearance to that problem then we run the machine. ','CAPA FOUND OK','','2018-05-18','prodn_aero(prodn)','prodn_aero(prodn)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Dinesh kulal()','no','','Stop the machine and inform to HAAS service engineer.','A3456','qas_aero|','2018-07-17|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10625,'35-229A','Saab AB','HINGE BRACKET 3','4754501 2','D576 50006 204','','D00',1,'1600223433/Forecast ','','73008','','0000-00-00',NULL,'yes','yes','yes','','','no','','','no','Dig mark on part.(on pocket side)','While running the production, base radius cutter dia 8 ball nose brokened, therefore dig mark observed on the part.\r<br/>','Tool life monitoring process to be strengthened and regularly monitor the same for the high volume parts(100nos/Batch qty)\r<br/>This will eliminate the sudden tool brakeage issues. ','Tool life monitoring process to be strengthened and regularly monitor the same for the high volume parts(100nos/Batch qty)\r<br/>This will eliminate the sudden tool brakeage issues. ','CA/PA found acceptable.','','2018-05-19','pe_sez(a)','        Diwakar R.B.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','1','','','','','','*Cross verified the tool tip and flute condition on the cutter.\r\n*Checked any over stock in the part for finishing tool.\r\n*Checked the tool holder, if any damage.\r\nNot found any deviations.\r\nReplaced with New tool and production started. ','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10626,'43-046','Composite Industrie','BLANKING PLATE ','720172 4A1','V2511255420000','NA','A00',1,'ATA25_ACH-7943','','74579','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','Tool dig on part center.','Trans cancel was not given at the end of interpolate program for dia 6.65 hole finish . Therefore tool ran in wrong location and the part got dig.','Check the program and gave trans cancel at the end of program for dia 6.65 hole finish and found the next part to be ok.','New tool dia 6.65dril will be ordered for this hole finish and the hole operation will be carried out with the drill only trans for the interpolate program will not be given in next production batches.','Tool Ordered and CA PA Found ok.','','2018-05-19','Subramanya L(Naik)','Sundar D.K.,Shivappa M B,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','1','no','BMV 45-1','Subramanya L(Naik)','no','','Check the program and trans cancel given at the end of interpolate program for dia 6.65 hole finish . next part found OK.','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10627,'51-126','THE BOEING COMPANY','BRACKET DETAIL','509851','332A2931-3','NA','PSDL REV -',1,'486998 MPP','','72961','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','WHEN DIA 16 FLAT ROUGH MACHINING TIME PART WAS LIFTED','Due to less Torque the part was lifted when \"i\" machining time ','The torque Grinch Nm value cross verified and correct reading stetted and Locked.  ','About Torque Grinch full awareness will give to all operators and training program will be arrange. |Specified torque value for the specific bolt chart will be displayed in the production floor.','CA PA Found ok.','','2018-05-20','pe_sez(a)','op_sez(s)','','0000-00-00','PART NOT CLAMPED PROPERLY','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','1','no','Misc','pe_sez(a)','no','','Production stopped. the Torque Grinch validated.  ','Z3456','qas|','2018-07-27|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10628,'47-110A','GKN Aerospace Filton','BLOCK COVER RH','7689502-1','D5725097420901','NA','PART ISSUE N',1,'GS68-LTA-2018','1','74358','1','2018-05-18',NULL,'no','yes','yes','yes','no','no','no','no','no','part will uncleared in 1st su  do not observed the part     ','r/m width will be minimum dimension so   ','adding the m00 command in program ','adding the m00 command in program to in from the supervisor  ','','','2018-05-20','pe_sez(a)','pe_sez(a)','1','2018-05-18','part uncleared  in fixture 1st set up b/c not clamping properly  ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','pe_sez(a)','no','','adding the m00 command in program  ','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10629,'35-457A','Saab AB','LATCH BRACKET','LL0102097','D522 73484 201 00','','PART ISSUE A',1,'OWED-LTA-002','1','72770','1','2018-05-19',NULL,'yes','yes','yes','no','no','no','no','no','no','Part was not clamped properly due to part profile was under sized.','CLAMPED THE PART SUITABLY AND CHECK WITH THE DIAL TO ENSURE THE PART WAS PROPERLY CLAMPED TO THE BUTTING SURFACE. ','INFORMED TO THE OPERATOR EVERY TIME LOADING THE PART ENSURE WITH THE DIAL PART WAS PROPERLY BUTTING TO THE BOTTOM SURFACE OF THE FIXTURE.','INFORMED TO THE OPERATOR EVERY TIME LOADING THE PART ENSURE WITH THE DIAL PART WAS PROPERLY BUTTING TO THE BOTTOM SURFACE OF THE FIXTURE. ','NEXT PART FOUND WITHIN ACCEPTABLE LIMIT.','','2018-05-20','op_sez(s)','op_sez(s)','1','2018-05-19','','F8003-S','Rev 0 dt 8-1-2009',0.00,'','Closed','no','yes','no','With Treatment','','03','no','Misc','op_sez(s)','no','','IN CLAMPING CONDITIONS TO CHECK THE PART AND SUTEBLE   CLAM WILL ARRANGE      ','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10630,'51-124','THE BOEING COMPANY','BRACKET ','659121','332A2930-88','NA','PSDL REV B',1,'486998 MPP','','72610','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','THICKNESS UNDER SIZED BY 0.18mm ','While part running part was lifted.Because clamping pressure was low','|After completing the roughing operation recheck the part butting with feeler gauge.','|Inform to operator to recheck the part butting with feeler gauge before running the finishing program. ','CA PA found ok.','','2018-05-21','pe_sez(a)','pe_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','Misc','qas_sez(a)','no','','|Stop the machine and re check the previous completed parts. ','Z3456','pe_sez|qas|','2018-07-27|2018-07-27|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10631,'51-124','THE BOEING COMPANY','BRACKET ','659121','332A2930-88','NA','PSDL REV B',2,'486998 MPP','','72611','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','thickness under sized by 0.18mm','While part running part was lifted.Because clamping pressure was low. ','|After completing the roughing operation recheck the part butting with feeler gauge. ','|Inform to operator to recheck the part butting with feeler gauge before running the finishing program. ','CAPA Found ok.','','2018-05-21','pe_sez(a)','pe_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','Misc','qas_sez(a)','no','','|Stop the machine and re check the previous completed parts. ','Z3456','pe_sez|qas|','2018-07-27|2018-07-27|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10632,'18-431A','Magellan Aerospace Wrexham','SPRING RETAINER ','CD703035/04952A','D321 40203 220','','L',2,'RP166211','','71034','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','OD Under size by 0.05mm','setting time micrometer error so od under size by -0.05mm.','micrometer set to zero and to be recheck with master before check the part.','next every setting time check the micrometer and after every part cross check the micrometer and run the part. ','Next Batches found ok.','','2018-05-21','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','Misc','Narasimha Murthy(R)','no','','zero set the micrometer and cross check the part in another micrometer and run the part.','E3456','qas|','2018-07-24|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10633,'18-110A','Magellan Aerospace Bournemouth','FORK END INTERMEDIATE ','CD701876/02368A','PID575 40494 202','','J',1,'423256','','74177','','0000-00-00',NULL,'yes','no','yes','no','yes','','','','','running time tool brack part dig mark.....','Machine displayed ATC time out alarm and after resetting wrong tool ran on the part. ','1) Switched off and switched on the machine and selected the correct tool as per the program requirement.\r<br/>','1) Informed the maintenance department regarding the alarm and caution given to operators to verify the tool selection if the alarm repeats.\r<br/>2) Machine maintenance supplier is called to attend the issue and to avoid repeating of issue.','Issues is addressed and no fault alarm has raised.','','2018-05-21','Anjinamurthy(H)','        Mallikarjuna D','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','07','','','','','','stopped the machine and checked the tool selected in the program.','E3456','qas|','2018-07-24|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10634,'35-457A','Saab AB','LATCH BRACKET','LL0102097','D522 73484 201 00','','PART ISSUE A',1,'OWED-LTA-002','1','72769','1','2018-05-17',NULL,'yes','yes','yes','no','no','no','no','no','no','WHEN PART CUT OUT TIME TOOL WILL BROKEN PART WILL DAMAGE ON TOP FACE ','WHEN THE RUNNING TIME  CARE FULL TO CHECK THE CLAMP AND RUNNING THE PART ','TO ENSURE THE CORRECT METHOD TO FLOWING NEXT RUNNING THE MACHINE   ','TO ENSURE THE CORRECT METHOD TO FLOWING NEXT RUNNING THE MACHINE   ','CA PA Found ok.','','2018-05-21','op_sez(s)','op_sez(s)','','2018-05-17','','F8003-S','Rev 0 dt 8-1-2009',0.00,'','Closed','no','yes','no','With Treatment','1','03','no','Misc','op_sez(s)','no','','WHEN THE RUNNING TIME  CARE FULL TO CHECK THE CLAMP AND RUNNING THE PART ','Z3456','qas|','2018-07-27|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10635,'51-045','THE BOEING COMPANY','BRACKET','741161','149A7371-9611','','PSDL REV A',1,'BOEING 001F','1','74298','1','2018-05-20',NULL,'no','yes','yes','yes','no','no','no','no','no','MACHINING TIME TOOL WILL BROKERED TOOL DIG MARK ON ON PART   ','   TO CHECK THE CORRECT METHOD OF FLOWING PROCESS FOR MACHINING TIME BE ALERT  |Tool worn out and got broken during the machining time.','IN RUNNING TIME NUMBER QUANTITY OF PRODUCTIONS TOOL BROKEN CHANCES IS THEIR TO CARE OF TOOL HEIGHT OF PERTIC0LOR PART ARE STAGE       |Informed the operator to check the life of the tool.',' TO CHECK THE CORRECT METHOD OF FLOWING PROCESS FOR MACHINING TIME BE ALERT  |ALL the operators are instructed to monitor the tool life of any new tool used in the machine.','CA PA Found ok.','','2018-05-21','op_sez(s)','op_sez(s)','1','2018-05-20','','F8003-S','Rev 0 dt 8-1-2009',0.00,'','Closed','no','yes','no','With Treatment','1','03','no','Misc','op_sez(s)','no','','IN RUNNING TIME NUMBER QUANTITY OF PRODUCTIONS TOOL BROKEN CHANCES IS THEIR TO CARE OF TOOL HEIGHT OF PERTIC0LOR PART ARE STAGE       |Stopped the machine and changed the new tool.','Z3456','qas|qas|','2018-07-27|2018-07-27|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10636,'35-464','Saab AB','FITTING','533635A2','D522 73408 201 00','','A',1,'OWED-LTA-001','','71129','','0000-00-00',NULL,'yes','yes','yes','','','','','no','','during operation mirror program not activated ','from mazak same program mooved to makino but in program mirror directions are there ps 105-2 mc mirror directions not activated during operation.','while programs are mooved  machine to machine on that time verify the mc specific directions like mirror activations and all.','while programs are moved to machine to machine on that time verify the machine specific directions like mirror activations and start the process.','CAPA found ok.','','2018-05-22','pe_sez(a)','        Kiran Kumar M','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','3','','','','','','on the spot inform to programmer, and stop the program.','Z3456','qas|','2018-07-27|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10637,'35-604','Saab AB','SHAFT , VENT HOOKS','2617','D5227352920200','NA','PART ISSUE B',1,'PA1687 LTA-1','','73803','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','total length under-size by -0.3mm.','part was not debarred and height was measured without checking the part whether it was debarred or not. then the part was inspected after the machining process and found that length was undersized.','each part will be debarred after  machining process and will be gauged.','to make sure that before loading each part the part will be thoroughly gauged and debarred.','Next batches found ok.','','2018-05-22','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Ravi(M)','no','','next part was debarred and inspected before loading onto the machine and the part was found OK.','E3456','qas|','2018-08-01|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10638,'35-231A','Saab AB','HINGE BRACKET 4 ','233915B8','D576 50007 208','','E00',1,'1600223433/Forecast ','','73011','','0000-00-00',NULL,'yes','yes','yes','','','no','','','no','part running time dia 8ball broken so part dig mark stage 01 op part reject.','part running time dia 8ball broken so part dig mark stage 01 op part reject.','For every batch quantities check the tool damage,life of tool and load to the machine.','For every batch quantities check the tool damage,life of tool and load to the machine.','CA/PA Acceptable.','','2018-05-22','pe_sez(a)','        Umesh B','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','1','','','','','','as per tool life decreasing and parameter should be changed','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10639,'35-412','Saab AB','BRACKET','531882E','D5227341220000','','A',2,'OWED-LTA-001','','73868','','2018-05-23',NULL,'yes','yes','yes','no','no','no','no','no','no',' machining time part will lifted so thickness will under size part rejected     ','to correct the program sequence to run the part care fully because part thickness 2.0 mm and 1.4   ','Training given to operator load and clamp as mentioned in the MPS carefully and run the machine.','Training given to operator load and clamp as mentioned in the MPS carefully and run the machine. ','CA/PA acceptable.','','2018-05-22','op_sez(s)','op_sez(s)','','2018-05-23','machine running time part will lifted thickness   will under size part will be reject      ','F8003-S','Rev 0 dt 8-1-2009',0.00,'','Closed','no','yes','no','With Treatment','','03','no','Misc','op_sez(s)','no','','to correct the program sequence to run the part care fully because part thickness 2.0 mm and 1.4  ','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10640,'18-090A','Magellan Aerospace Bournemouth','BUSH','CD702609/02618A','PID278 50164 200','','A',10,'423255','','72346','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','OD undersize 0.006 to 0.013 & ovality. *','Due improper coolent supply, chips cloted. *','Set coolent properly and run the production. ','Instructed operator to set the coolent properly before\r<br/>run the part.','CA PA found ok.','','2018-05-23','Dinakar(K)','Dinakar(K)','','0000-00-00','REJECTED','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','03','no','Misc','Dinakar(K)','no','','Set coolent properly and run the production. ','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10641,'35-475A','Saab AB','FRAME ','5386401 4','D5227338420100','NA','A',1,'OWED-LTA-001','','71186','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','base thickens under size by 0.16. ','Operator did not ensured the proper butting of part.','|Informed all the operator to ensure proper butting of the part before starting the cycle.','|Informed all the operator to ensure proper butting of part by using feeler gauge before starting the cycle.','Next batches found ok.','','2018-05-23','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','05','no','Misc','Anjinamurthy(H)','no','','|Immediately informed the operator to stop the machine and ensure proper butting of the part.','E3456','qas|','2018-08-09|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10642,'35-241','Saab AB','HANDLE','789426A4','425Z0634-2','','--C',1,'Forecast po for B787','','71671','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Outer profile wall dig 1mm.','Tool overhang mistake.','Entry the tool length inside the program.','Record the tool overhang file.Whenever next setting time we will observe that records.','CAPA FOUND OK','','2018-05-23','Dinesh kulal()','Manjunatha.S.T(M)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Ravi nayak()','no','','Correct the tool overhang.','A3456','qas_aero|','2018-07-17|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10643,'53-005','Triumph Aerostructures','STRAP ( STRG 5 & 6 )','510539','F572 50890 200 00','NA','PART ISSUE A',5,'LTA TRIUMPH 2018','','74653','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','DIG MARK FOUND ON PARTS','','','','THIS PROBLEM WILL NOT APPEAR IN FUTURE','','2018-05-23','Dhananjaya(N)','Paramaeshappa()','','0000-00-00','DIG MARK FOUND ON PARTS','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','Misc','Manu(P)','no','','CORRECTION OF PROGRAM FOR NEXT JOB','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10644,'28-016','Magellan Aerospace New York  Inc.','STOP FITTING','G23552K08','161A6119-1','15-5PH Per AMS 5659 ','N/C',1,'A000148797','','72409','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','Chamfer diameter oversize by 0.8mm.','For Hole diamter of 9.5 mm Drill bit of 9.6 mm diameter used in drilling machine for chamfer operation by manually holding the part in hand. ','1. Chamfer tool used.\r<br/>2.Awareness created among fitting persons by displaying an alert.','Only chamfer tool will be used to carry out chamfer operation.','CA PA found ok and next production batch found ok.','','2018-05-23','Irappa(Badiger)','Irappa(Badiger)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','7','no','Misc','Irappa(Badiger)','no','','Stopped the Machine and chamfer tool used for next parts.','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10645,'35-138','Saab AB','FLCD_DS_SUPPORT_DEFLECT_S','7560319','423Z6189-3','BAC1534-62C','---',1,'Forecast po for B787','','72687','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Profile not finished ','In coming RM Problem ','Next time informed to stores to give the RM ,To inspect properly  .','check the all RM  to take the before production  ','CAPA Found OK','','2018-05-24','Dhananjaya(N)','Raj Kumar,Narasimhamurthy C,dharshan d,Dhananjaya N,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','FI','no','VM2-3','Nagendra(SN)','no','','check the all parts and run the m/c ','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10646,'51-035','THE BOEING COMPANY','BRACKET','741191','149A7371-961','','PSDL REV A',1,'BOEING 001E','','71876','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Parts received from treatment were found paint damage at the edges and corners.','This is happen during the transportation as there was no safety in the inner layer of the box in which the parts were shipped','Parts were done manual touch up as per the specification and found ok','Instruction was given to the treatment house on packaging to put extra kushan type of material surronding the inner layer of the box to avoid such paint damages during the transportation.','Next Lot Received from the treatment supplier ,parts were checked and found visually acceptable to the requirement','','2018-05-24','qas_sez(a)','qas_sez(a)','','0000-00-00','PART MIX UP','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','With Treatment','DN40170','POST TREATMENT','no','Misc','qas_sez(a)','no','','parts were identified and segregated and the same was communicated to the treatment house','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10647,'35-589','Saab AB','BEAM','526168A2','D5227341020200','NA','PART ISSUE B',1,'PA1687 LTA-1','','73848','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Outer wall thickness less than requirement.','Part lifted in vice in 01 operation.','Guide the all operator to about part lifting in vice.','We are take care about this problem.and we are take care of the part lifting issue.','CAPA FOUND OK','','2018-05-25','prodn_aero(prodn)','Manjunatha.D()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Manjunatha.D()','no','','Guide the operator about part lifting in vice.','A3456','qas_aero|','2018-07-17|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10648,'47-183','GKN Aerospace Filton','TEE T/E RIB 5B OTBD','9753201','F57551281202','NA','PART ISSUE D',1,'1210042824','','74727','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','THICKNESS UNDERSIZE UPT 0.08MM','Due to part face polished part dimension undersized. |due to part face got chattering |due to vibration of wall|due to Tool overhang(outside of holder)|To avoid the fixture collision. ','|Changed the tool holder then rerun the same program part got OK.|Changed the tool holder then rerun the same program part got OK.','|we will advise the operator to use the length holder while A90 and A-90 side machining.|we will advise the operator to use the length holder while A90 and A-90 side machining.','Next part found within acceptable to the drawing requirements.','','2018-05-25','pe_sez(a)','pe_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','Misc','qas_sez(a)','no','','|Changed the tool holder then rerun the same program.|Changed the tool holder then rerun the same program.','Z3456','||cam|qas_sez|qas_sez|','2018-09-08|2018-09-08|2018-09-08|2018-09-08|2018-09-08|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10649,'47-184','GKN Aerospace Filton','TEE T/E RIB 5B OTBD','9753201','F57551281203','NA','PART ISSUE D',1,'1210042824','','74730','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','THICKNESS UNDERSIZE UPTO 0.08MM\r\n','Due to part face polished part dimension undersized.|due to part face got chattering|due to vibration of wall|due to Tool overhang (outside of holder)|To avoid the fixture collision.','|Changed the tool holder then rerun the same program part got OK.','|we will advise the operator to use the length holder while A90 and A-90 side machining.','Next part found within acceptable to the drawing requirements.','','2018-05-25','pe_sez(a)','pe_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','Misc','qas_sez(a)','no','','|Changed the tool holder then rerun the same program.','Z3456','cam|qas_sez|qas_sez|','2018-09-08|2018-09-08|2018-09-08|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10650,'35-627','Saab AB','LEVER','5378401 1','D5227331720300','NA','B',2,'OWED-LTA-004','','70475','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','part profile shifted ','Part profile shifted during the first off part proving time.|Wrong work offset given.|Operator entered 0.25 instead of 0.025 in the machine. |Operator typing error and he did not cross checked before starting the cycle.','|Remeasured the work offset and entered the correct value.','|Informed all the operator to cross check the offset values before starting the cycle.','Next batches produced by the operator found ok.','','2018-05-25','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','profile miss match ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','05','no','Misc','Rakeshbabu(V)','no','','|Immediately stopped the machine and cross checked the work offset of all the tools and corrected the wrongly entered ones.','E3456','qas|qas|','2018-09-05|2018-09-05|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10651,'07-004C','HAL-NASIK','WALL 2 ROOT PART - LH ','AS-28214','11.2000.2.111.002','','11.2000.2.111.001;002 Iss 01',1,'NK/M/2513(4520)/MP/O','','73154','','0000-00-00',NULL,'yes','','yes','','yes','','','','no','B axis angle tilted so outer wall and dia 8H9 holes 0.5mm shifted.\r\nAs per drawing wall thickness 5mm on the part measured at 5mm.\r\n(maintain the wall thickness 5.5 to 5.6mm)','while running time machine monitor got hanged so machine main has been switched OFF AND ON after that machine B axis angle got variation automatically..  |while running time machine monitor got hanged so machine main has been switched OFF AND ON after that machine B axis angle got variation automatically..|while running time machine monitor got hanged so machine main has been switched OFF AND ON after that machine B axis angle got variation automatically..  \r\n<br/>|while running time machine monitor got hanged so machine main has been switched OFF AND ON after that machine B axis angle got variation automatically..  \r\n<br/>\r\n<br/>\r\n<br/>','when ever machine got switched off and on every time B axis angel will be checked and the mandrill has been kept near the machine only to check the angle when ever machine got switched OFF and ON and for every operator instruction has been give to check the angel in every machine.','As per service engineer guidance the monitor cable and encoder of B axis has been decided to be replaced|As per service engineer guidance the monitor cable and encoder of B axis has been decided to be replaced|As per service engineer guidance the monitor cable and encoder of B axis has been decided to be replaced\r<br/>\r<br/>As per service engineer guidance the monitor cable and encoder of B axis has been decided to be replaced|As per service engineer guidance the monitor cable and encoder of B axis has been decided to be replaced\r<br/>\r<br/>\r<br/>\r<br/>','CA PA found ok part accepted by customer.','','2018-05-25','Narayanappa(G)','        Paramesh K','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','','no','','','03','','','','','','immediately informed to supervisor and supervisor called the DMG service engineer until that machine has been stopped later on the service engineer came and solved the problem..  ','E3456','pe|pe|pe|qas|qas|','2018-06-28|2018-07-01|2018-07-01|2018-07-02|2018-09-05|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10652,'35-426','Saab AB','BRACKET','704718','D522 73394 200 00','','A',1,'OWED-LTA-001','','73947','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Outer wall unclear. length less than requirement.','Butting wrong done by operator.','guide the operator about RM size variations.','we are all discus about this problem and concluded to fix the 1 off part in minimum gap to fixed jaws side.','CAPA FOUND OK','','2018-05-25','prodn_aero(prodn)','Lakshmi(Narasimha)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','01','no','Misc','Dinesh kulal()','no','','Take the again y work offset and the run the part.','A3456','qas_aero|','2018-07-17|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10653,'35-233A','Saab AB','HINGE BRACKET 5 ','233915B8','D576 50008 208','','D00',3,'1600223433/Forecast ','','74832','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Chattering mark is observed in Bore','Parts are running By the FMS. When Boring bar running time Chips are locked with Boring Bar. The bore\'s finished Surface was rubbed by the Chips.','Boring bar\'s insert changed. Coolant Flow increased by Cleaning of Coolant Motor and Filters.','The insert\'s cutting edges to be verify each and every FMS cycle start. Coolant flow pressure increased by the M code. when pressure fell Down the machine intimate the alarm. ','Next batches found ok.','','2018-05-26','Lohith(K)','        Nataraja C V','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','03','','','','','','Production stopped. completed parts are 100% inspection Done. no Error Found.','Z3456','qas|','2018-09-05|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10654,'35-456A','Saab AB','LATCH BRACKET','LL0102097','D522 73484 200 00','','PART ISSUE A',17,'OWED-LTA-002','1','72764','','2018-05-25',NULL,'yes','yes','yes','no','no','no','no','no','no','ZERO POINT SYSTEM  BUSS A AND B PIN M8 BOLTS TOP ON THE FIXTURE PART NOT CORRECTLY SUITED SO 17 NOS REJECT.','In setting process part did not clamped properly to the fixture and the operator continued the production without inspecting the parts so parts got rejected.','Stopped the machine and informed the operator to check all the completed parts and changed the zero point fixture bolt to the appropriate length and continued the production.','1) Informed all the operators to ensure proper butting of the fixture and parts before starting the production and to carry out new part setting only in the presence of senior operator.\r<br/>2) Informed all the operators not to continue production till first off clearance is given. ','NC Analyzed refer 5-Why.','','2018-05-26','op_sez(s)','op_sez(s)','','2018-05-25','ZERO POINT SYSTEM  BUSS A AND B PIN M8 BOLTS TOP ON THE FIXTURE PART NOT CORRECTLY SUITED SO 17 NOS REJECT   ','F8003-S','Rev 0 dt 8-1-2009',0.00,'','Closed','no','yes','no','With Treatment','','03','no','Misc','op_sez(s)','no','','TO INFORM THE SUPERVISORS AND CHECK THE FIXTURE THEN LOAD THE PART CORRECTLY   LOAD AN THE FIXTURE  THEN RUN THE PROGRAMS ','Z3456','qas|','2018-07-24|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10655,'35-233A','Saab AB','HINGE BRACKET 5 ','233915B8','D576 50008 208','','D00',1,'1600223433/Forecast ','','74832','','0000-00-00',NULL,'yes','yes','yes','','','','','','','part running time bore chattering so part line mark so reject..','Parts are running By the FMS. When Boring bar running time Chips are locked with Boring Bar. The bore\'s finished Surface was rubbed by the Chips.','Boring bar\'s insert changed. Coolant Flow increased by Cleaning of Coolant Motor and Filters. ','The insert\'s cutting edges to be verify each and every FMS cycle start. Coolant flow pressure\r<br/>increased by the M code. when pressure fell Down the machine intimate the alarm. ','CAPA found ok.','','2018-05-26','Lohith(K)','                Umesh B','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','03','','','','','','Production stopped. completed parts are 100% inspection Done. no Error Found. ','Z3456','qas|','2018-09-17|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10656,'18-069C','Magellan Aerospace Bournemouth',' 	M/C BRKT FWD WX 1727.0 ','10030','PID575 40237 200','','N',1,'423256','','74175','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Thickness under size 0.24 mm','Raw material taper not observed during first setup of milling operation. So the next setup of operation taper occurred. Due to that taper on part thickness under size occurred in one edge.','During first set up of operation raw material to be check and then load to the machine. Then that it to be ensure via face cleaning.','The raw material is getting from conventional machining that to be check their itself.','Next batch found ok.','','2018-05-27','Dhananjaya(N)','Prashanth Kumar M,Girish MS,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','FI','no','MAKINO SLIM-1','Narasimha Murthy(R)','no','','The remaining parts dimensions were checked and conforms taper not occurred.','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10657,'18-119B','Magellan Aerospace Bournemouth',' 	HOUSING OUT B DRG 3 ','1573705-1/QD84','PID275 40011 200','','D01',1,'423253','','72215','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','OD Groove width 0.12mm over size so part rejected,','The raw material issued was supplied with different length in RM and was separated length wise without identification. The second shift operator without measuring the length loaded the part and completed the production cycle later after seeing the face unfinished he re-passed the facing cycle to clear the face by shifting the work offset. due to which the groove width got oversize.','Before starting the production. All the operator\'s are instructed to ensure the length of the RM before running the part.','1) In program Alert Massage (ENSURE THE RM LENGTH) is Included.\r<br/>2) Total length of the part in RM Stage will be mentioned on both the face of the RM to identify easily.','Effectiveness of the operator to be measured refer 5Why.','','2018-05-27','Dinakar(K)','Santhosh Kumar(N)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','05','no','Misc','Raghavendra Rao(R)','no','','checked the finish parts and found OK.','E3456','qas|qas|','2018-07-09|2018-07-24|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10658,'35-234A','Saab AB','HINGE BRACKET 5 ','233915B8','D576 50008 209','','D00',1,'1600223433/Forecast ','','73014','','0000-00-00',NULL,'yes','yes','yes','','','','','','','bore running time chattering so bore line mark part reject.','Parts are running By the FMS. When Boring bar running time Chips are locked with Boring Bar. The bore\'s finished Surface was rubbed by the Chips.','Boring bar\'s insert changed. Coolant Flow increased by Cleaning of Coolant Motor and Filters. ','The insert\'s cutting edges to be verify each and every FMS cycle start. Coolant flow\r<br/>pressure\r<br/>increased by the M code. when pressure fell Down the machine intimate the alarm. ','CAPA found ok.','','2018-05-28','Lohith(K)','        Umesh B','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','03','','','','','','Production stopped. completed parts are 100% inspection Done. no Error Found. ','Z3456','qas|','2018-09-17|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10659,'35-671','Saab AB','SHAFT LEVER ','443305 B','D5227346221800','NA','PART ISSUE D',1,'OWED-LTA-001','','74255','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','part outer wall under size','while reducing the cycle time, the feed was increased due to which chattering and the part was dig. ','hence the program will not be changed, and will run as per the given program.','the process will be changed. since there is no support for the part while running.','','','2018-05-29','Gurukiran S(M)','Manohara M,Govindraju NR,Basavaraja S. Jr.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','7','no','VMC 70L','Narayanappa(G)','no','','the feed rate was changed to the previous program.','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10660,'35-671','Saab AB','SHAFT LEVER ','443305 B','D5227346221800','NA','PART ISSUE D',1,'OWED-LTA-001','','74255','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','part outer wall under size,','while reducing the cycle time, the feed and RPM was increased due to which chattering and the part was dig.','The program will not be edited to reduce any cycle time and hence run the given program.','The rejection was discussed with the CAD team and the program sequence changed and proved fair part .found ok','FAIR part Production done and part found ok.','','2018-05-29','Gurukiran S(M)','Manohara M,Govindraju NR,Basavaraja S. Jr.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','7','no','VMC 70L','Narayanappa(G)','no','','the edited program was replaced with the older one.','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10661,'53-008','Triumph Aerostructures','STRAP ( STRG 4 )','510539','F572 50890 206 00','NA','PART ISSUE A',3,'LTA TRIUMPH 2018','','74654','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','DIG MARK FOUND ON PART','','','','this problem will not appear in future','','2018-05-29','Dhananjaya(N)','Kammar(Nagaraj)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','Misc','Manu(P)','no','','Informed operator to clamp the job correctly henceforth','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10662,'35-623A','Saab AB','SHAFT 2','515372B','D5227280820000','NA','PART ISSUE A',1,'OWED-LTA-004','','74648','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Running time part was broken..','For the purpose of reducing the cycle time editing the program feed rate and rpm so running time part was broken.      ','For next part increase the Cv by step by step and reduced the cycle time. ','Next any CRN for decreasing the cycle time we are start the Cv in minimum side and set the program. ','\r\nCA PA found ok and next production batch found ok. ','','2018-05-29','Dinakar(K)','Dinakar K,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','5','no','QT100S-1','Dinakar(K)','no','','decrease the rpm and feed rate and run the production. ','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10663,'47-119A','GKN Aerospace Filton','TOP SPREADER PLT M/C ','6359202','F57451570200','NA','PART ISSUE B',1,'GS68-LTA-1-2018','','74893','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','part profile dig mark\r\n\r\n','whale program running time tool broken|During Outer wall finishing program,the lug rotated and tool dig mark occurred.\r\n\r\n|The bolt length selected was equal to thread length in the lug|operator not select the correct length bolt.\r\n|operator was not aware about the proper bolt length to be used','|proper bolts changed and continue the production.','|informed all the operators to use bolt of length 10mm greater then the part thickness.','CA PA found Ok.','','2018-05-29','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Narayanappa(G)','no','','|all proves part cross cheeked and all the parts are ok.','E3456','pe|qas|','2018-07-31|2018-07-31|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10664,'35-473A','Saab AB','LEVER CAM','B76735','D522 73537 200 00','','PART ISSUE A',1,'OWED-LTA-003','','72647','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','POWER TRIP OD DIG MARK.','POWER TRIP ,UPS PROBLEM ','SUPERVISOR ENSURED PROPER FUNCTIONING OF MACHINE AFTER THE RECOVER FORM POWER FAILURE','MAINTENANCE TEAM REPLACED THE UPS EARTHING UNIT.','CA PA found ok.','','2018-05-29','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','01','no','Misc','Raghavendra Rao(R)','no','','MACHINE STOPPED , UPS GOT FIRED AND WENT OUTSIDE TO OFF THE FIRE ','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10665,'51-045','THE BOEING COMPANY','BRACKET','741173','149A7371-9611','','PSDL REV A',1,'BOEING 001F','','71921','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Parts received from treatment were found paint damage at the edges and corners.','This is happen during the transportation as there was no safety in the inner layer of the box in which the parts were shipped','Parts were done manual touch up as per the specification and found ok','Instruction was given to the treatment house on packaging to put extra kushan type of material surronding the inner layer of the box to avoid such paint damages during the transportation.','Next Lot Received from the treatment supplier ,parts were checked and found visually acceptable to the requirement','','2018-05-30','Murali(M)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','DN40098','POST TREATMENT','yes','Misc','qas_sez(a)','no','','parts were identified and segregated and the same was communicated to the treatment house','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10666,'51-042','THE BOEING COMPANY','BRACKET','741173','149A7371-9604','','PSDL REV A',1,'BOEING 001C','','71898','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Parts received from treatment were found paint damage at the edges and corners.','This is happen during the transportation as there was no safety in the inner layer of the box in which the parts were shipped','Parts were done manual touch up as per the specification and found ok','Instruction was given to the treatment house on packaging to put extra kushan type of material surronding the inner layer of the box to avoid such paint damages during the transportation.','Next Lot Received from the treatment supplier ,parts were checked and found visually acceptable to the requirement','','2018-05-30','Girish(d)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','DN40276','POST TREATMENT','yes','Misc','qas_sez(a)','no','','parts were identified and segregated and the same was communicated to the treatment house','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10667,'35-481A','Saab AB','LOCK LEVER','C90875','D5227349820100','NA','PART ISSUE B',1,'OWED-LTA-003','','73793','','0000-00-00',NULL,'yes','no','yes','','yes','','','','','OD dig mark.','power cable connector fault so machine was tripped and part was rejected.','MAINTENANCE TEAM REPLACED THE cable connector.','MAINTENANCE TEAM REPLACED THE cable connector.','CA/PA Found satisfactory.','','2018-05-30','Dinakar(K)','        GUNDEGOWDA H.G.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','05','','','','','','machine stopped inform to maintenance team . ','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10668,'34-064','Magellan Aerospace Winnipeg','PIN SHEAR ACCESS DOOR','429596','400-12748-1','','EM105092 Iss G,EM104765 Iss G',1,'C46695 Rev.004','','74952','','2018-05-31',NULL,'yes','yes','yes','no','no','no','no','no','no','Total length under size......','Offset for the finishing tool was not given.','1)Entered correct offset to the tools and cross verified the same for all the tools.\r<br/>2)Instructed all the operators to check the tool offset twice before starting the production.','While first part running time ON the single block and cross verified the tool offset and prove out the parts and avoid such type of mistakes. ','CA PA Found ok.','','2018-05-30','Dinakar(K)','Dinakar(K)','','0000-00-00','Total length under size......','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','5','no','Misc','Seetharamu(D)','no','','Immediately stopped the machine and changed the tool offset.','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10669,'35-597','Saab AB','CORNER','529436A','D5227338620200','NA','PART ISSUE B',1,'OWED-LTA-001','','70893','','0000-00-00',NULL,'yes','no','yes','no','yes','no','no','no','no','part slot over size while running in 5 Axis .','machine parameter vary with actual parameter and kinamatic parameter .','Laser calibration and machine service done Jyoti m/c team','Every 3 months preventive maintenance done.','Maintenance record to be monitored.','','2018-05-30','Gurukiran S(M)','Govindraju(NR)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','05','no','Misc','Gurukiran S(M)','no','','stop the production and informed to maintenance team .','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10670,'35A-351A','Saab AB','Lift Actuator Support Fit','','423Z1223-1-50','','---',4,'787 Forecast','','A14528','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','yes','Is condition: Poor workmanship on touch-up on all parts around the bushings, too much paint, no paint and FOD in paint. Small nicks with bare metal on edge of some parts.\r\nShould be: Touch-up shall be smooth and evenly distributed and NO FOD allowed. No nicks and no bare metal allowed.\r\n\r\nThis issue is repeated in below parts also.\r\n1) w/o no: A14183, S/N: 1712 - 1731, Quantity: 20 pcs.\r\n2) w/o no: A14527, S/N: 1732 - 1755, Quantity: 24 pcs.','1) Inadequate knowledge on the requirements.\r\n<br/>2) Sufficient lighting source was not used to carry out visual inspection.','All similar parts are reinspected to ensure proper coverage and skip of part-marking overcoat.|','1) Quality Engineer to provide training to the assembly personnel on the customer and standard requirements on 21-Jun-2018.\r<br/>2) All the inspectors are instructed to carry out visual inspections only under dedicated tables with proper light source and this was put to be effective from 1-Jun-2018.|','Next batch found ok.','C64359','2018-05-31','qas_sez(a)','qas_sez(a)','OF-003033','2018-05-29','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','yes','Assembly','','CUST END','no','Misc','qas_sez(a)','no','','100% re-check is done on below area:\r\n1) Warehouse inventory (0 pcs)\r\n2) Products in production inkl. final inspection (0psc), \r\n3) Finished goods (0 psc).\r\nResults: No parts were affected as there was no parts in process.|','Z3456','qas|','2018-08-07|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10671,'35-308A','Saab AB','RIB INTER 3','783005A2','F575 54797 201 00','','SCH-ISSUE B, PART ISSUE A',2,'A330 NEO FORECAST -2','','67015','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','yes','Is conditon: RIB INTER 3 is marked F5755479720100\r\nShould be: F5755479620100\r\n\r\nThe part is marked with F5755479720100 and shipped to Saab as such. But the part is acctually a F5755479620100.','Checking gauges to ensure difference in profile was not effective.','Profile dimension of all the parts was verified manually using vernier during the receiving inspection before conforming to dispatch.|','Quality inspector to ensure the part profile by matching a template over the part while carrying out the receiving inspection and this will be effective from 23-Jun-2018.|','Next Batches found ok.','C63204','2018-05-31','qas_sez(a)','qas_sez(a)','OF-003034','2018-05-29','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','yes','With Treatment','DN36699','CUST END','no','Misc','qas_sez(a)','no','','100% re-check is done on below area:\r\n1) Warehouse inventory (13 pcs)\r\n2) Products in production inkl. final inspection (0 psc), \r\n3) Finished goods (13 psc).\r\nResults: 0 pcs out of toatal 13 pcs is found with similar nonconformance.|','Z3456','qas|','2018-08-07|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10672,'53-029','Triumph Aerostructures','SPREADER PLATE BOTTOM','755621','F574 55033 200 A02','NA','PART ISSUE A, ECN PG49999ST1KZ41',2,'LTA TRIUMPH 2018','','74680','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','dig mark found on part ','','','','this problem will not appear in future','','2018-05-31','Dhananjaya(N)','Kammar(Nagaraj)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','Misc','Manu(P)','no','','informed operator to clamp the job correctly henceforth','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10673,'34-055','Magellan Aerospace Winnipeg','BRACKET, AFT MOUNT-APU','G22697','400-12611-1','','EM105092 Iss G,EM104765 Iss G',1,'C46695 Rev.004','','74953','','0000-00-00',NULL,'yes','yes','yes','','','','','','',' \"D\" Value wrong correction ','|profile dig mark.','1.In CRC program tool and diameter number should be same, but machine operator was forget. |2.Supervisor given the instruction before running.because as same problem repeatedly occur with all operator |3.Operator was telling that I should be load the tool as same in the program.|4.Diameter value wrongly entered in program.','|1.correction give in D value enter & further part found ok.\r<br/>\r<br/>2.instruction to operator for checking \"D\" value before running on part.\r<br/>\r<br/>3. Training to operator  explain  \"D\" value & \"D\" program.','Effectiveness found ok.','','2018-05-31','Dhananjaya(N)','dharshan','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','07','','','','','','m/c stop|correct \"D\" value enter,','E3456','|qas|','2018-06-29|2018-07-03|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10674,'43-017','Composite Industrie','BRACKET','8790201 1','V251 11622 200','','A00, ECN PV100298ST1AD69',2,'LTA PO-2','','72805','','0000-00-00',NULL,'yes','no','yes','no','yes','no','no','no','no','Part profile -side','Due to Machine X axis repeat ability problem due to loose connection between the X axis motor connecting cable and the NC controller.','Given the machine to maintenance department to maintenance.After maintenance the machine connections were checked and the relevant parameters in the machine are corrected and the next part found OK.','Given the information to  maintenance department to check the connection cables and machine parameters of the machine after completion of every preventive maintenance. ','CA PA found OK. Preventive maintenance record to be monitored. ','','2018-05-31','Subramanya L(Naik)','Subramanya L Naik,Shivappa M B,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','3','no','BMV 45-1','Subramanya L(Naik)','no','','Stop the machine check the axis repeat-ability.','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10675,'51-046','THE BOEING COMPANY','BRACKET','741183','149A7371-9612','','PSDL REV A',1,'BOEING 001F','','74270','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','TOOL DIG MARK','Due to more in the roughing operation at the one corner, the finishing tool dia 12*3.18 bull nose make dig mark|Due to more stock left in the roughing operation at one corner the finishing tool damaged the part.','Semi finish NC program added for Re roughing. After that finished program was run. ','More stock area for the finishing tool should be identified. In that areas a semi fishing NC program to be add.  ','CA PA Found ok.','','2018-06-01','pe_sez(a)','op_sez(s)','','0000-00-00','Dig Mark','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','1','no','Misc','pe_sez(a)','no','','Production stopped. completed parts are checked. Found ok.','Z3456','qas|','2018-08-01|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10676,'18-411A','Magellan Aerospace Wrexham','PLUNGER','734875','D321 40205 200','','H01',1,'RP166210','','72103','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Vardex OD threading insert trial time effective diameter was under sized  so part rejected','Part ran by untrained operator without permission.','Corrected the thread height and continued the production.','Instruction given to all the operator about the parameters to be ensured while carrying out threading.','CA PA found ok.','','2018-06-01','Raghavendra Rao(R)','Ashoka(R)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','07','no','Misc','Raghavendra Rao(R)','no','','Stopped the machine and checked all the threading parameters.','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10677,'35-479A','Saab AB','SHAFT','B76570','D5227336520000','NA','PART ISSUE B',4,'OWED-LTA-004','','73343','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','OD UNDER SIZE BY -.013MM.','While running coolant not adjusted so due to wear out of\r<br/>insert OD under size.','Instructed to operator for checking coolant for every tool and check insert wear out regularly.','Instructed to operator for checking coolant for every tool and check insert wear out regularly.','CA/PA Found satisfactory.','','2018-06-01','Dinakar(K)','Ugraiah()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','05','no','Misc','Sathish(G)','no','','Change the insert corner and re-offset taken and run the part','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10678,'47-105A','GKN Aerospace Filton','TOP LUG MACHINED','1010901 1','D57550243200','NA','PART ISSUE A',1,'GS68-LTA-2018','','73699','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Y axis work offset wrong taken.','while stating condition y axis offset given manually by new operator during training period. ','1) Maintain the offset books correctly for all machines.\r<br/>','Training will be provided to all new operators on tool and work offset briefly.','Next batches found ok.','','2018-06-01','pe_sez(a)','pe_sez(a)','','0000-00-00','Y axis workoffeset wrong taken','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','1','no','Misc','pe_sez(a)','no','','maintain the offset books correctly and to trained the new operators and explain about tool offsets and work offsets briefly.','Z3456','qas|','2018-07-31|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10679,'34-015B','Magellan Aerospace Winnipeg','MOUNTING LUG- STRUT / STD','G22016K07','400-12607-1-905','','EM104302 Iss A, EM104765 Iss G, EM105092 Iss F, EM106399 Iss B, EM106400 Iss B, EM106401 Iss A, EM106404 Iss A, EM106522 Iss A, EM106602 Iss A',1,'B91379 Rev.026','','73994','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Bore over size ,0.06mm','wrong CRC given 0.03micron instead of 0.003micron. ','Information given to the all three shift operator .','Training given to the all the operator .','Operator Effectiveness to be measured regularly.','','2018-06-02','Gurukiran S(M)','SIDDESH()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','7','no','Misc','Gurukiran S(M)','no','','check the bore diameter and give the CRC Correctly,And check the all parts found OK.. ','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10680,'51A-032','THE BOEING COMPANY','BRACKET ASSY','','149A7371-42','','PSDL REV A',1,'BOEING 001H','','A15409','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','DIG MARK ON TEFLON COAT','1.The Teflon paint chip off surrounding the rivet during pressing the rivet|2.During pressing the rivet metal to metal contact|3.In butting block the  area where the parts were butting while riveting was not uniform |4.FOD of rivet accumulated in the butting block where the part was getting butted.','|1.Butting block was made uniform by giving a uniform cut','|1.Instruction given to operator to Change the adhesive tape frequently and clean the area where the parts gets butted before pressing the rivet','Next batch wo number A15411 assembly Completed and found ok,no evidence found for paint getting chipped','','2018-06-02','pe_sez(a)','pe_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Assembly','','FI','no','Misc','qas_sez(a)','no','','|1.Adhesive tape was appiexed on the butting block to avoid metal to metal contact','Z3456','qas_sez|','2019-01-06|','2019-01-06',NULL,NULL,NULL,NULL,NULL,NULL),(10681,'47-108A','GKN Aerospace Filton','BRACKET STRUT','1010901 2','D36150037201','NA','PART ISSUE C',1,'GS68-LTA-2018','1','74736','','2018-06-01',NULL,'yes','yes','yes','no','no','no','no','no','no','hole Dia. 9.525mm measures 10.00mm.','while doing back side chamfer for Dia 9.525mm hole. this hole got over size by 0.5mm.\r\n<br/> ','Maintain the reference books and mention the special tools function very clearly in all machines.','To train the operators and explain about special tools and their operations and to supervise their performance for continuous 10 batches of production.','Next Batches found ok.','','2018-06-02','op_sez(s)','Shivaraj K S,Lohith K,Kiran KM,','','2018-06-01','hole Dia 9.525mm measures 10.00mm.','F8003-S','Rev 0 dt 8-1-2009',0.00,'','Closed','no','yes','no','With Treatment','','3','no','Slim3n-4AHS-2','op_sez(s)','no','','maintain the reference books and mention the special tools clearly. and train the operator about special tools and their operations.','Z3456','qas|','2018-07-31|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10682,'35-600','Saab AB','FRAME','533394B','D5227338520400','NA','PART ISSUE C',1,'PA1687 LTA-1','','73959','','0000-00-00',NULL,'yes','no','yes','no','yes','no','no','no','no','Outer part profile tool dig mark.','During final operation in the machine an alarm of Z Axis serial date communication fault was displayed because of that Z Axis came down so the part was rejected. ','Informed to the service engineers they came and checked all the machine parameters and said that their is a fault in Z axis cable,and it was replaced by a new one.   ','The machine will be stopped as soon as alarm is displayed and we instructed the service engineer to check the cable every preventive maintenance.','CA PA Found Ok.','','2018-06-03','Narayanappa(G)','Rajesh B D,Mohan Kumar C.M.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','5','no','HAAS VM6','Narayanappa(G)','no','','Previously finished parts has been checked and all the parts are ok','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10683,'18-375B','Magellan Aerospace Bournemouth','GAMMA FITTINGS','8651','NSA840020-100PF','','L',3,'423231','','70059','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Out of inspection of 100No\'s of part no NSA840020-100 a Qty. of 3 No\'s is rejected due to observation of Part marking Invisibility, scratches, unapproved rework, unclear rear face, unclear front face, & Improper masking.','','','','','','2018-06-03','qas_sez(a)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','DN37452','POST DN','no','Misc','qas_sez(a)','no','','','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10684,'18-295A','Magellan Aerospace Bournemouth','BOLT','1573451-2/Q8C3','PID577 56145 200','','A',1,'423258','','67092','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','yes','1 off Bolt- Spoiler Jack part number PID577 56145 200 supplied with 0.75\"-20 UNJEF  class 3A thread missing.','1) Communication lapse between operators during shift change (becaose the overlap period was very minimal)\r<br/>2) Planning to carry out inspection activity was ineffective.||','1) Operators are instructed to move parts from one area to the other with proper identification and to store finished and semi-finshed parts in separate trays.\r<br/>2) Only one inspector is involved for one part no irrespective of batch qty.||','1) Special trays are to be ordered which allows to hold the part in up side down condition which helps the operator to identify missing of operation and also to avoid further skips.\r<br/>2) Tin Soldier visual technique to be implemented to improve the visual inspection technique.||','Next batch produced found ok.','C61419','2018-06-03','qas_sez(a)','qas_sez(a)','RDN 01949','2018-05-31','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','CUST END','no','Misc','qas_sez(a)','no','','Parts from FG belonging to WO# 71383(7), 72319(2), 72383(38) are inspected for similar issue and found that all the parts are ok without any similar deviation.\r\nParts that were in WIP belonging to WO#   72318(3), 72380(205), 72381(349),  and 74181(223) where inspected and found to be ok.||','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10685,'35-623A','Saab AB','SHAFT 2','515372B','D5227280820000','NA','PART ISSUE A',1,'OWED-LTA-004','','74648','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Hole position out from part outer profile.','1)running time part shacked due to Vice low tightness.|','1)M00 and massage given in program to check the vice tightness\r<br/>and doing mallet on the RM.|','1)Training given about vice tightening to operator. \r<br/>2)M00 and massage given in program to check the vice tightness and doing mallet on the RM.\r<br/>3)Instruction given to operator once again check the vice tightness before run the part.|','CA PA Found Ok.','','2018-06-03','Subramanya L(Naik)','Sundar D.K.,Subramanya L Naik,Raj Kumar,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','1','no','MakinoF5-2','Subramanya L(Naik)','no','','Check the all parts found OK .|','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10686,'53-018','Triumph Aerostructures','SPREADER PLATE ','755621','F574 50703 200 A01','NA','PART ISSUE A, ECN PG49999STLX239',1,'LTA TRIUMPH 2018','','75171','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','HOLE SHIFT UPTO 0.5 MM','Improper butting the part|Butting location pin damaged.|Tool run on the location pin.','|Location Pin Changed.','|Pin length reduced.','CAPA Found ok','','2018-06-04','Dhananjaya(N)','Kammar(Nagaraj)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','Misc','Manu(P)','no','','|Immediately stop the machine and Location Pin Changed.','E3456','pe|qas|','2018-12-18|2018-12-18|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10687,'35-650A','Saab AB','SHAFT','B76568','D5227346820200','NA','PART ISSUE C',6,'PA1687 LTA-2','','72059','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','TOTAL LENGTH UNDER SIZE 0.10 MM','We are maintain the total length in 05 operation and finish the OD in 07 operation with tail stock support that time total length was 0.2mm to 0.3mm undersized. ','For the next batch we are maintain the total length in 0.2mm oversize then after the 07 operation we are got the actual size. ','For the reference purpose and to avoid this type of errors we are comments added in the program top and list out this type of CRN, and training given to about this topic.   ','CA/PA Found satisfactory.','','2018-06-04','Dinakar(K)','Arun Kumar(A M)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','05','no','Misc','Raghavendra Rao(R)','no','','stop the machine and analyze the problem and we got the problem,it will be arising in 07th operation because of tail stock support.   ','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10688,'35-604','Saab AB','SHAFT , VENT HOOKS','2617','D5227352920200','NA','PART ISSUE B',1,'PA1687 LTA-1','','73803','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','total length under-size by -0.3mm.','part was not debarred and height was measured without checking the part whether it was debarred or not. then the part was inspected after the machining process and found that length was undersized.','each part will be debarred after  machining process and will be gauged.','to make sure that before loading each part the part will be thoroughly gauged and debarred.','CA PA found ok and next production batch found ok. ','','2018-06-04','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Ravi(M)','no','','next part was debarred and inspected before loading onto the machine and the part was found OK.','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10689,'35-624A','Saab AB','SHAFT 3','C87212','D5227281320000','NA','PART ISSUE B',1,'OWED-LTA-004','','73780','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','OD Under size 0,05mm.','during jaws boring process 0.05mm run out occurred on jaws bore. That was not ensured.  ','During jaws boring process run out to be check then part production to be carry on.','Without run out ensuring process part wont to be produce. So run out to be ensure on log book.   ','CAPA found ok.','','2018-06-04','Dinakar(K)','Ugraiah ,Subramanya ,Shivappa M B,Nandeesha N,Dinakar K,Arun Kumar A M,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','QT100S-5','Narasimha Murthy(R)','no','','Jaws boring process was again carried out. Then ensued the jaws run out was 0.01mm  ','E3456','qas|','2018-08-04|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10690,'35-623A','Saab AB','SHAFT 2','515372B','D5227280820000','NA','PART ISSUE A',1,'OWED-LTA-004','','74648','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dummy NC','For the purpose of reducing the cycle time editing the program feed rate and rpm so running time part was broken.      ','For next part increase the Cv by step by step and reduced the cycle time. ','Next any CRN for decreasing the cycle time we are start the Cv in minimum side and set the program. ','Dummy NC','','2018-06-04','Dinakar(K)','Dinakar K,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','With Treatment','','5','no','QT100S-1','Dinakar(K)','no','','decrease the rpm and feed rate and run the production. ','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10691,'51-049','THE BOEING COMPANY','BRACKET ','741181','149A7371-9623','NA','PSDL REV A',2,'BOEING 001P','','72285','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Parts received from treatment were found paint damage at the edges and corners.','This is happen during the transportation as there was no safety in the inner layer of the box in which the parts were shipped','Parts were done manual touch up as per the specification and found ok','Instruction was given to the treatment house on packaging to put extra kushan type of material surronding the inner layer of the box to avoid such paint damages during the transportation','Next Lot Received from the treatment supplier ,parts were checked and found visually acceptable to the requirement','','2018-06-04','Murali(M)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','DN40153','POST TREATMENT','yes','Misc','qas_sez(a)','no','','parts were identified and segregated and the same was communicated to the treatment house','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10692,'35-623A','Saab AB','SHAFT 2','515372B','D5227280820000','NA','PART ISSUE A',1,'OWED-LTA-004','','74648','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dummy NC','For the purpose of reducing the cycle time editing the program feed rate and rpm so running time part was broken.      ','For next part increase the Cv by step by step and reduced the cycle time. ','Next any CRN for decreasing the cycle time we are start the Cv in minimum side and set the program. ','Dummy NC','','2018-06-04','Dinakar(K)','Dinakar K,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','With Treatment','','5','no','QT100S-1','Dinakar(K)','no','','decrease the rpm and feed rate and run the production. ','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10693,'53-017','Triumph Aerostructures','SPREADER PLATE TOP','755621','F574 50217 202 B03','NA','PART ISSUE A',1,'LTA TRIUMPH 2018','','74664','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','dig mark found on part','','','','this problem will not appear in future','','2018-06-04','Dhananjaya(N)','Kammar(Nagaraj)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','fi','no','Misc','Manu(P)','no','','informed operator to correct the clamping','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10694,'51-130A','THE BOEING COMPANY','SPACER-POWER FEEDER CLAMP','524784-02','332W1912-103','NA','PSDL REV -',1,'BOEING 001W','','74902','','2018-06-05',NULL,'yes','yes','yes','no','no','no','no','no','no','PART RUNNING TIME TOOL WILL BROKEN PART WILL SHIFTED  ','PART RUNNING TIME TOOL WILL BROKEN PART WILL SHIFTED ','TO CHECK THE TOOL AND REPLACE THE TOOL THEN RUNNING M/C AS PER THE PROCESS ','CARE FULL THE PART LOADING AND RUNNING THE AS WELL AS ABOVE PROCESS FOR THE RUNNING TIME ','Next batches found ok.','','2018-06-05','op_sez(s)','op_sez(s)','','2018-06-05','','F8003-S','Rev 0 dt 8-1-2009',0.00,'','Closed','no','yes','no','With Treatment','','01','no','Misc','op_sez(s)','no','','TO CHECK THE TOOL AND REPLACE THE TOOL THEN RUNNING M/C AS PER THE PROCESS ','Z3456','qas|','2018-08-01|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10695,'51A-001','THE BOEING COMPANY','UPPER BEAM FWD SPLICE ASS','','315Z1301-1501','','NIL',1,'BOEING 001K','','A12924','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','no','Wrong masking tape was used.','Masking Tape used on the final finished parts was not meeting the requirements of BAC5034-4 electrical bonding area.','1) Head Procurement instructed the Supply chain team to highlight the masking requirements in the Purchase Order (PO).\r<br/>2) Head Engineering instructed his team to create a detailed work instruction and to revise the receiving inspection plan. ','1) Head Engineer to make a detailed Work Instruction describing the masking requirements.\r<br/>2) Head Engineer to revise the receiving inspection plan to cover the requirements of parameters to be ensured to attain drawing requirements.\r<br/>3) Head Engineer to train all the relevant personnel on the defect in the process and the corrections made in the process to overcome the defect.','Next batches found Ok.','','2018-06-05','qas_sez(a)','qas_sez(a)','CA1236524','2018-04-30','Wrong masking tape was used.','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER END','yes','Misc','qas_sez(a)','yes','','Quality Inspector inspected all the parts in FG and Assembly to ensure proper masking and found all the parts to be acceptable as per the drawing requirement.','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10696,'51A-002','THE BOEING COMPANY','UPPER BEAM FWD SPLICE ASS','','315Z1301-1502','','NIL',1,'BOEING 001K','','A12926','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','no','Wrong masking tape was used after assembly.','Engineering person did not mentioned the proper masking tape to be used in the APS.','|Tapes according to the drawing are purchased.','|BOM and APS revised. and delta FAIR submitted.','Next batches found ok.','','2018-06-05','qas_sez(a)','qas_sez(a)','CA1236524-00','2018-04-30','Wrong masking tape was used.','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER END','yes','Misc','qas_sez(a)','yes','','|Immediately stopped the assembly process and  informed the Engineering team to revise the BOM and APS according to the drawing.','Z3456','qas|','2018-08-09|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10697,'34-015B','Magellan Aerospace Winnipeg','MOUNTING LUG- STRUT / STD','G22016K07','400-12607-1-905','','EM104302 Iss A, EM104765 Iss G, EM105092 Iss F, EM106399 Iss B, EM106400 Iss B, EM106401 Iss A, EM106404 Iss A, EM106522 Iss A, EM106602 Iss A',2,'B91379 Rev.026','','73995','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','Base thinness 0.1mm under size, Nominal Required .12 +/- .01Inch Measures .1062 to .1098.','Due to improper Clamping parts base thickness get under sized.','1. The part was kept separately for further investigation and NC was raised. \r<br/>2. The program was studied in briefly so as to avoid the escapes. \r<br/>3. All the tool offset was reset.\r<br/>','After loading the part into the fixture,it will be checked for air gaps between the part and the fixture using the feeler gauge and then start the machining.\r<br/>','CA PA Found OK.','','2018-06-05','Dhananjaya(N)','Narasimhamurthy C,dharshan d,Dhananjaya N,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','5','no','HAASVF2SS-2','Dhananjaya(N)','no','','1) All the Previous parts are Inspected and found OK.\r\n2) All the Tool Offset re-ensured.','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10698,'35-408A','Saab AB','FRAME MID','701946 1D1','D522 73397 200 00','','PART ISSUE B',2,'OWED-LTA-001','','71190','','0000-00-00',NULL,'no','no','no','no','no','yes','yes','yes','no','Etching  operation part reject from ATPL. ','Blind holes occurred on part|After etching operation part was not cleaned properly on behind thread.|Due to that chemical reaction occurred and material was removed','|After etching process parts are to be ensure free of chemical by visually if it is there that to be clean','|As per the process sheet that visual inspection to be carried out','CAPA FOUND OK','','2018-06-05','qas_sez(a)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','DN38087','Post DN','no','Misc','qas_sez(a)','no','','|The parts which are all in process that was ensured free from the chemical after etching process.','Z3456','qas|','2018-08-07|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10699,'35-408A','Saab AB','FRAME MID','514457 B','D522 73397 200 00','','PART ISSUE B',4,'OWED-LTA-001','','71193','','0000-00-00',NULL,'no','no','no','no','no','yes','yes','yes','no','Etching  operation part reject from ATPL. ','','','','','','2018-06-05','qas_sez(a)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','DN38089','Post DN','no','Misc','qas_sez(a)','no','','','Z3456','qas_sez|','2018-09-27|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10700,'51-030','THE BOEING COMPANY','BRACKET','741162','149A7371-948','','PSDL REV A',1,'BOEING 001E','','73344','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Parts received from treatment were found paint damage at the edges and corners.','This is happen during the transportation as there was no safety in the inner layer of the box in which the parts were shipped','Parts were done manual touch up as per the specification and found ok','Instruction was given to the treatment house on packaging to put extra kushan type of material surronding the inner layer of the box to avoid such paint damages during the transportation.','Next Lot Received from the treatment supplier ,parts were checked and found visually acceptable to the requirement','','2018-06-05','Murali(M)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','DN40471','POST TREATMENT','yes','Misc','qas_sez(a)','no','','parts were identified and segregated and the same was communicated to the treatment house','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10701,'51-037','THE BOEING COMPANY','BRACKET','741161','149A7371-965','','PSDL REV A',1,'BOEING 001E','','73365','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Parts received from treatment were found paint damage at the edges and corners.\r\n','This is happen during the transportation as there was no safety in the inner layer of the box in which the parts were shipped','Parts were done manual touch up as per the specification and found ok','Instruction was given to the treatment house on packaging to put extra kushan type of material surronding the inner layer of the box to avoid such paint damages during the transportation.','Next Lot Received from the treatment supplier ,parts were checked and found visually acceptable to the requirement','','2018-06-05','Murali(M)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','DN40841','POST TREATMENT','yes','Misc','qas_sez(a)','no','','parts were identified and segregated and the same was communicated to the treatment house','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10702,'34-015B','Magellan Aerospace Winnipeg','MOUNTING LUG- STRUT / STD','G22016K07','400-12607-1-905','','EM104302 Iss A, EM104765 Iss G, EM105092 Iss F, EM106399 Iss B, EM106400 Iss B, EM106401 Iss A, EM106404 Iss A, EM106522 Iss A, EM106602 Iss A',2,'B91379 Rev.026','','73995','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','Base thinness 0.1mm under size, Nominal Required .12 +/- .01Inch Measures .1062 to .1098.','Due to improper Clamping parts base thickness get under sized.','1. The part was kept separately for further investigation and NC was raised. \r<br/>2. The program was studied in briefly so as to avoid the escapes. \r<br/>3. All the tool offset was reset.\r<br/>','After loading the part into the fixture,it will be checked for air gaps between the part and the fixture using the feeler gauge and then start the machining.\r<br/>','CA & PA Found OK.','','2018-06-05','Dhananjaya(N)','Narasimhamurthy C,dharshan d,Dhananjaya N,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','5','no','HAASVF2SS-2','Dhananjaya(N)','no','','1) All the Previous parts are Inspected and found OK.\r\n2) All the Tool Offset re-ensured.','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10703,'51-046','THE BOEING COMPANY','BRACKET','741173','149A7371-9612','','PSDL REV A',2,'BOEING 001F','','73042','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Parts received from treatment were found paint damage at the edges and corners.','This is happen during the transportation as there was no safety in the inner layer of the box in which the parts were shipped','Parts were done manual touch up as per the specification and found ok','Instruction was given to the treatment house on packaging to put extra kushan type of material surronding the inner layer of the box to avoid such paint damages during the transportation.','Next Lot Received from the treatment supplier ,parts were checked and found visually acceptable to the requirement','','2018-06-05','Murali(M)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','DN40422','POST TREATMENT','yes','Misc','qas_sez(a)','no','','parts were identified and segregated and the same was communicated to the treatment house','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10704,'51-029','THE BOEING COMPANY','BRACKET','741173','149A7371-947','','PSDL REV A',1,'BOEING 001E','','73334','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Parts received from treatment were found paint damage at the edges and corners.','This is happen during the transportation as there was no safety in the inner layer of the box in which the parts were shipped','Parts were done manual touch up as per the specification and found ok','Instruction was given to the treatment house on packaging to put extra kushan type of material surronding the inner layer of the box to avoid such paint damages during the transportation','Next Lot Received from the treatment supplier ,parts were checked and found visually acceptable to the requirement','','2018-06-05','Murali(M)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','DN40702','POST TREATMENT','yes','Misc','qas_sez(a)','no','','parts were identified and segregated and the same was communicated to the treatment house','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10705,'51-037','THE BOEING COMPANY','BRACKET','741192','149A7371-965','','PSDL REV A',1,'BOEING 001E','','71888','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Parts received from treatment were found paint damage at the edges and corners.','This is happen during the transportation as there was no safety in the inner layer of the box in which the parts were shipped','Parts were done manual touch up as per the specification and found VISUALLY ok','Instruction was given to the treatment house on packaging to put extra kushan type of material surronding the inner layer of the box to avoid such paint damages during the transportation.','Next Lot Received from the treatment supplier ,parts were checked and found visually acceptable to the requirement','','2018-06-05','Murali(M)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','DN40207','POST TREATMENT','yes','Misc','qas_sez(a)','no','','parts were identified and segregated and the same was communicated to the treatment house','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10706,'51-051','THE BOEING COMPANY','BRACKET','741182','149A7371-9627','','PSDL REV A',1,'BOEING 001C','','73384','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Parts received from treatment were found paint damage at the edges and corners.','This is happen during the transportation as there was no safety in the inner layer of the box in which the parts were shipped','Parts were done manual touch up as per the specification and found VISUALLY ok','Instruction was given to the treatment house on packaging to put extra kushan type of material surrounding the inner layer of the box to avoid such paint damages during the transportation.','Next Lot Received from the treatment supplier ,parts were checked and found visually acceptable to the requirement','','2018-06-05','Murali(M)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','yes','With Treatment','DN40419','POST TREATMENT','no','Misc','qas_sez(a)','no','','parts were identified and segregated and the same was communicated to the treatment house','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10707,'51-028','THE BOEING COMPANY','BRACKET','741173','149A7371-946','','PSDL REV A',1,'BOEING 001H','','71713','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Parts received from treatment were found paint damage at the edges and corners.','This is happen during the transportation as there was no safety in the inner layer of the box in which the parts were shipped','Parts were done manual touch up as per the specification and found ok','Instruction was given to the treatment house on packaging to put extra kushan type of material surronding the inner layer of the box to avoid such paint damages during the transportation','Next Lot Received from the treatment supplier ,parts were checked and found visually acceptable to the requirement','','2018-06-05','qas_sez(a)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','DN40560','POST TREATMENT','yes','Misc','qas_sez(a)','no','','parts were identified and segregated and the same was communicated to the treatment house','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10708,'51-044','THE BOEING COMPANY','BRACKET','741172','149A7371-9608','','PSDL REV A',1,'BOEING 001F','','72292','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Parts received from treatment were found paint damage at the edges and corners.','This is happen during the transportation as there was no safety in the inner layer of the box in which the parts were shipped','Parts were done manual touch up as per the specification and found VISUALLY  ok','Instruction was given to the treatment house on packaging to put extra kushan type of material surronding the inner layer of the box to avoid such paint damages during the transportation.','Next Lot Received from the treatment supplier ,parts were checked and found visually acceptable to the requirement','','2018-06-06','qas_sez(a)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','yes','With Treatment','DN40250','POST TREATMENT','no','Misc','qas_sez(a)','no','','parts were identified and segregated and the same was communicated to the treatment house','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10709,'51-050','THE BOEING COMPANY','BRACKET ','741181','149A7371-9624','NA','PSDL REV A',1,'BOEING 001P','','72289','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Parts received from treatment were found paint damage at the edges and corners.','This is happen during the transportation as there was no safety in the inner layer of the box in which the parts were shipped','Parts were done manual touch up as per the specification and found ok','Instruction was given to the treatment house on packaging to put extra kushan type of material surronding the inner layer of the box to avoid such paint damages during the transportation.','Next Lot Received from the treatment supplier ,parts were checked and found visually acceptable to the requirement','','2018-06-07','qas_sez(a)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','yes','With Treatment','DN40510','POST TREATMENT','no','Misc','qas_sez(a)','no','','parts were identified and segregated and the same was communicated to the treatment house','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10710,'51-048','THE BOEING COMPANY','BRACKET','741162','149A7371-9616','NA','PSDL REV A',1,'BOEING 001P','','73049','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Parts received from treatment were found paint damage at the edges and corners.','This is happen during the transportation as there was no safety in the inner layer of the box in which the parts were shipped','Parts were done manual touch up as per the specification and found VISUALLY ok','Instruction was given to the treatment house on packaging to put extra kushan type of material surronding the inner layer of the box to avoid such paint damages during the transportation.','Next Lot Received from the treatment supplier ,parts were checked and found visually acceptable to the requirement','','2018-06-07','qas_sez(a)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','DN40421','POST TREATMENT','no','Misc','qas_sez(a)','no','','parts were identified and segregated and the same was communicated to the treatment house','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10711,'51-034','THE BOEING COMPANY','BRACKET','741161','149A7371-954','','PSDL REV A',1,'BOEING 001E','','73530','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Parts received from treatment were found paint damage at the edges and corners.','This is happen during the transportation as there was no safety in the inner layer of the box in which the parts were shipped','Parts were done manual touch up as per the specification and found VISUALLY ok','Instruction was given to the treatment house on packaging to put extra kushan type of material surronding the inner layer of the box to avoid such paint damages during the transportation.','Next Lot Received from the treatment supplier ,parts were checked and found visually acceptable to the requirement','','2018-06-07','qas_sez(a)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','DN40723','POST TREATMENT','no','Misc','qas_sez(a)','no','','parts were identified and segregated and the same was communicated to the treatment house','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10712,'51-029','THE BOEING COMPANY','BRACKET','741162','149A7371-947','','PSDL REV A',1,'BOEING 001E','','73338','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Parts received from treatment were found paint damage at the edges and corners.','This is happen during the transportation as there was no safety in the inner layer of the box in which the parts were shipped','Parts were done manual touch up as per the specification and found VISUALLY ok','Instruction was given to the treatment house on packaging to put extra kushan type of material surronding the inner layer of the box to avoid such paint damages during the transportation.','Next Lot Received from the treatment supplier ,parts were checked and found visually acceptable to the requirement','','2018-06-07','qas_sez(a)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','DN40798','POST TREATMENT','no','Misc','qas_sez(a)','no','','parts were identified and segregated and the same was communicated to the treatment house','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10713,'51-027','THE BOEING COMPANY','BRACKET','741161','149A7371-945','','PSDL REV A',1,'BOEING 001E','','73324','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Parts received from treatment were found paint damage at the edges and corners.','This is happen during the transportation as there was no safety in the inner layer of the box in which the parts were shipped','Parts were done manual touch up as per the specification and found VISUALLY ok','Instruction was given to the treatment house on packaging to put extra kushan type of material surronding the inner layer of the box to avoid such paint damages during the transportation.','Next Lot Received from the treatment supplier ,parts were checked and found visually acceptable to the requirement','','2018-06-07','qas_sez(a)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','DN40846','POST TREATMENT','no','Misc','qas_sez(a)','no','','parts were identified and segregated and the same was communicated to the treatment house','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10714,'51-029','THE BOEING COMPANY','BRACKET','741173','149A7371-947','','PSDL REV A',2,'BOEING 001E','','71716','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Parts received from treatment were found paint damage at the edges and corners.','This is happen during the transportation as there was no safety in the inner layer of the box in which the parts were shipped','Parts were done manual touch up as per the specification and found VISUALLY ok','Instruction was given to the treatment house on packaging to put extra kushan type of material surronding the inner layer of the box to avoid such paint damages during the transportation.','Next Lot Received from the treatment supplier ,parts were checked and found visually acceptable to the requirement','','2018-06-07','qas_sez(a)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','yes','With Treatment','DN40269','POST TREATMENT','no','Misc','qas_sez(a)','no','','parts were identified and segregated and the same was communicated to the treatment house','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10715,'51-041','THE BOEING COMPANY','BRACKET','180534B0','149A7371-9603','','PSDL REV A',2,'BOEING 001F','','70226','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dummy Part','Dummy part','Dummy raw material was used for the to prove the NC program.','Dummy raw material was used for the to prove the NC program.','Dummy part.','','2018-06-07','pe_sez(a)','op_sez(s)','','0000-00-00','Part under the Quarantine Status','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','yes','With Treatment','','1','no','Misc','pe_sez(a)','no','','New tool added and continue the production.','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10716,'51-017','THE BOEING COMPANY','BRACKET ','789223A5','149A7371-923','NA','PSDL REV A',1,'BOEING 001L','','68487','','0000-00-00',NULL,'yes','no','no','no','no','yes','no','yes','no','','while drilling operation part vibrated so hole ob-longed. ','changed the operation sequence and run the new part and found ok','Review all the operation sequence before running the part.','Next batches found ok.','','2018-06-07','pe_sez(a)','pe_sez(a)','','0000-00-00','Mentioned in the drawing H2,H3,H7 and H8 Holes position measured out of the tolerance. ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','Misc','qas_sez(a)','no','','Checked program sequence and found defective','E3456','qas|','2018-09-05|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10717,'51A-052','THE BOEING COMPANY','BRACKET ASSY','','149A7371-626','','PSDL REV A',2,'BOEING 001G','','A15607','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','PAINT PEALUP ','1.The Teflon paint chip off surrounding the rivet during pressing the rivet|2.During pressing the rivet metal to metal contact|3.In butting block the  area where the parts were butting while riveting was not uniform|4.FOD of rivet accumulated in the butting block where the part was getting butted.','|2.Butting block was made uniform by giving a uniform cut','|1.Instruction given to operator to Change the adhesive tape frequently and clean the area where the parts gets butted before pressing the rivet to remove the FOD','Next batch wo number A15800 qty 8 nos  assembly done inspected and found ok,no evidence found for paint getting chipped','','2018-06-07','qas_sez(a)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','yes','Assembly','','FI','no','Misc','qas_sez(a)','no','','|Adhesive tape was appiexed on the butting block to avoid metal to metal contact','Z3456','qas_sez|','2019-01-06|','2019-01-06',NULL,NULL,NULL,NULL,NULL,NULL),(10718,'35-233A','Saab AB','HINGE BRACKET 5 ','233915B8','D576 50008 208','','D00',1,'1600223433/Forecast ','','74832','','0000-00-00',NULL,'yes','yes','yes','','','','','','','part running time bore chattering so part line mark so reject..','Parts are running By the FMS. When Boring bar running time Chips are locked with Boring Bar. The bore\'s finished Surface was rubbed by the Chips.','Boring bar\'s insert changed. Coolant Flow increased by Cleaning of Coolant Motor and Filters. ','The insert\'s cutting edges to be verify each and every FMS cycle start. Coolant flow pressure\r<br/>increased by the M code. when pressure fell Down the machine intimate the alarm. ','Next batches found ok.','','2018-06-07','Lohith(K)','                Umesh B','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','03','','','','','','Production stopped. completed parts are 100% inspection Done. no Error Found. ','Z3456','qas|','2018-09-05|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10719,'53-031','Triumph Aerostructures','SPREADER PLATE TOP','297622/001','F574 52127 200 00','NA','PART ISSUE A',1,'LTA TRIUMPH 2018','','74668','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','DIG MARK FOUND ON PART','Tool breakdown while running.|Tool over hang length was maximum.','|Put a comment on program about the tool over hanging length.','|Put a comment on program about the tool over hanging length. and training Gaven to the operator.','CAPA found OK','','2018-06-07','Dhananjaya(N)','Kammar(Nagaraj)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','Misc','Manu(P)','no','','INFORMED OPERATOR TO CLAMP THE PART CORRECTLY|Tool over hang length was changed.and run the machine.','E3456','pe|qas|qas|','2018-12-18|2018-12-18|2018-12-18|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10720,'51-032','THE BOEING COMPANY','BRACKET','741172','149A7371-952','','PSDL REV A',1,'BOEING 001H','','71866','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Parts received from treatment were found paint damage at the edges and corners.','This is happen during the transportation as there was no safety in the inner layer of the box in which the parts were shipped','Parts were done manual touch up as per the specification and found ok','Instruction was given to the treatment house on packaging to put extra kushan type of material surronding the inner layer of the box to avoid such paint damages during the transportation.','Next Lot Received from the treatment supplier ,parts were checked and found visually acceptable to the requirement','','2018-06-07','qas_sez(a)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','DN40418','POST TREATMENT','yes','Misc','qas_sez(a)','no','','parts were identified and segregated and the same was communicated to the treatment house','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10721,'51-046','THE BOEING COMPANY','BRACKET','741162','149A7371-9612','','PSDL REV A',4,'BOEING 001F','','73047','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Parts received from treatment were found paint damage at the edges and corners.','This is happen during the transportation as there was no safety in the inner layer of the box in which the parts were shipped','Parts were done manual touch up as per the specification and found visually ok','Instruction was given to the treatment house on packaging to put extra kushan type of material surronding the inner layer of the box to avoid such paint damages during the transportation.','Next Lot Received from the treatment supplier ,parts were checked and found visually acceptable to the requirement','','2018-06-07','qas_sez(a)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','DN40765','POST TREATMENT','yes','Misc','qas_sez(a)','no','','parts were identified and segregated and the same was communicated to the treatment house','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10722,'51-046','THE BOEING COMPANY','BRACKET','741162','149A7371-9612','','PSDL REV A',1,'BOEING 001F','','73044','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Parts received from treatment were found paint damage at the edges and corners.','This is happen during the transportation as there was no safety in the inner layer of the box in which the parts were shipped','Parts were done manual touch up as per the specification and found visually ok','Instruction was given to the treatment house on packaging to put extra kushan type of material surrounding the inner layer of the box to avoid such paint damages during the transportation.','Next Lot Received from the treatment supplier ,parts were checked and found visually acceptable to the requirement','','2018-06-07','qas_sez(a)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','DN40764','POST TREATMENT','yes','Misc','qas_sez(a)','no','','parts were identified and segregated and the same was communicated to the treatment house','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10723,'43A-005','Composite Industrie','BRACKET ASSY','','V251 13495 000','','A00, ECN PV100298ST1BJ54',1,'ATA25_ACH-4128-1','','K05789','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','no','Rivet shifted while Assembly.','While manually holding the two parts to make assembly Rivet get shifted.','1.Fixture created for next batch of parts.','1.Fixture created for next batch of parts.','Effectiveness found ok.','','2018-06-08','Ramesh(D)','Ramesh(D)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Assembly','','ONSITE','no','Misc','Mahesh(DV)','yes','','1.Fixture created for next batch of parts.','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10724,'35-228A','Saab AB','HINGE BRACKET 2 ','4755501 1','D576 50005 205','','D00',1,'1600223433/Forecast ','','74833','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Part slat width over sized. ','1.Part not butting to butting pin properly.\r<br/>2. Operator failed to check with feeler gauge.\r<br/>3. Butting method not adequate.\r<br/>','Fixture butting improvement done with spring load.\r<br/>','Similar arrangement done for other direction also.\r<br/>and for the parts of same family.','CAPA Found ok. Fixture alteration done, next production need to be monitored.','','2018-06-08','Subramanya L(Naik)','CHETANA(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','5','no','Misc','Subramanya L(Naik)','no','','Stop the machine and Check the part butting.','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10725,'43A-033','Composite Industrie','B BRACKET ASSY','','V251 15065 000 00','','B00, ECN PV100298ST1ZY72',2,'LTA PO-1','','K06909','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','no','Dig on part while assembly.','While doing assembly manually dig mark on part occurred.','Fixtures created for next batch and found ok.','Fixtures created for next batch and found ok.','Effectiveness found ok.','','2018-06-08','Ramesh(D)','Ramesh(D)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Assembly','','ONSITE','no','Misc','Mahesh(DV)','yes','','Fixtures created for next batch and found ok.','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10726,'35-165B','Saab AB','HOUSING PIN','330651','423Z1124-5-01','','--B',1,'787 Forecast','','73268','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Chamfer oversize up to 1mm.','Tool offset wrong.','Guide the operator.','Operator under observation.','CAPA FOUND OK','','2018-06-08','prodn_aero(prodn)','Manjunatha.S.T(M)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','11','no','Misc','Manjunatha.S.T(M)','no','','Correct the tool offset then run the production.','A3456','qas_aero|','2018-07-17|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10727,'51-089','THE BOEING COMPANY','HOUSING','G23752K08','312W5220-7','NA','PSDL REV -',1,'486998 MPP','','74771','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Outer Diameter reduced by 2mm.\r\n','Running time U-drill screw was broken and turret was taken the load so turret axis shifted become part outer diameter 2mm undersized. |1)U-drill insert screw failed, so excess load tilted the turret.\r<br/>2)Screw used on u-drill not tightened with wrench torque. \r<br/>3)Tightened done with the Allan key manually.','check the part inner and outer diameter it will become equally 2mm undersized so we got the problem so taken re-offset for all the tools and run the production.|Torque wrench is made compulsory for this tool. ','We inform to the maintenance team and correct the axis. and inform to the operator to if any type of accidents stop the machine and check the X and Z axis. |All inserts type cutting in turning section is recorded to be tightened with torque wrench only.','CA PA Closed.','','2018-06-09','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Raghavendra Rao(R)','no','','Remove the U-drill and use the HSS taper shank drill and run the production. |Checked all the completed parts of this work order and found okay.','E3456','pe|qas|','2018-06-29|2018-07-02|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10728,'35-412','Saab AB','BRACKET','531882E','D5227341220000','','A',1,'OWED-LTA-001','','73869','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Deep dent found on the part during the receiving inspection.','Dent mark observed after treatment process on part|Before ship into treatment house part that was not ensured |During Inspection the light intensity was low due to that that was not clearly shown in web surface','|The light intensity was implement 1000 lux level and the visual inspection to be carried out in that','|1000 lux light intensity is maintain during visual inspection','NEXT BATCH FOUND OK','','2018-06-10','pe_sez(a)','op_sez(s)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','pe_sez(a)','no','','|The remaining parts in Inspection was enured ok','Z3456','qas|','2018-08-07|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10729,'18-437B','Magellan Aerospace(Blackpool) Limited','MANIFOLD','6277','PI201274625','NA','NIL',1,'Bpp-529619 amed-2','','74643','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','yes','Damage to 25mm boss end face adjacent to 8.73 hole.','Damage of parts occurred due to improper handling.','1) Instruction given to the production and the packing personnel to prevent part to part contact and to use foam or bubble sheets to prevent the parts for touching each other.\r<br/>|','1) Proper trays will be used to move the parts from department to department and additional package will be given to all edges to avoid damages.|','CAPA found ok.','C64977','2018-06-11','qas_sez(a)','Nandishkumar(D.K.)','RDN-4755','2018-06-07','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','yes','Manufacture Only','','CUST END','no','Misc','qas_sez(a)','no','','All the parts are packed with sufficient packing.|','Z3456','qas|','2018-09-05|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10730,'18-438B','Magellan Aerospace(Blackpool) Limited','MANIFOLD ','2800','PI55-1213031-00','NA','NIL',1,'Bpp-529619 amed-2','','74644','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','1.) Damage to 25mm boss end face dwg. ref detail \'x\' adjacent to 8.73mm lee plug hole.\r\n2.) 17.48mm - 17.86mm 120 deg chamfers under-size, act. measure 17.25mm approximately.','1) Damage of parts occurred due to improper handling.\r\n<br/>2) Re-inspection of chamfer dimensions was not done after the completion of spot face rework.','1) Instruction given to the production and the packing personnel to prevent part to part contact and to use foam or bubble sheets to prevent the parts for touching each other.\r<br/>2) All the inspectors are instructed to carry out 100% inspection after the rework on relevant dimensions that are potentially affected due to rework.|','1) Proper trays will be used to move the parts from department to department and additional package will be given to all edges to avoid damages.\r<br/>2) Proper analysis and care will be taken during rework and inspection of the reworked parts.|','Next batches found ok.','C64975','2018-06-11','qas_sez(a)','Nandishkumar(D.K.)','RDN-4756','2018-06-07','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','yes','Manufacture Only','','CUST END','no','Misc','qas_sez(a)','no','','1) All the parts are packed with sufficient packing.\r\n2) No similar parts were in WIP and FG.|','Z3456','qas|','2018-09-05|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10731,'51-049','THE BOEING COMPANY','BRACKET ','741161','149A7371-9623','NA','PSDL REV A',1,'BOEING 001P','','73429','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dig mark observed on face.\r\n ','While part running time tool was broken.|Dia 16 flat tool holder changing and running...|CUTTING TOOL\'S HOLDING LENGTH IS NOT SUFFICIENT|THE STANDARD CUTTING TOOL TOTAL LENGTH 110MM ONLY. IN THIS OVER HANG LENGTH IS 82MM|AS PER NC PROGRAM, THE OPERATOR HOLD THE CUTTING TOOL OVER HANG 82MM IS MUST','|Dia 16 flat tool holder changing and tool offset checking tool tightness checking , and running. ','|Dia 16 flat tool holder changing and tool offset checking tool tightness checking , and running. ','CAPA found ok.','','2018-06-11','pe_sez(a)','pe_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','1','no','Misc','pe_sez(a)','no','','|dia 16 flat tool holder changing and running... ','Z3456','pe|qas|','2018-09-17|2018-09-24|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10732,'53-002','Triumph Aerostructures','FORK FITTING','4238303','F579 53444 202','NA','PART ISSUE A',1,'LTA Triumph ASSY 201','','75165','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','DIG MARK FOUND ON PART','','','','THIS PROBLEM WILL NOT APPEAR IN FUTURE','','2018-06-11','Dhananjaya(N)','Kammar(Nagaraj)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','With Treatment','','FI','no','Misc','Manu(P)','no','','INFORMED OPERATOT TO CLAMP THE PART CORRECTLY','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10733,'51A-086','THE BOEING COMPANY','KICK LINK ASSY','','251W3122-3','','PSDL REV -',1,'BOEING 001M','','A13441','','0000-00-00',NULL,'yes','no','no','no','no','yes','no','yes','no','Step observed on the part which is not meets the specification requirement.','DUE TO WRONG OFFSET VALUE ENTERED BY THE OPERATOR DURING CORRECTION OF THE PART.','|THE SUOERVISOR HAS TO RECHECK THE OFFSET VALUE INPUT BY THE OPERATOR.','|THE SUOERVISOR HAS TO RECHECK THE OFFSET VALUE INPUT BY THE OPERATOR.','CAPA FOUND SATISFACTORY','','2018-06-11','pe_sez(a)','pe_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','FI','yes','Misc','qas_sez(a)','no','','|MACHINE WAS STOPPED AND INFORMED TO THE SUPERVISOR','Z3456','qas_sez|','2019-02-13|','2019-02-13',NULL,NULL,NULL,NULL,NULL,NULL),(10734,'47-022B','GKN Aerospace Filton','FITTING- FWD INBD','1013901 5','F57550070201','NA','C01, MIS ISSUE F, F575ABSMCD Rev 39',1,'S.A.No. 6200005328','','74127','','0000-00-00',NULL,'yes','no','yes','','','','','yes','no','part thickness under size. ','1)Part not butt to fixture base.\r\n<br/>2)Operator cannot checked by feeler gauge to  part  base butting .\r\n<br/>3)fixture structure problem.','Do the mallet after roughing the part  and once again cross check the part  base butting. |','1)Discussed with engineering for change the fixing method.\r<br/>2)fixture will change.  |','CAPA found Ok.','','2018-06-11','Subramanya L(Naik)','        CHETANA K','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','3','','','','','','Checked all parts runned before found OK.|','E3456','qas|','2018-09-04|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10735,'53-003','Triumph Aerostructures','FORK FITTING','4238303','F579 53444 203','NA','PART ISSUE A',1,'LTA Triumph ASSY 201','','75167','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','dig mark found on part','Dia 10 cutter broke while roughing. Dig mark noticed part rejected.\r\n','|Cutting parameters found slightly higher. Remaining parts run with lesser feed. ','|Changed cutting parameters are found in the NC program with the help of engineering. ','CAPA Found OK','','2018-06-11','Dhananjaya(N)','Kammar(Nagaraj)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','fi','no','Misc','Manu(P)','no','','informed operator to clamp the part correctly','E3456','qas|','2018-12-18|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10736,'18-722A','Magellan Aerospace(Blackpool) Limited','SLAVE LINK UPPER','3750','PI 55-3569004-00','','PART REV PDM3',3,'BPP-529619 amed-1','','72812','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','Dig mark on part OD.','Running time chips was blocked in the part face so part OD dig mark.|1)CHIPS BLOCKED DURING OD TURNING.\r<br/>2)INEFFICIENT TOOL PATH.\r<br/>3)WRONG CUTTING SECTIONAL.','7 degree angle generate in the program for 5mm length  part found ok .|7 DEGREE ANGLE GENERATE IN THE PROGRAM.|RUN THE PARTS AND CHECK THE PART.|INFORMATION PASSED TO THE OPERATORS IN THE TRAINING|1)RUN THE NEXT BATCH PRODUCTION THIS PROBLEM NOT REPEATED.\r\n2)NC PROGRAM CORRECTED','Save the angle given program and run the another batch, same problem not repeated again.|1)NEW PROGRAM SAVED IN THE SERVER.\r<br/>2)MPS IS REVISED TO INCLUDE THE NEW PROCESSING METHOD.','CA PA found ok.','','2018-06-12','Sandhesh D(S)','Sandhesh D(S)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','05','no','Misc','Sandhesh D(S)','no','','stop the machine and analyze the problem |STOPPED THE MACHINE& CHECKED FOR PREVIOUS RUNNING PART. AND SEGREGATED THE PROBLEM PARTS.','E3456','pe|qas|','2018-06-29|2018-07-02|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10737,'34-070','Magellan Aerospace Winnipeg','HINGE R/H','G24067','400-12901-2','','EM104302 Iss A,EM105092 Iss G,EM104765 Iss G',0,'C46695 Rev.004','','74154','','0000-00-00',NULL,'','yes','yes','','','','yes','','','Dummy NC','Dummy NC','|Dummy NC','|Dummy NC','Dummy NC','','2018-06-12','Dhananjaya(N)','        Dhananjaya N','','0000-00-00','Dummy NC','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','','','','','01','','','','','','|Dummy NC','E3456','qas|','2018-09-05|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10738,'35-435A','Saab AB','RAMP X STOP','LL0107376','D522 73379 200 00','','PART ISSUE A',30,'OWED-LTA-002','','72781','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Steep notes in outer surface.','End mill blunt.|Tool life exceeded.','|Tool life is being monitored.','|Tool life is being monitored.','CA/PA found satisfactory. ','','2018-06-12','Lohith(K)','Rakesh  KC,Raj Kumar,','','0000-00-00','PART MACHINED FROM SEZ.','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','With Treatment','','FI','no','Fitting','Yashawantha(NH)','no','','Parts Checked in Transit, Production & Treatment house and found Ok. ','E3456','pe|nandishkumardk|nandishkumardk|','2018-11-27|2018-11-27|2018-11-27|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10739,'18-090A','Magellan Aerospace Bournemouth','BUSH','CD702609/02618A','PID278 50164 200','','A',36,'423255','','70224','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','OD under size in 0.010 to 0.020MM.*','Due to wear out of insert OD undersized.***||','Instructed to operator for  checking wear of insert in\r<br/>regular intervals and set frequency for changing inserts.||','Tool life was calculated in next batch and tool life was \r<br/>mentioned that part for tool.||','EFFECTIVENESS FOUND OK.','','2018-06-12','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','03','no','Misc','Dinakar(K)','no','','check the all previous running parts and set the frequency of changing inserts.||','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10740,'51A-051','THE BOEING COMPANY','BRACKET ASSY','','149A7371-625','','PSDL REV A',2,'BOEING 001C','','A15624','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','PAINT PEALUP(TEFLON CHIPOUT)','1.The Teflon paint chip off surrounding the rivet during pressing the rivet|2.During pressing the rivet metal to metal contact|3.In butting block the  area where the parts were butting while riveting was not uniform |4.FOD of rivet accumulated in the butting block where the part was getting butted.','|2.Butting block was made uniform by giving a uniform cut','|1.Instruction given to operator to Change the adhesive tape frequently and clean the area where the parts gets butted before pressing the rivet','Next batch wo number A15628 assembly Completed and found ok,no evidence found for paint getting chipped','','2018-06-12','pe_sez(a)','pe_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','yes','Assembly','','FI ','no','Misc','qas_sez(a)','no','','|Adhesive tape was appendix on the butting block to avoid metal to metal contact','Z3456','qas_sez|','2019-01-06|','2019-01-06',NULL,NULL,NULL,NULL,NULL,NULL),(10741,'34-051','Magellan Aerospace Winnipeg','MOUNTING LUG-GEARBOX','G24187','400-12608-1','','EM104302 Iss A,EM105092 Iss G,EM104765 Iss G',1,'C46695','','66642','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','- part has scratch can be felt with spherical radius probe (TG05010-2)\r\n- due to location of scratch an accurate measurement can not be achieved\r\n- scratch is approximately .170 length and .006 width','We have ensured utmost care for handling at machining at our end. We suspect the dent may be caused during material handling.','|Double checked the packing  procedures and refresh training was given to the packing personnel on the guidelines for standard packing as per Appendix-07.','','Next batch dispatched and no complaints received from customer.','C62875','2018-06-12','qas_sez(a)','qas_sez(a)','NR307137','2018-06-08','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','DN35845','CUST END','no','Misc','qas_sez(a)','no','','Visual Inspection carried out to all parts in Stock and found OK, No parts at WIP and Transit.','Z3456','qas|','2018-09-15|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10742,'35-672','Saab AB','SHAFT LEVER ','468066 D','D5227346221900','NA','PART ISSUE D',1,'OWED-LTA-001','','75227','','0000-00-00',NULL,'yes','no','yes','','yes','','','','','ID OVERSIZE BY 0.01MM','RUNNING TIME CARBIDE BORING TOOL (MINIATURE BORING) BAR WAS CHIP OUT SO. PART ID WAS 0.1MM OVER SIZER. |','1) CHANGE THE BORING BAR AND RE-OFFSET TAKEN THE TOOL .\r<br/>2) CROSS CHECK THE ADDITIONAL BORING BAR BEFORE LOADING .\r<br/>3) DIAL THE  BORING  TOOL IN 0.01 TO 0.02MM. \r<br/>4)COATING BORING BAR USED FOR INCREASE THE TOOL.LIFE AND PRODUCTION ACCURACY.\r<br/>|','COATING  MINIATURE BORING BAR USED FOR INCREASE THE TOOL.LIFE AND PART ACCURACY ,TO AVOID THIS TYPE OF ERRORS MAINTAIN THE TOOL KIT FOR PARTICULAR C.R.N|','EFFECTIVENESS FOUND OK.','','2018-06-12','Ravi(M)','        Ningaraj A N','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','11','','','','','','HUNDRED PERCENT ENSURE THE ALL PREVIOUS RUNNING PART AND CROSS  CHECK THE ADDITIONAL BORING TOOLS CONDITION|','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10743,'51-051','THE BOEING COMPANY','BRACKET','436272','149A7371-9627','','PSDL REV A',2,'BOEING 001C','','75801','','0000-00-00',NULL,'yes','','yes','','yes','','','','','51-051 part dia 16flat tool roughing time  tool down so part dig mark and thickness - side. 2nos part ....','dia 16 flat tool holder changing and running...|CUTTING TOOL\'S HOLDING LENGTH IS NOT SUFFICIENT|THE STANDARD CUTTING TOOL TOTAL LENGTH 110MM ONLY. IN THIS OVER HANG LENGTH IS 82MM|AS PER NC PROGRAM, THE OPERATOR HOLD THE CUTTING TOOL OVER HANG 82MM IS MUST','dia 16 flat tool holder changing  and tool offset checking  tool tightness checking , and running.|SPECIAL CUTTING TOOL WITH 150MM OVERHANG PURCHASED AND APPLIED','dia 16 flat tool holder changing  and tool offset checking  tool tightness checking , and running.|THE CUTTING TOOL WILL BE HOLD, MINIMUM 40MM IN THE HOLDER. THIS AWARENESS MASSAGE WILL PASS TO ALL PRODUCTION EMPLOYEES. ','CAPA found ok.','','2018-06-12','pe_sez(a)','                Diwakar R.B.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','01','','','','','','dia 16 flat tool holder changing and running...|PRODUCTION HOLD UP','Z3456','pe_sez|pe_sez|qas|','2018-09-17|2018-09-17|2018-09-24|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10744,'51-050','THE BOEING COMPANY','BRACKET ','741173','149A7371-9624','NA','PSDL REV A',1,'BOEING 001P','','74485','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','Dig Marked Found in Profile.','1.While running time tool broken and dig mark observed on part .This deviation is due to tool problem,\r\n|2.Cutting parameters was high','|1. Tool was changed\r<br/>2.All the tools retaining to the program ,tool offset was reset and new offset taken was taken and further continued production','|1.all the long series cutter to be checked internally and also informed to cutter supplier to check and validate the cutters before sending to us.\r<br/>2.We are on trails of WIDIA make long end mill tools and cutters with new tool configuration to eliminate above deviations.','By usage of the new tool with new configuration the CA/PA was satisfied and next produced parts was found with acceptable limit to the drawing/specifications.','','2018-06-12','Ramesh(Poojary)','Shivaraj K S,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','1','no','Slim3n-5AHS-1','pe_sez(a)','no','','|1.Machine was stopped\r\n2.All the tools was recalled and checked for the cutting edges and rigidity of the tool','Z3456','pe|qas_sez|','2018-09-17|2019-01-16|','2019-01-16',NULL,NULL,NULL,NULL,NULL,NULL),(10745,'51-041','THE BOEING COMPANY','BRACKET','741161','149A7371-9603','','PSDL REV A',1,'BOEING 001F','','72960','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Parts received from treatment were found deep dent','This is happen during the transportation as there was no safety in the inner layer of the box in which the parts were shipped','|Parts were done manual touch up as per the specification and found ok','|instruction was given to the treatment house on packaging to put extra kushan type of material surronding the inner layer of the box to avoid such paint damages during the transportation. ','Next Lot Received from the treatment supplier ,parts were checked and found visually acceptable to\r\nthe requirement ','','2018-06-12','Murali(M)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','yes','With Treatment','DN40824','POST TREATMENT','no','Misc','qas_sez(a)','no','','|parts were identified and segregated and the same was communicated to the treatment house','Z3456','qas_sez|','2019-02-20|','2019-02-20',NULL,NULL,NULL,NULL,NULL,NULL),(10746,'35A-356A','Saab AB','Pull Lift Actuator Suppor','','423Z1224-4','','---',1,'787 Forecast','','A15748','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Bore chatter mark absorbed on fine finish surface , 							\r\n','1.while boring operation running time coolant not present in boring tip.							\r\n|2.Adjust the coolant pipe direction to the boring tip.							\r\n|3.coolant supply not done properly so in the boring tip cutting edge to be clogged so bore on chatter							\r\n','|1.Adjust the coolant direction to the spindle. 							\r<br/>','|1.Training has to be conducted to all shift operators, effectiveness found ok 							\r<br/>','Effectiveness found ok','','2018-06-13','pe_sez(a)','pe_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','06','yes','Misc','pe_sez(a)','no','73249','|1.immediately stop the machine and check the all previous parts ,all parts found ok 							\r\n','Z3456','nagendra|pe_sez|qas_sez|','2018-08-01|2018-12-18|2018-12-18|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10747,'35A-356A','Saab AB','Pull Lift Actuator Suppor','','423Z1224-4','','---',1,'787 Forecast','','A15751','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','BORE OVER SIZE.','Production running time bore over size.|After 15 nos produced operator not check the insert or cutting edge.|Insert life not monitor.','|Index the insert set the bore then run the production.','|New boring bar trail in next batch.','Effectiveness found ok','','2018-06-13','pe_sez(a)','pe_sez(a)','','0000-00-00','BORE OVER SIZE.','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Assembly','','6','no','Misc','pe_sez(a)','no','73257','|Identification the rejection part.','Z3456','pe_sez|qas_sez|','2018-09-25|2018-12-18|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10748,'51A-017','THE BOEING COMPANY','BRACKET ASSY','','149A7371-3','','PSDL REV A',1,'BOEING 001D','','A15183','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Teflon paint chip off ','1.The Teflon paint chip off surrounding the rivet during pressing the rivet|2.During pressing the rivet metal to metal contact|3.In butting block the  area where the parts were butting while riviting was not uniform |4.FOD of rivet accumulated in the butting block where the part was getting butted.','|2.Butting block was made uniform by giving a uniform cut','|1.Instruction given to operator to Change the adhesive tape frequently and clean the area where the parts gets butted before pressing the rivet','Next batch wo number A15184 assembly Completed and found ok,no evidence found for paint getting chipped','','2018-06-13','pe_sez(a)','pe_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','yes','Assembly','','FINAL INSPECTION','no','Misc','qas_sez(a)','no','','|Adhesive tape was appendix on the butting block to avoid metal to metal contact','Z3456','qas_sez|','2019-01-06|','2019-01-06',NULL,NULL,NULL,NULL,NULL,NULL),(10749,'51A-053','THE BOEING COMPANY','BRACKET ASSY','','149A7371-629','','PSDL REV A',5,'BOEING 001G','','A15606','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','PAINT PEALUP(TEFLON COAT)','1.The Teflon paint chip off surrounding the rivet during pressing the rivet|2.During pressing the rivet metal to metal contact|3.In butting block the  area where the parts were butting while riveting was not uniform |4.FOD of rivet accumulated in the butting block where the part was getting butted.','|2.Butting block was made uniform by giving a uniform cut','|1.Instruction given to operator to Change the adhesive tape frequently and clean the area where the parts gets butted before pressing the rivet','Next batch wo number A15668 assembly Completed and found ok,no evidence found for paint getting chipped','','2018-06-13','pe_sez(a)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','FINAL INSPECTION','yes','Misc','qas_sez(a)','no','','|Adhesive tape was appendix on the butting block to avoid metal to metal contact','Z3456','qas_sez|','2019-01-06|','2019-01-06',NULL,NULL,NULL,NULL,NULL,NULL),(10750,'51A-051','THE BOEING COMPANY','BRACKET ASSY','','149A7371-625','','PSDL REV A',3,'BOEING 001C','','A15628','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','PAINT PEALUP(TEFLON COAT)','1.The Teflon paint chip off surrounding the rivet during pressing the rivet|2.During pressing the rivet metal to metal contact|3.In butting block the  area where the parts were butting while riveting was not uniform|4.FOD of rivet accumulated in the butting block where the part was getting butted.','|2.Butting block was made uniform by giving a uniform cut','|1.Instruction given to operator to Change the adhesive tape frequently and clean the area where the parts gets butted before pressing the rivet','Next batch wo number A15914 assembly Completed and found ok,no evidence found for paint getting chipped','','2018-06-13','pe_sez(a)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','FINAL INSPECTION','yes','Misc','qas_sez(a)','no','','|Adhesive tape was appendix on the butting block to avoid metal to metal contact','Z3456','qas_sez|','2019-01-06|','2019-01-06',NULL,NULL,NULL,NULL,NULL,NULL),(10751,'51-005','THE BOEING COMPANY','Upper Beam AFT Splice','703745B0','315Z1303-501','','NIL',1,'BOEING 001J','','71218','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','no','The quantity produced 1 number was shipped to the customer with the other shipment and this is the extra quantity of that shipment. ','Packing people was not ensured the quantity with COC quantity.','|Before closing the box packing supervisor will ensure the dispatch quantity.','|parts and applicable dispatch documents will handover to the packing people one day before to the dispatch date.','CAPA effectiveness found OK.','','2018-06-14','sppkg_sez(a)','sppkg_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','DN39929','CUSTOMER END','no','Misc','qas_sez(a)','yes','','|quantity ensured in the next dispatch.','Z3456','qas_sez|','2018-12-03|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10752,'51A-066','THE BOEING COMPANY','STRUT SUPPPORT ASSY','','113T1958-7','','PSDL REV A',2,'BOEING 001M','','A15775','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','BUSHING INTERNAL DIAMETER OVERSIZED.','1) Bore oversize during the boring operation.|2) CRC value was not given correctly.|3) End mill was used for the boring operation.','|Changed the CRC value and continued the boring operation.','|Implemented Reamer for the boring operation.','Implementation verified and found ok.','','2018-06-14','Karthineyan(V.S.)','Karthineyan(V.S.)','','0000-00-00','BUSHING INTERNAL DIAMETER OVERSIZED.','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Assembly','','5','no','Misc','assembly(assembly)','no','L07709','|Immediately stopped the boring operation and informed the supervisor.','E3456','qas|qas|','2018-11-27|2019-02-19|','2019-02-19',NULL,NULL,NULL,NULL,NULL,NULL),(10753,'47-128A','GKN Aerospace Filton','HINGE POST NO. 4','9753201','F5755106220203','NA','PART ISSUE D',1,'GS68-LTA-1-2018','','74640','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Rib thickness less than requirement.','Part loaded in reverse direction in zero point system.','Give the location type bolt in fixture for avoid the reverse direction loading.','Give the location type bolt in fixture for avoid the reverse direction loading And give the message in program for check the part direction.','CAPA FOUND OK','','2018-06-14','prodn_aero(prodn)','Dinesh kulal()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Dinesh kulal()','no','','Load the part in correct direction and then run the part.','A3456','qas_aero|','2018-07-17|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10754,'18-653A','Magellan Aerospace Bournemouth','BTM CORNER FTG F / SPAR','310682','L572 51927 200','','B00',1,'423262','','67864','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','FLANGE THICKNESS VARIATION','THE CNC SETTER RUN THE PROGRAM WHICH WAS GIVEN BY THE CAM ENGINEER. HE CHECKED THE THICKNESS WHICH WAS SHOWN IN MPS.|AS PER THE DRAWING, 0.8MM STOCK TO BE ADD PER SIDE IN ALL FLANGE THICKNESS. BUT THE PART MANUFACTURED WITH 0.8MM STOCK IN FLANGES |THE ENGINEER GAVE THE NC PROGRAM AS PER DRAWING SIZE ONLY. IN NC PROGRAM, 0.8MM STOCK NOT ADDED|THE ENGINEER NOT VALIDATE THE 3D MODEL PROPERLY ','|IN FLANGES 0.8MM STOCK ADDED.NEW NC PROGRAM COLLECTED. PROVED.','|THE SETTER WILL CONFIRM THE STOCK VALUE BEFORE MANUFACTURE THE PART. THE ENGINEER WILL REQUEST TO VALIDATE THE MODEL BEFORE GIVE THE NC PROGRAM  ','CAPA found ok and next batch produced found ok.','','2018-06-14','pe_sez(a)','Umesh B,Nataraja C V,Diwakar R.B.,','','0000-00-00','FLANGE THICKNESS VARIATION','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','3','no','i700-4','pe_sez(a)','no','','|PRODUCTION STOPPED. INFORMED TO ENGG DEPARTMENT','Z3456','qas|pe_sez|qas|','2018-07-27|2018-09-20|2018-10-12|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10755,'47-053C','GKN Aerospace Filton','SPAR MID MACHINED','8579401 2','F5755199420101','NA','A, MIS ISSUE G, F575ABSMCD Rev 39',1,'S.A.No. 6200005328','','74124','','0000-00-00',NULL,'yes','yes','yes','','','','','','','TOOL DIG MARK FOUND ON BASE DUE TO DIA 25R2 TOOL BROKENED IN RUNNING TIME','While part base finishing program running time dia 25R2 cutter\r\n<br/>was broken and part base dig so part got rejected   |While part base finishing program running time dia 25R2 cutter\r\n<br/>was broken and part base dig so part got rejected\r\n<br/>\r\n<br/>Based on the details available it looks like the threaded protion has snapped and hence cutter has come out of the adaptor.','New types of Dia25R2 cutter changed and dedicated tool running  in this CRN','|We will reanalyze the design aspect of the threaded portion of the cutter and take necessary steps to prevent such occurrence in future.\r<br/>','CA PA found ok suppler provided RCCA refer SCAR-243.\r\n\r\nHowever it is instructed to the supervisors to check the thread wear before loading to machine.','','2018-06-14','Narayanappa(G)','        Siddaramappa ','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','7','','','','','','All previous running parts are checked 20nos wall flange & base all features are ok ','E3456','pe|qas|','2018-07-02|2018-07-02|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10756,'35-282','Saab AB','GUIDE HARNESS LWR','192338B2','423Z1982-1','','---',15,'Forecast po for B787','','70918','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','yes','Is condition: Overcoat is missing on part marking, partly on some, completely on 2 pcs. On one part the label is slightly deattahached in one corner.\r\n\r\nShould be: Overcoat should be on part marking acc to BAC5307\r\nSee attached document GLB383186 Missing overcoat for pictures. Please also note that is seems like the overcoat is applied before the inc is completely dried. This has been a reoccuring issue on several part numbers so the suggestion is that the overall process of applying overcoat is reviewed and not only focused to this particular part and program.','Bar-code lacquering was carried out under poor light source.','|Informed all the assembly operator to properly ensure the coverage of lacquering on the part.','|Bar code lacquering will be carried out under proper light source.','Next batches found ok.','C65102','2018-06-15','qas_sez(a)','qas_sez(a)','OF-003069','2018-06-14','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','With Treatment','DN40578','Cust End','no','Misc','qas_sez(a)','no','','|All the similar parts in FG are rechecked and and the affected parts are reworked.','Z3456','qas|','2018-08-07|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10757,'34-065A','Magellan Aerospace Winnipeg','BASE FITTING,F/D HINGE LH','G23459','400-12780-1','NA','EM104302 Iss B,EM105092 Iss H,EM104765 Iss H',1,'C81597 Rev 001','','76011','','0000-00-00',NULL,'yes','yes','yes','','','','','','no','running time hole mill broken so part hole oversize by 0.2mm.','1.During 1st operation 5.08 hole mill broken and the hole got oblong.\r<br/>2. Roughing Operation Incomplete (Before Hole mill)\r<br/>3. Sub program sequence interchanged/ Wrong sequence called\r<br/>4. Typing Error while grouping sub-programs','1.Hole Mill changed.\r<br/>2. Program sequence corrected,\r<br/>3.Trained operators and created awareness before selecting Hole mill.','1.Corrected Program sequence is stored back in the Master copy.\r<br/>2. Operator and the supervisors are retrained.','Effectiveness Found OK.','','2018-06-15','Dhananjaya(N)','        Narasimhamurthy C','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','01','','','','','','1.Stopped Machine and new hole mill used next part found ok.','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10758,'51A-052','THE BOEING COMPANY','BRACKET ASSY','','149A7371-626','','PSDL REV A',1,'BOEING 001G','','A15804','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','PAINT PEAL UP(TEFLON COAT)','1.The Teflon paint chip off surrounding the rivet during pressing the rivet|2.During pressing the rivet metal to metal contact|3.In butting block the  area where the parts were butting while riveting was not uniform |4.FOD of rivet accumulated in the butting block where the part was getting butted.','|2.Butting block was made uniform by giving a uniform cut','|1.Instruction given to operator to Change the adhesive tape frequently and clean the area where the parts gets butted before pressing the rivet','Next batch wo number A16005 assembly Completed and found ok,no evidence found for paint getting chipped','','2018-06-16','pe_sez(a)','pe_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','yes','Assembly','','FINAL INSPECTION','no','Misc','qas_sez(a)','no','','|Adhesive tape was appendix on the butting block to avoid metal to metal contact','Z3456','qas_sez|','2019-01-06|','2019-01-06',NULL,NULL,NULL,NULL,NULL,NULL),(10759,'51A-052','THE BOEING COMPANY','BRACKET ASSY','','149A7371-626','','PSDL REV A',1,'BOEING 001G','','A15800','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','PAINT PEALUP(TEFLON COAT)','1.The Teflon paint chip off surrounding the rivet during pressing the rivet|2.During pressing the rivet metal to metal contact|3.In butting block the  area where the parts were butting while riveting was not uniform |4.FOD of rivet accumulated in the butting block where the part was getting butted.','|2.Butting block was made uniform by giving a uniform cut','|1.Instruction given to operator to Change the adhesive tape frequently and clean the area where the parts gets butted before pressing the rivet','Next batch wo number A16005 assembly Completed and found ok,no evidence found for paint getting chipped','','2018-06-16','pe_sez(a)','pe_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','yes','Assembly','','FINAL INSPECTION','no','Misc','qas_sez(a)','no','','|Adhesive tape was appendix on the butting block to avoid metal to metal contact','Z3456','qas_sez|','2019-01-06|','2019-01-06',NULL,NULL,NULL,NULL,NULL,NULL),(10760,'51A-027','THE BOEING COMPANY','BRACKET ASSY','','149A7371-35','','PSDL REV A',2,'BOEING 001E','','A15683','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','PAINT PEALUP(TEFLON COAT)','1.The Tefloan paint chip off surrounding the rivet during pressing the rivet|2.During pressing the rivet metal to metal contact|3.In butting block the  area where the parts were butting while riviting was not uniform |4.FOD of rivet accumulated in the butting block where the part was getting butted.','|2.Butting block was made uniform by giving a uniform cut','|1.Instruction given to operator to Change the adhesive tape frequently and clean the area where the parts gets butted before pressing the rivet','Next batch wo number A16006 assembly Completed and found ok,no evidence found for paint getting chipped','','2018-06-16','pe_sez(a)','pe_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','yes','Assembly','','FINAL INSPECTION','no','Misc','qas_sez(a)','no','','|Adseive tape was apixed on the butting block to avoid metal to metal contact','Z3456','qas_sez|','2019-01-06|','2019-01-06',NULL,NULL,NULL,NULL,NULL,NULL),(10761,'51-118','THE BOEING COMPANY','RIBPOST FRONT SPAR RIB 11','AJ18','112T2215-5','NA','PSDL REV -',2,'486998 MPP','','68776','','0000-00-00',NULL,'no','no','no','no','no','no','yes','yes','yes','AS IS:\r\nThe substitution raw material used is NOT Solution treated after rough machining it to less than 3 inches in all sections.\r\nSHOULD BE:\r\nFor substitute raw material M0000920, solution treat and age to T74 per BAC 5602 after rough machining all sections to less than 3 inches.','Requirement of solution treating and aging Aluminum alloy from 7175-01 to 7175-T74 was not captured by\r<br/>the engineering team during the process planning.','1) All the part nos are re-Verified to ensure there is no similar skips in process by Engineering department.\r<br/>2) Manufacturing Process Sheet (MPS) was amended by Manufacturing Engineer (ME) to include the requirement of capturing the solution treatment and aging of Aluminum alloy from 7175-01 to 7175-T74 after the completion of roughing of the part.\r<br/>3) Customer has given training on how to interpret the specification in conjunction with the engineering requirements.','1) Head Engineer or Authorized personal from the Engineering department will review and approve the planning order through ERP system before releasing to Production.\r<br/>2) \"Discus\" Auto ballooning software will be implemented tentatively on or before May 25, 2018 at CIM Tools, as this will highlight any un-captured features during the ballooning process.\r<br/>3) Quality Engineer to provide Delta FAIR capturing the missed requirements to the customer for review.\r<br/>4) Training program to be scheduled by Head Quality for the Quality engineers involved in the production and review of FAIR documents on importance of checking 100% documentation.\r<br/>5) Training program to be scheduled by Head Engineering for the engineering personnel to concentrate on the importance of capturing all the details from the Part list as well as the drawings during the planning process.','CAPA found ok. ','C61619','2018-06-16','qas_sez(a)','qas_sez(a)','CA1296263-00','2018-04-24','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','DN36792','Cust End','no','Misc','qas_sez(a)','no','','Notification of Escapement (NOE) was communicated to the customer on the escape of parts by Project Engineer.','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10762,'51A-027','THE BOEING COMPANY','BRACKET ASSY','','149A7371-35','','PSDL REV A',1,'BOEING 001E','','A15458','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','PAINT chip off','1.The Tefloan paint chip off surrounding the rivet during pressing the rivet|2.During pressing the rivet metal to metal contact|3.In butting block the  area where the parts were butting while riviting was not uniform |4.FOD of rivet accumulated in the butting block where the part was getting butted.','|2.Butting block was made uniform by giving a uniform cut','|1.Instruction given to operator to Change the adhesive tape frequently and clean the area where the parts gets butted before pressing the rivet','Next batch wo number A16006 assembly Completed and found ok,no evidence found for paint getting chipped','','2018-06-16','pe_sez(a)','pe_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','yes','Assembly','','FINAL INSPECTION','no','Misc','qas_sez(a)','no','','|Adseive tape was apixed on the butting block to avoid metal to metal contact','Z3456','qas_sez|','2019-01-06|','2019-01-06',NULL,NULL,NULL,NULL,NULL,NULL),(10763,'51A-037','THE BOEING COMPANY','BRACKET ASSY','','149A7371-63','','PSDL REV A',1,'BOEING 001E','','A15671','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','PAINT PEALUP(TEFLON COAT)','1.The Tefloan paint chip off surrounding the rivet during pressing the rivet|2.During pressing the rivet metal to metal contact|3.In butting block the  area where the parts were butting while riveting was not uniform |4.FOD of rivet accumulated in the butting block where the part was getting butted.','|2.Butting block was made uniform by giving a uniform cut','|1.Instruction given to operator to Change the adhesive tape frequently and clean the area where the parts gets butted before pressing the rivet','Next batch wo number A15936 assembly Completed and found ok,no evidence found for paint getting chipped','','2018-06-17','pe_sez(a)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','yes','Assembly','','FINAL INSPECTION','no','Misc','qas_sez(a)','no','','|Adhesive tape was appendix on the butting block to avoid metal to metal contact','Z3456','qas_sez|','2019-01-06|','2019-01-06',NULL,NULL,NULL,NULL,NULL,NULL),(10764,'51A-045','THE BOEING COMPANY','BRACKET ASSY','','149A7371-609','','PSDL REV A',2,'BOEING 001F','','A15667','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','PAINT PEALUP(TEFLON COAT)','1.The Teflon paint chip off surrounding the rivet during pressing the rivet|2.During pressing the rivet metal to metal contact|3.In butting block the  area where the parts were butting while riveting was not uniform |4.FOD of rivet accumulated in the butting block where the part was getting butted.','|2.Butting block was made uniform by giving a uniform cut','|1.Instruction given to operator to Change the adhesive tape frequently and clean the area where the parts gets butted before pressing the rivet','Next batch wo number A15759 assembly Completed and found ok,no evidence found for paint getting chipped','','2018-06-17','pe_sez(a)','pe_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','yes','Assembly','','FINAL INSPECTION','no','Misc','qas_sez(a)','no','','|Adhesive tape was appendix on the butting block to avoid metal to metal contact','Z3456','qas_sez|','2019-01-06|','2019-01-06',NULL,NULL,NULL,NULL,NULL,NULL),(10765,'51A-045','THE BOEING COMPANY','BRACKET ASSY','','149A7371-609','','PSDL REV A',1,'BOEING 001F','','A15760','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','PAINT PEALUP(TEFLON COAT)','1.The Teflon paint chip off surrounding the rivet during pressing the rivet|2.During pressing the rivet metal to metal contact|3.In butting block the  area where the parts were butting while riveting was not uniform |4.FOD of rivet accumulated in the butting block where the part was getting butted.','|2.Butting block was made uniform by giving a uniform cut','|1.Instruction given to operator to Change the adhesive tape frequently and clean the area where the parts gets butted before pressing the rivet','Next batch wo number A15948 assembly Completed and found ok,no evidence found for paint getting chipped','','2018-06-17','pe_sez(a)','pe_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','yes','Assembly','','FINAL INSPECTION','no','Misc','qas_sez(a)','no','','|Adhesive tape was appendix on the butting block to avoid metal to metal contact','Z3456','qas_sez|','2019-01-06|','2019-01-06',NULL,NULL,NULL,NULL,NULL,NULL),(10766,'51A-085','THE BOEING COMPANY','BRACKET ASSY','','332A2930-62','','PSDL REV B',6,'BOEING 001M','','A14713','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','yes','THERE ARE QTY 6 ACTUATOR BRACKETS P/N 332A2930-62\r\nTHAT HAVE THE FILLET SEAL DAMAGED AROUND THE LARGER\r\nBUSHING.THE SEALING IS PEELING OFF SHOWING VOIDS\r\nAND POOR ADHESION.','The fillet sealant deformed due to improper handling of part by the packing personnel.','1) Quality Engineer created a quality alert and displayed the same in assembly, final inspection and packing area.\r<br/>2) Instruction given to the assembly personnel to mention the start and end time of the sealant curing','In all Assembly work order the sealant curing time including duration will be added and effective from 1st week of July 2018.','CA PA found Ok and next batch production found ok.','C64587','2018-06-17','qas_sez(a)','qas_sez(a)','CA1310620-00','2018-05-11','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Assembly','','Cust End','no','Misc','qas_sez(a)','no','','Re-inspection of the similar and related parts in FG and WIP was carried out by quality inspector and approved by Quality\r\nEngineer ','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10767,'51A-054','THE BOEING COMPANY','BRACKET ASSY','','149A7371-630','','PSDL REV A',1,'BOEING 001G','','A15778','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','PAINT PEALUP(TEFLON COAT)','1.The Teflon paint chip off surrounding the rivet during pressing the rivet|2.During pressing the rivet metal to metal contact|3.In butting block the  area where the parts were butting while riveting was not uniform |4.FOD of rivet accumulated in the butting block where the part was getting butted.','|2.Butting block was made uniform by giving a uniform cut','|1.Instruction given to operator to Change the adhesive tape frequently and clean the area where the parts gets butted before pressing the rivet','Next batch wo number A15779 assembly Completed and found ok,no evidence found for paint getting chipped','','2018-06-18','pe_sez(a)','pe_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','yes','Assembly','','FINAL INSPECTION','no','Misc','qas_sez(a)','no','','|Adhesive tape was appendix on the butting block to avoid metal to metal contact','Z3456','qas_sez|','2019-01-06|','2019-01-06',NULL,NULL,NULL,NULL,NULL,NULL),(10768,'51A-031','THE BOEING COMPANY','BRACKET ASSY','','149A7371-41','','PSDL REV A',1,'BOEING 001E','','A15787','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','PAINT PEALUP(TEFLON COAT)','1.The Teflon paint chip off surrounding the rivet during pressing the rivet|2.During pressing the rivet metal to metal contact|3.In butting block the  area where the parts were butting while riveting was not uniform |4.FOD of rivet accumulated in the butting block where the part was getting butted.','|2.Butting block was made uniform by giving a uniform cut','|1.Instruction given to operator to Change the adhesive tape frequently and clean the area where the parts gets butted before pressing the rivet','Next batch wo number A15788 assembly Completed and found ok,no evidence found for paint getting chipped','','2018-06-18','pe_sez(a)','pe_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','yes','Assembly','','FINAL INSPECTION','no','Misc','qas_sez(a)','no','','|Adhesive tape was appendix on the butting block to avoid metal to metal contact','Z3456','qas_sez|','2019-01-06|','2019-01-06',NULL,NULL,NULL,NULL,NULL,NULL),(10769,'51A-038','THE BOEING COMPANY','BRACKET ASSY','','149A7371-64','','PSDL REV A',2,'BOEING 001E','','A15764','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','PAINT PEALUP(TEFLON COAT)','1.The Tefloan paint chip off surrounding the rivet during pressing the rivet|2.During pressing the rivet metal to metal contact|3.In butting block the  area where the parts were butting while riveting was not uniform |4.FOD of rivet accumulated in the butting block where the part was getting butted.','|2.Butting block was made uniform by giving a uniform cut','|1.Instruction given to operator to Change the adhesive tape frequently and clean the area where the parts gets butted before pressing the rivet','Next batch wo number A15765 assembly Completed and found ok,no evidence found for paint getting chipped','','2018-06-18','pe_sez(a)','pe_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','yes','Assembly','','FINAL INSPECTION','no','Misc','qas_sez(a)','no','','|Adhesive tape was appendix on the butting block to avoid metal to metal contact','Z3456','qas_sez|','2019-01-06|','2019-01-06',NULL,NULL,NULL,NULL,NULL,NULL),(10770,'47-172','GKN Aerospace Filton','TEE PANEL SUPPT BEAM','9753201','F5755034220501','NA','PART ISSUE D',1,'1210042824','','74836','','0000-00-00',NULL,'yes','no','no','no','no','yes','no','yes','no','Flange thickness 5+0.25/-0.2 measures 5.31/5.32\r\nWeb thickness 3.5+0.13/-0.08 measures 3.73','Due Fixture thickness under Size 0.2, Program was kept 0.2 Stock.','|New Fixture manufactured.\r<br/>Old Fixture Rejected.','|Before Loading to the Machine, Fixture Thickness has to be Ensured. ','CA PA Found ok. ','','2018-06-18','Ramesh(Poojary)','Ramesh(Poojary)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','','FI','yes','Misc','Ranjith(G)','no','','|Part was Re-worked. ','E3456','qas|','2018-09-26|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10771,'43A-001','Composite Industrie','B BRACKET ASSY','','V251 11616 000','','A00, ECN PV100298ST1AE38',1,'LTA PO-2','','K14034','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','yes','Varnish is missing.','Why-1: Part without varnish (Part-Marking Overcoat) reached customer end.|Why-2: Quality Inspector carrying out Final Inspection after assembly did not identified the part missed out with varnish.|Why-3: Methodology carried out in visual inspection was not effective. |Why-4: The parts were inspected one by one under improper lighting condition.','|1) Instruction given to all the assembly operators to recheck the parts for the completion of operations before forwarding for the next operation.\r<br/>2) Instruction given to all the Inspectors to carry out visual inspection only under the dedicated tables with proper light source.','|1) All the Quality Inspectors are instructed to follow TIN SOLDIER technique while carrying out visual inspection to avoid similar non-conformity.  ','Next Batches found ok.','C63047','2018-06-18','qas_sez(a)','qas_sez(a)','180411-031','2018-06-18','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','Assembly','','Cust End','no','Misc','qas_sez(a)','no','','|All the parts in WIP and FG are inspected and no defects found.','Z3456','qas|qas|qas|','2018-07-03|2018-07-03|2018-08-07|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10772,'43A-005','Composite Industrie','BRACKET ASSY','','V251 13495 000','','A00, ECN PV100298ST1BJ54',1,'ATA25_ACH-2945','','K04586','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','no','PARTS Rejected in Assembly.','While manually holding the two parts to make assembly Rivet get shifted. ','1.Fixture created for next batch of parts. ','1.Fixture created for next batch of parts. ','Effectiveness found ok. ','','2018-06-19','Ramesh(D)','Ramesh(D)','','0000-00-00','NC CLOSED','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Assembly','','ONSITE','no','Misc','Mahesh(DV)','yes','','While manually holding the two parts to make assembly Rivet get shifted. ','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10773,'43A-005','Composite Industrie','BRACKET ASSY','','V251 13495 000','','A00, ECN PV100298ST1BJ54',1,'ATA25_ACH-2945','','K04588','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','no','PARTS Rejected in Assembly. ','While manually holding the two parts to make assembly Rivet get shifted. ','1.Fixture created for next batch of parts. ','1.Fixture created for next batch of parts. ','Effectiveness found ok. ','','2018-06-19','Ramesh(D)','Ramesh(D)','','0000-00-00','NC CLOSED','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Assembly','','ONSITE','no','Misc','Mahesh(DV)','yes','','While manually holding the two parts to make assembly Rivet get shifted. ','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10774,'51A-051','THE BOEING COMPANY','BRACKET ASSY','','149A7371-625','','PSDL REV A',1,'BOEING 001C','','A15415','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','PAINT PEALUP(TEFLON COAT)','1.The Teflon paint chip off surrounding the rivet during pressing the rivet|2.During pressing the rivet metal to metal contact|3.In butting block the  area where the parts were butting while riviting was not uniform|4.FOD of rivet accumulated in the butting block where the part was getting butted.','|2.Butting block was made uniform by giving a uniform cut','|1.Instruction given to operator to Change the adhesive tape frequently and clean the area where the parts gets butted before pressing the rivet','Next batch wo number A15418 assembly Completed and found ok,no evidence found for paint getting chipped','','2018-06-19','pe_sez(a)','pe_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','yes','Assembly','','FI','no','Misc','qas_sez(a)','no','','|Adhesive tape was appendix on the butting block to avoid metal to metal contact','Z3456','qas_sez|','2019-01-06|','2019-01-06',NULL,NULL,NULL,NULL,NULL,NULL),(10775,'51A-042','THE BOEING COMPANY','BRACKET ASSY','','149A7371-602','','PSDL REV A',3,'BOEING 001C','','A15954','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','PAINT PEALUP(TOP COAT)','1.The Teflon paint chip off surrounding the rivet during pressing the rivet|2.During pressing the rivet metal to metal contact|3.In butting block the  area where the parts were butting while riveting was not uniform|4.FOD of rivet accumulated in the butting block where the part was getting butted.','|2.Butting block was made uniform by giving a uniform cut','|1.Instruction given to operator to Change the adhesive tape frequently and clean the area where the parts gets butted before pressing the rivet','Next batch wo number A15955 assembly Completed and found ok,no evidence found for paint getting chipped','','2018-06-19','pe_sez(a)','pe_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','yes','Assembly','','FINAL INSPECTION','no','Misc','qas_sez(a)','no','','|Adhesive tape was appendix on the butting block to avoid metal to metal contact','Z3456','qas_sez|','2019-01-06|','2019-01-06',NULL,NULL,NULL,NULL,NULL,NULL),(10776,'51A-042','THE BOEING COMPANY','BRACKET ASSY','','149A7371-602','','PSDL REV A',2,'BOEING 001C','','A15792','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','PAINT PEALUP(TEFLON COAT)','1.The Teflon paint chip off surrounding the rivet during pressing the rivet|2.During pressing the rivet metal to metal contact|3.In butting block the  area where the parts were butting while riveting was not uniform|4.FOD of rivet accumulated in the butting block where the part was getting butted.','|2.Butting block was made uniform by giving a uniform cut','|1.Instruction given to operator to Change the adhesive tape frequently and clean the area where the parts gets butted before pressing the rivet','Next batch wo number A15955 assembly Completed and found ok,no evidence found for paint getting chipped','','2018-06-19','pe_sez(a)','pe_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','yes','Assembly','','FINAL INSPECTION','no','Misc','qas_sez(a)','no','','|Adhesive tape was appendix on the butting block to avoid metal to metal contact','Z3456','qas_sez|','2019-01-06|','2019-01-06',NULL,NULL,NULL,NULL,NULL,NULL),(10777,'18-419A','Magellan Aerospace(Blackpool) Limited','BRACKET','221829','PI55-2120010-00','','NIL',1,'BPP-533304','','73291','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Base thickness - side. (0.2mm)','Base thickness is out of tolerance.|Part was not properly butted and the operator did not ensured proper butting of the part.|Operator did not ensured the part butting with filler gauge.|Inadequate training and negligence.','|1) Trained all the new operator\'s to how to check proper butting of part.','|1) All the new operators are supervised by senior operator\'s and the production supervisors.\r<br/>2) Working nature of all the new operators are monitored and adequate training is provided.','CAPA found ok.','','2018-06-19','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','3','no','Misc','Dhananjaya(N)','no','','|Checked the base thickness of all the parts and found ok.','E3456','qas|qas|','2018-07-24|2018-07-24|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10778,'18-418A','Magellan Aerospace(Blackpool) Limited','BRACKET','221829','PI55-2119010-00','','NIL',1,'BPP-533302','','73282','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Base thickens - side (0.3mm) ','Base thickness is out of tolerance.|Part was not properly butted and the operator did not ensured proper butting of the part.|Operator did not ensured the part butting with filler gauge.|Inadequate training and negligence.','|1) Trained all the new operator\'s to how to check proper butting of part. ','|1) All the new operators are supervised by senior operator\'s and the production supervisors.\r<br/>2) Working nature of all the new operators are monitored and adequate training is provided.','CA PA found ok.','','2018-06-19','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','3','no','Misc','Dhananjaya(N)','no','','|\r\nChecked the base thickness of all the parts and found ok. ','E3456','qas|qas|','2018-07-24|2018-07-24|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10779,'18-418A','Magellan Aerospace(Blackpool) Limited','BRACKET','221823','PI55-2119010-00','','NIL',1,'BPP-533302','','73281','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Base thickens - side (0.3mm) ','Base thickness is out of tolerance.|Part was not properly butted and the operator did not ensured proper butting of the part.|Operator did not ensured the part butting with filler gauge.|Inadequate training and negligence.','|1) Trained all the new operator\'s to how to check proper butting of part. ','|1) All the new operators are supervised by senior operator\'s and the production supervisors.\r<br/>2) Working nature of all the new operators are monitored and adequate training is provided.','CA PA Found Ok.','','2018-06-19','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','3','no','Misc','Dhananjaya(N)','no','','|Checked the base thickness of all the parts and found ok. ','E3456','qas|qas|','2018-07-24|2018-07-24|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10780,'35-275','Saab AB','PIN','G23122K02','426Z3601-1','','--A',2,'PA 1510 FORECAST-3','','65939','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Magnetic Particle Inspection failed','During handling scoring marks witnessed on the parts.','|Separate try and rubber sleeves introduced to avoaid the metal to metal contact that avoaids the marks on OD.','|Separate try and rubber sleeves introduced to avoaid the metal to metal contact that avoaids the marks on OD.','Next batch found satisfactory.','','2018-06-20','qas_sez(a)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','DN35047','POST DN','no','Misc','qas_sez(a)','no','','|INSTRUCT TO PACKING PERSON DONT SEND THE PARTS WITH OUT RUBBER SLEEVES.','Z3456','nagendra|','2018-08-07|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10781,'51A-028','THE BOEING COMPANY','BRACKET ASSY','','149A7371-36','','PSDL REV A',2,'BOEING 001H','','A15643','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','PAINT PEALUP(TEFLON COAT)','1.The Teflon paint chip off surrounding the rivet during pressing the rivet|2.During pressing the rivet metal to metal contact|3.In butting block the  area where the parts were butting while riveting was not uniform|4.FOD of rivet accumulated in the butting block where the part was getting butted.','|2.Butting block was made uniform by giving a uniform cut','|1.Instruction given to operator to Change the adhesive tape frequently and clean the area where the parts gets butted before pressing the rivet','Next batch wo number A15806 assembly Completed and found ok,no evidence found for paint getting chipped','','2018-06-20','pe_sez(a)','pe_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','yes','Assembly','','FINAL INSPECTION','no','Misc','qas_sez(a)','no','','|Adhesive tape was appendix on the butting block to avoid metal to metal contact','Z3456','qas_sez|','2019-01-06|','2019-01-06',NULL,NULL,NULL,NULL,NULL,NULL),(10782,'51A-028','','','','','','',0,'','','','','0000-00-00',NULL,'no','no','no','no','no','no','no','no','no','','','','','','','2018-06-20','select','','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Cancelled','no','no','no','','','','no','','select','no','','','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10783,'51A-028','THE BOEING COMPANY','BRACKET ASSY','','149A7371-36','','PSDL REV A',2,'BOEING 001H','','A15644','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','PAINT PEALUP(TEFLON COAT)','1.The Teflon paint chip off surrounding the rivet during pressing the rivet|2.During pressing the rivet metal to metal contact|3.In butting block the  area where the parts were butting while riveting was not uniform|4.FOD of rivet accumulated in the butting block where the part was getting butted.','|2.Butting block was made uniform by giving a uniform cut','|1.Instruction given to operator to Change the adhesive tape frequently and clean the area where the parts gets butted before pressing the rivet','Next batch wo number A15806 assembly Completed and found ok,no evidence found for paint getting chipped','','2018-06-20','pe_sez(a)','pe_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','yes','Assembly','','FINAL INSPECTION','no','Misc','qas_sez(a)','no','','|Adhesive tape was appendix on the butting block to avoid metal to metal contact','Z3456','qas_sez|','2019-01-06|','2019-01-06',NULL,NULL,NULL,NULL,NULL,NULL),(10784,'51A-028','THE BOEING COMPANY','BRACKET ASSY','','149A7371-36','','PSDL REV A',2,'BOEING 001H','','A15645','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','PAINT PEALUP(TEFLON COAT)','1.The Teflon paint chip off surrounding the rivet during pressing the rivet|2.During pressing the rivet metal to metal contact|3.In butting block the  area where the parts were butting while riveting was not uniform|4.FOD of rivet accumulated in the butting block where the part was getting butted.','|2.Butting block was made uniform by giving a uniform cut','|1.Instruction given to operator to Change the adhesive tape frequently and clean the area where the parts gets butted before pressing the rivet','Next batch wo number A15806 assembly Completed and found ok,no evidence found for paint getting chipped','','2018-06-20','pe_sez(a)','pe_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','yes','Assembly','','FINAL INSPECTION','no','Misc','qas_sez(a)','no','','|Adhesive tape was appendix on the butting block to avoid metal to metal contact','Z3456','qas_sez|','2019-01-06|','2019-01-06',NULL,NULL,NULL,NULL,NULL,NULL),(10785,'43A-023','Composite Industrie','FASTENING ASSY','','V531 23246 000 00','','A00, ECN PV106572ST3AC02',1,'LTA PO-1','','A13765','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','yes','Type B marking is missing','Improper identification and verification method.|','All the parts to be identified with Bag and Label are identified appropriately during the final inspection by the quality inspector.|','1) It is instructed to all the Inspectors to tag the Bag and Label with the part before individually covering it after the completion of final inspection.\r<br/>2) All the inspectors are instructed to re-verify the parts to ensure proper identification is done with respect to the drawing before certifying the same for dispatch.|','Next batches produced found OK.','C63009','2018-06-20','qas_sez(a)','qas_sez(a)','180410-039','2018-06-06','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','Assembly','','Cust End','no','Misc','qas_sez(a)','no','','All the similar parts in FG and WIP are inspected and found with proper identification.|','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10786,'51-041','THE BOEING COMPANY','BRACKET','436278','149A7371-9603','','PSDL REV A',1,'BOEING 001F','','76350','','0000-00-00',NULL,'yes','','yes','','yes','','','','','atc problem tool changing problem so part wall thickness dig mark..','atc problem tool changing problem so part wall thickness dig mark.','M/C STOP NEXT ALL TOOLS REMOVING AND M/C ATC CLEANING AND WARM UP THE TOOL CHANGING..','M/C STOP NEXT ALL TOOLS REMOVING AND M/C ATC CLEANING AND WARM UP THE TOOL CHANGING..','Information given to Maintenance team on the ATC problem.','','2018-06-20','pe_sez(a)','        Diwakar R.B.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','01','','','','','','atc problem tool changing problem so part wall thickness dig mark.','Z3456','qas|','2018-09-24|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10787,'47-110A','GKN Aerospace Filton','BLOCK COVER RH','7689502-1','D5725097420901','NA','PART ISSUE N',1,'GS68-LTA-2018','','75741','','0000-00-00',NULL,'yes','no','no','no','yes','yes','no','no','no','Thickness under size by 1mm','Running time tool broken.','Changed the broken tool and informed the tool\'s in-charge about the issue.','1) Tool life of new tools will be monitored.\r<br/>2) Informed the operator to check all the tool edges before starting the cycle.','Next batches found ok.','','2018-06-21','Lohith(K)','Shivaraj K S,Lohith K,Kiran Kumar M,Kiran KM,','','0000-00-00','suspected by machine','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','Slim3n-4AHS-3','Nandishkumar(D.K.)','no','','Checked the thickness of all the previous parts and changed the tool.','E3456','qas|','2018-10-12|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10788,'07-004C','HAL-NASIK','WALL 2 ROOT PART - LH ','AS-28214','11.2000.2.111.002','','11.2000.2.111.001;002 Iss 01',1,'NK/M/2513(4520)/MP/O','','73154','','0000-00-00',NULL,'yes','','yes','','yes','','','','','Refer This NCR No 10651\r\n(This NC Is Dummy)','Refer This NCR No 10651','Refer This NCR No 10651','Refer This NCR No 10651','Refer NC 10651','','2018-06-21','Narayanappa(G)','        Paramesh K','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','','yes','','','03','','','','','','immediately informed to supervisor and supervisor called the DMG service engineer until that machine has been stopped later on the service engineer came and solved the problem..  ','E3456','pe|qas|','2018-07-02|2018-07-10|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10789,'51-115','THE BOEING COMPANY','RIBPOST FRONT SPAR RIB 5 ','AJ16','112T2212-8','NA','PSDL REV -',1,'486998 MPP','','68737','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','no','As part marked, Qty (1) 112T2212-7 Ribpost does not\r\nmeet Dwg requirements. The incorrectly marked part\r\nmeets the configuration of a 112T2212-8 Ribpost and\r\ns/b part marked as such per SSP, Dwg 112T2212 Sht 2\r\nRev - and BAC5307 Code M.The 112T2212-8 is opposite\r\nto the 112T2212-7. MRSA QA notes that Qty (2) shims\r\nwere bonded to the part by production prior to.\r\n\r\n112T2212-8 Part was sent with the 112T2212-7 part with 112T2212-7 part mark content.','Part marking interchanged due to improper identification.','|informed the part-marking operator to verify the part to the drawing view before carrying out the part marking.','|Part marking library to be created which contains the view of the part, part marking location, and part marking content.','CAPA found ok.','','2018-06-21','qas_sez(a)','qas_sez(a)','N1560033494','2018-03-27','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','DN36415','CUST END','no','Misc','qas_sez(a)','yes','','|Checked all the parts in process and FG and no similar defective parts identified.','E3456','qas|','2019-01-03|','2019-01-03',NULL,NULL,NULL,NULL,NULL,NULL),(10790,'35-600','Saab AB','FRAME','531963C','D5227338520400','NA','PART ISSUE C',2,'PA1687 LTA-1','','73198','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Refer NC NO 10930','Refer NC NO 10930|Refer NC NO 10930|Refer NC NO 10930','|Refer NC NO 10930','|Refer NC NO 10930','Refer NC NO 10930','','2018-06-21','Krishna(Chowdary.G.P.)','Rakeshbabu(V)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','07','no','Misc','Narayanappa(G)','no','','|Refer NC NO 10930','E3456','pe|qas|','2018-07-31|2018-07-31|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10791,'51-114','THE BOEING COMPANY','RIBPOST FRONT SPAR RIB 5 ','AJ16','112T2212-7','NA','PSDL REV -',1,'486998 MPP','','68735','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','yes','As part marked, Qty (1) 112T2212-7 Ribpost does not\r\nmeet Dwg requirements. The incorrectly marked part\r\nmeets the configuration of a 112T2212-8 Ribpost and\r\ns/b part marked as such per SSP, Dwg 112T2212 Sht 2\r\nRev - and BAC5307 Code M.The 112T2212-8 is opposite\r\nto the 112T2212-7. MRSA QA notes that Qty (2) shims\r\nwere bonded to the part by production prior to','1) MPS not uploaded in the cimsoft/not flow down to the assembly person to do part mark.|2) Due to unavailability of MPS wrong part mark done|3)part marking operator not able to identified the LH and RH hence LH part mark carried for RH part. ','|1) MPS was uploaded in the CIM soft.\r<br/>2)Training was provided for both the inspectors and part marking operator to identify the LH and RH part. ','|1) MPS was uploaded in the CIM soft.\r<br/>2)Training was provided for both the inspectors and part marking operator to identify the LH and RH part. ','CA/PA found was satisfied.','C61145','2018-06-22','qas_sez(a)','qas_sez(a)','N1560033494','2018-03-27','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','DN36475','CUSTOMER END','no','Misc','qas_sez(a)','no','','|1) Internal NC was raised.\r\n2) Inspected all the FG quantities for the above deviations.\r\n3)All FG parts are found within the acceptable.','Z3456','qas_sez|','2019-01-05|','2019-01-05',NULL,NULL,NULL,NULL,NULL,NULL),(10792,'35-162','Saab AB','BEAM-LOWER_INNER_AFT','583271A2','423Z1403-2-02','','---',1,'1600068414','','28797','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','part dig mark observed\r\n','The movement of the FG peenya to SEZ site during this transport damage observed.\r\n','|Other Fg parts checked Found ok\r<br/>','|instruct paking personal to aviod this transport damage by using wrapping the bubble sheet or foam sheet \r<br/>','Next batch Found oK','','2018-06-22','QA(App)','QA(App)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','DN10919','On site','no','Misc','QA(App)','no','','|Other Fg parts checked Found ok\r\n','E3456','nagendra|','2018-08-10|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10793,'51-136','THE BOEING COMPANY','CLEVIS - LOWER, LH THREAD','H7J11/161021','112A7112-4','NA','PSDL REV B',1,'BOEING 001W','','76113','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','1.Part running time rotated.\r\n2.part slot width over size . ','program cutting direction wrong .','change the program tool path immediately,','|Visual Checklist will be done','CAPA FOUND OK ','','2018-06-22','Ramesh(Poojary)','Ramesh(Poojary)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','07','no','Misc','Gurukiran S(M)','no','','change the program tool path immediately,','E3456','cam|qas|qas|','2018-08-07|2018-12-19|2018-12-19|','2018-12-19',NULL,NULL,NULL,NULL,NULL,NULL),(10794,'51-114','THE BOEING COMPANY','RIBPOST FRONT SPAR RIB 5 ','AJ16','112T2212-7','NA','PSDL REV -',1,'486998 MPP','','69511','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Tool Dig','the tool was over hanged |Mimi mum clamping area for the is 30 mm ,but the operator has clamped for 20 mm|The tool offset taken was not validate and compared with the log book in which previous batch tool offset was recorded|The operator didn’t follow the Instruction given in the MPS','|1.Awareness given to operators to follow the instruction given in the MPS and to follow the check list provided for setting.\r<br/>2.Intruction given to all the operators to get the check list approved from the supervisor and senior opeartors once the setting is done.','|refer CA','next batch wo #79770 machined and found Ok','','2018-06-23','qas_sez(a)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','yes','With Treatment','','FI','no','Misc','qas_sez(a)','no','','|1.The part was rejected and internal NCR was raised.\r\n2.All the tools pertaining to the program was recalled and new offset was taken.','Z3456','qas_sez|','2019-04-16|','2019-04-16',NULL,NULL,NULL,NULL,NULL,NULL),(10795,'51-084A','THE BOEING COMPANY','BRACKET DETAIL','763731','332A2930-63','NA','PSDL REV B',2,'BOEING 001U','','74028','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','*BORE OVER SIZE.','While part running time new tool added but CRC D VALUE not entered.|Measure and ensure  the Bore diameter value |Cross check the CRC value in  tool offset D value |Enter the correct CRC value in tool offset D value','|Enter the correct CRC value in tool offset D value','|Before Run the Bore program Cross check the CRC value in tool offset D value and M00  MSG given inside the program multiple commands.   ','Next Batches found ok.','','2018-06-23','pe_sez(a)','pe_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','3','no','Misc','pe_sez(a)','no','','|Previous part Bore value measured and ensure','Z3456','pe_sez|qas|','2018-09-11|2018-09-14|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10796,'47-172','GKN Aerospace Filton','TEE PANEL SUPPT BEAM','9753201','F5755034220501','NA','PART ISSUE D',1,'1210042824','','74836','','0000-00-00',NULL,'yes','no','no','no','no','yes','no','yes','no','Flange thickness 5+0.25/-0.2 measures 5.31/5.32\r\nWeb thickness 3.5+0.13/-0.08 measures 3.73','Due Fixture thickness under Size 0.2, Program was kept 0.2 Stock.','New Fixture manufactured. \r<br/>Old Fixture Rejected.','Before Loading to the Machine, Fixture Thickness has to be Ensured.','CA PA Found ok.','','2018-06-23','Ramesh(Poojary)','Ramesh(Poojary)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','','FI','yes','Misc','Ranjith(G)','no','','Part was Re-worked.','E3456','qas|','2018-07-31|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10797,'51-136','THE BOEING COMPANY','CLEVIS - LOWER, LH THREAD','H7J11/161021','112A7112-4','NA','PSDL REV B',1,'BOEING 001W','','76415','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','part profile not achieved \r\n','Due Wrong tool loaded.|Due to refereeing the data sheet.|Due to manual editing of the tool name.|Program cannot be read by the machine without manual editing.|CAM Software doesn’t output the program name as machine required.','|Program was changed and program proved part found OK, Obsolete the old program and new proved program saved in to data base.','|When giving the program the program name will be four eye checked.','Next batches found ok.\r\nError communicated to the software supplier and expected to be addressed during the upcoming updates.','','2018-06-24','Ramesh(Poojary)','Nandeep()','','0000-00-00','part profile not achieved ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','07','no','Misc','Gurukiran S(M)','no','','As per customer drawing,part profile not achieved.|Program was changed and program proved part found OK','E3456','cam|qas|','2018-08-06|2018-10-12|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10798,'47-188','GKN Aerospace Filton','BRKT JACK MTG (INNER)','9753201','F5755203020101','NA','PART ISSUE A',1,'1210042824-1','','76990','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dia 4.83 hole over size.','While part running time dia 4.83 hole over size.|Overhang the tool length, so tool run out.   ','|Inform to operator long tool loading time check the run-out mandatory  ','|Inform to operator long tool loading time check the run-out mandatory','CA/PA found ok.','','2018-06-24','pe_sez(a)','Shivaraj K S,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','3','no','Slim3n-4AHS-1','pe_sez(a)','no','','|Change the proper holder after continue the production.','Z3456','pe_sez|mahesh_sez|','2018-09-11|2018-09-11|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10799,'51-135','THE BOEING COMPANY','CLEVIS - UPPER, RH THREAD','B7F57/160812','112A7112-3','NA','PSDL REV B',1,'BOEING 001W','','76412','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','DUMMY ','','','','DUMMY','','2018-06-24','Ramesh(Poojary)','Nandeep()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','With Treatment','','07','no','Misc','Gurukiran S(M)','no','','part dept of cut 1mm so part rotated. ','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10800,'18-117B','Magellan Aerospace Bournemouth',' 	HOUSING-OUT BD BRG','1593408-2/SDKC','PID275 40004 200','','C01',1,'423253','','74173','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','collar thickness undersized. ','while after changing the finishing insert this problem was occurred |','1)After changing the insert taken the both x and z offset.\r<br/>2)For the safety purpose taken safer side in wear offset.\r<br/>3)Before given the cut check the every parts run-out \r<br/>4)Setting time using the new cutting edge inserts.\r<br/>5)Ensure the all tool nose radius and jaws run-out    |','For the purpose to avoid this type of errors we are given the training about pre-post setting check list.|','EFFECTIVENESS FOUND OK.','','2018-06-25','Ravi(M)','Ashoka(R)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','011','no','Misc','Narasimhamurthy(K.G.)','no','','Check the all previous running part and segregate the parts separately   |','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10801,'53A-002','','','','','','',0,'','','','','0000-00-00',NULL,'no','no','no','no','no','no','no','no','no','','','','','','','2018-06-25','select','','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Cancelled','no','no','no','','','','no','','select','no','','','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10802,'53A-002','Triumph Aerostructures','FORK FITTING ASSY','','F579 53444 002 A02','','PART ISSUE A',2,'LTA Triumph ASSY 201','','A16109','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','no','BUSH CAME OUT OF FLANGE WHILE DOING ASSEMBELY','|','|','|','THIS PROBLEM WILL NOT APPEAR IN FUTURE','','2018-06-25','qas_sez(a)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','FI','yes','Misc','Manu()','yes','','THICKNESS MAINTAINED IN MEAN|','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10803,'35A-671','Saab AB','SHAFT LEVER ASSY','','D5227346201800','','PART ISSUE D',1,'OWED-LTA-001','','A16191','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','wrong fixture selection so part bend.','wrong fixture selection so part bend.|The fixture was not identified','|The fixture is identified with fixture number','|The fixture number is identified in APS and during assembly process which will be follow as per APS','CAPA found ok','','2018-06-25','Ramesh(D)','Ramesh(D)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Assembly','','OP 03','no','Misc','Ramesh(D)','no','','|The correct fixture was selected','E3456','qas|','2018-12-20|','2018-12-20',NULL,NULL,NULL,NULL,NULL,NULL),(10804,'35A-600','Saab AB','FRAME ASSY','','D5227338500800','','PART ISSUE C',21,'1600214688','','A15883','','0000-00-00',NULL,'no','no','no','no','no','no','yes','yes','yes','Is: Selant is not applied correctly in hole in area H12 in drawing D52273385. The sealant doesn\'t cover the unprotected area. See picture.\r\nShould be: Sealant should be applied in accordance with AIPS-01-02-019 section 4.1.3.1: The sealant shall similarly be applied on any area of the housing which remains unprotected (seats, countersinks, fillet radii, etc.).\r\n\r\nWO No.:A15884 Qty-15 Is also subjected for the same issue.','Part is accepted as per the drawing and specification requirement.|Part is accepted as per the drawing and specification requirement.|Part is accepted as per the drawing and specification requirement.','|Part is accepted as per the drawing and specification requirement.','|Part is accepted as per the drawing and specification requirement.','Part Accepted.','C65950','2018-06-26','qas_sez(a)','qas_sez(a)','OF-003081','2018-06-21','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','Assembly','','Cust End','no','Misc','qas_sez(a)','no','','|Part is accepted as per the drawing and specification requirement.','Z3456','qas|','2018-08-07|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10805,'18-355C','Magellan Aerospace Wrexham','SADDLE C / R STRAKE','1573454-3/QGDH','F575 51398 201 PF','','C',1,'162895','','72944','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Profile dig mark occurred (new operator)','Wrong part loading done on machine|1)Part improperly butted on the vice.|2)Operator did not ensured the proper butting of part during loading.|3)Information\'s given in the MPS was not sufficient to ensure the proper butting of part.|4)Butting view and the RM Dimension mentioned in the MPS was not clear.','Operator was educated and Profile marking program is additionally added||1) Instruction given to all operators in the proper loading of part during the first setup operation.\r<br/>\r<br/>2) Additional profile program was included to mark the profile on the part by removing minimum thickness to ensure correct loading of the part before starting the cycle.','Profile marking program is additionally added||1)MPS to be revised to correct the butting method and dimension and to include the revised program on or before 30-Jul-2018.','CA PA found ok.','','2018-06-26','Dhananjaya(N)','        Dhananjaya N','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','03','','','','','','Machine was stopped and instructions given to the operator regarding the specific part loading on machine||Stopped the machine and instructed the operator on how to load the part.','E3456','qas|qas|','2018-09-05|2018-09-05|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10806,'51-070','THE BOEING COMPANY','FITTING, OUTBD','374831','112T7057-7','NA','PSDL REV -',1,'BOEING 001Q','','74042','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','A chips in boring bar holder while tool changing by CNC mode in the machine so tool becomes run out and bore over size.','A chips in boring bar holder while tool changing by CNC mode in the machine so tool becomes run out and bore over size.','|Inform to operator boring operation running before clean the tool pockets and spindle.\r<br/>Every time boring operation running clean the ATC arm.','|1) M0 optional program stop was provided in the program.\r<br/>2)Training provided to all operators and supervisors for visual inspections in the intermediate CNC stop to ensure no chips in the bore and tool.\r<br/>3)The same above alert was displayed near the machine.','CA/PA found satisfied.','','2018-06-28','pe_sez(a)','Umesh B,NataRaj.CV ,Diwakar R.B.,','','0000-00-00','FINE BORE GOT OVALITY','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','3','no','i700-4','pe_sez(a)','no','','|1.M0 intermediate stop or optional stop was given in the program to ensure if any chips in tools and for tool cleaning. ','Z3456','qas_sez|','2019-01-16|','2019-01-16',NULL,NULL,NULL,NULL,NULL,NULL),(10807,'43-013','Composite Industrie','B BRACKET','1750027542','V251 11738 200','','A00, ECN PV100298ST1BP90',1,'LTA PO-2','','72801','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Dig mark found on part.','1) Used wrong length  bolt.\r\n|2)Mixed both previous setting bolts and present setting bolts on the table.\r\n|3)Inefficient house keeping. ','|Checked the bolt length and replaced with correct length bolts loaded next part found OK. ','|1) Take out of unnecessary bolts away from the working table.\r<br/>2)All the bolts and nets in the shop floor are separated and sorted.    ','CA PA Found ok. All the Bolts are stored and identified separately.','','2018-06-28','Subramanya L(Naik)','        Shivappa M B','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','3','','','','','','|Checked all previous parts found OK.','E3456','pe|qas|','2018-07-07|2018-07-26|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10808,'35-644','Saab AB','LATCH FORK','LL0109408','D5227348920400','NA','C',8,'OWED-LTA-004','','73187','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no',' 19.05 bore over size.','1part running time chips present in spindle so tool run out occur 							\r\n|2.To give the proper training for operator while running time check the tool clamping before running 							\r\n|3.Monitor to check the tool-holder for bore finish tool 							\r\n|4.inform to all operators and check the critical dimension 1:1 ratios 							\r\n|5.Further parts are found ok 							\r\n','|Clean the tool holder and spindle,ATC ARM 							\r<br/>','|1.once a week clean the ATC Shutter and information pass the all 3 shift operator,							\r<br/>2.TO every part setting time to check and ensure the m/c ATC arm and shutter door . 							\r<br/>','CAPA FOUND OK','','2018-06-28','Krishna(Chowdary.G.P.)','Rakeshbabu(V)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','05','no','Misc','Anjinamurthy(H)','no','','|Based on the usage of the part [Assembly Requirement], since a shaft gets into the bore, the checking method was changed and all the rejected parts were subjected to re-inspection using a GO and NOGO Plug Gage. 							\r\n','E3456','pe|qas|','2018-08-12|2018-08-12|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10809,'35-644','Saab AB','LATCH FORK','LL0109408','D5227348920400','NA','C',37,'OWED-LTA-004','','73188','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Due to ovality in the internal diameter at a single point which was inspected by Bore Gage, 17 Nos .and 37 Nos were found to be defective [by 0.01 mm to 0.02mm]','','','','Parts accepted NC closed.','','2018-06-28','Krishna(Chowdary.G.P.)','Rakeshbabu(V)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','With Treatment','','05','no','Misc','Anjinamurthy(H)','no','','|Based on the usage of the part [Assembly Requirement], since a shaft gets into the bore, the checking method was changed and all the rejected parts were subjected to re-inspection using a GO and NOGO Plug Gage.','E3456','qas|qas|','2018-07-20|2018-10-12|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10810,'51-072','THE BOEING COMPANY','BANJO FITTING','G23991K05','113T1204-2','NA','NIL',1,'BOEING 001S','','73101','','0000-00-00',NULL,'yes','yes','yes','','','','','','','od under size -0.04mm  ','Why 1: Outer diameter undersized.|Why 2: Operator entered the offset wrongly to the roughing tool instead of finishing tool.|Why 3: Operator did not ensured the tool before giving the work offset.|Why 4: Lack of concentration.','|Changed the tool from the tool pocket and placed in provided re-took the work offset.','|Roughing and finishing tool will be clamped to alternate holders and double check will be carried out before conforming the offset and continuing production.','Operator effectiveness will be monitored for next 10 Batches.','','2018-06-28','Ravi(M)','        Sunil Gowda B N','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','11','','','','','','|Immediately stopped the machine changed the work offset to the correct tool.','E3456','pe|qas|qas|','2018-07-03|2018-08-09|2018-08-09|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10811,'35-227A','Saab AB','HINGE BRACKET 2','4755501 1','D576 50005 204','','D00',1,'1600223433/Forecast ','','75044','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Base Thikness Less Then Requirment.up to 0.7MM','Clamps overtighting ,so part DIG.','|I telling to all operaters clamps not over tighting & observe the clamps buttom chips.','|when this CRN loading the machine we are take care of clamps.','CAPA FOUND OK','','2018-06-28','prodn_aero(prodn)','Kiran.K.S(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Kiran.K.S(K)','no','','|Clamps not over tighting & clamps tighting only in man power/hand tighting.','A3456','prodn_aero|qas_aero|','2018-07-07|2018-07-17|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10812,'35-412','Saab AB','BRACKET','531882E','D5227341220000','','A',1,'OWED-LTA-001','','73868','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','deep dent found on the part during the receiving inspection.','During receipt of parts, plating found to be shipping off.\r\n\r\n|During transit parts have rub with one another|Due to insufficient packing.','|1)Improved the packing method. ','|1)Improved the packing method.\r<br/>2)Additionally packing sleeve will be put on the Outer surface of the part. ','Next batch found ok.','','2018-06-28','Yashawantha(NH)','','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','DN41930','POST TREATMENT','yes','','qas_sez(a)','no','','|informed to Supplier, verified parts at supplier end before dispatch to CIM. ','E3456','qas|','2019-01-06|','2019-01-06',NULL,NULL,NULL,NULL,NULL,NULL),(10813,'51A-070','THE BOEING COMPANY','FITTING ASSY, OUTBD','','112T7057-3','','PSDL REV -',1,'BOEING 001Q','','A16082','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','no','Planed operations as per the assembly process sheet(APS) APS/51A-070 REV-00 was completed without\r\naccepting/signing on the work orders for the below work order numbers.\r\nA16082 A16083 A16084 A16085 A16086 . And one quantity from the work order A16082(1) bearing assembly test was failed after required load applied','1) Operator did not signed the work order immediately after completing the operation.|2) All the work orders were placed separately and were usually signed later the completion of all operations.|3) Organization process was not followed by the assembly personnel.','|Signed the work orders with the recorded data of assembly and returned the completed work order.','|Training given to all the assembly personnel regarding the AAM requirement and informed them to check weather previously completed operation is signed before starting the new operation.','Work orders of the parts in Assembly in process, Inspection and in Finished Goods were cross checked and found ok.','','2018-06-29','pe_sez(a)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','FI','yes','','qas_sez(a)','yes','','|Informed all the assembly operators and supervisors to check all the parts and work orders for signature of acceptance for all the completed operations through out the CIM.','Z3456','qas|','2019-05-17|','2019-05-17',NULL,NULL,NULL,NULL,NULL,NULL),(10814,'51A-006','','','','','','',1,'','','','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','yes','Wrong part mark was used.','','','','','','2018-06-29','qas_sez(a)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','','','CUSTOMER END','yes','','qas_sez(a)','no','','','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10815,'35-235A','Saab AB','JACK BRACKET 1 ','253414B7','D576 50009 206','','D00',1,'1600223433/Forecast ','','74868','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','','part Base tool dig mark. |Operator tool offset wrong enter.|Tool offset taken in zoller system and enter in note book.|Same tool offset enter in same tool geometry but enter time operator typing error.|Entering the Offset after cross check once again.','|Enter correct tool offset run production.','|In farther tool offset enter in directly load in zoller to machine','CAPA FOUND OK','','2018-06-30','Rangaswamy()','Manukumar(H M)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','05','no','Misc','Rangaswamy()','no','','|Enter correct tool offset run production.','E3456','pe|nagendra|','2018-07-05|2018-07-25|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10816,'53-018','Triumph Aerostructures','SPREADER PLATE ','755621','F574 50703 200 A01','NA','PART ISSUE A, ECN PG49999STLX239',1,'LTA TRIUMPH 2018','','76545','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dig mark on part. (0.3mm)','1)a)  Operator missed to sign the work order after the completion of operation.\r\nb) Bearing failed load test after assembly.\r\n|2) a) Due to lack of awareness operator missed to sign the work order.\r\nb) Due to low pressure during the staking operation the bearing failed during the load test.\r\n|3) b) The pressure dropped due to leakage in the hose.','|a) Informed all the operators to sign the work order immediately after the completion of operation.\r<br/>b) Informed the maintenance department and changed the hose.\r<br/>','|1) Refresher training given to all the operators on the importance of Acceptance Authority Media.\r<br/>2) All air hoses will be checked for leakage weekly once.\r<br/>','CA PA found ok.','','2018-06-30','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','1','no','','Dhananjaya(N)','no','','|Immediately checked all the completed parts and found ok.\r\nImmediately checked all the work order in-process and signed the work orders for completed operations.\r\n','E3456','qas|','2019-04-26|','2019-04-26',NULL,NULL,NULL,NULL,NULL,NULL),(10817,'53-006','Triumph Aerostructures','STRAP ( STRG 4 )','510539','F572 50890 202 00','NA','PART ISSUE A',1,'LTA TRIUMPH 2018','','75967','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','THICKNESS MINUS 0.6 MM ','1.Part was lifted while running time so thickness was undersized.|2.Part running time bolt head broken.','|Informed the operators to change the bolt for every 20nos','|A particular BOLT KIT has been made for this CRN.','CAPA FUOND SATISFACTORY','','2018-06-30','Rangaswamy()','Rangaswamy()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','Misc','Manu()','no','','|Checked the previous machined parts found ok.\r\nChanged the bolt for next batch of production.','Z3456','pe_sez|qas_sez|','2019-01-17|2019-02-13|','2019-02-13',NULL,NULL,NULL,NULL,NULL,NULL),(10818,'18-392B','Magellan Aerospace Bournemouth','END COVER','19278','D278 50167 200','','D',11,'423241','','75420','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','ID OVERSIZE BY 0.01MM TO 0.03MM','1) Operator did not ensured the Inner Diameter of the part to the drawing requirement.\r\n\r\n|2) The operator did not calculated the Air gauge reading properly.|3) The Air gauge was set to Dia. 40.011mm and it has to be measured between -11Micron and +14Micron, but the operator calculated the air gauge reading as 40.00mm and +25Micron.|4) Inadequate knowledge on the measuring instrument.','|1) Corrected the Wear offset in the machine according to the drawing requirement and checked the next part and found ok.\r<br/>2) Informed all the Operator\\\'s to once again recheck the master and the reading in both air gauge and bore gauge before using the instrument to check the part.','|Fresher training is given to the new operator and refresher training is planned to be given to all the senior and experienced operator\\\'s on the measuring instruments.','CA PA found ok.','','2018-06-30','Dinakar(K)','Rudresh(k)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','01','no','Misc','Dinakar(K)','no','','|Stopped the machine and inspected all the previously completed parts and found a total of 11 no\'s non-conforming.','E3456','bmandyam|qas|','2018-07-31|2018-08-01|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10819,'35A-613','Saab AB','ASSY LEVER 1','','D5227280500100','','PART ISSUE A',1,'OWED-LTA-003','','A16212','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','IN PROCESS WHILE ASSEMBLY DENT DONE BY OPERATOR.','1) Part dented during the assembly operation because of improper tool.|2) Tool fixed during the assembly operation was not subjected to hardening operation because of which the tool got blunted and dented the part.','|New tool made and continued the assembly.','|sent the new tool for hardening and in future all the high strength tool\'s will be subjected to hardening process before put to use.','CA Pa found ok.','','2018-06-30','Phaniraj(G)','Phaniraj(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','IN PROCESS','yes','','Phaniraj(G)','no','','|Immediately stopped the assembly and informed the supervisor.','E3456','qas|','2019-04-26|','2019-04-26',NULL,NULL,NULL,NULL,NULL,NULL),(10820,'35A-469','Saab AB','ASSY ROD','','D522 73514 000 00','','A',1,'OWED-LTA-004','','K16244','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Length not adjusted properly.','1) Length not adjusted according to the drawing during the assembly process.|2) usually the length was calculated based on the number of rotations manually during the assembly.|3) No jig fixture was available to ensure the length.','|Adjusted the length of the part and informed all the assembly operator to ensure the length with vernier at every stage.','|Checking jig will be designed to check the length.','CA PA found ok.','','2018-06-30','Ramesh(D)','Ramesh(D)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','IN PROCESS','yes','','Ramesh(D)','no','','|Checked all the completed parts for length adjustment with vernier and found ok.','E3456','qas|','2019-04-26|','2019-04-26',NULL,NULL,NULL,NULL,NULL,NULL),(10821,'35A-470','Saab AB','ASSY ROD','','D522 73514 001 00','','A',1,'OWED-LTA-004','','K16251','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Length Adjustment properly not done.','1) Length not adjusted according to the drawing during the assembly process.|2) usually the length was calculated based on the number of rotations manually during the assembly.|3) No jig fixture was available to ensure the length.','|Adjusted the length of the part and informed all the assembly operator to ensure the length with vernier at every stage.','|Checking jig will be designed to check the length.','CA PA found ok.','','2018-06-30','Ramesh(D)','Ramesh(D)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','IN PROCESS','yes','','Ramesh(D)','no','','|Checked all the completed parts for length adjustment with vernier and found ok.','E3456','qas|','2019-04-26|','2019-04-26',NULL,NULL,NULL,NULL,NULL,NULL),(10822,'46-018A','Mahindra Aerostructures Pvt.Ltd','STRAP','5095403 2','D575-41654-200MH','','E01',1,'MAPL Forecast ','','76438','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Dig mark observed on face.','Material in the bolting region rotated and tilted the part from its original orientation therefore part got dig.|Due to inadequate clamping of the part with bolt the extra material in the clamping leg rotated and shifted the part.|operator used the bolt of smaller length which resulted in the inadequate clamping of the part.|operator was unaware of the bolt length to be used.','|1) Instructed all the operator to use the proper bolt length based on the RM thickness.','|1) Instructed all the operator to use the bolts that are 10mm extended from the material surface.','CA PA found ok.','','2018-06-30','Rangaswamy()','        Kiran KM','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','3','','','','','','|Immediately stopped the machine checked the thickness of the previously completed parts and changed the length of the bolt.','Z3456','pe_sez|pe_sez|qas|qas|','2018-07-02|2018-07-30|2018-07-30|2018-09-04|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10823,'46-013A','Mahindra Aerostructures Pvt.Ltd','STRAP','2535503 5','D575-50167-201MH','','D01, ECN NG26090ST1KC94',1,'MAPL Forecast ','','76131','','0000-00-00',NULL,'yes','yes','yes','','','','','','','part running dia. 8mm flat end mill broken so part dig mark..','Tool broken due to overload during the machining time.|The material removed was high due to high depth of cut given by supervisor. |Trial was carried out to reduce the cycle time of the machine in the roughing stage.','|Informed all the supervisors to carry out cycle reduction process with proper guidance from the engineering team.','|Instruction given to all supervisor and operator to not to change the feed rate and depth of cut parameters other than the one specified by the Engineering team in the program.','CAPA found ok.','','2018-06-30','Rangaswamy()','        Manikanta AV ','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','3','','','','','','|stopped the machine and changed the new tool and continued the old process.','Z3456','pe_sez|qas|qas|','2018-07-02|2018-07-30|2018-09-04|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10824,'35-589','Saab AB','BEAM','515015A','D5227341020200','NA','PART ISSUE B',1,'OWED-LTA-001','','75618','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Overall part shifted up to 15mm.','Fixture loaded reverse direction in ZPS .','','Give the dowel pin at bottom face of the fixture for avoid the reverse direction fixture loading and give the message in starting program to check the fixture side.','CAPA FOUND OK','','2018-07-01','prodn_aero(prodn)','prodn_aero(prodn)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Dinesh kulal()','no','','Correct the fixture direction then run the production.','A3456','qas_aero|','2018-07-17|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10825,'51-135','THE BOEING COMPANY','CLEVIS - UPPER, RH THREAD','B7F57/160812','112A7112-3','NA','PSDL REV B',1,'BOEING 001W','','76703','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','part rotated due to over load  ','Depth of cut Problem','|Informed the operator to run the revised program.','|New program back up updated in the server and the old program moved to obsolete.','CA PA found ok.','','2018-07-02','Ramesh(Poojary)','Ramesh(Poojary)','','0000-00-00','part rotated','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','7','no','','Gurukiran S(M)','no','','change the program 1mm instead of 0.5mm ','E3456','qas|','2019-04-26|','2019-04-26',NULL,NULL,NULL,NULL,NULL,NULL),(10826,'35-225A','Saab AB','HINGE BRACKET 1 ','4761501 1','D576 50004 206','','D00',1,'1600223433/Forecast ','','74964','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Bore Under Size 0.005MM to 0.015MM','Why-1: Part with ovality got mixed up with the correct parts and reached final inspection.|Why-2: End mill was used to carry out the boring operation in Slim3n-5AHT-1 as there was no provision to clamp the boring tool in the machine and this resulted in ovality of the part.|Why-3: Trial of proving part in Slim was carried out to have an alternative for the Mazak and the rework was planned to be completed at the end of the production of that batch so the part was kept separate without identification.|Why-4: During the shift change there due to communication gap the part separated for rework got mixed up with the good parts and got handed over to Inspection for final inspection.','|Instruction given to all the operators to properly identify the parts with identification tag immediately after identifying the deviation from requirements.','|1) 100% part will be checked near the machine and the rework will be completed immediately in the machine.','CA PA Accepted and the part found acceptable after rework.','','2018-07-02','Rangaswamy()','Shivaraj K S,Kiran Kumar M,Kiran KM,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','','FI','yes','Slim3n-5AHT-1','qas_sez(a)','no','','|Immediately after the identification of ovality in the part the part was separated and the machine was stopped and adjusted the C.R.C. value to eliminate the ovality.','Z3456','qas|qas|','2018-07-05|2018-07-26|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10827,'53-009','Triumph Aerostructures','STRAP ( STRG 4 )','510539','F572 50890 302 00','NA','PART ISSUE A',1,'LTA TRIUMPH 2018','','76523','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Hole oblong due to chips present in holder.','1.Chips present in spindle.|2.|2.while running reamer H7 hole over size by 20 micron.','|Cleaned the spindle and tool holder','|Every setting time clean the ATC arm,spindle and tool holder.\r<br/>Inform to every shift operators to ensue the ATC,spindle and tool holders.','CAPA FOUND SATISFACTORY','','2018-07-02','pe_sez(a)','Manikanta AV()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','Misc','Manu()','no','','|Checked the previous machined parts,found ok.','Z3456','pe_sez|pe_sez|pe_sez|qas_sez|','2018-10-11|2019-01-17|2019-01-17|2019-02-13|','2019-02-13',NULL,NULL,NULL,NULL,NULL,NULL),(10828,'35-232A','Saab AB','HINGE BRACKET 4 ','4756501 2','D576 50007 209','','E00',1,'1600223433/Forecast ','','76776','','0000-00-00',NULL,'yes','yes','yes','','no','','','no','','During operation part was lift.','Tool over hang length maximum length reached ,|operation on this type of parts will change the process.|part clamping and tool rigidity identify ,  |Clamping of the part was not adequate.|Parts was clamped in the machine with the help of vice and proper torque wrench was also used during clamping process but the part lifted during the machining process.','|while proving the fair the length tool can not be used  |1) Immediately stopped the machine and informed the operators to apply additional tightness to the clamping and to run the machine in reduced cycle speed.\r<br/>2) Communicated the engineering team about the issue and instructed to change the Jaws of the vice. ','|while proving the fair the length tool can not be used .and information passed on production team |All similar vice with unhardened jaws are scrapped and instructed the Engineering team to provide with new jaws which has under gone hardening process. ','CAPA FOUND OK','','2018-07-02','Rangaswamy()','        Kiran Kumar M','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','1','','','','','','|inform to cad team ,to change the process |All the parts were rechecked to ensure there is any dimensional deviation and found ok. ','Z3456','pe_sez|pe|pe_sez|pe_sez|qas|','2018-07-02|2018-07-07|2018-07-11|2018-07-12|2018-08-12|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10829,'51-045','THE BOEING COMPANY','BRACKET','436263','149A7371-9611','','PSDL REV A',1,'BOEING 001F','','75486','','0000-00-00',NULL,'no','yes','yes','yes','no','no','no','no','no','RM PROBLEM','','','','','','2018-07-02','Rangaswamy()','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Cancelled','no','yes','no','With Treatment','','1','no','','Rangaswamy()','no','','','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10830,'35-480A','Saab AB','LOCK LEVER','C90875','D5227349820000','NA','PART ISSUE B',1,'OWED-LTA-003','','73790','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','outer profile - side (program wrong)','NC program wrong generated.|Tool path is not defined correctly.','|Changed the program and continued the production.','|Program will be simulated, and reviewed before releasing to production.','CA PA found ok.','','2018-07-02','Ramesh(Poojary)','Ramesh(Poojary)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','3','no','','Dhananjaya(N)','no','','|Immediately stopped the machine and informed the engineering department.','E3456','qas|','2019-04-26|','2019-04-26',NULL,NULL,NULL,NULL,NULL,NULL),(10831,'35-480A','Saab AB','LOCK LEVER','C90875','D5227349820000','NA','PART ISSUE B',1,'OWED-LTA-003','','73791','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','DRILL OUT PROBLEM','Dummy NC|Dummy NC|Dummy NC|Dummy NC|Dummy NC','|Dummy NC','|Dummy NC','NC repeated while raising. NC Closed.','','2018-07-03','Sandhesh D(S)','Sathisha(K.C.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','07','no','','Sandhesh D(S)','no','','|Dummy NC','E3456','qas|qas|','2018-07-25|2018-07-25|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10832,'51-127','THE BOEING COMPANY','NUT','71770/03/00','251W4145-2','NA','PSDL REV A',1,'BOEING 001Q','','75845','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','OD UNDER SIZE BY -0.5MM.','1)OPERATOR INSTEAD OF GIVING STOCK FOR ID PROGRAM MISTAKENLY GIVEN STOCK (MINUS VALUE)FOR OD PROGRAM(WEAR OFFSET). |2)AFTER TAKING RADIUS PROGRAM FROM ENGINEERING TEAM PROGRAM WAS EDITED AND SUPERVISOR INSTRUCTED OPERATOR TO RUN THE ID PROGRAM (TOOL NO-4)WITH SOME STOCK AND THEN FINISH THE ID TO CROSS CHECK WHETHER THE RADIUS FORMED PROPERLY.|3)WHILE ID FINISHING SHARP EDGE WAS FORMED.|4)RADIUS PROGRAM NOT GIVEN IN THE PROGRAM HENCE SHARP EDGE WAS FORMED.|5)WHILE DOING THE FAIR PART RADIUS WAS FORMED USING HAND TOOLS THEREFOR RADIUS PROGRAM WAS NOT GIVEN DURING THE PRODUCTION.','|OPERATOR IN PRESENCE OF SUPERVISOR CORRECTED THE WEAR OFFSET AND RUN THE NEXT PART, PART FOUND OK.','|RADIUS PROGRAMS AND DE BUR PROGRAMS WILL BE INCLUDED FOR ALL APPLICABLE PARTS DURING THE FAIR PART PROVING TIME ITSELF MANUAL TOOL USAGE WILL BE REDUCED.  ','CAPA found ok.','','2018-07-03','Dinakar(K)','Anjinamurthy(H)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','05','no','','Ravi(M)','no','','|SINCE THIS IS THE FIRST PRODUCTION BATCH OPERATOR CHECKED THE OD DIMENSION AND NOTED THAT DIMENSION IS UNDERSIZED BY 0.5MM\r\n\r\nOPERATOR STOPPED THE MACHINE AND INFORMED THE SUPERVISOR ABOUT THIS PROBLEM.','E3456','pe|qas|','2018-09-12|2018-09-14|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10833,'35-232A','Saab AB','HINGE BRACKET 4 ','233915B8','D576 50007 209','','E00',1,'1600223433/Forecast ','','76777','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Part running time part was lifted.','Clamping of the part was not adequate.|Parts was clamped in the machine with the help of vice and proper torque wrench was also used during clamping process but the part lifted during the machining process.|The vice was subjected to expansion and contraction during the machining process which resulted in the inadequate tightness and lifted the part during machining. |The vice used for the clamping of parts was not hardened before use.|The requirement of hardening the vice was not considered during the trial of new process.','|1) Immediately stopped the machine and informed the operators to apply additional tightness to the clamping and to run the machine in reduced cycle speed.\r<br/>2) Communicated the engineering team about the issue and instructed to change the Jaws of the vice.','|All similar vice with unhardened jaws are scrapped and instructed the Engineering team to provide with new jaws which has under gone hardening process.','CA PA implemented and maintained effectively.','','2018-07-03','Lohith(K)','        Maruthi  D R ','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','1','','','','','','|All the parts were rechecked to ensure there is any dimensional deviation and found ok.','Z3456','pe|qas|qas|qas|','2018-07-11|2018-07-11|2018-07-26|2018-10-06|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10834,'51-086','THE BOEING COMPANY','KICK LINK','G24256K05','251W3122-4','NA','PSDL REV -',1,'BOEING 001M','','73451','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Transit damage on the part(dig mark observed.','1) Part got dented due to improper handling.|2) Insufficient packing around the edges during transit.|3) Supplier shipped the parts by packing one after the other with single layer of bubble sheet due to which the weaker portion of the packing got affected and resulted in the damage of the part.','|Communicated to the supplier about the poor packing and provided guidelines on how to pack the parts to prevent damages even during the poor handling conditions.','|only individual parts are packed in a wrap and shipped by supplier.','Next batches found ok.','','2018-07-04','sppkg_sez(a)','sppkg_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','DN41238','FI','no','Misc','qas_sez(a)','no','','|Informed the supplier about the poor packing method and checked all the parts in the package and no defects were found.','Z3456','qas|','2018-11-10|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10835,'51-128','THE BOEING COMPANY','SPACER','525335-03','332W1912-79','NA','PSDL REV -',1,'486998 MPP','','74010','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dig mark observed on face.','An accident occurred due to the neglect of the operator.|The operator does not have the right work offset.','after x and y offset after cross check the raw material lengths.','after x and y offset after cross check the raw material lengths.','CA/PA satisfied.','','2018-07-04','pe_sez(a)','pe_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','1','no','Misc','pe_sez(a)','no','','during work offset x direction offset taken wrong.\r\nafter x and y offset after cross check the raw material lengths.','Z3456','pe_sez|qas_sez|','2018-09-28|2019-01-07|','2019-01-07',NULL,NULL,NULL,NULL,NULL,NULL),(10836,'35-649','Saab AB','HANDLE STOP','280752 A','D5227282820000','NA','A',2,'OWED-LTA-003','','76294','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Base thickness less than requirement. 			\r\n','Part taper butting in fixture.			\r\n|Part not checked in the feeler gauge before running the program.							\r\n|Part over tighten clamp bent but not observed before run the machine.							\r\n|Part lifting while tightening operator dint identify that problem							\r\n','|Check the part in feeler gauge before run the program. 				\r<br/>','|Message given in the program when this CRN loaded to the machine for check the butting. 				\r<br/>','CAPA FOUND OK','','2018-07-04','Krishna(Chowdary.G.P.)','Rakeshbabu(V)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','3','no','Misc','Subramanya L(Naik)','no','','|Feeler gauge check the part butting face. 			\r\n','E3456','pe|qas|','2018-08-12|2018-08-12|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10837,'53-037','Triumph Aerostructures','SPREADER PLATE BOTTOM','4264401','F574 52715 202 00','NA','PART ISSUE A, ECN PG205026001KD84',2,'LTA TRIUMPH 2018','','76582','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Refer NC NO:10744','Refer NC NO:10744','|Refer NC NO:10744','|Refer NC NO:10744','Refer NC NO:10744','','2018-07-04','Rangaswamy()','Manikanta AV()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','Misc','Manu()','no','','|Refer NC NO:10744','Z3456','qas_sez|','2019-01-16|','2019-01-16',NULL,NULL,NULL,NULL,NULL,NULL),(10838,'18-090A','Magellan Aerospace(Polska) Sp','BUSH','833467','PID278 50164 200','','A',1,'104569','','76220','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Thickness undersized by 0.05 to 0.1mm.','1)OD Undersized -0.015mm beyond drawing limit.|2)OD undersized during the re-pass operation as the re-pass ran twice.|3)Re-pass ran twice with same -0.15 wear offset as the operator provided +0.2mm wear offset during the insert change.|4)To maintain stock in the ID after the insert change the operator provided -0.2mm in the initial stage and after measuring the diameter he provided -0.15mm to remove the stock and finish to the drawing requirement during this time the re-pass operation was carried out and resulted in diameter was undersized.|5)Operator was unaware that the program for OD runs twice with different stock levels to achieve finish in the final operation.','|1Changed the wear offset from +0.2mm to +0.1mm in the next part and after the completion changed the offset to -0.02mm according to the program(after considering both the pass) and found the next part OK','|Informed all the operator to check the relevant features after the insert change and provide of the offset accordingly with proper guidance from the supervisor or senior operators','Effectiveness Found OK.','','2018-07-04','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','FI','no','Misc','Narasimha Murthy(R)','no','','|Immediately stopped the machine and changed the wear offset and continued the production on the next part.','E3456','pe|qas|','2018-09-04|2018-09-05|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10839,'51A-042','THE BOEING COMPANY','BRACKET ASSY','','149A7371-602','','PSDL REV A',1,'BOEING 001C','','A16259','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','APPLYING TEFLON COAT IS NOT DONE PROPERLY. ','1.The Teflon paint chip off surrounding the rivet during pressing the rivet|2.During pressing the rivet metal to metal contact|3.In butting block the  area where the parts were butting while riveting was not uniform |4.FOD of rivet accumulated in the butting block where the part was getting butted.','|2.Butting block was made uniform by giving a uniform cut','|1.Instruction given to operator to Change the adhesive tape frequently and clean the area where the parts gets butted before pressing the rivet','Next batch wo number A16450 assembly Completed and found ok,no evidence found for paint getting chipped','','2018-07-05','pe_sez(a)','pe_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','yes','Assembly','','FI','no','Misc','qas_sez(a)','no','','|Adhesive tape was appendix on the butting block to avoid metal to metal contact','Z3456','qas_sez|','2019-01-06|','2019-01-06',NULL,NULL,NULL,NULL,NULL,NULL),(10840,'35-071','Saab AB','9900976-380','8-16-04342-5','L579 50517 200','TA11','B00',2,'Forecast po for A380','','75098','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Thickness Over size.Requierd 4.4 to 4.6MM,measured 4.65 to 4.70','When part running time cutting tool got weariness |The Operator not check the part at the particular area |The new operator not have sufficient knowledge about the cutting tool life','|Proper training given to Operator about the cutting tool life and how to inspect the Part','|The cutting tool life will be monitor by the Tool Crib and the senior Operator.','CAPA FOUND OK','','2018-07-06','Lohith(K)','Shivaraj K S,Kiran Kumar M,Kiran KM,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','','FI','yes','PS105-01','Nagendra(SN)','no','','|The wearied cutting found out, removed from the machine and sent to resharpening  ','E3456','pe|qas|','2018-07-12|2018-08-12|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10841,'51A-082','THE BOEING COMPANY','BRACKET ASSY','','332A2930-1','','PSDL REV B',4,'BOEING 001M','','A13631','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','yes','(As Is): Sealing not smooth and continuous and with cracks.\r\n(Should Be): As per BAC5000 (AP), § 11.2.1 - All seals must be smooth and continuous, with no visible voids, holes, bubbles, cracks, or entrapped articles','Why-1: The fillet sealant deformed due to improper handling of part before curing.|Why-2: The fillet sealant was touched by hand before completely getting dried.|Why-3: No sufficient curing time was given.|Why-4: In adequate knowledge on curing duration requirement.|Why-5: Misinterpretation of the curing duration of sealant as per the standard requirements.','|1) Quality Engineer created a quality alert and displayed the same in assembly, final inspection and packing area on Jun 16, 18.\r<br/>2) Instruction given to the assembly personnel to mention the start and end time of the sealant curing from May 24, 2018.','|1) Training will imparted to all the Assembly Operators for the sealant applications as per Customer requirements on or before 20-June 2018 by Manufacturing engineer.\r<br/>2) In all Assembly work order the sealant curing time including duration will be added and effective from 1st week of July 2018.','Next batch produced found ok.','C62301','2018-07-06','qas_sez(a)','qas_sez(a)','CA1211227-01','2018-03-06','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Assembly','','Cust End','no','Misc','qas_sez(a)','no','','|1) Management Representative (MR) E-mailed SER to communicate the escapement within the organization on May 14, 2018.\r\n2) Head Quality called through E-mail for a CFT meeting to Discus on the immediate and permanent measures to be taken to prevent similar escapement on May 14, 2018.\r\n3) Re-inspection of the similar and related parts in FG and WIP was carried out by quality inspector and approved by Quality Engineer on May 16, 2018.','E3456','qas|qas|','2018-07-07|2018-07-07|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10842,'47-159','GKN Aerospace Filton','STRAP JOINT FLANGE','184883 C','F57255080202','NA','PART ISSUE C',1,'1210042824','','77121','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','PROFILE 2MM SHIFT (WRONG PROGRAM)','Due Wrong tool loaded.|Due to refereeing the data sheet.|Due to manual editing of the tool name.|Program cannot be read by the machine without manual editing.|CAM Software doesn’t output the program name as machine required.','|Program was changed and program proved part found OK, Obsolete the old program and new proved program saved in to data base.','|When giving the program the program name will be four eye checked.|2) Discussed with the CAM software supplier to provide an option which provides the tool name during the output along with the program.','CAPA found ok.','','2018-07-07','Ramesh(Poojary)','Ramesh(Poojary)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','Misc','Nandishkumar(D.K.)','no','','|Program was changed and program proved part found OK.','E3456','cam|qas|','2018-07-11|2018-09-15|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10843,'51A-068','THE BOEING COMPANY','FITTING ASSY, INBD','','112T7057-1','','PSDL REV -',1,'BOEING 001Q','','A16436','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','no','NC: The organization shall monitor and measure the characteristics of the product to verify that product requirements have been met this shall be carried out at appropriate stages of the product realization process in accordance with the planned arrangements (per AS9100 section 8.2.4 Monitoring and measurement of product)\r\n\r\nObjective evidence: For example, supplier did measure the characteristics of the product to verify that product requirements have been met and one of the engineering specification BAC5435 section 8.3.6 requirement of check the proper position of the bearing outer ring with respect to the housing was missed to measure in the boeing part number 112T7057-1, WO NO A16436(1).','For example, supplier did measure the characteristics of the product to verify that product requirements have been met and one of the engineering specification BAC5435 section 8.3.6 requirement of check the proper position of the bearing outer ring with respect to the housing was missed to measure in the boeing part number 112T7057-1, WO NO A16436(1), 112T7057-2, WO NO A16180(1). 112T7057-3, WO NO A16447(1).','|\r<br/>Internal meeting was conducted on 07-July-2018 along with Cross Functional Team (CFT), quality inspectors and assembly operator to discuss, identify and resolve the root cause.\r<br/>\r<br/>Sr.Quality engineer and head quality informed to the quality inspector keep only one-part number of all quantities from the same part number near the instruments for final inspection and extra one more surface table was arranged to keep all quantities near the instrument (electronic height gauge).this implementation was started on 9-07-2018.\r<br/>To avoid confusion, mix up of inspected and not inspected parts on the inspection table near the instrument will provide the small stickers to attach on the inspected parts with serial numbers for identification and this implementation was started on 7-7-2018 and later quality inspector will remove once confirm all parts inspection completed.\r<br/>Till to implement standard stickers will manage final inspection with the existing available stickers. \r<br/>','|\r<br/>Internal meeting was conducted on 07-July-2018 along with Cross Functional Team (CFT), quality inspectors and assembly operator to discuss, identify and resolve the root cause.\r<br/>\r<br/>Sr.Quality engineer and head quality informed to the quality inspector keep only one-part number of all quantities from the same part number near the instruments for final inspection and extra one more surface table was arranged to keep all quantities near the instrument (electronic height gauge).this implementation was started on 9-07-2018.\r<br/>To avoid confusion, mix up of inspected and not inspected parts on the inspection table near the instrument will provide the small stickers to attach on the inspected parts with serial numbers for identification and this implementation was started on 7-7-2018 and later quality inspector will remove once confirm all parts inspection completed.\r<br/>Till to implement standard stickers will manage final inspection with the existing available stickers. \r<br/>','CA/PA was found satisfied.','','2018-07-08','pe_sez(a)','pe_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','FI','yes','Misc','qas_sez(a)','yes','','|Rejected all the quantities which are not meeting the boeing drawing specification requirements and Internal NC was raised Refer NC number 10843,10844 and 10845 raised on 09-07-2018 by quality engineer and moved all rejected parts into rejection area/room.\r\n\r\nImmediately check the FG stock and no parts are available in FG and this is verified by quality engineer on 07-07-2018.\r\n\r\nRe-inspected all the produced parts on 07-07-2018 by quality engineer and all are acceptable to the drawing specification requirements refer results in the final inspection report\r\n\r\n Quality engineer and manufacturing engineer was conducted the meeting on the 07-07-2018 in the assembly area and informed to all operators/supervisors on the deviated part numbers. \r\n','Z3456','qas_sez|','2019-01-05|','2019-01-05',NULL,NULL,NULL,NULL,NULL,NULL),(10844,'51A-069','THE BOEING COMPANY','FITTING ASSY, INBD','','112T7057-2','','PSDL REV -',1,'BOEING 001Q','','A16180','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','no','NC: The organization shall monitor and measure the characteristics of the product to verify that product requirements have been met this shall be carried out at appropriate stages of the product realization process in accordance with the planned arrangements (per AS9100 section 8.2.4 Monitoring and measurement of product)\r\n\r\nObjective evidence: For example, supplier did measure the characteristics of the product to verify that product requirements have been met and one of the engineering specification BAC5435 section 8.3.6 requirement of check the proper position of the bearing outer ring with respect to the housing was missed to measure in the boeing part number 112T7057-2, WO NO A16180(1). \r\n','Refer NC NO :10843','|Refer NC NO :10843','|Refer NC NO :10843','','','2018-07-08','pe_sez(a)','pe_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','FI','yes','Misc','qas_sez(a)','yes','','|Refer NC NO :10843','Z3456','qas_sez|','2019-01-05|','2019-01-05',NULL,NULL,NULL,NULL,NULL,NULL),(10845,'51A-070','THE BOEING COMPANY','FITTING ASSY, OUTBD','','112T7057-3','','PSDL REV -',1,'BOEING 001Q','','A16447','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','NC: The organization shall monitor and measure the characteristics of the product to verify that product requirements have been met this shall be carried out at appropriate stages of the product realization process in accordance with the planned arrangements (per AS9100 section 8.2.4 Monitoring and measurement of product)\r\n\r\nObjective evidence: For example, supplier did measure the characteristics of the product to verify that product requirements have been met and one of the engineering specification BAC5435 section 8.3.6 requirement of check the proper position of the bearing outer ring with respect to the housing was missed to measure in the boeing part number  112T7057-3, WO NO A16447(1).\r\n','Refer NC NO :10843','|Refer NC NO :10843','|Refer NC NO :10843','Refer NC NO :10843','','2018-07-08','pe_sez(a)','pe_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Assembly','','FI','no','Misc','qas_sez(a)','no','','|Refer NC NO :10843','Z3456','qas_sez|','2019-01-05|','2019-01-05',NULL,NULL,NULL,NULL,NULL,NULL),(10846,'51A-071','THE BOEING COMPANY','FITTING ASSY, OUTBD','','112T7057-4','','PSDL REV -',1,'BOEING 001Q','','A16083','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','no','NC: The organization shall monitor and measure the characteristics of the product to verify that product requirements have been met this shall be carried out at appropriate stages of the product realization process in accordance with the planned arrangements (per AS9100 section 8.2.4 Monitoring and measurement of product)\r\n\r\nObjective evidence: For example, supplier did measure the characteristics of the product to verify that product requirements have been met and one of the engineering specification BAC5435 section 8.3.6 requirement of check the proper position of the bearing outer ring with respect to the housing was missed to measure in the boeing part number 112T7057-4.','Refer NC NO :10843','|Refer NC NO :10843','|Refer NC NO :10843','Refer NC NO :10843','','2018-07-08','pe_sez(a)','pe_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','FI','yes','Misc','qas_sez(a)','yes','','|Refer NC NO :10843','Z3456','qas_sez|','2019-01-05|','2019-01-05',NULL,NULL,NULL,NULL,NULL,NULL),(10847,'35-077','Saab AB','BUSH','L37145','D575 40147 200','DTD-197','B ECN NG29999ST2TT59',2,'1600219297','','76786','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','03 operation missing.','Part with incomplete operations sent to final inspection.|The part was separated for rework.|The total length of the part was oversize so the operator separated the part and did not informed the supervisor.|The operator missed to communicate due to work priorities.','|Part was again loaded to the machine and the facing operation was completed.','|1) Informed all the operators to mention the work order no and the completed operation no on the face of the part till the completion of the final operation.\r<br/>2) Informed the operator to carry out visual inspection of all the parts placing together at the end of every setup. ','CA PA found ok.','','2018-07-09','Raghavendra Rao(R)','Rajesh T,Dinakar K,Devaraj K.C.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','With Treatment','','FI','no','DX 200-1','Yashawantha(NH)','no','','|Informed all the operators to identify the rework parts with identification tag. ','E3456','qas|qas|nandishkumardk|','2018-07-25|2018-07-25|2018-07-27|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10848,'35-077','Saab AB','BUSH','L37145','D575 40147 200','DTD-197','B ECN NG29999ST2TT59',1,'1600214065','','76804','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','03 operation missing.','Part with incomplete operations sent to final inspection.|The part was separated for rework.|The total length of the part was oversize so the operator separated the part and did not informed the supervisor.|The operator missed to communicate due to work priorities.','|Part was again loaded to the machine and the facing operation was completed.','|1) Informed all the operators to mention the work order no and the completed operation no on the face of the part till the completion of the final operation.\r<br/>2) Informed the operator to carry out visual inspection of all the parts placing together at the end of every setup.','CA PA Found ok.','','2018-07-09','Raghavendra Rao(R)','Rajesh T,Dinakar K,Devaraj K.C.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','With Treatment','','fi','no','DX 200-1','Yashawantha(NH)','no','','|Informed all the operators to identify the rework parts with identification tag.','E3456','qas|qas|nandishkumardk|','2018-07-25|2018-07-25|2018-07-27|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10849,'18-284A','Magellan Aerospace Bournemouth',' 	SPINDLE FOR CLACK ALVES','1501784-6/LNZX','PIA281-40019-200','','A',2,'423253','','71848','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','OD Under size by 0.05 to .18mm.','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 -0.15 wear offset as the operator provided +0.2mm 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.','','2018-07-09','Dinakar(K)','Dinakar K()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','FI','no','Misc','Narasimha Murthy(R)','no','','|Immediately stopped the machine and changed the wear offset and continued the production on the next part.','E3456','pe|qas|','2018-09-04|2018-09-05|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10850,'47-166','GKN Aerospace Filton','PLATE SPREADER UPPER','8713201-1','F57455042200','NA','PART ISSUE B',1,'1210042824-1','','75457','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Outer profile dig mark up to -1mm','NC post problem|cross check the tool path|correct the Tool path','|Taken the new corrected  program and and run','|Before we Run the program cross check the Tool path direction and run ','CAPA FOUND OK','','2018-07-09','Ravi nayak()','prodn_aero(prodn)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','1','no','Misc','Ravi nayak()','no','','|cross check the tool path direction and inform to CAD Engineer','A3456','prodn_aero|qas_aero|qas_aero|','2018-09-06|2018-09-06|2018-09-06|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10851,'18-412A','Magellan Aerospace Wrexham','ROD END','1562058-3/PL6X','D321 53012 200','','F01',3,'RP166211','','74632','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','face unclear, and total length under size   ','Operator did not checked the total length of the part while providing the offset and continued the production.','|Informed all the operator to check the total length of the RM before loading to the machine and continuing the production.','|1) All the RM will be separated based on the length and the length of the RM will be marked on the face of the material.\r<br/>2) Material with different size will be separated and machined separately.','CAPA found ok.','','2018-07-10','Dinakar K()','Rudresh(k)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Sathish(G)','no','','|Immediately stopped the machine and changed the offset and continued the production.','E3456','qas|qas|','2018-08-01|2018-08-01|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10852,'18-664A','Magellan Aerospace Bournemouth','GAMMA FITTINGS','9237','NSA840020-150','','L',6,'428939','','75688','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','1)2 nos paint Damage\r\n2)4 nos Rust Mark in side the bore on the anodize layer','1)Paint chip off occurred\r\n2)Rust marks are occurred after anodizing process |1)After paint application proper handling not done\r\n2)Parts ship into treatment house the rust was not observed in inspection  |1)During visual inspection on parts chip off was not ensured in treatment house\r\n2)So Inspection not done properly|1)So Inspection not done properly','|1)Parts handling process was improved \r<br/>2)Visual inspection carried out properly in 1000lux intensity','|1)Parts handling method improved in trolly instead of manually\r<br/>2)Visual inspection carried out in 4eye check','CAPA FOUND OK','','2018-07-10','pe_sez(a)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','DN41627','POST TREATMENT','yes','Misc','qas_sez(a)','no','','|1)In treatment house the parts which are all in process that was ensured paint inspection\r\n2)The parts which are all ship into treatment that was ensured rust free if is there that was removed','Z3456','qas|qas|','2018-08-07|2018-08-07|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10853,'18-664A','Magellan Aerospace Bournemouth','GAMMA FITTINGS','9236','NSA840020-150','','L',6,'428939','','75685','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Paint Damage and rust found in Anodic Layer','1)Paint chip off occurred\r\n2)Rust marks are occurred after anodizing process |1)After paint application proper handling not done\r\n2)Parts ship into treatment house the rust was not observed in inspection  |1)During visual inspection on parts chip off was not ensured in treatment house\r\n2)So Inspection not done properly|1)So Inspection not done properly','|1)Parts handling process was improved \r<br/>2)Visual inspection carried out properly in 1000lux intensity','|1)Parts handling process was improved \r<br/>2)Visual inspection carried out properly in 1000lux intensity','CAPA FOUND OK','','2018-07-10','pe_sez(a)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','DN41623','POST TREATMENT','yes','Misc','qas_sez(a)','no','','|1)In treatment house the parts which are all in process that was ensured paint inspection\r\n2)The parts which are all ship into treatment that was ensured rust free if is there that was removed','Z3456','qas|qas|','2018-08-07|2018-08-07|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10854,'18-664A','Magellan Aerospace Bournemouth','GAMMA FITTINGS','9236','NSA840020-150','','L',6,'428939','','75683','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Paint Damage and rust','1)Paint chip off occurred\r\n2)Rust marks are occurred after anodizing process |1)After paint application proper handling not done\r\n2)Parts ship into treatment house the rust was not observed in inspection  |1)During visual inspection on parts chip off was not ensured in treatment house\r\n2)So Inspection not done properly|1)So Inspection not done properly','|1)Parts handling process was improved \r<br/>2)Visual inspection carried out properly in 1000 lux intensity','|1)Parts handling process was improved \r<br/>2)Visual inspection carried out properly in 1000 lux intensity','CAPA FOUND OK','','2018-07-10','op_sez(s)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','DN41624','POST TREATMENT','yes','Misc','qas_sez(a)','no','','|1)In treatment house the parts which are all in process that was ensured paint inspection\r\n2)The parts which are all ship into treatment that was ensured rust free if is there that was removed','Z3456','qas|qas|','2018-08-07|2018-08-07|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10855,'18-665A','Magellan Aerospace Bournemouth','GAMMA FITTINGS','28428487-G','NSA840020-200','','L',8,'428939','','75689','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','paint damage and rust','1)Paint chip off occurred\r\n2)Rust marks are occurred after anodizing process |1)After paint application proper handling not done\r\n2)Parts ship into treatment house the rust was not observed in inspection  |1)During visual inspection on parts chip off was not ensured in treatment house\r\n2)So Inspection not done properly|1)So Inspection not done properly','|1)Parts handling process was improved \r<br/>2)Visual inspection carried out properly in 1000lux intensity','|1)Parts handling process was improved \r<br/>2)Visual inspection carried out properly in 1000lux intensity','CAPA FOUND OK','','2018-07-10','op_sez(s)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','DN41628','POST TREATMENT','yes','Misc','qas_sez(a)','no','','|1)In treatment house the parts which are all in process that was ensured paint inspection\r\n2)The parts which are all ship into treatment that was ensured rust free if is there that was removed','Z3456','qas|','2018-08-07|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10856,'18-665A','Magellan Aerospace Bournemouth','GAMMA FITTINGS','28163030-A','NSA840020-200','','L',1,'428939','','75691','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','paint damage','Paint chip off occurred|After paint application proper handling not done|During visual inspection on parts chip off was not ensured in treatment house|So Inspection not done properly','|Parts handling process was improved ','|Parts handling process was improved','CAPA FOUND OK','','2018-07-10','op_sez(s)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','DN41630','POST TREATMENT','yes','Misc','qas_sez(a)','no','','|In treatment house the parts which are all in process that was ensured paint inspection','Z3456','qas|','2018-08-07|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10857,'34-065A','Magellan Aerospace Winnipeg','BASE FITTING,F/D HINGE LH','G23459','400-12780-1','NA','EM104302 Iss B,EM105092 Iss H,EM104765 Iss H',1,'C81597 Rev 001','','77471','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Part dig mark occurred on wall side.','Dig mark occurred on part during machining\r\n|The program was verified while that time half program was showed in memory.|The program overlapping occurred|The Program was copied from backup via pen-drive so the program was overlapped or corrupted in pen-drive','|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','CA PA Found ok.','','2018-07-10','Dhananjaya(N)','        Narasimhamurthy C','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','03','','','','','','|The corrupted program was removed from machine and the correct program was verified in a system then loaded into machine ','E3456','pe|qas|','2018-07-16|2018-07-19|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10858,'35-531A','Saab AB','SHAFT LATCH','C90596.QYF2','D5227349020200','NA','PART ISSUE C',33,'OWED-LTA-002','','73919','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','OD Oversize Nominal 18.78/18.767, Measures 18.781/18.788.','','','','Parts Accepted after Rework.','','2018-07-10','Dinakar(K)','Rakeshbabu(V)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','With Treatment','','Production','no','Misc','Manu(P)','no','','','E3456','qas|qas|','2018-10-30|2018-10-30|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10859,'18-664A','Magellan Aerospace Bournemouth','GAMMA FITTINGS','9236','NSA840020-150','','L',1,'428939','','75686','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','RUST INSIDE BORE IN ANODIZE LAYER','Rust marks are occurred after anodizing process|During parts ship into treatment house the rust was not observed in inspection  |So visual Inspection not done properly','|Visual inspection carried out properly in 1000 lux intensity','|Visual inspection carried out properly in 1000 lux intensity','CAPA FOUND OK','','2018-07-11','pe_sez(a)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','DN41625','POST TREATMENT','yes','Misc','qas_sez(a)','no','','|The parts which are all ship into treatment that was ensured rust free if is there that was removed','Z3456','qas|','2018-08-07|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10860,'35-576','Saab AB','BRACKET','532730A','D5227343420000','NA','PART ISSUE A',1,'PA1687 LTA-1','','73844','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Dent Mark Observed.','Dent occurred on part due to improper clamping.|Part was loaded to the butting block for which the height was not determined due to which the part got dented.|Due to variation in the height additional support was given to the part during which the part was not properly butted.|man to man variation occurred during the clamping of part using additional support.','|Provided proper butting block to clamp the parts and continued the production.','|Part clamping process changed with providing proper vice.','Next batches found ok.','','2018-07-11','Krishna(Chowdary.G.P.)','Rakeshbabu(V)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','Production','no','Misc','Manu(P)','no','','|Immediately stopped the machine and checked the previously completed parts.','E3456','qas|','2018-11-07|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10861,'35-189','Saab AB','INTERCOSTAL_MIDSPAN_NO_2 ','482883A','423Z1170-1-06','','---',1,'PA 1510 FORECAST-2','','56576','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','yes','Paint release occur when receiving inspector should clean an dirty area with MEK (Methyl Ethyl\r\nKeton). ','Improper paint adhesion on the part. ','|Informed the supplier about the issue and instructed the supplier to strip and reprocess the parts.','|Supplier to carry out 100% tape test before dispatching the parts.','Next batches found ok.','C50860','2018-07-12','Yashawantha(NH)','Nagendra(SN)','OF-001980','2016-12-12','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','DN27689','custmer end','yes','Misc','Nagendra(SN)','no','','|Checked all the parts and the affected parts are sent back for reprocessing.','E3456','qas|','2018-09-14|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10862,'35-227A','Saab AB','HINGE BRACKET 2','221458B3','D576 50005 204','','D00',1,'1600223433/Forecast ','','76174','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Base ThiknessLess Then Requirment.up to 0.9MM','Clamp Over Tighting.so part DIG.','Clamps not over tight & absorve the clamp bottom step.After loading the part check the feeler gauge then run the part','All four clamps chenged. & new clamps applyed.','CAPA FOUND OK','','2018-07-12','prodn_aero(prodn)','Manjunatha.D()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Manjunatha.D()','no','','Clamp not over tigthing & clamp tighting only hand tight.','A3456','qas_aero|','2018-07-17|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10863,'35-258','Saab AB','BRACKET, DEFLECTION STOP','G23050K02','423Z6187-6','','---',1,'PA 1510 FORECAST-2','','62758','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','yes','Wrong Part marking.','During part marking it was interchanged and same was not picked by the operator and inspector.\r\n','| We have checked the stock parts and found correct \r<br/>','|1) We will stop to take the label print out same time for same similar kind family parts like LH and RH. \r<br/>2)We will take number of label print out as per work order quantity that will indirectly avoids the interchange.\r<br/>','Next batches found ok\r\n','C61293','2018-07-12','qas_sez(a)','qas_sez(a)','OF-003108','2018-07-09','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','DN32948','Cust End','no','Misc','qas(qas)','no','','| We have checked the stock parts and found correct \r\n','E3456','nagendra|','2018-08-07|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10864,'51-051','THE BOEING COMPANY','BRACKET','436272','149A7371-9627','','PSDL REV A',1,'BOEING 001C','','75803','','0000-00-00',NULL,'yes','no','yes','no','yes','no','no','no','no','PART RUNNING TIME CUTTING TOOL BROKEN','PREVIOUS  i MACHINING OPERATION TIME DIA 12*R3.18 CUTTING TOOL BROKEN|DUE TO HIGH CUTTING SPEED AND CUTTING TOOL WEARINESS |TO ACHIEVE THE PRODUCTIVITY ','PROGRAM CUTTING SPEED AND MACHINING METHOD CHANGED ','FOR THE ABOVE SIMILARLY PART THE ENGG DEPT WILL GIVE THE CURRECT CUTTING SPEED AND LOW STEP OVER ','Corrected cutting speed and low step over details are updated and next production batch found ok.','','2018-07-12','pe_sez(a)','Nataraja C V,Diwakar R.B.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','1','no','i700-5','pe_sez(a)','no','','ABOUT  THE PARTICULAR PROGRAM DISCUSSED WITH ENGG DEPT. DELETED FROM THE PROGRAM FILE WITH PERMISSION OF ENGG DEPT   ','Z3456','qas|','2018-09-24|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10865,'51-084A','THE BOEING COMPANY','BRACKET DETAIL','BA48110','332A2930-63','NA','PSDL REV B',1,'BOEING 001U','','74029','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Tool drop from holder so base dig mark.','While Roughing program running time tool remove from from holder and tool broken.|Remove the tool from spindle and cross check locking screw tight|Tool holder Locking screw was loosen ','|insert the new holder,tool taken the  tool offset value entered  and   run the machine ','|We have  given instruction to operators while roughing program running  monitoring the tool life  and check the  tool holder locking screw tight cross check in every shift.    ','Next Batches found ok.','','2018-07-13','pe_sez(a)','pe_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','3','no','Misc','pe_sez(a)','no','','|Cross check the previous machining completed parts','Z3456','pe_sez|qas|','2018-09-11|2018-09-14|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10866,'35-453A','Saab AB','SEAL RETAINER ','515370A','D522 73425 200 00','','PART ISSUE B',1,'OWED-LTA-002','','76933','','0000-00-00',NULL,'yes','no','yes','no','yes','no','no','no','no','cut out running time part cut so part damage ','1.while part proving time base cutout on zero surface so part rotated .|2.Due to cutout finish size less than minimum stock.','|1.informed to cad team to control the base stock minimum 0.3mm for all parts ','|1.training given to operator before starting the cutout program check the program ending value is minimum 0.3mm up or not,otherwise change program immediately. ','CA/PA found satisfied.','','2018-07-13','Rangaswamy()','pe_sez(a)','','0000-00-00','cut out running time part cut so part damage ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','05','no','Misc','pe_sez(a)','no','','|Every part cutout stock to be ensure ,','Z3456','pe_sez|qas_sez|','2018-12-18|2019-01-05|','2019-01-05',NULL,NULL,NULL,NULL,NULL,NULL),(10867,'47-142','GKN Aerospace Filton','STIFFENER 5 TOP SKIN','4200901 1','D57250496203','NA','PART ISSUE N',1,'1210042824-1','','75450','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','part dig mark absorbed on base thickness','part thickness under size |Due to Extra Material Removed|lug out was on process then chisel mark happen|Lug was manually cutout','|proper training given to fitting operator|proper training was given to fitting operator and also program was given for lug cutout','|part clamping to fixture ,|Program will be given for LUG cutout in machine only','CA PA found ok.','','2018-07-13','Ramesh(Poojary)','Raghu(A.N.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Ramesh(Poojary)','no','','proper training given to fitting operator |Program was given for lug cutout instead of manual','E3456','pe|cam|qas|','2018-07-13|2018-08-22|2018-09-05|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10868,'53-017','Triumph Aerostructures','SPREADER PLATE TOP','755621','F574 50217 202 B03','NA','PART ISSUE A',1,'LTA TRIUMPH 2018','','77448','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','dig mark found','improper tool holding\r\n|Tool holding minimum length of tool in holder.|Tool over all length is short.','|New HANITA make tool loaded with holding length of minimum 40mm.message added in the program about holding length of 40mm.','|Message added in the program about holding length of 40mm.','CAPA Found OK','','2018-07-14','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Krishna(Chowdary.G.P.)','no','','|stop the production & ensure the all parts. ','E3456','pe|qas|','2018-12-18|2018-12-18|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10869,'35-623A','Saab AB','SHAFT 2','532730A','D5227280820000','NA','PART ISSUE A',1,'OWED-LTA-004','','76735','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','OD UNDER SIZE BY -0.015MM.','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 -0.15 wear offset as the operator provided +0.2mm 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. ','CAPA FOUND OK','','2018-07-16','Sandhesh D(S)','Arun Kumar(A M)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','05','no','Misc','Ravi(M)','no','','|Immediately stopped the machine and changed the wear offset and continued the production on the next part. ','E3456','pe|qas|','2018-09-05|2018-09-07|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10870,'46-004B','Mahindra Aerostructures Pvt.Ltd','STRAP','4470401 2','D575-40862-200MH','','F',1,'MAPL Forecast ','','77855','','0000-00-00',NULL,'yes','yes','yes','','','','','','','PART ACCEPTED','PART ACCEPTED|PART ACCEPTED|PART ACCEPTED|PART ACCEPTED|PART ACCEPTED','|PART ACCEPTED','|PART ACCEPTED','Part is accepted.','','2018-07-16','Lohith(K)','        HariPrasad ','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','','','','03','','','','','','|PART ACCEPTED','Z3456','pe|pe_sez|qas|','2018-08-30|2018-09-05|2018-09-26|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10871,'35-628A','Saab AB','','C90733','D5227349320400','NA','PART ISSUE D',3,'OWED-LTA-001','','75659','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Bore over size.\r\ndia requierd  18.840 to 18.861\r\nMeasured 18.876 To 18.890','1part running time chips present in spindle so tool run out occur 							\r\n|2.To give the proper training for operator while running time check the tool clamping before running 						\r\n|3.Monitor to check the tool-holder for bore finish tool 							\r\n|4.inform to all operators and check the critical dimension 1:1 ratios 							\r\n|5.Further parts are found ok 				','|Clean the tool holder and spindle,ATC ARM 		','|1.TO every part setting time to check and ensure the m/c ATC arm and shutter door . 		\r<br/>2.once a week clean the ATC Shutter and information pass the all 3 shift operator, 							\r<br/>			','CAPA FOUND OK','','2018-07-16','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','Misc','Nagendra(SN)','no','','|Based on the usage of the part [Assembly Requirement], since a shaft gets into the bore, the checking method was changed and all the rejected parts were subjected to re-inspection using a GO and NOGO Plug Gage							\r\n','E3456','pe|qas|','2018-08-12|2018-08-12|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10872,'35-580A','Saab AB','LEVER','LL0109408','D5227346720400','NA','PART ISSUE C',3,'OWED-LTA-003','','75176','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Drawing required 2.80 +/- 0.1mm. measured 2.60/2.62mm.',' while running time Tool broken \r\n|improper tool life monitoring ','|replaces the new tool and Continue  the production','|monitor the tool life \r<br/>set the frequency and change the tool every 25 number part','CAPA found ok','','2018-07-16','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','Misc','Yashawantha(NH)','no','','|Previous all part checked found ok ','E3456','pe|qas|qas|','2018-12-19|2018-12-19|2018-12-19|','2018-12-19',NULL,NULL,NULL,NULL,NULL,NULL),(10873,'51A-004','THE BOEING COMPANY','LOWER BEAM FWD INBD SPLIC','','315Z1302-1502','','NIL',2,'BOEING 001K','','A14902','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Hole pitch shifted in gang channel ','1) Hole shifted during the assembly process.|2) Hole position in the fixture was shifted due to improper fixture design.','|Changed the fixture and continued the assembly.','|New fixtures will be validated for all controlled features before starting the assembly.','CA PA found ok.','','2018-07-17','Ramesh(D)','Phaniraj(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','Assembly','','10','no','','Phaniraj(G)','no','','|Immediately stopped the assembly and informed the engineering department about the shift in hole in the fixture.','E3456','qas|qas|','2018-08-10|2019-02-19|','2019-02-19',NULL,NULL,NULL,NULL,NULL,NULL),(10874,'51A-004','THE BOEING COMPANY','LOWER BEAM FWD INBD SPLIC','','315Z1302-1502','','NIL',2,'BOEING 001K','','A14902','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Due to hole shifted in gang channel rivet removed.  ','1) Due to fixture error hole shifted.','|Changed the fixture and continued the assembly.','|New fixtures will be validated for control features and then the assembly will be continued.','CAPA found.','','2018-07-17','Ramesh(D)','Phaniraj(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','Assembly','','10','no','','Phaniraj(G)','no','','|1) Immediately stopped the assembly and informed the engineering department.','E3456','qas|qas|','2018-08-10|2019-02-19|','2019-02-19',NULL,NULL,NULL,NULL,NULL,NULL),(10875,'51A-007','THE BOEING COMPANY','LOWER BEAM AFT INBD SPLIC','','315Z1304-1502','','NIL',4,'BOEING 001K','','A14912','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Flushnes problem so rivet removed. ','1) Due to improper CSK formation during the rework flushness was not achieved.|2) CSK rework was carried out to remove the paint which was applied during the painting operation.','|Informed all the operators to properly check the CSK formation during the rework.','|Standard rework tool for CSK purchased and put to use','CA PA found ok.','','2018-07-17','Ramesh(D)','Ramesh(D)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Assembly','','10','no','','Phaniraj(G)','no','','|Immediately stopped the assembly and checked the CSK formation of all the other parts and found ok.','E3456','qas|','2019-04-26|','2019-04-26',NULL,NULL,NULL,NULL,NULL,NULL),(10876,'51A-007','THE BOEING COMPANY','LOWER BEAM AFT INBD SPLIC','','315Z1304-1502','','NIL',1,'BOEING 001K','','A16721','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Hole pitch shifted in gang channel ','Part located properly.|Guide pins for locating the part not available.','|Informed the engineering team to redesign the Fixture with providing guiding pins.','|Guiding pins included in the fixture to locate the part.','ca pa found ok.','','2018-07-17','Guru(Kiran)','Guru(Kiran)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Assembly','','10','no','','Phaniraj(G)','no','','|Immediately stopped the machine and checked the previously completed parts and found ok.','E3456','qas|','2019-04-26|','2019-04-26',NULL,NULL,NULL,NULL,NULL,NULL),(10877,'51A-007','THE BOEING COMPANY','LOWER BEAM AFT INBD SPLIC','','315Z1304-1502','','NIL',2,'BOEING 001K','','A16721','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Hole shifted','Location pin for locating the part not available in the fixture.','|Informed the engineering department to include guiding pin in the fixture.','|Location pin included in the fixture.','CA PA Found ok.','','2018-07-17','Ramesh(D)','Ramesh(D)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Assembly','','10','no','','Phaniraj(G)','no','','Due to hole shifted in gang channel rivet removed. ','E3456','qas|','2019-04-26|','2019-04-26',NULL,NULL,NULL,NULL,NULL,NULL),(10878,'53-001','Triumph Aerostructures','HOUSING SIDE ROLLER','9384901 1','F579 53065 202 B02','','PART ISSUE B',1,'4500108799','','63629','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','BORE OVER SIZE BY 15 MICRONS','','','','','','2018-07-17','Rangaswamy()','Manikanta AV()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','Misc','Manu()','no','','','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10879,'53-040','Triumph Aerostructures','STRAP LOWER F/S R27','1585102','F5725550320006','NA','PART ISSUE A',1,'LTA2 Triumph 2018','','78284','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','hole pitch shifted ','hole pitch shifted in jig boring machine|operator not see the DRo reading|operator  noticed  only  the digits after decimal point|operator not concentrated on the full hole pitch reading|concentration diverted ','Quality Alert displayed at the machine so that operator will be aware while doing next batch ','Quality Alert displayed at the machine so that operator will be aware while doing next batch |Requested engineer team to included the hole operation in the NC program.','CA PA found ok.','','2018-07-17','Anjinamurthy(H)','Jayarama(M.B.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','3','no','Misc','Narayanappa(G)','no','','previous all part cross checked','E3456','pe|pe|qas|','2018-07-31|2018-07-31|2018-07-31|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10880,'35-143A','Saab AB','BCD_LATCH_PROBE_FTG_HOUSI','694581','424Z6115-3-01','','--C',1,'Forecast po for B787','','71634','','0000-00-00',NULL,'no','yes','yes','yes','no','no','no','no','no','Drill run in opposite direction.\r\n1.27 position error.','Part loaded in reverse direction.\r\n|Without noticing the message.|Did not check the feeler gauge while part butting.\r\n|.|.','Checked all the message and feeler gauge before part loading.','Informed all operators regarding this mistake to take care about the above NC.','CAPA FOUND OK','','2018-07-18','Ravi nayak()','prodn_aero(prodn)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','09','no','Misc','prodn_aero(prodn)','no','','Due to part symmetry.','A3456','qas_aero|','2018-07-30|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10881,'56-015','GKN Aerospace Orangeburg','SUPPORT BRACKET - LWR','260816B4','119A1216-603','NA','PSDL REV-',1,'LTA Orangeburg 737 W','','77998','','0000-00-00',NULL,'yes','no','yes','no','yes','no','no','no','no','Profile point out of tolerance','Dimension of a 3D point from a hole measured out of tolerance.|Hole Shifted during the 5axis machining time.|Rotary did not tilted to the required angle.|Problem with the movement of the rotary.','|1) Loaded the FAIR part in other machine and proved the program.','|Maintenance team from machine supplier arrived onsite and solved the rotary issue and the problem is not repeated.','Next batched manufactured in the machine found ok.','','2018-07-18','op_sez(s)','op_sez(s)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','op_sez(s)','no','','|1) Immediately stopped the machine and informed the maintenance team.','Z3456','qas|qas|','2018-08-03|2018-08-03|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10882,'51A-053','THE BOEING COMPANY','BRACKET ASSY','','149A7371-629','','PSDL REV A',1,'BOEING 001G','','A15796','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','TEFLON COAT PEAL UP','1.The Teflon paint chip off surrounding the rivet during pressing the rivet|2.During pressing the rivet metal to metal contact|3.In butting block the  area where the parts were butting while riveting was not uniform |4.FOD of rivet accumulated in the butting block where the part was getting butted.','|2.Butting block was made uniform by giving a uniform cut','|1.Instruction given to operator to Change the adhesive tape frequently and clean the area where the parts gets butted before pressing the rivet','Next batch wo number A15816 assembly Completed and found ok,no evidence found for paint getting chipped','','2018-07-19','pe_sez(a)','pe_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','yes','Assembly','','FI','no','Misc','qas_sez(a)','no','','|Adhesive tape was appendix on the butting block to avoid metal to metal contact','Z3456','qas_sez|','2019-01-06|','2019-01-06',NULL,NULL,NULL,NULL,NULL,NULL),(10883,'18-411A','Magellan Aerospace Bournemouth','PLUNGER','734875','D321 40205 200','','H01',19,'423244','','72104','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','OD UNDER SIZE.','Outer dimension is not achieved according to the drawing requirement.|Operator did not checked the dimension of the part after changing the revolving center.|Depth of the Dia. 1.6mm hole in the part was minimum therefore the operator changed the revolving center of according to the requirement and did not ensured the run out of the newly loaded revolving center.|New operator was running the machine and changed the revolving center without supervision.','|Informed all the operators about the issue and instructed to verify run out of the revolving centers before starting the production.','|All New operators will be supervised properly before completion of all required training to the new operator.','CA PA found ok.','','2018-07-19','Dinakar(K)','Dinakar K()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Ravi(M)','no','','|Supervisor immediately stopped the machine and changed the revolving center and continued the production.','E3456','qas|qas|','2018-08-01|2018-08-01|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10884,'18-391B','Magellan Aerospace Bournemouth','END COVER','28163030-C','D278 50166 200','','A',1,'423234','','75423','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','FACE DIG MARK.','1) Outer profile damaged during the machining process.|2) Chamfer tool stroked the outer wall in the last pass.|3) Tool part defined in the program was not correct to the requirement.|4) While transferring the program the end program got corrupted and was not noticed. |5) No alarm was displayed regarding the corrupted program was displayed in the machine monitor.','|1) Informed the Engineering team about the corrupted program and removed them from the machine and copied the correct program.\r<br/>2) Re-verified the parameters of the program along with the engineering team after copying the program to the machine.','|Instructed all the supervisors to recheck the program after copying/transferring them from the server to the machine.','CA PA found Ok.','','2018-07-19','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Ravi(M)','no','','|Checked the entire program to ensure proper tool patch and corrected the affected files.','E3456','qas|qas|','2018-07-24|2018-07-24|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10885,'18-209B','Magellan Aerospace Wrexham','BODY','28428487-F','D321 40204 202','','D, ECN NR29999ST1KM15, NR29999ST2KF65, WQN DFB09775',7,'RP166210','','74442','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','ID OVERSIZE.','Tool offset wrong|During the tool offset of the X axis mistake by operator','|Reset the tool offset and run the production.','|Instructed operator to take the tool offset correctly and\r<br/>cross check before run the tool.','capa found ok','','2018-07-19','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','01','no','Misc','Ravi(M)','no','','|Stop production & ensure the every part.','E3456','pe|qas|qas|','2018-12-18|2018-12-18|2018-12-18|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10886,'35A-601','Saab AB','FRAME ASSY','','D5227338501000','','PART ISSUE C',1,'OWED-LTA-001','','A16222','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','yes','Is condition: Several parts have marks in surface treatment. Anchor nuts are missing visible sealant and Deviation report is missing in delivery e.g. electrical bonding not performed to specification. See pictures below.\r\n\r\nShould be condition: Continuous and covering surface treatment all over. Annular sealant squeeze out under fasteners. Deviation report referred to on COC and in part delivery.\r\n\r\nA total of 28 No\'s are to be reworked which belongs to the W/O A16222, A16223, A16224.','Why 1:\r\n1) Part at customer end were found with defects in paint layer\'s.\r\n2) Sealant was not applied during the assembly of anchor nut.|Why 2:\r\n1) Paint chipped off at edges.\r\n2) Application of sealant was not mentioned in the APS.|Why 3:\r\n1)Improper packing of part caused damage during transit.\r\n2) Improper interpretation of the electrical bonding spec.|Why 4:\r\n1) Multiple parts are packed place one after other without sufficient packing between them.\r\n2) Assembly for electrical bonding was new to CIM and was not aware of how to carry out the assembly.|Why 5: Trial was carried out to reduce the packing consumables.','|Quality Engineer communicated to the Head Packing on the issues caused due to  improper packing and informed the packing team to change the packing method from multiple part to one part per packing method and this was put ti place from 1-Aug-18.','|APS for the subjected part was amended according to the requirement as per the guidance from customer and the delta FAI for the same is submitted to SAAB on 13-Aug-2018.','Delta FAI carried out and CAPA implementation found ok.','C66405','2018-07-20','qas_sez(a)','qas_sez(a)','OF-003120','2018-07-20','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','Cust End','yes','Misc','qas_sez(a)','no','','|Immediately checked the parts in Stock and no similar parts were found.','E3456','qas|','2018-12-10|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10887,'35-476B','Saab AB','CAM ROLLER PIN','C91195.RQJ6','D5227331520000','NA','PART ISSUE C',1,'OWED-LTA-005','','75961','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','OD UNDER SIZE.','Tool edge wear.|Tool life parameters was not established for this batch.','|Tool life parameters set and advised the operators to index before tool failure occurs.','|Tool life parameter set and advised the operators to index before tool failure occurs.','CA/PA Found ok','','2018-07-20','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','01','no','Misc','Ravi(M)','no','','|Tool life parameters was set and there was no rejection after this particular piece. ','E3456','qas|qas|','2018-08-22|2018-09-05|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10888,'35-480A','Saab AB','LOCK LEVER','C90875','D5227349820000','NA','PART ISSUE B',1,'OWED-LTA-003','','73789','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','8MM HOLE OFFSET 0.8MM.  ','1) DIA. 8mm Hole oblong during the machining time. |2) Drill went cross through the hole due to overload caused by blunt cutting edge.|3) MS drill was used as to carry out the hole operation the life of cutting edge was not monitored.|4) This operation was usually carried out using the Carbide drill but the tool was sent to re-sharpening during the production of this batch. Therefore MS drill was used to complete the production. |5) The availability of Carbide drill was less.','|1) Purchased new carbide drills of the same length and instructed all the operators not to use MS drills.\r<br/>2) Monitored the tool life of the new Carbide drill and instructed the operators to have sufficient spares of Carbide drill while performing this operation.\r<br/>','|Instruction given to all the operator to replace the Drill once in every 20 No\'s of production and to ensure the sharpness of the cutting edges before starting the cycle.','Next batch production verified and CA PA found effective.','','2018-07-20','Ravi(M)','Ravi(M)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','07','no','Misc','Ravi(M)','no','','|Stopped the machine and checked the previous production parts and found ok.','E3456','qas|qas|','2018-07-25|2018-07-25|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10889,'35-629A','Saab AB','','C90733','D5227349320500','NA','PART ISSUE D',6,'OWED-LTA-001','','75663','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Bore over size by 0.020mm.','1) Bore oversized due to chip-off in the cutting edge of the reamer.|2) Due to hard material and rough machining condition the cutting edge got chipped off and the ID got oversized.|3) Tool life was not freezed and was under RD stage.','|Informed all the  operators to change the reamer once in 5 Parts.','|Informed the tooling supplier and purchased high grade reamers to withstand the machining conditions.','CAPA found ok.','','2018-07-20','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','Misc','Yashawantha(NH)','no','','|Immediately stopped the machine and changed the reamer tool and continued the production.','E3456','qas|','2018-11-07|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10890,'35-628A','Saab AB','','C90733','D5227349320400','NA','PART ISSUE D',1,'OWED-LTA-001','','75655','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Bore over size by 0.020mm.','1part running time chips present in spindle so tool run out occur 							\r\n|2.To give the proper training for operator while running time check the tool clamping before running 							|3.Monitor to check the tool-holder for bore finish tool 							\r\n|4.inform to all operators and check the critical dimension 1:1 ratios 							\r\n|5.Further parts are found ok 				\r\n','|Clean the tool holder and spindle,ATC ARM 		\r<br/>','|1.TO every part setting time to check and ensure the m/c ATC arm and shutter door . 					\r<br/>2.once a week clean the ATC Shutter and information pass the all 3 shift operator, 							\r<br/>','CAPA FOUND OK','','2018-07-20','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','Misc','Yashawantha(NH)','no','','|Based on the usage of the part [Assembly Requirement], since a shaft gets into the bore, the checking method was changed and all the rejected parts were subjected to re-inspection using a GO and NOGO Plug Gage							\r\n','E3456','pe|qas|','2018-08-12|2018-08-12|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10891,'51-084A','THE BOEING COMPANY','BRACKET DETAIL','781290A2','332A2930-63','NA','PSDL REV B',1,'BOEING 001U','','74023','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','* Bore diameter oversized by 0.030MM.','cross check the CRC value in  tool offset D value |Enter the correct CRC value in tool offset D value|Measure and ensure  the Bore diameter value ','|Enter the correct CRC value in tool offset D value','|Before Run the Bore program Cross check the CRC value in tool offset D value and M00  MSG given inside the program multiple commands','CAPA found ok.','','2018-07-20','pe_sez(a)','pe_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','Misc','qas_sez(a)','no','','|Previous part Bore value measured and ensure','Z3456','pe_sez|qas|','2018-09-11|2018-09-14|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10892,'56-022','GKN Aerospace Orangeburg','SUPPORT ANGLE, LWR','395824','119A1440-612','NA','PSDL REV B',1,'LTA Orangeburg 737 W','1','78004','','2018-07-19',NULL,'yes','yes','yes','no','no','no','no','no','no','wrong loading the fixture ','wrong loading the fixture|to the machining time to check the fixture front side ca-rectally load   |to the machining time to check the fixture front side ca-rectally load  |to the machining time to check the fixture front side ca-rectally load  ','|Inform to operator every time part loading cross check the fixture front face.','|Inform to operator every time part loading cross check the fixture front face.','CA AND PA FOUND OKAY','','2018-07-20','op_sez(s)','op_sez(s)','','2018-07-19','','F8003-S','Rev 0 dt 8-1-2009',0.00,'','Closed','no','yes','no','With Treatment','','03','no','Misc','op_sez(s)','no','','to the machining time to check the fixture front side ca-rectally load  ','Z3456','pe_sez|qas_sez|','2018-11-15|2018-11-15|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10893,'35-406','Saab AB','BRACKET ','745697','D522 73395 200 00','','A',1,'OWED-LTA-001','','75576','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Base thickness less than requirement.','Part taper butting in fixture.|Part not checked in the feeler gauge before running the program.|Part over tighten clamp bent but not observed before run the machine.|Part lifting while tightening operator dint identify that problem.','Check the part in feeler gauge before run the program.','Message given in the program when this CRN loaded to the machine for check the butting.','CAPA FOUND OK','','2018-07-21','prodn_aero(prodn)','Manjunatha.D()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Dinesh kulal()','no','','Feeler gauge check the part butting face.','A3456','qas|','2018-08-12|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10894,'35-600','Saab AB','FRAME','521026C1','D5227338520400','NA','PART ISSUE C',2,'OWED-LTA-001','','78202','','0000-00-00',NULL,'yes','no','no','no','yes','yes','no','no','no','Web thickness got undersized which measures 1.1mm to 1.3mm instead of 1.6+/-0.2mm','part thickness under size|part not proper  butted|part was not clamped sufficient|part was bend, operator did not noticed bend in the part','|1, Inform the store person about the bend in the raw material.\r<br/>2, Inform the all the operator to load the raw material with bend only under presence of supervisor','|add one more operation to remove materiel from one face.','Operation included in D00 format. and the changes to be included in the CRN Up-issue.','','2018-07-21','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','NC CREATE','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','Misc','Ranjith(G)','no','','|check the all raw material','E3456','pe|qas|','2018-07-31|2018-07-31|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10895,'56-015','GKN Aerospace Orangeburg','SUPPORT BRACKET - LWR','260816B4','119A1216-603','NA','PSDL REV-',1,'LTA Orangeburg 737 W','','78430','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','PART RUNNING TIME FIXTURE GOT DISTURB ','IMPROPER CLAMPING OF FIXTURE','|ENSURED THE PROPER CLAMPING OF THE FIXTURE AND HAVE TAKEN CLEARANCE FROM THE SUPERVISOR PRIOR THE START OF THE PROCESS  ','|OPERATOR IS INSTRUCTED TO CROSS-CHECK THE FIXTURE CLAMPING BEFORE THE COURSE OF ACTION','CA AND PA FOUND OKAY','','2018-07-21','pe_sez(a)','Lohith K,','','0000-00-00','FIXTURE DISTURB PART PROFILE CHANGED ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','3','no','Slim3n-5AHS-1','pe_sez(a)','no','','|PROCESS IS STOPPED AND INFORMED TO PRODUCTION SUPERVISOR ABOUT THE ERROR HAPPENED DURING THE COURSE OF ACTION','Z3456','cam|qas_sez|','2018-10-30|2018-11-15|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10896,'35-415','Saab AB','SHAFT LATCH LINK','M789340','D522 73496 200 00','','A',1,'OWED-LTA-004','','75694','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','OD UNDER SIZER ON 0.015MM','Outer diameter under sized during the last operation.|Trial was carried out to avoid the center mismatch.|Initially the part was machined 250mm at one pass and 250mm in the second pass, in order to reduce the setup timing and to reduce the cycle time the part was loaded to the full length due to which tapper occurred.|Due to high length the material over hanged and resulted in tapper. ','|1) Informed all the operator to continue the machining in the old process.\r<br/>2) Similar trial was conducted in the turn-mill machine in SEZ and found the part accepted.','|1) Requested the engineering team to revise the MPS and NC program according to the turn-mill machine in SEZ to avoid similar deviation.','CA PA Found ok.','','2018-07-21','Raghavendra Rao(R)','Raghavendra Rao(R)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Raghavendra Rao(R)','no','','|Immediately stopped the machine and changed the machine setup to the old process and continued the production.','E3456','qas|qas|','2018-08-01|2018-08-01|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10897,'56-045','GKN Aerospace Orangeburg','FAIRING SUPPORT - L.E., L','260816B4','119A1542-603','NA','PSDL REV -',1,'LTA Orangeburg 737 W','','78008','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','HOLE CO-ORDINATE MEASURED OUT OF TOLERANCE 0.1mm to 0.2mm DUE TO THIS POSITION WAS 0.5mm ','Machine (Rotary) Parameter not checked while installation of the machine.\r\nDue to rotary(Autocam) error this deviation observed.|The Rotary activation process has to be carried out by the OEM during the fabrication of the machine which was not done and was also not validated by the OEM installers during the machine installation.','|MAKINO application engineer came and parameter corrected.','|All the 3 slim machines  (slim3n-5AHS-1,slim3n-5AHT-2,slim3n-5HT-1) 5axis parameter cross check and one dummy part which have Holes position tolerance, manufactured and checked in CMM and found ok.','CAPA found ok.','','2018-07-23','pe_sez(a)','Shivaraj K S,Lohith K,Kiran Kumar M,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','Slim3n-5AHS-1','qas_sez(a)','no','','|Informed to OEM MAKINO regarding the error.','Z3456','pe|qas|','2018-12-15|2018-12-15|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10898,'35-456A','Saab AB','LATCH BRACKET','LL97302','D522 73484 200 00','','PART ISSUE A',2,'OWED-LTA-002','','72768','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dig mark on part','While part 1st operation running time part was lifted.\r\n\r\n','|Inform to operator before running the programs check part clamping properly. \r<br/>','|Inform to operator each and every part check the RM size after load the part and continue the production. \r<br/>','CAPA FOUND OK','','2018-07-23','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','3','no','Misc','Prashanth Kumar(M)','no','','|Inform to operator before running the programs check part clamping properly. \r\n','E3456','pe|qas|','2018-08-12|2018-08-12|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10899,'51-014','THE BOEING COMPANY','DRIP-SHIELD PAN MOUNTING ','616873','673Z3480-23','','NIL',1,'BOEING 001J','','75746','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','RM loading wrong shown,40mm instead off 30mm  in MPS.','RM loading wrong shown,40mm instead off 30mm in MPS.|Typo Error|Corrected the typing mistake in MPS|Another person from the department is checking the MPS|Prepared the Visual check list ','|Another person from the department is checking the MPS','|Preparing the Visual check list ','CAPA found ok','','2018-07-24','Ramesh(Poojary)','Sathisha(K.C.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','1','no','Misc','Subramanya L(Naik)','no','','|Correction of typo error in MPS','E3456','pe|cam|qas|qas|','2018-07-28|2018-08-06|2018-12-19|2018-12-19|','2018-12-19',NULL,NULL,NULL,NULL,NULL,NULL),(10900,'34-072A','Magellan Aerospace Winnipeg','FITTING HINGE LUG R/H-FWD','58008-1','400-12910-2','NA','EM104302 Iss B,EM105092 Iss H,EM104765 Iss H',1,'C81597 Rev 001','','78011','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Profile dig mark on part,','Due to the wrong location of the fixture, the fixture was put in reversed way.|Due to wrong identification on fixture location.|Respective CRN was not engraved on the fixture to be identified.|As the same in-terminate plate was used for several fixtures the engraving was not done for identification.','|1.Fixture location has been changed.\r<br/>2.Engraved \"front\" on the fixture for the identification.','|1)In-terminate plates has been fixed for each fixture, and the CRN is also been engraved on the respective fixture.\r<br/>\r<br/>2)Before running time,idle pass is been performed without loading the work piece on to the fixture.','CAPA Found ok.','','2018-07-25','Dhananjaya(N)','Narasimhamurthy C,dharshan d,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','3','no','HAASVF2SS-2','Dhananjaya(N)','no','','|1.Checked the previous parts that was being manufactured.\r\n2.In-terminate plate and the fixture is fixed permanently.\r\n','E3456','pe|qas|','2018-07-26|2018-07-31|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10901,'35-531A','Saab AB','SHAFT LATCH','C90596.QYF2','D5227349020200','NA','PART ISSUE C',2,'OWED-LTA-002','','73919','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','OD UNDER SIZE. ','OD Undersized -0.015mm beyond drawing limit.|OD undersized during the re-pass operation as the re-pass ran twice.|Re-pass ran twice with same -0.15 wear offset as the operator provided +0.2mm wear offset during the insert change.|To maintain stock in the ID after the insert change the operator provided -0.2mm in the initial stage and after measuring the diameter he provided -0.15mm to remove the stock and finish to the drawing requirement during this time the re-pass operation was carried out and resulted in diameter was undersized.|Operator was unaware that the program for OD runs twice with different stock levels to achieve finish in the final operation.\r\nContainment Action:','|Changed the wear offset from +0.2mm to +0.1mm in the next part and after the completion changed the offset to -0.02mm according to the program(after considering both the pass) and found the next part OK. ','|Informed all the operator to check the relevant features after the insert change and provide of the offset accordingly with proper guidance from the supervisor or senior operators ','Next batch shipments monitored and found ok. ','','2018-07-25','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','10','no','Misc','Yashawantha(NH)','no','','|\r\nImmediately stopped the machine and changed the wear offset and continued the production on the next part. ','E3456','pe|qas|','2018-10-26|2018-10-30|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10902,'35-441B','Saab AB','HINGE','C91073','D5227338720000','NA','B',36,'OWED-LTA-002','','71310','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','yes','Is condition: Wrong part, is marked D5227338720000 but is a D5227338720200.\r\nShould be: D5227338720000 according to order.','Part of D5227338720000 is marked with part no D5227338720200 and vice versa.|Part marking operator mixed up the parts during the part marking operation.|Operator took both the similar parts together for the marking rocess.|Operator was not aware that both are different part with similar view.','|Informed the receiving inspection department to verify the part marking of done on the part before shipment.','|Supplier to individually individual parts with tag\' no\'s that are mentioned on the work orders through out the process and the part marking operator to confirm the label with the work order and to remove the label after the completion of part marking.','Next batches found ok.','C65349','2018-07-25','qas_sez(a)','qas_sez(a)','OF-003122','2018-07-24','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','DN40530','Cust End','yes','Misc','qas_sez(a)','no','','|All the parts in FG and WIP are inspected and no similar parts found affected.','E3456','qas|','2018-12-10|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10903,'56-031','GKN Aerospace Orangeburg','FAIRING SUPPORT - LE, LH','233038','119A1540-603','NA','PSDL REV -',1,'LTA Orangeburg 737 W','','78532','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Hole Position not achieved due to error in the Rotary table. ','HOLE POSITION IS NOT ACHIEVED. SINCE, THE ERROR IN MACHINE ACCURACY','|ABRUPT ACTION TAKEN & MACHINE IS DONE WITH FINE TUNE ','|PERIODICALLY THE MACHINE HAS TO BE CHECKED FOR THE ACCURACY MAINTENANCE ','CA and PA found okay','','2018-07-25','pe_sez(a)','Lohith K,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','1','no','Slim3n-4AHS-1','pe_sez(a)','no','','|STOPPED THE PRODUCTION PROCESS AND INFORMED TO PRODUCTION HEAD REGARDING THE ERROR ','Z3456','pe_sez|qas_sez|','2018-11-16|2018-11-16|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10904,'35-456A','Saab AB','LATCH BRACKET','HR288202','D522 73484 200 00','','PART ISSUE A',1,'OWED-LTA-002','','76916','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Running part rotate',' program running time tool broken|During Outer wall finishing program,the lug rotated and tool dig mark occurred. \r\n','|proper bolts changed and continue the production\r<br/>','|informed all the operators to use bolt of length 10mm greater then the part thickness. \r<br/>','CAPA FOUND OK','','2018-07-26','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Prashanth Kumar(M)','no','','|All proves part cross cheeked and all the parts are ok. \r\n','E3456','pe|qas|','2018-08-12|2018-08-12|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10905,'35-456A','Saab AB','LATCH BRACKET','LL0102097','D522 73484 200 00','','PART ISSUE A',2,'OWED-LTA-002','','72764','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','BORE OVER SIZE BY 0.040MM.','CRC value entered wrongly by the operator.\r\n','|Informed all the operator to check the CRC value before starting the production. \r<br/>','|All the Operators are informed not to run the machine until supervisor confirms the CRC value entered. \r<br/>','CAPA FOUND OK','','2018-07-26','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','06','no','Misc','Yashawantha(NH)','no','','|Immediately stopped the machine and changed the CRC value. \r\n','E3456','pe|qas|','2018-08-12|2018-08-12|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10906,'35-646','Saab AB','LEVER 3','533740C','D5227280920300','NA','B',1,'PA1687 LTA-2','','73912','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','TOOL DIG MARK.','Tool overhang. |Tool length not mentioned on MPS.','|Tool length added on program.','|Tool length added on program.','CA/PA found satisfactory.','','2018-07-26','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','06','no','Misc','Yashawantha(NH)','no','','|reset the tool length and run the program.','E3456','pe|nandishkumardk|','2018-11-27|2018-11-27|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10907,'35-611A','Saab AB','LEVER 1','532795C','D5227281620100','NA','PART ISSUE B',1,'PA1687 LTA-2','','73722','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','part Found Dig upto 1 mm in inside the slot','1.part handling time lift into the floor |2.part surface contact to raw material while takeing','|1.All finishing parts will covered with sleeves .','|1.proper training will be given to all employes.','CA/PA Found satisfied.','','2018-07-26','HariPrasad()','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','DN42777','FI','no','Misc','qas_sez(a)','no','','|1.Next time operator will be handled care fully.','Z3456','qas_sez|pe_sez|qas_sez|','2018-07-26|2018-12-18|2019-01-05|','2019-01-05',NULL,NULL,NULL,NULL,NULL,NULL),(10908,'56-020','GKN Aerospace Orangeburg','SUPPORT ANGLE, UPR','395824','119A1440-608','NA','PSDL REV B',1,'LTA Orangeburg 737 W','','77987','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','Due to Program Error part dent mark observed.','','','','','','2018-07-26','pe_sez(a)','pe_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','With Treatment','','03','no','Misc','pe_sez(a)','no','','','Z3456','qas_sez|','2018-07-27|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10909,'56-015','GKN Aerospace Orangeburg','SUPPORT BRACKET - LWR','260816B4','119A1216-603','NA','PSDL REV-',1,'LTA Orangeburg 737 W','','77979','','0000-00-00',NULL,'yes','no','yes','no','yes','no','no','no','no','Hole Position not achieved due to error in the Rotary table.','HOLE POSITION IS NOT ACHIEVED. SINCE, THE ERROR IN MACHINE ACCURACY','|ABRUPT ACTION TAKEN & MACHINE IS DONE WITH FINE TUNE','|PERIODICALLY THE MACHINE HAS TO BE CHECKED FOR THE ACCURACY MAINTENANCE','CA AND PA FOUND OKAY','','2018-07-26','pe_sez(a)','pe_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','pe_sez(a)','no','','|STOPPED THE PRODUCTION PROCESS AND INFORMED TO PRODUCTION HEAD REGARDING THE ERROR ','Z3456','cam|cam|qas_sez|','2018-10-30|2018-10-30|2018-11-15|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10910,'56-016','GKN Aerospace Orangeburg','SUPPORT BRACKET - LWR','260816B4','119A1216-604','NA','PSDL REV -',1,'LTA Orangeburg 737 W','','77980','','0000-00-00',NULL,'yes','no','yes','no','yes','no','no','no','no','Hole Position not achieved due to error in the Rotary table.','HOLE POSITION NOT ACHIEVED. SINCE, THE ERROR IN MACHINE ACCURACY','|ABRUPT ACTION TAKEN & THE MACHINE IS DONE WITH FINE TUNE','|PERIODICALLY THE MACHINE HAS TO BE CHECKED FOR THE ACCURACY MAINTENANCE','CA AND PA FOUND OKAY','','2018-07-26','pe_sez(a)','pe_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','01','no','Misc','pe_sez(a)','no','','|STOPPED THE PRODUCTION PROCESS AND INFORMED TO PRODUCTION HEAD REGARDING THE ERROR','Z3456','cam|qas_sez|','2018-10-30|2018-11-15|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10911,'51-076','THE BOEING COMPANY','FTG - AFT FAIRING FRAME 2','340972','112U7625-13','NA','PSDL REV-',1,'BOEING 001V','','75642','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','BORE OVER SIZE DUE TO PROGRAM FAULT','The program posted to the machine was having an error|The Geometry selected was offset wrong|The Geometry selected was offset by 0.1mm in radius|This offset was intended to maintain a stock in the roughing stage. But the direction of offset was taken in the opposite direction.','|The geometry selection and offset verification was reviewed for this part, at the regions where the program is done using a offset surface.','|The program will be reviewed by a senior CAD/CAM Engineer before release.','Next produced parts are meet the drawing requirements and the parts are accepted.','','2018-07-27','pe_sez(a)','Umesh B,','','0000-00-00','BORE OVER SIZE DUE TO PROGRAM FAULT','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','3','no','i700-1','pe_sez(a)','no','','|The geometry was re-selected and the offset was given in the direction so as to maintain the stock in the roughing stage.','Z3456','cam|qas_sez|','2018-07-27|2018-07-27|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10913,'51A-061','THE BOEING COMPANY','FITTING ASSY PANEL SUPPOR','','115W3665-9','','PSDL REV -',1,'BOEING 001M','','A16908','','0000-00-00',NULL,'yes','no','yes','no','yes','no','no','no','no','at the time of reaming bush over size','1) Ovality formation inside the bore.|2) Due to run out in the reamer ID oversized due to ovality.|3) Chips were struck inside the holder and operator did not cleaned and noticed the inside of the holder before loading the reamer to it.','|Removed all the chips from the holder and cleaned the Holding area.','|informed the operator to clean the ID of holder during every tool change and to check the Run out of the tool after the tool change.','CA PA found ok.','','2018-07-27','Ramesh(D)','Karthineyan(V.S.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Assembly','','In processes','no','','Ramesh(D)','no','L07712','|Immediately stopped the machine and checked the run out of the reamer and cleaned the holding area.','E3456','qas|','2019-04-26|','2019-04-26',NULL,NULL,NULL,NULL,NULL,NULL),(10914,'46-036B','Mahindra Aerostructures Pvt.Ltd','STRAP ','24989','D575-40868-201-01','NA','G01, BOM ISS J,ECN NG29999ST2TX44',1,'3101296455','','78417','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','chf over size,(0.3mm)','Tool offset error after replacing the tool.','|Operator should check on a test block, to check the tool offset for any error before machining the actual part after every cutting tool replacement sequence.','|Need to cross-check the tool offset with a test block, after a tool replacement, mainly for the tools which involves critical operations and control dimensions.','','','2018-07-27','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','3','no','Misc','Dhananjaya(N)','no','','|All the completed parts are checked and found ok.','E3456','pe|qas|','2018-10-25|2018-10-27|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10915,'56-020','GKN Aerospace Orangeburg','SUPPORT ANGLE, UPR','395824','119A1440-608','NA','PSDL REV B',1,'LTA Orangeburg 737 W','','78002','','0000-00-00',NULL,'no','no','yes','no','no','no','yes','yes','no','**Tool dig mark on face. this is program fault.','Tool dig mark observed on face|Program was generated on wrong side|UCS selection was wrong','|UCS changed and program was regenerated and given to production.','|Before giving any program, Verify by simulation and cross check with senior programmer.','NEXT PART FOUND OKAY.','','2018-07-27','pe_sez(a)','Shivaraj K S,Lohith K,Kiran KM,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','3','no','Slim3n-5AHT-1','pe_sez(a)','no','','|Immediately stopped machine and checked the program,machine offset and tool.','Z3456','cam|qas_sez|','2018-11-16|2018-11-16|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10916,'51-128','THE BOEING COMPANY','SPACER','525335-03','332W1912-79','NA','PSDL REV -',1,'486998 MPP','','73084','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dig mark observed on side face.','MORE CUTTING SPEED AND ROUGHING STOCK MORE IN PARTICULAR AREA|THE RAW MATERIAL LENGTH IS UPPER LIMIT. SO THE CUTTING TOOL STRUGGLED TO REMOVE THE EXCESS MATERIAL','|THE MORE LENGTH PARTS IDENTIFIED. EXCESS LENGTH ARE PRE- MACHINED. LOW CUTTING SPEED PROGRAM RECEIVED FROM ENGG.dEPT AND PROVED. ','|THE MORE LENGTH PARTS IDENTIFIED. EXCESS LENGTH ARE PRE- MACHINED. LOW CUTTING SPEED PROGRAM RECEIVED FROM ENG.dept AND PROVED AND PROGRAM SAVED.','Cutting parameters revised and next batches produced found ok.','','2018-07-28','pe_sez(a)','Shivaraj K S,Kiran KM,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','3','no','PS105-01','pe_sez(a)','no','','|PRODUCTION STOPPED. COMPLETED PARTS ARE CHECKED AND FOUND OK.','Z3456','pe_sez|qas|','2018-09-24|2018-09-27|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10917,'51-051','THE BOEING COMPANY','BRACKET','436272','149A7371-9627','','PSDL REV A',2,'BOEING 001C','','75807','','0000-00-00',NULL,'yes','yes','yes','','','','','','','PART RUNNING TIME 16*FLAT BROKEN SO PART  DING MARK PART REJECTED.','MORE CUTTING SPEED AND ROUGHING STOCK MORE IN PARTICULAR AREA|THE RAW MATERIAL LENGTH IS UPPER LIMIT. SO THE CUTTING TOOL STRUGGLED TO REMOVE THE  EXCESS MATERIAL |THE CUTTING OVER HANG ALSO MORE','|THE MORE LENGTH PARTS IDENTIFIED. EXCESS  LENGTH ARE PRE MACHINED. LOW CUTTING SPEED PROGRAM RECEIVED FROM ENGG.dEPT AND PROVED. ','|THE MORE LENGTH PARTS IDENTIFIED. EXCESS  LENGTH ARE PRE MACHINED. LOW CUTTING SPEED PROGRAM RECEIVED FROM ENGG.dEPT AND PROVED. ','Changes implemented and next batches produced found ok.','','2018-07-28','Karthineyan(V.S.)','        Umesh B','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','03','','','','','','|PRODUCTION STOPPED. COMPLETED PARTS ARE CHECKED AND FOUND OK.','Z3456','pe|pe_sez|qas|','2018-08-30|2018-09-20|2018-09-26|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10918,'35-600','Saab AB','FRAME','531963C','D5227338520400','NA','PART ISSUE C',2,'PA1687 LTA-1','','73198','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','part profile tool dig mark','Outer part profile tool dig mark. |During final operation in the machine an alarm of Z Axis serial date communication fault was displayed because of that Z Axis came down so the part was rejected. |TO Inform to service engineer and services provide on proper timings ,','Informed to the service engineers they came and checked all the machine parameters and said that their is a fault in Z axis cable,and it was replaced by a new one. ','The machine will be stopped as soon as alarm is displayed and we instructed the service engineer to check the cable every preventive maintenance. ','CA PA found Ok.','','2018-07-30','Krishna(Chowdary.G.P.)','Rakeshbabu(V)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','07','no','Misc','Narayanappa(G)','no','','Previously finished parts has been checked and all the parts are ok ','E3456','qas|','2018-07-31|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10919,'35-644','Saab AB','LATCH FORK','LL0109408','D5227348920400','NA','C',37,'OWED-LTA-004','','73188','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','part boring operation running time chips present in spindle .','1part running time chips present in spindle so tool run out occur |2.To give the proper training for operator while running time check the tool clamping before running \r\n|3.Monitor to check the tool-holder for bore finish tool |4.inform to all operators and check the critical dimension 1:1 ratios |5.Further parts are found ok ','Clean the tool holder and spindle,ATC ARM','1.once a week clean the ATC Shutter and information pass the all 3 shift operator,\r<br/>2.TO every part setting time to check and ensure the m/c ATC arm and shutter door . ','CAPA FOUND OK','','2018-07-30','Krishna(Chowdary.G.P.)','Rakeshbabu(V)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','With Treatment','','05','no','Misc','Anjinamurthy(H)','no','','Based on the usage of the part [Assembly Requirement], since a shaft gets into the bore, the checking method was changed and all the rejected parts were subjected to re-inspection using a GO and NOGO Plug Gage.','E3456','qas|qas|','2018-08-12|2018-11-19|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10920,'51A-061','THE BOEING COMPANY','FITTING ASSY PANEL SUPPOR','','115W3665-9','','PSDL REV -',1,'BOEING 001M','','A16908','','0000-00-00',NULL,'yes','no','yes','no','yes','no','no','no','no','Bush over sized due to reaming.','1) Ovality formation inside the bore.|2) Due to run out in the reamer ID oversized due to ovality.|3) Chips were struck inside the holder and operator did not cleaned and noticed the inside of the holder before loading the reamer to it.','|Removed all the chips from the holder and cleaned the Holding area.','|Informed the operator to clean the ID of holder during every tool change and to check the Run out of the tool after the tool change.','CA PA found ok.','','2018-07-30','Ramesh(D)','Karthineyan(V.S.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Assembly','','In Processes','no','Misc','Ramesh(D)','no','L07726','|Immediately stopped the machine and checked the run out of the reamer and cleaned the holding area.','E3456','qas|','2019-02-21|','2019-02-21',NULL,NULL,NULL,NULL,NULL,NULL),(10921,'47-097B','GKN Aerospace Filton','BRACKET FT5 FWD','W2713','F57550783001','NA','PART ISSUE E04',1,'LTA GKN GS72 - Forgi','','76282','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','Due to program changing time part wall -ve side. ','part rejected due to process proving time wrong program given, |Due to NC Program Problem .|wrong UCS Selected ,Due to changing in new roughing Program 40 FM Instead of 32 face mill. |program wall stock not distributed equally so part wall dig mark absorbed in finishing stage |At first time 32Facemill running in long cycle time so changing the roughing program dia 40face mill on that time wrong program generated.','Updated NC program and Executed on Machine and Part Found OK. ','Before Execution the program on Machine Programmer has to double cross check program. ','Effectiveness found ok.','','2018-07-30','Ramesh(Poojary)','Niranjan(Murthy)','','0000-00-00','part wall under size ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Gurukiran S(M)','no','','Updated NC program and Executed on Machine and Part Found OK. Obsolete old program and New updated program moved to Program Data Storage ','E3456','qas|','2018-07-30|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10922,'47-099B','GKN Aerospace Filton','BRACKET M/C TRACK 2 FWD ','02318122','F57550193001','NA','PART ISSUE H02',4,'LTA-GKN-002','','77293','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Due to program changing time part wall -ve side. ','part rejected due to process proving time wrong program given,|Due to NC Program Problem .|wrong UCS Selected ,Due to changing in new roughing Program 40 FM Instead of 32 face mill.|program wall stock not distributed equally so part wall dig mark absorbed in finishing stage | At first time 32Facemill running in long cycle time so changing the roughing program dia 40face mill on that time wrong program generated.','\r<br/>Updated NC program and Executed on Machine and Part Found OK','Before Execution the program on Machine Programmer has to double cross check program. ','CA PA found ok.','','2018-07-30','Ramesh(Poojary)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','01','no','Misc','Gurukiran S(M)','no','','Updated NC program and Executed on Machine and Part Found OK. Obsolete old program and New updated program moved to Program Data Storage ','E3456','qas|','2018-08-09|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10923,'35-230A','Saab AB','HINGE BRACKET 3 ','4754501 2','D576 50006 205','','D00',1,'1600219297','','77841','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Rib thickness under size.','Part running time part will shifted rib thinness will out off tolerance   |Operator not tight correctly.','','','','','2018-07-30','Lohith(K)','        Kiran KM','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','','','','1','','','','','','','Z3456','pe|pe_sez|qas_sez|','2018-08-12|2018-09-28|2018-10-29|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10924,'35A-464','Saab AB','FITTING ASSY','','D522 73408 001 00','','A',4,'OWED-LTA-001','','A16254','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','yes','Is condition: Damage in paint layer.\r\nShould be: No Damage, Continuous and covering surface treatment all over.','Paint chip-off on the part surface|Due to improper packing method the paint layer got damaged during transit.|Parts were packed one after the other with a single layer of bubble sheet wrapped around the part due to witch the paint layer on the part got damaged during transit.|Packing trials was carried out.','|Informed all the packing individuals to pack only one part in a package.','|Informed all the packing individuals to pack only one part in a package.','Next batch shipments monitored and found ok.','C66846','2018-07-31','Dharanishankar()','Dharanishankar()','OF-003123','2018-07-25','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','Cust End','yes','Misc','qas(qas)','no','','|Immediately informed the packing team verified the packing done to similar parts and changed the method.','E3456','qas|','2018-11-27|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10925,'35A-464','Saab AB','FITTING ASSY','','D522 73408 001 00','','A',1,'OWED-LTA-001','','A16253','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','yes','Is condition: Damage in paint layer.\r\nShould be: No Damage, Continuous and covering surface treatment all over.','Paint chip-off on the part surface|Due to improper packing method the paint layer got damaged during transit.|Parts were packed one after the other with a single layer of bubble sheet wrapped around the part due to witch the paint layer on the part got damaged during transit.|Packing trials was carried out.','|Informed all the packing individuals to pack only one part in a package. ','|Informed all the packing individuals to pack only one part in a package. ','Next batch shipments monitored and found ok. ','C66466','2018-07-31','Dharanishankar()','Dharanishankar()','OF-003123','2018-07-25','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','Cust End','yes','Misc','qas(qas)','no','','|Immediately informed the packing team verified the packing done to similar parts and changed the method.','E3456','qas|','2018-11-27|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10926,'35A-464','Saab AB','FITTING ASSY','','D522 73408 001 00','','A',1,'OWED-LTA-001','','A16239','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','yes','Is condition: Damage in paint layer.\r\nShould be: No Damage, Continuous and covering surface treatment all over.','Paint chip-off on the part surface|Due to improper packing method the paint layer got damaged during transit.|Parts were packed one after the other with a single layer of bubble sheet wrapped around the part due to witch the paint layer on the part got damaged during transit.|Packing trials was carried out.','|Informed all the packing individuals to pack only one part in a package.','|Informed all the packing individuals to pack only one part in a package.','Next batch shipments monitored and found ok.','C66472','2018-07-31','Dharanishankar()','Dharanishankar()','OF-003123','2018-07-25','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','Cust End','yes','Misc','qas(qas)','no','','|Immediately informed the packing team verified the packing done to similar parts and changed the method.','E3456','qas|','2018-11-27|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10927,'47-099B','GKN Aerospace Filton','BRACKET M/C TRACK 2 FWD ','02318122','F57550193001','NA','PART ISSUE H02',1,'LTA-GKN-002','','77292','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','part wall thickness -vie side','part rejected due to process proving time wrong program given, |Due to NC Program Problem .|wrong UCS Selected ,Due to changing in new roughing Program 40 FM Instead of 32 face mill. |program wall stock not distributed equally so part wall dig mark absorbed in finishing stage |At first time 32Facemill running in long cycle time so changing the roughing program dia 40face mill on that time wrong program generated.','Updated NC program and Executed on Machine and Part Found OK. ','Before Execution the program on Machine Programmer has to double cross check program.','CAPA found ok.','','2018-07-31','Ramesh(Poojary)','SIDDESH ,','','0000-00-00','Due to program changing time part wall -ve side.','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','1','no','HMC 440','Ramesh(Poojary)','no','','Updated NC program and Executed on Machine and Part Found OK. Obsolete old program and New updated program moved to Program Data Storage ','E3456','qas|','2018-08-09|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10928,'35A-561','Saab AB','VENT HOOK ASSY','','D522 73530 002 00','','PART ISSUE B',11,'OWED-LTA-003','','A16017','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','yes','Is condition: Wrong part, is marked D5227353000300 but is a D5227353000200, CoC is wrong as well.\r\nShould be: D5227353000200 according to order.','Part marking interchanged due to improper identification.|Similar parts are taken from FG for packing together and identified together|Parts are stored in FG with group identification and when the COC was released the parts were taken together for individual identification and dispatch.|After the completion of receiving inspection the parts were handed over to FG separatedly with group identification (i.e. lables for the entire work order in a single sheet)|Insufficiant time allocation because this operation was supposed to be carried out by supplier and was not done because the output from the barcode machine in the suplier location was breakdown.','|1) CIM Quality Engineer visited the supplier and corrected the program parameters.\r<br/>2) CIM issued the New PO to the supplier and the parts to be identified with proper label by supplier from 1-Oct-18.','|1) Supplier to print the label and identify the parts from 1-Oct-18 and CIM to verify the label along with the parts before handing over to FG.\r<br/>2) For the assembly parts the part marking to be done by the assembly operator and the final part will be inspected the quality inspector.','Next shipments monitored and no similar non-conformance occurred','C66353','2018-07-31','Dharanishankar()','Dharanishankar()','OF-003124','2018-07-26','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','Cust End','yes','Misc','qas(qas)','no','','|All parts in FG and WIP inspected and no similar parts found affected.','E3456','qas|','2018-12-10|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10929,'47-104','GKN Aerospace Filton','BRACKET FT4 FWD','W2948','F57550777003','NA','PART ISSUE E',1,'1210042293-1','','76248','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','part wall thickness -vie side ','part rejected due to process proving time wrong program given, |Due to NC Program Problem .|wrong UCS Selected ,Due to changing in new roughing Program 40 FM Instead of 32 face mill. |program wall stock not distributed equally so part wall dig mark absorbed in finishing stage |At first time 32Facemill running in long cycle time so changing the roughing program dia 40face mill on that time wrong program generated.','\r<br/>Updated NC program and Executed on Machine and Part Found OK.','Before Execution the program on Machine Programmer has to double cross check program. ','CA PA found ok.','','2018-07-31','Krishna(Chowdary.G.P.)','SIDDESH ,Niranjan Murthy,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','11','no','HMC 440','Gurukiran S(M)','no','','Updated NC program and Executed on Machine and Part Found OK. Obsolete old program and New updated program moved to Program Data Storage ','E3456','qas|','2018-08-09|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10930,'35-600','Saab AB','FRAME','531963C','D5227338520400','NA','PART ISSUE C',2,'PA1687 LTA-1','','73198','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','part profile tool dig mark','During Outer wall finishing program,the lug rotated and tool dig mark occurred. |The bolt length selected was equal to thread length in the lug  |operator not select the correct length bolt.|operator was not aware about the proper bolt length to be used','proper bolts changed and continue the production.','informed  all the operators to use bolt of length 10mm greater then the part thickness.','CA PA Found ok.','','2018-07-31','Krishna(Chowdary.G.P.)','Rakeshbabu(V)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','07','no','Misc','Narayanappa(G)','no','','all proves part cross cheeked and all the parts are ok.  ','E3456','qas|','2018-07-31|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10931,'51-083A','THE BOEING COMPANY','BRACKET DETAIL','659121','332A2930-8','NA','PSDL REV B',1,'BOEING 001U','','74016','','0000-00-00',NULL,'no','yes','yes','yes','no','no','no','no','no','While running 2nd operation profile measured undersized.','1.The RM cutting was not done as per the requirement\r\n|2.While Cutting the RM got slipped and the cutting took crossly','|The Material was identified and issued to production to check if the parts can be manufactured with the reduced RM size.','|Training was provided to the RM stores team on the cutting requirements and the cutting layout by engineering.','CA/PA satisfied.','','2018-07-31','pe_sez(a)','Shivaraj K S,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','3','no','Slim3n-03','pe_sez(a)','no','','|1)Stop the RM cutting work and informed operator to the supervise.\r\n2)All the previously cut size are re-inspected and found acceptable.','Z3456','qas_sez|','2019-01-16|','2019-01-16',NULL,NULL,NULL,NULL,NULL,NULL),(10932,'34-052A','Magellan Aerospace Winnipeg','MTG LUG, GEARBOX, RH','G22347','400-12608-2','NA','EM104302 Iss B,EM105092 Iss H,EM104765 Iss H',1,'C81597 Rev 001','','76683','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','WALL THICKNESS MINES....','Part wall thickness undersized.|Part shifted during the machining time.|Part tilted during the machining time as the part was not properly butted on the fixture.|Bore was having tapper due to which the part butted in the eye point during the manual clamping time and while machining due to the tool load the part shifted and thickness got undersized.','|Informed the milling supervisors about the issue and reworked the parts with bore tapper and continued the production.','|1) Informed the milling department to finish the bore to close tolerance from the mean value to eliminate improper butting of the part.\r<br/>2) Informed all the turning operator to dial the Jaw\'s during the setting time which helps in identifying the improper butting of part during the running time.','CA PA found ok.','','2018-07-31','Dinakar K()','Dinakar K()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','07','no','Misc','GUNDEGOWDA(H.G.)','no','','|Immediately stopped the machine and checked the bore of the remaining parts.','E3456','qas|qas|','2018-08-14|2018-08-17|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10933,'51A-083A','THE BOEING COMPANY','BRACKET ASSY','','332A2930-7','','PSDL REV B',3,'BOEING 001U','','A16149','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','tool dig mark in hole','Refer NC NO:10744','|Refer NC NO:10744','|Refer NC NO:10744','Refer NC NO:10744','','2018-07-31','qas_sez(a)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Assembly','','FI','no','Misc','qas_sez(a)','no','','|Refer NC NO:10744','Z3456','qas_sez|','2019-01-18|','2019-01-18',NULL,NULL,NULL,NULL,NULL,NULL),(10934,'51A-083A','','','','','','',0,'','','','','0000-00-00',NULL,'no','no','no','no','no','no','no','no','no','','','','','','','2018-07-31','sppkg_sez(a)','','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Cancelled','no','no','no','','','','no','','select','no','','','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10935,'51-046','THE BOEING COMPANY','BRACKET','436263','149A7371-9612','','PSDL REV A',1,'BOEING 001F','','75345','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Running time tool broken so part dig mark found.\r\n','MORE CUTTING SPEED AND ROUGHING STOCK MORE IN PARTICULAR AREA|THE RAW MATERIAL LENGTH IS UPPER LIMIT. SO THE CUTTING TOOL STRUGGLED TO REMOVE THE EXCESS MATERIAL |THE CUTTING TOOL OVER HANG ALSO MORE.','|THE MORE LENGTH PARTS IDENTIFIED. EXCESS LENGTH ARE         PRE-MACHINED. LOW CUTTING SPEED PROGRAM RECEIVED FROM ENG.dept AND PROVED.','|THE MORE LENGTH PARTS IDENTIFIED. EXCESS LENGTH ARE         PRE-MACHINED. LOW CUTTING SPEED PROGRAM RECEIVED FROM ENG.dept AND PROVED.','CAPA found ok.','','2018-07-31','pe_sez(a)','Raghu B()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','01','no','Misc','pe_sez(a)','no','','|PRODUCTION STOPPED. COMPLETED PARTS ARE CHECKED AND FOUND OK. ','Z3456','pe_sez|qas|','2018-09-24|2018-09-27|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10936,'35-622','Saab AB','FLAP, VENT','5334681B','D5227280420000','NA','PART ISSUE A',1,'OWED-LTA-003','','73684','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dia 9.995 H7 hole chamfer over size.','Dia 10*45 chamfer Tool wear offset value 0.5 up|Cross check the Tool offset wear value |Tool wear offset wear value given 0.0 and run','|Cross check the tool offset value and entered the corrected tool wear offset value and run.','|M00 MSG given in program inside and when the we run the double side chamfer program Do not put the value in tool wear offset +/-.   ','CAPA FOUND OK','','2018-08-01','Ravi nayak()','prodn_aero(prodn)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','05','no','Misc','Ravi nayak()','no','','|Cross check the Tool offset value and Tool offset wear value. ','A3456','qas_aero|qas_aero|','2018-09-06|2018-09-06|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10937,'51-119','THE BOEING COMPANY','RIBPOST - FRONT SPAR RIB ','AJ18','112T2215-6','NA','PSDL REV -',1,'486998 MPP','','69143','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Requirement of solution treating and aging Aluminum alloy from 7175-01 to 7175-T74 was not captured by\r\nthe engineering team during the process planning.','1. Requirement of solution treating and aging Aluminium alloy from 7175-T01 to 7175-T74 was not captured by the engineering team during the process planning.\r\n2. Missed to bubble the requirement of solution treating and aging Aluminium alloy from 7175-T01 to 7175-T74 during the FAIR documentation stage.|1. Missed to understand the Solution treating and aging Aluminium alloy from 7175-T01 to 7175-T74 from the part list during the  initial planning stage by the engineering team.\r\n2. Bubbling of drawing and Parts list for FAIR was done manually and this Parts List note was not captured or identified during FAIR review.|1. Mis-Interpretation of Part List and specification called out in the drawing.\r\n2. Bubbling had to be done manually as the electronic software for bubbling was not available in CIM Tools. Missing feature was not identified during the FAIR review because the reviewer was only concentrating on the bubbled points.|1. CIM was new to this requirement and specification.\r\n2. Electronic bubbling software was not in place at CIM Tools.\r\n3. FAIR not reviewed thoroughly','|1. All the part nos are re-Verified to ensure there is no similar skips in process by Engineering department from Apr 02, 2018 to April 05, 2018.\r<br/>2. Manufacturing Process Sheet (MPS) was amended by Manufacturing Engineer (ME) to include the requirement of capturing the solution treatment and aging of Aluminum alloy from 7175-01 to 7175-T74 after the completion of roughing of the part on Apr 9, 2018.\r<br/>3. Customer has given training on how to interpret the specification in conjunction with the engineering requirements on Mar 13, 2018','|1. Head Engineer or Authorized personal from the Engineering department will review and approve the planning order through ERP system before releasing to Production from May 4, 2018.\r<br/>2. \"Discus\" Auto ballooning software will be implemented tentatively on or before May 25, 2018 at CIM Tools, as this will highlight any un-captured features during the ballooning process.\r<br/>3. Training program to be scheduled by Head Quality for the Quality engineers involved in the production and review of FAIR documents on importance of checking 100% documentation on Jun 22, 2018.\r<br/>4. Training program to be scheduled by Head Engineering for the engineering personnel to concentrate on the importance of capturing all the details from the Part list as well as the drawings during the planning process on Jun 29, 2018.','Next Batch Wo#72714-4nos,73515-1no,74228-4nos,78536-1no,78537-1no,78538-2nos was machined as per the drawing PL requriments and MPS/51-119/Rev-01 and found OK.\r\n2.Delta FAIR was submitted for The Same FAIR #F51119002','','2018-08-01','qas_sez(a)','Umesh B,Nataraja C V,Diwakar R.B.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','DN36780','FI','no','i700-5','qas_sez(a)','no','','|1. Head Engineering raised an Inter Departmental memo (IDM) to call for a Cross Functional Team (CFT) meeting to notify the\r\nescapement and to find the cause of the escape Mar 30, 2018\r\n2. This issue was initially identified by CIM Tools on March 26, 2018, immediately all parts in stock and WIP was quarantined.\r\n3. Notification of Escapement (NOE) was communicated to the customer on the escape of parts by Project Engineer on Mar 27, 2018 ','Z3456','cam|qas_sez|','2018-11-22|2018-11-22|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10938,'51-119','THE BOEING COMPANY','RIBPOST - FRONT SPAR RIB ','AJ18','112T2215-6','NA','PSDL REV -',4,'486998 MPP','','70880','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Requirement of solution treating and aging Aluminum alloy from 7175-01 to 7175-T74 was not captured by\r\nthe engineering team during the process planning.','1. Requirement of solution treating and aging Aluminium alloy from 7175-T01 to 7175-T74 was not captured by the engineering team during the process planning. \r\n2. Missed to bubble the requirement of solution treating and aging Aluminium alloy from 7175-T01 to 7175-T74 during the FAIR documentation stage.|1. Missed to understand the Solution treating and aging Aluminium alloy from 7175-T01 to 7175-T74 from the part list during the initial planning stage by the engineering team. 2. Bubbling of drawing and Parts list for FAIR was done manually and this Parts List note was not captured or identified during FAIR review.|1. Mis-Interpretation of Part List and specification called out in the drawing. \r\n2. Bubbling had to be done manually as the electronic software for bubbling was not available in CIM Tools. Missing feature was not identified during the FAIR review because the reviewer was only concentrating on the bubbled points.|1. CIM was new to this requirement and specification. \r\n2. Electronic bubbling software was not in place at CIM Tools. 3. FAIR not reviewed thoroughly','|1. All the part nos are re-Verified to ensure there is no similar skips in process by Engineering department from Apr 02, 2018 to April 05, 2018.\r<br/>2. Manufacturing Process Sheet (MPS) was amended by Manufacturing Engineer (ME) to include the requirement of capturing the solution treatment and aging of Aluminum alloy from 7175-01 to 7175-T74 after the completion of roughing of the part on Apr 9, 2018.\r<br/>3. Customer has given training on how to interpret the specification in conjunction with the engineering requirements on Mar 13, 2018 ','|1. Head Engineer or Authorized personal from the Engineering department will review and approve the planning order through ERP system before releasing to Production from May 4, 2018.\r<br/>2. \"Discus\" Auto ballooning software will be implemented tentatively on or before May 25, 2018 at CIM Tools, as this will highlight any un-captured features during the ballooning process.\r<br/>3. Training program was conducted by Head Quality for the Quality engineers involved in the production and review of FAIR documents on importance of checking 100% documentation.\r<br/>4. Training program was conducted by Head Engineering for the engineering personnel to concentrate on the importance of capturing all the details from the Part list as well as the drawings during the planning process. ','Discuss software effectively used for capturing all the applicable requirements.Engineering captures all the details from the parts list and drawings during the planning process is well in place. Quality Personnel involve during the FAIR and production stage to review the Customer Specifications requirements and document the same.(FAIR Documents with Bubbling details)   ','','2018-08-01','qas_sez(a)','Umesh B,Nataraja C V,Diwakar R.B.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','DN38592','FI','no','i700-4','qas_sez(a)','no','','|1. Head Engineering raised an Inter Departmental memo (IDM) to call for a Cross Functional Team (CFT) meeting to notify the escapement and to find the cause of the escape Mar 30, 2018 \r\n2. This issue was initially identified by CIM Tools on March 26, 2018, immediately all parts in stock and WIP was quarantined. \r\n3. Notification of Escapement (NOE) was communicated to the customer on the escape of parts by Project Engineer on Mar 27, 2018','Z3456','cam|qas_sez|qas_sez|','2018-11-22|2018-12-05|2018-12-05|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10939,'51A-032','THE BOEING COMPANY','BRACKET ASSY','','149A7371-42','','PSDL REV A',2,'BOEING 001H','','A15783','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','no','PAINT PEALUP(TOP COAT)','1.The Teflon paint chip off surrounding the rivet during pressing the rivet|2.During pressing the rivet metal to metal contact|3.In butting block the  area where the parts were butting while riveting was not uniform |4.FOD of rivet accumulated in the butting block where the part was getting butted.','|2.Butting block was made uniform by giving a uniform cut','|1.Instruction given to operator to Change the adhesive tape frequently and clean the area where the parts gets butted before pressing the rivet','Next batch wo number A15814 assembly Completed and found ok,no evidence found for paint getting chipped','','2018-08-01','pe_sez(a)','pe_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','FI','yes','Misc','qas_sez(a)','yes','','|Adhesive tape was appendix on the butting block to avoid metal to metal contact','Z3456','qas_sez|','2019-01-06|','2019-01-06',NULL,NULL,NULL,NULL,NULL,NULL),