(10940,'51A-028','THE BOEING COMPANY','BRACKET ASSY','','149A7371-36','','PSDL REV A',3,'BOEING 001','','A15928','','0000-00-00',NULL,'no','no','no','no','no','no','yes','yes','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 A16046 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,'$','Closed','no','no','no','Assembly','','FI','yes','Misc','qas_sez(a)','yes','','|Adhesive tape was appendix on the butting block to avoid metal to metal contact','Z3456','qas_sez|','2019-01-06|','2019-01-06',NULL,NULL,NULL,NULL,NULL,NULL),(10941,'51A-035','THE BOEING COMPANY','BRACKET ASSY','','149A7371-59','','PSDL REV A',1,'BOEING 001E','','A13213','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','no','PAINT PEALUP(TOP COAT)','1.The Teflon paint chip off surrounding the rivet during pressing the rivet|2.During pressing the rivet metal to metal contact|3.In butting block the  area where the parts were butting while riviting was not uniform |4.FOD of rivet accumulated in the butting block where the part was getting butted.','|2.Butting block was made uniform by giving a uniform cut','|1.Instruction given to operator to Change the adhesive tape frequently and clean the area where the parts gets butted before pressing the rivet','Next batch wo number A13214 assembly Completed and found ok,no evidence found for paint getting chipped','','2018-08-01','pe_sez(a)','pe_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','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),(10942,'51-118','THE BOEING COMPANY','RIBPOST FRONT SPAR RIB 11','AJ18','112T2215-5','NA','PSDL REV -',2,'486998 MPP','','68777','','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. 2. 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. 2. 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. 2. 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 ','1.Next Batch WO #73022,Qty-4nos,74762 Qty-6nos,78477 Qty-3nos   ,78478 Qty-3nos,78479 QTy-2 nos  machined as per the Drawing requirement and MPS/51-118/Rev-01 and found Ok.\r\n2.Delta FAIR Was Submitted To the Customer.FAI NO-F51118002','','2018-08-01','qas_sez(a)','Umesh B,Diwakar R.B.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','DN36746','FI','no','i700-3','qas_sez(a)','no','','|1. Head Engineering raised an Inter Departmental memo (IDM) to call for a Cross Functional Team (CFT) meeting to notify the escapement and to find the cause of the escape Mar 30, 2018 2. This issue was initially identified by CIM Tools on March 26, 2018, immediately all parts in stock and WIP was quarantined. 3. Notification of Escapement (NOE) was communicated to the customer on the escape of parts by Project Engineer on Mar 27, 2018 ','Z3456','cam|qas_sez|','2018-11-22|2018-11-22|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10943,'51A-038','THE BOEING COMPANY','BRACKET ASSY','','149A7371-64','','PSDL REV A',2,'BOEING 001E','','A15930','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','PAINT PEALUP(TOP COAT)','1.The Teflon paint chip off surrounding the rivet during pressing the rivet|2.During pressing the rivet metal to metal contact|3.In butting block the  area where the parts were butting while riveting was not uniform |4.FOD of rivet accumulated in the butting block where the part was getting butted.','|2.Butting block was made uniform by giving a uniform cut','|1.Instruction given to operator to Change the adhesive tape frequently and clean the area where the parts gets butted before pressing the rivet','Next batch wo number A15952 assembly Completed and found ok,no evidence found for paint getting chipped','','2018-08-01','pe_sez(a)','pe_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','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),(10944,'43-037','Composite Industrie','B BRACKET','534435 A','V251 15092 200 00','','A00, ECN PV100298ST1-',1,'LTA PO-1','','76345','','0000-00-00',NULL,'yes','yes','yes','','no','','','','','wall thickness - side','Tool run out|Chips blocked in spindle.|while roughing operation chips was spread on ATC arm and finish tool changing time chips blocked in spindle.|ATC not cleaned after rough tool run.','|1.Clean the ATC & Spindle by tissue paper \r<br/>2.M00 given after rough tool run.','|1.M00 & message given Clean the ATC arm in program.\r<br/>2.Instruction give to operator to clean the ATC arm after any roughing operation by pressured air ','CA PA found ok.','','2018-08-01','Subramanya L(Naik)','        Subramanya L Naik','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','5','','','','','','|checked all part found OK.','E3456','pe|qas|','2018-08-08|2018-08-08|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10945,'51-034','THE BOEING COMPANY','BRACKET','436263','149A7371-954','','PSDL REV A',1,'BOEING 001E','','75199','','0000-00-00',NULL,'no','yes','yes','no','no','no','yes','no','no','MACHINING TIME TOOL WILL BROKERED TOOL DIG MARK ON ON PART ','TO CHECK THE CORRECT METHOD OF FLOWING PROCESS FOR MACHINING TIME BE ALERT |Tool worn out and got broken during the machining time.','|IN RUNNING TIME NUMBER QUANTITY OF PRODUCTIONS TOOL BROKEN CHANCES IS THEIR TO CARE OF TOOL HEIGHT OF PERTIC0LOR PART ARE STAGE\r<br/>Informed the operator to check the life of the tool. ','|TO CHECK THE CORRECT METHOD OF FLOWING PROCESS FOR MACHINING TIME BE ALERT\r<br/>ALL the operators are instructed to monitor the tool life of any new tool used in the machine. ','Next batches of parts found within the drawing/customer requirements.','','2018-08-02','pe_sez(a)','Umesh B,Diwakar R.B.,','','0000-00-00','RAW MATERIAL MISSING','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','1','no','i700-3','pe_sez(a)','no','','|IN RUNNING TIME NUMBER QUANTITY OF PRODUCTIONS TOOL BROKEN CHANCES IS THEIR TO CARE OF TOOL HEIGHT OF PERTIC0LOR PART ARE STAGE\r\nStopped the machine and changed the new tool. ','Z3456','pe|qas_sez|','2018-12-25|2019-01-01|','2019-01-01',NULL,NULL,NULL,NULL,NULL,NULL),(10946,'51-118','THE BOEING COMPANY','RIBPOST FRONT SPAR RIB 11','BB02','112T2215-5','NA','PSDL REV -',1,'486998 MPP','','74762','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','1 quantity from this work order was used for heat treatment test by supplier newton.','The solution treatment process calls for a pull test that needs to be carried out on a sample which is processed with the batch. For which we had no extra/ Spare material.|We had not sent any sample/Spare material with the parts. Additionally we had no raw material available to spare for pull test.|As the requirement was new to CIM we had to ask the treatment house to carry out the pull test of one of the part. Thus a part had to be sacrificed.','|The process was re-validated and checked if this sample size can be cut form the material before taking the parts to rough machining. The details are given to stores to cut the raw material before sending it to machine. The MPS will be up issued before 12-Dec-18.','|1. 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/>2. Training program was conducted Head Engineering for the engineering personnel to concentrate on the importance of capturing all the details from the Part list/Specifications as well as the drawings during the planning process.|A sample along with the parts will be sent from next batch for heat treatment at newton.','Discuss software effectively used for capturing all the applicable requirements.Engineering captures\r\nall the details from the parts list and drawings during the planning process is well in place.\r\nQuality Personnel involve during the FAIR and production stage to review the Customer Specifications\r\nrequirements and document the same.(FAIR Documents with Bubbling details) ','','2018-08-02','qas_sez(a)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','DN41334','POST DN','no','Misc','qas_sez(a)','no','','|The sample size required for pull test was enquired and got the sample size to be 6inch X 2inch X 2inch','Z3456','cam|cam|qas_sez|','2018-11-22|2018-11-22|2018-12-05|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10947,'35-456A','Saab AB','LATCH BRACKET','LL0102097','D522 73484 200 00','','PART ISSUE A',2,'OWED-LTA-002','','72764','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dig mark observed on face.','Part not clamped properly on the part.			\r\n','|Part butting face cross checked with feeler gauge part was machined found ok. 			\r<br/>','|Operator was asked to check the Part butting face by Feeler gauge before machining for each and every Part. At the same the Operator Was asked to do the Visual inspection each and every Part. 						\r<br/>','CAPA FOUND OK','','2018-08-02','pe_sez(a)','pe_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','3','no','Misc','pe_sez(a)','no','','|Production stopped. Part bend cross checked. Completed part cross checked.Found ok. 				\r\n								\r\n','Z3456','pe|qas|','2018-08-12|2018-08-12|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10948,'51A-048','THE BOEING COMPANY','BRACKET ASSY','','149A7371-614','','PSDL REV A',4,'BOEING 001F','','A15798','','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 A15957 assembly Completed and found ok,no evidence found for paint getting chipped','','2018-08-02','pe_sez(a)','pe_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','FI','yes','Misc','qas_sez(a)','no','','|Adhesive tape was appendix on the butting block to avoid metal to metal contact','Z3456','qas_sez|','2019-01-06|','2019-01-06',NULL,NULL,NULL,NULL,NULL,NULL),(10949,'44-009','Saab AB','FRAME INT 4 ','523485','E5347562920001','','A',1,'AAI-DP-LTA-15SS','','78695','','0000-00-00',NULL,'yes','no','yes','','','','','yes','','part wrong loading ','1.Profile dig mark.\r\n|2.Wrong loading of the part.|3.Both location pins are in the same dia, so the part can be loaded in reverse way.|4.Profile was not noticed by the operator.','|1.Location pin has been changed.\r<br/>2.Fixture modification will be done for the next batch of this CRN to be manufactured.','|1.For next batch of this CRN the fixture will be changed.\r<br/>2.Guidance has been given to the operator to see the profile properly and locate it.\r<br/>3.separate fixture are been made for this CRN. ','CA PA found ok.','','2018-08-03','Dhananjaya(N)','        dharshan d','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','5','','','','','','|1.Checked the previous machined parts and found all \"ok\".','E3456','pe|pe|Deshpande|qas|','2018-08-03|2018-08-08|2018-08-08|2018-08-08|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10950,'46-038B','Mahindra Aerostructures Pvt.Ltd','STRAP ','24987','D575-40872-201-01','NA','K02, BOM ISS J, ECN NG26090ST1KD02',1,'3101173229 AMD 1','','78767','','0000-00-00',NULL,'no','yes','yes','no','no','no','yes','no','no','Dig mark found on part.','Part hit on other part while debarring and handling. ','|All material handling trays provided with partitions.','|Need to provide adequate handling trays to suit component size.','Next batches found ok.','','2018-08-03','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','1','no','Misc','Dhananjaya(N)','no','','|All the parts are visually re-inspected and the parts affected are reworked.','E3456','pe|qas|','2018-10-25|2018-10-27|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10951,'35-525A','Saab AB','ROD BODY','M973530','D5227333620000','NA','PART ISSUE B',3,'OWED-LTA-005','','75438','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','In Roughing Operation OD Get undersized.','Part machining time insert was loose.|CHIPS BLOCKED DURING OD TURNING.\r\n','|1) Removed the tool holder and changed the screw of the SIM and tightened the SIM and retaken the offset and continued the production.\r<br/>\r<br/> Informed the operators to ensure the SIM tightness and all required parameters during the setting operation and specially when borrowing tool from another machine. ','|1) Spare tool will be issued to the machine to avoid the movement of tools from machine to machine.\r<br/>\r<br/>Informed to operator to ensure the SIM tightness once in every 5 Parts.','CAPA found ok','','2018-08-03','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','Production','no','Misc','Manu(P)','no','','||Immediately stopped the machine and checked all the previously completed parts.','E3456','pe|qas|','2018-12-18|2018-12-18|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10952,'51-001','THE BOEING COMPANY','Upper Beam FWD Splice','387004','315Z1301-501','','NIL',1,'BOEING 001K','','77506','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','wall dig mark','Due to tool broken wall got dig marked.|Due to tool wear tool got broken and broke.|New tool was used for continual improvement purpose during which the tool got broken as the tool life was not aware.','|Informed the tool grib personnel to clearly address the tool life of new tools when purchased. ','|Care will be taken during the trial of new tools. ','CA/PA accepted','','2018-08-04','pe_sez(a)','Tejas ,Shivaraj K S,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','3','no','Slim3n-4AHS-3','pe_sez(a)','no','','|Immediately stopped the machine and continued the production with the previously used tool. ','Z3456','pe|qas_sez|','2019-01-17|2019-01-18|','2019-01-18',NULL,NULL,NULL,NULL,NULL,NULL),(10953,'47-152','GKN Aerospace Filton','LWR ANGLE ATTACHMENT','560504A3','F57254364204','NA','PART ISSUE C',1,'1210042824-2','','79058','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Fillet radius and base dig up to 0.8mm.','Wrong tool offset entry in machine.|wrong tool offset register maintain ','Correct the tool offset.','Maintain the tool offset register properly and guide the operator about the tool offset register.','CAPA FOUND OK','','2018-08-04','prodn_aero(prodn)','Dinesh kulal()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Dinesh kulal()','no','','Initially tool offset valve entered in register.','A3456','qas_aero|','2018-09-06|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10954,'18-209B','Magellan Aerospace Wrexham','BODY','17494382-A','D321 40204 202','','D, ECN NR29999ST1KM15, NR29999ST2KF65, WQN DFB09775',2,'RP166210','','74444','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','ID DIA GET OVER SIZE 0.3MM ','While reworking the part it get rejected.|ID under size found.|because of Insert wear out while running time.|Improper Coolant supply|Chip disturbed the coolant pipe direction.','|Coolant pipe Aline with the wright direction and then run the machine. ','|MO1 updated in program, because of coolant pipe cross check at the finishing pass.','capa found ok','','2018-08-06','Krishna(Chowdary.G.P.)','Raghavendra P,Narasimhamurthy C,KRISHNAMURTHY N,dharshan d,','','0000-00-00','NC CREATION','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','DX200-4','Manjunatha(P)','no','','|Immediately cross check with the available part in machining.(2nd operation completed parts)','E3456','pe|qas|','2018-12-18|2018-12-18|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10955,'35-672','Saab AB','SHAFT LEVER ','468065 B','D5227346221900','NA','PART ISSUE D',1,'OWED-LTA-001','','74253','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','process problem.','This part contains many critical features.|There was 2 process for same part due to many critical features.|One process failed.|Process failed due to Critical dimension not achieved.|Another process succeeded.','Plan B process achieved Critical dimensions, So Plan A process was done Obsolete','Continued Plan B process for Fair as well as for Production parts.','EFFECTIVENESS FOUND OK. ','','2018-08-06','Ramesh(Poojary)','Ramesh(Poojary)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','05','no','Misc','Gurukiran S(M)','no','','Plan A process was replaced by Plan B process.','E3456','qas|','2018-12-12|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10956,'35-526','Saab AB','ROD BODY','515370A','D522 73337 200 00','','A',12,'OWED-LTA-004','','70173','','0000-00-00',NULL,'no','yes','no','yes','no','yes','no','no','no','We used alternative material but customer did not accept. ','The alternate material specified in the drawing was not accepted by the end customer. Therefore the parts are rejected.','|Customer specified another alternate which is approved by the end customer.','|Machining to be continued used the new alternate.','Alternate material specified initially by the customer is changed.','','2018-08-06','Rakeshbabu(V)','Rakeshbabu(V)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','10','no','Misc','Yashawantha(NH)','no','','|Query raised to the customer on the material to be used.','E3456','qas|qas|','2018-08-07|2018-08-07|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10957,'35-526','Saab AB','ROD BODY','515370A','D522 73337 200 00','','A',42,'OWED-LTA-004','','70177','','0000-00-00',NULL,'no','yes','no','yes','no','yes','no','no','no','We used alternative material but customer did not accept.','The alternate material specified in the drawing was not accepted by the end customer. Therefore the parts are rejected.','|Customer specified another alternate which is approved by the end customer.','|Machining to be continued used the new alternate.','Alternate material specified initially by the customer is changed.','','2018-08-06','Rakeshbabu(V)','Rakeshbabu(V)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','10','no','Misc','Yashawantha(NH)','no','','|Query raised to the customer on the material to be used.','E3456','qas|qas|','2018-08-07|2018-08-07|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10958,'35-663','Saab AB','BRACKET','515371C','D5227342920400','NA','PART ISSUE D',45,'OWED-LTA-002','','71585','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Due to Design change.','Change in customer supplied design.','|Informed engineering team to revise the process according to the new design.','|Fair to be submitted for the new design.','Part design Changed by the Customer due to failure in previous design.','','2018-08-06','Rakeshbabu(V)','Rakeshbabu(V)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','06','no','Misc','Yashawantha(NH)','no','','|Requested customer to provide the new revised design.','E3456','qas|qas|','2018-08-07|2018-08-07|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10959,'35-473A','Saab AB','LEVER CAM','C86484','D522 73537 200 00','','PART ISSUE A',42,'OWED-LTA-003','','73853','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Profile point out,','Profile point no measured according to the drawing requirement.|The profile point shifted from the center bore while machining and the dimension was not ensured.|Butting land between the part and the fixture was very less due to which part did not got fixed rigidly and got shifted during the machining and left unnoticed.|Vibration during machining was not taken to account during the fixture manufacturing and the Dimension to be measured was also not captured in the MPS.','|Immediately scrapped the old fixture and informed the engineering team to revise the process and change the fixture.','|1) MPS to be amended for the revised process and FAIR Document to be made to re-ensure the fit and function of the part after the change in process.\r<br/>2) Informed all the production supervisors to check the fixtures which are manufactured in similar method.','Old fixture is not scrapped but the fixture is redesigning is initiated.','','2018-08-06','Dhananjaya(N)','Dhananjaya(N)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','9','no','Misc','Dhananjaya(N)','no','','|Immediately checked all the completed parts and informed the engineering team and called the CFT team for discussion.','E3456','qas|qas|','2018-08-08|2018-08-08|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10960,'44-012','Saab AB','FRAME INT 5 ','5736201 2','E5347563020102','','A',1,'1600190066','','70729','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Hole pitch problem.','Drawing was the master for the part, Which was released by the Customer|Part was machined as per the drawing supplied by the customer|After the part was manufactured, COS was released by the Customer|When Compared to COS the hole pitch was varying','|Part was manufactured as per the COS by the customer.','|Will confirm for all the documents released by the customer before only, And will start to machine the part.','CAPA FOUND OK','','2018-08-06','Ramesh(Poojary)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','7','no','Misc','Narayanappa(G)','no','','|Part was rejected and Again new part was manufactured as per the COS','E3456','cam|qas|','2018-08-07|2018-08-07|',NULL,NULL,NULL,NULL,NULL,NULL,NULL);
INSERT INTO `nc4qa` VALUES (10961,'51A-083A','THE BOEING COMPANY','BRACKET ASSY','','332A2930-7','','PSDL REV B',5,'BOEING 001U','','A16151','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','HOLE DIAMETER OVERSIZE ','REFER NC NO:10806.','|REFER NC NO:10806.','|REFER NC NO:10806.','REFER NC NO:10806.','','2018-08-07','qas_sez(a)','qas_sez(a)','','0000-00-00','HOLE DIAMETER OVERSIZE ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Assembly','','FI','no','Misc','qas_sez(a)','no','','|REFER NC NO:10806.','Z3456','qas_sez|','2019-01-16|','2019-01-16',NULL,NULL,NULL,NULL,NULL,NULL),(10962,'51A-083A','THE BOEING COMPANY','BRACKET ASSY','','332A2930-7','','PSDL REV B',5,'BOEING 001U','','A16412','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','HOLE DIAMETER OVERSIZE(NO GO ENTERING) ','REFER NC NO:10806.','|REFER NC NO:10806.','|REFER NC NO:10806.','REFER NC NO:10806.','','2018-08-07','qas_sez(a)','qas_sez(a)','','0000-00-00','HOLE DIAMETER OVERSIZE','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Assembly','','FI','no','Misc','qas_sez(a)','no','','|REFER NC NO:10806.','Z3456','qas_sez|','2019-01-16|','2019-01-16',NULL,NULL,NULL,NULL,NULL,NULL),(10963,'51A-083A','THE BOEING COMPANY','BRACKET ASSY','','332A2930-7','','PSDL REV B',5,'BOEING 001U','','A16505','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','HOLE DIAMETER OVERSIZE(NO GO ENTERING)','REFER NC NO:10806.','|REFER NC NO:10806.','|REFER NC NO:10806.','REFER NC NO:10806.','','2018-08-07','qas_sez(a)','qas_sez(a)','','0000-00-00','HOLE DIAMETER OVERSIZE(NO GO ENTERING)','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Assembly','','FI','no','Misc','qas_sez(a)','no','','|REFER NC NO:10806.','Z3456','qas_sez|','2019-01-16|','2019-01-16',NULL,NULL,NULL,NULL,NULL,NULL),(10964,'51A-083A','THE BOEING COMPANY','BRACKET ASSY','','332A2930-7','','PSDL REV B',5,'BOEING 001U','','A16150','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','HOLE DIAMETER OVERSIZE(NO GO ENTERING)','REFER NC NO:10806.','|REFER NC NO:10806.','|REFER NC NO:10806.','REFER NC NO:10806.','','2018-08-07','qas_sez(a)','qas_sez(a)','','0000-00-00','HOLE DIAMETER OVERSIZE(NO GO ENTERING)','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Assembly','','FI','no','Misc','qas_sez(a)','no','','|REFER NC NO:10806.','Z3456','qas_sez|','2019-01-16|','2019-01-16',NULL,NULL,NULL,NULL,NULL,NULL),(10965,'47-141','GKN Aerospace Filton','STIFFENER 5 TOP SKIN','1010901 2','D57250496202','NA','PART ISSUE N',1,'1210042824-1','','79527','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','THICKNESS 1.5 +0.13/-0.08 MEASURING 1.30 AT ONE END','Due to improper butting of part in fixture.|Fixture was in stock|Fixture validation was not done','|New fixture was manufactured','|Upcoming fixtures will be validated through QAD and will be taken for part prove out','CAPA found ok.','','2018-08-07','Ramesh(Poojary)','Ramesh(Poojary)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','Misc','Nandishkumar(D.K.)','no','','|Fixture was validated and built new fixture','E3456','cam|qas|','2018-08-22|2018-09-05|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10966,'47-144','GKN Aerospace Filton','STIFFENER 6 TOP SKIN','1011901 2','D57250497203','NA','PART ISSUE H',1,'1210042824-1','','79529','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','THICKNESS 1.5 +0.13/-0.08 MEASURING 1.32 AT ONE END','Due to improper butting of part in the fixture\r\n\r\n|Fixture was in stock|Fixture validation was not done','|Changed the fixture','|Upcoming fixtures will be validated through QAD & will be taken for part prove out','CA/PA CLOSED','','2018-08-07','Ramesh(Poojary)','Ramesh(Poojary)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','Misc','Nandishkumar(D.K.)','no','','|fixture was validated & built new fixture','E3456','cam|qas|','2018-11-12|2018-12-04|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10967,'35-526','Saab AB','ROD BODY','515370A','D522 73337 200 00','','A',10,'OWED-LTA-004','','70172','','0000-00-00',NULL,'no','yes','no','yes','no','yes','no','no','no','We used alternative material but customer did not accept. ','The alternate material specified in the drawing was not accepted by the end customer. Therefore the parts are rejected.','|Customer specified another alternate which is approved by the end customer.','|Machining to be continued used the new alternate.','Alternate material specified initially by the customer is changed.','','2018-08-07','Rakeshbabu(V)','Rakeshbabu(V)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','10','no','Misc','Yashawantha(NH)','no','','|Query raised to the customer on the material to be used.','E3456','qas|qas|','2018-08-07|2018-08-07|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10968,'35-526','Saab AB','ROD BODY','515370A','D522 73337 200 00','','A',40,'OWED-LTA-004','','70175','','0000-00-00',NULL,'no','yes','no','yes','no','yes','no','no','no','We used alternative material but customer did not accept. ','The alternate material specified in the drawing was not accepted by the end customer. Therefore the parts are rejected.','|Customer specified another alternate which is approved by the end customer.','|Machining to be continued used the new alternate.','Alternate material specified initially by the customer is changed.','','2018-08-07','Rakeshbabu(V)','Rakeshbabu(V)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','10','no','Misc','Yashawantha(NH)','no','','|Query raised to the customer on the material to be used.','E3456','qas|','2018-08-07|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10969,'35-526','Saab AB','ROD BODY','515370A','D522 73337 200 00','','A',40,'OWED-LTA-004','','70174','','0000-00-00',NULL,'no','yes','no','yes','no','yes','no','no','no','We used alternative material but customer did not accept. ','The alternate material specified in the drawing was not accepted by the end customer. Therefore the parts are rejected.','|Customer specified another alternate which is approved by the end customer.','|Machining to be continued used the new alternate.','Alternate material specified initially by the customer is changed.','','2018-08-07','Rakeshbabu(V)','Rakeshbabu(V)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','10','no','Misc','Yashawantha(NH)','no','','|Query raised to the customer on the material to be used.','E3456','qas|qas|','2018-08-07|2018-08-07|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10970,'35-526','Saab AB','ROD BODY','515370A','D522 73337 200 00','','A',40,'OWED-LTA-004','','70176','','0000-00-00',NULL,'no','yes','no','yes','no','yes','no','no','no','We used alternative material but customer did not accept. ','The alternate material specified in the drawing was not accepted by the end customer. Therefore the parts are rejected.','|Customer specified another alternate which is approved by the end customer.','|Machining to be continued used the new alternate.','Alternate material specified initially by the customer is changed.','','2018-08-07','Rakeshbabu(V)','Rakeshbabu(V)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','10','no','Misc','Yashawantha(NH)','no','','|Query raised to the customer on the material to be used.','E3456','qas|qas|','2018-08-07|2018-08-07|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10971,'35-531A','Saab AB','SHAFT LATCH','C90596','D5227349020200','NA','PART ISSUE C',13,'OWED-LTA-002','','73921','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','OD UNDER SIZE. ','OD Undersized -0.015mm beyond drawing limit.|OD undersized during the re-pass operation as the re-pass ran twice.|Re-pass ran twice with same -0.15 wear offset as the operator provided +0.2mm wear offset during the insert change.|To maintain stock in the ID after the insert change the operator provided -0.2mm in the initial stage and after measuring the diameter he provided -0.15mm to remove the stock and finish to the drawing requirement during this time the re-pass operation was carried out and resulted in diameter was undersized.|Operator was unaware that the program for OD runs twice with different stock levels to achieve finish in the final operation.\r\nContainment Action:','|Changed the wear offset from +0.2mm to +0.1mm in the next part and after the completion changed the offset to -0.02mm according to the program(after considering both the pass) and found the next part OK. ','|Informed all the operator to check the relevant features after the insert change and provide of the offset accordingly with proper guidance from the supervisor or senior operators ','Next batch shipments monitored and found ok. ','','2018-08-07','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','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),(10972,'35-663','Saab AB','BRACKET','515371C','D5227342920400','NA','PART ISSUE D',30,'OWED-LTA-002','','71584','','0000-00-00',NULL,'no','no','no','no','no','yes','yes','yes','no','Due to Design change.\r\n','Change in customer supplied design.','|Informed engineering team to revise the process according to the new design.','|Fair to be submitted for the new design.','Part design Changed by the Customer due to failure in previous design.','','2018-08-07','Rakeshbabu(V)','Rakeshbabu(V)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','04','no','Misc','Yashawantha(NH)','no','','|Requested customer to provide the new revised design.','E3456','qas|','2018-08-07|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10973,'35-408A','Saab AB','FRAME MID','701946 1D1','D522 73397 200 00','','PART ISSUE B',2,'OWED-LTA-001','','71190','','0000-00-00',NULL,'no','no','no','no','no','yes','yes','yes','no','Etching  operation part reject from ATPL. ','Blind holes occurred on part|After etching operation part was not cleaned properly on behind thread.|Due to that chemical reaction occurred and material was removed','After etching process parts are to be ensure free of chemical by visually if it is there that to be clean ','As per the process sheet that visual inspection to be carried out','CAPA FOUND OK','','2018-08-07','qas_sez(a)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','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.','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10974,'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. ','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','','2018-08-07','qas_sez(a)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','DN38089','Post DN','no','Misc','qas_sez(a)','no','','The parts which are all in process that was ensured free from the chemical after etching process.','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10975,'53A-002','Triumph Aerostructures','FORK FITTING ASSY','','F57953444002A02','','PART ISSUE A',1,'LTA Triumph ASSY 201','','A17193','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Bore oversized.','REFER NC NO:10806.','|REFER NC NO:10806.','|REFER NC NO:10806.','REFER NC NO:10806.','','2018-08-07','pe_sez(a)','Rangaswamy()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Assembly','','FI','no','Misc','Manu()','no','','|REFER NC NO:10806.','Z3456','qas_sez|','2019-01-16|','2019-01-16',NULL,NULL,NULL,NULL,NULL,NULL),(10976,'51-145','THE BOEING COMPANY','CLEVIS - UPPER, RH THREAD','SN10171','112A7112-612','NA','PSDL REV B',1,'BOEING 001W','','78774','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','wall thickness under size by 0.1','Face mill insert indexing wrongly.|insert life is gone due to high thick material . |Now also change the new cutters and inserts |New developing cutter will try it and solve the problem |.','Development stage we will change the cutters depending on supplier .','depth of cut and tool insert life monitoring the operator ,|depth of cut and tool insert life will be  monitored by the operator till suitable cutters are used for this material(Titanium).','Effectiveness Found ok.','','2018-08-07','pe_sez(a)','pe_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','5','no','Misc','pe_sez(a)','no','','in this material tool life is not secured due to insert contact life is too shot . ','Z3456','qas|','2018-09-04|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10977,'18-418A','Magellan Aerospace(Blackpool) Limited','BRACKET','C0201787644/33745977','PI55-2119010-00','','NIL',1,'BPP-533302','','79199','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','pin no go enter.(hole over size)','dummy nc','|dummy nc','|dummy nc','dummy nc','','2018-08-08','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','03','no','Misc','Prashanth Kumar(M)','no','','|dummy nc','E3456','pe|ranjith|','2018-10-25|2018-11-15|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10978,'28-041','Magellan Aerospace New York  Inc.','LEVER ASSY-SECONDARY SPOI','158334','65-46358-16','','PL_E, DL_N/C, Sketch # 1',1,'A000148833','','73992','','0000-00-00',NULL,'yes','yes','yes','','','','','','','ID OVER SIZE.','ID OVER SIZE DURING THE FIRST OFF PART PROVING TIME.|WHILE PROVIDING THE WEAR OFFSET IN THE X-AXIS OPERATOR DID NOT CALCULATE THE PROPER OFFSET VALUE.|THREE POINT MICROMETER WAS USED BY THE OPERATOR TO MEASURE THE ID DUE TO WHICH OPERATOR DID WRONG CALCULATION.|OPERATOR WAS NEW TO THREE POINT MICROMETER AND HE WAS NOT TRAINED SUFFICIENT TO USE THE THREE POINT MICROMETER.','|CHANGED THE VALUE GIVEN IN OFFSET.                     CHECKED THE PART IN AIR GAUGE AND GAVE THE VALUE IN THE OFFSET.                               ','|INSTRUCTED ALL OPERATORS TO TAKE SUPPORT FROM SUPERVISOR OR SENIOR OPERATORS WHILE HANDLING WITH NEW INSTRUMENTS.     SUFFICIENT TRAINING TO BE PROVIDED TO ALL THE OPERATORS ON RANDING AND MEASURING USING THE NEW INSTRUMENT.    ','Proper training to be given to the operator about the three point micrometer. CAPA found ok.','','2018-08-09','Ravi(M)','        Ningaraj A N','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','13','','','','','','|IMMEDIATELY STOPPED THE MACHINE AND WITH THE HELP AT SUPERVISOR THE WEAR OFFSET PARAMETER WERE CORRECTED AND NEXT PART FOUND OK.','E3456','pe|pe|qas|','2018-08-09|2018-08-18|2018-09-04|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10979,'35-442B','Saab AB','HINGE','C90880','D5227338720200','NA','B',1,'OWED-LTA-002','','76299','','0000-00-00',NULL,'no','no','yes','yes','no','no','no','yes','no','Material Crack observed during machining.','During the stage 01 the material braked at one end.|Due to the cross cutting of the material the edge got broken.','|Informed all the operators to visually inspect the material from all sides before loading to the machine.','|Informed the stores personnel to strengthen the visual inspection in the receiving inspection area.','CAPA found ok.','','2018-08-09','Nagaraja (G)','Sunil Kumar(K.R.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','01','no','Misc','Anjinamurthy(H)','no','','|Immediately stopped the machine and checked all the material and returned the similar cross cutted material to the stores.','E3456','qas|','2018-09-05|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10980,'18-209B','Magellan Aerospace Wrexham','BODY','17494382-A','D321 40204 202','','D, ECN NR29999ST1KM15, NR29999ST2KF65, WQN DFB09775',3,'RP166210','','74444','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','bore oversize to required dimension.','Error dimension maintain in the air gauge. \r\n|Improper air gauge setting.\r\n|He don\'t have a proper knowledge about air gauge.\r\n|He don\'t get the proper training about the air gauge. \r\n|Air gauge setting method was wrong.\r\n','|Training given to the operator about setting the air gauge and 10 times set the air gauge in front of the supervisor.\r<br/>','|If air gauge requirement of any CRN set the air gauge  in front of the supervisor.\r<br/>','CA/PA Found OK.','','2018-08-09','Dinakar K()','Dinakar(K)','','0000-00-00','REJECTED','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','01','no','Misc','Dinakar(K)','no','','|segregated the problem parts and NC raised for the problem parts. \r\n','E3456','pe|qas|','2018-09-19|2018-09-21|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10981,'51A-079','THE BOEING COMPANY','ASSY - FTG, AFT FAIRING F','','112U7625-16','','PSDL REV-',1,'BOEING 001V','','K17407','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Dummy NC.','','','','','','2018-08-10','pe_sez(a)','pe_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','Assembly','','FI','no','Misc','qas_sez(a)','no','','','Z3456','qas_sez|','2018-08-28|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10982,'18-091A','Magellan Aerospace(Polska) Sp','BUSH','437671','PID278 50164 202','','A',4,'104569','','78327','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','OD under size.','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.','Effectiveness Found ok.','','2018-08-10','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','01','no','Misc','Ravi(M)','no','','|Immediately stopped the machine and changed the wear offset and continued the production on the next part.','E3456','pe|qas|','2018-09-04|2018-09-05|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10983,'35-228A','Saab AB','HINGE BRACKET 2 ','4755501 1','D576 50005 205','','D00',1,'1600223433/Forecast ','','76791','','0000-00-00',NULL,'no','yes','yes','no','no','no','yes','no','no','Part loaded in reverse direction','Did not observe the part front side|Part butting on wrong side|Not checked the part before running the program|Did not notice the fixture also|.','|observed all the dimensions and part .before loading','|Informed all the operators about this problem and gave the message inside the programe(check the part front side and run) ','CAPA FOUND OK','','2018-08-11','Dinesh kulal()','prodn_aero(prodn)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','01','no','Misc','Dinesh kulal()','no','','|Part butting on wrong side','A3456','prodn_aero|qas_aero|','2018-09-05|2018-09-06|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10984,'18-779A','Magellan Aerospace Wrexham','BRACKET AFT M/C','1578760-2/QL3D','F57551860201','NA','PART ISSUE A',1,'RP171304','','74372','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Bore over size ','while part proving time bore over size by 0.04|previous part bore not finish so change the insert and different supplier insert so |customer recommended parameter not accurate on this type of operation   |This high RPM S1200 Is grater than vc so bore over size |Why1-In first part surface Finish inside Bore was not acheived. \r\nWhy2-Bore finish done with RPM of 1200.\r\nWhy3-Insert changed for the next part which resulted in Bore oversize.\r\n','while these type of part proving time to increase the bore stock and finish next shot, |1.Instead of Interpolation Boring Bar used with respective tool parameters','these type of parts proving time we select the particular insert ,boring bar and holder,rpm feed will be fix ,  ','Effectiveness found ok.','','2018-08-11','Gurukiran S(M)','Gurukiran S(M)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','5','no','Misc','Gurukiran S(M)','no','','change the recommended rpm and feed |RPM and feed changed according to Tool Manufacturers guide.','E3456','qas|','2018-08-30|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10985,'35-585A','Saab AB','HANDLE','518610C','D5227342720200','NA','PART ISSUE D',2,'OWED-LTA-005','','78305','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Part hole over size by 20micron.','1.while boring bar correction wrong given by operator|2.while bore proving time operator correction done by 0.02 instead of 0.002micron |3,','|proper training given to operators .','|Training conducted to all operators,once again cross check the trainee.effectiveness found ok. ','ca pa found ok ','','2018-08-11','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Prashanth Kumar(M)','no','','|immediately stop the machine and check the all parts ,all parts found ok.','E3456','pe|qas|','2018-12-18|2018-12-18|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10986,'18-664A','Magellan Aerospace Bournemouth','GAMMA FITTINGS','99867','NSA840020-150','','L',2,'428939','','77231','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','2 NOS PARTS FOUND DEEP LINE IN INTERNAL GROVE AND OD DAMETER','1)Chip was observed on tool.\r\n2)Due to this deep line created in the OD surface.\r\n','|1)M0 optional stop was provided in the program for the operation OD due to this operator can visually inspect and ensure no chip was stuck in the tool and parallel operator clean the tool and inserts to ensure no chip observed.','|1)M0 optional stop was provided in the program for the operation OD due to this operator can visually inspect and ensure no chip was stuck in the tool and parallel operator clean the tool and inserts to ensure no chip observed.','CA/PA found satisfied.','','2018-08-11','pe_sez(a)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','DN42536','FI','no','Misc','qas_sez(a)','no','','|1)Machine was stopped immediately and informed to the supervisor.\r\n2)Visually inspected the produced quantities.\r\n','Z3456','qas_sez|','2019-01-18|','2019-01-18',NULL,NULL,NULL,NULL,NULL,NULL),(10987,'18-664A','Magellan Aerospace Bournemouth','GAMMA FITTINGS','99867','NSA840020-150','','L',2,'428939','','77232','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','2 NOS FOUND DEEP LINE ON OD','Refer NC NO:10986','|Refer NC NO:10986','|Refer NC NO:10986','Refer NC NO:10986','','2018-08-11','pe_sez(a)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','DN42537','POST TREATMENT','no','Misc','qas_sez(a)','no','','|Refer NC NO:10986','Z3456','qas_sez|','2019-01-18|','2019-01-18',NULL,NULL,NULL,NULL,NULL,NULL),(10988,'56A-019','GKN Aerospace Orangeburg','SUPPORT ANGLE ASSY,  UPR','','119A1440-605','','PSDL REV B',1,'LTA Orangeburg 737 W','','A17500','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','CSK(CHAFER) OVERSIZE','1) CSK oversize because of increased depth.|2) Depth was controlled by manual load application as the CSK formation was carried out by hand manually.','|All the CSK were checked using a similar rivet and depth was increased gradually until the required Diameter was achieved.','|Purchased drill machine for which the standard CSK tool will be installed and height will be fixed from the result of first hole formation.','CAPA found ok','','2018-08-11','pe_sez(a)','pe_sez(a)','','0000-00-00','CSK(CHAFER) OVERSIZE','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Assembly','','FINAL INSPECTION','no','Misc','qas_sez(a)','no','','|Immediately stopped the assembly process and informed to the supervisor and checked all the completed parts and found ok.','Z3456','qas|','2019-02-21|','2019-02-21',NULL,NULL,NULL,NULL,NULL,NULL),(10990,'18-377B','Magellan Aerospace Bournemouth','GAMMA FITTINGS','4125','NSA840020-200PF','','L',5,'423232','','74796','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','dent found on OD and edges','1.Transits Damage|2.Improper handling of Parts at supplier end|3.Thin Polythene cover used for packing','|The same was communicated to the supplier on the visual defect','|Informed to supplier on material handling and change the packing method so as to avoid transits damages.','Next batch inspected and found visually ok ,no dent was evidenced','','2018-08-11','pe_sez(a)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','DN43220','POST TREATMENT','no','Misc','qas_sez(a)','no','','|1.100% parts were inspected and separated the parts which has a visual defect.\r\n2.NC was raised and sent to supplier','Z3456','qas_sez|','2019-01-06|','2019-01-06',NULL,NULL,NULL,NULL,NULL,NULL),(10991,'18-377B','Magellan Aerospace Bournemouth','GAMMA FITTINGS','M940330/20715','NSA840020-200PF','','L',1,'423232','','74802','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','DENT ON OD','1.Transits Damage|2.Improper handling of Parts at supplier end|3.Thin Polythene cover used for packing','|The same was communicated to the supplier on the visual defect','|Informed to supplier on material handling and change the packing method so as to avoid transits damages.','Next batch inspected and found visually ok ,no dent was evidenced','','2018-08-11','pe_sez(a)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','DN43221','POST TREATMENT','no','Misc','qas_sez(a)','no','','|1.100% parts were inspected and separated the parts which has a visual defect.\r\n2.NC was raised and sent to supplier','Z3456','qas_sez|','2019-01-06|','2019-01-06',NULL,NULL,NULL,NULL,NULL,NULL),(10992,'18-376B','Magellan Aerospace Bournemouth','GAMMA FITTINGS','99867','NSA840020-150PF','','L',2,'423228','','74743','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Parts received from treatment were found dent on OD','This is happen during the transportation as there was no safety in the inner layer of the box in which the parts were shipped','|The same was flow down to the Supplier on the packing Conditions','|Instruction was given to the treatment house on packaging to put extra kushan type of material surrounding the inner layer of the box to avoid such paint damages during the transportation','Next Lot Received from the treatment supplier ,parts were checked and found visually acceptable to the requirement','','2018-08-11','pe_sez(a)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','DN43148','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|','2018-11-27|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10993,'35-618','Saab AB','SHAFT HANDLE ','M789340','D5227348520200','','PART ISSUE C',1,'PA1687 LTA-1','','78355','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','while doing full length turning operation 445.50mm. we got outer diameter chattering.\r\nouter diameter required 22.05 to 22.1mm. measured by 22.03mm. under size\r\nby 0.020mm. ','while doing full length turning operation 445.50mm. we got outer diameter chattering. |before that we used to finish in two setup (half length).|we are going to prove in new machine. ','|1) we took new CCGT TOOL FOR FINISHING OPERATION.\r<br/>2) We are adjusted RPM and feed. ','|we are going to use same tools,rpm and feed from next batch on wards. |2) Informed the Engineering team about the change in process and Engineering team will amend the MPS to the revised Process.','CA PA found ok.','','2018-08-13','Dinakar K()','Dinakar K()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','01','no','Misc','Dinakar K()','no','','','Z3456','pe_sez|qas|','2018-09-06|2018-09-07|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10994,'35-415','Saab AB','SHAFT LATCH LINK','M789340','D522 73496 200 00','','A',1,'OWED-LTA-004','','79212','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','while doing full length turning operation 506.0mm. we got outer diameter chattering.                                          outer diameter required 22.05 to 22.1mm.\r\nmeasured by 21.8mm.\r\nunder size by 0.25mm.                                                        ','while doing full length turning operation 506.0mm. we got outer diameter chattering. |before that we used to finish in two setup (half length).|we are going to prove in new machine. ','|1) we took new CCGT TOOL FOR FINISHING OPERATION. \r<br/>2) We are adjusted RPM and feed.','|we are going to use same tools,rpm and feed from next batch on wards.                 |2) Informed Engineering team about the change in process and the MPS will be amended to the new revised process.','CA PA found ok.','','2018-08-13','Dinakar K()','Dinakar K()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','01','no','Misc','Dinakar K()','no','','','Z3456','pe_sez|qas|','2018-09-06|2018-09-07|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10995,'56-038','GKN Aerospace Orangeburg','CLOSEOUT - RIB, ANTICOLLI','374021','119A1442-604','NA','PSDL REV -',1,'LTA Orangeburg 737 W','','79029','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','UNWANTED MACHINING DUE TO PROGRAM ERROR','There was an error in post process file|because, upgraded from older version to new version|advance features were available in new version','|post had been changed and new post process received from software end and validated the post process before the post program','|post has been validated on duplicate part','NEXT PART FOUND OKAY','','2018-08-13','pe_sez(a)','Umesh B,Diwakar R.B.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','1','no','i700-5','pe_sez(a)','no','','|stopped the production and informed to software supplier','Z3456','cam|qas_sez|qas_sez|','2019-02-06|2019-02-07|2019-02-07|','2019-02-07',NULL,NULL,NULL,NULL,NULL,NULL),(10996,'35-622','Saab AB','FLAP, VENT','2270601','D5227280420000','NA','PART ISSUE A',1,'OWED-LTA-003','','78651','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Tool dig mark on the part.','Operator not holding required length.|Operator not read the tool overhang in program.|More training required. |The cutting tool over hang length was not mentioned in the programm,tool dig mark on the part due to short length of the tool hence dig mark of the tool holder.','|OVERHANG LENGTH = 70.0mm holding then run the part|In future the required cutting tool length will be mentioned in the programm and same will be crosschecked by the supervisor.','|Training the operator if any part setting before read the process sheet or input take in your seiner operator.','','','2018-08-13','Rangaswamy()','        Thaveni D M ','','0000-00-00','TOOL OVERHANG (TOOL LENTH ) PROBLEM.....','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','01','','','','','','|Inform to supervisor.|The machine was stopped after the dig mark found on the part.\r\nThe program was cross checked in the machine.\r\nThe previous parts produced were inspected and found ok.','Z3456','pe_sez|pe_sez|pe_sez|qas_sez|','2018-09-06|2018-09-25|2018-12-17|2018-12-17|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10997,'47-192','GKN Aerospace Filton','POST OTBD STRAKE M/C','628653','F57555057201','NA','PART ISSUE A',2,'1210042824-2','','79538','','0000-00-00',NULL,'yes','no','no','no','yes','yes','no','no','no','WEB THICKNESS IS 2.2 +0.13 / -0.08 MM.\r\nMEASURED WEB THICKNESS IS 2.04 / 2.10 MM.\r\nUNDER SIZE BY 0.02 TO 0.08 MM.','Gap observed between component and fixture surface after clamping.|Component butting was not correct.\r\n|Taper observed on fixture top surface(Component butting area)','|Fixture reworked to correct the taper.','|All fixtures will be inspected before loading on machine and on machine before running the part.','Next batches found ok.','','2018-08-14','CAD(sez)','CAD(sez)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','01','no','Misc','qas_sez(a)','no','','|Stopped production and inspected component, program and fixture.','Z3456','cam|qas|','2018-11-27|2018-12-10|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10998,'18-384B','Magellan Aerospace Wrexham','NUT RING OUTER','1579010-1/QA3B','D575 40038 200','','A',20,'162892','','77085','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Dia. 1.3 pin go not answering.','why1-Hole deburr not done properly which resulted in non entering of 1.3 pin gauge.|Why2-Burr folded inside hole while drilling operation in Fitting.','|1.Final Inspection of drill diameter will be carried out after drilling operation by Fitting department.','|1.Awareness created among Fitting persons about the burr folded after drilling operation.\r<br/>2.Visual Inspection awareness given for Fitting team to remove the burrs after drilling operation.','Effectiveness Found OK.','','2018-08-14','Irappa(Badiger)','Shivakumar S,SHIVAKUMAR ,Ravi M,Raghavendra P,KRISHNAMURTHY N,BHUVANAPRAKASH  J.S,','','0000-00-00','Fitting not done properly.','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','','FI','yes','Fitting','Narasimha Murthy(R)','no','','|1.Deburred the parts and crosschecked again all parts to ensure the entry of 1.3 dia pin.','E3456','qas|','2018-09-04|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(10999,'47-149','GKN Aerospace Filton','LWR ANGLE ATTACHMENT','560504A3','F57254364200','NA','PART ISSUE C',1,'1210042824','','78600','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','profile shift 1MM','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. ','CAPA found ok.','','2018-08-14','Ravi nayak()','prodn_aero(prodn)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Ravi nayak()','no','','Program was changed and program proved part found OK.','E3456','qas|','2018-12-10|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11000,'35-192','Saab AB','SUPPORT-FTG','223359B1','423Z1202-14','','---',2,'787 Forecast','','76943','','0000-00-00',NULL,'yes','no','yes','no','yes','no','no','no','no','Bore oversize up to 50microns.','Chips clamp/clot at  taper shank of holder.','Clean the overall tool pockets and tool changer arm.','We are check the reapetablity of run out of boring tool for lot of time it achieve constant.','CAPA FOUND OK','','2018-08-14','prodn_aero(prodn)','Kiran.K.S(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','05','no','Misc','Kiran.K.S(K)','no','','Clean the taper shank and check the run out.','A3456','qas_aero|','2018-09-06|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11001,'35-426','Saab AB','BRACKET','533388C','D522 73394 200 00','','A',1,'OWED-LTA-001','','75929','','0000-00-00',NULL,'no','yes','yes','no','no','no','yes','no','no','Side rib broken.','Part over righted in 03 operation.','Operator under observation.','Guide the all operator to this issue and guide the all operator. ','CAPAFOUND OK','','2018-08-14','prodn_aero(prodn)','prodn_aero(prodn)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Dinesh kulal()','no','','Guide the operator about tighting part.','A3456','qas_aero|','2018-09-06|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11002,'51-089','THE BOEING COMPANY','HOUSING','G24256K05','312W5220-7','NA','PSDL REV -',1,'486998 MPP','','74788','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Thickness 3.01mm -0.1mm undersized.','Thickness undersized while doing the rework.|Operator did not monitored the life of the tool due to which the cutting edge got broken and resulted in chattering. In order to remove the chattering operator took work offset after changing the cutting edge instead of taking the wear offset after the change of tool.|Operator was not aware of the rework procedure and method of rework.','|Changed the work offset and wear offset with the help of senior operator and continued the production.','|1) Supervisors to properly train the new operators before authorizing for doing rework.\r<br/>2) Informed all the operators to inform the concern supervisors before carrying out rework.','Operator effectiveness to be measured.','','2018-08-14','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','09','no','Misc','Sandhesh D(S)','no','','|Immediately stopped the machine and informed the senior operator and changed the offset values.','E3456','qas|qas|','2018-08-16|2018-08-17|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11003,'28-003A','Magellan Aerospace New York  Inc.','PIN-ATTACHMENT WALKING BE','SG1333B4-H10','161A7305-1','','PL-Rev-NC, DL Rev-B',1,'A000153663','','78217','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','ID OVER SIZE 0.05 MM...','Why 1 - ID oversized 0.05mm beyond drawing limit.|Why 2 - ID oversized during the re-pass operation as the re-pass ran twice.|Why 3 - Re-pass ran twice with same 0.15 wear offset as the operator provided -0.2mm wear offset during the insert change.|Why 4 - To maintain stock in the ID after the insert change the operator provided -0.2mm in the initial stage and after measuring the bore 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 Bore oversize.|Why 5 - Operator was unaware that the program for ID runs twice with different stock levels to achieve finish in the final operation.','|1) 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.','','2018-08-14','Raghavendra Rao(R)','Dinakar K,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','13','no','DX 200-2 ','GUNDEGOWDA(H.G.)','no','','|Immediately stopped the machine and changed the wear offset and continued the production on the next part.','E3456','qas|qas|','2018-08-16|2018-08-22|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11004,'28-041','Magellan Aerospace New York  Inc.','LEVER ASSY-SECONDARY SPOI','158334','65-46358-16','','PL_E, DL_N/C, Sketch # 1',1,'A000148833','','73992','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','REWORK TIME ID DEPTH WAS OVERSIZED.','DURING THE REWORK OPERATION DEPTH GOT OVERSIZED AS THE OPERATOR CONFUSED WITH X Z AXIS. |PART PROFILE WAS HAVING BEND AFTER  THE COMPLETION OF MILLING OPERATION DUE TO WHICH THE DEPTH WAS NOT ACHIEVED ON ONE SIDE |DURING THE COMPLETION OF MILLING OPERATION PART WAS HAVING FACE OUT DUE TO WHICH THE DEPTH WAS NOT ACHIEVED IN MACHINING. ','|TAKEN OFFSET FOR EVERY PART AND CORRECTED THE X AND Z AXIS ROTATION AND FOUND THE NEXT PART OK.','|1.IT HAS BEEN TOLD TO THE MILLING CENTER SUPERVISOR TO MACHINE THE PARTS WITH OUT ANY BEND AND TO GIVE THE PART FOR THE NEXT OPERATION WITH OUT ANY BENT PROFILE.          \r<br/>2.CHECK THE BEND BEFORE MACHINING AND SEPARATE THE PARTS WITH BEND AND CARE WILL BE TAKEN TO THESE PARTS WHILE MACHINING. ','Root cause analysis to be continued in the next batch production.','','2018-08-16','Ravi(M)','Vasu(SN)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','013','no','Misc','Sandhesh D(S)','no','','|CHECKED THE PREVIOUS MACHINED PARTS AND FOUND OK.','E3456','pe|qas|','2018-08-18|2018-09-04|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11005,'47-143','GKN Aerospace Filton','STIFFENER 6 TOP SKIN','1011901 2','D57250497202','NA','PART ISSUE H',1,'1210042824-1','','79606','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','Wall thickens taper & -side.(0.13mm proses problem) ','Due to improper butting of part in fixture.|Fixture was in stock.|Fixture validation was not done.','|Changed the fixture.','|Upcoming fixtures will be validated through QAD and will be taken for part prove out.','Same fixture was used to manufacture 47-141 & 47-143. CAPA found ok.','','2018-08-16','Ramesh(Poojary)','Sathisha(K.C.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','3','no','Misc','Dhananjaya(N)','no','','|Fixture was validated and built new fixture.','E3456','cam|qas|','2018-08-22|2018-09-05|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11006,'18-101A','Magellan Aerospace Bournemouth','TUBE -STRUT','B87/17','PID572 50464 202','','F',1,'428863','','79296','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1NOS Hole operation missing.','','','','','','2018-08-16','Irappa(Badiger)','Raghavendra P,GUNDEGOWDA H.G.,Devaraj K.C.,','','0000-00-00','Fitting.hole operation. missing.','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','Manufacture Only','','FI','no','DX200-4','Narasimha Murthy(R)','no','','','E3456','qas|','2018-08-18|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11007,'51-085A','THE BOEING COMPANY','BRACKET DETAIL','BA47920','332A2930-64','NA','PSDL REV B',1,'BOEING 001U','','74038','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','LEG THICKNESS MEASURED BELOW THE SPECIFICATION\r\nSPECIFICATION-6.22/6.1\r\nMEASURED-6.09/6.11','1.While part running time chips present in part butting face so part thickness -ve side ','|1.check the fixture top surface before loading the part,','|1.informed to all shift operators ,Before loading any parts clean the fixture top face mandatory.','CA/PA satisfied','','2018-08-16','pe_sez(a)','pe_sez(a)','','0000-00-00','LEG THICKNESS MEASURED BELOW THE SPECIFICATION\r\nSPECIFICATION-6.22/6.1\r\nMEASURED-6.09/6.11','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','Misc','qas_sez(a)','no','','|1.stop the m/c and check the previous parts found ok','Z3456','pe_sez|qas_sez|','2019-01-17|2019-01-18|','2019-01-18',NULL,NULL,NULL,NULL,NULL,NULL),(11008,'35A-457A','Saab AB','LATCH BRACKET ASSY','','D522 73484 001 00','','PART ISSUE B',1,'OWED-LTA-002','','A17576','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','ZN-NI PLATING CHIP OUT.','1.The parts are having plating chip off|2.The parts from treatment house plating chip off occurred|3.Before assembly process which is not identified from inspection','|During treated parts inspection the parts are to be checked for any chip off and damages','|The defected parts details sent to supplier and informed them to check clearly for surface treatments','CAPA found ok','','2018-08-16','Yashawantha(NH)','Yashawantha(NH)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Assembly','','FI','no','Misc','Yashawantha(NH)','no','','|The remaining parts are checked and verified ok','E3456','qas|','2018-12-20|','2018-12-20',NULL,NULL,NULL,NULL,NULL,NULL),(11009,'28-039','Magellan Aerospace New York  Inc.','SPACER WASHER, BUSHING - ','L34636','161A2303-1','','PL _A, PSDL_ N/C',1,'A000153814','','78223','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Total length under size(0.04 MM) ','Part length was got undersized during turning facing operation |Part was not properly loaded in chuck|Due to burr seated on 3 jaw chuck part was not properly arrested|So before loading part into 3 jaw chuck cleaning and checking was not done properly','|For every part loading time the chuck to be clean by using  Air gun and that to be ensure free of FOD\r<br/>Then the every part\'s dimension is to be check','|Awareness given to the operator regarding Foreign Objects Debris cleaning','CA PA found ok.','','2018-08-17','Ravi(M)','Seetharamu D,Santhosh Kumar N,Ravi M,Ningaraj A N,KRISHNAMURTHY N,Ashoka R,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','FI','no','DX 200-3','Nandishkumar(D.K.)','no','','|The WIP parts length was checked and ensured OK\r\nThen cleaning and checking is doing before part loaded into chuck','E3456','qas|qas|','2018-08-17|2018-08-17|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11010,'35A-601','Saab AB','FRAME ASSY','','D5227338501000','','PART ISSUE C',22,'OWED-LTA-001','','A16622','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','yes','Lot No: 1600237626-13-1\r\nw/o no: A16622/73964, Quantity: 21 pcs\r\nw/o no: A16625/73202, Quantity: 12 pcs\r\nw/o no: A16670/73963, Quantity: 7 pcs\r\nLot No: 1600234150-22-2\r\nw/o no: A16623/73200, Quantity: 9 pcs\r\nw/o no: A16624/73200, Quantity: 3 pcs\r\nIs condition: 1. 5 parts have marks in top coat, primer is not damaged, 2 parts are damaged in top coat\r\nand primer, bare metal.\r\n2. Anchor nuts are missing visible sealant - all 52 pcs\r\nFor reference, please see pictures below.\r\nShould be: Continuous and covering surface treatment all over. Annular sealant shall be squeezed out under fasteners.','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  impr0per 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.\r<br/>\r<br/>','Delta FAI carried out and CAPA implementation found ok.','C66866','2018-08-17','Yashawantha(NH)','Yashawantha(NH)','OF-003130','2018-08-07','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','Cust End','yes','Misc','qas(qas)','no','','|Immediate stock check carried out and no similar affected parts were fund in FG.','E3456','qas|','2018-12-10|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11011,'35-621','Saab AB','PIN','C80552.SD4W','D5227281820000','NA','PART ISSUE A',1,'OWED-LTA-004','','71759','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','yes','Is condition: PIN has no groove in the head or hole through threads. See drawing and photos below.\r\nShould be: Groove and hole according to the drawing D52272818','1.The part was not having groove and hole on thread|2.During inspection part was not identified regarding missing operation','|During final inspection the parts are to identify with the completion of all operations','|The missing operation to be control in machine itself','CAPA found ok','C63949','2018-08-17','Yashawantha(NH)','Yashawantha(NH)','OF-003131','2018-08-08','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','DN39422','Cust End','no','Misc','qas(qas)','no','','|The parts in FG and inprocess found ok','E3456','qas|','2018-12-20|','2018-12-20',NULL,NULL,NULL,NULL,NULL,NULL),(11012,'35-599','Saab AB','BEAM','533635B1','D5227338120400','NA','PART ISSUE C',30,'OWED-LTA-001','','75977','','0000-00-00',NULL,'yes','no','no','no','no','yes','no','yes','no','In MPS no. MPS/35-599 Rev. 00 the hole Dia is 3.6 +0.1 Shown, \r\nbut as per Customer Drawing the required hole Dia is 3.6D10 (3.63/3.678). Physically Hole Dia measuring 3.6mm.\r\n','ERROR IN MASTER PROCESS SHEET|DUE TO TYPO ERROR|DURING THE PROCESS, DID NOT NOTICE THE PARAMETER 3.6D10','|WE HAVE CHANGED THE MPS & HAVE GIVEN THE REFERENCE COPY. NEXT BATCH PARTS FOUND OK','|MPS WILL BE CROSS-CHECKED WITH THE MASTER DOCUMENTS, BEFORE UPLOADING TO CIMSOFT','Next batches found ok.','','2018-08-18','Ramesh(Poojary)','Nandeep()','','0000-00-00','NC','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','','Production','yes','Misc','Manu(P)','no','','|WE NOTICED THE VALUE & INSTRUCTED THE OPERATOR TO CHANGE THE TOOL','E3456','cam|qas|','2018-11-15|2018-11-15|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11013,'35-531A','Saab AB','SHAFT LATCH','C90596','D5227349020200','NA','PART ISSUE C',1,'OWED-LTA-002','','75910','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Side Hole position change','','','','','','2018-08-18','pe_sez(a)','Dinakar K,','','0000-00-00','Side Hole position change','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','7','no','QT100S-3','pe_sez(a)','no','','','Z3456','qas|qas_sez|','2018-08-25|2018-10-03|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11014,'35-231A','Saab AB','HINGE BRACKET 4 ','218591B6','D576 50007 208','','E00',2,'1600223433/Forecast ','','77763','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Part lifting from the vice on production time.','Part lifting from the vice on production time then part taper upto 1.0mm','|All taper parts facing at butting surface.','|All raw materials facing at part butting surface & taper checked in outside.','CAPA FOUND OK','','2018-08-20','Dinesh kulal()','Kiran.K.S(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','Production','no','Misc','Dinesh kulal()','no','','|Nexr part loading time parts taper checked & loaded the machine.','A3456','prodn_aero|qas_aero|','2018-10-13|2018-10-13|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11015,'51A-085A','THE BOEING COMPANY','BRACKET ASSY','','332A2930-62','','PSDL REV B',1,'BOEING 001U','','A17487','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','BUSH BORE OVER SIZE IN CERTAIN POINT','UNEVEN STOCK FOR REAMER|ROUGHING BORE SIZE NOT MAINTAINED PROPERLY|THE OPERATOR NOT MONITOR THE ROUGHING BORE SIZE|THE OPERATOR ONLY CONSECRATE ON THE FINAL READING WHICH WAS DONE BY REAMER ','|ROUGHING BORE DIMENSION CHECKED BY THE BORE DIAL GAUGE. IT WAS MAINTAINED BY THE 0.05MM PER SIDE STOCK','|A HOLE MILL WILL BE ADDED WHICH WILL MAINTAIN THE 0.05MM PER SIDE STOCK EVEN','CA/PA satisfied.','','2018-08-20','pe_sez(a)','op_sez(s)','','0000-00-00','Bush bore is ovality ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Assembly','','06','no','Misc','pe_sez(a)','no','M05484','|PRODUCTION STOPPED','Z3456','pe_sez|qas_sez|','2018-08-20|2019-01-07|','2019-01-07',NULL,NULL,NULL,NULL,NULL,NULL),(11016,'35-231A','Saab AB','HINGE BRACKET 4 ','218591B6','D576 50007 208','','E00',1,'1600223433/Forecast ','','77763','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','part taper','Part lifting from the vice in production time then part taper. ','|All taper parts facing at part butting surface.','|All raw materials facing & taper checked before loading the machine.','CAPA FOUND OK','','2018-08-20','Dinesh kulal()','prodn_aero(prodn)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','','Production','yes','Misc','Dinesh kulal()','no','','|Parts loading time taper checked & loaded the machine.','A3456','prodn_aero|qas_aero|','2018-10-13|2018-10-13|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11017,'51A-041','THE BOEING COMPANY','BRACKET ASSY','','149A7371-601','','PSDL REV A',1,'BOEING 001F','','A17373','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','H6 HOLE CSK OVERSIZE','1) CSK oversize because of increased depth.|2) Depth was controlled by manual load application as the CSK formation was carried out by hand manually.','|All the CSK were checked using a similar rivet and depth was increased gradually until the required Diameter was achieved.','|Purchased drill machine for which the standard CSK tool will be installed and height will be fixed from the result of first hole formation.','CA PA found ok.','','2018-08-20','pe_sez(a)','pe_sez(a)','','0000-00-00','H6 HOLE CSK SIZE OVERSIZE','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Assembly','','FI','no','Misc','qas_sez(a)','no','','|Immediately stopped the assembly process and informed to the supervisor and checked all the completed parts and found ok. ','Z3456','qas|','2019-02-21|','2019-02-21',NULL,NULL,NULL,NULL,NULL,NULL),(11018,'56-005','GKN Aerospace Orangeburg','SPLICE PLATE FWD UPR','14336DC','119A1213-603','NA','PSDL REV -',1,'LTA GKN 737 Winglet','','77192','','0000-00-00',NULL,'yes','no','yes','no','yes','no','no','no','no','HOLE POSITION NOT ACHIEVED ','Dimension of a Hole position from a Datum measured out of tolerance.|Hole Shifted during the 5axis machining time.(Positional 5-Axis)|Rotary did not tilted to the required angle.|Problem with the movement of the rotary.|Problem with the Pivot point measurement in the machine & CAM post processor.','|1) Loaded the FAIR part in other machine and proved the program. ','|1)Maintenance team from rotary supplier (U-CAM) arrived onsite and solved the rotary issue and fixed the pivot point value.\r<br/>2)Application engineer from CAM software arrived onsite and trails done to fix the pivot point on the rotary table.  ','NEXT PART FOUND OKAY','','2018-08-20','pe_sez(a)','Kiran Kumar M,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','3','no','PS105-01','pe_sez(a)','no','','|1) Immediately stopped the machine and informed the maintenance team. \r\nand Maintenance team & Engineering team discussed with Rotary table supplier and CAM software supplier. ','Z3456','pe_sez|pe|qas_sez|','2018-08-21|2018-12-22|2018-12-22|','2018-12-22',NULL,NULL,NULL,NULL,NULL,NULL),(11019,'35-622','Saab AB','FLAP, VENT','2270601','D5227280420000','NA','PART ISSUE A',1,'OWED-LTA-003','','78651','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Z OFF SET 3P6 MM DOWN SO PART THICKNESS UNDER SIZE.   ','This is communication gap.|That part 1st setup No:1 pallet and 2nd setup running.1st running time tool brokered.|1st shift operator check the part before unloading. then tool broken area near 3mm dig mark observed.|Again run the same part work offset wear correction -3.5mm.|Not effect the 1st setup. but 2nd setup running before offset wear zero not correction so part 3.6mm under size.2nd setup run in 2nd shift.','|Finally part rejected. remove the part again taken z offset and cross check X&y offset run next part. |Cutting tool offset input and cross checking method was implemented which is by using Zoller machine.','|If any deviation first inform to supervisor and discus cad/cam engineer.  ','','','2018-08-20','Rangaswamy()','        Manu ','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','03','','','','','','|Inform to supervisor and 1st shift operator.|The machine was stopped.\r\nAll cutting tool offset was cross checked in the program.\r\nPrevious parts were inspected and found ok.\r\nInformed to the supervisor.\r\n','Z3456','pe_sez|pe_sez|qas_sez|','2018-09-25|2018-12-17|2018-12-17|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11020,'35-231A','Saab AB','HINGE BRACKET 4 ','218591B6','D576 50007 208','','E00',1,'1600223433/Forecast ','','76785','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','DIG MARK OBSERVED ON WALL.','','','','','','2018-08-21','pe_sez(a)','Shivaraj K S,Kiran KM,','','0000-00-00','.','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','3','no','Slim3n-5AHT-1','pe_sez(a)','no','','','Z3456','qas_sez|','2018-10-29|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11021,'18-382B','Magellan Aerospace Wrexham','SLEEVE BEARING','A1141Z W89730','D575 40037 200 PF','','A',1,'RP143022','','77739','','0000-00-00',NULL,'yes','yes','yes','','','','','','','id dig mark. ','running time air pressure low ,so id dig mark. ','|we are inform to the maintenance for the proper connection. ','|we are inform to the maintenance for the proper connection. ','Clogging of inlet and out let of the compressor and drop of pressure due to power fluctuation need to be addressed and monitored during every preventive maintenance.','','2018-08-21','Ravi(M)','        Ningaraj A N','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','11','','','','','','|checked the previous machined parts found ok.','E3456','pe|qas|','2018-09-03|2018-09-04|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11022,'46-037B','Mahindra Aerostructures Pvt.Ltd','STRAP ','24990','D575-40872-200-01','NA','K02, BOM ISS J, ECN NG26090ST1KD02',2,'3101173229 AMD 1','','79223','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','outer rib broken ','Datum presetting error by operator on the machine','|Instructed operators also to cross check with additional datum  hole during fixture re-setting for every new batch of production.','|Need to add additional datum hole on all fixture for cross checking during initial setup.','Next batches found ok.','','2018-08-21','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','01','no','Misc','Narayanappa(G)','no','','|Immediately stopped the machine and changed the machine parameters and continued the production.','E3456','pe|qas|','2018-10-25|2018-10-27|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11023,'47-200','GKN Aerospace Filton','BRACKET M/C','487485B','F57555656201','NA','PART ISSUE B',1,'1210042824-2','','79715','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','wall rib thickness minus 6mm','program post problem|due to wrong ucs selection|due to negative ucs wrong selection','|positive ucs selection','|prepared the visual other engineer person visually checking|Senior Engineer to verify the UCS with respect to the customer supplied data before loading to the machine.','CAPA found ok.','','2018-08-22','Ravi nayak()','prodn_aero(prodn)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Ravi nayak()','no','','|correct ucs selected','A3456','prodn_aero|qas|','2018-08-22|2018-09-05|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11024,'35-159','Saab AB','FLCD_DS_DEFLECT_STOP','852710-03','423Z6187-8','','---',1,'Forecast po for B787','','77911','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','BASE THICKNESS UNDER SIZE BY 0.15MM\r\n(AS PER REQUIRED 3.05 +/- 0.254 MEASURED 2.65 TO 2.67MM)','While running time part was lifted.|Part clamping not properly.','|Inform to operator before cycle start the machine cross check the all clamps.','|Inform to operator before cycle start the machine cross check the all clamps.\r<br/>Apply the \'M00\' Message at starting of the  program.','CAPA found ok for next batch.','','2018-08-22','Lohith(K)','Shivaraj K S,Maruthi  D R ,Kiran Kumar M,Kiran KM,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','PS105-01','Nagendra(SN)','no','','|Immediately Cross check the clamping, continue the production.','E3456','pe|nagendra|','2018-09-05|2018-12-06|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11025,'35-159','Saab AB','FLCD_DS_DEFLECT_STOP','852710-03','423Z6187-8','','---',1,'Forecast po for B787','','77911','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','PART DIG MARK OBSERVED ON SIDE FACE.','While part running time tool was broken.|The Tool sharp edges are wearied out.\r\n ','|Informed to operator to check the tool condition after completion of the part.','|Informed to operator change the tool when the cutting tool noise is more.','CAPA Found OK','','2018-08-22','Lohith(K)','Shivaraj K S,Maruthi  D R ,Kiran Kumar M,Kiran KM,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','PS105-01','Nagendra(SN)','no','','|Informed to operator to check the tool condition after completion of the part.','E3456','pe|nagendra|','2018-09-05|2018-12-06|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11026,'18-119B','Magellan Aerospace Bournemouth',' 	HOUSING OUT B DRG 3 ','1649701-2/WSGW','PID275 40011 200','','D01',2,'428868','','79532','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','COLLAR THICKNESS UNDERSIZE BY -0.3MM.','Why 1:- While running time insert broken.|Why 2:- Since the material(S130) is hard material we used to change the insert once in every 5 Parts. But this time the cutting edge of the insert got broken for the second part itself then the cutting edge was changed and this time the insert broken for the first part and the thickness got undersized.|Why 3:- Shim used to align the insert was found broken from the bottom face when the entire assembly of the insert was removed and inspected and this crack not visible from the top face during the insert change and because of which the insert got broken for the second time.','|1) Changed the new shim and insert and retaken the offset and continued the production.\r<br/>2) Informed the tool\'s in-charge to inform the insert supplier about the issue.\r<br/>3) Informed all the operators to check the insert cutting edges after the completion of every single part.','|1) Informed all the operators and supervisors to check the shim completely during the setting time.\r<br/>2) Sumitomo (Insert Supplier) informed to use upgraded insert for these kind of hard materials.','CAPA found ok.','','2018-08-22','Raghavendra Rao(R)','Raghavendra(P)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','05','no','Misc','Ravi(M)','no','','|Immediately stopped the machine and checked the thickness of all the completed parts and found ok.','E3456','qas|qas|','2018-08-22|2018-09-04|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11027,'47-144','GKN Aerospace Filton','STIFFENER 6 TOP SKIN','1011901 2','D57250497203','NA','PART ISSUE H',1,'1210042824-1','','79529','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','THICKNESS 1.5 +0.13/-0.08 MEASURING 1.32 AT ONE END','Due to improper butting of part in fixture.|Fixture was in stock.|Fixture validation was not done.','Changed the fixture. ','Upcoming fixtures will be validated through QAD and will be taken for part prove out. ','CAPA found ok (Same fixture was used for 47-141, 142, 143 & 144 and the part proving was done on the same date.','','2018-08-22','Ramesh(Poojary)','Ramesh(Poojary)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','Misc','Nandishkumar(D.K.)','no','','Fixture was validated and built new fixture.','E3456','qas|','2018-09-05|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11028,'18-008A','Magellan Aerospace Wrexham','Plate Cover','670593','D572 52518 200','L97 T351','A',3,'175175','','80000','','0000-00-00',NULL,'yes','yes','yes','','','','','','','center axis has been shifted for 2mm','1)THE PART WAS LOADED IN 18-088A FIXTURE,DUE TO THAT PLAY OCCURRED AND THE CENTER HAS BEEN SHIFTED.\r\n|2)INSTEAD OF LOADING 18-008A CRN FIXTURE,18-088A FIXTURE WAS LOADED.|3)OPERATOR DID NOT NOTICE THE FIXTURE IDENTIFICATION AND LOADED THE WRONG FIXTURE WITHOUT PROPER GUIDANCE.','|INDEXED THE FIXTURE AND PART WAS FOUND \"OK\".','|SEPARATE FIXTURE WILL BE MADE FOR BOTH CRN\'S 18-008A AND 18-088A.','New fixture manufactured and CAPA implemented and found ok.','','2018-08-22','Raghavendra Rao(R)','        Dinakar K','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','03','','','','','','|INDEXED THE FIXTURE. ','E3456','pe|pe|qas|','2018-08-22|2018-08-22|2018-09-04|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11029,'18-119B','Magellan Aerospace Bournemouth',' 	HOUSING OUT B DRG 3 ','1649701-2/WSGW','PID275 40011 200','','D01',1,'428868','','79532','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','BORE DEPTH OVER SIZE BY 0.45MM.','CHANGED THE BORING TOOL DUE TO CHATTERING.|WHILE PERFORMING BORING OPERATION CHATTERING OCCURRED.|INSTEAD OF PUTTING LEFT HAND TOOL,RIGHT HAND TOOL WAS INSTEAD.|SPINDLE ROTATION HAD TO BEEN ALTERED ,BUT IT WAS NOT DONE.|DUE TO WRONG ROTATION OF THE SPINDLE THE PART CAME OUT OF THE JAWS AS THE PRESSURE OF JAWS WAS SET LESS.','|CHANGED THE SPINDLE SPEED AND ROTATION AND THE OTHER PARTS WHICH WAS BEING MANUFACTURED IS FOUND OK.','|SPINDLE ROTATION AND TYPE OF TOOL TO BE USED i.e; LEFT HAND TOOL OR RIGHT HAND TOOL AND LENGTH OF THE TOOL.','CAPA found ok.','','2018-08-22','Ravi(M)','Ravi(M)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','11','no','Misc','Ravi(M)','no','','|CHECKED THE PREVIOUS MACHINED PARTS FOUND OK.','E3456','pe|qas|','2018-08-22|2018-09-04|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11030,'47-199','GKN Aerospace Filton','BRACKET M/C','391945 C','F57555656200','NA','PART ISSUE B',1,'1210042824-2','','79714','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','program Run the part reverse direction','actual part is 47-199 but Program Run 47-200|program problem|wrong naming of program ','|program will be cross checked twice|Changed the name of the program and deleted the wrong program.','|double cross checking visually|Informed all the engineers and the operator to verify the program name before loading to the machine and starting the cycle.','CA PA found ok.','','2018-08-22','Ravi nayak()','prodn_aero(prodn)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Ravi nayak()','no','','|program was changed|Checked all the program name and the programs copied and changed the name of the affected programs.','A3456','prodn_aero|qas|','2018-08-22|2018-09-05|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11031,'47-142','GKN Aerospace Filton','STIFFENER 5 TOP SKIN','4200901 1','D57250496203','NA','PART ISSUE N',1,'1210042824-1','','78046','','0000-00-00',NULL,'no','yes','yes','no','no','no','yes','no','no','L and LT, direction wrong ','RM L & LT, direction wrong selection |not give the correct direction sheets |RM L & LT correct Drawing sheets ','|prepared RM L & LT correct Drawing sheets |Changed the L & LT direction both in the MPS and the RM cutting sheet.','|RM L & LT mention on Reference Cutting sheet |All the reference and machining documents will be approved for release only after the review of the senior engineer.','','','2018-08-22','Ramesh(Poojary)','                        Sathisha(K.C.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Sathisha(K.C.)','no','','|RM L & LT, direction correct selection|Checked all other parameters in the MPS with respect to the drawing.','E3456','cam|cam|pe|qas|','2018-08-22|2018-08-22|2018-09-04|2018-09-05|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11032,'51-038','THE BOEING COMPANY','BRACKET','436278','149A7371-966','','PSDL REV A',10,'BOEING 001E','','75319','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','OVERALL PROFILE THICKNESS UNDERSIZED BY 0.8mm','1.Part rejected due to process proving time wrong program given|2.Due to NC program fault.|3.Wrong UCS selected,due to changing in program.|4.Program wall stock was not distributed equally so part wall dig mark observed in finishing stage.','|Updated NC program and executed on machine and part found ok.','|Before execution the program on machine programmer has to double cross check the program.','CAPA FOUND SATISFACTORY.','','2018-08-22','pe_sez(a)','pe_sez(a)','','0000-00-00','OVERALL PROFILE THICKNESS UNDERSIZED BY 0.8mm','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','Misc','qas_sez(a)','no','','|Updated NC program and executed on machine and parts was found ok.Absolute old program and new updated program moved to program data storage','Z3456','pe_sez|qas_sez|','2019-01-17|2019-02-13|','2019-02-13',NULL,NULL,NULL,NULL,NULL,NULL),(11033,'18-120C','Magellan Aerospace Bournemouth',' 	HOUSING OUT B D BRG 3 ','1649704-2/WSGX','PID275 56121 200','',' 	E01, ECN NG27011ST1KA83',1,'428868','','79013','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Part Marking operation missing.','One off part with no part marking reaching QAD.|Part marking operation was missed on that part.|Operator stored the part marking completed part along with the pending part and got confused which is not marked and which is marked.|The batch qty was high and the space was less to accommodate all the parts therefore he stored the completed parts along with the pending ones and did not rechecked them before forwarding to next operation.','|Redone the part marking on the missed out part and handed over to inspection.','|1) Both the finished and pending parts will not be stored together and will be stored separately.\r<br/>2) Re-inspection of all the parts for the completion of part marking will be done before sending to next operation.','CAPA found ok.','','2018-08-23','Anjinamurthy(H)','Vasu SN,Santhosh Kumar N,S. Shiva Kumar,Raghavendra P,Paramaeshappa ,BHUVANAPRAKASH  J.S,Ashoka R,','','0000-00-00','Part Marking santhosh.','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','Manufacture Only','','FI','no','BMV 60-1','Narasimha Murthy(R)','no','','|Checked part marking of all the other parts and remaining parts were found ok.','E3456','pe|qas|qas|','2018-09-05|2018-09-05|2018-09-08|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11034,'35-630','Saab AB','SUPPORT SEAL RETAINER ','203993B1','423Z1834-1-03','NA','---',1,'Forecast po for B787','','75999','','0000-00-00',NULL,'yes','yes','yes','','no','','','','','35-630 1st part running time tool off set wrong entry.so dig mark occurred on part.','During milling operation alarm came on machine pocket magzine.|So the another tool pocket needs to be called up.|so another pocket required on offset.|During that offset data entry time wrong value entered.|The manual error occurred on offset.','|The maintenance work taken on magzine pockets due to that during milling operation alarm does not show.\r<br/>And the offset data wont to be enter directly tool offset will be taken','|The machine maintenance to be carried out periodically to avoid alarms.','CAPA found ok.','','2018-08-24','Gurukiran S(M)','                Basavaraja S. Jr.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','05','','','','','','|During the next part process time correct offset taken.','E3456','qas|qas|','2018-08-27|2018-09-05|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11035,'35-599','Saab AB','BEAM','533635B1','D5227338120400','NA','PART ISSUE C',1,'OWED-LTA-001','','75977','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','HOLDER DIG MARK ON THE PART','SELECTION OF TOOL HOLDER MISTAKE, WHEN THE DIA 10*45 DEG CHAMBER TOOL RUNNING TIME, THE TOOL HOLDER HEAD RUB THE PART|THE NEW OPERATOR ONLY OBSERVED THE CUTTING TOOL OVER HANG. HE UNKNOWN ABOUT THE TOOL HOLDER.|THE CORRECT TOOL HOLDER NOT MENTIONED IN THE NC PROGRAM DETAIL. ','|PENCIL TYPE TOOL HOLDER REPLACED. PENDING PROGRAMS PROVED.','|FOR SIMILAR OPERATIONS THE TOOL HOLDER DETAILS WILL BE MENTIONED THE PROGRAM. THE DETAILS OF THE CRITICAL OPERATION WILL DISCUSSED BEFORE THE SETTING START AND THE INFORMATION WILL PASS TO ALL MACHINE SETTERS AND OPERATORS   ','proper training on the selection of tool holder need to be provided to all the new operators before certifying them to run the machine individually. ','','2018-08-25','pe_sez(a)','Umesh B,Nataraja C V,NataRaj.CV ,Diwakar R.B.,','','0000-00-00','DIG MARK ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','3','no','i700-1','op_sez(s)','no','','|SETTING STOPPED. ','Z3456','pe_sez|qas|','2018-08-28|2018-10-12|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11036,'51A-072','THE BOEING COMPANY','BEARING ASSY','','113T1204-1','','NIL',1,'BOEING 001S','','A17211','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','DENT MARK FOUND ON BEARING','Due to the transit damage the above dent was observed ','|1)The transits damage was informed to the standard part suppliers.\r<br/>2)Supplier informed us to incorporate the new packing method.\r<br/>3)They packed the parts to each individual qty in the one cover sheet.','|1)The transits damage was informed to the standard part suppliers.\r<br/>2)Supplier informed us to incorporate the new packing method.\r<br/>3)They packed the parts to each individual qty in the one cover sheet.','CA/PA found satisfied.','','2018-08-25','pe_sez(a)','pe_sez(a)','','0000-00-00','DENT MARK FOUND ON BEARING','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','FI','yes','Misc','qas_sez(a)','no','','|1)Immediately internal NC was raised and re-inspected all the FG quantities.\r\n','Z3456','qas_sez|','2019-01-18|','2019-01-18',NULL,NULL,NULL,NULL,NULL,NULL),(11037,'18-741A','Magellan Aerospace Wrexham','STRIP','63026/02','F57252299202','NA','A',4,'176541','','78521','','0000-00-00',NULL,'yes','no','no','no','no','yes','no','yes','no','Drawing dimension required hole pitch is 32 typ but 29.744 to 34.988 is measured.. ','Improper butting of part during machining|The part was not butted to the reference stopper during OP-02|While clamping due to the  pressure the part was drawn back while clamping ','|1.A Separate tool was called out in the program to cross verify whether the part is butted properly to the reference\r<br/>2.Instructed Operator to cross check whether the part is butted properly after the reference.','|Refer to CA','Next batch wo #79712 machined and found ok','','2018-08-25','pe_sez(a)','pe_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','Misc','qas_sez(a)','no','','|1.The part was rejected and internal NCR was raised.\r\n2.Checked wether the stopper given for the reference is zero and found ok.','Z3456','qas_sez|','2019-04-17|','2019-04-17',NULL,NULL,NULL,NULL,NULL,NULL),(11038,'18-741A','Magellan Aerospace Wrexham','STRIP','63026/02','F57252299202','NA','A',4,'176541','','78423','','0000-00-00',NULL,'yes','no','no','no','no','yes','no','yes','no','1)Drawing dimension required hole pitch is 32 typ but 29.744 to 34.988 is measured.\r\n2)RD3.20 in 3 place required but 4 place in part.','Improper butting of part during machining|The part was not butted to the reference stopper during OP-02|While clamping due to the  pressure the part was drawn back while clamping ','|1.A Separate tool was called out in the program to cross verify whether the part is butted properly to the reference\r<br/>2.Instructed Operator to cross check whether the part is butted properly after the reference.','|refer to CA','next batch machined wo#79712 found ok ','','2018-08-25','pe_sez(a)','pe_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','Misc','qas_sez(a)','no','','|1.The part was rejected and internal NCR was raised.\r\n2.Checked whether the stopper given for the reference is zero and found ok.','Z3456','qas_sez|','2019-04-17|','2019-04-17',NULL,NULL,NULL,NULL,NULL,NULL),(11039,'51A-072','THE BOEING COMPANY','BEARING ASSY','','113T1204-1','','NIL',2,'BOEING 001S','','A15481','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','no','DENT MARK FOUND ON BOUGHT ITEM(BEARING)','REFER NC NO:11036','|REFER NC NO:11036','|REFER NC NO:11036','REFER NC NO:11036','','2018-08-27','pe_sez(a)','pe_sez(a)','','0000-00-00','DENT MARK FOUND ON BOUGHT ITEM(BEARING)','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','FI','yes','Misc','qas_sez(a)','yes','','|REFER NC NO:11036','Z3456','qas_sez|','2019-01-18|','2019-01-18',NULL,NULL,NULL,NULL,NULL,NULL),(11040,'51A-072','THE BOEING COMPANY','BEARING ASSY','','113T1204-1','','NIL',1,'BOEING 001S','','A17209','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','no','DENT MARK FOUND ON BOUGHT ITEM(BEARING)','REFER NC NO:11036','|REFER NC NO:11036','|REFER NC NO:11036','REFER NC NO:11036','','2018-08-27','pe_sez(a)','pe_sez(a)','','0000-00-00','DENT MARK FOUND ON BOUGHT ITEM(BEARING)','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','FI','yes','Misc','qas_sez(a)','yes','','|REFER NC NO:11036','Z3456','qas_sez|','2019-01-18|','2019-01-18',NULL,NULL,NULL,NULL,NULL,NULL),(11041,'51A-072','THE BOEING COMPANY','BEARING ASSY','','113T1204-1','','NIL',1,'BOEING 001S','','A17210','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','no','DENT MARK FOUND ON BOUGHT ITEM(BEARING)','REFER NC NO:11036','|REFER NC NO:11036','|REFER NC NO:11036','REFER NC NO:11036','','2018-08-27','pe_sez(a)','pe_sez(a)','','0000-00-00','DENT MARK FOUND ON BOUGHT ITEM(BEARING)','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','FI','yes','Misc','qas_sez(a)','yes','','|REFER NC NO:11036','Z3456','qas_sez|','2019-01-18|','2019-01-18',NULL,NULL,NULL,NULL,NULL,NULL),(11042,'56-014','GKN Aerospace Orangeburg','FAIRING SUPPORT - AFT','770293A9','119A1521-604','NA','PSDL REV A',2,'LTA Orangeburg 737 W','','77995','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','BASE THICKNESS 1.2MM UNDER SIZE ','NO STOCK IN BASE FOR MACHINING AND ACHIEVE THE REQUIREMENT DIMENSIONS.   |IN BEND REMOVING OPERATIONS MORE STOCK REMOVED INSTEAD OF 0.5MM|PART PEND WAS MORE AFTER THE ROUGHING OPERATIONS WHICH HAVE ONLY 1.5MM PER SIDE STOCK','|INFORMED TO ENGG DEPARTMENT TO INCREASE THE ROUGHING STOCK VALUE. NEW NC PROGRAM COLLECTED. RUN. AGING DONE. PART PEND VERIFIED IN THE SURFACE TABLE BY USING FEELER GAUGE. PART PEND WITH THE PLANNED LIMIT.','|REQUESTED  TO ENGG DEPART TO GIVE THE CORRECT ROUGHING WITH ALLOWABLE ROUGHING STOCK. AND THE OPERATOR ALSO REQUESTED TO CHECK THE STOCK VALUE EACH AND EVERY OPERATION COMPLETED.   |informed the engineering team to ensure the program generated before loading to the machine.','Stock not maintained in the program for the roughing operation therefore during the bend removal and finishing operation the thickness got undersized and resulted in the rejection of the part.\r\n','','2018-08-27','pe_sez(a)','op_sez(s)','','0000-00-00','BASE THICKNESS 1.2MM UNDER SIZE ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','pe_sez(a)','no','','|FURTHER OPERATIONS AND PRODUCTION STOPPED.  ','Z3456','pe_sez|qas|','2018-08-31|2018-10-12|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11043,'18-090A','Magellan Aerospace(Polska) Sp','BUSH','833467','PID278 50164 200','','A',26,'104569','','77971','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','OD UNDER SIZE.','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.','|1)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.','Effectiveness Found ok','','2018-08-27','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','03','no','Misc','Ravi(M)','no','','|Immediately stopped the machine and changed the wear offset and continued the production on the next part.','E3456','pe|qas|','2018-09-04|2018-09-05|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11044,'35-464','Saab AB','FITTING','533635A1','D522 73408 201 00','','A',1,'OWED-LTA-001','','76100','','0000-00-00',NULL,'yes','yes','yes','','','','','','','35-464 part setting time bore oversize ','THE OPERATOR CHANGED THE CUTTING TOOL DIAMETER FORMAT VALUE D38 INSTEAD OF D0.|THE OPERATOR NOT FULLY UNDERSTAND THE CUTTING TOOL COMPENSATE CONCEPT IN MAZATROL CONTROL. |THE OPERATOR HAVE INSUFFICIENT KNOWLEDGE IN MAZATROL CONTROL. ','|CORRECT CUTTING TOOL COMPENSATE VALUE GIVEN IN D0. THE FINE BORE DIAMETER ACHIEVED AS PER IN REQUIREMENT.  ','|THE SUFFICIENT TRAINING WILL GIVE TO THE OPERATOR REGARDING CUTTER COMPENSATE DIAMETER  VALUE AND ITS WORKING CONCEPT. THE DRY RUN OPERATION WILL BE CARRY OUT BEFORE MACHINING THE CRITICAL BORE.  ','CAPA found ok.','','2018-08-27','Rangaswamy()','        Diwakar R.B.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','03','','','','','','|SETTING STOPPED. ','Z3456','pe_sez|pe_sez|qas|','2018-08-27|2018-09-03|2018-09-27|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11045,'47-028A','GKN Aerospace Filton','RUBBING STRIP','D656850','F57550373200','NA','C, MIS ISSUE B',1,'S.A.No. 6200005328','','79621','','0000-00-00',NULL,'yes','yes','yes','','','','','','','12mm width 0.3 - side ','Part thickness is under size |Part was not butting in the fixture profile |Part was bend & twisted|while Raw material sharing time part found bend & twist','|part bend removing was done and continued the production','|Two location pin as been done in the fixture and raw materiel will be butted to that pin ','CAPA FOUND OK\r\n','','2018-08-27','Narayanappa(G)','        Rajesh B D','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','1','','','','','','|previous all part checked and founded ok','E3456','pe|pe|qas|','2018-09-04|2018-09-04|2018-09-05|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11046,'51-027','THE BOEING COMPANY','BRACKET','258462B1','149A7371-945','','PSDL REV A',4,'BOEING 001E','','79940','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','THICKNESS OVERSIZED NOMINAL MIN 0.14 AND MAX 0.16\r\nMEASURED 0.1640','While part running time operator not observe the tool.|The finishing tool already so many parts are running.','|Inform to the operator every part completed time check the part thickness mandatory. ','|Inform to the operator every part completed time check the part thickness mandatory. ','Rework done and inspected all quantities parts found within acceptable tolerance limits.','','2018-08-27','pe_sez(a)','Shivaraj K S,Kiran Kumar M,Kiran KM,','','0000-00-00','THICKNESS OVERSIZED NOMINAL MIN 0.14 AND MAX 0.16\r\nMEASURED 0.1640','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','With Treatment','','FI','no','Slim3n-5AHS-1','qas_sez(a)','no','','|New tool added after continue the production.','Z3456','pe_sez|qas_sez|qas_sez|','2018-09-29|2018-10-11|2018-10-11|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11047,'51-027','THE BOEING COMPANY','BRACKET','258462B1','149A7371-945','','PSDL REV A',9,'BOEING 001E','','79939','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','THICKNESS OVERSIZED NOMINAL MIN 0.14 AND MAX 0.16\r\nMEASURED 0.1640','While part running time operator not observe the tool.|The finishing tool already so many parts are running.','|Inform to the operator every part completed time check the part thickness mandatory.','|Inform to the operator every part completed time check the part thickness mandatory. ','Rework done and inspected all quantities parts found within acceptable tolerance limits.','','2018-08-27','pe_sez(a)','Kiran Kumar M,','','0000-00-00','THICKNESS OVER SIZE MIN 0.1400 AND MAX 0.1600 MEASURED 0.1632/0.1640','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','With Treatment','','FI','no','Slim3n-5AHS-1','qas_sez(a)','no','','|New tool added after continue the production. ','Z3456','pe_sez|qas_sez|qas_sez|','2018-09-29|2018-10-11|2018-10-11|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11048,'35-689','Saab AB','BRACKET','473615 C','D5227283320100','NA','PART ISSUE A',3,'OWED-LTA-004','','79756','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','part dig mark occurred','1.During running time tool was broken|2.Tool overhang occurred|3.Operator made mistake during tool load on holder','|Tool to be load on holder as per the data sheet','|Training to be given to the operator','CAPA FOUND OK','','2018-08-27','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Prashanth Kumar(M)','no','','|Suddenly machine was stopped and tool was loaded into holder correctly','E3456','pe|qas|','2018-12-19|2018-12-20|','2018-12-20',NULL,NULL,NULL,NULL,NULL,NULL),(11049,'35-644A','Saab AB','LATCH FORK','HR521404','D5227348920400','NA','PART ISSUE C',3,'OWED-LTA-004','','78566','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Bore over size by 0.020mm.\r\n','1) Bore oversized due to chip-off in the cutting edge of the reamer.\r\n|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.','|\r<br/>Informed the tooling supplier and purchased high grade reamers to withstand the machining conditions.\r<br/>','CAPA FOUND OK ','','2018-08-27','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Prashanth Kumar(M)','no','','|Immediately stopped the machine and changed the reamer tool and continued the production.','E3456','pe|qas|','2018-11-13|2018-11-19|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11050,'51-045','THE BOEING COMPANY','BRACKET','741161','149A7371-9611','','PSDL REV A',3,'BOEING 001F','','74298','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Parts received from treatment were found paint damage at the edges and corners.','This is happen during the transportation as there was no safety in the inner layer of the box in which the parts were shipped|parts were identified and segregated and the same was communicated to the treatment house','|Parts were done manual touch up as per the specification and found ok ','|Instruction was given to the treatment house on packaging to put extra kushan type of material surronding the inner layer of the box to avoid such paint damages during the transportation. ','Next Lot Received from the treatment supplier ,parts were checked and found visually acceptable to\r\nthe requirement ','','2018-08-27','pe_sez(a)','pe_sez(a)','','0000-00-00','PART MIX UP','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','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),(11051,'35-248','Saab AB','FILLER CENTERING 6-16','850836-07','423Z1466-1','','---',2,'Forecast po for B787','','77937','','0000-00-00',NULL,'yes','yes','yes','','','','','','','operation was shifted,new operator he couldn\'t observed trance value in x axis.','during operation machine maintenance massage will come,on that time running program in side added the trance value,that time make the external work offset zero. |after work offset zero we can start the same program.','|make sure the trance values and make it zero and run the program.','|starting and ending we will added the cancellation codes in trance value programs only.\r<br/>','Proper training to be given to the new operators before certifying to run the machine individually.','','2018-08-27','pe_sez(a)','        Kiran Kumar M','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','1','','','','','','|starting and ending we will added the cancellation codes in trance value programs only,and about the trance briefly we will explain the operator.','Z3456','pe_sez|pe_sez|pe_sez|qas|','2018-08-28|2018-08-28|2018-09-07|2018-10-12|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11052,'47-149','GKN Aerospace Filton','LWR ANGLE ATTACHMENT','560504A3','F57254364200','NA','PART ISSUE C',1,'1210042824','','80048','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Total length -1MM','wrong program selection|cross check the previous program |New corrected program given by CAD engineer after run the part','|communicate with CAD engineer and taken new program and run','|M00 and Message description given inside the program before run the program ','CAPA FOUND OK','','2018-08-28','Ravi nayak()','prodn_aero(prodn)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Ravi nayak()','no','','|cross check the previous program and new corrected program ','A3456','qas_aero|qas_aero|','2018-08-28|2018-09-06|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11053,'51A-079','THE BOEING COMPANY','ASSY - FTG, AFT FAIRING F','','112U7625-16','','PSDL REV-',1,'BOEING 001V','','K17407','','0000-00-00',NULL,'no','yes','yes','no','no','no','yes','no','no','Dent mark in BOI','Dent marked found on the BOI part.','|communication given to the supplier about the affected part.','|All the BOI will be inspected visually before taking for use.','CA PA found ok.','','2018-08-28','Ramesh(D)','Nithin(S)','','0000-00-00','Dent mark in BOI','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Assembly','','Stage','no','Misc','Ramesh(D)','no','A17371','|Immediately informed the BOI in charge and checked all the other BOI part and found ok.','E3456','qas|','2019-04-25|','2019-04-25',NULL,NULL,NULL,NULL,NULL,NULL),(11054,'18-105A','Magellan Aerospace Bournemouth',' 	FORKEND ASSEMBLY ','1626008-2/TNAD','PID572 50462 200','','J01',1,'428864','','79006','','0000-00-00',NULL,'yes','yes','yes','','','','','','','part running time Rotate...manual part tight by mistake   ','1) operator did not tightened the part properly.|2) Operator manually tightened the part on the bush by hand and loaded to the machine without completely tightening it.|3) Operator got confused as he was running two machines continuously.','|1) Informed all the operator to properly double check the tightness of the part before starting the cycle.\r<br/>2) Informed the operator to tight the bush to the part only by using spanner after guiding the bush inside the part manually for two threads.','|Comment included in the program to notify the operator to ensure proper tightness of the part before starting the cycle.','Comment included in the program and CAPA found ok.','','2018-08-29','Anjinamurthy(H)','        Kammar Nagaraj','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','07','','','','','','|Immediately stopped the machine and checked the previous completed parts and found ok.','E3456','pe|qas|qas|','2018-08-30|2018-09-04|2018-09-04|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11055,'35-531A','Saab AB','SHAFT LATCH','C90596','D5227349020200','NA','PART ISSUE C',3,'OWED-LTA-002','','75910','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','OD Under size 0.010mm to 0.020mm.','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. ','','2018-08-29','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','PRODUCTION','no','Misc','Manu(P)','no','','|\r\nImmediately stopped the machine and changed the wear offset and continued the production on the next part. ','E3456','pe|qas|','2018-10-26|2018-10-30|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11056,'35-466B','Saab AB','BUSHING','HR288202','D5227347420000','NA','PART ISSUE A',6,'OWED-LTA-005','','78322','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','OD Measures minus side.','1)OD Undersized -0.015mm beyond drawing limit.|2)OD undersized during the re-pass operation as the re-pass ran twice.|3)Re-pass ran twice with same -0.15 wear offset as the operator provided +0.2mm wear offset during the insert change.|4)To maintain stock in the ID after the insert change the operator provided -0.2mm in the initial stage and after measuring the diameter he provided -0.15mm to remove the stock and finish to the drawing requirement during this time the re-pass operation was carried out and resulted in diameter was undersized.|5)Operator was unaware that the program for OD runs twice with different stock levels to achieve finish in the final operation','|Changed the wear offset from +0.2mm to +0.1mm in the next part and after the completion changed the offset to -0.02mm according to the program(after considering both the pass) and found the next part OK.','|Informed all the operator to check the relevant features after the insert change and provide of the offset accordingly with proper guidance from the supervisor or senior operators.','Effectiveness found ok.','','2018-08-29','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','01','no','Misc','Dinakar(K)','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),(11057,'35-603A','Saab AB','OUTER HANDLE SHAFT','C86598.SSHF','D5227354020600','','PART ISSUE D',1,'OWED-LTA-004','','78374','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','od under size -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.|To maintain stock in the ID after the insert change the operator provided -0.2mm in the initial stage and after 4)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.','|1) 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. ','','2018-08-29','Sandhesh D(S)','Sathish(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','05','no','Misc','Sathish(G)','no','','|Immediately stopped the machine and changed the wear offset and continued the production on the next part. ','E3456','pe|qas|','2018-09-04|2018-09-05|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11058,'18-091A','Magellan Aerospace(Polska) Sp','BUSH','437671','PID278 50164 202','','A',2,'104569','','78328','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','od under size -0.015mm','1)OD Undersized -0.015mm beyond drawing limit.|2)OD undersized during the re-pass operation as the re-pass ran twice.|3)Re-pass ran twice with same -0.15 wear offset as the operator provided +0.2mm wear offset during the insert change.|4)To maintain stock in the ID after the insert change the operator provided -0.2mm in the initial stage and after measuring the diameter he provided -0.15mm to remove the stock and finish to the drawing requirement during this time the re-pass operation was carried out and resulted in diameter was undersized.|5)Operator was unaware that the program for OD runs twice with different stock levels to achieve finish in the final operation.','|Changed the wear offset from +0.2mm to +0.1mm in the next part and after the completion changed the offset to -0.02mm according to the program(after considering both the pass) and found the next part OK.','|Informed all the operator to check the relevant features after the insert change and provide of the offset accordingly with proper guidance from the supervisor or senior operators.','Effectivess Found ok','','2018-08-29','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','01','no','Misc','Ravi(M)','no','','|Immediately stopped the machine and changed the wear offset and continued the production on the next part.','E3456','pe|qas|','2018-09-04|2018-09-05|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11059,'35-577A','Saab AB','SHAFT','C84690','D5227344120000','NA','PART ISSUE B',1,'OWED-LTA-004','','78764','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','part thickness 0.2 -side.','Clamp not tight properly.|While tightening the bolt thread was damaged in fixture.|Fixture thread weakened.|Continuously tight and loosing of bolt every part .','|For the damaged fixture tread did drill and taped and putted a helical.','|Taking out of the clamps from the tread for every 10 part and checking the condition of the tread in the fixture .','CAPA found ok.','','2018-08-29','Subramanya L(Naik)','Yogesha K,Subramanya L Naik,CHETANA K,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','7','no','MakinoF5-4','Subramanya L(Naik)','no','','|Checked the all previous machined parts found OK. ','E3456','pe|qas|','2018-09-04|2018-09-04|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11060,'35-475A','Saab AB','FRAME ','528986A2','D5227338420100','NA','A',1,'PA1687 LTA-2','','73762','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Base thickness Under Size upto 0.1mm. Required 4 +/- 0.2mm, Measures 3.7mm.','improper part butting|part was bend during the finishing operation.|insufficient ageing time','|inform to operator for checking the proper butting by using feeler gauge before start the machining.','|inform to operator for checking the proper butting by using feeler gauge before start the machining.','CAPA Found OK','','2018-08-29','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','Misc','Manu(P)','no','','|Stop the machine & check all part cross checked found OK','E3456','pe|qas|','2018-12-18|2018-12-18|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11061,'35-260','Saab AB','SUPPORT_DEFLECT STOP','852182-13','423Z6190-4','','--A',14,'Forecast po for B787','','78686','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','BORE DIAMETER MAX 0.6380 AND MIN 0.6340.\r\nIN PART IT MEASURES OVER SIZE BY 0.0007 TO 0.001','Part Accepted|Part Accepted','|Part Accepted','|Part Accepted','Part Accepted','','2018-08-30','Rangaswamy()','Upendra N ,Thaveni D M ,Nagaraju P K ,Karthik Raj T ,HariPrasad ,','','0000-00-00','BORE DIAMETER MAX 0.6380 AND MIN 0.6340.\r\nIN PART IT MEASURES OVER SIZE BY 0.002 TO 0.003','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','With Treatment','','FI','no','a51nx-01','qas_sez(a)','no','','|Part Accepted','Z3456','pe_sez|qas|','2018-09-03|2018-09-04|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11062,'18-328B','Magellan Aerospace Wrexham','NUT ANCHOR','0422','D57251346200','NA','A',1,'175157','','80143','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','part wrong loading..','Wrongly loaded the part |top face loaded wrongly to bottom face |not observed top and bottom face |at the same time loading of the part to anther machine  |not concentration on fixture while butting the part ','|checking every part top and bottom side of the part  ','|mentioning the top and bottom side of the part by marked before butting  ','CAPA found ok.','','2018-08-30','Anjinamurthy(H)','Girish(MS)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Girish(MS)','no','','|checked all previews machined parts dimensions found are all  k   ','E3456','pe|qas|','2018-08-30|2018-09-04|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11063,'51A-074','THE BOEING COMPANY','BRACKET ASSY','','322U8810-8','','NIL',1,'BOEING 001Q','','A17834','','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','','2018-08-30','pe_sez(a)','qas_sez(a)','','0000-00-00','STEP FOUND ON PART','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Assembly','','FI','no','Misc','qas_sez(a)','no','','|Refer NC NO:10744','Z3456','qas_sez|','2019-01-16|','2019-01-16',NULL,NULL,NULL,NULL,NULL,NULL),(11064,'51-082','THE BOEING COMPANY','BRACKET DETAIL','659762','332A2930-2','NA','PSDL REV B',1,'BOEING 001M','','77325','','0000-00-00',NULL,'yes','no','no','no','no','yes','no','yes','no','BORE DIAMETER MAX 12.715 AND MEASURED BY 12.735','Cross check the CRC value in tool offset D value|Enter the correct CRC value in tool offset D value|Measure and ensure the Bore diameter value','|Enter the correct CRC value in tool offset D value ','|Before Run the Bore program Cross check the CRC value in tool offset D value and M00 MSG given inside the program multiple commands. ','Next batches produced found ok.','','2018-08-30','pe_sez(a)','Shivaraj K S,Kiran Kumar M,','','0000-00-00','BORE DIAMETER MAX 12.715 AND MEASURED BY 12.735','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','Slim3n-4AHS-2','qas_sez(a)','no','','|Previous part Bore value measured and ensure','Z3456','pe_sez|qas|','2018-10-12|2018-10-12|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11065,'35A-601','Saab AB','FRAME ASSY','','D5227338501000','','PART ISSUE C',12,'OWED-LTA-001','','A16222','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','yes','Sealant Application not done in fasteners.','Sealant is not visible on the part.|Very less amount of sealant applied during the assembly.|Miss-interpretation of standard requirements with respect to the electrical bonding.','|Received guidelines from customer on how to carry out the assembly and continued to carry out the assembly as per the customer given instructions.','|APS amended to incorporate the change in process and delta FAI for the same was carried out.','Delta FAI done and no similar escapements happened after the implementation of the corrective action.','C66406','2018-08-30','qas_sez(a)','qas_sez(a)','GLB387498','2018-07-24','NC','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER END','yes','Misc','qas_sez(a)','no','','|Immediately stopped the assembly and checked all the parts in FG and taken back for rework.','Z3456','qas|','2018-12-10|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11066,'35A-601','Saab AB','FRAME ASSY','','D5227338501000','','PART ISSUE C',6,'OWED-LTA-001','','A16223','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','yes','Sealant Application not done in fasteners.','Sealant is not visible on the part.|Very less amount of sealant applied during the assembly.|Miss-interpretation of standard requirements with respect to the electrical bonding.','|Received guidelines from customer on how to carry out the assembly and continued to carry out the assembly as per the customer given instructions.','|APS amended to incorporate the change in process and delta FAI for the same was carried out.','Delta FAI done and no similar escapements happened after the implementation of the corrective\r\naction.','C66406','2018-08-30','qas_sez(a)','qas_sez(a)','GLB387498','2018-07-24','nc','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER END','yes','Misc','qas_sez(a)','no','','|Immediately stopped the assembly and checked all the parts in FG and taken back for rework. ','Z3456','qas|','2018-12-10|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11067,'35A-601','Saab AB','FRAME ASSY','','D5227338501000','','PART ISSUE C',10,'OWED-LTA-001','','A16224','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','yes','Sealant Application not done in fasteners.','Sealant is not visible on the part.|Very less amount of sealant applied during the assembly.|Miss-interpretation of standard requirements with respect to the electrical bonding.','|Received guidelines from customer on how to carry out the assembly and continued to carry out the assembly as per the customer given instructions.','|APS amended to incorporate the change in process and delta FAI for the same was carried out.','Delta FAI done and no similar escapements happened after the implementation of the\r\ncorrective action. ','C66406','2018-08-30','qas_sez(a)','qas_sez(a)','GLB387498','2018-07-24','dn','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER END','yes','Misc','qas_sez(a)','no','','|Immediately stopped the assembly and checked all the parts in FG and taken back for rework.','Z3456','qas|','2018-12-10|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11068,'18-090A','Magellan Aerospace(Polska) Sp','BUSH','CD705189/03523A','PID278 50164 200','','A',11,'104569','','77978','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','OD UNDER SIZE.','OD Undersized -0.015mm beyond drawing limit.|OD undersized during the re-pass operation as the re-pass ran twice.|Re-pass ran twice with same -0.15 wear offset as the operator provided +0.2mm wear offset during the insert change.|To maintain stock in the ID after the insert change the operator provided -0.2mm in the initial stage and after measuring the diameter he provided -0.15mm to remove the stock and finish to the drawing requirement during this time the re-pass operation was carried out and resulted in diameter was undersized.|Operator was unaware that the program for OD runs twice with different stock levels to achieve finish in the final operation.','|Changed the wear offset from +0.2mm to +0.1mm in the next part and after the completion changed the offset to -0.02mm according to the program(after considering both the pass) and found the next part OK. ','|Informed all the operator to check the relevant features after the insert change and provide of the offset accordingly with proper guidance from the supervisor or senior operators. ','CA/PA Found ok.','','2018-08-31','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','03','no','Misc','Ravi(M)','no','','|Immediately stopped the machine and changed the wear offset and continued the production on the next part. ','E3456','pe|qas|','2018-09-19|2018-09-21|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11069,'28-052','Magellan Aerospace New York  Inc.','DIAPHRAGM / PART CLASS 2 ','9050401-1','55-3575004-00PUR','NA','NIL',40,'A000159331','','77904','','0000-00-00',NULL,'no','no','no','no','no','no','yes','yes','yes','PARTS RECEIVED WITH SCRATCHES, NICKS AND GOUGES ON EDGES MEASURING APPROX .25 LONG X .0600 WIDE. PARTS WILL BE REWORKED IN HOUSE TO SUPPORT PRODUCTION/DELIVERY.','Parts got damaged during transit due to no proper partision between one part and the other while packed inside the box.','|1) Additional Bubble wrap will be done all over the part-Refer Attachment 1.\r<br/>2) Center partition will be provided between the parts and will be closely packed to avoid movement of parts during transit- Refer Attachment 1.','|1) New packing method will be implemented from the next dispatches.','Next Batch shipments monitored and found ok.','C67755','2018-08-31','Nandishkumar(D.K.)','Narasimha Murthy(R)','NR# 115202','2018-08-30','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Manufacture Only','','Cust End','yes','Misc','Nandishkumar(D.K.)','no','','|1) Immediate stock check was carried out and we had 4 Nos in FG from CIM Work order 77909 which are free from defects as specified in the NR.\r\n2) Quality alert displayed in Production, Quality and Packing area to create awareness on the defect.','E3456','qas|','2019-02-15|','2019-02-15',NULL,NULL,NULL,NULL,NULL,NULL),(11070,'56-014','GKN Aerospace Orangeburg','FAIRING SUPPORT - AFT','BA61920','119A1521-604','NA','PSDL REV A',2,'LTA Orangeburg 737 W','','80119','','0000-00-00',NULL,'yes','no','yes','no','yes','no','no','no','no','3D FLANGE THICKNESS UNDER SIZE DUE TO PREVIOUS OPERATION MISTAKE ','THE OPERATOR MAINTAINED THE THICKNESS 0.7MM EXTRA.  |THE CORRECT DIA 32MM FACE MILL PROGRAM WAS SKIPPED IN THE MAZATROL SUB PROGRAM CALLING.|SAME NC PROGRAM WHICH HAVE 0.7MM EXTRA STOCK FOR PEND REMOVING PURPOSE IS KEPT IN MACHINE MEMORY SPACE. THIS NC PROGRAM ONLY RUN WHEN CALL THE MAZATROL SUB PROGRAM INSTEAD OF HARD DISK PROGRAM WHICH HAVE THE CORRECT NC PROGRAM ','|THE EXCESS PROGRAM IN MACHINE MEMORY AREA, DELETED. ONLY CURRENT RUNNING PROGRAMS ONLY KEPT IN MACHINE','|THE SAME NAME PROGRAMS NOT MAINTAIN IN MACHINE. THE REQUIREMENT NC PROGRAMS ARE ONLY IN MACHINE MEMORY','Machine application engineer visited and rectified the problem and no similar problems raised.','','2018-08-31','pe_sez(a)','NataRaj.CV ,Diwakar R.B.,','','0000-00-00','5 AXIS WALL UNDER SIZE','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','3','no','i700-2','pe_sez(a)','no','','|PRODUCTION STOPPED. INFORMED TO MACHINE APPLICATION   ENGINEER ','Z3456','pe_sez|qas|','2018-09-20|2018-10-12|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11071,'34-064A','Magellan Aerospace Winnipeg','PIN,SHEAR,ACCESS DOOR','429977','400-12748-1','NA','EM105092 Iss H,EM104765 Iss H',1,'C81597 Rev 001','','80427','','0000-00-00',NULL,'yes','yes','yes','','','','','','','THREAD  NOGO ANSWER  ....','1)Thread no go answering and dent observed during the first off part proving time.|2)Due to wrong Z-offset the tool crashed over the part during the first thread pass and due to which the part got bend and resulted in thread no go answering.|3)Operator was not aware of how to take the offset for this part.|4) Usually the offset were taken from the cutting edge of the threading insert but for this part the offset had to be taken from the face of the threading insert as there is very less space for relief after the end of the thread and the operator was not aware of that.','|Retaken the Z-offset for the threading insert from the insert face and continued the production and next part found ok.\r<br/>\r<br/>Instructed all the operators to take the Z-offset for this part from the face of the insert.','|Message included in the program stating “Take the Z-offset for the threading tool from the face of the insert”.','CAPA Found ok.','','2018-09-01','Dinakar(K)','        GUNDEGOWDA H.G.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','05','','','','','','|Immediately stopped the machine and retaken the z-Offset as per the supervisor guidance and continued the production.','E3456','pe|qas|qas|','2018-09-04|2018-09-06|2018-09-06|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11072,'35-588','Saab AB','LOCK SECTOR','532746C','D5227349920200','NA','PART ISSUE C',2,'PA1687 LTA-1','','73772','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Bore chatter mark absorbed on fine finish surface , 							\r\n','1.while boring operation running time coolant not present in boring tip.							\r\n|2.Adjust the coolant pipe direction to the boring tip.							\r\n|3.coolant supply not done properly so in the boring tip cutting edge to be clogged so bore on chatter							\r\n','|1.Adjust the coolant direction to the spindle. 							\r<br/>','|1.Training has to be conducted to all shift operators, effectiveness found ok 							\r<br/>','CA/PA satisfied','','2018-09-03','pe_sez(a)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','DN44528','POST TREATMENT','yes','Misc','Dharani(Shankar)','no','','|1.immediately stop the machine and check the all previous parts ,all parts found ok 							\r\n','Z3456','pe_sez|qas_sez|','2018-12-18|2019-01-18|','2019-01-18',NULL,NULL,NULL,NULL,NULL,NULL),(11073,'35-588','Saab AB','LOCK SECTOR','532747B','D5227349920200','NA','PART ISSUE C',7,'OWED-LTA-003','','76125','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Deep pit marks observed inside the bore near drill cone angle','•Parts might not be rinsed properly during the process\r\n.|•Parts might have contacted with other untreated / carbon steel parts','|A separated DM water connection pipe was provided to rinse the part correctly between the process','|Jigging method changed so as to the parts will rinsed thoroughly in between the process','Next batch found ok','','2018-09-03','pe_sez(a)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','DN44651','POST TREATMENT','no','Misc','Dharani(Shankar)','no','','|1.All the parts were checked 100% visually and found pits in some of the parts\r\n2.The non conforming parts was identified and NCR was raised\r\n3.Informed to the supplier regarding the issuse','Z3456','qas_sez|','2019-02-15|','2019-02-15',NULL,NULL,NULL,NULL,NULL,NULL),(11074,'35-588','Saab AB','LOCK SECTOR','533740C','D5227349920200','NA','PART ISSUE C',2,'PA1687 LTA-1','','73773','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Deep pit marks observed inside the bore near drill cone angle','•Parts might not be rinsed properly during the process\r\n.\r\n|•Parts might have contacted with other untreated / carbon steel parts','|A separated DM water connection pipe was provided to rinse the part correctly between the process','|Jigging method changed so as to the parts will rinsed thoroughly in between the process','Next batch found ok','','2018-09-03','pe_sez(a)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','DN44527','POST TREATMENT','no','Misc','Dharani(Shankar)','no','','|1.All the parts were checked 100% visually and found pits in some of the parts\r\n2.The non conforming parts was identified and NCR was raised\r\n3.Informed to the supplier regarding the issuse','Z3456','qas_sez|qas_sez|','2019-02-15|2019-02-15|','2019-02-15',NULL,NULL,NULL,NULL,NULL,NULL),(11075,'35-473B','Saab AB','LEVER CAM','C86484','D5227353720000','NA','PART ISSUE C',1,'OWED-LTA-003','','78369','','0000-00-00',NULL,'yes','no','yes','','yes','','','','','part hole shifted 3.5mm.','Machine y axis shifted.|Y axis drive battery weakened.  |This battery is used from 6 years.|Operator referenced the machine but not cross check the work offset.','|Replaced the battery and reset the y axis home position.the next part found OK.','|1) We will replace the battery every three years.\r<br/>2) we will Cross check the reference while machine OFF and ON. ','CA PA found ok.','','2018-09-03','Subramanya L(Naik)','        Subramanya L Naik','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','7','','','','','','|Checked the previous machined parts found OK.   ','E3456','pe|pe|qas|','2018-09-05|2018-09-08|2018-09-11|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11076,'18-416A','Magellan Aerospace(Blackpool) Limited','BRACKET','263954/1951','PI55-2119004-00','','NIL',1,'BPP-533300','','79175','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Base thickness - side (-2.00mm). 		','Operator not part butting properly.			\r\n','|5nos continuous checking found ok. 			','|Training to operator in front of machine. 		\r<br/>','CA/PA found satisfactory. ','','2018-09-04','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','05','no','Misc','Prashanth Kumar(M)','no','','|Inform to supervisor and taken guidance then run production. 							\r\n','E3456','pe|nandishkumardk|','2018-11-07|2018-11-27|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11077,'35-525A','Saab AB','ROD BODY','34778216-B','D5227333620000','NA','PART ISSUE B',1,'OWED-LTA-005','','78231','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Total length undersized(-1.5mm).','Total length undersized|Multiple passes were performed on the finished parts itself.|Re-loading of the finished part|The finished part under gone all the operations again and in the final operation where the total length is maintained then total length got under sized. ','|1.Before loading the part the operator should ensure the total length.\r<br/>2.Training and instructions are give to the operators.','|1.Separation of finished parts and semi finished parts are done.\r<br/>2.Identification of Finished and Semi-finished parts are done by using separate trays.','CAPA found ok.','','2018-09-04','Dinakar K()','Dinakar K()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','05','no','Misc','Dinakar K()','no','','|Checked the previous machined parts found ok.\r\n','Z3456','pe|qas|','2018-10-23|2018-10-30|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11078,'35-288','Saab AB','BEAM FITTING','245884B2','424Z1140-2','','--B',1,'Forecast po for B787','','77756','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Part not tighten properly due to over length bolt','Bolt not tighten properly|Use of lengethy bolt|Did not notice the length of bolt while tightening|Not lifted the part be before running the programme|And also didnot check the part with feeler gauge','Used the correct length bolt ','Checked the part with a feeler gauge and also inform all operator about this problem','CAPA FOUND OK','','2018-09-04','Dinesh kulal()','Vinod.K(V)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','2','no','Misc','Dinesh kulal()','no','','Increased the depth of healical in fixture','A3456','qas_aero|','2018-10-11|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11079,'35-650A','Saab AB','SHAFT','C87212','D5227346820200','NA','PART ISSUE C',2,'PA1687 LTA-2','','75885','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Part send to ATPL for ZINC NICKEL plating (Trail).','Trail for ZINC NICKEL plating to ATPL.','|Trail for ZINC NICKEL plating to ATPL.','|Trail for ZINC NICKEL plating to ATPL.','reject.','','2018-09-05','qas_sez(a)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','DN42779','POST DN','no','Misc','qas_sez(a)','no','','|Trail for ZINC NICKEL plating to ATPL.','Z3456','qas_SEZ|','2018-09-05|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11080,'18-003A','Magellan Aerospace Wrexham','BRACKET SUPPORT','5162301 1','D361 50111 200','ABM3 1029 T7651','A',1,'175151','','77400','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Outer profile dig mark UP TO 3MM.','part lifted one side.|clamp not tightened properly.','|clamp the part properly and cross check the tight and run.','|guide lines given to operator after loading the part cross check part clamp if tightened or not and the run. ','CAPA found OK','','2018-09-05','prodn_aero(prodn)','prodn_aero(prodn)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','Fitting','no','Misc','prodn_aero(prodn)','no','','|cross check the clamp tight.','A3456','qas_aero|','2018-10-26|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11081,'28-007A','Magellan Aerospace New York  Inc.','Shaft Support Lever','H7B35/136410','251A1747-1','Ti-6AL-4V Per Mil-T-','N/C',3,'A000152175','','78224','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Dummy ','Dummy','|Dummy','|Dummy','Dummy','','2018-09-06','Ravi(M)','Sunil Gowda B N,Sudhakar C.M,Santhosh Kumar N,Sandhesh D S,Raghavendra P,KRISHNAMURTHY N,Dinakar K,Ashoka R,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','With Treatment','','FI','no','QT100S-1','Nandishkumar(D.K.)','no','','|Dummy','E3456','qas|qas|','2018-09-06|2018-09-06|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11082,'18-098B','Magellan Aerospace Bournemouth','VALVE- SEAT','23719486','D282 50060 204','','D',1,'423241','','74227','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','one number found deep step on the profile(0.6-1mm)after treatment','The part was missed during the inspection and the same was dispatched to treatment.|Inspector didnt notice the step during inspection.','|Training will planned and given to all the inspectors on the visual inspection requirements like dent ,scratches and other defects','|Refer to CA','Wo #79558 was checked by the inspector and the same was validated by head QAD for visual requirements and found OK','','2018-09-06','pe_sez(a)','S. Shiva Kumar,Punith G S,Narasimhamurthy C,Kammar Nagaraj,Girish HP,dharshan d,Dhananjaya N,BHUVANAPRAKASH  J.S,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','DN45039','FI','yes','BMV 60-1','Manu(CR)','no','','|The part was identified at the inward  after treatment and informed to the Head QAD.\r\n','Z3456','qas_sez|','2019-04-12|','2019-04-12',NULL,NULL,NULL,NULL,NULL,NULL),(11083,'18-419A','Magellan Aerospace(Blackpool) Limited','BRACKET','C0201787644/33745977','PI55-2120010-00','','NIL',12,'BPP-533304','','80721','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','SPOT SPACE OPERATION missing.','Part with incomplete operations sent to final inspection.							\r\n|The part was separated for rework.		\r\n|The spot face not missing. operator separated the part and did not informed the supervisor.			\r\n|The operator missed to communicate due to work priorities.			\r\n','|Part was again loaded to the machine and the facing operation was completed. 						\r<br/>','|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/>\r<br/>2) Informed the operator to carry out visual inspection of all the parts placing together at the end of every setup. 							\r<br/>','CA PA FOUND SATISFACTORY.','','2018-09-08','Dhananjaya(N)','Dhananjaya(N)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','Manufacture Only','','FI','no','Misc','Narasimha Murthy(R)','no','','|Informed all the operators to identify the rework parts with identification tag. 					\r\n','E3456','pe|qas|','2018-09-12|2018-09-12|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11084,'35-261','Saab AB','RODEND','G24288K02','424Z3411-2','','--B',3,'Forecast po for B787','','76656','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Thread damage on the parts','In this part re taping time thread dig mark observed |while doing OD drill thread gauge not answer properly so re tap done on every part ,  |chips clogging the tap gauge so manually rotate the tap ,on that time thread damage found |Tap condition will check on next batches ,|Ensure all the parts threads Correctly ','|1.while doing re-taping lubrication oil and chips cleaned by using air. ','|1.inform to fitting and turning department check and ensure the threads gauge properly, ','CAPA found ok.','','2018-09-08','Gurukiran S(M)','Sudhakar C.M,MANJE GOWDA S,KIRAN  M V,Ashoka R,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','QT100S-1','Nagendra(SN)','no','','|1.check the tap threads on every batch while doing re tapping .\r\n2.Guide the fitting operator while doing re taping. ','E3456','pe|qas|','2018-09-08|2018-09-14|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11085,'18-438B','Magellan Aerospace(Blackpool) Limited','MANIFOLD ','263901 1427','PI55-1213031-00','NA','NIL',1,'Bpp-529619 amed-2','','77364','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','DIG mark observed on part hole.','FAI Part proving time drill broken so part hole dig mark observed |Drill length 265mm long so while proving time broken  |RPM and feed will constant for the part hole drills|Pre drill program provided on on this type of operation.|parameter not stetted on the long drill ','1.IN this special cases long drills proving on a dummy materials.','1.In side program tool length mentioned and MSG ,will given on particular program\r<br/> \r<br/>\r<br/>','CA/PA Found satisfactory.','','2018-09-08','Gurukiran S(M)','ABHISHEK(M G)','','0000-00-00','Part hole dig mark ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','03','no','Misc','Gurukiran S(M)','no','','1.Given a training for operator while proving on FAI parts carefully.\r\n ','E3456','nandishkumardk|nandishkumardk|','2018-09-08|2018-09-08|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11086,'47-111A','GKN Aerospace Filton','CTR BTM LUG MACHINED','1140401 2','D57550246200','NA','PART ISSUE A',6,'GS68-LTA-2018','','79127','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','THICKNESS UNDERSIZE REQUIRED 11.10/11.35 MEASURING 10.92/11.05\r\nTHICKNESS UNDERSIZE REQUIRED 3.8/4.30 MEASURES 3.55/3.80','This part identified in final inspection.|Annalise the reason of rejection. |1)Part not proper clamping.|2)Not cleaning the butting area.|3)operator setting time \"B\" axis offset wrong taken.or fixture top face dialing not done.','|Next batch Annalise. ','|Next batch Annalise. ','Exact root cause not identified yet analysis will be done during the next batch production.','','2018-09-11','Rangaswamy()','Nagaraju P K ,Karthik Raj T ,HariPrasad ,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','a51nx-06','qas_sez(a)','no','','|Inform to operator last batch 6no rejection identified in final inspection.\r\n','Z3456','pe_sez|qas|','2018-09-17|2018-09-24|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11087,'18-090A','Magellan Aerospace(Polska) Sp','BUSH','CD705189/03523A','PID278 50164 200','','A',19,'104569','','79548','','0000-00-00',NULL,'yes','yes','yes','no','no','no','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.','|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.','','2018-09-11','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','03','no','Misc','Seetharamu(D)','no','','|Immediately stopped the machine and changed the wear offset and continued the production on the next part. ','E3456','pe|qas|','2018-09-19|2018-09-21|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11088,'35-455A','Saab AB','BRACKET ','LL0100697','D5227345720000','NA','PART ISSUE A',1,'OWED-LTA-005','','80586','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','part outer profile unclear.','Chattering on the part profile occurred during the roughing operation.\r\n|Screw used to lock the insert got loosed during the machining operation.\r\n|The head of the align key used to tight the insert screw was blunt because of which the insert got loosed during the machining and affected the profile','|Informed all the operator to check the align key head before taking to use.\r<br/>','|Scrapped all the old and worn out align keys','CAPA found ok','','2018-09-11','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','1','no','Misc','Subramanya L(Naik)','no','','|Immediately stopped the machine checked the previous parts and changed the align key and re-tighten the screw and continued the production.\r\n','E3456','pe|qas|qas|','2018-12-17|2018-12-19|2018-12-20|','2018-12-20',NULL,NULL,NULL,NULL,NULL,NULL),(11089,'35-604','Saab AB','SHAFT , VENT HOOKS','2878','D5227352920200','NA','PART ISSUE B',1,'PA1687 LTA-1','','79731','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','OD Undersized by 0.015mm.','1.OD under sized due over pressure in tail stock,as the pressure was given was 2BAR\'s.|2.The min. pressure in the new machine\'s is 1BAR, but in the old machines it was 0.5BAR.  |3.Due to over pressure the part had bent,the operator was not having the knowledge about the pressure that had to be given to the tail stock. |4.After the part had bent the OD operation was performed and the OD was achieved,but after removing the part from the chuck and measured it again the OD was undersized by 0.015mm. |Why 5: Usually the tail stock pressure maintained was 1.5bar but in the new machine the pressure was varying 1bar, 2bar, 3bar,etc. therefore the operator got confused and provided 2bar pressure to avoid rotation of the part during machining.','|Reduced the tail stock pressure from 2BAR\'s to 1BAR. |1) Reduced the Tail Sock pressure from 2bar to 1bar as per the guidance of Mazak application engineer.','|1.Training will be given to the operators about the machine and its accessories.  \r<br/>2.Reduced the tail stock pressure.\r<br/>3.Message has been provided in the program.|1) Alert message included in the program to maintain the tail stock pressure at 1bar.\r<br/>2) In future after the installation of new machine all the machine specifications will be clarified on spot from the concern application engineer.','CAPA found Ok.','','2018-09-12','Dinakar K()','Dinakar K()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Dinakar K()','no','','|Contacted the Mazak machine person and the guidance given by them is followed. |Contacted the Mazak machine application engineer about the tail stock pressure setting method and followed the same and next part produced found ok.','Z3456','pe_sez|qas|qas|','2018-09-12|2018-09-12|2018-09-12|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11090,'18-395A','Magellan Aerospace Bournemouth','VALVE','182613/J9HJ','A284 40012 200','','A',1,'423233','','74288','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Carrosion observed on od','Part has undergone secondary process along with the corrosion pits. |Corrosion was not identified at the initial stage|Poor visual Inspection.|Sufficient light source was not used by the inspector. ','|Awareness was given to the inspector to carry out the visual inspection in good lightining area minimum 1200 lux .\r<br/>2.Good lightining will be provided for visual inspection table.','|Refer to CA','CAPA found Satisfactory','','2018-09-12','qas_sez(a)','Dinakar K,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','DN45483','FI','no','DX 200-3','Manu(CR)','no','','|The parts was rejected after treatment and NCR was raised','Z3456','pe|qas_sez|','2018-09-14|2019-04-12|','2019-04-12',NULL,NULL,NULL,NULL,NULL,NULL),(11091,'47-071','GKN Aerospace Filton','BUSH FLANGED ','1401574880','F575 54095 200 01','','A',4,'LTA-GKN-002','','62936','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','BUSHES HAVE BEEN PRODUCED MEASURING 12,VMM ON BORE COMPLETE TO DRAWING CONDITION OF SUPPLY STATES TO BUSHES TO BE SUPPLIED UNDERSIZE TO ALLOW FOR JIG BORING POST ASSEMBLY BORE SHOULD MEASURE 11,900 - 11.950MM1 BUSH IS DAMAGED AS HAS BEEN FITTED AND REMOVED FROM RIB BORE STILL MEASURABLE AT 12,7MM.','Due to improper handling of non conforming parts the rejected parts got mixed up with the finished parts and got shipped to customer.','|Informed all the individuals to identify the parts with proper rejection tag and move to the designated area immediately.','|Separate colored tag\'s are made red color for rejection white color for quarantine and yellow color for rework.','CAPA found ok.','C66880','2018-09-12','Nandishkumar(D.K.)','qas(qas)','201134605','2018-08-17','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','DN32302','Cust End','no','Misc','qas(qas)','no','','|Immediately carried out 100% stock check and no similar mix up of parts identified.','E3456','qas|','2019-01-10|','2019-01-10',NULL,NULL,NULL,NULL,NULL,NULL),(11092,'18-102A','Magellan Aerospace Bournemouth','BARREL-STRUT','CD703435/06400A','PID572 50463 200','','F',1,'423256','','74386','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Carrosion observed on part','Part has undergone secondary process along with the corrosion pits. |Corrosion was not identified at the initial stage|Poor visual Inspection.|Sufficient light source was not used by the inspector. ','|\r<br/>Awareness was given to the inspector to carry out the visual inspection in good lightining area minimum 1200 lux .\r<br/>2.Good lightining will be provided for visual inspection table. ','|Refer to CA ','\r\nCAPA found Satisfactory\r\n	\r\n	','','2018-09-14','qas_sez(a)','S. Shiva Kumar,Rakesh  KC,KRISHNAMURTHY N,Girish HP,Dinakar K,BHUVANAPRAKASH  J.S,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','DN45137','FI','no','DX 200-2 ','Manu(CR)','no','','|The parts was rejected after treatment and NCR was raised ','Z3456','qas_sez|','2019-04-12|','2019-04-12',NULL,NULL,NULL,NULL,NULL,NULL),(11093,'35-644A','Saab AB','LATCH FORK','HR521404','D5227348920400','NA','PART ISSUE C',1,'OWED-LTA-004','','79749','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Bore over size by 0.020mm.\r\n','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 ','','2018-09-14','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','5','no','Misc','Subramanya L(Naik)','no','','|Immediately stopped the machine and changed the reamer tool and continued the production.','E3456','pe|qas|','2018-11-13|2018-11-19|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11094,'47-071','GKN Aerospace Filton','BUSH FLANGED ','10074680055','F575 54095 200 01','','A',4,'LTA-GKN-002','','62544','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','no','PART REJECTED DUE TO BORE OVER SIZE 0.8 MM','Due to improper handling of non conforming parts the rejected parts got mixed up with the finished parts and got shipped to customer.','|Informed all the individuals to identify the parts with proper rejection tag and move to the designated area immediately','|Separate colored tag\'s are made red color for rejection white color for quarantine and yellow color for rework.','CAPA found ok.','','2018-09-14','Nandishkumar(D.K.)','Nandishkumar(D.K.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','ONSITE','no','Misc','Nandishkumar(D.K.)','yes','','|Immediately carried out 100% stock check and no similar mix up of parts identified. ','E3456','qas|','2019-01-10|','2019-01-10',NULL,NULL,NULL,NULL,NULL,NULL),(11095,'47-071','GKN Aerospace Filton','BUSH FLANGED ','10074680055','F575 54095 200 01','','A',1,'1210038562 Amnd 1','','62537','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','no','BORE OVER SIZE BY 0.8MM','Wrong drawing Interpretation.\r\nBORE SHOULD MEASURE 11,900 - 11.950MM|1.Parts checked  in QAD as per Drawing and COS not referred(Model not shared from customer since it is a drawing master part)\r\n2.Wrong drawing interpretation.\r\n|1.Parts Mnufactured by Engineering without referring COS.|CONDITION OF SUPPLY STATES TO BUSHES TO BE SUPPLIED UNDERSIZE TO ALLOW\r\nFOR JIG BORING POST ASSEMBLY','|1.Awareness created among Engineering and QAD to red the COS along with drawings as COS superseeds drawing when specifically noted.','|1.Complete drawing set to be referred in Fairs starting from picture sheet to Engineering change note.','CAPA FOUND OK','','2018-09-14','Nandishkumar(D.K.)','Nandishkumar(D.K.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','ONSITE','no','Misc','Nandishkumar(D.K.)','yes','','|COS referred after some partial quantities manufactured.\r\nparts under process are again re-verified to COS dimension','E3456','qas|qas|qas|','2018-09-17|2018-09-17|2018-09-19|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11096,'35-686A','Saab AB','LEVER','509667C','D5227353620400','NA','PART ISSUE D',1,'OWED-LTA-005','','80922','','0000-00-00',NULL,'yes','no','no','no','no','yes','no','yes','no','Refer NC NO:10744','Refer NC NO:10744','|Refer NC NO:10744','|Refer NC NO:10744','Refer NC NO:10744','','2018-09-14','pe_sez(a)','pe_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','Misc','Manu()','no','','|Refer NC NO:10744','Z3456','qas_sez|','2019-01-16|','2019-01-16',NULL,NULL,NULL,NULL,NULL,NULL),(11097,'18-104A','Magellan Aerospace Bournemouth','BODY TURNBUCKLE ','A0780Z','PID575 40490 200','','E',1,'428863','','78671','','0000-00-00',NULL,'yes','yes','yes','','','','','','','tool offset wrong taken so part will be rejected','1) Part rejected during the first off part proving time due to wrong work offset calculation.|2) Tool offset need to be calculated from the machine bed and the rotary center need to be incremented and made zero but the operator made the machine bed as zero without increasing the rotary center.|3) Operator did not concentrated on the calculation and did not rechecked the offset values before running the part.|4) Operator was not aware of the offset crosschecking procedure.','|1) Under the supervision of the senior operator the work offset of the tools was changed and the production was continued and the next part found ok.\r<br/>2) Instructed all the operators to cross check the offset value before starting the production.','|1) Practical training of calculating the work offset was given to the new operator by the senior operator.\r<br/>2) New operators will be monitored till proper training effectiveness is measured.','CAPA found ok.','','2018-09-15','Anjinamurthy(H)','        BHUVANAPRAKASH  J.S','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','5','','','','','','|Immediately stopped the machine and with the help of senior operator cross checked the offset value of all the tools and entered the correct offset.','E3456','pe||qas|','2018-09-15|2018-09-16|2018-09-16|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11098,'35-687A','Saab AB','LEVER','509667C','D5227353620500','NA','PART ISSUE D',1,'OWED-LTA-005','','80924','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Dia 22.225H8 No Go Answered(Approximately +0.02 Over Sized). ','why1. During rib top profile milling operation excess amount of material removed top surface due to that which was getting undersized\r\n|why2. The tool on Z axis direction moved into downwards\r\n|why3. The chips were blocked on ATC before loaded into tool holder due to that tool height Z value changed\r\n|why4. The empty pockets are available on machine during milling operation chips flowed on the empty pockets\r\n|why5. Due to that chips blocking on ATC tool downwards occurred on Z axis','|All ATC pockets to be filled with tool holders and that to be avoid chips blocking on ATC pockets.\r<br/>After every roughing cycle operation operator needs to be clean the tool pocket.','|Install chips guard to prevent chips from entering inside the tool pocket ','CAPA found ok','','2018-09-15','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','DN46243','Production','no','Misc','Manu(P)','no','','|The tool holder is removed and the chips were cleaned and the remaining parts checked and ensured ok','E3456','pe|qas|','2018-12-17|2018-12-19|','2018-12-19',NULL,NULL,NULL,NULL,NULL,NULL),(11099,'18-296B','Magellan Aerospace Bournemouth','PIN GUIDE ','B000077382','PIL575 52882 200','','B00',8,'428872','','80935','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1) 4 no\'S 10.446mm to 10.464mm OD measures 10.522mm to 10.474mm.(OD Oversize)\r\n2) 8 No\'s 0.5*45 degree chamfer measures 0.25*45 degree.(Chamfer Under size)','1.Diameter oversize occurred on edge\r\n2.During turning operation part shift occurred in back side|1.During turning operation burr fold occurred\r\n2.The back side empty space is there|1.That burr was not removed\r\n2.Due to that part is moved to back during tool to part approach time|1.Due to that edges Diameter shows oversize\r\n2.Due to that chamfer under size occurred','|1.During turning operation after completion of the operation the edge burrs are removed in machining itself\r<br/>2.The back stopper is implemented due to that part wont to be ship in to back','|1.During turning operation after completion of the operation the edge burrs are removed in machining itself\r<br/>2.The back stopper is implemented due to that part wont to be ship in to back','','','2018-09-15','Ravi(M)','Vasu SN,Ravi M,Ashoka R,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','','FI','yes','QT100S-1','Narasimha Murthy(R)','no','','|The parts in FG, WIP is checked, that is not available.','E3456','qas|','2018-09-21|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11100,'18-296B','Magellan Aerospace Bournemouth','PIN GUIDE ','B000077382','PIL575 52882 200','','B00',1,'428872','','77261','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','thread no go answering.','DURING INSERT CHANGE WRONG DATA ENTRY OCCURRED ON X OFFSET. |LAST INSERT CHIP OFF OCCURRED DUE TO THAT NEW INSERT LOADED,DURING THAT TIME X OFFSET WRONG ENTERED.|DUE TO THAT INITIAL FOUR THREAD NO GO ANSWERED.','|TRAINING GIVEN TO THE OPERATORS.','|TRAINING GIVEN TO THE OPERATORS.','CAPA found ok.','','2018-09-15','Ravi(M)','Ravi M,Kammar Nagaraj,Ashoka R,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','QT100S-1','Narasimha Murthy(R)','no','','|THE THREADING OPERATION COMPLETED PARTS ARE ENSURED OK AND THEN X OFFSET TAKEN CORRECTLY.','E3456','pe|qas|','2018-09-17|2018-09-21|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11101,'35A-601','Saab AB','FRAME ASSY','','D5227338501000','','PART ISSUE C',1,'1600214688','','A18518','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','counter shunk holes over size','1) Due to manual countersink formation the depth of tool increased.|2) The depth was controlled manually.','|Informed the operator to use a rivet to check the depth required on each and every step.','|Purchased a fixed drilling machine and standard CSK tool to control he depth and to achieve proper CSK formation.','CA PA found ok.','','2018-09-15','Ramesh(D)','Nithin(S)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Assembly','','1','no','Misc','Ramesh(D)','no','','|Immediately stopped the operation and informed the supervisor.','E3456','qas|','2019-04-25|','2019-04-25',NULL,NULL,NULL,NULL,NULL,NULL),(11102,'35-671','Saab AB','SHAFT LEVER ','521026A2','D5227346221800','NA','PART ISSUE D',1,'OWED-LTA-001','','80478','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Inner diameter was getting over size up to dia 11.70mm ins ted of dia11.20 -0.1mm','1) During turning operation part twisted from jaws.               |2)Due low presser on jaws.  |3)part shaft wall thickness is low due to that low presser given.|4)jaws id diameter and part Od diameter in mismatch occurred.|5)SO machining method was wrong.','|The correct dia jaws to be use to machining the part.|The correct dia jaws to be use to machining the part.|The correct Dia jaws to be use to machining the part.','|The correct dia jaws to be use to machining the part.|The correct dia jaws to be use to machining the part.|The correct Dia jaws to be use to machining the part.|1) Instructed all the operator to select suitable jaws based on the part to be hold and also instructed to get support from supervisor or senior operator while selecting the jaws. ','CAPA found ok.','','2018-09-16','Sandhesh D(S)','Venkatesh(S)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','11','no','Misc','Raghavendra Rao(R)','no','','|The machine was stopped and the jaws diameter maintained as per the part od diameter and the remaining parts machining started.|The machine was stopped and the jaws diameter maintained as per the part od diameter and the remaining parts machining started.|The machine was stopped and the jaws diameter maintained as per the part Od diameter and the remaining parts machining started.','E3456','|||qas|qas|','2018-09-16|2018-09-16|2018-09-16|2018-09-16|2018-09-21|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11103,'56-014','GKN Aerospace Orangeburg','FAIRING SUPPORT - AFT','BA61920','119A1521-604','NA','PSDL REV A',2,'LTA Orangeburg 737 W','','80119','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','PART HOLE DRILLING TIME  DRILL CUTTING EDGE BROKEN, DAMAGE THE HOLE SHAPE','THE BURR NOT COME OUT WHEN DRILLING TIME|ITS A COMBINATIONS TOOL. DIA 2.55MM DRILL AND DIA 6*100 DEG COUNTER SINK  MADE TOGETHER IN A SINGLE SHANK. ','|THE NEW COMBINATION TOOL REPLACED. THE CHIP AND COOLANT FLOW MONITORING DONE.  ','|BEFORE LOAD OR USE THE CUTTING TOOL, THE GEOMETRY OF THE CUTTING TOOL ONCE ENSURED IN ZOLLER MACHINE. THE SHANK DIAMETER ALSO WILL BE CONSIDER WHEN CUTTING TOOL OVER HANG IS MORE.  ','Trough coolant drill is ordered and to be replaced for the existing drill.','','2018-09-17','pe_sez(a)','Umesh B,Nataraja C V,NataRaj.CV ,Diwakar R.B.,','','0000-00-00','DRILL BROKEN','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','9','no','i700-2','pe_sez(a)','no','','|DRILLING OPERATION STOPPED. ','Z3456','pe_sez|qas|','2018-09-25|2018-10-12|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11104,'18-737A','Magellan Aerospace Wrexham','A/NUT STRIP','63026/02','F57250047200','NA','A',3,'176541','','78514','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','PROFILE DIG MARK.','1)Part improperly butted on the vice.		\r\n|2)Operator did not ensured the proper butting of part during loading.							\r\n','|Instruction given to all operators in the proper loading of part during the first setup operation.			\r<br/>','| Additional profile program was included to mark the profile on the part by removing minimum thickness to ensure correct loading of the part before starting the cycle							\r<br/>','Next batch found Ok.','','2018-09-17','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','1','no','Misc','Dhananjaya(N)','no','','|Machine was stopped and instructions given to the operator regarding the specific part loading on machine							\r\n|All previously machined Parts are cross checked & found ok','E3456','pe|qas|','2018-11-07|2018-11-12|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11105,'18-030A','Magellan Aerospace(Polska) Sp','PIN','1610732-3/SWTG','D278 50156 200','S130 FHT','A',1,'104569','','79562','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','NO EVIDENCE FOUND FOR HARDNESS TEST ON THE PART.','100% process not done by the supplier |100% inspection not done by the supplier |parts were mixed during processing |separate bins were not available for process completed and under process','|1.Informed to the supplier regarding the issues and the NCR was shared to to supplier\r<br/>Input by the supplier\r<br/>2.Supplier has informed to bi forget the routing like processed parts separate bins and WIP in separate bind','|Input by the supplier\r<br/>separate bins were in place for process completed and under process so as to avoid the mix up','DN46559 (283),nos received from the supplier and inspected and found all parts hardness test were done.','','2018-09-18','op_sez(s)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','DN45619','POST TREATMENT','yes','Misc','Dharani(Shankar)','no','','|1.100% inspection visual inspection done and found 1 no have no evidence for hardness test\r\n2.The defected part was identified with the rejected tag\r\n3.NC raised and sent to the supplier','Z3456','qas_sez|','2019-01-06|','2019-01-06',NULL,NULL,NULL,NULL,NULL,NULL),(11106,'18-333B','Magellan Aerospace Bournemouth','PLATE COVER','0513402','PID282 50280 200','','A',1,'428873','','78141','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Tool offset wrong.','1) Tool offset measured and entered wrong.|2) Operator did not measured the tool offset properly and noted the wrong reading.|3) The reference plane picked by the operator during the tool offset measurement was wrong for the first time and the second time he measured correctly but entered the first time reading to the machine.|4) operator confused with the readings noted in the log book as he had noted both the correct and wrong readings in the same log book.','|Re-measured the tool offset under the supervision of senior operator and entered the correct reading to the machine and continued production.','|1)Informed all the operator to cross check the tool offset by making the standard block zero on the height gauge and then measure the tool length.\r<br/>2) informed all the operators to cross check the offset value inserted to the machine is the same as the reading noted in the book and informed the operators to not to wright multiple measurements for the same tool in the same log book.','CAPA found ok Operator effectiveness need to be measured.','','2018-09-18','Anjinamurthy(H)','        Paramaeshappa ','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','03','','','','','','|Ensured offset of all the other tools loaded and corrected the defective offsets.','E3456','pe|qas|qas|','2018-09-20|2018-09-27|2018-09-27|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11107,'18-329A','Magellan Aerospace Wrexham','FLANGE MACHINED ','27589015','F282 50078 200','','A',1,'175157','','79853','','0000-00-00',NULL,'yes','no','no','no','yes','yes','no','no','no','Drawing dimension required 15+/-0.3 mm measured 14.20 mm.','Total Length under-size.|After the completion of machining the operator observed that the face was not cleared and then separated the part and stored without identification. The next shift operator without knowing the issue loaded the part to the machine and continued the next operation.|Lack of awareness on the need of identification and traceability and improper communication between operators during shift Change.','|Informed all the operator to provide proper updates to the next shift operator during the relieving time and to identify the deviated parts with proper tag and inform the supervisor about the deviation immediately after the identification of the defect.','|1) Provide proper training on the need of identification and traceability to the operator.\r<br/>2) Operator to mention all the discrepancies and deviations observed, reworked or identified in the production entry log book which is maintained near the machine. ','capa found ok','','2018-09-19','Dinakar(K)','SHIVAKUMAR ,Seetharamu D,S. Shiva Kumar,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','0','FI','no','ST20','Nandishkumar(D.K.)','no','','|Immediately checked the total length of all the other parts and found ok.','E3456','qas|qas|','2018-09-28|2018-11-28|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11108,'18-121A','Magellan Aerospace Bournemouth','BARREL - STRUT','CD703435/06400A','PID572 50463 201','','F',1,'428863','','79578','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','HOLE OVER SIZE BY 0.12MM.','Running time drill chip off . |This tool was run previous batch production but tool was good.  ','|Replaced the new tool.','|Dia 4.5 Pre drill done before 4.93 hole finish .','Tool Life to be monitored CAPA found ok.','','2018-09-22','Subramanya L(Naik)','Sunil G S,Sundar D.K.,Shivappa M B,Mohan Trishul D P,Dinakar K,Arun Kumar R,Anil S,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','FI','no','BMV 45-1','Narasimha Murthy(R)','no','','|Checked the previews machined parts.','E3456','pe|qas|','2018-09-24|2018-10-01|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11109,'35-576','Saab AB','BRACKET','532729C','D5227343420000','NA','PART ISSUE A',1,'1600217568','','80330','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','While machining tools broken so part dig.','Tool wear out and got broken.|Tool wear life was not properly monitored and no proper tool standardization was maintained.|Improper awareness on the need to maintain the tool standard.','|1) Informed all the operator to use only the prescribed tool in the production floor.\r<br/>2) Informed the tool grib personnel to only procure tools from the standard tool suppliers.\r<br/>3) Tool life monitoring charts are displayed near the machine.','|Only standard tools will be purchased and all other tools present in the production floor are maintained under the control of tool grib and will be issued only to the supervisors on reasonable demand.','CA PA found ok.','','2018-09-22','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','01','no','Misc','Prashanth Kumar(M)','no','','|Immediately stopped the production and collected all the tools from the shop floor and verified the tools for wear and then the accepted once are sent back to the production floor.','E3456','qas|','2018-11-07|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11110,'18-739A','Magellan Aerospace Wrexham','A/NUT STRIP','63026/02','F57250047204','NA','A',1,'176541','','78517','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Profile dig mark,\r\n','1)Part improperly butted on the vice.		\r\n','|Instruction given to all operators in the proper loading of part during the first setup operation.							\r<br/>','|Additional profile program was included to mark the profile on the part by removing minimum thickness to ensure correct loading of the part before starting the cycle							\r<br/>','Next Batch found ok','','2018-09-22','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','01','no','Misc','Prashanth Kumar(M)','no','','|Machine was stopped and instructions given to the operator regarding the specific part loading on machine							\r\n','E3456','pe|qas|','2018-11-07|2018-11-12|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11111,'53-026','Triumph Aerostructures','STRAP, LWR JOINT, TRACK 9','20161453','F5745171920100','NA','PART ISSUE A, ECN PG205026001KD08',1,'LTA TRIUMPH 2018','','80947','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Base thinness - side 0.15mm (part bend)  ','Part accepted by Customer.','|Part accepted by Customer.','|Part accepted by Customer.','Part accepted by Customer.','','2018-09-24','Dhananjaya(N)','Narasimhamurthy(C)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','With Treatment','','3','no','Misc','Dhananjaya(N)','no','','|Part accepted by Customer.','E3456','qas|','2018-09-27|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11112,'18-119B','Magellan Aerospace Bournemouth',' 	HOUSING OUT B DRG 3 ','1649701-2/WSGW','PID275 40011 200','','D01',100,'428868','','79531','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','DENT MARK OBSERVED ON FACE','Dent mark parts sent to final inspection.|All parts was  not seen. |Not inspected all the machined parts|Not checked all the parts correctly','|All dented parts are removed by polishing.','|cleaning the fixture with oil stone and removing all the chips out of the fixture ','CAPA FOUND OK','','2018-09-24','Punith G(S)','Sundar D.K.,Sudhakar C.M,Santhosh Kumar N,S. Shiva Kumar,Raghavendra P,Patel Appaaji,Paramaeshappa ,Manoj Kumar D,KRISHNAMURTHY N,Hanumantha Rao,Girish MS,Girish HP,BHUVANAPRAKASH  J.S,Ashoka R,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','Manufacture Only','','FI','no','BMV 60-1','Narasimha Murthy(R)','no','','|Informed  to all the operators to identify the  dent mark & rework parts with identification tag','E3456','pe|qas|','2018-09-24|2018-09-24|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11113,'51-045','THE BOEING COMPANY','BRACKET','741161','149A7371-9611','','PSDL REV A',3,'BOEING 001F','','74298','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','DUMMY NCR','MORE CUTTING SPEED AND ROUGHING STOCK MORE IN PARTICULAR AREA\r\nTHE RAW MATERIAL LENGTH IS UPPER LIMIT. SO THE CUTTING TOOL STRUGGLED TO REMOVE THE EXCESS MATERIAL\r\nTHE CUTTING OVER HANG ALSO MORE.|DUMMY NCR|DUMMY NCR|DUMMY NCR|DUMMY NCR','THE MORE LENGTH PARTS IDENTIFIED. EXCESS LENGTH ARE PRE MACHINED. LOW CUTTING SPEED PROGRAM RECEIVED FROM ENGG.dEPT AND PROVED. |DUMMY NCR','THE MORE LENGTH PARTS IDENTIFIED. EXCESS LENGTH ARE PRE MACHINED. LOW CUTTING SPEED PROGRAM RECEIVED FROM ENGG.dEPT AND PROVED. |DUMMY NCR','Dummy NCR','','2018-09-24','pe_sez(a)','pe_sez(a)','','0000-00-00','PART MIX UP','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','Misc','qas_sez(a)','no','','PRODUCTION STOPPED. COMPLETED PARTS ARE CHECKED AND FOUND OK. |DUMMY NCR','Z3456','pe_sez|qas|','2018-09-24|2018-10-12|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11114,'35A-548','Saab AB','LIFT ARM','','D522 73353 001 00','','PART ISSUE A',9,'1600217568','','A13315','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','yes','Sealant not covers the bush. ','1) Excess material in the detail part is bot covered by sealant after the bush assembly.|2) Installation of bush is carried out through shrink fit method.|3) According to AIPS 01-02-19 Method B sealant only need t be squeezed out from the bush and should be uniform around the joints, which is achieved in the parts. ','|Communicated to the customer about the specification requirements and acceptance of part.','|Communicated to the customer about the specification requirements and acceptance of part.','Justification accepted by customer and NC Closed.','C61916','2018-09-26','qas_sez(a)','op_sez(s)','.','2018-05-23','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','',' 	CUSTOMER END','yes','Misc','qas_sez(a)','no','','|Communicated the assembly and inspection team and carried out stock check and no similar deviated parts were found.','Z3456','qas|','2019-02-16|','2019-02-16',NULL,NULL,NULL,NULL,NULL,NULL),(11115,'46-021A','Mahindra Aerostructures Pvt.Ltd','STRAP','9810201 4','D575-40881-201MH','','H',1,'MAPL Forecast ','','65176','','0000-00-00',NULL,'no','no','no','yes','no','yes','no','yes','no','corrosion pit marks  observation','1.Corrosion marks are not identified on parts during inspection|2.During inspection part was free of corrosion marks but after that fitting work carried out|3.In fitting due to FOD corrosion pit marks created','|After fitting operation parts to be ensure free of FOD and protect with rust preventive oil','|Parts to be protect with free of FOD','CAPA found ok','','2018-09-26','Nandishkumar(D.K.)','Ravindra(Kumar)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','DN35571','post dn','no','Misc','Ravindra(Kumar)','no','','|The parts which are all in FG, Fitting and WIP ensure free of FOD and Corrosion','E3456','pe|qas|','2018-12-19|2018-12-19|','2018-12-19',NULL,NULL,NULL,NULL,NULL,NULL),(11116,'18-437B','Magellan Aerospace(Blackpool) Limited','MANIFOLD','30564 6277','PI201274625','NA','NIL',5,'Bpp-529619 amed-2','','80189','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Required rib thickness 5.00mm+/-0.25 but measured 4.40/4.5mm.					\r\n','Operator wrong correction.|Work order qty 16nos, 11nos Part all dimension found ok ,after  correction the tool wear value. because cutout stock 0.5mm in final program. |After complete the part, extra material not easily broken so operator down in tool offset value.|The same tool maintain the rib thickness, but not observed.|After correction operator not inform the seiner shift operator and supervisor.','|Next batch final operation cutout program changed.','|Training the operator, explain the operation wise dimension and every tool description and any correction inform to seiner operator or supervisor before correction.  ','CA/PA Found satisfactory.','','2018-09-27','Rangaswamy()','Karthik Raj T()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','03','no','Misc','Rangaswamy()','no','','|Another operator identified the correction value and identified the rejection parts and inform the supervisor.','Z3456','pe_sez|pe_sez|nandishkumardk|','2018-09-27|2018-10-23|2018-11-27|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11117,'18-437B','Magellan Aerospace(Blackpool) Limited','MANIFOLD','30564 6277','PI201274625','NA','NIL',1,'Bpp-529619 amed-2','','80190','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Required rib thickness 5.00mm+/-0.25 but measured 4.40/4.5mm.					\r\n','Operator wrong correction.\r\n|Work order qty 16nos, 11nos Part all dimension found ok ,after  correction the tool wear value. because cutout stock 0.5mm in final program. \r\n|After complete the part, extra material not easily broken so operator down in tool offset value.\r\n|The same tool maintain the rib thickness, but not observed.\r\n|After correction operator not inform the seiner shift operator and supervisor.\r\n','|Next batch final operation cutout program changed.\r<br/>','|Training the operator, explain the operation wise dimension and every tool description and any correction inform to seiner operator or supervisor before correction.  \r<br/>','CA/PA Found satisfactory.','','2018-09-27','Rangaswamy()','Karthik Raj T()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','03','no','Misc','Rangaswamy()','no','','|Another operator identified the correction value and identified the rejection parts and inform the supervisor.\r\n','Z3456','pe_sez|pe_sez|nandishkumardk|','2018-09-27|2018-10-23|2018-11-27|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11118,'18-376B','Magellan Aerospace Bournemouth','GAMMA FITTINGS','20028','NSA840020-150PF','','L',3,'428932','','78127','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Parts received from treatment were found paint damage at the edges and corners.','This is happen during the transportation as there was no safety in the inner layer of the box in which the parts were shipped','|Parts were done manual touch up as per the specification and found ok','|Instruction was given to the treatment house on packaging to put extra kushan type of material surronding the inner layer of the box to avoid such paint damages during the transportation','Next Lot Received from the treatment supplier ,parts were checked and found visually acceptable to the requirement','','2018-09-27','qas_sez(a)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','DN44980','POST DN','no','Misc','qas_sez(a)','no','','|parts were identified and segregated and the same was communicated to the treatment house','Z3456','qas_sez|','2018-11-27|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11119,'51A-068','THE BOEING COMPANY','FITTING ASSY, INBD','','112T7057-1','','PSDL REV -',1,'BOEING 001Q','','A16025','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','yes','AS IS:\r\nThe assembly part is without the pilot hole as called in the SSP. The SSP was received after the manufacturing of the parts. The SSP calls for the higher Assembly drawing 112T7101 Sheet 1 for which we do not have access as this is not a part of our contract. We have requested for the drawing. The required holes will be incorporated for next batch only after the receipt of the higher Assembly drawing.\r\n\r\nSHOULD BE:\r\nThe pilot hole to be drilled as per the SSP received at the Assembly stage.\r\nReference Drawings\r\n112T7101-501\r\n112T7057-1, SSP, REV A\r\n112T7057, PL, SH 2 REV -\r\n112T7057, SH 1 ZN A7, REV -','1) Pilot hole not drilled.|2) Requirement of pilot hole is mentioned in the higher level drawing and the requirement is not flowed down because the higher level drawing is not contractually offered to CIM.','|MRB accepted by customer and no further actions required until higher level drawing is flowed down.','|MRB accepted by customer and no further actions required until higher level drawing is flowed down.','CA PA found ok.','C66495','2018-09-28','Sathish(G)','Basavaraj(Kuri)','CA1406234-00','2018-09-26','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','yes','Assembly','','Cust End','no','Misc','qas(qas)','no','','|MRB raised in the Boeing portal and information given to the Boeing team.','E3456','qas|','2019-04-25|','2019-04-25',NULL,NULL,NULL,NULL,NULL,NULL),(11120,'35-622','Saab AB','FLAP, VENT','2270601','D5227280420000','NA','PART ISSUE A',1,'OWED-LTA-003','','78657','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Tool broken out while running ','Tool wear out|Tool life was not noticed','Tool changed life of tool data is mentioned','Informed all operators to check the tool life data','CAPA FOUND OK','','2018-09-28','prodn_aero(prodn)','Manjunatha.S.T(M)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','PRODUCTION','no','Misc','prodn_aero(prodn)','no','','Life of tool was not checked .Machine run.','A3456','qas_aero|','2018-10-26|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11121,'35-182B','Saab AB','EDGE HOUSING','467652','423Z1121-5-02','','--B',1,'Forecast po for B787','','77758','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Bore over size','Part reloaded after completion of bore.|Did not observe the completion of bore setup.|.|.|.','Checked bore size and notice the mistake and observed all the parts before loading in that setup.','Informed all the operator about this mistake and next part loaded carefully.  ','','','2018-09-28','prodn_aero(prodn)','Santhosh Kumar.R()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','05','no','Misc','Santhosh Kumar.R()','no','','Did not observe the part before loading to the machine.','A3456','qas_aero|','2018-10-13|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11122,'35-275','Saab AB','PIN','972169','426Z3601-1','','--A',1,'PA 1510 FORECAST-3','','76632','','0000-00-00',NULL,'yes','yes','yes','','','','','','','part thickness - side by 0.08 mm. ','Correction given in TRANS  for thickens maintain.   |Wrong correction given in TRANS.|Negative value not changed  to positive value in given correction . |After correction given not cross checked.','|Positive value given in TRANS. so next part found OK. ','|1)instruction given to operator that do not change in TRANS value and  give the correction only in tool offset ware  while first part run .\r<br/>2)Cross check the given correction value by another operator.','CAPA found ok.','','2018-09-28','Subramanya L(Naik)','        Sunil G S','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','11','','','','','','|Checked all program found OK.','E3456','pe|pe|qas|','2018-09-29|2018-10-03|2018-10-11|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11123,'28-027','Magellan Aerospace New York  Inc.','GUIDE ','MA20143791','141T6274-4','','PL_A + ADCN # 3 & 4, DL_N/C',1,'A000159399','','80863','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','OD UNDER SIZE BY -0.035MM.','1.part heads to be lock properly on fixture otherwise ovality occur. |2.during part tightening on fixture in sufficient pressure tight applied.|3.due to that low pressure part loosed from fixture.|4.due to that od dimension under size occured.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                             |                          ','|during part tightening on fixture during that time tight pressure to be ensure manually.','|the part tightening to be conform via torque wrench.','capa found ok','','2018-09-28','Ravi(M)','Manoj Kumar(D)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','09','no','Misc','Ravi(M)','no','','|that next part was tightened properly and ensured manually. ','E3456','pe|qas|','2018-10-15|2018-11-28|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11124,'18-008A','Magellan Aerospace Wrexham','Plate Cover','670593','D572 52518 200','L97 T351','A',1,'175175','','80004','','0000-00-00',NULL,'yes','no','no','no','no','yes','no','yes','no','Required range 29.00 to 32.00% IACS and observed conductivity range is 38.6/38.7% IACS.','The mechanical properties of the material changed due to the increase in temperature.|Temperature increased during the Machining process because of insufficient coolant flow.|Coolant filter was blocked by micro particles that were mixed up in the coolant.','|Changed the Coolant filter in the machine and ensured proper coolant flow.','|Daily check list displayed near the machines which also includes ensuring proper flow of coolant.','Next batch produced in the machine sent for conductivity test and found ok.','','2018-09-29','stores_sez(a)','stores_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','DN45962','POST DN','no','Misc','qas_sez(a)','no','','|1) Checked the conductivity of the RM from the same batch and found ok.\r\n2)Informed the maintenance team and the production department to Check the coolant filter in all the machines for any block and change the blocked filters immediately.','Z3456','qas|','2019-05-17|','2019-05-17',NULL,NULL,NULL,NULL,NULL,NULL),(11125,'34-015C','Magellan Aerospace Winnipeg',' 	MOUNTING LUG- STRUT / S','G22948K07','400-12607-1-905','NA','EM105092 Iss H, EM104302 Iss B, EM104765 Iss H, EM106399 Iss B, EM106400 Iss B, EM106401 Iss B, EM106404 Iss A, EM106522 Iss A, EM106602 Iss A',1,'C86722','','81459','','0000-00-00',NULL,'yes','yes','yes','','','','','','','BASE THICKNESS -.5 MM RUNNING TIME ','Base thickness under-size.|Part not properly clamped in the fixture due to which the part lifted during machining.|Part is clamped with the help of fixture which holds the parts 360 degree in the form of vice, but due to chips blocking between both the jaw\'s the part got clamped temporarily and during the vibration caused in machining the clamping force reduced and caused the part to lift at one end.|Operator did not ensured the absence of chips in between the jaws.','|1) Removed the movable jaw completely and cleaned all the chips between them and continued the production.\r<br/>2) Informed all the operator to check absence of chips in the butting area and clamping area of the part.','|1) Comment included in the machine to alert the operator to check the proper removal of the chips during the completion of every operation.','Next parts produced are found ok and comment mentioned in the program to clean the gaps between jaws.','','2018-09-29','Dhananjaya(N)','        Narasimhamurthy C','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','5','','','','','','|Immediately stopped the machine and checked the thickness of previously completed parts and found ok.','E3456','pe|qas|qas|','2018-09-29|2018-09-29|2018-10-09|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11126,'51-001','THE BOEING COMPANY','Upper Beam FWD Splice','BA40830','315Z1301-501','','NIL',1,'BOEING 001K','','80532','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Thickness under size 0.12 mm','Part running time part was lifted.|Butting area not cleaned.|When doing the production operator do not clean the fixture top face.|Part loading and unloading time fixture top face part butting face machining chips clogging in the fixture,operator couldn\'t observed and loading the part take more cut an tool part get under size.\r\n  ','Inform to operator every part completed after clean the part butting area properly.','Next part loading time cleaning the fixture and loading the part and part get found ok.','Operator performance need to  be monitored.','','2018-09-29','pe_sez(a)','Shivaraj K S,Kiran Kumar M,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','3','no','Slim3n-4AHS-4','pe_sez(a)','no','','Inform to operator every part completed after clean the part butting area properly.','Z3456','qas|','2018-10-12|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11127,'18-648A','Magellan Aerospace Wrexham','SPACER','M064650/27683','D579 55060 202','','B',1,'175169','','80383','','0000-00-00',NULL,'yes','yes','yes','','','','','','','RUNNING TIME M5 BOLT HEAD BROKEN SO PART HOLE POSITION SHIFT 0.4MM ','M5 bolt head broken.|M5 bolts using for part clamping.|Bolt quality not good.|Operator over tight is chances of  head broken. ','|Change the bolt using stainless steel bolts.','|using stainless steel bolts.for part clamping.|Informed Operators to verify the bolts before using to clamp the parts.','','','2018-09-29','Rangaswamy()','        Manu ','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','05','','','','','','|Remove the bolt use another M5 bolt.and inform to tooling department.','Z3456','pe_sez|pe_sez|qas|','2018-10-03|2018-10-11|2018-11-06|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11128,'35-468A','Saab AB','SHAFT CAM ','34778216-B','D5227351320000','NA','PART ISSUE C',1,'OWED-LTA-004','','78201','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Parts received from treatment were found paint damage at the edges and corners.','This is happen during the transportation as there was no safety in the inner layer of the box in which the parts were shipped','|Parts were done manual touch up as per the specification and found VISUALLY  ok','|Instruction was given to the treatment house on packaging to put extra kushan type of material surronding the inner layer of the box to avoid such paint damages during the transportation','Next Lot Received from the treatment supplier ,parts were checked and found visually acceptable to the requirement','','2018-10-01','qas_sez(a)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','DN44820','POST DN','no','Misc','qas_sez(a)','no','','|parts were identified and segregated and the same was communicated to the treatment house','Z3456','qas_sez|','2018-12-06|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11129,'35-525A','Saab AB','ROD BODY','34778216-B','D5227333620000','NA','PART ISSUE B',1,'OWED-LTA-005','','78230','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','TOTAL LENGTH UNDER SIZE.','TOTAL LENGTH UNDER SIZE.|Multiple passes were performed on the finished parts itself.|Re-loading of the finished part|The finished part under gone all the operations again and in the final operation where the total length is maintained then total length got under sized. ','|1.Before loading the part the operator should ensure the total length.\r<br/>2.Training and instructions are give to the operators.','|1.Separation of finished parts and semi finished parts are done.\r<br/>2.Identification of Finished and Semi-finished parts are done by using separate trays.','CA PA found ok.','','2018-10-01','Dinakar(K)','Dinakar(K)','','0000-00-00','REJECTED','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','05','no','Misc','Dinakar(K)','no','','|Checked the previous machined parts found ok.\r\n','E3456','pe|qas|','2018-10-23|2018-12-10|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11130,'18-001A','Magellan Aerospace Wrexham','BRACKET SUPPORT-LH','4193901 1','D361 50110 200','ABM3 1029 T7651','A',1,'162890','','77090','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dia 3.2 hole ablong.','Part not butted properly in 3rd setup.','Location pin length increased','Part properly butted to the location pin in fixture.','CAPA FOUND OK','','2018-10-04','Dinesh kulal()','prodn_aero(prodn)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','Production','no','Misc','Dinesh kulal()','no','','Height of the location pin Changed.','A3456','qas_aero|','2018-10-12|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11131,'35-628A','Saab AB','','C90880','D5227349320400','NA','PART ISSUE D',3,'OWED-LTA-001','','78555','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Bore over size. dia requierd 18.840 to 18.861 Measured 18.876 To 18.890','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 |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\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/>','CA/PA found satisfactory. ','','2018-10-04','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','Misc','Yashawantha(NH)','no','','|Based on the usage of the part [Assembly Requirement], since a shaft gets into the bore, the checking method was changed and all the rejected parts were subjected to re-inspection using a GO and NOGO Plug Gage','E3456','pe|nandishkumardk|','2018-11-13|2018-11-27|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11132,'35-629A','Saab AB','','C91212','D5227349320500','NA','PART ISSUE D',1,'OWED-LTA-001','','78560','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','BORE OVER SIZE BY 0.010MM.','1) Bore oversized due to chip-off in the cutting edge of the reamer.|2) Due to hard material and rough machining condition the cutting edge got chipped off and the ID got oversized|3) Tool life was not freezed and was under RD stage.','|Informed all the operators to change the reamer once in 5 Parts. ','|Informed the tooling supplier and purchased high grade reamers to withstand the machining conditions. ','Next batches found ok.','','2018-10-04','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','06','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),(11133,'35-287','Saab AB','BEAM FITTING','709812B2','424Z1139-2','','--B',1,'Forecast po for B787','','80752','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Part dig up to 1mm.','While running time tool release from tool holder.|Tightening stud crack in holder.|Tool not proper tight in holder.','Guide the all operator about this issue and inform to check the holder and tool daily.','Guide the all operator to once again cross check the stud and tightening of tool in tool holder.','CAPA FOUND OK','','2018-10-04','Dinesh kulal()','Dinesh kulal()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Dinesh kulal()','no','','Change the tightening stud of the tool holder.','A3456','qas_aero|','2018-10-26|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11134,'18-001A','Magellan Aerospace Wrexham','BRACKET SUPPORT-LH','4193901 1','D361 50110 200','ABM3 1029 T7651','A',1,'175154','','77094','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Part shifted up to 3mm.','Part not located in location pin properly.','Make the new location pin to ass per required.','After inserted new location pin part will located properly.','CAPA FOUND OK','','2018-10-04','Dinesh kulal()','Dinesh kulal()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Dinesh kulal()','no','','Change the location pin height.','A3456','qas_aero|qas_aero|','2018-10-12|2018-10-12|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11135,'18-392B','Magellan Aerospace(Polska) Sp','END COVER','M940330/20715','D278 50167 200','','D',1,'104569','','79196','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Thickness undersized by 0.13 to 0.15mm. ','Thickness undersized |Due to part butting problem|Due to clogging of chips on the part butting face the part was not butt properly.|Supporting bush was not clamped properly','|Clamp the the supporting bush properly.\r<br/>Instruction given to the operator.','|Frequently cleaning the part butting face to avoid the clogging of chips.\r<br/>','CAPA found ok. operator performance need to be monitored.','','2018-10-04','Dinakar K()','Dinakar K()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','3','no','Misc','Dinakar K()','no','','|checked the previous machined parts found ok','Z3456','pe_sez|qas|','2018-10-23|2018-10-30|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11136,'43A-047','','','','','','',0,'','','','','0000-00-00',NULL,'no','no','no','no','no','no','no','no','no','','','','','','','2018-10-04','select','','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','','','','no','','select','no','','','E3456','qas|','2019-01-06|','2019-01-06',NULL,NULL,NULL,NULL,NULL,NULL),(11137,'43A-047','Composite Industrie','FASTENING ASSY','','V5312324600200','','B00',20,'LTA COMPOSITE 2018','','A17149','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','yes','The FA005 treatment is missing on the rivet, as mentioned in BOM.\r\nthis defect is also observed in A17144(1), A17147 (6), A17152(12), A17153(3), A17151 (4), A17152(1).','Part without application of the FA005 reached customer.|Assembly operator missed to apply the topcoat(FA005) on the rivets and the quality inspector missed to verify the completion of operations.|Assembly operator did not followed the process sequence and the quality inspector did not verified to the Assembly process and drawing requirement during the final inspection.|Assembly operator was improperly trained on the need to follow the assembly operations. Since the Assembly Process Sheets(APS) and drawing were not readily available for the quality inspector he hesitated to refer to the drawing and the APS.','|1) Informed all the assembly operators to follow the process sequence without fail.\r<br/>2) Informed all the Quality inspectors to refer to the APS or customer supplier drawing during the final inspection.','|1) Quality alert displayed in the assembly and Final Inspection area.\r<br/>2) Tabs are issued to the Quality Inspectors to have easy access to the process sheets and customer drawings.','','C67432','2018-10-04','Sathish(G)','Mahesh(DV)','180903-043, 180831-020, 180903-021','2018-09-19','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','Cust End','yes','Misc','qas(qas)','no','','|All the parts in in-process, FG,and under inspection were rechecked and affected parts of similar kind are reworked.','E3456','qas|','2018-10-23|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11138,'35A-474A','Saab AB','FRAME ASSY','','D5227338400000','','B',1,'OWED-LTA-001','','A16225','','0000-00-00',NULL,'no','no','no','no','no','no','yes','yes','yes','The parts have been measured laying on a flat surface, 7,5 kg weight on each end and the use of feelar gauge, 0,4 mm.\r\nThe following is the result:\r\nD5227338400000:\r\n1600237628-10-2\r\nW/O: 73573, 73176\r\n15 pcs, none passed the requirement\r\n1600234150-35-2\r\nW/O:73175\r\n20 pcs, 2 pcs were found to pass the requirement\r\nD5227338400100:\r\n1600237628-7-2\r\nW/O: 73759\r\n9 pcs, none passed the requirement\r\n1600234253-6-2\r\nW/O: 73181\r\n6 pcs, none passed the requirement\r\n1600237628-7-1\r\nW/O:73181, 73179\r\n27 pcs, 1 pcs was found to pass the requirement','1) Part deformation post machining.|2) Due to improper intermediate aging process the parts got deformed after the completion of machining.|3) usually intermediate aging was carried out for parts longer than 1meter but since this part is lesser than 1meter intermediate ageing was not taken to consideration.','|Intermediate aging of the parts in WIP were implemented and continued the production.','|MPS revised to introduce the aging and change in inspection method to avoid deformation of part and escapement.','Next batches produced found ok.','C66460','2018-10-04','Yashawantha(NH)','Manu(P)','OF-003226','2018-09-28','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','yes','Assembly','','Cust End','no','Misc','qas(qas)','no','','|Immediately Checked all the parts in WIP and FG and quarantined and reinspected them.','E3456','qas|','2018-12-10|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11139,'35-687A','Saab AB','LEVER','509667C','D5227353620500','NA','PART ISSUE D',1,'OWED-LTA-005','','81994','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','TOOL DIG MARK ON LEG.','1.During milling operation tool dig mark occurred|2.Tool overhang occurred on part|3.Operator was made mistake to load the tool','|Training was given to the operator','|Training record will be maintain ','CAPA found ok','','2018-10-05','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','08','no','Misc','Yashawantha(NH)','no','','|Tool length was adjusted','E3456','pe|qas|','2018-12-19|2018-12-19|','2018-12-19',NULL,NULL,NULL,NULL,NULL,NULL),(11140,'18-090A','Magellan Aerospace(Polska) Sp','BUSH','CD704211/00460A','PID278 50164 200','','A',6,'104569','','76230','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','OD UNDER SIZE 0.03MM','IMPROPER BUTTING OF INSERT ON TOOL HOLDER.|WEAR OUT OF INSERT CLAMPING SCREW.|DUE TO HEAVY LODE APPLIED ON THE SCREW. ','|DAMAGE CLAMPING SCREW WERE REPLACED  WITH NEW ONE AND TIGHTEN IT TO THE REQUIREMENT .','|ENSURE THE SELECTION OF SCREW BEFORE LOADING  AND REQUIRED TORQUE APPLIED.','CA/PA Found OK.','','2018-10-05','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','03','no','Misc','Raghavendra Rao(R)','no','','|CHANGE THE SCREW PROPER INSERT BUTTING TAKE THE OFFSET RUN THE PART FOUND OK.','E3456','pe|qas|','2018-11-28|2018-11-28|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11141,'51-083A','THE BOEING COMPANY','BRACKET DETAIL','717200A0','332A2930-8','NA','PSDL REV B',1,'BOEING 001U','','78818','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Bore 20micron over size.','Tool run out in holder.|Tool tip chip off.|Operator not checked the tool run out.','|Fix the tool fore this bore size.','|Maintain the tool fore this size bore.','CAPA FOUND OK','','2018-10-05','Ravi nayak()','Dinesh kulal()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','Production','no','Misc','Ravi nayak()','no','','|Change the reamer and the run the part.','A3456','prodn_aero|qas_aero|','2018-10-26|2018-10-26|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11142,'18-309B','Magellan Aerospace Wrexham','SPIGOT ','1573448-2/Q8LF','F575 51290 200 PF','','B',3,'162895','','75774','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','DENTS OBSERVED ON PARTS','1) Part got dented due to improper handling.|2) Insufficient packing around the edges during transit.|3) Supplier shipped the parts by packing one after the other with single layer of bubble sheet due to which the weaker portion of the packing got affected and resulted in the damage of the part.','|Communicated to the supplier about the poor packing and provided guidelines on how to pack the parts to prevent damages even during the poor handling conditions.','|only individual parts are packed in a wrap and shipped by supplier.','NEXT BATCH PARTS RECEIVED FROM SUPPLIER AND PACKING METHOD WAS AND PARTS FOUND OK.','','2018-10-06','qas_sez(a)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','DN45554','POST DN','yes','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_sez|','2018-12-06|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11143,'18-313A','Magellan Aerospace Bournemouth','STUD ','256898 642246','D278 50006 204 01','','D',1,'428929','','79165','','0000-00-00',NULL,'yes','','yes','','','','','yes','','chf plus side 0.4mm','1) Chamfer oversize by 0.2mm beyond tolerance.|2) While providing the tool wear the operator provided 0.15mm increment instead of 0.4mm.|3) The tool used for the chamfer operation was a new tool made to carry out the chamfer operation on the inside edge of a wall.|4) The previous tool used was not providing proper life therefore the new tool was purchased and during trial the wear value provided by the operator was not adequate.|5) Operator did not calculated the exact tool offset as the tool was under trial.','|1) Removed the wall thickness and the base thickness and maintained them to the mean value since the thickness on both the side was on the maximum side.','|1) Next time the trial activities of any tool will be carried out during the presence of Supervisor and the tooling in-charge.','CAPA found ok and the part found accepted after rework.','','2018-10-06','Anjinamurthy(H)','        S. Shiva Kumar','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','','','','','05','no','','','','','|Immediately stopped the machine and changed the wear offset as per the guidance of senior operator.','E3456','qas|qas|qas|','2018-10-25|2018-10-25|2018-10-25|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11144,'35-228A','Saab AB','HINGE BRACKET 2 ','4755501 2','D576 50005 205','','D00',1,'1600223433/Forecast ','','81969','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Bore chatter mark absorbed on fine finish surface ,','1.while boring operation running time coolant not present in boring tip.|2.Adjust the coolant pipe direction to the boring tip.|3.coolant supply not done properly so in the boring tip cutting edge to be clogged so bore on chatter','|1.Adjust the coolant direction to the spindle.','|1.Training has to be conducted to all shift operators, effectiveness found ok','Effectiveness found ok','','2018-10-06','Rangaswamy()','NataRaj.CV()','','0000-00-00','bore chattring','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','NataRaj.CV()','no','','|1.immediately stop the machine and check the all previous parts ,all parts found ok','Z3456','pe_sez|qas_sez|','2018-12-18|2018-12-18|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11145,'18-075A','Magellan Aerospace Wrexham','ADAPTOR','M061590/27262','D282 50044 200PF','','A',2,'175162','','79279','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','profile under size -0.1mm.','Thickness undersized |Due to part butting problem|Due to clogging of chips on the part butting face the part was not butt properly.|Supporting bush was not clamped properly','|Clamp the the supporting bush properly.\r<br/>Instruction given to the operator.','|Frequently cleaning the part butting face to avoid the clogging of chips.','Next batched produced found ok.','','2018-10-09','Narasimhamurthy(K.G.)','Rasika(R)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','03','no','Misc','Ravi(M)','no','','|checked the previous machined parts found ok','E3456','pe|qas|','2018-10-23|2018-12-10|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11146,'51-016','THE BOEING COMPANY','DRIP-PAN MOUNTING BRACKET','641121','673Z3480-25','','NIL',1,'BOEING 001J','','81131','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','UNDER CUT OBSERVED AND THICKNESS MINES MEASURED VALUE 0.9779 \r\nMINIMUM VALUE 1.016','After roughing operation stock was not there for finishing operation|In tool offset,Z-axis was kept 3mm above the required Z0 level|Operator failed to take the correct toll Offset |The checklist was not filled and approved after the setting of first part was done','|The checklist provided for setting validation must be filled and approved by concerned supervisor or Senior operator. ','|refer to CA ','the next part in this work order was machined provided with the check list for setting. Thickness\r\nand profile checked and found within the requirement. ','','2018-10-09','pe_sez(a)','Kiran KM,','','0000-00-00','UNDER CUT OBSERVED AND THICKNESS MINES MEASURED VALUE 0.9779 \r\nMINIMUM VALUE 1.016','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','Slim3n-4AHS-2','qas_sez(a)','no','','|Required tool Offset was taken before continuing the rest of the programs. The next run part was found OK. ','Z3456','qas_sez|','2019-04-12|','2019-04-12',NULL,NULL,NULL,NULL,NULL,NULL),(11147,'35-597','Saab AB','CORNER','532701B','D5227338620200','NA','PART ISSUE B',1,'OWED-LTA-001','','81796','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Profile Dig of .6mm (AT SEZ MAZZAK I-700 MACHINE)','NC program Boarder rating reading problem|Machine capacity memory problem','|Mazak Maintenance team came and re-installed the MAZAKTROL software.','|Mazak Maintenance team came and re-installed the MAZAKTROL software.','CA PA FOUND OK','','2018-10-09','Ravi nayak()','prodn_aero(prodn)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','PRODUCTION','no','Misc','Ravi nayak()','no','','|Immediately machine stop and informed to the machine maintenance team.','A3456','prodn_aero|pe|qas_aero|qas_aero|','2018-11-28|2019-01-17|2019-06-08|2019-06-08|','2019-06-08',NULL,NULL,NULL,NULL,NULL,NULL),(11148,'56-041','GKN Aerospace Orangeburg','ARROWHEAD - UPR','1450014710','119A1333-9601','NA','NIL',1,'A000044561','','81812','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','part rib broken','During milling operation rib got broken|Due to tool path problem|Incorrect program','|Program was changed parallaly butting support implemented ','|Process was changed','Effectiveness found ok','','2018-10-10','Ramesh(Poojary)','Siddaramappa ,Sathish Y.R.,Gajendra Singh C.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','3','no','UNIPRO 5000-1','Narayanappa(G)','no','','|Program was re modified with corrected tool path','E3456','pe|qas|','2018-12-19|2018-12-19|','2018-12-19',NULL,NULL,NULL,NULL,NULL,NULL),(11149,'35-183B','Saab AB','EDGE HOUSING','467651','423Z1121-6-02','','--B',1,'Forecast po for B787','','77792','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','PART DIG UP TO 1 MM SO Thickness actual 2.54+/- 0.254 , measure 1.84/.90','Tool broken in 03 operation so part dig up to 2.2 mm.','|Change the tool run the part.','|Maintain the tool life register and tarin the operator about this issue.','CAPA FOUND OK','','2018-10-11','Ravi nayak()','Dinesh kulal()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','04','no','Misc','Ravi nayak()','no','','|Record tool life register when long cycle runnning time.','A3456','prodn_aero|qas_aero|','2018-10-26|2018-10-26|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11150,'35-710','Saab AB','LEVER','C90771','D5227346621100','NA','PART ISSUE D',1,'OWED-LTA-004','','81935','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','HOLE POSITION PROBLEM.','1.During milling operation hole ovality occurred|2.Drill bit was burnt|3.Drill bit tool life was expired','|Tool life will be monitor','|Tool life monitor to be load on machines','CAPA found ok','','2018-10-11','Ramesh(Poojary)','Kammar Nagaraj,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','3','no','HAASVF2SS-1','Dhananjaya(N)','no','','|Drill bit was changed','E3456','pe|qas|','2018-12-19|2018-12-19|','2018-12-19',NULL,NULL,NULL,NULL,NULL,NULL),(11151,'35-650A','Saab AB','SHAFT','C84690','D5227346820200','NA','PART ISSUE C',1,'PA1687 LTA-2','','80790','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Total length 0.03mm undersized.','part was not debarred.\r\n|improper butting in JAWS','|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.','CAPA Found Ok','','2018-10-11','Sandhesh D(S)','Sathish(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','07','no','Misc','Sandhesh D(S)','no','','|next part was debarred and inspected before loading onto the machine and the part was found OK.','E3456','pe|qas|','2018-12-18|2018-12-18|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11152,'35-709','Saab AB','LEVER','C84535','D5227346621000','NA','PART ISSUE D',1,'OWED-LTA-004','','81934','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','CHF OVER SIZE.','During chamfer operation excess amount of material was removed|Program was wrong','|Correct tool number was updated on program','|The updated program was stored and old one was removed','CAPA found ok','','2018-10-11','Ramesh(Poojary)','Kammar Nagaraj,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','3','no','HAASVF2SS-1','Dhananjaya(N)','no','','|The correct program was loaded','E3456','pe|qas|','2018-12-19|2018-12-19|','2018-12-19',NULL,NULL,NULL,NULL,NULL,NULL),(11153,'18-112A','Magellan Aerospace Bournemouth','BODY TURNBUCKLE INNER','CD702610/09014B','PID575 41541 200','','A',1,'428867','','77230','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Bore over size ,actual size is 12.7(0.018),measured value is 12.738 ,out of 20 micron ,','1.1st part proving time crc value wrong given .|2.1st part bore ovality present in H7 hole so on that time correction given in wrong ,  |3.Tool run out is present in tool so bore ovality more than required tolerance. |4.Next time part proving time cross check and run the program |5.while proving the H7 hole check the tool run out within 10 micron , ','|while proving the H7 hole check the tool run out within 10 micron other wise change the new tool and holders ,','|in this type of operation bore proving training given to operators on all three shift operator |Instructed All the operator to check the tool run out whether it is within 10micron and based on the run out provide the CRC correction in the machine.','CAPA found Ok.','','2018-10-12','Subramanya L(Naik)','        Sundar D.K.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','5','','','','','','|1.stop the m/c and check the part bore size ,\r\n\r\n2.Next part proving time crc value increase for checking the ovality and check the bore size correctly ,ensure the bore is correct so run the production batch.\r\n\r\n2.while proving the H7 hole check the tool run out within 10 micron , ','E3456','pe|qas|','2018-10-24|2018-10-30|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11154,'51A-028','THE BOEING COMPANY','BRACKET ASSY','','149A7371-36','','PSDL REV A',1,'BOEING 001H','','A13288','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','no','diameter oversize','REFER NC NO:10806.','|REFER NC NO:10806.','|REFER NC NO:10806.','REFER NC NO:10806.','','2018-10-12','pe_sez(a)','pe_sez(a)','','0000-00-00','CSK OVERSIZE','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Assembly','','IN PROCESS','no','Misc','qas_sez(a)','yes','','|REFER NC NO:10806.','Z3456','qas_sez|','2019-01-16|','2019-01-16',NULL,NULL,NULL,NULL,NULL,NULL),(11155,'47-099B','GKN Aerospace Filton','BRACKET M/C TRACK 2 FWD ','02318122','F57550193001','NA','PART ISSUE H02',1,'LTA-GKN-002','','79906','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Part wall dig mark.','Why1-Wrong program selected by operator.|Why2-All programs were in the same folder in a USB drive.','|1.Right program selected and further parts found ok.','|1.While running particular program only that program will be saved in the USB drive.','CA/PA Found OK.','','2018-10-12','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','01','no','Misc','Krishna(Chowdary.G.P.)','no','','|1.Stopped the Machine , Rechecked the program.','E3456','qas|qas|','2018-10-23|2018-10-25|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11156,'35-281','Saab AB','GUIDE HARNESS UPR','247809B7','423Z1929-3','','---',1,'Forecast po for B787','','77821','','0000-00-00',NULL,'yes','no','no','no','yes','yes','no','no','no','THICKNESS UNDER SIZE MINIMUM VALUE 2.286 MEASURED VALUE 2.1844','1. Tool offset wrong taken by operator so thickness as to be -ve side |2.while changing the part setting time operator not feel properly with height block.','|1.Re offset taken  by the operator','|1.proper training has to be conducted to all operators .','Effectiveness found ok','','2018-10-12','pe_sez(a)','Thaveni D M ,Nagaraju P K ,Manu ,Karthik Raj T ,HariPrasad ,','','0000-00-00','THICKNESS UNDER SIZE MINIMUM VALUE 2.286 MEASURED VALUE 2.1844','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','a51nx-06','qas_sez(a)','no','','|1.for next part tool length to be adjust properly,','Z3456','pe_sez|qas_sez|','2018-12-18|2018-12-18|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11159,'35-146','Saab AB','CED_HINGE_FTG_FWD','9404442','425Z0301-6','7050 - T7451 ALUMINU','--A',2,'Forecast po for B787','','76055','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Base Dig Mark 3mm.','Part not tightened properly.|Running time part lifted one side.|while running time lift the part tool broken and dig.','|cross check the tightened and runned','|Guidelines given to operator after loading the part cross check tightening and run.','CAPA found ok','','2018-10-12','Ravi nayak()','Dinesh kulal()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','01','no','Misc','Ravi nayak()','no','','|cross check the tightened','A3456','qas_aero|','2018-10-26|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11160,'56A-020','GKN Aerospace Orangeburg','SUPPORT ANGLE ASSY, UPR','','119A1440-606','','PSDL REV B',2,'LTA Orangeburg 737 W','','A19079','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','PILOT HOLE SHIFTED 0.5MM.','BUTTING NOT DONE PROPERLY','|IMMEDIATELY STOP THE PRODUCTION CHECK ALL PREVIOUS MACHINED PARTS.ALL PARTS FOUND OKAY ','|INSTRUCTION GIVEN TO THE OPERATOR, PLEASE ENSURE THE PART IS LOADED PROPERLY OR NOT AFTER CLAMPING THE PART CHECK WITH FILLER GAUGE FOR BUTTING AREA. ','NEXT PART FOUND OKAY.','','2018-10-12','op_sez(s)','op_sez(s)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Assembly','','ASSEMBLY','no','Misc','Mahesh(N)','no','80129','|PREVIOUS ALL PARTS INSPECTED FOUND OKAY.','Z3456','qas_sez|','2018-10-12|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11161,'35-622','Saab AB','FLAP, VENT','2270601','D5227280420000','NA','PART ISSUE A',1,'OWED-LTA-003','','78658','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dia 8 H7 hole over size by 0.08.','chips clot inside hole after run the hole mill program.|after run the hole mill program chips not removed.|Through spindle coolant (TSC)not on.','|Cross check the hole diameter and run','|After run the hole mill program M00 given inside the program to read and clean the hole before run the reamer program','CAPA found OK','','2018-10-13','Dinesh kulal()','prodn_aero(prodn)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Ravi nayak()','no','','|Cross check the hole diameter hole is over sized guide the operator clean the chips after run the hole mill program and run','A3456','qas_aero|','2018-10-26|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11162,'35-458A','Saab AB','ROD BODY','34778216-B','D5227350920000','NA','PART ISSUE B',3,'OWED-LTA-005','','81125','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Total length undersized.','Total length under sized.|The remaining stock for the finishing operation is entered manually in the program.|Wrong parameters were added in the program and the program was executed so the total length got undersized. |Part was not but properly to the front stopper.','|1.Correct butting of parts to the stopper.','|1.Butting the part to the back stopper and no editing in the finishing program will be done.','CA/PA satisfied.','','2018-10-13','Narasimhamurthy(K.G.)','Dinakar K()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','7','no','Misc','Dinakar K()','no','','|Checked the previous machined parts found ok','Z3456','pe|pe_sez|qas_sez|','2018-10-13|2018-10-23|2019-01-07|','2019-01-07',NULL,NULL,NULL,NULL,NULL,NULL),(11163,'35-480B','Saab AB','LOCK LEVER','C90875','D5227349820000','NA','PART ISSUE C',2,'OWED-LTA-003','','78360','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Running time  hole over size by 0.1mm. ','Hole Ablong by 0.1mm.|Tool Shank rubbed the outside diameter.|Lower flute length selected.|Not Adjusted the depth in program cycle, after selecting tool with lower flute length.','|1) Depth in program cycle adjusted and further parts found ok.\r<br/>\r<br/>2) Relief Clearance made in the tool( Flute length Relief).','|1) Depth in the program cycle adjusted such that any tool selected length with more than the OD Will not in oversize or Ablong.\r<br/>\r<br/>2) Tool Set box created & the same tool will be used in further batches & the same in updated in program.','NEXT BATCH FOUND OK.','','2018-10-14','Dhananjaya(N)','        Mallikarjuna D','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','13','','','','','','|1) Previous parts hole diameter checked & found Ok.\r\n\r\n2) Stopped the machine & checked the flute length.','E3456','pe|qas|qas|qas|','2018-10-25|2018-10-26|2018-10-29|2018-10-31|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11164,'43-017','Composite Industrie','BRACKET','544935 B','V2511162220000','NA','A00, ECN PV100298ST1AD69',1,'LTA COMPOSITES 2018-','','81390','','0000-00-00',NULL,'yes','no','yes','','','','','yes','','Part thickness under sized.','Correction given Due to part 2mm thickness maintain .|Part to part thickness becomes variation 0.1mm to 0.2mm. |Machine was -16mm correction taken instead off -0.16mm due to while given correction decimal point was missed. |While given correction was not crosschecked and not concentrated.  ','|Asked the supervisor about wrong correction and problem of thickness variation and  given right correction .\r<br/>','|Instruction given to the operator that again and once again crosscheck the given any correction and concentrate on his work.\r<br/>Importation was given to engineering for this problem. \r<br/>|Information given to the Engineering team about the issue and the process will be changed.','CAPA found ok.Change in process will be monitored during the next production.','','2018-10-14','Subramanya L(Naik)','        Yogesha K','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','05','','','','','','|Checked previews parts found OK. ','E3456','pe|pe|qas|','2018-10-24|2018-10-27|2018-10-30|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11165,'18-648A','Magellan Aerospace Wrexham','SPACER','M064650/27682','D579 55060 202','','B',2,'175169','','80385','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Base thickness minus.','program running time tool down.so part rejected.( one time 2nos loading )|Dia 16flat using for all roughing.|chances off tool down.\r\n\r\n1) Tool cutting edge chip-up.|2) Not sufficient holding.|3)Tool holder or collect damage and operator not checking tool flutes.','|Checking the tool in every shift.|Checking the tool in every shift.|Checking the tool in every shift.','|Next batch tool life monitor.and set tool life. ','','','2018-10-15','Rangaswamy()','HariPrasad()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Rangaswamy()','no','','|Change the cutting tool and tool holder.and inform to tool department.|Change the cutting tool and tool holder.and inform to tool department.|Change the cutting tool and tool holder.and inform to tool department.','Z3456','|||pe_sez|qas|','2018-10-23|2018-10-23|2018-10-23|2018-10-23|2018-11-06|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11166,'35-583A','Saab AB','BRACKET','532730C','D5227334820600','NA','PART ISSUE B',1,'OWED-LTA-005','','80497','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','id over size by +0.02mm.','Operator did not ensured the Inner Diameter of the part to the drawing requirement. |The operator did not calculated the Air gauge reading properly.|The Air gauge was set to Dia. 19.05mm and it has to be measured with in +21Micron, but the operator calculated the air gauge reading as 19.00mm and +25Micron.|Inadequate knowledge on the measuring instrument.','|1)Corrected the Wear offset in the machine according to the drawing requirement and checked the next part and found ok. \r<br/>2) Informed all the Operator\\\'s to once again recheck the master and the reading in both air gauge and bore gauge before using the instrument to check the part.|Informed all the operators to request assist from senior operator or supervisor if any corrections to the checking instruments or program parameters to be made.','|Fresher training is given to the new operator and refresher training is planned to be given to all the senior and experienced operator\\\'s on the measuring instruments.','Next batches found ok.','','2018-10-15','Narasimhamurthy(K.G.)','Narasimhamurthy(K.G.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Ravi(M)','no','','|Checked the previous machined parts found ok.\r\n|Senior operator corrected the Air gauge and the machine parameters and continued the production and the next parts produced found ok.','E3456','pe|qas|qas|','2018-10-23|2018-11-06|2018-12-10|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11167,'56A-019','GKN Aerospace Orangeburg','SUPPORT ANGLE ASSY,  UPR','','119A1440-605','','PSDL REV B',2,'LTA Orangeburg 737 W','','A19067','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','PILOT HOLE SHIFTED 0.5MM.','1) Hole Position shifted during the drilling operation.|2) The hole was drilled after the assembly manually.|3) Because of the difficulty in clamping the part after assembly in machine the hole was drilled manually.','|Parts were clamped in the jig Boring machine and the drilling operation was carried out.','|Pilot holes are drilled in the detail part machining stage itself.','Next batches verified and found ok.','','2018-10-15','op_sez(s)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Assembly','','FI','no','','Mahesh(N)','no','80128','|1) Stopped the assembly and informed the engineering team.\r\n2) Checked all the previously completed parts and found ok.','Z3456','qas|','2019-05-17|','2019-05-17',NULL,NULL,NULL,NULL,NULL,NULL),(11168,'56-040','GKN Aerospace Orangeburg','ROOT FITTING','786662 1B1','119A1210-604','NA','PSDL REV B',1,'A000044561','','81615','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','NO STOCK FOR FINISHING OPERATIONS. EXTRA MATERIAL REMOVED WHEN ROUGHING OPERATION','Improper tool holding \r\nDue to over hanging of tool and cutting force\r\n \r\n','|select the suitable tool and holder run the program with validated cutting forces.','|select the suitable tool and holder run the program with validated cutting forces.','CA/PA found ok','','2018-10-15','Karthineyan(V.S.)','op_sez(s)','','0000-00-00','MATERIAL UNWASH','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','3','no','Misc','pe_sez(a)','no','','|Informed to the supervisor and  engineering  team,\r\n','Z3456','pe|qas_sez|','2018-10-23|2019-02-01|','2019-02-01',NULL,NULL,NULL,NULL,NULL,NULL),(11169,'35A-357A','Saab AB','Latch Actuator Support Fi','','423Z1225-1-50','','---',3,'787 Forecast','','A15007','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Is condition:Parts returned from assembly line due to tight fit on meeting article in hole. See attached document 802040-00289736\r\n#1796: 22.21-22.217mm = 0.8744-0.8746\'\'\r\n#1798: 22.20-22.23mm = 0.8740-0,8752\'\'\r\n#1799: 22.23-22.24mm = 0,8752\'-0,8756\'\'\r\nShould be: Final hole size at 0.8745-0.8765\'\' in accordance to CDS-802-092\r\n','Quality inspector ensure the bore diameter by bore gauge instead of checking mandrill.','|Instruct to quality inspector & machine operator for using the mandrill to ensure the bore dia meter. ','|Q-Alert to be displayed at machining center & assembly department.','CAPA Found OK','C67540','2018-10-22','qas_sez(a)','qas_sez(a)','LB396815/GLB397664)','2018-10-22','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER END','yes','Misc','qas_sez(a)','no','','|no such parts found in FG.','Z3456','qas_sez|nagendra|','2018-10-22|2018-12-06|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11170,'35-618','Saab AB','SHAFT HANDLE ','M789340','D5227348520200','','PART ISSUE C',1,'OWED-LTA-004','','82064','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','OD Undersized by 0.02mm.','OD undersized |While the machining was in process suddenly power failure occurred|Due to power failure the executed program was forcefully stopped in the middle of the process.|As the program executed was incomplete due to power failure, re-pass was given to finish the operation. |While performing re-pass operation the OD got undersized','|Keep the tool up in ware offset |Keep the tool up in the ware and perform a idle/skin pass and then perform the operations.|Keep the tool up in the ware and perform a idle/skin pass and then perform the operations.','|Check the tool offset before processing |Check the tool offset and take a new offset again before performing the operations.  |Check the tool offset and take a new offset again before performing the operations.  ','CAPA found ok.','','2018-10-23','Dinakar(K)','Dinakar K()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','01','no','Misc','Dinakar K()','no','','|Checked the previous machined parts found all ok|Checked the previous machined parts found ok|Checked the previous machined parts found ok','Z3456','pe|||qas|','2018-10-24|2018-10-24|2018-10-24|2018-10-30|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11171,'35-481A','Saab AB','LOCK LEVER','C90875','D5227349820100','NA','PART ISSUE B',6,'OWED-LTA-003','','73794','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','ELECTROLYTIC ZINC-NICKEL PLATING Chip Off.','During receipt of parts, plating found to be shipping off.|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. ','CA PA found ok.','','2018-10-23','Yashawantha(NH)','Manu(P)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','DN44114','DN','no','Misc','Manu(P)','no','','|Informed to Supplier, verified parts at supplier end before dispatch to CIM. ','E3456','qas|qas|','2019-01-05|2019-01-06|','2019-01-06',NULL,NULL,NULL,NULL,NULL,NULL),(11172,'35-481A','Saab AB','LOCK LEVER','C90875','D5227349820100','NA','PART ISSUE B',10,'OWED-LTA-003','','73793','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','ELECTROLYTIC ZINC-NICKEL PLATING Chip Off.','','','','','','2018-10-23','Yashawantha(NH)','Manu(P)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','With Treatment','DN44113','DN','no','Misc','Manu(P)','no','','','E3456','qas|','2018-10-23|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11173,'35-480A','Saab AB','LOCK LEVER','C90875','D5227349820000','NA','PART ISSUE B',9,'OWED-LTA-003','','73791','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','ELECTROLYTIC ZINC-NICKEL PLATING Chip Off.','During receipt of parts, plating found to be  shipping off.|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 batches found ok.','','2018-10-23','Yashawantha(NH)','Manu(P)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','DN42780','DN','no','Misc','Manu(P)','no','','|Informed to Supplier, verified parts at supplier end before dispatch to CIM.','E3456','pe|qas|','2018-12-26|2019-01-06|','2019-01-06',NULL,NULL,NULL,NULL,NULL,NULL),(11174,'35-481A','Saab AB','LOCK LEVER','C90875','D5227349820100','NA','PART ISSUE B',7,'OWED-LTA-003','','73793','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','ELECTROLYTIC ZINC-NICKEL PLATING Chip Off.','During receipt of parts, plating found to be shipping off.\r\n\r\n|During transit parts have rub with one another|Due to insufficient packing.','|1)Improved the packing method. ','|1)Improved the packing method.\r<br/>2)Additionally packing sleeve will be put on the Outer surface of the part. ','CA PA found ok.','','2018-10-23','Yashawantha(NH)','Manu(P)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','DN44113','DN','no','Misc','Manu(P)','no','','|Informed to Supplier, verified parts at supplier end before dispatch to CIM. ','E3456','qas|qas|','2019-01-05|2019-01-06|','2019-01-06',NULL,NULL,NULL,NULL,NULL,NULL),(11175,'18-392B','Magellan Aerospace(Polska) Sp','END COVER','M940330/20715','D278 50167 200','','D',1,'104569','','79196','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Thickness undersized by 0.13 to 0.15mm. ','Thickness undersized |Due to part butting problem|Due to clogging of chips on the part butting face the part was not butt properly.|Supporting bush was not clamped properly','Clamp the the supporting bush properly.\r<br/>Instruction given to the operator. |<Dummy NC>','Frequently cleaning the part butting face to avoid the clogging of chips. |<Dummy NC>','CAPA FOUND  OK','','2018-10-23','Dinakar K()','Dinakar K()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','3','no','Misc','Dinakar K()','no','','checked the previous machined parts found ok|<Dummy NC>\r\n','E3456','pe|qas|','2018-10-23|2018-12-10|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11176,'35-712','Saab AB','LEVER','HR521404','D5227346720900','NA','PART ISSUE D',1,'OWED-LTA-004','','82496','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Wall thickness -side.. ','1.Running time chips present in holder so|2.while tool changing time chips placed on in between spindle and holder so tool runout occure,|3.In the part wall finishing time wall -ve side occure','|Every batch setting time clean the ATC arm and spindle ','|Training given to all three shift operators ,','CA PA FOUND OK','','2018-10-23','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','01','no','Misc','Prashanth Kumar(M)','no','','|stop the machine and check the previous parts ,all parts ok but current part wall -ve side by 0.02mm','E3456','pe|qas|','2018-12-18|2018-12-18|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11177,'35-711','Saab AB','LEVER','HR521404','D5227346720800','NA','PART ISSUE D',1,'OWED-LTA-004','','82492','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Thread mill dia over size','Inner diameter of the part got oversized.|CRC value given was not correct|Operator did not entered the the CRC value during the setting time and while cross checking the values he found that the CRC value was not entered then he entered the value to the machine with out pressing the reset button due to which the machine did not accepted the value included, later when the operator started the cycle the tool ran for the default CRC value and hence the part got rejected.|No Check point for the operator to ensure the data before starting the cycle.','|Corrected the crc value of the thread mill tool and continued the production.','|1) 1st off operation will be carried out on the dummy material before doing it on the part.\r<br/>2) Setting flow chart will be displayed near the machine.\r<br/>3) Message alert will be added on the program to remind operator to set and check the CRC.','CAPA found ok','','2018-10-23','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Prashanth Kumar(M)','no','','|Immediately stopped the machine and checked the reference values of all the tools and found ok.','E3456','pe|qas|qas|qas|','2018-12-17|2018-12-19|2018-12-19|2018-12-19|','2018-12-19',NULL,NULL,NULL,NULL,NULL,NULL),(11178,'18-778A','Magellan Aerospace Wrexham','BRACKET AFT M/C','A0088Y','F57551860200','NA','PART ISSUE A',1,'RP174264','','78156','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dia6.35mm hole over size, 				\r\n','while doing dia 6.35 mm hole deburing dia 7 mm drill used by that hole got over size.				\r\n','|From next batch dia10 drill will be used for deburing by that hole cant get over size and finish will. ','| Training has been given to take care will deburing.\r<br/>\r<br/>Before starting the work instruction will be given.	\r<br/>','Next batches produced found ok.','','2018-10-23','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','no go answer','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','01','no','Misc','Krishna(Chowdary.G.P.)','no','','|Changed the debarring tool dia 10mm and continue the production. 							\r\n','E3456','pe|qas|','2018-11-07|2018-12-10|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11179,'18-779A','Magellan Aerospace Wrexham','BRACKET AFT M/C','A0088Y','F57551860201','NA','PART ISSUE A',1,'RP174264','','78159','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','part width under size','1.During milling operation  width was getting under size|2.Offset wrong occurred |3.Operator made mistake during offset taken on part','|Training will be given to the operator','|Training record to be maintain','CAPA found ok','','2018-10-23','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','part width under size','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','01','no','Misc','Krishna(Chowdary.G.P.)','no','','|The offset was corrected','E3456','pe|qas|','2018-12-19|2018-12-19|','2018-12-19',NULL,NULL,NULL,NULL,NULL,NULL),(11180,'51A-083A','THE BOEING COMPANY','BRACKET ASSY','','332A2930-7','','PSDL REV B',6,'BOEING 001U','','A17852','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','HOLE OVERSIZE NOGO ANSWERING 9.54mm','REFER NC NO:10806.','|REFER NC NO:10806.','|REFER NC NO:10806.','REFER NC NO:10806.','','2018-10-23','qas_sez(a)','qas_sez(a)','','0000-00-00','HOLE OVERSIZE NOGO ANSWERING 9.54mm','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Assembly','','FINAL INSPECTION','no','Misc','qas_sez(a)','no','','|REFER NC NO:10806.','Z3456','qas_sez|','2019-01-16|','2019-01-16',NULL,NULL,NULL,NULL,NULL,NULL),(11181,'51A-142','THE BOEING COMPANY','CLEVIS FITTING ASSY - LOW','','112A7112-608','','PSDL REV B',1,'BOEING 001W','','A18953','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','bore over size','While performing the boring operation ovality occurred.|Preformed the operation in the end mill.|Performed in end mill due to boring holder and boring bar was not available.','|Moved the parts to JIG BORING','|Operation will be performed in JIG BORING machine.','CAPA found ok.','','2018-10-24','Lohith(K)','Jayarama(M.B.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Assembly','','6','no','Misc','Lohith(K)','no','M07374','|Immediately stopped the production. ','E3456','pe|qas|','2018-10-24|2019-01-28|','2019-01-28',NULL,NULL,NULL,NULL,NULL,NULL),(11182,'35-650A','Saab AB','SHAFT','B76568','D5227346820200','NA','PART ISSUE C',4,'PA1687 LTA-2','','72059','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','D5227346820200 Shaft\r\nIs condition: Shaft is out of tolerance, Shaft is measured to 5.01 mm. (detail B on drawing) Surface treatment seems incorrect, very dark in color. See attached picture.\r\nShould be: Shaft should be 4,940-4,986 mm according to drawing. Surface treatment should be metallic blue according to AIPS 02-04-006.\r\n\r\nD5227280720000 Shaft-1\r\nIs condition: Outside diameter of the two long cylindrical part is out of tolerance (too large). It is the part closest to the edge that is most outside of tolerance. The two cylindrical parts are both slightly conical. Meeting part does not fit.\r\nThe returned SHAFT 1 are: between 7.93-7.97 mm. See photo.\r\nShould be: The larger diameter of SHAFT 1 shall be: 7.875 - 7.936 mm.','1) Outer Diameter of part D5227280720000 was measuring beyond upper limit after nickle platting.\r\n2) Parts from part no D5227280720000 were measuring out of tolerance after platting and were shipped to customer.|1) The Diameter of the part gets increased gradually from the mid of the part towards the edges therefore the edges of the part are measuring out of tolerance.\r\n2) Parts were inspected and found acceptable according to the drawing and specification.|1) Due to accumulation of current at the edges the nickel platting thickness at the edges gets increased.\r\n2) According to Section 5.2.1.1 in AIPS-02-04-006 the thickness of platting needed to be measured not less than 6mm from any edge(Refer Below Snippet) according to which the parts were measured and found confirming.','|Trials are being carried out at TPL to reduce the platting thickness to maintain the thickness to the lower limit so that the part suits best in the assembly.','|Trials are being carried out at TPL to reduce the platting thickness to maintain the thickness to the lower limit so that the part suits best in the assembly.','Reason accepted by customer and cancelled the NC.','C66935','2018-10-25','Sathish(G)','Dharani(Shankar)','OF-003265','2018-10-19','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','yes','With Treatment','DN41971','Cust End','no','Misc','Yashawantha(NH)','no','','|Immediately informed the supplier and 100% inspection of in process part and Source inspection was carried out.','E3456','qas|','2019-01-30|','2019-01-30',NULL,NULL,NULL,NULL,NULL,NULL),(11183,'35-464','Saab AB','FITTING','932489A','D522 73408 201 00','','A',3,'OWED-LTA-001','','81171','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','rib thickness undersized ','Rib thickness undersized|The rib thickness was undersized as their was a step on the part and had to remove the the step in the polishing process due to over polishing the thickness was undersized|The fitter thought that their was enough stoke to remove the step on the part.|No instruments where provided to check the part thickness,so the fitter was not having the knowledge of the remaining stock.','|Check each part before performing polishing with the help of micrometer.\r<br/>\r<br/> ','|Use the drawing while performing the process.\r<br/>Training has been given to the fitters to maintain the dimensions with in the tolerance.','CAPA found ok.','','2018-10-25','pe_sez(a)','pe_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','Fitting','no','Misc','pe_sez(a)','no','','|Checked the previous polished parts found ok.','Z3456','pe_sez|qas|','2018-11-12|2018-12-01|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11184,'18-123A','Magellan Aerospace Bournemouth','FORK END OUT BD','CD703008/08180B','PID575 41546 202','','B',1,'428864','','79016','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Refer NC NO:10744','Refer NC NO:10744','|Refer NC NO:10744','|Refer NC NO:10744','Refer NC NO:10744','','2018-10-26','qas_sez(a)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','DN46465','POST TREATMENT','no','Misc','Dharani(Shankar)','no','','|Refer NC NO:10744','Z3456','qas_sez|','2019-01-16|','2019-01-16',NULL,NULL,NULL,NULL,NULL,NULL),(11185,'35-231A','Saab AB','HINGE BRACKET 4 ','5879601 1','D576 50007 208','','E00',1,'1600223433/Forecast ','','81964','','0000-00-00',NULL,'yes','no','no','no','yes','yes','no','no','no','UNDER CUT OVER SIZE OBSERVED IN THE CORNER RADIUS ','','','','','','2018-10-26','pe_sez(a)','Umesh B,Nataraja C V,NataRaj.CV ,Diwakar R.B.,','','0000-00-00','UNDER CUT OVER SIZE OBSERVED IN THE CORNER RADIUS ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','','FI','yes','i700-3','qas_sez(a)','no','','','Z3456','qas_sez|qas_sez|','2018-10-26|2018-10-30|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11186,'35-598','Saab AB','CORNER','532701A','D5227338620300','NA','PART ISSUE B',1,'OWED-LTA-001','','82335','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Refer NC NO:10744','Refer NC NO:10744','|Refer NC NO:10744','|Refer NC NO:10744','Refer NC NO:10744','','2018-10-26','qas_sez(a)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','DN47799','POST TREATMENT','no','Misc','Dharani(Shankar)','no','','|Refer NC NO:10744','Z3456','qas_sez|','2019-01-16|','2019-01-16',NULL,NULL,NULL,NULL,NULL,NULL),(11187,'18-742A','Magellan Aerospace Wrexham','STRIP','63026/02','F57252299204','NA','A',1,'176541','','78524','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Wall thickness dig mark....','1) Error in the generated Program.|2) Input parameters given during the program generation was not correct.\r\n|3) Engineer did not verified the approach value during the programing time.','|1) Changed the approach value in the program and regenerated the program.','|All the NC programs will be Simulated and the reports from the simulation program will be verified before providing the program to the machine.','CA/PA Found satisfactory.','','2018-10-27','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','01','no','Misc','Prashanth Kumar(M)','no','','|Immediately Stopped the machine and checked the program and informed the engineer about the error in program.','E3456','qas|nandishkumardk|','2018-10-29|2018-11-27|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11188,'18-745A','Magellan Aerospace Wrexham','STRIP','63026/02','F57252299212','NA','A',1,'176541','','78527','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Wrong program running. ','1) Wrong tool no called in the machine.|2) Operator did not ensured the tool dia. to the M.P.S. requirement while loading to the machine.|3) No proper validation process was available to validate whether proper tool no is called out in the program in the machine.','|1) Instructed the operator to verify the tool no called in the program before starting the production.','|1) Introducing Check list to verify the basic machining parameters which the operator need to verify and the supervisor need to certify before starting the production.\r<br/>','CA/PA Found satisfactory.','','2018-10-27','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','01','no','Misc','Prashanth Kumar(M)','no','','|Immediately stopped the machine and changed the tool no and continued the production.','E3456','qas|pe|nandishkumardk|','2018-10-29|2018-10-29|2018-11-27|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11189,'35-166B','Saab AB','HOUSING PIN ','708183B9','423Z1124-6-01','','--B',1,'1600181656','','80406','','0000-00-00',NULL,'yes','no','yes','no','yes','no','no','no','no','Wall dig during machining of 1.49mm.','Machine ball screw problem.\r\nalarm:\r\n1. 549-internal feed error detected.\r\n2. 103-x axis position error.','|Replace the new ball screw and run the machine. ','|Replace the new ball screw and run the machine. ','CAPA FOUND OK','','2018-10-29','Dinesh kulal()','prodn_aero(prodn)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','Production','no','Misc','Dinesh kulal()','no','','|Informing to HAAS service engineer. and stop the machine.','A3456','prodn_aero|qas_aero|','2018-11-02|2018-11-27|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11190,'51A-082','THE BOEING COMPANY','BRACKET ASSY','','332A2930-1','','PSDL REV B',1,'BOEING 001M','','A18432','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Refer NC NO:10744','Refer NC NO:10744','|Refer NC NO:10744','|Refer NC NO:10744','Refer NC NO:10744','','2018-10-29','pe_sez(a)','pe_sez(a)','','0000-00-00','STEP FOUND','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Assembly','','FINAL INSPECTION','no','Misc','qas_sez(a)','no','','|Refer NC NO:10744','Z3456','qas_sez|','2019-01-16|','2019-01-16',NULL,NULL,NULL,NULL,NULL,NULL),(11191,'35-618','Saab AB','SHAFT HANDLE ','M789340','D5227348520200','','PART ISSUE C',1,'OWED-LTA-004','','82064','','0000-00-00',NULL,'yes','yes','yes','','','','','','','DUMMY part used for trial purpose.','DUMMY part used for trial purpose.','|DUMMY part used for trial purpose.','|DUMMY part used for trial purpose.','DUMMY part used for trial purpose.','','2018-10-29','Rangaswamy()','        Manu K','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','5','','','','','','|DUMMY part used for trial purpose.','Z3456','pe_sez|pe_sez|qas_sez|','2018-11-22|2018-12-19|2019-01-18|','2019-01-18',NULL,NULL,NULL,NULL,NULL,NULL),(11192,'47-121A','GKN Aerospace Filton','CROSS MEMBER AFT M/C','1013901 3','F57550098201','NA','PART ISSUE C01',1,'GS68-LTA-1-2018','','73695','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','yes','WRONG PART NUMBER','1) LH Part was Shipped to customer instead of RH part.|2) LH part was packed instead of RH part mistakenly by the packing person. |3) Assembly personnel didn\'t verified the part marking details along with the COC details.|4) The person involved in the packing of part was not sufficiently trained to interpret the details.','|Trained all the personnel in the packing to how and what are the details to be verified while packing the parts for shipment.','|4 Eye check method implemented to verify the parts packed.','Next batch shipments monitored and found ok.','C69246','2018-10-29','Manohara(M)','Manohara(M)','201136531','2018-09-28','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','With Treatment','DN42042','Cust End','no','Misc','qas(qas)','no','','|Shipped the correct part at zero invoice to the customer during the next shipment.','E3456','qas|','2018-10-29|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11193,'35-160','Saab AB','STOP SUPPORT','853181-06','423Z6188-5','','---',1,'Forecast po for B787','','82349','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Refer NC NO:10744','Refer NC NO:10744','|Refer NC NO:10744','|Refer NC NO:10744','Refer NC NO:10744','','2018-10-30','Rangaswamy()','        Karthik Raj T ','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','3','','','','','','|Refer NC NO:10744','Z3456','pe_sez|qas_sez|','2018-11-22|2019-01-16|','2019-01-16',NULL,NULL,NULL,NULL,NULL,NULL),(11194,'35A-601','Saab AB','FRAME ASSY','','D5227338501000','','PART ISSUE C',1,'OWED-LTA-001','','A17131','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','yes','Is condition: See attached pictures GLB-390338-Sketch\r\n#1     Some kind of corrosion or residue from ?\r\n#2-3  Too much sealant around and in Bushing, w/o A17131, A17132, A17133 \r\n#4      Sealant has not squeezed into enough in Anchor nut, w/o A17131, A17132, A17133 \r\n\r\nShould be:  Without any sealant residue, Suspected Corrosion, or Sealant missing.\r\n\r\nTotal Qty: 34','1) Improper application and improper cleaning of sealant.|2) Excess sealant was applied during the assembly operation and the excess squeezed out sealant was not completely removed after the completion of assembly. |3) In the earlier method the fillet formation during the squeeze out was not uniform therefore the assembly operator applied excess sealant and missed to wipe out the excess sealant from the bore.|4) operator and the inspector missed to ensure the complete removal of excess sealant from the bore after the completion of assembly.|5) The assembly operator and the inspector visually inspected the fillet formation and the completion of operations and any chip-offs but not the removal of sealant inside the bush as there was no dimensional requirements to be maintained on the bush the concentration on these areas was less. ','|Instructed all the assembly operator and the quality inspector to verify the proper and complete removal of sealant from the unneeded areas.','|Quality alert is displayed on the assembly area to create awareness on the improper cleaning of the sealant from bore after assembly.','Next Batches manufactured found ok.','C67468','2018-10-30','Sathish(G)','Dharani(Shankar)','OF-003153','2018-08-30','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','Cust End','yes','Misc','qas_sez(a)','no','','|Checked all the in-process and completed parts and no similar defects was identified. ','E3456','qas|','2018-10-30|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11195,'18-032A','Magellan Aerospace(Polska) Sp','BUSH','1638723-2/W8KC','PID278 50165 200','','A',34,'104569','','81244','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Out of 1340 no\'s 1 No identified with total length under size by 0.6mm beyond tolerance, 7No\'s Face chattering, 26No\'s OD undersized from 0.006mm to 0.007mm beyond tolerance.','1) operator did not identified the deviated parts during the machining.|2) Operator did sampling inspection of once in 20No\'s cycle and did not checked the dimensions during the insert change.|3) During the sampling inspection the part were found ok and due to improper insert life monitoring the intermediate parts are deviated and left unidentified.','|1) Changed the Sampling method from 20No\'s to 100% inspection.\r<br/>2) Proper Insert life monitoring chart displayed near the machine.','|1) Instructed all the operator to carry out 100% inspection and monitor the tool life properly.\r<br/>2) Instructed all the supervisors to strictly monitor the tool life monitoring chart for proper updates.\r<br/>3) Awareness training to be provided to the operators on the tool life monitoring.','capa found ok','','2018-10-30','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','FI','no','Misc','Narasimha Murthy(R)','no','','|Re-inspected all the parts and no similar parts are identified.','E3456','qas|qas|','2018-10-30|2018-11-28|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11196,'35-604','Saab AB','SHAFT , VENT HOOKS','2878','D5227352920200','NA','PART ISSUE B',40,'OWED-LTA-004','','81911','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Total Run out required 0.1mm, measuring 0.25mm.','The concept of measuring the run out was not enough to the inspector|The part was not butted properly while checking the run out','|1.On-Job training provided to all the inspector on checking method of GD&T parameters.','|Refer CA','Next batch machined parts found OK.','','2018-10-30','qas_sez(a)','Dinakar K ,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','With Treatment','','FI','no','100MY-01','qas_sez(a)','no','','|1.All the parts was reinspected by the senior inspector and run found within the limits.\r\n2.Parts accepted','Z3456','qas_sez|qas_sez|','2018-12-20|2019-04-16|','2019-04-16',NULL,NULL,NULL,NULL,NULL,NULL),(11197,'35-604','Saab AB','SHAFT , VENT HOOKS','2878','D5227352920200','NA','PART ISSUE B',28,'OWED-LTA-004','','81913','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Total Run out required 0.1mm, measuring 0.25mm.','The concept of measuring the run out was not enough to the inspector|The part was not butted properly while checking the run out','|1.On-Job training provided to all the inspector on checking method of GD&T parameters. ','|\r<br/>Refer CA ','Next batch machined parts found OK. ','','2018-10-30','op_sez(s)','Sagar C.V,Dinakar K ,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','With Treatment','','FI','no','100MY-01','qas_sez(a)','no','','|1.All the parts was reinspected by the senior inspector and run found within the limits. 2.Parts accepted ','Z3456','qas_sez|qas_sez|','2018-12-20|2019-04-16|','2019-04-16',NULL,NULL,NULL,NULL,NULL,NULL),(11198,'35-672','Saab AB','SHAFT LEVER ','521026A2','D5227346221900','NA','PART ISSUE D',2,'OWED-LTA-001','','80481','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','PART DAMAGED DURING CHEMICAL PROCESS','','','','','','2018-10-31','qas_sez(a)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','DN46787','POST TREATMENT','no','Misc','qas_sez(a)','no','','','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11199,'51-096','THE BOEING COMPANY','U JOINT','G23552K07','65B80423-3','NA','PSDL REV -',1,'BOEING 001Y','','81008','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','Total length undersized because of program fault.','','','','','','2018-10-31','pe_sez(a)','op_sez(s)','','0000-00-00','\"CAD\" program fault, \"total length\" undersized','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Cancelled','no','yes','no','With Treatment','','03','no','Misc','pe_sez(a)','no','','','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11200,'46-017A','Mahindra Aerostructures Pvt.Ltd','STRAP','9819202 3','D575-40864-201','NA','J01, ECN NG26090ST1KC54',1,'MAPL forecast 2018','','81513','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','PART ACCEPTED QTY:1','PART ACCEPTED QTY:1','|PART ACCEPTED QTY:1','|PART ACCEPTED QTY:1','PART ACCEPTED QTY:1','','2018-10-31','qas_sez(a)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','With Treatment','DN47207','POST TREATMENT','no','Misc','Mahesh(N)','no','','|PART ACCEPTED QTY:1','Z3456','qas_sez|qas_sez|','2018-11-13|2018-11-13|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11201,'34-027D','Magellan Aerospace Winnipeg','SPACER','G23322K01','400-12618-1-905','NA','EM104302 Iss B, EM104765 Iss H, EM105092 Iss H, EM106399 Iss B, EM106400 Iss B, EM106401 Iss B, EM106404 Iss A, EM106522 Iss A, EM106602 Iss A ',1,'C81597 Rev 001','','81462','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','id over size.','Drill broken during the ID operation.|Drill was used under trial to reduce the cycle time hence while changing the feed and speed the tool burned out and got broken.|The drill used was made of MS and hence due to high cutting parameters the tool got broken.','|1) Informed the operator to continue the production with the old cutting parameters.\r<br/>2) Informed the Operator to ensure the tool wear once in every 5 parts and change the tool if any wear in edge is observed.','|Informed the tooling department to provide carbide tool for Id operations which can withstand high cutting strategies.','CAPA found ok.','','2018-10-31','Ravi(M)','Ravi(M)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','05','no','Misc','Ravi(M)','no','','|Immediately stopped the machine and changed the new tool and checked the previous machined parts and found ok.','E3456','qas|','2018-11-02|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11202,'18-722A','Magellan Aerospace(Blackpool) Limited','SLAVE LINK UPPER','1426','PI 55-3569004-00','','PART REV PDM3',3,'BPP-529619 amed-1','','82373','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','od under size by -0.2mm.','1) While part running time the SIM used under the insert got loosed due to which the OD got undersized, and the operator did not checked the part.|2) The tool was previously used in roughing operation in another machine and then the tool was removed from the previous machine and then loaded to the machine and continued the production without checking the tightness of the SIM.|3) Operator did not checked all the parts immediately after the completion of operations because of which the operator did not identified the looseness of the SIM. ','|1) Removed the tool holder and changed the screw of the SIM and tightened the SIM and retaken the offset and continued the production.\r<br/>2) Informed the operators to ensure the SIM tightness and all required parameters during the setting operation and specially when borrowing tool from another machine. ','|1) Spare tool will be issued to the machine to avoid the movement of tools from machine to machine.\r<br/>2) Informed to operator to ensure the SIM tightness once in every 5 Parts.','CAPA found OK and implemented immediately.','','2018-10-31','Ravi(M)','Ravi(M)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','03','no','Misc','Ravi(M)','no','','|Immediately stopped the machine and checked all the previously completed parts and identified two more parts with similar deviation.','E3456','qas|','2018-11-02|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11203,'35-480A','Saab AB','LOCK LEVER','C90875','D5227349820000','NA','PART ISSUE B',1,'OWED-LTA-003','','73348','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','no','Wrong specification masking tape was used.','Refer Customer CA NO:CA1245692-00,Date Issued 20-Feb-2018.','|Refer Customer CA NO:CA1245692-00,Date Issued 20-Feb-2018.','|Refer Customer CA NO:CA1245692-00,Date Issued 20-Feb-2018.','Refer Customer CA NO:CA1245692-00,Date Issued 20-Feb-2018.','C70399','2018-11-02','Dharani(Shankar)','Dharani(Shankar)','mail','2018-10-31','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','With Treatment','DN44120','CUSTOMER END','no','Misc','qas_sez(a)','no','','|Refer Customer CA NO:CA1245692-00,Date Issued 20-Feb-2018.','Z3456','qas_sez|qas_sez|','2019-01-18|2019-01-18|','2019-01-18',NULL,NULL,NULL,NULL,NULL,NULL),(11204,'35-585A','Saab AB','HANDLE','2290601','D5227342720200','NA','PART ISSUE D',2,'OWED-LTA-005','','82036','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Part loading mistake.','1) Operator ran the same program on the same part second time without taking reference.|2) During the first time the part was not loaded properly (one end was loaded on the higher point of contact and the other side was loaded on the lower point).|3) No proper Fool proof method was allotted to avoid the improper loading of part.','|Immediately stopped the production and provided the butting block to the vice and continued the production.','|Clamping fixture to be redesigned by providing base height and guiding pins to lock the features and avoid similar occurrence.','Effectiveness will be updated on 14-Nov-2018 by authorized QAD.\r\nImplementation verified and found ok.','','2018-11-02','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','01','no','Misc','Prashanth Kumar(M)','no','','|Immediately stopped the production and Checked the previously completed parts and reworked the defected part.','E3456','pe||nandishkumardk|qas|','2018-11-02|2018-11-02|2018-11-12|2018-12-18|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11205,'35-526','Saab AB','ROD BODY','2878','D522 73337 200 00','','A',1,'OWED-LTA-001','','81921','','0000-00-00',NULL,'yes','yes','yes','','','','no','','','DUMMY NC ','DUMMY NC ','|DUMMY NC ','|DUMMY NC ','DUMMY NC ','','2018-11-02','Dinakar K()','        Dinakar K ','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','','','','05','','','','','','|DUMMY NC ','Z3456','pe_sez|qas_sez|','2018-11-20|2019-01-18|','2019-01-18',NULL,NULL,NULL,NULL,NULL,NULL),(11206,'51-116','THE BOEING COMPANY','BEAM - INBOARD NACELL, WI','209917B4','116U3250-13','NA','PSDL REV -',1,'BOEING 001Y','','81006','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','The profile of the part had a deviation than the actual part configuration','The tool has removed the material during the rapid movement from one position to other position|The Retract height of the tool was not moving the tool out to the safe zone before going to the next start point|Programs were merged without considering the two different retract heights|The safety Retract height given during the programming was wrong','|Each Toolpath was verified for the correctness by Simulation verification. Retract Value must be considered when merging different tool path with the single cutting tool if the retract height is altered manually while programming','|Maintain a standard retract height by using tool path templates while programming.','CA/PA Found satisfactory.','','2018-11-02','Ramesh(Poojary)','                Ramesh(Poojary)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','11','no','Misc','Narayanappa(G)','no','','|Part identified as rejected. The safety retract height for all the programs was cross verified and was found okay','E3456','cam|qas|Deshpande|cam|nandishkumardk|','2018-11-15|2018-12-19|2019-10-18|2019-10-30|2019-11-05|','2019-11-05',NULL,NULL,NULL,NULL,NULL,NULL),(11207,'35-526','Saab AB','ROD BODY','2878','D522 73337 200 00','','A',1,'OWED-LTA-004','','81918','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Refer NC NO:10744','Refer NC NO:10744','|Refer NC NO:10744','|Refer NC NO:10744','Refer NC NO:10744','','2018-11-03','pe_sez(a)','                Pradeep B.D','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','07','','','','','','|Refer NC NO:10744','Z3456','pe_sez|pe_sez|qas_sez|','2018-11-03|2018-11-22|2019-01-16|','2019-01-16',NULL,NULL,NULL,NULL,NULL,NULL),(11208,'35-526','Saab AB','ROD BODY','2878','D522 73337 200 00','','A',1,'OWED-LTA-004','','81918','','0000-00-00',NULL,'yes','yes','yes','','','','','','','part rotated(dia 10r2bn tool) running,so dig mark found on 1no...','DUE TO OD UNDER SIZE, THE PART WAS NOT CLAMPED PROPERLY IN THE SET OF 4 NOS AT A TIME MACHINING|THE OPERATOR NOT CROSS CHECK THE OD VALUE BEFORE LOADING','|1.THE GAB BETWEEN THE TOP CLAMPS AND THE FIXTURE FACE IS ENSURED BY USING FEELER GAUGE\r<br/>\r<br/>\r<br/>2.SAME OD VALUE PARTS ARE LOADED','|THE OPERATOR IS REQUESTED TO CHECK THE OD VALUE BEFORE LOADING AND TO CLAMP THE UNIFORM OD VALUE PARTS IN ONE SET.','CA/PA satisfied.','','2018-11-03','pe_sez(a)','        Pradeep B.D','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','07','','','','','','|PRODUCTION HOLD UP. ALL PARTS OD VALUE CROSS CHECKED','Z3456','pe|pe_sez|qas_sez|','2018-11-03|2018-11-27|2019-01-07|','2019-01-07',NULL,NULL,NULL,NULL,NULL,NULL),(11209,'51A-003','THE BOEING COMPANY','LOWER BEAM FWD INBD SPLIC','','315Z1302-1501','','NIL',1,'BOEING 001K','','A19158','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','CSK DIAMETERE OVERSIZE','AFTER ASSEMBLY RIVET FLUSHNESS SHOULD BE 0.00/0.25 MM AS PER THE REQURIMENT|TO ACHIVE THIS FLUSHNESS CSK IS DONE MANUALLY AFTER TREATMENT TO SUIT THE RIVET PARAMETERS|OPERATOR WAS NOT AWARE OF HOW MUCH DEPTH THE CSK HAS TO BEEN DONE TO ACHIVE THE FLUSHNESS|SETTING PART ,OPERATOR WHILE SETTING THE DEPTH OF CSK HAS GIVEN MORE DEPTH|WRONG SELECTION OF CSK TOOL','|1.CORRECT TOOL WAS SELECTED FOR DOING THE CSK OPERATION.\r<br/>2.CORRECT DEPTH WAS SETTED TO ACHIVE THE FLUSHNESS AFTER ASSEMBLY','|1.A SEPARATE TOOL SET IS IN PLACE AND IDENTIFIED , PARTICULARLY FOR SUCH MANUAL OPERATION FOR ASSEMBLY.\r<br/>2.INSTRUCTION GIVEN TO THE OPERATOR TO MAINTAIN STOCK FOR THE FIRST SETTING PART AND TAKE CLEARANCE FROM THE QA DEPARTMENT\r<br/>3.FIXTURE WILL BE PLANNED FOR HOLDING THE PARTS WHILE PERFORMING THE CSK OPERATION ','NEXT PART CSK AND ASSEMBLY DONE FOUND THE FLUSHNESS AND THE RIVET PARAMETERS WAS WITHIN THE SPECIFICATION.','','2018-11-03','pe_sez(a)','Karthik Raj T()','','0000-00-00','CSK maximum side','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Assembly','','05','no','Misc','pe_sez(a)','no','','|THE PART WAS IDENTIFIED AND REJECTED AND NCR WAS RAISED INTERNALLY','Z3456','qas_sez|','2019-01-24|','2019-01-24',NULL,NULL,NULL,NULL,NULL,NULL),(11210,'35-600','Saab AB','FRAME','3810602','D5227338520400','NA','PART ISSUE C',1,'OWED-LTA-001','','81626','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Part profile shift 0.6.','1) Due to improper movement in y-axis the profile got shifted.|2) During roughing operation excess chips got placed over the bed, due to which the axis movement got affected.|3) No cleaning method implemented after the roughing operation.','|Cleaned the machine bed and continued the production.','|informed all the operators to remove the chips from machine bed after the completion of roughing operation.','CA PA implementation found effective.','','2018-11-03','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Punith G(S)','no','','|immediately stopped the machine and checked the previously finished parts and found ok.','E3456','qas|','2018-12-18|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11211,'35-601','Saab AB','FRAME','4215601','D5227338520600','NA','PART ISSUE C',1,'OWED-LTA-001','','81635','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Web thickness 0.4mm getting undersize','why1. During rib top profile milling operation excess amount of material removed top surface due to that which was getting undersized|why2. The tool on Z axis direction moved into downwards|why3. The chips were blocked on ATC before loaded into tool holder due to that tool height Z value changed|why4. The empty pockets are available on machine during milling operation chips flowed on the empty pockets |why5. Due to that chips blocking on ATC tool downwards occurred on Z axis','|All ATC pockets to be filled with tool holders and that to be avoid chips blocking on ATC pockets.\r<br/>After every roughing cycle operation operator needs to be clean the tool pocket.','|Install chips guard to prevent chips from entering inside the tool pocket ','Effectiveness will be provide on 20-11-2018.\r\nImplementation verified and found ok.','','2018-11-03','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','05','no','Misc','Punith G(S)','no','','|The tool holder is removed and the chips were cleaned and the remaining parts checked and ensured ok','E3456','nandishkumardk|qas|','2018-11-13|2018-12-18|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11212,'35-601','Saab AB','FRAME','4215601','D5227338520600','NA','PART ISSUE C',1,'OWED-LTA-001','','81635','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Part rib top radius unclear. ','why1. During rib top profile milling operation excess amount of material removed top surface due to that which was getting undersized|why2. The tool on Z axis direction moved into downwards|why3. The chips were blocked on ATC before loaded into tool holder due to that tool height Z value changed|why4. The empty pockets are available on machine during milling operation chips flowed on the empty pockets|why5. Due to that chips blocking on ATC tool downwards occurred on Z axis','|All ATC pockets to be filled with tool holders and that to be avoid chips blocking on ATC pockets.\r<br/>After every roughing cycle operation operator needs to be clean the tool pocket.','|Install chips guard to prevent chips from entering inside the tool pocket','Effectiveness will be provide on 20-11-2018.\r\nImplementation verified and found ok.','','2018-11-03','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Punith G(S)','no','','|\r\nThe tool holder is removed and the chips were cleaned and the remaining parts checked and ensured ok','E3456','qas|qas|','2018-11-13|2018-12-18|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11213,'35-644A','Saab AB','LATCH FORK','HR521404','D5227348920400','NA','PART ISSUE C',2,'OWED-LTA-004','','79752','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Bore dimension measures 18.95mm instead of 18.8 E7','WHY1. During 2nd setup of machining process bore dial gauge setting was made wrong|WHY2. The chosen setting bore dial gauge least count is 0.01mm instead of 0.001mm |WHY3. Due to that pressure was set into 0.5mm instead of 0.05mm on bore dial gauge.|WHY4. Due to that improper selection of dial gauge 0.15mm oversize occurred on part','|The checking method is changed into Air Gauge instead of setting of Bore dial gauge','|Training will be given to the operator regarding boring bar operation and boring bar adjustment then that soft copy will be submit to the Quality Clinic','Training record will be submit on 16-11-2018\r\nAir Gauge application from Jan 2019\r\nTool life monitoring record 16-11-2018.\r\nImplementation verified and found ok.','','2018-11-05','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Prashanth Kumar(M)','no','','|The parts which were all completed in second setup boring operation that was checked and ensured ok','E3456','nandishkumardk|qas|','2018-11-13|2018-12-18|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11214,'35-404','Saab AB','BEAM 2','532390B2','D522 73392 200 01','','A',2,'OWED-LTA-001','','80321','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','A chips in boring bar holder while tool changing by CNC mode in the machine so tool becomes run out\r\nand bore over size. ','A chips in boring bar holder while tool changing by CNC mode in the machine so tool becomes run out and bore over size.|operator did not notice the chips in the boring holder. |The chips was very minimal and was not visible to the operatoe.|\r\n','|Inform to operator boring operation running before clean the tool pockets and spindle.\r<br/>Every time boring operation running clean the ATC arm.','|1) M0 optional program stop was provided in the program.\r<br/>2)Training provided to all operators and supervisors for visual inspections in the intermediate CNC stop to ensure no chips in the bore and tool.\r<br/>3)The same above alert was displayed near the machine','Next 3 parts machine in the same workorder and  found bore was measuring within the tolerance ','','2018-11-05','Mr.Lohit','Thaveni D M()','','0000-00-00','Bore over size','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','05','no','Misc','pe_sez(a)','no','','|\r\nM00 COMMAND intermediate stop or optional stop was given in the program to ensure if any chips in tools and for tool cleaning.','Z3456','qas_sez|','2019-04-12|','2019-04-12',NULL,NULL,NULL,NULL,NULL,NULL),(11215,'51A-071','THE BOEING COMPANY','FITTING ASSY, OUTBD','','112T7057-4','','PSDL REV -',1,'BOEING 001Q','','A16084','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','no','Paint Thickness over size by 0.03 mm ','the requirement of the paint for this parts was single coat ,but the parts were painted for 2 coats.|Painter was in an assumption that the requirement is 2 coat for this part|Painter dint study and  follow the Routing requirement','|Supplier has given training to there Painters on referring the Routing and requirements of painting.','|Refer to CA','CAPA found Satisfactory','','2018-11-05','qas_sez(a)','qas_sez(a)','','0000-00-00','Paint thickness oversize.','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER','yes','Misc','qas_sez(a)','yes','','|1.The parts were moved to quarantine and Rework NCR was raised.\r\n2.The parts were sent back to the supplier as request by the supplier for rework of paint.','Z3456','qas_sez|','2019-04-12|','2019-04-12',NULL,NULL,NULL,NULL,NULL,NULL),(11216,'18-411A','Magellan Aerospace Bournemouth','PLUNGER','771908','D321 40205 200','','H01',7,'423245','','72107','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','OD UNDER SIZE.','WHY1. During semi finishing operation extra material removed|WHY2. semi finishing operation offset value getting wrong|WHY3. Manual typing error occurred on  semi finishing offset value','|During insert changing process semi finished diameter to be check and maintain from tools offset value ','|Training will be provide to Operator','Training record will be provide on 20-11-2018.\r\nCAPA found ok.','','2018-11-05','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Ravi(M)','no','','|Offset value corrected and remaining parts checked and verified ok','E3456','qas|qas|','2018-11-16|2018-12-18|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11217,'18-075A','Magellan Aerospace Wrexham','ADAPTOR','M061590/27262','D282 50044 200PF','','A',1,'175162','','79632','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','FACE UNCLEAR.','Raw material cutting was cross cutting.|Because of cross cutting the face was unclear. |Operator did not notice the cross cutting face while issued by the stores.','|A master piece will be maintained for the required size.','|Have informed the stores to avoid cross cutting.\r<br/>To change the blade frequently.\r<br/>Check each part before machining with the master.','CAPA found ok.','','2018-11-05','Narasimhamurthy(K.G.)','Narasimhamurthy(K.G.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','01','no','Misc','Ravi(M)','no','','|Checked the previous machined parts found ok.','E3456','pe|qas|','2018-11-30|2018-12-18|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11218,'51A-068','THE BOEING COMPANY','FITTING ASSY, INBD','','112T7057-1','','PSDL REV -',1,'BOEING 001Q','','A19824','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','HOLE CO ORDINATES MEASURING OUT OF TOLERANCE','The reference in the program was wrongly captured during programming| No relation was there between the datum and the reference was taken from some other plane.|Misinterpretation of drawing','|1.The interpenetration on the position and the datum was reexplained to the programmers and the reference to be taken from the datum planes only.\r<br/>','|Refer To CA','Next part in this work order machined and bore Position found ok within the limits','','2018-11-05','CAD(sez)','CAD(sez)','','0000-00-00','HOLE CO ORDINATES MEASURING OUT OF TOLERANCE','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Assembly','','FI','no','Misc','qas_sez(a)','no','','|1.the part was rejected and NCR was raised\r\n2.The reference was taken as per the drawing and run the production.','Z3456','qas_sez|','2019-04-17|','2019-04-17',NULL,NULL,NULL,NULL,NULL,NULL),(11219,'51-141A','THE BOEING COMPANY','CLEVIS - UPPER, RH THREAD','SN02078','112A7112-610','NA','PSDL REV B',3,'BOEING 001AA','','82664','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','Outer profile undersized by 6.00 mm.','1.Program error,\r\n|2.Tool selection in the program is wrong .\r\n|3.Instead of diameter 20.00 mm high feed cutter ,dia 12.00 mm  end mill was selected.|4.Roughing and finishing tools are interchanged in the program.|5.Post processor rename was done wrong.','|1.NC program was re-verified and validated.\r<br/>2.Program was renamed with correct identification .','|1.Standardization of tools and tool path in the form of template in software.\r<br/>2.All programs will be reviewed and validated by senior programmer and same will be evidenced in checklist for FAIR part and re-engineering parts.\r<br/>3.','Effectivness was ensured after production of 93 qty’s.No above deviation was found hence CA/PA found was satisfied.','','2018-11-06','pe_sez(a)','Thaveni D M ,HariPrasad ,','','0000-00-00','OUT SIDE PROFILE UNDER SIZE','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','7','no','a51nx-02','pe_sez(a)','no','','|1.Party was rejected and NCR was raised in ERP.\r\n2.Inform to engineering about the problem.','Z3456','pe_sez|qas_sez|','2018-11-06|2019-01-05|','2019-01-05',NULL,NULL,NULL,NULL,NULL,NULL),(11220,'28-003A','Magellan Aerospace New York  Inc.','PIN-ATTACHMENT WALKING BE','G24667K02','161A7305-1','','PL-Rev-NC, DL Rev-B',1,'A000154134','','80575','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','ID dig mark.','1) During running time insert broken and resulted in dig mark of the part.|2) The previous tool used was worn out due to which the new tool was used as a trial during which insert broken dented the part.|3) Trial was carried out on the original part and resulted in rejection.','|Purchased new tool and continued the production.','|Proved spare tool will be maintained and will be used as an alternate if one tool is affected.','Spare tool availability checked and found ok.','','2018-11-06','Raghavendra Rao(R)','GUNDEGOWDA(H.G.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','13','no','Misc','Sandhesh D(S)','no','','|Immediately stopped the machine and ordered the new tool.','E3456','qas|','2018-11-28|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11221,'51-142A','THE BOEING COMPANY','CLEVIS - LOWER, LH THREAD','SN10219','112A7112-611','NA','PSDL REV B',1,'BOEING 001AA','','82678','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Thread damage.','The length of thread was maximum as the part came outside of the jaws.|The part came outside of the jaws as the chuck pressure was kept at low pressure.','|Increased the chuck pressure.','|Message has been mentioned in the program and informed the CAD members to highlight the pressure in MPS.','NEXT BATCH FOUND OKAY','','2018-11-06','Dinakar K()','Dinakar K()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Dinakar K()','no','','|Immediately stopped machining and checked the previous machined parts and found ok. ','Z3456','pe|qas_sez|','2018-11-30|2018-12-06|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11222,'18-648A','Magellan Aerospace Wrexham','SPACER','M064650/27682','D579 55060 202','','B',2,'175169','','80385','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Base thickness minus.','program running time tool down.so part rejected.( one time 2nos loading )|Dia 16flat using for all roughing.|chances off tool down.\r\n\r\n1) Tool cutting edge chip-up.|2) Not sufficient holding.|3)Tool holder or collect damage and operator not checking tool flutes.','','Informed all the operator to check the tool edge on the completion roughing operation.','CAPA found ok.','','2018-11-06','Rangaswamy()','HariPrasad()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','With Treatment','','03','no','Misc','Rangaswamy()','no','','','E3456','qas|qas|','2018-11-06|2018-11-06|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11223,'47-097B','GKN Aerospace Filton','BRACKET FT5 FWD','W2713','F57550783001','NA','PART ISSUE E04',1,'LTA GKN GS72 - Forgi','','75944','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Part  Rejected/part not found ','1.While part proving time wrong program given by cad cam.|2.wrong post given to wall finish so wall thickness under size by 0.2mm |3.','|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. 							\r<br/>','CAPA found ok','','2018-11-06','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','Part  Rejected/part not found ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','01','no','Misc','Krishna(Chowdary.G.P.)','no','','|Updated NC program and Executed on Machine and Part Found OK. Obsolete old program and New updated program moved to Program Data Storage 							\r\n','E3456','pe|pe|qas|','2018-12-18|2018-12-19|2018-12-19|','2018-12-19',NULL,NULL,NULL,NULL,NULL,NULL),(11224,'35A-356A','Saab AB','Pull Lift Actuator Suppor','','423Z1224-4','','---',1,'787 Forecast','','A15748','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Tool Dig during boring operation .','','','','','','2018-11-07','Mr.Lohit','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','no','yes','no','Assembly','','06','no','','Mr.Lohit','no','M01961','','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11225,'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','Tool Dig during boring operation .','Bush was turned during the boring operation.|Sealant was not uniform between the bush and parts|Due to manual application uniformity vary from person to person.','|Necessary training was given to Sealant applicator','|Inform the Sealant applicator to ensure the uniformity of sealant around the bore.','CAPA found OK.','','2018-11-07','Lohith(K)','Karthineyan(V.S.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Assembly','','06','no','Misc','Phaniraj(G)','no','M01967','|Bush was removed and re install the bush and boring operation was done and part found OK.','E3456','qas|','2018-12-18|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11226,'35A-356A','Saab AB','Pull Lift Actuator Suppor','','423Z1224-4','','---',1,'787 Forecast','','A15751','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Tool Dig during boring operation .','Bush was turned during the boring operation.|Sealant was not uniform between the bush and parts|Due to manual application uniformity vary from person to person.','|Necessary training was given to Sealant applicator','|Inform the Sealant applicator to ensure the uniformity of sealant around the bore.','CA PA found ok.','','2018-11-07','Lohith(K)','Karthineyan(V.S.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Assembly','','06','no','Misc','Phaniraj(G)','no','M01967','|Bush was removed and re install the bush and boring operation was done and part found OK.','E3456','qas|','2018-12-18|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11227,'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','Tool Dig during boring operation .','Bush was turned during the boring operation.|Sealant was not uniform between the bush and parts|Due to manual application uniformity vary from person to person.','|Necessary training was given to Sealant applicator','|Inform the Sealant applicator to ensure the uniformity of sealant around the bore.','CA PA found ok.','','2018-11-07','Lohith(K)','Karthineyan(V.S.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Assembly','','06','no','Misc','Phaniraj(G)','no','M01967','|Bush was removed and re install the bush and boring operation was done and part found OK.','E3456','qas|','2018-12-18|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11228,'18-418A','Magellan Aerospace(Blackpool) Limited','BRACKET','C0201787644/33745977','PI55-2119010-00','','NIL',1,'BPP-533302','','79199','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Base thickness - side.(0.2mm) 			\r\n','Base thickness is out of tolerance.			\r\n	\r\n|Part was not properly butted and the operator did not ensured proper butting of the part.			\r\n','1) Trained all the new operator\'s to how to check proper butting of part. 				\r<br/>\r<br/>','Working nature of all the new operators are monitored and training is provided. 			\r<br/>','CAPA found ok.','','2018-11-07','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','03','no','Misc','Prashanth Kumar(M)','no','','Checked the base thickness of all the parts and found ok. \r\n	\r\n','E3456','qas|','2018-11-15|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11229,'35A-356A','Saab AB','Pull Lift Actuator Suppor','','423Z1224-4','','---',1,'787 Forecast','','A15751','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Refer NC NO:10744','Refer NC NO:10744','|Refer NC NO:10744','|Refer NC NO:10744','Refer NC NO:10744','','2018-11-07','pe_sez(a)','pe_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Assembly','','FI','no','Misc','qas_sez(a)','no','M01967','|Refer NC NO:10744','Z3456','qas_sez|','2019-01-16|','2019-01-16',NULL,NULL,NULL,NULL,NULL,NULL),(11230,'35-480A','Saab AB','LOCK LEVER','C90875','D5227349820000','NA','PART ISSUE B',7,'OWED-LTA-003','','73791','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Paint over flow inside the hole and Improper  masking ','Refer NC NO:11215','|Refer NC NO:11215','|Refer NC NO:11215','Refer NC NO:11215','','2018-11-07','qas_sez(a)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','DN42780','POST TREATMENT','yes','Misc','Dharani(Shankar)','no','','|Refer NC NO:11215','Z3456','qas_sez|','2019-01-18|','2019-01-18',NULL,NULL,NULL,NULL,NULL,NULL),(11231,'18-210B','Magellan Aerospace Wrexham','BODY','28428487-C','D321 40204 204','','D, ECN NR29999ST1KM15, NR29999ST2KF65, WQN DFB09775',1,'RP166211','','74828','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','2 Extra holes made in the part ','Instead of 4 holes ,6 holes made in part.|Why1.2 extra holes added in the part.|Why2.Operator not suited the Jig properly and drilled the 2 extra holes. |Why3.Negligence of operator resulted in the above situation.','|Instructed operators to suit the Jig Properly such that it butted to the Fixture and then drilling operation to be started.|Drill jig was modified by the addition of location holes and pins to suit part properly and the drill jig is non rotatable to avoid  extra holes.','|1.Alerts with Visual Boards are added so that every Fitting operators are aware of it.|The additional location pin will be on visual projection on drill jig. So this is not removable so the extra holes wont to be happen which was instructed in Quality Alert','Fixture reworked and changed the guide pins.Next batch manufacturing need to be analyzed.','','2018-11-09','Irappa(Badiger)','Kailash(Patil)','','0000-00-00','NC','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','11','no','Misc','Irappa(Badiger)','no','','|1.Drilling Finished parts were rechecked for any other extra hole Inclusions and those parts Found OK.','E3456','qas|nandishkumardk|qas|','2018-11-09|2018-11-12|2018-11-17|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11232,'51-105','THE BOEING COMPANY','RADIUS FILLER ','32377490 45124A','112T7057-9','NA','PSDL REV -',1,'BOEING 001R','','83579','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Corner radius as per the drawing requirement was not DONE. ','After roughing there was no enough stock in the material to finish the radius|operator failed to change the location pin in the fixture during Setting time|the check provided for setting was followed by the operator ,hence he missed out to change the location pin.','|Standing instruction was given to all the operators and setters to fill the check list provided prior to setting the part and get it approved by the supervisors and senior operator to avoid such rejection.','|Refer to CA','while resetting the part in the same workorder ,the part was setted using the check list  provide for setting in front of CFT team and the next part was machined and found ok as per the drawing requriments.','','2018-11-09','pe_sez(a)','        Somashekar ','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','1','','','','','','|1.The part was rejected and NCR was raised.\r\n2.The fixture was removed from the machine and the required locating pin was replaced.\r\n3.RE-Offset was taken and continued production.','Z3456','pe_sez|qas_sez|','2018-11-14|2019-04-12|','2019-04-12',NULL,NULL,NULL,NULL,NULL,NULL),(11233,'18A-305','Magellan Aerospace Wrexham','HINGE O.W.P.ASSY MID.','','D57259245000','','B',4,'175164','','A18527','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','BUSH ID DIAMETER MEASURES 11.135/11.147 INSTEAD OF 11.115/11.135','WHY1. After lapping process bush id diameter over size and oval ensured|WHY2. After bush assembly and before lapping process bush diameter not ensured|WHY3. Lapping process was carried out by without checking of bush diameter','After bush assembly the assembled bush diameter to be check initially then lapping process will be carry out','|.|.|Mandrel for lapping will be modify with arrangement of one layer of Emery and the emery sheet and grade to be change','Mandrill implementation verified and found ok.','','2018-11-10','Ramesh(D)','Venkatesh Prasad(D R)','','0000-00-00','NC CREATE','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Assembly','','01','no','Misc','Venkatesh Prasad(D R)','no','M02931','The remaining parts are checked and ensured ok','E3456','|||||||qas|qas|','2018-11-16|2018-11-16|2018-11-16|2018-11-16|2018-11-16|2018-11-16|2018-11-16|2018-11-16|2019-01-06|','2019-01-06',NULL,NULL,NULL,NULL,NULL,NULL),(11234,'35-241','Saab AB','HANDLE','784527A4','425Z0634-2','','--C',20,'Forecast po for B787','','75733','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','With reference to Customer SCAR OF-003225 these material from FG are quarantined to carry out re-inspection.','N/A','|N/A','|N/A','All the parts are reinspected and no deviations found, so the parts are moved back to the FG.','','2018-11-12','Sathish(G)','Nagendra(SN)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','With Treatment','DN45409','FI','no','Misc','Sathish(G)','no','','|N/A','E3456','qas|','2018-11-13|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11235,'35-241','Saab AB','HANDLE','784527A4','425Z0634-2','','--C',16,'Forecast po for B787','','75734','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','With reference to Customer complaint SCAR OF-003225 these material from FG are quarantined to carry out re-inspection.','N/A','|N/A','|N/A','All the parts are reinspected and no deviations found, so the parts are moved back to the FG.','','2018-11-12','Sathish(G)','Nagendra(SN)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','With Treatment','DN45461','FI','no','Misc','Sathish(G)','no','','|N/A','E3456','qas|qas|','2018-11-13|2018-11-13|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11236,'35-241','Saab AB','HANDLE','784527A4','425Z0634-2','','--C',20,'Forecast po for B787','','75735','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','With reference to Customer complaint SCAR OF-003225 these material from FG are quarantined to carry out re-inspection.','N/A','|N/A','|N/A','All the parts are reinspected and no deviations found, so the parts are moved back to the FG.','','2018-11-12','Sathish(G)','Nagendra(SN)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','With Treatment','DN45410','FI','no','Misc','Sathish(G)','no','','|N/A','E3456','qas|','2018-11-13|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11237,'35-241','Saab AB','HANDLE','784527A4','425Z0634-2','','--C',14,'Forecast po for B787','','75736','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','With reference to Customer complaint SCAR OF-003225 these material from FG are quarantined to carry out re-inspection.','N/A','|N/A','|N/A','All the parts are reinspected and no deviations found, so the parts are moved back to the FG.','','2018-11-12','Sathish(G)','Nagendra(SN)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','With Treatment','DN45462','FI','no','Misc','Sathish(G)','no','','|N/A','E3456','qas|','2018-11-13|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11238,'35-241','Saab AB','HANDLE','784527A4','425Z0634-2','','--C',11,'Forecast po for B787','','75737','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','With reference to Customer complaint SCAR OF-003225 these material from FG are quarantined to carry out re-inspection.','N/A','|N/A','|N/A','All the parts are reinspected and no deviations found, so the parts are moved back to the FG.','','2018-11-12','Sathish(G)','Nagendra(SN)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','With Treatment','DN45411','FI','no','Misc','Sathish(G)','no','','|N/A','E3456','qas|','2018-11-13|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11239,'35-261','Saab AB','RODEND','G24288K02','424Z3411-2','','--B',4,'Forecast po for B787','','76656','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','All these parts are quarantined based on the customer complaint OF-003166.','N/A','|N/A','|N/A','Re-inspect the parts are found ok','','2018-11-12','Sathish(G)','Sudhakar C.M,MANJE GOWDA S,KIRAN  M V,Ashoka R,','','0000-00-00','NC raised post treatment.','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','With Treatment','DN46101','FI','no','MakinoF3-1','Sathish(G)','no','','|N/A','E3456','nagendra|','2018-12-06|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11240,'35-601','Saab AB','FRAME','4215601','D5227338520600','NA','PART ISSUE C',1,'OWED-LTA-001','','81635','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Part rib top surface unclear. ','why1. During rib top profile milling operation excess amount of material removed top surface due to that which was getting undersized|why2. The tool on Z axis direction moved into downwards|why3. The chips were blocked on ATC before loaded into tool holder due to that tool height Z value changed|why4. The empty pockets are available on machine during milling operation chips flowed on the empty pockets |why5. Due to that chips blocking on ATC tool downwards occurred on Z axis','All ATC pockets to be filled with tool holders and that to be avoid chips blocking on ATC pockets.\r<br/>After every roughing cycle operation operator needs to be clean the tool pocket. ','Install chips guard to prevent chips from entering inside the tool pocket ','Effectiveness will be provide on 20-11-2018.\r\nImplementation verified and found ok.','','2018-11-13','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Punith G(S)','no','','The tool holder is removed and the chips were cleaned and the remaining parts checked and ensured ok ','E3456','qas|qas|','2018-12-18|2018-12-18|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11241,'47-103','GKN Aerospace Filton','BRACKET FT4 FWD','W2948','F57550777002','NA','PART ISSUE E',1,'1210042293-1','','76280','','0000-00-00',NULL,'no','no','no','no','no','no','yes','yes','yes','Machine chatter marks on bearing spot face.','1) Due to vibration in machining the chatter mark formed on the part as there was no support to resist the vibration and reached the customer without identification.|2) Due to the machining constrain the tool length selected was high but the chattering formed was less which was cleared by manual rework, but during this time the chattering marks formed was high and got moved to the next operation.|3) During the final inspection the inspector identified the chattering and sent the part back to rework but did not re-inspected the part after the rework.|4) Inspector thought that the Chattering mark would be cleared by the fitter during rework.','|Received the affected part from customer and rework for the same is under progress and will be completed by 23-Nov-18.','|1) Changed the NC program and the tool used for the spot face formation to avoid the manual rework caused due to chattering.\r<br/>2) MPS to be changed to mention the change in Program and Tool.\r<br/>3) Delta FAI to be carried out along with next production. ','New Part manufactured and Delta FAI found ok.','C67708','2018-11-13','Dharanishankar()','qas_sez(a)','QN201138236','2018-11-12','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','DN43496','Cust End','yes','Misc','qas(qas)','no','','|1) All the parts from the FG is quarantined and moved for the re-inspection of the chatter marks and these parts will be moved back the FG based on the successful completion of re-inspection.\r\n2) Quality alert is displayed in all concern department to alert the individual about the escapement.','E3456','qas||qas|','2018-11-15|2018-11-19|2018-12-18|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11242,'51-145A','THE BOEING COMPANY','CLEVIS - UPPER, RH THREAD','SN10171','112A7112-612','NA','PSDL REV B',1,'BOEING 001AA','','82685','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Flange thickness under size by 0.25MM.','1) 0.1MM step observed on face.|2) The step observed because of insert was damaged/warm out.|3) The same single insert was used for both roughing and finishing operations.|4)To remove the observed step repeats the finishing operation since no material stock in the part due to this vibration found in the parts and thickness was undersized. ','|1)MPS updated to use separate tools and inserts for both roughing and finishing operations.\r<br/>2)Two separate face mill tools included in MPS for roughing and finishing operations.','|1)Machine stop(M0)CNC code was added in the program to do visual inspection for steps in face milling operation.\r<br/>2)Same above instruction was displayed near the machine as alert.','After ensuring the 80 numbers produced parts no such deviations observed hence CA/PA found was satisfactory.','','2018-11-14','pe_sez(a)','Manu ,','','0000-00-00','FLANGE THICKNESS UNDERSIZE','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','7','no','a51nx-04','pe_sez(a)','no','','|1)Stop the machine after identifying the vibration sound of part.\r\n2)Cross checked the tools,inserts clamping and holding of part.','Z3456','qas_sez|','2018-11-15|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11243,'43-024','Composite Industrie','FLANGE','1881901 4','V251 13464 200 00','','B00, ECN PV100298ST1ZX12',10,'LTA- PO-1','','73489','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','yes','PN NC sur marquage de type \"B\" V\r\n 2511346420000\r\n\r\nSur etiquette \"V5311346420000\"\r\n\r\nNon conform marking on the label :\r\n\"V2511346420000\" is expected\r\n\"V5311346420000\" is written','1. Part number was printed wrong|2. There was no check point for verifying the label after printing|3. Typo error','|1.Label was reprinted with the correct part number and send to customer.\r<br/>2.verification system of the bag and label by different person will be  adopted.','|1.Check point like prepared by and verified by added to the bag and label in the print so that bag label will be prepared by one person and verified by other person before putting on the bag.\r<br/>2) Note will be added to the work order stating bag and label verified by and will be signed by the respective supervisors.','Next batched found ok.','C70268','2018-11-14','Dharanishankar()','qas_sez(a)','181109-017','2018-11-09','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','DN41427','Cust End','yes','Misc','qas(qas)','no','','|1.Checked the parts which was in FG for bag and label and found ok.\r\n2.Request was sent to customer to change the bag and label at customer end','E3456','qas|qas|','2018-11-23|2018-12-18|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11244,'51-142A','THE BOEING COMPANY','CLEVIS - LOWER, LH THREAD','SN10219','112A7112-611','NA','PSDL REV B',1,'BOEING 001AA','','82678','','0000-00-00',NULL,'yes','yes','yes','','','','','','','FULL LENGTH THREAD FOUND','in programm the length of the thread was captured wrongly|Calculatation of the thread was wrongly definded|The concept of thread rolling was new to the operators','|Onjob training given to all operators and thread length calculation and thread rolling process.','|REFER TO CA','Next part in this work setted and thread length found ok to the requriments','','2018-11-14','Dinakar K()','        Dinakar K ','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','5','','','','','','|1.Machine was stopped and the part Was identified and rejected.\r\n2.Correct thread was captured and re-entered in the programm','Z3456','pe_sez|qas_sez|','2018-11-22|2019-04-17|','2019-04-17',NULL,NULL,NULL,NULL,NULL,NULL),(11245,'47-103','GKN Aerospace Filton','BRACKET FT4 FWD','W2948','F57550777002','NA','PART ISSUE E',1,'1210042293-1','','81119','','0000-00-00',NULL,'no','no','no','no','no','yes','yes','yes','no','With reference to the customer complaint QN201138236 these parts are moved from FG and quarantined to re-inspect for any chatter marks on them.','N/A','|N/A','|N/A','Part re-inspected and the no similar defect found.','','2018-11-15','Sathish(G)','Dharanishankar()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','yes','With Treatment','DN46479','Post FI','no','Misc','qas(qas)','no','','|N/A','E3456','qas|','2018-11-20|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11246,'47-103','GKN Aerospace Filton','BRACKET FT4 FWD','W2948','F57550777002','NA','PART ISSUE E',2,'1210042293-1','','81613','','0000-00-00',NULL,'no','no','no','no','no','yes','yes','yes','no','With reference to the customer complaint QN201138236 these parts are moved from FG and quarantined to re-inspect for any chatter marks on them.','N/A','|N/A','|N/A','Parts re-inspected and no similar defects found.','','2018-11-15','Sathish(G)','Dharanishankar()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','yes','With Treatment','DN47490','Post FI','no','Misc','qas(qas)','no','','|N/A','E3456','qas|','2018-11-20|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11247,'51A-003','THE BOEING COMPANY','LOWER BEAM FWD INBD SPLIC','','315Z1302-1501','','NIL',1,'BOEING 001K','','A19159','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','PROFILE OUT OF TOLERANCE ','the RM was not butted in the Vice fully|The Rm was placed on the chips present in the vice and reference was taken|the Vice used for clamping the RM was not cleaned properly before loading the RM|due to more stock in finishing the profile was minus by 0.25 mm|The operator didn\'t not follow the MPS requirements.','|Awareness given to the operator to clean the vice and FOD if any prior to loading the RM and Also to Cross check the stock before finishing.','|Refer to CA','Next part in this workorder machined and profile found OK.','','2018-11-16','pe_sez(a)','pe_sez(a)','','0000-00-00','PROFILE OUT OF TOLERANCE ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Assembly','','FI','no','Misc','qas_sez(a)','no','','|1.The part was rejected and NCR was raised.','Z3456','qas_sez|','2019-04-12|','2019-04-12',NULL,NULL,NULL,NULL,NULL,NULL),(11248,'56-004','GKN Aerospace Orangeburg','GAS DUMPER FITTING','155708B1','475Z3604-19','NA','NIL',1,'A000044745','','83123','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','bore 17.465mm to 17.477mm.\r\nmeasured= 17.515mm.','1.Bore over size by 0.035mm as the bore was reworked in fitting.|2.There was dent in the bore during polishing the inner wall.|3.there was a Step of 0.1mm in the inner wall due multiple pass was done during finishing the slot|4.Flute length of 10R3 finishing tool was 20mm  instead of 50mm','|After this first part getting rejected using polishing machine ,All the parts of above said work order the step was removed by hand manually using the emery sheet instead of using machine.','|1.10R3 finishing tool,flute length 50mm will be procured and changed for the next batch to avoid multiple pass in the slot and steps.','CAPA found ok.','','2018-11-19','pe_sez(a)','Somashekar ,Raghu B,Kiran Kumar M,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','Slim3n-4AHS-4','Mahesh(N)','no','','|1.All the part was inspected  (wo 83131-qty 14nos,wo83122-qty 8nos,wo83123 qty 2nos) and found 1no bore over size in wo 83123 qty 1no remaining all bore found ok.\r\n\r\n2.Part was identified and internal NC was raised','Z3456','qas_sez|qas|','2018-11-20|2018-12-19|','2018-12-19',NULL,NULL,NULL,NULL,NULL,NULL),(11249,'35-644A','Saab AB','LATCH FORK','HR521404','D5227348920400','NA','PART ISSUE C',1,'OWED-LTA-004','','79752','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Dia 8.1H8 hole under size.\r\nPart measured 7.90 to 7.95mm.','Due to skip of reaming operation the hole got undersized.|During the reaming operation the operator taught that the part is finished to the requirement and unloaded the part.|Usually the hole on the part was semi finished to 7.9mm and undergoes a slotting operation and was supposed to be de-clamped and clamped to avoid ovality formation in the hole during which the operator miss-interpreted the hole visually as completed and removed the part.','|Checked all the parts and informed the operators to check the hole diameter before removing the part from machine.','|Holing and reaming operation will be carried out together after the completion of slotting operation.','Change in process will be implemented on next batch production estimated to be on Jan-2019).','','2018-11-19','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','With Treatment','','FI','no','Misc','Yashawantha(NH)','no','','In formed to production team.','E3456','qas|qas|','2018-11-28|2018-12-06|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11250,'35A-671','Saab AB','SHAFT LEVER ASSY','','D5227346201800','','PART ISSUE D',2,'OWED-LTA-001','','A19872','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','1.Bore oversized by 0.02mm ','1. Checked the bore diameter 100% for the parts which was finished and found satisfying.\r\n\r\n|2.Tools and insert were verified and found ok.','|1.After roughing ,the bore was checked for rough diameter using bore gauge to ensure the stock.\r<br/>2.M00 given in the program to check for chips clogging in the tool.\r<br/>','','1.Next all produced all produced parts are found within the limits and parts are accepted','','2018-11-19','Dharani(Shankar)','Manu(CR)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Assembly','','FI','no','Misc','qas_sez(a)','no','','|1.Bore measures 0.02 mm ,oversized.\r\n2. Chips clogging in boring bar tool.\r\n3.No sufficient stock after roughing .\r\n4.No sufficient coolant flow during finishing of the  boring operation.\r\n5.Chips in the tool were not cleaned after completion of setup.\r\n6.Feed and RPM variations while running the machine.\r\n','Z3456','qas_sez|','2019-01-05|','2019-01-05',NULL,NULL,NULL,NULL,NULL,NULL),(11251,'35A-671','Saab AB','SHAFT LEVER ASSY','','D5227346201800','','PART ISSUE D',7,'OWED-LTA-001','','A19870','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','DEEP PITTING OBSERVED IN THE BORE AFTER TREATMENT','1.Corrosion Pitts observed inside the bore after anodizing\r\n|2.Due to different machining strategy,due to long lead time process Corrosion inhibited inside the part\r\n','|1. Informed all the operators to apply rust prof oil for long lead process\r<br/>','|1.Rust preventive oil will be applied in between operation and during transistor\r<br/>','1.Next batches sent for treatment verified and found OK\r\n','','2018-11-19','Dharani(Shankar)','Manu(CR)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Assembly','','FI','no','Misc','qas_sez(a)','no','','|1.All in process parts are checked and found ok\r\n','Z3456','qas_sez|','2019-04-16|','2019-04-16',NULL,NULL,NULL,NULL,NULL,NULL),(11252,'35A-671','Saab AB','SHAFT LEVER ASSY','','D5227346201800','','PART ISSUE D',7,'OWED-LTA-001','','A19871','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','DEEP PITTING OBSERVED IN THE BORE AFTER TREATMENT','1.Corrosion Pitts observed inside the bore after anodizing\r\n|2.Due to different machining strategy,due to long lead time process Corrosion inhibited inside the part\r\n','|1. Informed all the operators to apply rust prof oil for long lead process\r<br/>','|1.Rust preventive oil will be applied in between operation and during transistor\r<br/>','1.Next batches sent for treatment verified and found OK\r\n','','2018-11-19','Dharani(Shankar)','Manu(CR)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Assembly','','FI','no','Misc','qas_sez(a)','no','','|1.All in process parts are checked and found ok\r\n','Z3456','qas_sez|','2019-04-16|','2019-04-16',NULL,NULL,NULL,NULL,NULL,NULL),(11253,'35A-672','Saab AB','SHAFT LEVER ASSY','','D5227346201900','','PART ISSUE D',1,'OWED-LTA-001','','A19928','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','DEEP PITTING OBSERVED IN THE BORE AFTER TREATMENT','1.Corrosion Pitts observed inside the bore after anodizing\r\n|2.Due to different machining strategy,due to long lead time process Corrosion inhibited inside the part\r\n','|1. Informed all the operators to apply rust prof oil for long lead process\r<br/>','|1.Rust preventive oil will be applied in between operation and during transistor\r<br/>','1.Next batches sent for treatment verified and found OK\r\n','','2018-11-19','Dharani(Shankar)','Manu(CR)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Assembly','','FI','no','Misc','qas_sez(a)','no','','|1.All in process parts are checked and found ok\r\n','Z3456','qas_sez|','2019-04-16|','2019-04-16',NULL,NULL,NULL,NULL,NULL,NULL),(11254,'35-526','Saab AB','ROD BODY','2878','D522 73337 200 00','','A',2,'OWED-LTA-001','','81922','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','TOTAL LENGTH UNDERSIZED','1.While adjusting the final size(length) of the part manually  in the program, the operator entered wrong length value in the stopper	\r\n| 2.Due to the wrong input of the length, the part length dimension is undersized','|Implementing the fixture to hold the part to remain constant before finishing the length of the part','|Implementing the fixture to hold the part to remain constant before finishing the length of the part','CA/PA is effectively implemented so that the fixture remains constant to hold the part and produce the required length','','2018-11-20','Dinakar K()','pe_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','05','no','Misc','pe_sez(a)','no','','|1.Inspected the length of the previously produced parts\r\n2.Informed to the supervisors \r\n','Z3456','qas_sez|','2019-01-05|','2019-01-05',NULL,NULL,NULL,NULL,NULL,NULL),(11255,'35-531A','Saab AB','SHAFT LATCH','B90458','D5227349020200','NA','PART ISSUE C',2,'OWED-LTA-002','','83188','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','OD Dig mark','1.Groove mark observed on OD for a depth of 0.5mm and width of 0.5mm|2.Machine was emergency stopped automatically due to low air pressure |3.tool was stationary and excess material removed during the idle time.|4.No electrical power ','|Refer NC No:10744','|Refer NC No:10744','Refer NC No:10744','','2018-11-20','Dinakar K()','Maruthi()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','05','no','Misc','Dinakar K()','no','','|Refer NC No:10744','Z3456','qas_sez|qas_sez|','2018-11-20|2019-01-18|','2019-01-18',NULL,NULL,NULL,NULL,NULL,NULL),(11256,'51-146','THE BOEING COMPANY','REAR SPAR COVER','8-28-06662-1/29515','312Z3112-501','NA','NIL',1,'BOEING 001X','','77143','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Trail part used to analyze the process risk.','NA','|NA','|NA','NA','','2018-11-20','qas_sez(a)','Kiran KM,Dinakar K ,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','DN44477','FI','no','200MY-01','qas_sez(a)','no','','|NA','Z3456','qas_sez|','2018-11-20|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11257,'51-147','THE BOEING COMPANY','REAR_SPAR_RING-DOUBLER','8-33-06422-1/29552','312Z3113-501','NA','NIL',1,'BOEING 001X','','77144','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Trail part used to analyze the process risk.','NA','|NA','|NA','NA','','2018-11-20','qas_sez(a)','Lohith K,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','DN44478','FI','no','PS105-02','qas_sez(a)','no','','|NA','Z3456','qas_sez|','2018-11-20|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11258,'18-009A','Magellan Aerospace Wrexham','Plate Cover','0515401','D572 52519 200','L97 T351','A',1,'162884','','74249','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dent mark on part.','WHY1. FOD affected on part|WHY2. Part was stored in non allocated area|WHY3. Tools and finished parts were stored in same table','|The tools were stored in separate tray which wont to be affect on part','|The parts, tools and jaws stored in separately dedicated rack and tray.','5S re-audit score card\r\nKaizen implementation \r\nsubmission date: 22-11-2018.\r\nImplementation verified and found ok.','','2018-11-20','Raghavendra Rao(R)','Raghavendra Rao(R)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','1','no','Misc','Raghavendra Rao(R)','no','','|The parts under process were verified for any dent mark\r\nThe parts and tools are stored in different rack arrangement','E3456','pe|nandishkumardk|qas|','2018-11-20|2018-11-22|2018-12-18|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11259,'35-404','Saab AB','BEAM 2','2729601','D522 73392 200 01','','A',2,'OWED-LTA-001','','81730','','0000-00-00',NULL,'yes','yes','yes','','','','','','','M/C RUNNING TIME COOL-LENT NOT FLOWING BECAUSE OF THE DIA 12 E/M HEAT THIS WHY WALL RUBBING SO PART REJECT ......\r\n    ','The coolant nozzle was not aligned to the tool cutting edge during machining |operator didn\'t check the weather the coolant nozzle was aligned with the tool or not|Since the tool was true coolant ,operator refused to check the coolant nozzle','|Check list for setting the part will be update to check the coolant flow and the same will be instructed to all the operators to check during the setting time','|refer to CA','Next part in this workorder ,the coolant was adjusted and alligned on to the cutting tool.\r\npart machined and found ok','','2018-11-20','pe_sez(a)','        Umesh B','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','5','','','','','','|1.All the tools pertaining to the part was recalled and checked wether the coolant flows on the tool cutting edge.\r\n2.12dia EM was replaced and continued the production.','Z3456','pe_sez|qas_sez|','2018-11-22|2019-04-12|','2019-04-12',NULL,NULL,NULL,NULL,NULL,NULL),(11260,'51-142A','THE BOEING COMPANY','CLEVIS - LOWER, LH THREAD','SN10219','112A7112-611','NA','PSDL REV B',3,'BOEING 001AA','','82677','','0000-00-00',NULL,'yes','yes','yes','','','','','','','A chips in boring bar holder while tool changing by CNC mode in the machine so tool becomes run out\r\nand bore over size. ','A chips in boring bar holder while tool changing by CNC mode in the machine so tool becomes run out and bore over size.','|Inform to operator boring operation running before clean the tool pockets and spindle.\r<br/>Every time boring operation running clean the ATC arm. ','|1) M0 optional program stop was provided in the program.\r<br/>2)Training provided to all operators and supervisors for visual inspections in the intermediate CNC stop to ensure no chips in the bore and tool.\r<br/>3)The same above alert was displayed near the machine. ','Next 3 parts machine and found bore was measuring within the tolerance','','2018-11-21','pe_sez(a)','        Thaveni D M ','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','7','','','','','','|1.M00 COMMAND  intermediate stop or optional stop was given in the program to ensure if any chips in tools and for tool cleaning.','Z3456','pe_sez|qas_sez|','2018-11-22|2019-01-24|','2019-01-24',NULL,NULL,NULL,NULL,NULL,NULL),(11261,'51-198','THE BOEING COMPANY','TENSION TUBE','F00280238-0001','251A3149-902','NA','PSDL REV-',1,'BOEING 001AA','','84181','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','LENGTH UNDERSIZED.','Improper inspection using Analog vernier		\r\n		\r\n		\r\n		\r\n|Vernier reading by the operator done wrong (Analog)		\r\n		\r\n		\r\n		\r\n|Operator entered wrong value in the program (on plus side)		\r\n		\r\n		\r\n		\r\n|Back stopper in the chuck was not planned for this operation		\r\n		\r\n		\r\n		\r\n|Back stopper in the chuck was not planned for this operation		\r\n		\r\n		\r\n		\r\n','|Back stoper will be provided insaid the check to avoid manual errors.','|4A principal methods will be adopted. to ensure the required length will be maintain the excess material length to be machined will be maintained by the both physical and CNC program by super wiser and operator.','','','2018-11-22','Dinakar K()','Dinakar K ,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','3','no','200MY-02','pe_sez(a)','no','','|1. Fair work order 84138 production work order 84181 done together.\r\n2. Fair part stage inspection for total length clearance given as per requirment. \r\n3. Production work order 84171-51 Qty,84178-52 Qty, 84180-52 Qty, 84181-52 Qty, 84182-48 Qty. All Qty checked and length found ok.\r\n4. No stock in FG and NO parts dispatched to the costumer.','Z3456','qas_sez|','2018-11-24|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11262,'56-023','GKN Aerospace Orangeburg','CLOSEOUT FAIRING - AFT, U','711206B3','119A1522-603','NA','PSDL REV -',1,'LTA Orangeburg 737 W','','82823','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Part dig mark occurred up to 3.00mm','WHY1. During counter sink operation dig mark occurred|WHY2. The selection of counter sink program was wrong|WHY3. While cross checking Z value on program during that time program executed from the Z value which was not taken from initial|WHY4. During CSK operation wear offset needs to be ensure while that time Z value checked and wrongly executed.|WHY5. Operation is wrongly executed program','|The required Z value for CSK offset to be ensure from previous reference ','|The Z value will be shows default during before CSK operation on program.','Default comment on program\r\nDocument to be submit on 23-11-2018','','2018-11-22','Dinesh kulal()','Lakshmi(Narasimha)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','01','no','Misc','Lakshmi(Narasimha)','no','','|The dig mark made tool was checked for any wear out or any breaking and replaced','A3456','qas|qas_aero|','2018-11-26|2018-11-27|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11263,'53-057','Triumph Aerostructures','FORK FITTING ','457425A','F57953444200','NA','PART ISSUE A',1,'LTA 4 - TRIUMPH 2018','','84362','','0000-00-00',NULL,'yes','no','yes','','','','','yes','','Dig mark  on part surface.','Due to manufacturing process error.|Programmer planned to minimize the process setup and cycle time,due to this vibration was observed in finishing program.|The process was not effective.','|NC was raised and handover the parts the parts to the QAD.\r<br/>Part was rejected by the inspector.','|NC was raised and handover the parts the parts to the QAD.\r<br/><br/>Part was rejected by the inspector.','Effectiveness was ensured for the proper limits.','','2018-11-22','pe_sez(a)','        Tejas ','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','1','','','','','','|1.Increased the finishing operation stock by 0.5mm to 1mm to withstand the vibration.\r\n2.Tool path is improved.','Z3456','pe_sez|pe_sez|qas_sez|qas_sez|','2018-11-22|2018-12-20|2019-01-05|2019-01-16|','2019-01-16',NULL,NULL,NULL,NULL,NULL,NULL),(11264,'18-420A','Magellan Aerospace(Blackpool) Limited','STOP PAD','30356*4882','PI55-2115001-00','','NIL',7,'P/501842','','56065','','2017-09-13',NULL,'no','yes','no','no','no','no','yes','no','yes','Parts are etched CIM 66257(Should be CIM 56065,ref CIM C of C, no C58734.','WHY1. Wrong part marking(Work order number in the part is not as per the COC)|WHY2. COC was raised to the parent WO and was not manually amended|WHY3. Initially the parts are shipped with bag and label during which WO for the part was(56265) then due to change in customer for scribe marking the remaining parts from FG were swapped to the new WO(66257) and scribe marked to the new WO','|Hand amended the COC and sent to customer','|When material is swapped the release document(COC) will be cross verified with the part before dispatch.','CAPA found ok.','C58734','2018-11-22','Nandishkumar(D.K.)','Ranjith(G)','RDN 4838','2018-08-07','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','CUSTOMER NC','no','Misc','Ranjith(G)','no','','|FG check was carried out and parts from 78687(13), 78688(20), 79177(7), 79178(16), 79179(16) are found ok','E3456','nandishkumardk|qas|','2018-11-22|2018-12-18|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11265,'47-098B','GKN Aerospace Filton','BRACKET M/C TRACK 2 FWD ','02318122','F57550193000','NA','PART ISSUE H02',1,'LTA-GKN-002','','78789','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','BORE OVER SIZE BY 0.075MM REQUIRED 74.60/74.63 MEASURING 74.70/74.705','Why-1: Dig mark observed on bore.|Why-2: Boring bar orientation wrong.|Why-3: Boring bar head wrong assembly during service.','|1) Tool assembly orientation verification training given to all the operators.','|1) Quality Alert to be displayed near the machine.','','','2018-11-22','Gurukiran S(M)','Shivanand D.B.,Niranjan Murthy,Harishkumar B N,Balaji ,ABHISHEK M G,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','With Treatment','','FI','no','HMC 440','Nandishkumar(D.K.)','no','','|Reset the boring bar head to correct orientation and next part found ok. ','E3456','qas|qas|','2018-11-26|2018-11-29|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11266,'56-088','GKN Aerospace Orangeburg','CHANNEL FWD','221904B6','119A1212-601','NA','NIL',1,'A000047469','','84491','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','Tool Dig Mark was evident on the base of the part which was not meeting the Required Part configuration','The program given to the machine had a Wrong Approach of cutting tool in Z-Axis|Multiple tool paths were manually merged to make it a single tool path which had resulted in a wrong tool approach which was not seen in program simulation|Programs were not verified before giving it to machine [G-Code Simulator/Verification]','|The programs given to the machine to run the Re-FAIR part was verified for such errors and was found okay','|NC Programs shall be cross verified with G-code simulator prior to transferring to the machine for machining for all 3-Axis tool paths','','','2018-11-22','pe_sez(a)','                Diwakar R.B.,','','0000-00-00','UNWANTED MACHINING DUE TO POST PROCESS ERROR','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','3','no','i700-1','pe_sez(a)','no','','|Part identified as rejected.','Z3456','pe_sez|CAM|qas_sez|Deshpande|cam|qas_sez|','2018-12-20|2018-12-24|2019-01-07|2019-10-18|2019-10-30|2019-11-05|','2019-11-05',NULL,NULL,NULL,NULL,NULL,NULL),(11267,'56-090','GKN Aerospace Orangeburg','CHANNEL AFT','221904B6','119A1212-603','NA','NIL',1,'A000047469','','84509','','0000-00-00',NULL,'no','','yes','','','','yes','yes','','Tool Dig Mark was evident on the base of the part which was not meeting the Required Part configuration','The program given to the machine had a Wrong Approach of cutting tool in Z-Axis|Multiple tool paths were manually merged to make it a single tool path which had resulted in a wrong tool approach which was not seen in program simulation|Programs were not verified before giving it to machine [G-Code Simulator/Verification]','|The programs given to the machine to run the Re-FAIR part was verified for such errors and was found okay','|NC Programs shall be cross verified with G-code simulator prior to transferring to the machine for machining for all 3-Axis tool paths','','','2018-11-23','pe_sez(a)','                        Rajesha A.R','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','1','','','','','','|Part identified as rejected.','Z3456','pe_sez|pe_sez|CAM|qas_sez|Deshpande|cam|qas_sez|','2018-11-23|2018-12-20|2018-12-24|2019-01-07|2019-10-18|2019-10-30|2019-11-05|','2019-11-05',NULL,NULL,NULL,NULL,NULL,NULL),(11268,'51-142A','THE BOEING COMPANY','CLEVIS - LOWER, LH THREAD','SN02075','112A7112-611','NA','PSDL REV B',1,'BOEING 001AA','','82850','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Tool dig mark on internal diameter surface','1.Due to insert and tool damage while running in the machine|2.Due to tool damage dig mark observed in hole surface|3.Due to over length of the tool, vibration is observed\r\n','|1.Planned to purchase a new tool for next production, having minimum length of the tool to minimize the vibration\r<br/>2.Discussion with the tool supplier to provide a good insert seating area\r<br/>','|\r<br/>1.Planned to purchase a new tool for next production, having minimum length of the tool to minimize the vibration\r<br/>2.Discussion with the tool supplier to provide a good insert seating area\r<br/>','CA/PA has been efficiently implemented for the rest of components','','2018-11-23','pe_sez(a)','Karthik Raj T()','','0000-00-00','Part rejected due to tool dig mark in bore.......','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','07','no','Misc','pe_sez(a)','no','','|1.Due to the vibration observation, machine was stopped immediately\r\n2.Then the tool was checked, verified and inserted\r\n3.Visually inspected the manufactured quantities from the previous work orders\r\n4.Then all parts are visually accepted\r\n','Z3456','qas_sez|qas_sez|','2019-01-05|2019-01-16|','2019-01-16',NULL,NULL,NULL,NULL,NULL,NULL),(11269,'18-104A','Magellan Aerospace Bournemouth','BODY TURNBUCKLE ','CD703094/02891A','PID575 40490 200','','E',1,'428863','','79644','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Part 2time loading dia 3mm hole both side running so part reject.','Why-1: 2times part has been processed.|Why-2: Processed part was loaded instead of unprocessed part.|Why-3: No clear identification of  rack between processed and unprocessed part.','|Informed all the operators to store the finished and under process parts separately.','|1) Tag will be implemented to identify processed and unprocessed part.\r<br/>2) Training for operator on M/C for tagging.','Training given to operator and witnessed by supervisor and CAPA found effective.','','2018-11-23','Anjinamurthy(H)','Girish(HP)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','05','no','Misc','Punith G(S)','no','','|Whole batch visually inspected and found ok.','E3456','qas|qas|','2018-11-26|2018-11-28|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11270,'35-597','Saab AB','CORNER','548050A','D5227338620200','NA','PART ISSUE B',1,'OWED-LTA-001','','81800','','0000-00-00',NULL,'yes','no','yes','no','yes','no','no','no','no','Profile Dig 0.60mm.( AT SEZ MAZZAK I-700 MACHINE)','NC program Boarder rating reading problem|Machine capacity memory problem','|Mazak Maintenance team came and re-installed the MAZAKTROL software','|Mazak Maintenance team came and re-installed the MAZAKTROL software','CAPA FOUND OK','','2018-11-23','prodn_aero(prodn)','prodn_aero(prodn)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','05','no','Misc','Ravi nayak()','no','','|Immediately machine stop and informed to the machine maintenance team','A3456','prodn_aero|pe|qas_aero|','2018-11-28|2019-01-17|2019-06-08|','2019-06-08',NULL,NULL,NULL,NULL,NULL,NULL),(11271,'35-146','Saab AB','CED_HINGE_FTG_FWD','9366805','425Z0301-6','7050 - T7451 ALUMINU','--A',1,'1600203627','','80722','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Wall Thickness Minus.','','','','','','2018-11-23','prodn_aero(prodn)','prodn_aero(prodn)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','prodn_aero(prodn)','no','','','A3456','qas_aero|','2018-11-28|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11272,'35-598','Saab AB','CORNER','548921 B','D5227338620300','NA','PART ISSUE B',1,'OWED-LTA-001','','81801','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Profile dig 1mm.','','','','','','2018-11-23','prodn_aero(prodn)','prodn_aero(prodn)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','no','yes','no','With Treatment','','05','no','Misc','Ravi nayak()','no','','','A3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11273,'18-418A','Magellan Aerospace(Blackpool) Limited','BRACKET','C0201787644/33745977','PI55-2119010-00','','NIL',1,'BPP-533302','','84195','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','BASE THICKNESS -0.8MM SIDE, ','part lifted during clamping.|improper butting of part, operator did not ensure the same|Due to improper clamping method and no relief used in fixture.','|Will ensure proper butting of the part.','|profile relief and locating pin will be implemented on fixture.','Implementation verified and found ok.','','2018-11-24','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','03','no','Misc','Punith G(S)','no','','|parts re-inspected and found ok','E3456','pe|qas|','2018-11-27|2018-12-18|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11274,'35A-353A','','','','','','',0,'','','','','0000-00-00',NULL,'no','no','no','no','no','no','no','no','no','','','','','','','2018-11-26','select','','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Cancelled','no','no','no','','','','no','','select','no','','','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11275,'35A-353A','Saab AB','LIFT PIN HOUSING FWD','','423Z1124-5-52','','1',5,'LTA SAAB B787 Assemb','','A19685','','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','','2018-11-26','pe_sez(a)','pe_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Assembly','','FI','no','Misc','qas_sez(a)','no','78265|423Z1124-5-01','|Refer NC NO:10744','Z3456','qas_sez|','2019-01-16|','2019-01-16',NULL,NULL,NULL,NULL,NULL,NULL),(11276,'35A-354A','Saab AB','LIFT PIN HOUSING FWD','','423Z1124-6-52','','1',2,'LTA SAAB B787 Assemb','','A19302','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Refer NC NO:10744','Refer NC NO:10744','|Refer NC NO:10744','|Refer NC NO:10744','','','2018-11-27','pe_sez(a)','pe_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Assembly','','FI','no','Misc','qas_sez(a)','no','77021|423Z1124-6-01','|Refer NC NO:10744','Z3456','qas_sez|','2019-01-16|','2019-01-16',NULL,NULL,NULL,NULL,NULL,NULL),(11277,'51-144','THE BOEING COMPANY','STRUT, AFT','H27626','112A7111-602','NA',' PSDL REV -',1,'BOEING 001W','','82847','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Hole position is shifted by 12 degree','\r\n1.Due to error in the program.\r\n|2.Program related C value was not mentioned in the program. |3.Operator/supervisor did not have much awareness on the turn mill machining/programming.','|1.Training will be conducted for the programmer, operator and the supervisor.','|1.Training will be conducted for the programmer, operator and the supervisor.','Next part was found within the acceptable tolerance.','','2018-11-27','pe_sez(a)','Dinakar K ,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','5','no','200MY-01','pe_sez(a)','no','','|1.The machine was stopped.\r\n2.The program was checked for errors.\r\n','Z3456','qas_sez|','2019-01-05|','2019-01-05',NULL,NULL,NULL,NULL,NULL,NULL),(11278,'35-526','Saab AB','ROD BODY','2878','D522 73337 200 00','','A',1,'OWED-LTA-004','','81920','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','RUNNING TIME PART ROTATE ','Outside diameter is maintained between 11.9 to 12.2 in turning operation and hence 11.9 diameter maintained parts not holds properly in milling fixture of 12mm diameter.So this made the part rotated while milling operation ','|1.After separating the parts dimension wise the clamping was adjusted accordingly variation wise.\r<br/>2.Instruction given to the operator to check the OD before loading to the machine','|1.The O.D of 12 mm is added as a Key charectristics in MPS.  and the tolerance was definded as +/-0.05 as a process CTQ','Next part machine and found ok .','','2018-11-27','pe_sez(a)','Vijay Kumar H.J,Pradeep B.D,Dhanush J.K,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','7','no','a51nx-01','pe_sez(a)','no','','|All the parts were checked for OD dimension and separated accordingly variation wise','Z3456','qas_sez|','2019-01-22|','2019-01-22',NULL,NULL,NULL,NULL,NULL,NULL),(11279,'35-146','Saab AB','CED_HINGE_FTG_FWD','9366805','425Z0301-6','7050 - T7451 ALUMINU','--A',1,'1600203627','','80722','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Wall Thickness Minus.','WHY 1.Wrong Tool Called In The Program,operator Did Not  Ensured Proper Tool Before Starting The Cycle.|WHY 2.Operator Taught That The Tool No Called In The Program Is Acc To The Tools Loaded In The Program. |WHY 3.There Was no Check Point For The Operator To Ensure The Tool.','Changed The Correct Tool And Run The Program.','Tool Check List Will Be Updated By Operator  & Will Be Verified By Supervisor.','Check list Updated 27-11-2018.','','2018-11-27','prodn_aero(prodn)','prodn_aero(prodn)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','prodn_aero(prodn)','no','','Immediately Stop The Machine And Checked Diameter Of The Tool.','A3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11280,'53-051','Triumph Aerostructures','PLATE/UPR SPREADER,A330/3','4264401','F57451568200A02','NA','PART ISSUE A',1,'LTA4 TRIUMPH 2018','','84377','','0000-00-00',NULL,'yes','no','no','no','no','yes','no','yes','no','OVER ALL THICKNESS OF THE PART OVER SIZE BY 1MM','ROTARY CENTRE OUTPUT IN THE PROGRAM WAS TAKEN INCORRECTLY (LESS THAN THE REQUIRED DIMENSION)|PROGRAM ERROR','|THE OUTPUT DIMENSION WILL BE GIVEN BY THE PROGRAMMER AND THE PROGRAM WILL BE CHECKED BY THE OPERATOR AND IT WILL BE CROSS CHECKED BY THE SUPERVISOR.','','NEXT PART PRODUCED ME THE REQUIREMENT OF THE DRAWING AND CAPA FOUND SATISFACTORY.','','2018-11-27','CAD(sez)','Somashekar ,Raghu B,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','','FINAL','yes','Slim3n-4AHS-3','Manu(CR)','no','','|PART INSPECTED AS PER THE DRAWING AND THICKNESS FOUND 1MM OVERSIZE SO REWORK NC RAISED','Z3456','qas_sez|','2019-02-13|','2019-02-13',NULL,NULL,NULL,NULL,NULL,NULL),(11281,'35-482A','Saab AB','ROLLER ','B90488','D5227331620000','NA','PART ISSUE B',4,'OWED-LTA-005','','82070','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Total length under size by 0.015 to 0.057mm.\r\nDrawing required 9.50 +/- 0.1, parts measured 9.385 to 9.343mm.','Why-1: Due to face run out the total length of the part got undersized.|Why-2: Due to run out in the jaws ID the part has face out.|Why-3: Due to improper jaws boring & operator did not dialed the jaws before loading the part.','|Re-bored the jaws and continued the production.','|Instructions displayed near the machine to explain operator to how to bore the jaws & check it before running the part.','CAPA found ok.','','2018-11-27','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','NC','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','Misc','Yashawantha(NH)','no','','|Immediately stopped the machine, dialed the jaws and re-bored the jaws verified the next part and found ok.','E3456','qas|qas|','2018-12-03|2018-12-18|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11282,'35-526','Saab AB','ROD BODY','2878','D522 73337 200 00','','A',2,'OWED-LTA-001','','81922','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','TOTAL LENGTH UNDER SIZE BY 0.2 MM. MINIMUM 175.50, MEASURED 175.30 ','Part length was got undersized during turning facing operation|Part was not properly loaded in chuck Due to burr seated on 3 jaw chuck |part was not properly arrested So before loading part into 3 jaw chuck cleaning and checking was not done properly ','|Coolant nozzle was adjusted in such a way that the burr while machining should not get clocked at the butting and clamping area to prevent such kind of rejection','|Awareness given to the operator to clean the butting area for every part before loading the part using air gun and to check if any burr presence and Foreign Objects Debris cleaning','CAPA found satisfactory.100% inspection done for this workorder and found only 2 parts getting deviated out if tolerance.','','2018-11-28','pe_sez(a)','Vijay Kumar H.J,Pradeep B.D,Dinakar K ,','','0000-00-00','TOTAL LENGTH UNDER SIZE BY 0.2 MM. MINIMUM 175.50, MEASURED 175.30 ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','100MY-01','qas_sez(a)','no','','|the jaws were cleaned using air gun and removed if any burr presence in the butting area','Z3456','qas_sez|','2019-01-22|','2019-01-22',NULL,NULL,NULL,NULL,NULL,NULL),(11283,'35-712','Saab AB','LEVER','HR521404','D5227346720900','NA','PART ISSUE D',1,'OWED-LTA-004','','82502','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Profile unclear.','Chattering on the part profile occurred during the roughing operation.|Screw used to lock the insert got loosed during the machining operation.|The head of the align key used to tight the insert screw was blunt because of which the insert got loosed during the machining and affected the profile. ','|Informed all the operator to check the align key head before taking to use.','|Scrapped all the old and worn out align keys.','CAPA found ok.','','2018-11-29','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','05','no','Misc','Prashanth Kumar(M)','no','','|Immediately stopped the machine checked the previous parts and changed the align key and re-tighten the screw and continued the production.','E3456','qas|','2018-12-06|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11284,'35-644A','Saab AB','LATCH FORK','HR521404','D5227348920400','NA','PART ISSUE C',2,'OWED-LTA-004','','79752','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','','Bore dimension measures 18.95mm instead of 18.8 E7 \r\n\r\nRefer NC# 11213.','Refer NC# 11213.|Refer NC# 11213.|Refer NC# 11213.|Refer NC# 11213.','|Refer NC# 11213.','|Refer NC# 11213.','Refer NC# 11213.','','2018-11-29','Anjinamurthy(H)','Anjinamurthy(H)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','Misc','Yashawantha(NH)','no','','|Refer NC# 11213.','E3456','qas|','2018-11-29|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11285,'35-711','Saab AB','LEVER','HR521404','D5227346720800','NA','PART ISSUE D',1,'OWED-LTA-004','','82494','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dia 5 +0.018\r\nDia 5.12 pin enter so part reject.','why1. During rib top profile milling operation excess amount of material removed top surface due to that which was getting undersized|why2. The tool on Z axis direction moved into downwards|why3. The chips were blocked on ATC before loaded into tool holder due to that tool height Z value changed|why4. The empty pockets are available on machine during milling operation chips flowed on the empty pockets|why5. Due to that chips blocking on ATC tool downwards occurred on Z axis','|All ATC pockets to be filled with tool holders and that to be avoid chips blocking on ATC pockets.\r<br/>After every roughing cycle operation operator needs to be clean the tool pocket. ','|Install chips guard to prevent chips from entering inside the tool pocket ','Effectiveness will be provide on 03-12-2018 .\r\nProvided evidences verified and found ok.','','2018-11-29','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','05','no','Misc','Prashanth Kumar(M)','no','','|The tool holder is removed and the chips were cleaned and the remaining parts checked and ensured ok','E3456','qas|qas|','2018-12-01|2018-12-05|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11286,'35-711','Saab AB','LEVER','HR521404','D5227346720800','NA','PART ISSUE D',1,'OWED-LTA-004','','82494','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Thread mill dia over size.','Inner diameter of the part got oversized.|CRC value given was not correct|Operator did not entered the the CRC value during the setting time and while cross checking the values he found that the CRC value was not entered then he entered the value to the machine with out pressing the reset button due to which the machine did not accepted the value included, later when the operator started the cycle the tool ran for the default CRC value and hence the part got rejected.|No Check point for the operator to ensure the data before starting the cycle.','|Corrected the crc value of the thread mill tool and continued the production.','|1) 1st off operation will be carried out on the dummy material before doing it on the part.\r<br/>2) Setting flow chart will be displayed near the machine.\r<br/>3) Message alert will be added on the program to remind operator to set and check the CRC.','Effectiveness will be provided on 07-Dec-2018.\r\nImplementation verified and found ok.','','2018-11-29','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Prashanth Kumar(M)','no','','|Immediately stopped the machine and checked the reference values of all the tools and found ok.','E3456','qas|qas|','2018-12-06|2018-12-18|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11287,'47-141','GKN Aerospace Filton','STIFFENER 5 TOP SKIN','4193901 1','D57250496202','NA','PART ISSUE N',1,'1210042824-1','','75449','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','WALL THICKNESS 1.5 +0.13/-0.08 MEASURING 1.30 AT ONE END ','Due to improper butting of part in fixture.|Fixture had stock.|Fixture validation was not done.','|New fixture created for next parts.','|1.Upcoming fixtures will be validated before starting any new parts. ','CAPA found ok.','','2018-11-29','Ramesh(Poojary)','Sathisha(K.C.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','3','no','Misc','Narayanappa(G)','no','','|Fixture was validated and built new fixture. ','E3456','pe|qas|','2018-11-29|2018-12-18|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11288,'47-143','GKN Aerospace Filton','STIFFENER 6 TOP SKIN','628652','D57250497202','NA','PART ISSUE H',1,'1210042824-1','','75451','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Wall thickens taper & -side.(0.13mm proses problem) ','Due to improper butting of part in fixture.|Fixture was in stock.|Fixture validation was not done.','|\r<br/>Changed the fixture. ','|Upcoming fixtures will be validated before loading any new parts.','CAPA found ok.','','2018-11-29','Ramesh(Poojary)','Sathisha(K.C.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','3','no','Misc','Sathisha(K.C.)','no','','|Fixture was validated and built new fixture. ','E3456','pe|qas|','2018-11-29|2018-12-18|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11289,'47-144','GKN Aerospace Filton','STIFFENER 6 TOP SKIN','628652','D57250497203','NA','PART ISSUE H',1,'1210042824-1','','75452','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','THICKNESS 1.5 +0.13/-0.08 MEASURING 1.32 AT ONE END ','Due to improper butting of part in the fixture |Fixture was in stock|Fixture validation was not done','|\r<br/>Changed the fixture','|New fixtures will be validated before loading any new parts.','CA/PA Found ok.','','2018-11-29','Ramesh(Poojary)','Sathisha(K.C.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','3','no','Misc','Sathisha(K.C.)','no','','|fixture was validated & built new fixture ','E3456','pe|qas|','2018-11-29|2018-12-04|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11290,'47-104','GKN Aerospace Filton','BRACKET FT4 FWD','W9640','F57550777003','NA','PART ISSUE E',1,'1210042293-1','','83080','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Wall dig mark observed by 5mm on spot-face area . ','During Re-Engineering process|To avoid Charting mark on spot face|Selection of tool in that process is wrong','|The program was corrected and given to production.','|Posting flow chart will be displayed in Engg department. ','Posting Flow chart verified and found ok.','','2018-11-29','Ramesh(Poojary)','Lokesh(B.D.)','','0000-00-00','part rejected due to dig mark observed .','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','11','no','HMC 440','Ramesh(Poojary)','no','','|stopped  the production and informed to Engg team','E3456','qas|qas|','2018-12-10|2019-02-14|','2019-02-14',NULL,NULL,NULL,NULL,NULL,NULL),(11291,'51A-066A','THE BOEING COMPANY','STRUT SUPPORT ASSY','','113T1958-7','','PSDL REV A',1,'BOEING 001AA','','A20494','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','','Dummy NCR|Dummy NCR|Dummy NCR|Dummy NCR|Dummy NCR','|Dummy NCR','|Dummy NCR','Dummy NCR','','2018-11-29','pe_sez(a)','pe_sez(a)','','0000-00-00','Part got damaged due to laser problem','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Assembly','','06','no','Misc','pe_sez(a)','no','','|Dummy NCR','Z3456','pe_sez|qas_sez|','2018-11-29|2019-04-17|','2019-04-17',NULL,NULL,NULL,NULL,NULL,NULL),(11292,'35-442B','Saab AB','HINGE','C91212','D5227338720200','NA','B',1,'OWED-LTA-002','','81192','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Improper cutting of material.','1) Material cross cutting during the RM cutting stage.|2) While cutting time nut used to clamp the blade got loosen and resulted in the cross cutting.|3) Clamping nut got worn out.','|Informed all the operator to verify the clamping nut before starting the cutting operation.','|Change the clamping nut with new one once in a month.','CAPA found ok.','','2018-11-30','Sunil Kumar(K.R.)','Ravi R,Kammar Nagaraj,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','1','no','HAASVF2SS-1','Dhananjaya(N)','no','','|Immediately stopped the machine changed the clamping nut and continued the cutting.','E3456','qas|','2018-12-17|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11293,'18-117B','Magellan Aerospace Bournemouth',' 	HOUSING-OUT BD BRG','1647348-2/XBDW','PID275 40004 200','','C01',1,'428867','','80667','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','ID CHAMFER OVER SIZE.','1) Due to tool dig mark ID chamfer got oversized.|2) The work offset provided by the operator to rework the part was wrong.|3) Due to unclear face on the part the operator tried to reface the part during which he entered wrong correction in the offset.|4) Due to improper size of the RM.|5) The tolerance provided in the previous operation was not suitable to achieve the requirement.','|Informed all the operators to check the total length of the part before loading to the machine.','|Informed the Engineering team about the issue and advised to change the dimension and tolerance from 41mm+/-2mm to 39.5mm+0.5mm.','MPS changes to be done on 4-Dec-2018.\r\nCAPA found ok.','','2018-11-30','Ravi(M)','Karibasappa(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','03','no','Misc','Ravi(M)','no','','|Immediately stopped the machine and checked all the completed parts and found ok.','E3456','qas|qas|','2018-11-30|2018-12-18|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11294,'47-091A','GKN Aerospace Filton','BUSH AFT PIN FWD LUG GR ','L32098','L57558296200','NA','A00',1,'LTA-GKN-003','','79359','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','HELICAL GROVES SHIFTED','Why-1: Pitch of the helical grove measured beyond the drawing requirement.|Why-2: During the fair proving time the grove pitch was not clearly studied.|Why-3: It was critical to understand the drawing.','|New program created and next part produced found ok.','|Informed the project team to verify the drawing completely and to discuss with the customer in case of complexity before launching the FAIR.','CAPA found ok.','','2018-11-30','Nandishkumar(D.K.)','Nandishkumar(D.K.)','','0000-00-00','INSTEAD OF SUHAS NC CREATED IN THE NAME OF SUHAS','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','DN46551','FI','no','Misc','nandeesh(kumar)','no','','|Immediately informed the engineering team and verified the part along with the golden sample and the model.','E3456','qas|','2019-01-06|','2019-01-06',NULL,NULL,NULL,NULL,NULL,NULL),(11295,'56-101','GKN Aerospace Orangeburg','CLOSEOUT RIB - AFT, UPR','9388941','119A1383-604','NA','PSDL REV -',1,'A000047469','','84533','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','The part Profile was shifted by an angle which was not acceptable to the profile seen in the model','The program given to the machine was running at 3 degree angle to the Work Offset|The Co-ordiante system selected to generate the Program was wrong|Machine simulation was not verified before loading the program','|Each Toolpath was verified for the correctness by running the Machine Simulation','|The Co-Ordinate System selection before posting the programs need to be validated using machine simulation only. A training will be provided to all programmers','','','2018-12-01','pe_sez(a)','                pe_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','pe_sez(a)','no','','| Part identified as rejected. The parts programming was verified for any such wrong selections','Z3456','pe_sez|pe_sez|CAM|qas_sez|Deshpande|cam|qas_sez|','2018-12-01|2018-12-20|2018-12-24|2019-01-07|2019-10-18|2019-10-30|2019-11-05|','2019-11-05',NULL,NULL,NULL,NULL,NULL,NULL),(11296,'51-144','THE BOEING COMPANY','STRUT, AFT','42EB/25048A','112A7111-602','NA',' PSDL REV -',1,'BOEING 001AA','','82856','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dia 1.9mm drill shift.','when running the drilling program. part shifted from butting face. |Improper cleaning at the butting area','|\r<br/>The butting area was cleaned and the offset was taken again and further ensured that the part is butted properly and rigidly','|stopper was given in the fixture for location so that the part has to lock and butt rigidly during running the machine','Next part WO #82857 qty 8 nos machined and founnd ALL THE HOLE CO-ORDINATE was meeting the drawing\r\nrequried position ','','2018-12-03','pe_sez(a)','Maruthi ,Dinakar K ,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','5','no','200MY-01','pe_sez(a)','no','','|\r\n1.machine was stopped 2.The part was identified and NCR raised 3.The butting area was cleaned and the offset was taken again ','Z3456','qas_sez|','2019-01-22|','2019-01-22',NULL,NULL,NULL,NULL,NULL,NULL),(11297,'51-083A','THE BOEING COMPANY','BRACKET DETAIL','717200A0','332A2930-8','NA','PSDL REV B',23,'BOEING 001U','','78811','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','BORE DIAMETER OVERSIZED BY 0.015MM','1.Due to tool run out|2.Because of Collet problem run out was formed.|3.Damaged collet was used.','|Changed the damaged collet and replaced it with a new collet.With the help dial checked the run out for the new collet and found it ok.','|Instruction give to the operator to check the run out for each boring bar operation.','CA/PA satisfied','','2018-12-03','pe_sez(a)','pe_sez(a)','','0000-00-00','BORE DIAMETER OVERSIZED BY 0.015MM','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','DN47380','FI','no','Misc','qas_sez(a)','no','','|Checked the previous machined parts found ok.','Z3456','pe_sez|qas_sez|','2019-01-17|2019-01-18|','2019-01-18',NULL,NULL,NULL,NULL,NULL,NULL),(11298,'18-083A','Magellan Aerospace Wrexham','STUD PLATE','1902601','D278 50007 201','ABM3 1029','D01',5,'175154','','83518','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','VISUAL DEFECTS OCCURRED ON PARTS','1) Due to improper de-burring operation.|2) The de-burring tool rubbed over the part and affected the visual of the part.|3) Due to high speed of cut operator was not able to hold the tool rigidly.','|Informed all the operators to provide sufficient speed and feed during the de-burring operation.','|Quality alert displayed near in the fitting areas.','CAPA found ok.','','2018-12-04','Dhananjaya(N)','Raj Kumar,Patel Appaaji,Paramaeshappa ,Girish MS,BHUVANAPRAKASH  J.S,Anjinamurthy H,','','0000-00-00','NC CREATE','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','','FI','yes','Fitting','Narasimha Murthy(R)','no','','|Re-checked all the completed parts and separated the affected parts.','E3456','qas|','2018-12-18|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11299,'35-446A','Saab AB','PIN','B80292','D5227353120000','NA','PART ISSUE B',8,'OWED-LTA-004','','82644','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1)12g7 Outer Dia under size.(7 nos)\r\n2) Tool Dig mark 1 no. ','1) 7No\'s OD undersized parts were identified in the inspection.|2) Due to chips rubbing mark in the OD the parts got line marks in order to remove the line marks the operator used scratch bright to polish the od and after the completion of polishing operation the OD got undersized and the operator did not identified it.|Improper checking method.','|Informed the operators to set dial gauge to inspect the close tolerance OD\'s which don\'t have Air gauge.','|Air gauge will be ordered and used for the close tolerance OD\'s','CAPA found ok.','','2018-12-04','Dinakar(K)','Yogesha K,Shanmukha R,Ravi K,Eranna K,CHETANA K,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','MakinoF5-4','Yashawantha(NH)','no','','|Checked all the other completed parts and found ok.','E3456','qas|','2018-12-06|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11300,'51-197','THE BOEING COMPANY','END FITTING-','20233630','3-48675-901','NA','PSDL REV -',2,'BOEING 001AA','','84170','','0000-00-00',NULL,'yes','no','no','no','yes','yes','no','no','no','7/16-20UNF-3B Thread plug Gauge NOGO Is  Entering ','NoGo gauge answered on thread 7/16-20UNF-3B |Re-tapping done due to that nogo gauge answering|During burr removal process burrs folded on inside due to that re-tapping carried out|Before threading process de-burr chamfer operation was not done sufficiently, due to that burr folding occurred','|During machining process de-burr chamfer to be maintain at maximum value','|During machining process de-burr chamfer to be maintain at maximum value','Next batches verified and found Ok.','','2018-12-05','pe_sez(a)','pe_sez(a)','','0000-00-00','7/16-20UNF3B Thread plug Gauge NOGO is  Entering ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FINAL INSPECTION','no','Misc','qas_sez(a)','no','','|Parts in WIP found ok','Z3456','pe|qas|','2019-05-17|2019-05-17|','2019-05-17',NULL,NULL,NULL,NULL,NULL,NULL),(11301,'35-604','Saab AB','SHAFT , VENT HOOKS','2878','D5227352920200','NA','PART ISSUE B',2,'OWED-LTA-004','','81911','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','OD undersized by 0.008-0.015 micron.','TOOL OFFSET WAS TAKEN WRONG IN BETWEEN THE PRODUCTION BATCH.|DUE TO INSERT WEAR OUT DURING THE PRODUCTION|TOOL INSERT WEAR OUT WAS NOT MONITORING.|TOOL MONITORING CHART WAS NOT HANDY.','|TOOL MONITORING CHART IS DISPLAYED NEAR THE MACHINE.','|TOOL MONITORING CHART IS DISPLAYED NEAR THE MACHINE.','CA/PA satisfied','','2018-12-05','pe_sez(a)','pe_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','05','no','Misc','pe_sez(a)','no','','|CHECKED ALL WORK ORDER QUANTITY.\r\nCHECKED FOR TOOL OFFSET.','Z3456','qas_sez|qas_sez|','2018-12-06|2019-01-18|','2019-01-18',NULL,NULL,NULL,NULL,NULL,NULL),(11302,'34-055A','Magellan Aerospace Winnipeg','BRACKET, AFT MOUNT-APU ','G25209','400-12611-1','NA','EM105092 Iss H,EM104765 Iss H',1,'C81597 Rev 001','','83600','','0000-00-00',NULL,'yes','','yes','','yes','','','','','Ruining time Z axis done so dig mark on part,  ','1) Tool dig mark because of wrong reference.|2) After entering the CRC the operator performed step run to verify the wall thickness but after verifying the operator pressed reset and entered the correction and started the cycle without instructing proper reference.|3) Operator block searched in the program to enter the CRC value, after entering the value he did not started the program from the beginning insterd he pressed the cycle start from the point he entered correction due to which the reference value was not properly calculated by the machine and caused to dig the part.','|1) Training given to all the operators on the procedure to be carried out while performing block search.\r<br/>2) Instruction chart will be displayed near the machine regarding procedure while entering corrections.','|Machining process is replaced with new fixture to avoid verifying the part in between.','CA PA implementation verified and found ok.','','2018-12-05','Dhananjaya(N)','        Dileep Kumar','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','7','','','','','','|Immediately stopped the machine and verified the references of the machine and offsets of all the tools verified.','E3456','pe|qas|qas|','2018-12-05|2018-12-17|2018-12-18|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11303,'35-526','Saab AB','ROD BODY','2878','D522 73337 200 00','','A',1,'OWED-LTA-004','','81918','','0000-00-00',NULL,'yes','no','no','no','yes','yes','no','no','no','GO THREAD GAUGE NOT ANSWERING','THE BORING OPERATION WILL BE DONE AFTER THE INTERNAL THREAD CUTTING SO BURR GOT FOLDED AFTER THE BORING OPERATION DUE TO WHICH THE THREAD GUAGE WAS NOT ANSWERING.','|EVERY THREAD PART WILL BE CHECKED IN THE FITTING AND RETAPPED IF THE GAUGE NOT ANSWERING BEFORE MOVING THE PARTS TO QUALITY. ','','REWORK DONE FOR THE PART AND ALL THE PARTS PRODUCED AFTERWORDS ARE FOUND OK','','2018-12-06','pe_sez(a)','Vijay Kumar H.J,Ravi Kumar G.B,Pradeep B.D,Dinakar K ,','','0000-00-00','5/16-24 UNJF-3B THREAD GAUGE. GO THREAD GAUGE IS NOT ANSWERING ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','','FI','yes','200MY-02','qas_sez(a)','no','','|ALL THE PARTS WERE CHECKED FOR THE THREAD PLUG GAUGE AND FOUND OK.\r\n','Z3456','qas_sez|qas_sez|','2019-02-13|2019-10-12|','2019-10-12',NULL,NULL,NULL,NULL,NULL,NULL),(11304,'35-082','Saab AB','HOUSING-SIDE ROLLER','6261301','F579 53065 202','ABM3-1029 T7651','B, PG52307ST4KA80',1,'1600207161','','80742','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','THREAD OPERATION NOT DONE','','','','','','2018-12-07','qas_sez(a)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','With Treatment','DN48405','POST DN','no','Misc','qas_sez(a)','no','','','Z3456','qas_sez|','2018-12-07|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11305,'18-117B','Magellan Aerospace Bournemouth',' 	HOUSING-OUT BD BRG','1593408-2/SDKC','PID275 40004 200','','C01',1,'428867','','79671','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','OD under-size up-to 0.02mm due to ovality','why1. Part fall done on ground unfortunately|why2. Due to insufficient place on table|why3. The part was loaded on corner portion of the table which has insufficient place to hold the part','|During machining operation the sufficient amount of parts only load on table and extra parts to be move on Tray / Rack','|The floor mat will be put on ground where the tables are available . That will be protect the parts from damages on impact on ground','CAPA found ok.','','2018-12-08','Ravi(M)','Ravi(M)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','011','no','Misc','Ravi(M)','no','','|The finished parts are moved to tray and table is maintaining to sufficient quantity of parts','E3456','qas|qas|','2018-12-10|2019-01-06|','2019-01-06',NULL,NULL,NULL,NULL,NULL,NULL),(11306,'43-026','Composite Industrie','BRACKET ','545816 B','V251 11617 201 00','','A00, ECN PV100298ST1AC92',1,'LTA COMPOSITES 2018-','','81426','','0000-00-00',NULL,'no','yes','yes','no','no','no','yes','no','no','Dig mark occurred on outer profile of the part','why1. Selection of tool is wrong|why2. During clamping hole operation another tool done on clamping hole instead of correct one.|why3. The tool number was not identified on program so the another tool selected on operation','|The program was update \'pop up\' message on tool selection during execution of program','|Instruction manual will be put on machines','Instruction manual will put on machines on 13-12-2018.\r\nImplementation verified and found ok.','','2018-12-08','Subramanya L(Naik)','Sunil G S,Eranna K,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','1','no','BMV 45-1','Subramanya L(Naik)','no','','|The tool number was updated on program and the next part was found ok','E3456','qas|qas|','2018-12-10|2018-12-18|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11307,'51-086','THE BOEING COMPANY','KICK LINK','G24256K05','251W3122-4','NA','PSDL REV -',1,'BOEING 001M','','83697','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','BACK SIDE WALL THICKNESS -0.2 SIDE','1) During roughing operation excess amount of material removed.|2) The newly generated program was leaving less stock during the roughing operation.|3) Due to chattering marks in the previous method program was revised during which the stock to be left in the part was not increased.','|Checked the program and corrected the stock value.','|1) New program generated with uniform stock value and next part produced found ok.\r<br/>2) MPS to be changed to the update with new program.','CA PA found ok.','','2018-12-08','Dhananjaya(N)','Dhananjaya(N)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','05','no','Misc','Punith G(S)','no','','|Immediately stopped the machine and informed the engineering department.','E3456','qas|qas|','2018-12-17|2019-04-08|','2019-04-08',NULL,NULL,NULL,NULL,NULL,NULL),(11308,'56-107','GKN Aerospace Orangeburg','FAIRING SUPPORT - FWD','1217701-1','119A1520-604','NA','PSDL REV A',1,'A000047469','','84549','','0000-00-00',NULL,'yes','no','no','no','no','yes','no','yes','no','Tool Dig Mark was evident on the base of the part which was not meeting the Required Part configuration','The program given to the machine had a Wrong Approach of cutting tool in Z-Axis|Multiple tool paths were manually merged to make it a single tool path which had resulted in a wrong tool approach which was not seen in program simulation|Programs were not verified before giving it to machine [G-Code Simulator/Verification]','|The programs given to the machine to run the Re-FAIR part was verified for such errors and was found okay','|NC Programs shall be cross verified with G-code simulator prior to transferring to the machine for machining for all 3-Axis tool paths','','','2018-12-08','CAD(sez)','                CAD(sez)','','0000-00-00','RIB THICKNESS NOMINAL DIMENTION IS 2.54 MM , MEASURED VALUE IS 1.55MM TO 2.7MM','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FAIR STAGE','no','Misc','qas_sez(a)','no','','|Part identified as rejected.','Z3456','cam|qas_sez|Deshpande|cam|qas_sez|','2018-12-21|2018-12-21|2019-10-18|2019-10-30|2019-11-05|','2019-11-05',NULL,NULL,NULL,NULL,NULL,NULL),(11309,'18-091A','Magellan Aerospace(Polska) Sp','BUSH','1649123-1/X7C7','PID278 50164 202','','A',9,'104569','','81472','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','1NO OD DIG MARK 1NO CHAMFER DOUBLED SIDE','1)a) Due to power fluctuation the Outer Diameter of the part got dig mark.\r\nb) The operator reloaded the part and continued the same cycle because of which the chamfer foe formed on both the side.|2)b) Due to un-clear face the operator loaded the same part and continued the entire cycle instead of running the facing cycle.|3)b) Lack of awareness on the rework procedure.','|Informed to the supervisor about the issue and segregated the parts with tapper face. ','|All the RM will be checked before loading to the machine and the RM\'s with more than .5mm taper will returned back to stores.','CAPA found ok.','','2018-12-08','Dinakar K()','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','01','no','Misc','GUNDEGOWDA(H.G.)','no','','|Immediately stopped the machine and checked the previously produced part for un-clear face and no similar parts were found.','E3456','qas|','2019-04-08|','2019-04-08',NULL,NULL,NULL,NULL,NULL,NULL),(11310,'35-458A','Saab AB','ROD BODY','34778216-B','D5227350920000','NA','PART ISSUE B',1,'OWED-LTA-005','','81123','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','outer diameter chamfer over size up to 0.8 instead of 0.2','Outer diameter chamfer over size|Tool nose compensation was not given properly.|Wrong value was input in the tool nose compensation. |The previous running tool was replaced with another tool,so the previous tool nose compensation was executed ','|Checked the offset value and changed the tool nose compensation value','|Check the tool nose compensation before machining.','CAPA found ok.','','2018-12-10','Dinakar(K)','Yogesha K,Shanmukha R,Ravi K,Eranna K,CHETANA K,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','MakinoF5-4','Yashawantha(NH)','no','','|Stopped the machine and informed the supervisor.','E3456','pe|qas|','2018-12-17|2018-12-18|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11311,'35-513','Saab AB','BRACKET','2290602','D522 73459 200 00','','A',1,'OWED-LTA-002','','84146','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','THICKNESS UNDER SIZE BY 0.1 MM','Due to Z axis down|Due to draw bar problem.  ','|1)Before starting the M/C draw bar will be cross checked.\r<br/>2)Now the M/C is under observation.','|1)Suspected Z axis encoder problem.\r<br/>2)Replaced Z axis motor.','Maintenance report verified and found ok.','','2018-12-10','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Punith G(S)','no','','|Inform to service Engineer. ','E3456','pe|qas|','2018-12-26|2019-01-06|','2019-01-06',NULL,NULL,NULL,NULL,NULL,NULL),(11312,'51-148','THE BOEING COMPANY','UPR SKIN COVER','R6J06/153800','312Z3121-501','NA','NIL',1,'BOEING 001X','','85357','','0000-00-00',NULL,'yes','no','no','no','no','yes','no','yes','no','Profile measured out of tolerance.','ENGINEERING POST PROCESSOR PROBLEM  G CODE OUT PUT PROBLUME |PROGRAM SIMULATION FOUND OK BUT G CODE OUT PUT WAS ERROR','|INFORMED TO THE SOFTWARE APPLICATION ENGINEERING ','|INFORMED TO THE SOFTWARE APPLICATION ENGINEERING ','SOFTWARE ENGINEERING HAS CAME AND CLEARED PROBLEM ','','2018-12-11','CAD(sez)','Shivaraj K S,Rajesha A.R,Anand ,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','PS105-02','qas_sez(a)','no','','|1.IDENTIFIED AND MACHINE STOPPED \r\n2.TOOL, PROGRAM, INSERT, AND OFFSET VERIFIED \r\n3.PART IDENTIFIED AS REJECTED \r\n4.INFORMED TO SUPERVISOR AND NCR WAS  RAISED ','Z3456','qas_sez|','2019-02-13|','2019-02-13',NULL,NULL,NULL,NULL,NULL,NULL),(11313,'18-371B','Magellan Aerospace Bournemouth','GAMMA FITTINGS','M034850','NSA840007-150PF','','N',2,'428930','','80275','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','ID Over size by 0.015 to 0.04mm.','operator has not identified ovality during operation.|In clamped condition dimension was measured using bore gauge.','|100% inspection by production team from next batch','|Improvement in clamping method is to be done.','Next batch found ok.(Inspection Qty-140 no\'s)','','2018-12-11','Dinakar(K)','Sathish G,Narasimha Murty S,Manoj Kumar D,Kantharaju M,Girish HP,Arun Kumar A M,Anil S,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','FI','no','QT100S-4','Narasimha Murthy(R)','no','','|100% Inspection done on remaining parts. ','E3456','pe|qas|','2018-12-12|2019-01-05|','2019-01-05',NULL,NULL,NULL,NULL,NULL,NULL),(11314,'18-371B','Magellan Aerospace Bournemouth','GAMMA FITTINGS','M034850','NSA840007-150PF','','N',1,'428930','','80275','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','ID Under size by 0.1mm.','M00 cycle was called.|To remove the formation of chips from the tool.\r\n|To improve the surface finish.','|100% inspection by production team from next batch.','|100% inspection by production team from next batch.\r<br/>Additional tool is added to avoid M00 cycle.','CA PA found ok.','','2018-12-11','Dinakar(K)','Sathish G,Narasimha Murty S,Manoj Kumar D,Kantharaju M,Girish HP,Arun Kumar A M,Anil S,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Manufacture Only','','FI','yes','QT100S-4','Narasimha Murthy(R)','no','','|100% Inspection done on remaining parts.','E3456','pe|qas|','2018-12-12|2018-12-18|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11315,'18-395A','Magellan Aerospace Bournemouth','VALVE','1826113/J9HJ','A284 40012 200','','A',7,'428872','','83343','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','OD Under size 0.005 to 0.012 mm.','1) Outer Diameter is measuring below the tolerance.|2) During the manual rework operator applied excess feed because of which excess amount of material was removed and resulted in under-size and the operator did not ensured the dimension of the part after rework.|3) Due to tapper formation in the part the operator need to provide correction during which the operator did not provided roper correction and resulted in oversize for which the rework was carried out. Operator did not verified the part because of lack of awareness to ensure the thickness after rework.','|Informed all the operator to separate the parts with proper identification tag in cause of rework.','|Rework operation will be carried out only in the presence of supervisor.','CAPA found ok.','','2018-12-13','Dinakar(K)','Rohith M,Dinakar K,Anil S,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','DX 200-2','Narasimha Murthy(R)','no','','|Checked all the completed parts and deviated parts separated.','E3456','qas|','2018-12-14|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11316,'18-395A','Magellan Aerospace Bournemouth','VALVE','182613/J9HJ','A284 40012 200','','A',12,'428872','','83342','','0000-00-00',NULL,'yes','no','no','no','yes','yes','no','no','no','OD Under size 0.008 to 0.020 mm.','1) Outer Diameter is measuring below the tolerance.|2) During the manual rework operator applied excess feed because of which excess amount of material was removed and resulted in under-size and the operator did not ensured the dimension of the part after rework.|3) Due to tapper formation in the part the operator need to provide correction during which the operator did not provided roper correction and resulted in oversize for which the rework was carried out. Operator did not verified the part because of lack of awareness to ensure the thickness after rework.','|Informed all the operator to separate the parts with proper identification tag in cause of rework.','|Rework operation will be carried out only in the presence of supervisor.','CAPA found ok.','','2018-12-13','Dinakar(K)','Rohith M,Dinakar K,Anil S,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','DX 200-2','Narasimha Murthy(R)','no','','|Checked all the completed parts and deviated parts separated.','E3456','qas|','2018-12-14|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11317,'18-395A','Magellan Aerospace Bournemouth','VALVE','182613/J9HJ','A284 40012 200','','A',1,'428872','','83342','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','OD Over size 0.05mm.','1) Outer Diameter is measuring below the tolerance.|2) Due to improper taper correction the outer diameter of the part got oversize and the part reached inspection without identification.|3) Improper communication between operator and supervisor about the rework and the operator was not aware of the identification requirements.','|Informed all the operators to properly identify the parts and carry out rework only in the presence of supervisor.','|Training to be given to the operator on rework procedure and need of identification.','CAPA found ok.','','2018-12-13','Dinakar(K)','Rohith M,Dinakar K,Anil S,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','With Treatment','','FI','no','DX 200-2','Narasimha Murthy(R)','no','','|Checked all the completed parts and identified the similar parts.','E3456','qas|qas|qas|','2018-12-14|2018-12-17|2019-03-30|','2019-03-30',NULL,NULL,NULL,NULL,NULL,NULL),(11318,'18-437B','Magellan Aerospace(Blackpool) Limited','MANIFOLD','29098139-2','PI201274625','NA','NIL',15,'Bpp-529619 amed-2','','81161','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Out of tolerance surface finishes due to excessive frazing','1.The fitting work carried on outside of the part due to that surface finish value exceeded the tolerance value|2.During milling operation step mismatches occurred on outside surface due to that fitting work carried out in the grade of 180|3.The tool overhanging occurred on machining due to that steps mismatch occurred|4.During tool loading and offset process the tool overhanging was not considered','|Quality alert created for fitting operation regarding during fitting operation the using emery paper grade is changed from 180 to 220 and the tool length also to be monitor','|During milling operation the tool overhanging to be consider and that should be control via Zoller Machine offset controller which gives the correct tool length value for to avoid overhanging on machine and that will be avoid surface mismatches. And the emery grade of 220 also to avoid surface mismatches','CAPA FOUND OK','C70655','2018-12-13','Nandishkumar(D.K.)','Ranjith(G)','RDN 5091','2018-12-11','NC CREATE','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','CUST END','no','Misc','Ranjith(G)','no','','|The parts in FG are ensured that surface finish value attained as per drawing requirement','E3456','qas|qas|','2018-12-24|2018-12-24|','2018-12-24',NULL,NULL,NULL,NULL,NULL,NULL),(11319,'18-438B','Magellan Aerospace(Blackpool) Limited','MANIFOLD ','263901 1428','PI55-1213031-00','NA','NIL',2,'Bpp-529619 amed-2','','81156','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Out of tolerance surface finishes due to excessive frazing','Why-1:a) The final finished part\'s surface mismatch cleared via fitting rework.\r\nb) Surface finish was ensured via surface comparator. |Why-2: a) During milling operation surface mismatches occurred due to tool overhanging.\r\nb) The tool offset was adjusted manually.|Why-3: The tool offset was adjusted manually.|Why-4:The method followed for adjusting tool offset was not robust.','|Process: Tool offset adjustment will be done in machine(Zoller Machine).\r<br/>Quality: Using Surface Roughness Tester to ensure Surface roughness value.','|Process: Tool offset adjustment will be done in machine(Zoller Machine).\r<br/>Quality: Using Surface Roughness Tester to ensure Surface roughness value.','CA PA found ok.','C70656','2018-12-13','Nandishkumar(D.K.)','Ranjith(G)','RDN 5093','2018-12-11','NC CREATE','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','CUST END','no','Misc','Ranjith(G)','no','','|The parts in FG (Total quantity of 29 nos) are ensured that surface finish value attained as per drawing requirement','E3456','qas|','2019-01-06|','2019-01-06',NULL,NULL,NULL,NULL,NULL,NULL),(11320,'47-193','GKN Aerospace Filton','M/C HINGE POST 4 I/A','520635','F5755516720003','NA','PART ISSUE A',1,'GKN-GS-068 PHASE2- L','','84610','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Refer NC NO:10744','Refer NC NO:10744','|Refer NC NO:10744','|Refer NC NO:10744','Refer NC NO:10744','','2018-12-13','pe_sez(a)','HariPrasad()','','0000-00-00','<NC Fill>','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','pe_sez(a)','no','','|Refer NC NO:10744','Z3456','qas_sez|','2019-01-16|','2019-01-16',NULL,NULL,NULL,NULL,NULL,NULL),(11321,'42-009','RAFAEL Advanced Defence Systems Ltd.','UPPER ENVELOPE','22279326','CU2G0002A','','111.22 Rev 2, TILDOCS#172373 Rev 14, RAFDOCS5224238 Rev 5, 111.21 Rev 9',1,'347692469','','60493','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Chamfer oversize by 0.5mm','Hole chamfer oversize due to high depth. |Since the tool used for the hole operation is a combination of both hole drill and chamfer operation.|The depth of the drill was not controlled in the program.|CAD engineer did not considered the tool length and depth requirement before generating the program.','|Adjusted the tool height and regenerated the program and next part found ok.','|Standard tooling dimensions and programing requirements will be captured before generating the program.','Next programs proving time verified and found ok.','','2018-12-14','Ramesh(Poojary)','Lokesh(B.D.)','','0000-00-00','NC CREATE','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','02','no','Misc','Nandishkumar(D.K.)','no','','|Immediately stopped the machine and informed the engineering department.','E3456','qas|','2019-01-07|','2019-01-07',NULL,NULL,NULL,NULL,NULL,NULL),(11322,'51-134','THE BOEING COMPANY','STRUT, FWD','8-27-06662','112A7111-1','NA','PSDL REV -',1,'BOEING 001W','','83851','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Running time insert was broken so double thread was formed.','Chip clocked in the insert|No suffient coolant on the tool while running the ID thread|Insert life was definded','|1.threading insert was was replaced and correct offset was taken.\r<br/>2.The flow of the coolant was adjusted on to the thread so as to avoid the heat generated while cutting the material','|For all the parts in which the bore length is very big ,operators were instructed to set the coolant flow and then run the production.','Next part machined and thread found ok ','','2018-12-14','pe_sez(a)','pe_sez(a)','','0000-00-00','NC Fill.......','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','05','no','Misc','pe_sez(a)','no','','|1.The part was identified and Internal NCR was raised\r\n2.The machine was stopped and informed to the supervisor\r\n','Z3456','qas_sez|','2019-01-22|','2019-01-22',NULL,NULL,NULL,NULL,NULL,NULL),(11323,'35-586A','Saab AB','HANDLE','2290602','D5227342720300','NA','PART ISSUE D',1,'OWED-LTA-005','','83751','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Tool dig mark.','Instead of 10R2 ball nose 9.52 hole mill called.|Due to tool magazine problem tool interchanged.|machine controlled hanged.','|Informed all the operators to cross check the tool magazines after any controlled issue before starting the cycle.','|During every preventive maintenance machine controlled will be cross checked.','CA PA found ok.','','2018-12-15','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Dhananjaya(N)','no','','|Immediately machine was stopped and called the service engineer to solve the issue.','E3456','qas|','2018-12-18|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11324,'56-005','GKN Aerospace Orangeburg','SPLICE PLATE FWD UPR','14336DC','119A1213-603','NA','PSDL REV -',1,'LTA GKN 737 Winglet','','77192','','0000-00-00',NULL,'yes','no','yes','no','yes','no','no','no','no','HOLE POSITION NOT ACHIEVED ','Dimension of a 3D point from a hole measured out of tolerance.|Hole Shifted during the 5axis machining time.|Rotary did not tilted to the required angle.|Problem with the movement of the rotary.|Rotary was not activated by the OEM(U-CAM) during the machine manufacturing.','1) Loaded the FAIR part in other machine and proved the program. (i700 machine)','Maintenance team from machine supplier and Solid cam programmers arrived onsite and solved the rotary issue and the problem is not repeated. ','Problem is rectified by OEM onsite and no further issues occurred.','','2018-12-15','pe_sez(a)','Kiran Kumar M,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Cancelled','no','yes','no','With Treatment','','3','no','PS105-01','pe_sez(a)','no','','Immediately stopped the machine and informed the maintenance team. and maintenance team informed to OEM (U-CAM) for the site visit.','E3456','qas|','2018-12-15|',NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11325,'35A-016','Saab AB','ASSY - SIDE ROLLER','','L579 50525 000','','A',1,'1600219291','','A20723','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','TAP NOT DONE','the part was removed from the machine before the tapping operation completed|The drill was broken prior to tapping and the broken drill was not able to remove in the machine ,so planned to do the tapping manually in hand|The part was not identified and the same was moved forward for further operation.','|1.Instruction given to all the operators if any non conformance observed during machining to first raise an NCR and identify the parts with tag and move to Quality Clinic.','|Refer to CA','next batch machined and found ok ','','2018-12-17','qas_sez(a)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','Assembly','','FI','no','Misc','qas_sez(a)','no','','|1.All the parts were once again checked 100% for tapping operation and found ok.\r\n2.This one number manually tapping was done and accepted','Z3456','qas_sez|qas_sez|qas_sez|','2018-12-18|2018-12-19|2019-04-17|','2019-04-17',NULL,NULL,NULL,NULL,NULL,NULL),(11326,'35-427','Saab AB','BRACKET','745697','D522 73394 201 00','','A',1,'1600186297','','82997','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','PART OVER TIGHT SO PART IS BROKEN','Part over tighten|1) During the second set up operation the x0, y0 offset taken was wrong.|2) The part was loaded to the fixture which was critical for the operator and was not comfortable due to which the reference plane varies between parts and because of this the tool dropped over the part directly and resulted in bend of the part.|3) Constrains on the given engineering process.','part tighted medium|Corrected the reference of the tools and continued the production.','to inform all the operaters to maintain medium tight|Re-Engineering process to be carried out on first Feb-2019.','NC is closed temporarily and will be revisited bi-week once.','','2018-12-18','Dinesh kulal()','prodn_aero(prodn)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','2ND','no','Misc','prodn_aero(prodn)','no','','stop the machine and check the part','A3456','qas|','2018-12-19|','2018-12-19',NULL,NULL,NULL,NULL,NULL,NULL),(11327,'35-525A','Saab AB','ROD BODY','30685304B','D5227333620000','NA','PART ISSUE B',2,'OWED-LTA-005','','81143','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','PITCH DIMENSION UNDER SIZE BY 0.1MM TO 0.15MM, NOMINAL 10MM ','WRONG LOADING|OPERATOR HAS NOT FOLLOWED THE INSTRUCTIONS GIVEN BY SUPERVISOR','|OPERATOR IS TRAINED AND ADVISED TO FOLLOW THE INSTRUCTIONS PROPERLY. ','|WORK INSTRUCTIONS WILL BE DISPLAYED NEAR THE MACHINE','capa found satisfactory','','2018-12-18','pe_sez(a)','pe_sez(a)','','0000-00-00','PITCH DIMENSION UNDER SIZE BY 0.1MM TO 0.15MM, NOMINAL 10MM ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','Misc','qas_sez(a)','no','','|MACHINE WAS STOPPED AMD INFORMED TO THE SUPERVISOR','Z3456','qas_sez|qas_sez|','2019-02-14|2019-04-12|','2019-04-12',NULL,NULL,NULL,NULL,NULL,NULL),(11328,'35-525A','Saab AB','ROD BODY','34778216-A','D5227333620000','NA','PART ISSUE B',1,'OWED-LTA-005','','81144','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Total length undersized.','Why-1: Due to face run out the total length of the part got undersized.|Why-2: Due to run out in the jaws ID the part has face out.|Why-3: Due to improper jaws boring & operator did not dialed the jaws before loading the part. ','|1.The jaws were re bored \r<br/>2.Run Checked and found it was with in 0.01 mm','|Instructions displayed near the machine to explain operator to how to bore the jaws & check it before running the part.','Next part machined and total length was measuring with in the drawing tolerance','','2018-12-18','Dinakar K()','Dinakar K()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','05','no','Misc','Dinakar K()','no','','|1.Machine was stopped\r\n2.Run out in the jaws was checked and found runt out was 0.2mm \r\n','Z3456','qas_sez|','2019-01-22|','2019-01-22',NULL,NULL,NULL,NULL,NULL,NULL),(11329,'35-428A','Saab AB','BRACKET','532747C','D5227341520000','NA','PART ISSUE A',1,'OWED-LTA-001','','83002','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','RM Reverse loaded so part width minus upto 1mm','1. Rm side of 32mm loaded instead of 30mm|2. Operator could not identify visually the right side to be loaded.|3. No clear indication on RM for size/loading orientation.','|RM to be marked with \"TOP\" WRT M/C loading orientation.\r<br/>Training to be given to operator regarding the same.','|Alert message to be introduced in program so as to alert operator.','CA/PA found acceptable.','','2018-12-18','Dinesh kulal()','prodn_aero(prodn)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','1ST','no','Misc','prodn_aero(prodn)','no','','|Inspected the batch and found OK.','A3456','qas|qas_sez|','2018-12-19|2019-05-15|','2019-05-15',NULL,NULL,NULL,NULL,NULL,NULL),(11330,'56-035','GKN Aerospace Orangeburg','CLOSEOUT RIB - LWR, FWD','445511','119A1440-603','NA','PSDL REV B',1,'LTA Orangeburg 737 W','','82891','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Profile miss match','OPERATOR ENTERED THE WRONG OFFSET VALUE  |RUNNING TIME DUE TO OFFSET PROBLEM MISMATCH WAS FOUND ','|1.RE CHECKED THE ALL OFFSET VALUE AND CHANGED THE READING WHICH WAS ENTERED\r<br/>2.CHANGED THE SOME TOOLS.  ','|1. TRAINING THE OPERATOR AND GUIDING HIM \r<br/>2. IMPLEMENTING THE TOOL OFFSET BY USING ZOOLAR MACHINE\r<br/>3. WHICH GIVE TOOL OFFSET READING \r<br/> ','IMPLEMENTATION OF THE OFFSET BY USING ZOOLAR MACHINE FOUND SATISFACTORY ','','2018-12-18','pe_sez(a)','pe_sez(a)','','0000-00-00','NC FILL......','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','pe_sez(a)','no','','|1.INFORMED TO THE SUPERVISOR  \r\n2.INSPECTED THE PART FULLY AND ENSURED THE PARTS OTHER DIMENSION OK \r\n','Z3456','pe_sez|qas_sez|','2018-12-25|2019-02-13|','2019-02-13',NULL,NULL,NULL,NULL,NULL,NULL),(11331,'35-184','Saab AB','CED_LATCH_FITTING-AFT','1750036386','425Z0610-16','','---',2,'Forecast po for B787','','82785','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Position out of tolerance.','1) During hole operation time the hole position got shifted.`|2) The hole operation and the reference point for the hole are carried out in two different setups due to which the position got shifted.|3) The part processing method was not convenient for the operator to locate the reference point. ','|Informed the operator to check the location of the part before continuing the production.','|Re-Engineering to be carried out to change the process.','Re-Engineering process to be completed on or before 1-Feb-19.','','2018-12-19','Dinesh kulal()','Dinesh kulal()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','07','no','Misc','Dinesh kulal()','no','','|Immediately stopped the production and given correction to the program and continued the production.','A3456','qas|','2018-12-19|','2018-12-19',NULL,NULL,NULL,NULL,NULL,NULL),(11332,'47-214','GKN Aerospace Filton','BLOCK COVER LH','8078501-1','D5725097420802','NA','N',1,'GKN-GS-068 PHASE1- L','','84247','','0000-00-00',NULL,'yes','no','no','no','no','yes','no','yes','no','Refer NC NO:10744','Refer NC NO:10744','|Refer NC NO:10744','|Refer NC NO:10744','Refer NC NO:10744','','2018-12-19','pe_sez(a)','Tejas M,Somashekar ,Rajesha A.R,Raghu B,Madhu Kumar N,Kiran KM,','','0000-00-00','TOOL DIG MARK ON THE PART.','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','Slim3n-4AHS-4','qas_sez(a)','no','','|Refer NC NO:10744','Z3456','qas_sez|','2019-01-16|','2019-01-16',NULL,NULL,NULL,NULL,NULL,NULL),(11333,'35-689','Saab AB','BRACKET','473615 C','D5227283320100','NA','PART ISSUE A',3,'OWED-LTA-004','','79756','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','part dig mark occurred','1.During running time tool was broken|2.Tool overhang occurred|3.Operator made mistake during tool load on holder','','','CAPA found ok','','2018-12-19','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Prashanth Kumar(M)','no','','','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11334,'35-455A','Saab AB','BRACKET ','LL0100697','D5227345720000','NA','PART ISSUE A',1,'OWED-LTA-005','','80586','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','part outer profile unclear.','Chattering on the part profile occurred during the roughing operation.\r\n|Screw used to lock the insert got loosed during the machining operation.\r\n|The head of the align key used to tight the insert screw was blunt because of which the insert got loosed during the machining and affected the profile','','','CAPA found ok','','2018-12-19','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','1','no','Misc','Subramanya L(Naik)','no','','','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11335,'35-710','Saab AB','LEVER','C90771','D5227346621100','NA','PART ISSUE D',1,'OWED-LTA-004','','81935','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','HOLE POSITION PROBLEM.','1.During milling operation hole ovality occurred|2.Drill bit was burnt|3.Drill bit tool life was expired','','','CAPA found ok','','2018-12-19','Ramesh(Poojary)','Kammar Nagaraj,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','3','no','HAASVF2SS-1','Dhananjaya(N)','no','','','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11336,'35-600','Saab AB','FRAME','3809601','D5227338520400','NA','PART ISSUE C',1,'OWED-LTA-001','','81628','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','part plian face dig mark,','Part got dig mark on the bottom face.|Chips from the broken tool got located under the part during the machining and caused dig mark on the part.|Tool got broken during the machining time and the operator did not cleaned the butting faces properly before loading the next part.|During the movement of semi finished material on the fixture the broken chips got relocated in between the part and the fixture.','|Informed all the operators to lift and place the part on the fixture and not to drag on the machine surface.','|Chips and scraps from the machine bed to be cleaned once in 4 Hrs incase of bigger materials.','CA PA found ok.','','2018-12-20','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','05','no','Misc','Anjinamurthy(H)','no','','|Immediately stopped the machine and cleaned the complete machine bed and fixture.','E3456','qas|','2019-01-06|','2019-01-06',NULL,NULL,NULL,NULL,NULL,NULL),(11337,'35-621','Saab AB','PIN','C80552.SD4W','D5227281820000','NA','PART ISSUE A',1,'OWED-LTA-004','','71759','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','yes','Is condition: PIN has no groove in the head or hole through threads. See drawing and photos below.\r\nShould be: Groove and hole according to the drawing D52272818','1. Part is not having groove and hole on thread|2. During final inspection the operation missing was not identified|3. During machining the operation missing occurred','During inspection the parts are all to be identify with all operations','During machining the operations to be complete as per MPS  required operations of the part and move into inspection','CAPA found ok','C63949','2018-12-20','Yashawantha(NH)','Yashawantha(NH)','OF-003131','2018-08-08','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','DN39422','Cust End','no','Misc','qas(qas)','no','','The parts in FG and in process found ok','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11338,'18-295A','Magellan Aerospace Bournemouth','BOLT','718445','PID577 56145 200','','A',1,'423258','','81792','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Part OD Dig mark.','Why-1: During turning operation OD dig mark occurred.|Why-2: Due to insufficient air pressure.|Why-3: Problem on pressurized air supply source.|Why-4: leakage in pressure hose.','|continued the production when the required pressure was achieved.','|Air hoses to be reviewed during every preventive maintenance.','CA PA found ok.','','2018-12-20','Ravi(M)','        Ningaraj A N','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','09','','','','','','|Compressed air supply hose was replaces and verified for leakage.','E3456','pe|pe|qas|','2018-12-21|2018-12-21|2019-01-06|','2019-01-06',NULL,NULL,NULL,NULL,NULL,NULL),(11339,'35-454A','Saab AB','SEAL RETAINER ','788619','D522 73425 201 00','','PART ISSUE B',1,'OWED-LTA-002','','84145','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Refer NC NO:10744','Refer NC NO:10744','|Refer NC NO:10744','|Refer NC NO:10744','Refer NC NO:10744','','2018-12-21','pe_sez(a)','pe_sez(a)','','0000-00-00','part cut out running time tool dig mark','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','NataRaj.CV()','no','','|Refer NC NO:10744','Z3456','qas_sez|','2019-01-16|','2019-01-16',NULL,NULL,NULL,NULL,NULL,NULL),(11340,'51-140','THE BOEING COMPANY','STRUT, FWD','H7L00/177972','112A7111-601','NA','PSDL REV -',2,'BOEING 001W','','83874','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Refer NC NO:10744','Refer NC NO:10744','|Refer NC NO:10744','|Refer NC NO:10744','Refer NC NO:10744','','2018-12-22','pe_sez(a)','pe_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Cancelled','no','yes','no','With Treatment','','07','no','Misc','pe_sez(a)','no','','|Refer NC NO:10744','Z3456','qas_sez|','2019-01-16|','2019-01-16',NULL,NULL,NULL,NULL,NULL,NULL),(11341,'18-119B','Magellan Aerospace Bournemouth',' 	HOUSING OUT B DRG 3 ','1646266/WKM7','PID275 40011 200','','D01',2,'428868','','81767','','0000-00-00',NULL,'yes','yes','yes','','','','','','','due to an wrong CRC given and run the tool so part will be undersize upto 2mm','1.During milling operation excess amount of material was removed|2.Wrong cutter composition was given|3.During change of tool, the cutter composition needs to be given, but that was not given. The milling operation was carried out as per the last tool\'s cutter composition','|The cutter composition option to be remove on the program, and tool control on program itself, their is no need of manual entry','|To avoid of manual entry, the cutter composition option on program to be removed','NC program changed and MPS up issued.','','2018-12-22','Anjinamurthy(H)','        BHUVANAPRAKASH  J.S','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','07','','','','','','|The cutter composition was corrected and ran the remaining parts.','E3456','qas|qas|qas|','2018-12-22|2018-12-22|2019-01-06|','2019-01-06',NULL,NULL,NULL,NULL,NULL,NULL),(11342,'18-749A','Magellan Aerospace Wrexham','CONNECTOR RIB 15','25458141','D2825102120101','NA','A',1,'178778','','84722','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','Tool Dig Mark was evident on the part which was not meeting the Required Part configuration.','The program given to the machine had followed a wrong path while running the 5 axis tool path.|The G-Codes output was following a wrong tool path which was not seen in program simulation|Program was generated by Mirroring the proved program of the LH Part which has given a wrong output|The Programming Process/Sequence was not correct which was not verified |Programs were not verified before giving it to machine [G-Code Simulator/Verification]','|Mirrored 5-Axis programs was cross verified before giving it to machine','|All NC Programs given to a 5 axis machine shall be cross verified with G-code simulator prior to transferring to the machine for machining. CAM Software team was informed to get a Permanent counter measure','','','2018-12-24','CAD(sez)','                CAD(sez)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','11','no','Misc','pe_sez(a)','no','','|Part identified as rejected.Similar parts with similar merged programs where Cross-verified and they were all found okay','Z3456','|qas_sez|Deshpande|cam|qas_sez|','2018-12-24|2019-01-16|2019-10-18|2019-10-30|2019-11-05|','2019-11-05',NULL,NULL,NULL,NULL,NULL,NULL),(11343,'47-028A','GKN Aerospace Filton','RUBBING STRIP','D656850','F57550373200','NA','C, MIS ISSUE B',1,'S.A.No. 6200005328','','81829','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','DIA 2.46MM HOLE POSITION 0.82MM SHIFTED.','Locating pin miss placed in wrong hole, due to which bend in the part was not arrested.|Fixture X0Y0 hole(dia 8mm) is in line with the ho;e on part which didnot arrest the locating pin(Dia 2.4mm)','|Fixture design will be modified.','|Fixture design will be modified.','Fixture correction and process sheet correction also verified and found ok.','','2018-12-24','Narayanappa(G)','Mohan Kumar C.M.,Manjunatha N.R.,Balaji ,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','HASS VR11','Nandishkumar(D.K.)','no','','|Whole batch was inspected and found OK.','E3456','pe|qas|','2019-01-06|2019-01-06|','2019-01-06',NULL,NULL,NULL,NULL,NULL,NULL),(11344,'18-437B','Magellan Aerospace(Blackpool) Limited','MANIFOLD','M670080/3686','PI201274625','NA','NIL',5,'Bpp-529619 amed-2','','81158','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Out of tolerance surface finish due to excessive frazing','Why-1:a) The final finished part\'s surface mismatch cleared via fitting rework.\r\nb) Surface finish was ensured via surface comparator.\r\n|Why-2: a) During milling operation surface mismatches occurred due to tool overhanging.\r\nb) The tool offset was adjusted manually.\r\n|Why-3: The tool offset was adjusted manually.|Why-4: The method followed for adjusting tool offset was not robust.','|Process: Tool offset adjustment will be done in machine (Zoller Machine).\r<br/>Quality: Using Surface Roughness Tester to ensure Surface roughness value.\r<br/>','|Process: Tool offset adjustment will be done in machine (Zoller Machine).\r<br/>Quality: Using Surface Roughness Tester to ensure Surface roughness value.\r<br/>','CA PA found ok.','C70107','2018-12-24','Nandishkumar(D.K.)','Ranjith(G)','5094','2018-12-14','NC CREATE','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','CUST END','no','Misc','Ranjith(G)','no','','|The parts in FG (Total quantity of 29 no’s) are ensured that surface finish value attained as per drawing requirement','E3456','qas|','2019-01-06|','2019-01-06',NULL,NULL,NULL,NULL,NULL,NULL),(11345,'18-437B','Magellan Aerospace(Blackpool) Limited','MANIFOLD','29098139-2','PI201274625','NA','NIL',7,'Bpp-529619 amed-2','','81159','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Out of tolerance surface finish due to excessive frazing','Why-1:a) The final finished part\'s surface mismatch cleared via fitting rework.\r\nb) Surface finish was ensured via surface comparator.\r\n|Why-2: a) During milling operation surface mismatches occurred due to tool overhanging.\r\nb) The tool offset was adjusted manually.\r\n|Why-3: The tool offset was adjusted manually.|Why-4: The method followed for adjusting tool offset was not robust.','|Process: Tool offset adjustment will be done in machine (Zoller Machine).\r<br/>Quality: Using Surface Roughness Tester to ensure Surface roughness value.\r<br/>','|Process: Tool offset adjustment will be done in machine (Zoller Machine).\r<br/>Quality: Using Surface Roughness Tester to ensure Surface roughness value.\r<br/>','CA PA found ok.','C70107','2018-12-24','Nandishkumar(D.K.)','Ranjith(G)','5094','2018-12-14','NC CREATE','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','CUST END','no','Misc','Ranjith(G)','no','','|The parts in FG (Total quantity of 29 no’s) are ensured that surface finish value attained as per drawing requirement.','E3456','qas|','2019-01-06|','2019-01-06',NULL,NULL,NULL,NULL,NULL,NULL),(11346,'18-437B','Magellan Aerospace(Blackpool) Limited','MANIFOLD','29098139-2','PI201274625','NA','NIL',4,'Bpp-529619 amed-2','','81160','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Out of tolerance surface finish due to excessive frazing','Why-1:a) The final finished part\'s surface mismatch cleared via fitting rework.\r\nb) Surface finish was ensured via surface comparator.\r\n|Why-2: a) During milling operation surface mismatches occurred due to tool overhanging.\r\nb) The tool offset was adjusted manually.\r\n|Why-3: The tool offset was adjusted manually.|Why-4: The method followed for adjusting tool offset was not robust.','|Process: Tool offset adjustment will be done in machine (Zoller Machine).\r<br/>Quality: Using Surface Roughness Tester to ensure Surface roughness value.\r<br/>|Process: Tool offset adjustment will be done in machine (Zoller Machine).\r<br/>Quality: Using Surface Roughness Tester to ensure Surface roughness value.\r<br/>','|Process: Tool offset adjustment will be done in machine (Zoller Machine).\r<br/>Quality: Using Surface Roughness Tester to ensure Surface roughness value.\r<br/>|Process: Tool offset adjustment will be done in machine (Zoller Machine).\r<br/>Quality: Using Surface Roughness Tester to ensure Surface roughness value.\r<br/>','CA PA found ok.','C70108','2018-12-24','Nandishkumar(D.K.)','Ranjith(G)','5094','2018-12-14','NC CREATE','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','CUST END','no','Misc','Ranjith(G)','no','','|The parts in FG (Total quantity of 29 no’s) are ensured that surface finish value attained as per drawing requirement.|The parts in FG (Total quantity of 29 no’s) are ensured that surface finish value attained as per drawing requirement.','E3456','qas|qas|','2019-01-06|2019-01-06|','2019-01-06',NULL,NULL,NULL,NULL,NULL,NULL),(11347,'18-436B','Magellan Aerospace(Blackpool) Limited','MANIFOLD ','C0201787385','PI201274624','NA','NIL',2,'Bpp-529619 amed-2','','77840','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Out of tolerance surface finish due to excessive frazing','Why-1:a) The final finished part\'s surface mismatch cleared via fitting rework.\r\nb) Surface finish was ensured via surface comparator.\r\n|Why-2: a) During milling operation surface mismatches occurred due to tool overhanging.\r\nb) The tool offset was adjusted manually.\r\n|Why-3: The tool offset was adjusted manually.|Why-4: The method followed for adjusting tool offset was not robust.|The parts in FG (Total quantity of 29 no’s) are ensured that surface finish value attained as per drawing requirement.','|Process: Tool offset adjustment will be done in machine (Zoller Machine).\r<br/>Quality: Using Surface Roughness Tester to ensure Surface roughness value.\r<br/>','|Process: Tool offset adjustment will be done in machine (Zoller Machine).\r<br/>Quality: Using Surface Roughness Tester to ensure Surface roughness value.\r<br/>','CA PA found ok.','C70145','2018-12-24','Nandishkumar(D.K.)','Ranjith(G)','5095','2018-12-14','NC CREATE','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','CUST END','no','Misc','Ranjith(G)','no','','|The parts in FG (Total quantity of 29 no’s) are ensured that surface finish value attained as per drawing requirement.','E3456','qas|','2019-01-06|','2019-01-06',NULL,NULL,NULL,NULL,NULL,NULL),(11348,'18-436B','Magellan Aerospace(Blackpool) Limited','MANIFOLD ','M989980/24194','PI201274624','NA','NIL',14,'Bpp-529619 amed-2','','81163','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Out of tolerance surface finish due to excessive frazing','Why-1:a) The final finished part\'s surface mismatch cleared via fitting rework.\r\nb) Surface finish was ensured via surface comparator.\r\n|Why-2: a) During milling operation surface mismatches occurred due to tool overhanging.\r\nb) The tool offset was adjusted manually.\r\n|Why-3: The tool offset was adjusted manually.|Why-4: The method followed for adjusting tool offset was not robust.','|Process: Tool offset adjustment will be done in machine (Zoller Machine).\r<br/>Quality: Using Surface Roughness Tester to ensure Surface roughness value.\r<br/>','|Process: Tool offset adjustment will be done in machine (Zoller Machine).\r<br/>Quality: Using Surface Roughness Tester to ensure Surface roughness value.\r<br/>','CA PA found ok.','C70145','2018-12-24','Nandishkumar(D.K.)','Ranjith(G)','5095','2018-12-14','NC CREATE','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','CUST END','no','Misc','Ranjith(G)','no','','|The parts in FG (Total quantity of 29 no’s) are ensured that surface finish value attained as per drawing requirement.','E3456','qas|','2019-01-06|','2019-01-06',NULL,NULL,NULL,NULL,NULL,NULL),(11349,'18-116B','Magellan Aerospace Bournemouth','ASSEMBLY FORKEND','7111','F575 51377 200','','A',1,'428867','','83245','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Thread effective diameter under size.','Run out observed on shaft.|Cone face improper butting in fixture.|Spear diameter is in higher tolerance.|  ','|Informed to Supervisor and operator to maintain the spear diameter in lower tolerance.   ','|1)Informed to Supervisor and operator to maintain the spear diameter in lower tolerance.\r<br/>2)Amended the MPS to reduce the spear tolerance.\r<br/> ','Effectiveness will be measured on Feb-18.','','2018-12-24','Raghavendra Rao(R)','Mohan Trishul(D P)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','07','no','Misc','Raghavendra Rao(R)','no','','|Ensured the diameter for the remaining parts and run the M/C.','E3456','|qas|','2018-12-25|2019-01-06|','2019-01-06',NULL,NULL,NULL,NULL,NULL,NULL),(11350,'35-601','Saab AB','FRAME','2313602','D5227338520600','NA','PART ISSUE C',1,'OWED-LTA-001','','81633','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','wall dig marak','Due to tool broken wall got dig marked.|Due to tool wear tool got broken and broke.|New tool was used for continual improvement purpose during which the tool got broken as the tool life was not aware.','|Informed the tool grib personnel to clearly address the tool life of new tools when purchased.','|Care will be taken during the trial of new tools.','CA PA found ok.','','2018-12-24','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','05','no','Misc','Anjinamurthy(H)','no','','|Immediately stopped the machine and continued the production with the previously used tool.','E3456','qas|','2019-01-06|','2019-01-06',NULL,NULL,NULL,NULL,NULL,NULL),(11351,'51-198','THE BOEING COMPANY','TENSION TUBE','F00280238-0001','251A3149-902','NA','PSDL REV-',1,'BOEING 001AA','','84182','','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','','2018-12-24','qas_sez(a)','Siddesha Y.V,Sagar C.V,Dinakar K ,','','0000-00-00','HOLE DAMAGE ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','DN49820','FI','no','200MY-02','qas_sez(a)','no','','|Refer NC NO:10744','Z3456','qas_sez|','2019-01-16|','2019-01-16',NULL,NULL,NULL,NULL,NULL,NULL),(11352,'35-600','Saab AB','FRAME','2313601','D5227338520400','NA','PART ISSUE C',1,'OWED-LTA-001','','81624','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','rib tao un clear ','Why 1: Due to bend in the part the rib top got uncleared.|Why 2: Due to revision of process the part got bend.|Why 3: In-order to improve the cycle time of the process the machining process was revised during which the part got excess bend and while correcting the excess bend the rib top got uncleared.','|Continued the production with previous proven process.','|Improved process will be verified through simulation before proving on the part.','CA PA found ok.','','2018-12-24','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','05','no','Misc','Anjinamurthy(H)','no','','|Immediately stopped the production and informed the engineering department.','E3456','qas|','2018-12-31|','2018-12-31',NULL,NULL,NULL,NULL,NULL,NULL),(11353,'56-099','GKN Aerospace Orangeburg','CLOSEOUT - CHORD, LWR','7609601-2','119A1381-604','NA','PSDL REV -',1,'A000047469','','85677','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','profile width undersized','The cut out program has run with wrong tool.|The pocket number entered for specified tool was wrong.|The program was edited by the operator.','|1.The part  run with the correct tool which is checked by the supervisor.\r<br/>2.The correct tool will be loaded in the pocket as specified in the program.','','CA/PA is satisfied.','','2018-12-24','pe_sez(a)','Madhu Kumar(N)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','pe_sez(a)','no','','|1.Machine was stopped and cross checked for the tool.\r\n2.the correct tool was loaded as per the program.','Z3456','|qas_sez|','2018-12-26|2019-01-07|','2019-01-07',NULL,NULL,NULL,NULL,NULL,NULL),(11354,'56-099','GKN Aerospace Orangeburg','CLOSEOUT - CHORD, LWR','7609601-2','119A1381-604','NA','PSDL REV -',1,'A000047469','','85677','','0000-00-00',NULL,'yes','yes','yes','','','','','','','profile undersize','Dummy|Dummy|Dummy|Dummy','|Dummy','|Dummy','Dummy','','2018-12-24','pe_sez(a)','                Madhu Kumar N','','0000-00-00','DUMMY NC','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','03','','','','','','|Dummy','Z3456','pe_sez|pe_sez|qas_sez|','2018-12-25|2018-12-31|2019-01-18|','2019-01-18',NULL,NULL,NULL,NULL,NULL,NULL),(11355,'51-158','THE BOEING COMPANY','FITTING','709650B6','349T2200-9447','NA','PSDL REV J',1,'BOEING 001AA','','84731','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dia 3.2 hole shifted 1.0mm.','when running the drilling program. part shifted from butting face. |Improper cleaning at the butting area','|The butting area was cleaned and the offset was taken again and further ensured that the part is butted properly and rigidly','|stopper was given in the fixture for location so that the part has to lock and butt rigidly during running the machine','Next part WO #84732 qty 2 nos machined and founnd ALL THE HOLE CO-ORDINATE was meeting the drawing requried position','','2018-12-25','op_sez(s)','Nagaraju P K ,HariPrasad ,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','1','no','a51nx-03','op_sez(s)','no','','|1.machine was stopped \r\n2.The part was identified and NCR raised\r\n3.The butting area was cleaned and the offset was taken again','Z3456','qas_sez|','2019-01-22|','2019-01-22',NULL,NULL,NULL,NULL,NULL,NULL),(11356,'46-039','Mahindra Aerostructures Pvt.Ltd','BRACKET UPP','7146601','V5754048020000','NA','A00,BOM ISS A00,ECN SG109881ST01JA35',3,'3101293478','','82168','','0000-00-00',NULL,'no','no','no','yes','no','no','no','yes','no','Material wrong cutting and part per billet was two initially which was not possible during FAI proving.','One number is rejected as the material was having a quantity per billet at 2 numbers but this material was used for producing one number. The proving of the parts was planned for 2 parts, and this was not executed in the first trials. The process done for 2 parts per billet needed a fixture which was not available at the time of parts being loaded to machine. Unavailability of fixture for cross cutting.','||Fixture is manufactured for the cross cutting and its handed over to stores department.','||Fixture is manufactured for the cross cutting and its handed over to stores department.','capa found satisfactory','','2018-12-26','CAD(sez)','CAD(sez)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','00','no','Misc','pe_sez(a)','yes','','','Z3456','qas_sez|','2019-02-14|','2019-02-14',NULL,NULL,NULL,NULL,NULL,NULL),(11357,'46-040','Mahindra Aerostructures Pvt.Ltd','DIAPHRAGM','1797601','V5754047820000','NA','A00,BOM ISS A00,ECN SG109881ST01JA36',2,'3101293478','','82170','','0000-00-00',NULL,'no','no','no','yes','no','no','no','yes','no','Material wrong cutting ','One number is rejected as the material was having a quantity per billet at 2 numbers but this material was used for producing one number.|The proving of the parts was planned for 2 parts, and this was not executed in the first trials.|The process done for 2 parts per billet needed a fixture which was not available at the time of parts being loaded to machine.|Unavailability of fixture for cross cutting.','|Fixture is manufactured for the cross cutting and its handed over to stores department.','|The fixtures, data and materials required are to be kept ready before loading the parts on to the machine or before starting the process.','CA/PA found ok.','','2018-12-26','CAD(sez)','CAD(sez)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','00','no','Misc','pe_sez(a)','yes','','|The next parts were proved with a process of one part per billet. The parts were accepted and dispatched for the required schedule.','Z3456','cam|qas_sez|','2018-12-26|2019-01-16|','2019-01-16',NULL,NULL,NULL,NULL,NULL,NULL),(11358,'46-041','Mahindra Aerostructures Pvt.Ltd','DIAPHRAGM','1797601','V5754047820100','NA','A00,BOM ISS A00,ECN SG109881ST01JA36',2,'3101293478','','82181','','0000-00-00',NULL,'no','no','no','yes','no','no','no','yes','no','Material wrong cutting','The quantity per billet is 2 parts thus 2 Numbers are rejected because of billet cross cutting|The billet cutting was done in a wrong direction. Cross cutting was done in a wrong direction.|There was no fixture given for the cross cutting to the stores department.|Unavailability of fixture for cross cutting.\r\n','|Fixture is manufactured for the cross cutting and its handed over to stores department.','|The fixtures, data and materials required are to be kept ready before loading the parts on to the machine or before starting the process.','CA/PA found ok.','','2018-12-26','CAD(sez)','CAD(sez)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','00','no','Misc','pe_sez(a)','yes','','|The next parts were proved with a process of one part per billet. The parts were accepted and dispatched for the required schedule.','Z3456','cam|qas_sez|','2018-12-26|2019-01-16|','2019-01-16',NULL,NULL,NULL,NULL,NULL,NULL),(11359,'46-039','Mahindra Aerostructures Pvt.Ltd','BRACKET UPP','7146601','V5754048020000','NA','A00,BOM ISS A00,ECN SG109881ST01JA35',3,'3101293478','','82168','','0000-00-00',NULL,'no','no','no','yes','no','no','no','yes','no','Material wrong cutting and part per billet was two initially which was not possible during FAI proving.','1. The quantity per billet is 2 parts thus 2 Numbers are rejected because of billet cross cutting\r\n2. One number is rejected as the material was having a quantity per billet at 2 numbers but this material was used for producing one number.|1. The billet cutting was done in a wrong direction. Cross cutting was done in a wrong orientation.\r\n2. The proving of the parts was planned for 2 parts, and this was not executed in the first trials.|1. There was no fixture given for the cross cutting to the stores department.\r\n2. The process done for 2 parts per billet needed a fixture which was not available at the time of parts being loaded to machine. |Unavailability of fixture for cross cutting. ','Fixture is manufactured for the cross cutting and needs to be handed over to stores department','The fixtures, data and materials required are to be kept ready before loading the parts on to the machine or before starting the process.','CA PA Found ok.','','2018-12-26','CAD(sez)','CAD(sez)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','00','no','Misc','pe_sez(a)','yes','','The next parts were proved with a process of one part per billet. The parts were accepted and dispatched for the required schedule.','E3456','qas|','2019-01-06|','2019-01-06',NULL,NULL,NULL,NULL,NULL,NULL),(11360,'35-672','Saab AB','SHAFT LEVER ','701946 1D1','D5227346221900','NA','PART ISSUE D',1,'OWED-LTA-001','','85827','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','dia 15.68 od under size (-0.04)','1) OD under size because of run out on the part.|2) Eccentricity between the M/C spindle and the Tail Stock was not equal. |3) After M/C maintenance the Eccentricity of the spindle and the tail stock was not checked.|4) Possibility of variation in the eccentricity was not taken into account during the M/C maintenance.','|Informed the maintenance team about the issue and carried out re-maintenance on the machine to correct the eccentricity of the machine.','|During every preventive maintenance time the eccentricity of the M/C spindle and the Tail stock will be checked and adjusted.','CA PA found ok.','','2018-12-26','Sandhesh D(S)','Veerabadraswamy(TB)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','05','no','Misc','Sathish(G)','no','','|Immediately stopped the machine and informed the supervisor, checked the eccentricity of the machine and defective.','E3456','qas|','2019-04-08|','2019-04-08',NULL,NULL,NULL,NULL,NULL,NULL),(11361,'51-158','THE BOEING COMPANY','FITTING','709650B6','349T2200-9447','NA','PSDL REV J',1,'BOEING 001AA','','84730','','0000-00-00',NULL,'yes','no','no','no','no','yes','no','yes','no','OD UNDERSIZED, Ø OD 12.4889 INCH IS MEASURED 12.4729 INCH\r\n','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. ','|1.complete program for the part rechecked by the engineering team\r<br/>2.Tool Offset was taken once again and started production','|RADIUS PROGRAMS AND DE BUR PROGRAMS WILL BE INCLUDED FOR ALL APPLICABLE PARTS DURING THE FAIR PART PROVING TIME ITSELF TO AVOID SUCH REJECTIONS. ','NEXT PART PRODUCED AND DIAMETER INSPECTED ,DIA FOUND WITH IN THE TOLERANCE AS PER THE DRAWING REQUIREMENTS.','','2018-12-31','pe_sez(a)','Thaveni D M ,Nagaraju P K ,Maruthi ,HariPrasad ,Dinakar K ,','','0000-00-00','OD UNDERSIZED, Ø OD 12.4889 INCH IS MEASURED 12.4729 INCH\r\n','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','200MY-02','qas_sez(a)','no','','|1.machine was stopped\r\n2.The parts was identified and internally NC was raised\r\n3.all the were recalled and checked for the tool offset','Z3456','qas_sez|','2019-01-24|','2019-01-24',NULL,NULL,NULL,NULL,NULL,NULL),(11362,'56-100','GKN Aerospace Orangeburg','CLOSEOUT RIB - AFT, UPR','1682402','119A1383-603','NA','PSDL REV -',1,'A000047470','','85741','','0000-00-00',NULL,'no','no','yes','no','no','no','yes','yes','no','Refer NC NO:10744','Refer NC NO:10744','|Refer NC NO:10744','|Refer NC NO:10744','Refer NC NO:10744','','2018-12-31','CAD(sez)','CAD(sez)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','pe_sez(a)','no','','|Refer NC NO:10744','Z3456','qas_sez|','2019-01-16|','2019-01-16',NULL,NULL,NULL,NULL,NULL,NULL),(11363,'47-025B','GKN Aerospace Filton','FITTING AFT OUTB','564564A3','F57550073200','NA','C01, MIS ISSUE F, F575ABSMCD Rev 39',1,'GKN GS-034 KIT -2018','','85819','','0000-00-00',NULL,'yes','yes','yes','','','','','','','base ticknes minimam -0.12','Improper butting of part to fixture.|Operator could not check the gap b/w part and fixture.|Fixture is designed such operator have no option to check the gap visually or feeler gauge. ','|1)S slot has to be introduced in fixture to run parts.\r<br/>2)With risk involved batch has been completed by production team','|Re- Engineering has to be carried out.','CA PA found ok.','','2019-01-01','Subramanya L(Naik)','        CHETANA K','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','','','03','no','','','','','|Stop the M/C and checked the previously runned parts.','E3456','pe|pe|qas|','2019-01-01|2019-01-01|2019-04-23|','2019-04-23',NULL,NULL,NULL,NULL,NULL,NULL),(11364,'18-584A','Magellan Aerospace Wrexham','FITTING FWD SPAR','504280C','L575 51870 201','','A00',1,'162904','','85325','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','THICKNESS -0.06 UNDER SIZE.','Part not properly butted to fixture.|Due to burr on fixture.|Operator has not effectively cleaned the fixture.','|Operator has been trained to double check for burr or any other particles on the fixture.','|Operator has been trained to double check for burr or any other particles on the fixture.','Training record verified and operator effectiveness will be monitored.','','2019-01-02','Subramanya L(Naik)','Yogesha K,CHETANA K,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','MakinoF5-4','Narasimha Murthy(R)','no','','|Inspected the other parts, found OK.','E3456','pe|qas|','2019-01-04|2019-01-31|','2019-01-31',NULL,NULL,NULL,NULL,NULL,NULL),(11365,'18-437B','Magellan Aerospace(Blackpool) Limited','MANIFOLD','30564 6277','PI201274625','NA','NIL',4,'Bpp-529619 amed-2','','81157','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Out of tolerance surface finishes due to excessive frazing.[Ref previous reject reports 5091,5092,5093.]','Why-1:a) The final finished part\'s surface mismatch cleared via fitting rework.\r\nb) Surface finish was ensured via surface comparator.\r\n|Why-2: a) During milling operation surface mismatches occurred due to tool overhanging.\r\nb) The tool offset was adjusted manually.\r\n|Why-3: The tool offset was adjusted manually.|Why-4: The method followed for adjusting tool offset was not robust.','|Process: Tool offset adjustment will be done in machine (Zoller Machine).\r<br/>Quality: Using Surface Roughness Tester to ensure Surface roughness value.\r<br/>','|Process: Tool offset adjustment will be done in machine (Zoller Machine).\r<br/>Quality: Using Surface Roughness Tester to ensure Surface roughness value.\r<br/>','CA PA found ok.\r\n','C69604','2019-01-03','Nandishkumar(D.K.)','Ranjith(G)','RDN-5099','2019-01-02','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Manufacture Only','','Cust End','yes','Misc','Nandishkumar(D.K.)','no','','|The parts in FG (Total quantity of 29 no’s) are ensured that surface finish value attained as per drawing requirement.','E3456','qas|','2019-01-06|','2019-01-06',NULL,NULL,NULL,NULL,NULL,NULL),(11366,'18-437B','Magellan Aerospace(Blackpool) Limited','MANIFOLD','30564 6277','PI201274625','NA','NIL',11,'Bpp-529619 amed-2','','80189','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Out of tolerance surface finishes due to excessive frazing.','Why-1:a) The final finished part\'s surface mismatch cleared via fitting rework.\r\nb) Surface finish was ensured via surface comparator.\r\n|Why-2: a) During milling operation surface mismatches occurred due to tool overhanging.\r\nb) The tool offset was adjusted manually.\r\n|Why-3: The tool offset was adjusted manually.|Why-4: The method followed for adjusting tool offset was not robust.','|Process: Tool offset adjustment will be done in machine (Zoller Machine).\r<br/>Quality: Using Surface Roughness Tester to ensure Surface roughness value.\r<br/>','|Process: Tool offset adjustment will be done in machine (Zoller Machine).\r<br/>Quality: Using Surface Roughness Tester to ensure Surface roughness value.\r<br/>','CA PA found ok.','C69603','2019-01-03','Nandishkumar(D.K.)','Ranjith(G)','RDN-5100','2019-01-02','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Manufacture Only','','Cust End','yes','Misc','Nandishkumar(D.K.)','no','','|The parts in FG (Total quantity of 29 no’s) are ensured that surface finish value attained as per drawing requirement.','E3456','qas|','2019-01-06|','2019-01-06',NULL,NULL,NULL,NULL,NULL,NULL),(11367,'18-411A','Magellan Aerospace Wrexham','PLUNGER','771908','D321 40205 200','','H01',4,'175174','','81325','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','1)ID THREAD NO GO ANSWER 4-NOS.                  \r\n','1. ID Thread high point on higher side Thread gauge no go answering.\r\n |2. Thread insert was replaced with new one.|3. Thread insert was broken.|4. Due to low insert life, insert broken.','|Insert life has been reduced and well be monitored.','|Different grade of insert is under trial.','next batches trial found ok.','','2019-01-03','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','07','no','Misc','Raghavendra Rao(R)','no','','|previous parts were inspected and found OK, further parts will be monitored.','E3456','pe|qas|','2019-01-04|2019-01-24|','2019-01-24',NULL,NULL,NULL,NULL,NULL,NULL),(11368,'35-230A','Saab AB','HINGE BRACKET 3 ','5880601 2','D576 50006 205','','D00',1,'1600223433/Forecast ','','84356','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Bore Position Shift','X ,Y VALUE WRONGLY ENTERED IN THE WORK OFFSET.\r\n\r\n|THE OPERATOR HAS TYPED THE WRONG VALUE\r\n\r\n','|THE WORK OFFSET WAS CROSS CHECKED AND FOUND THE ENTERED VALUE WAS WRONG AND FROM THE NEXT PART THE WORK OFFSET WAS ENTERED CORRECTLY. ','|FOR THE FUTURE PRODUCTION BATCH NEW WORK OFFSET WILL BE TAKEN WHERE THERE WONT BE ANY OPTION FOR THE OPERATOR ENTERING OF THE OFFSET VALUE.','CA/PA satisfied','','2019-01-04','pe_sez(a)','pe_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','05','no','Misc','pe_sez(a)','no','','','Z3456','qas_sez|qas_sez|','2019-01-11|2019-01-18|','2019-01-18',NULL,NULL,NULL,NULL,NULL,NULL),(11369,'35-158','Saab AB','FLCD_DS_SUPPORT_DEFLECT-S','58561-2RB1','423Z6187-7','','---',1,'1600197455','','85903','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Thickness undersized','Second setup ruining time base thickness - side because part bend, ','|1.The cutting parameters was regenerated.\r<br/>2.Operators were instructed to monitor the Life of the insert after the cutting parameters was regenerated','|1.provide sufficient clamp to butting the part properly . \r<br/>2.Instruction given to the operator to cross check if any gap presence after clamping by using the feeler gauge.','Next part produced and found that thickness was well with in the required tolerance ','','2019-01-04','pe_sez(a)','pe_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','pe_sez(a)','no','','|1.the part was checked for the bend and separated.\r\n2.Informed to engineering department regarding the bend','Z3456','qas_sez|','2019-01-22|','2019-01-22',NULL,NULL,NULL,NULL,NULL,NULL),(11370,'35A-354A','Saab AB','LIFT PIN HOUSING FWD','','423Z1124-6-52','','1',1,'1600204275','','A12055','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Bore oversized.','REFER NC NO:10806.','|REFER NC NO:10806.','|REFER NC NO:10806.','REFER NC NO:10806.','','2019-01-04','pe_sez(a)','pe_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Assembly','','FI','no','Misc','qas_sez(a)','no','L05627|BACB28AP20Z253','|REFER NC NO:10806.','Z3456','qas_sez|','2019-01-16|','2019-01-16',NULL,NULL,NULL,NULL,NULL,NULL),(11371,'35A-354A','Saab AB','LIFT PIN HOUSING FWD','','423Z1124-6-52','','1',2,'787 Forecast','','A11710','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','BORE OVALITY SO BORE OVER SIZE','REFER NC NO:10806.','|REFER NC NO:10806.','|REFER NC NO:10806.','REFER NC NO:10806.','','2019-01-04','pe_sez(a)','pe_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Assembly','','FI','no','Misc','qas_sez(a)','no','L05627|BACB28AP20Z253','|REFER NC NO:10806.','Z3456','qas_sez|','2019-01-16|','2019-01-16',NULL,NULL,NULL,NULL,NULL,NULL),(11372,'35-597','Saab AB','CORNER','548052B','D5227338620200','NA','PART ISSUE B',1,'PA1687 LTA-1','','82625','','0000-00-00',NULL,'yes','no','yes','no','yes','no','no','no','no','Profile Dig of .6mm (AT SEZ MAZZAK I-700 MACHINE','NC program Boarder rating reading problem|Machine capacity memory problem','|Mazak Maintenance team came and re-installed the MAZAKTROL software.','|Mazak Maintenance team came and re-installed the MAZAKTROL software.','CAPA FOUND OK','','2019-01-04','Ravi nayak()','Ravi nayak()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','05','no','Misc','Ravi nayak()','no','','|Immediately machine stop and informed to the machine maintenance team. ','A3456','pe|qas_aero|','2019-01-17|2019-07-01|','2019-07-01',NULL,NULL,NULL,NULL,NULL,NULL),(11373,'51-095','THE BOEING COMPANY','SCU STANCHION FITTING','476153','476Z2941-7','NA','NIL',1,'BOEING 001N','','85393','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','WALL HEIGHT UNDER SIZE . MINIMUM VALUE IS 25.14MM . MEASURED VALUE IS 24.48MM.','1.Running time chips present in holder so  |2.while tool changing time chips placed on in between spindle and holder so tool runout occure,|3.In the part wall finishing time wall -ve side occure ','|1.Once again the tool offset was taken for all the tools pertaining to the parts and continued the production','|when ever there is a new setting ,instruction was given to the operator to unload all the tools ,check for the cutting edge,and any FOD presence in the holder and then again reload all the tools to the machine.','Next Part Machined and total height found with in tolerance ','','2019-01-05','pe_sez(a)','Thaveni D M ,Ravi Kumar G.B,Nagaraju P K ,Dhanush J.K,','','0000-00-00','WALL HEIGHT UNDER SIZE . MINIMUM VALUE IS 25.14MM . MEASURED VALUE IS 24.48MM.','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','a51nx-05','qas_sez(a)','no','','|1.All the tools were recalled and unclamped \r\n2.tools holder were cleaned and re clamped the tool.\r\n','Z3456','qas_sez|','2019-01-22|','2019-01-22',NULL,NULL,NULL,NULL,NULL,NULL),(11374,'51-095','THE BOEING COMPANY','SCU STANCHION FITTING','BA74630','476Z2941-7','NA','NIL',1,'BOEING 001N','','85382','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','WALL HEIGHT UNDER SIZE. MINIMUM VALUE IS 25.146MM. MEASURED VALUE IS 24.90','1.Running time chips present in holder so  |2.while tool changing time chips placed on in between spindle and holder so tool runout occure,|3.In the part wall finishing time wall -ve side occure ','|1.Once again the tool offset was taken for all the tools pertaining to the parts and continued the production','|when ever there is a new setting ,instruction was given to the operator to unload all the tools ,check for the cutting edge,and any FOD presence in the holder and then again reload all the tools to the machine.','Next Part Machined and total height found with in tolerance ','','2019-01-05','pe_sez(a)','Vijay Kumar H.J,Ravi Kumar G.B,','','0000-00-00','WALL HEIGHT UNDER SIZE. MINIMUM VALUE IS 25.146MM. MEASURED VALUE IS 24.90','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','a51nx-02','qas_sez(a)','no','','|1.All the tools were recalled and unclamped \r\n2.tools holder were cleaned and re clamped the tool.\r\n','Z3456','qas_sez|','2019-01-22|','2019-01-22',NULL,NULL,NULL,NULL,NULL,NULL),(11375,'47-173','GKN Aerospace Filton','BRACKET','520635','F5755098220002','NA','PART ISSUE F01',1,'1210042824-2','','84589','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Bore diameter over size','REFER NC NO:10806.','|REFER NC NO:10806.','|REFER NC NO:10806.','REFER NC NO:10806.','','2019-01-06','pe_sez(a)','        Somashekar ','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','03','','','','','','|REFER NC NO:10806.','Z3456','pe_sez|qas_sez|','2019-01-06|2019-01-16|','2019-01-16',NULL,NULL,NULL,NULL,NULL,NULL),(11376,'35-270','Saab AB','STOP INSERT','851172-11','424Z6413-1','','--A',1,'Forecast po for B787','','85732','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Profile width under sized','During milling process part was shifted from the located area|The located bold was broken due to that part was shifted |Due to heavy tight on the bolt','|During part loading process torque wrench is using to tighten the bolts','|During part loading process torque wrench is using to tighten the bolts','','','2019-01-07','pe_sez(a)','Pradeep(B.D)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','pe_sez(a)','no','','|The broken bolt was removed and new bolt was used and tightened properly remaining parts found ok','Z3456','pe|qas|','2019-05-17|2019-05-17|','2019-05-17',NULL,NULL,NULL,NULL,NULL,NULL),(11377,'46-022A','Mahindra Aerostructures Pvt.Ltd','ANGLE','525129A3','F574-51232-214','NA','G01',4,'MAPL Forecast 2018-1','','85987','','0000-00-00',NULL,'yes','yes','yes','','','','','','','THICKNESS UNDER SIZE BY -0.5','Z-axes tool offset wear out.|During tool changing process chips locking in tool holder.|During roughing operation chips on ATC arm & tools magazine.','|after roughing operation add massage \"CLEAN THE ATC ARM\" & add  M00 in program for clean the ATC arm.','|after roughing operation add massage \"CLEAN THE ATC ARM\" & add  M00 in program for clean the ATC arm.','Next batch parts found OK.','','2019-01-07','Subramanya L(Naik)','        Sundar D.K.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','03','','','','','','|Stop the machine,clean all tool holders by tissue paper & cross check the offset.','E3456','pe||qas|','2019-01-10|2019-01-10|2019-01-16|','2019-01-16',NULL,NULL,NULL,NULL,NULL,NULL),(11378,'18-436B','Magellan Aerospace(Blackpool) Limited','MANIFOLD ','C0201787385','PI201274624','NA','NIL',12,'Bpp-529619 amed-2','','77365','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Out of tolerance surface finishes due to excessive frazing','1) The final finished part\'s surface mismatch cleared via fitting rework.\r\n2) Surface finish was ensured via surface comparative.|1) During milling operation surface mismatches occurred due to tool overhanging.\r\n2) Selection of instrument is wrong|1) The tool offset was adjusted manually.\r\n2) Selection of instrument is wrong to measure the surface roughness|1) The method followed for adjusting tool offset was not robust.','|Process: Tool offset adjustment will be done in machine(Zoller Machine).\r<br/>Quality: Using Surface Roughness Tester to ensure Surface roughness value.','|Process: Tool offset adjustment will be done in machine(Zoller Machine).\r<br/>Quality: Using Surface Roughness Tester to ensure Surface roughness value','Next batches verified and found ok.','C69521','2019-01-10','Nandishkumar(D.K.)','Ranjith(G)','RDN-5117','2019-01-10','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Manufacture Only','','Cust End','yes','Misc','Nandishkumar(D.K.)','no','','|The parts in FG (Total quantity of 29 nos) are ensured that surface finish value attained as per drawing requirement','E3456','qas|','2019-01-30|','2019-01-30',NULL,NULL,NULL,NULL,NULL,NULL),(11379,'18-075A','Magellan Aerospace Wrexham','ADAPTOR','M037890/27097','D282 50044 200PF','','A',1,'175162','','84010','','0000-00-00',NULL,'yes','no','yes','no','yes','no','no','no','no','Running time power trip so tool got dig on the wall.','while running the machine POWER TRIP , and tool digged on the part ','|1.SUPERVISOR ENSURED PROPER FUNCTIONING OF MACHINE AFTER THE RECOVER FORM POWER FAILURE.\r<br/>2.TOOL OFFSET WAS TAKEN ONCE AGAIN.','|MAINTENANCE TEAM REPLACED THE UPS EARTHING UNIT.\r<br/>THE ALARM BUSSER TO BE CHECK DAILY AND MAINTENANCE TO BE CARRY OUT EVERY WEEK','CAPA FOUND SATISFACTORY ','','2019-01-10','pe_sez(a)','Manu(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','03','no','Misc','pe_sez(a)','no','','|The tool was recalled and checked for the cutting edge.\r\n','Z3456','qas_sez|','2019-01-22|','2019-01-22',NULL,NULL,NULL,NULL,NULL,NULL),(11380,'44-007A','Saab AB','FRAME INT 2','476545 A','E5347562720001','NA','PART ISSUE B',1,'AAI-DP-LTA-31SS','','85460','','0000-00-00',NULL,'yes','yes','yes','','','','','','','44-007a running time program block no double. due to VIRUS problem.so part deg.','1.part running time block doubled due to virus problem |2.Check the drive virus found and remove the virus ','|1.Every time part running time check the program blocks and run the program ,','|1.scan the drive and transfer the program while transferring program .\r<br/>\r<br/>2.Anti virus installed to program transfer file ','Anti virus installation verified and founds ok. ','','2019-01-11','Gurukiran S(M)','                                Basavaraja S. Jr.','','0000-00-00','Part dig observed on wall','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','07','','','','','','|stop the machine and check the all program blocks ','E3456','pe|pe|pe|pe|qas|','2019-03-09|2019-03-12|2019-03-12|2019-03-12|2019-03-30|','2019-03-30',NULL,NULL,NULL,NULL,NULL,NULL),(11381,'56-048','GKN Aerospace Orangeburg','TIP CAP','549723','119A1370-604','NA','PSDL REV -',1,'A000047470','','85663','','0000-00-00',NULL,'yes','yes','yes','','','','','','','dia 8 chamfer tool wrong offset entered, chamfer (csk) dia oversize part will be rejected','THE TOOL OFFSET VALUE ENTERED WAS WRONG.\r\n','|THE OPERATOR HAS TO GIVE THE PROPER INSTRUCTIONS BEFORE RELIEVING FROM THE SHIFT TO THE NEXT SHIFT OPERATOR.\r<br/>THE OPERATOR HAS TO CROSS VERIFY THE INPUTS GIVEN BEFORE RUNNING THE MACHINE.','|CHECKLIST NEED TO BE PREPARED AND TO BE FILLED BY EVERY OPERATOR BEFORE RELIEVING FROM THE SHIFT SAYING THAT ALL THE INSTRUCTIONS HAVE BEEN PASSED TO THE NEXT SHIFT OPERATOR AND WHICH SHOULD BE VERIFIED BY THE NEXT SHIFT INCHARGE.','Next part inspected and found all the parameters was with in the requriments.','','2019-01-12','pe_sez(a)','        Raghu B','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','03','','','','','','|TOOL OFFSET WAS CORRECTED AND ALL THE PARTS PRODUCED FOUND OK','Z3456','pe_sez|qas_sez|qas_sez|','2019-01-23|2019-02-13|2019-02-20|','2019-02-20',NULL,NULL,NULL,NULL,NULL,NULL),(11382,'51A-086','THE BOEING COMPANY','KICK LINK ASSY','','251W3122-3','','PSDL REV -',1,'BOEING 001M','','A21795','','0000-00-00',NULL,'no','yes','yes','no','no','no','yes','no','no',' butting supporting block not given while bush pressing ','Due to supporting block was not provided while bush pressing.','|One more butting block was provided while bush pressing.','|One more butting block was provided while bush pressing.','CA/PA satisfied.','','2019-01-13','Ramesh(D)','Nithin(S)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Assembly','','04','no','Misc','Phaniraj(G)','no','M03632|251W3135-2','|One more butting block was provided while bush pressing.','E3456','assembly.cim|','2019-01-21|','2019-01-21',NULL,NULL,NULL,NULL,NULL,NULL),(11383,'51A-086','','','','','','',0,'','','','','0000-00-00',NULL,'no','no','no','no','no','no','no','no','no','','','','','','','2019-01-13','select','','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Cancelled','no','no','no','','','','no','','select','no','','','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11384,'35-305A','Saab AB','RIB INTER 2','0448501 1','F575 54796 200 00','','SCH-ISSUE B, PART ISSUE A',1,'A330 NEO FORECAST-20','','73578','','0000-00-00',NULL,'yes','yes','yes','','','','','','','tool dig at finishing wall.','1) 16R2 base finish tool tamped on the wall and caused the dig mark.|2) Program was called from the beginning as the operator pressed the cycle start immediately after pressing the reset button.|3) During the cycle running time the operator has provided the single block in between the cycle to correct the wear in order to avoid the machine mismatch on the base of the part during which the operator provided 20 micron wear offset on the positive side and then instead of pressing the cycle start operator pressed the restart button.|3) Due to regular practice of pressing the restart button during the first off part cycle start operator followed the same during the intermediate of the cycle.','|Training given to the operator on the tool wear and how to start the cycle when the machine was stopped intermediate to the program.','|1) List of manual errors occurred in the machine will be displayed near the machine.\r<br/>2) Z command will be given to all the 3 Axis programs.','CA PA Found ok.','','2019-01-14','Narayanappa(G)','        Sathish Y.R.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','7','','','','','','|Immediately stopped the machine and checked the spindle axis and no deviation was found in B-axis and no error in spindle run-out.','E3456','qas|qas|','2019-01-14|2019-01-16|','2019-01-16',NULL,NULL,NULL,NULL,NULL,NULL),(11385,'35A-687A','Saab AB','LEVER ASSY','','D5227353600500','','PART ISSUE D',3,'OWED-LTA-005','','A20855','','2018-12-11',NULL,'yes','yes','no','no','no','yes','no','no','no','DEEP DENT OBSERVED AFTER TREATMENT','Part damaged during the transit.|Due to insufficient packing material around the edges and because of hard dandling by the transporters the parts got damaged.','|Informed the supplier and the transported about the damage caused and instructed to provide additional care during the packing and transportation of parts.','|Added bubble wrap to the packing method to avoid damages during transit.','Next batches shipped verified and found ok.','','2019-01-14','qas_sez(a)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Assembly','47582','FI','no','Misc','Dharani(Shankar)','no','81079|D5227353620500','|Checked all the other parts received along with the shipment and parts with minor damages were reworked.','Z3456','qas|','2019-05-17|','2019-05-17',NULL,NULL,NULL,NULL,NULL,NULL),(11386,'18-209B','Magellan Aerospace Wrexham','BODY','3165','D321 40204 202','','D, ECN NR29999ST1KM15, NR29999ST2KF65, WQN DFB09775',1,'175173','','81292','','0000-00-00',NULL,'yes','yes','yes','','','','','','','8.3mm thickness 8.1mm measured. ','Part shifted during machining operation.|Part clamping was not tightened.|Chuck movement was tight because of which operator taught that part is fully clamped and continued the production.  ','|Chuck service done , next production continue & parts found ok','|Every preventive maintenance check service will be done.','CAPA found ok.','','2019-01-17','Subramanya L(Naik)','        Subramanya L Naik','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','05','','','','','','|Stop the machine & informed the operator.','E3456','pe|qas|qas|','2019-01-17|2019-02-21|2019-02-21|','2019-02-21',NULL,NULL,NULL,NULL,NULL,NULL),(11387,'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','HOLE DIAMETER 0.3750+0.0006 INCH AND MEASURED VALUE IS 0.3761 INCH','1.While running time tool broken and due to this bore observed oversize .This deviation is due to tool problem,\r\n2.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\r\nfound with acceptable limit to the drawing/specifications. ','','2019-01-18','qas_sez(a)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Assembly','','FI','no','Misc','qas_sez(a)','no','','Machine was stopped 2.All the tools was recalled and checked for the cutting edges and rigidity of the tool ','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11388,'51A-083A','THE BOEING COMPANY','BRACKET ASSY','','332A2930-7','','PSDL REV B',3,'BOEING 001U','','A16149','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','HOLE DIAMETER 0.3750+0.0006 INCH AND MEASURED VALUE IS 0.3761 INCH','1.While running time tool broken and hole diameter observed oversized on part .This deviation is due to tool problem,\r\n2.Cutting parameters was high','1. Tool was changed\r<br/>2.All the tools retaining to the program ,tool offset was reset and new offset taken was taken and further continued production ','1.all the long series cutter to be checked internally and also informed to cutter supplier to check and validate the cutters before sending to us.\r<br/>2.We are on trails of WIDIA make long end mill tools and cutters with new tool configuration to eliminate above deviations. ','By usage of the new tool with new configuration the CA/PA was satisfied and next produced parts was\r\nfound with acceptable limit to the drawing/specifications. ','','2019-01-18','qas_sez(a)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Assembly','','FI','no','Misc','qas_sez(a)','no','','1.Machine was stopped 2.All the tools was recalled and checked for the cutting edges and rigidity of the tool ','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11389,'51-179','THE BOEING COMPANY','ADAPTER - FLANGED, BULKHE','20228749','272U1230-2','NA','PSDL REV B',1,'BOEING 001Z','','85880','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Program rotation was given wrong in Mazatrola so the profile is undersized by 4mm','1) Program Wrong generated during the FAIR proving time.|2) Direction of rotation generated in the program was wrong.|3) Wrong data entry done by the engineer.|4) Engineer did not reviewed the program along with Drawing before releasing for FAIR proving.','|Changed the program and continued the production and next part found ok.','|New programs will be reviewed with the drawing requirement before releasing to the Production.','Next Batches program verified and found ok.','','2019-01-18','pe_sez(a)','pe_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','pe_sez(a)','no','','|Immediately stopped the machine and informed the Engineering team about the issue.','Z3456','qas|','2019-05-17|','2019-05-17',NULL,NULL,NULL,NULL,NULL,NULL),(11390,'35-485','Saab AB','BRACKET','518610C','D522 73363 201 00','','A',1,'1600192682','','80294','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Position shift up to 0.3mm.','During M/C running time, clamping bolt cut.|Due to over tightening of clamping bolt.','|Clamping bolt grade changed to SS material.','|Clamping bolt grade changed to SS material.','CAPA found ok','','2019-01-18','Dinesh kulal()','Santhosh Kumar.R()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','DN51957','03','no','Misc','Santhosh Kumar.R()','no','','|Informed to Operator not to over tight.\r\ninspected the other bolts and continued production.','A3456','pe|qas|','2019-01-22|2019-02-14|','2019-02-14',NULL,NULL,NULL,NULL,NULL,NULL),(11391,'35-227A','Saab AB','HINGE BRACKET 2','5881601 1','D576 50005 204','','D00',1,'1600223433/Forecast ','','83574','','0000-00-00',NULL,'yes','yes','yes','','','','','','','TOOL DIG MARK ON THE RIB','THE TOOL OFFSET VALUE ENTERED WAS WRONG.|Operator entered wrong value in the Tool Offset.|The offset value taken by the operator was not recorded in the log book and by memory operator inputted some other value','|\r<br/>THE OPERATOR HAS TO GIVE THE PROPER INSTRUCTIONS BEFORE RELIEVING FROM THE SHIFT TO THE NEXT SHIFT OPERATOR.\r<br/>THE OPERATOR HAS TO CROSS VERIFY THE INPUTS GIVEN BEFORE RUNNING THE MACHINE.\r<br/>','|\r<br/>CHECKLIST NEED TO BE PREPARED AND TO BE FILLED BY EVERY OPERATOR BEFORE RELIEVING FROM THE SHIFT SAYING THAT ALL THE INSTRUCTIONS HAVE BEEN PASSED TO THE NEXT SHIFT OPERATOR AND WHICH SHOULD BE VERIFIED BY THE NEXT SHIFT INCHARGE.\r<br/>','Next batch machined and all the parameters was check and found Ok WO:84210 Qty:55 nos','','2019-01-19','pe_sez(a)','        Shivaraj K S','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','01','','','','','','','Z3456','pe_sez|qas_sez|qas_sez|','2019-01-23|2019-02-13|2019-04-12|','2019-04-12',NULL,NULL,NULL,NULL,NULL,NULL),(11392,'47-167','GKN Aerospace Filton','TEE T/E RIB 2','249043B1','F57550130200','NA','PART ISSUE D02',1,'GKN-GS-068 PHASE2- L','','84559','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Tool dig mark found.\r\n\r\nTo match up the dig we run the part after making work offset down and even after that part rejected since the dig affected the total height in second setup Machining.','Tool dig mark found.|While 1st setup Machining part lifted from the fixture.|Part lifted due to improper clamping.','|1.Instructions/Awareness created among  operators about rejection of parts due to part lifted.','|1.MO added to cross check the clamping and proper butting before running the programs.','CAPA FOUND SATISFACTORY.','','2019-01-20','pe_sez(a)','                Madhu Kumar N','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','01','','','','','','|Stopped the Machining and cross checked all the setting values and the same informed to Supervisor.\r\nPrevious parts machined found OK.','Z3456','pe_sez|pe_sez|mahesh_sez|qas_sez|','2019-01-23|2019-01-23|2019-01-23|2019-02-13|','2019-02-13',NULL,NULL,NULL,NULL,NULL,NULL),(11393,'18-090A','Magellan Aerospace(Polska) Sp','BUSH','1670510-3/YT27','PID278 50164 200','','A',31,'104569','','84855','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','OD UNDER SIZE BY -0.01MM TO -0.05MM.','OD under size due to improper wear offset. |During insert change the operator did not properly calculated the wear correction and continued the production with out checking the part.|Due to improper awareness the operator did not ensured the dimension of the part machined after insert change.','|Informed the operator to continue production under senior operator supervision only.','|Informed the operators to carry out insert change and new settings only under the supervision of senior operators.','CA PA found ok.','','2019-01-21','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','03','no','Misc','Ravi(M)','no','','|Immediately stopped the machine and checked the previously running parts and separated the parts that were undersized.','E3456','qas|','2019-04-08|','2019-04-08',NULL,NULL,NULL,NULL,NULL,NULL),(11394,'35-623A','Saab AB','SHAFT 2','532729A','D5227280820000','NA','PART ISSUE A',2,'OWED-LTA-004','','78472','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','1)1 nos part broken....                                           2)1 nos drill broken...','1a)1st part setting time part broken.\r\n2a)center bit broken. |1b)Revolving center offset not done. \r\n2a)M0 code not given. \r\n|1c)offset value not entered in system.\r\n2c)This cause was not happened for that material.   ','|1a)Training given by the operator.\r<br/>2a)Add the M0 code in program.   |1a)Training given by the operator.\r<br/>2a)Add the M0 code in program.   ','|1a)Training given by the operator.\r<br/>2a)Add the M0 code in program.   \r<br/>   |1a)Training given by the operator.\r<br/>2a)Add the M0 code in program.   \r<br/>   ','Training record verified and operator effectiveness will be verified after one month.','','2019-01-21','Dinakar(K)','Sathish(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','07','no','Misc','Sathish(G)','no','','|1a)re-enter the offset value and run the M/C.\r\n2a)Call the M0 Code and run the M/C.|1a)re-enter the offset value and run the M/C.\r\n2a)Call the M0 Code and run the M/C.','E3456','||qas|','2019-01-21|2019-01-21|2019-01-31|','2019-01-31',NULL,NULL,NULL,NULL,NULL,NULL),(11395,'35-601','Saab AB','FRAME','3810601','D5227338520600','NA','PART ISSUE C',1,'OWED-LTA-001','','83943','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','PART RIB TOP DIG MARK,','Power failure|interrupted and restored position was wrong.|XYZ Co-ordinate on the machine display and block select was wrong.','|1. After power failure, always move Z axis to home position first.\r<br/>2. Select the proper program as per process sheet.\r<br/>3. Restart the program from beginning of the interrupted tools or operation sequence.','|1. After power failure, always move Z axis to home position first.\r<br/>2. Restart the program from beginning of the interrupted tools or operation sequence. start with block T** M06.\r<br/>3. Never start the program from middle of operation sequence.','CAPA implementation verified and found ok.','','2019-01-21','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','05','no','Misc','Punith G(S)','no','','|Reset the machine\r\nRestart the program from beginning.','E3456','pe|qas|','2019-01-22|2019-01-28|','2019-01-28',NULL,NULL,NULL,NULL,NULL,NULL),(11396,'35-601','Saab AB','FRAME','3810601','D5227338520600','NA','PART ISSUE C',1,'OWED-LTA-001','','83943','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','PART INSIDE POCKET OBLONG,','Cutting tool broken|Found lot of chips near the machining area.|suspect chip clogging.','|Still under observation\r<br/>Added M0 in program to clean the chips if any and continue the operation.','|Still under observation,\r<br/>No chips found during the operation at M0\r<br/>','CAPA implementation verified and found ok.','','2019-01-21','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','05','no','Misc','Punith G(S)','no','','|cleaned the chips.\r\nReplaced the tool and continued the operation.','E3456','pe|qas|','2019-01-22|2019-01-28|','2019-01-28',NULL,NULL,NULL,NULL,NULL,NULL),(11397,'35-601','Saab AB','FRAME','4215601','D5227338520600','NA','PART ISSUE C',1,'OWED-LTA-001','','83950','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','WALL RIB DIG MARK,','during implementation of new process.|warpage on the part after 1st operation.|improper resting of the part on the fixture due to warpage|More depth od cut along the side wall.','|Stopped the new process\r<br/>Continued production with old process.','|Need further study of operation,\r<br/>need to optimize the depth of cut corresponding to clamping condition.','CAPA implementation verified and found ok.','','2019-01-21','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','05','no','Misc','Punith G(S)','no','','|Stopped the new process\r\nContinued production with old process.','E3456','pe|qas|','2019-01-22|2019-01-28|','2019-01-28',NULL,NULL,NULL,NULL,NULL,NULL),(11398,'35-601','Saab AB','FRAME','4215601','D5227338520600','NA','PART ISSUE C',1,'OWED-LTA-001','','83950','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','BORE (+) SIDE,','Bore diameter was measured beyond the tolerance.\r\n|Due to Run out in the boring tool.|Chips floated and got struck inside between the spindle and the tool holder because of which the tool run out occurred.','|Informed the operator to ensure the tool run out before starting the boring cycle.','|Informed the tooling department to provide rejected or dummy holders to fill them inside the empty pockets in the tool holder magazine.','CA PA found ok.','','2019-01-21','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','05','no','Misc','Punith G(S)','no','','|Immediately stopped the machine and checked the previously completed parts and found ok.','E3456','qas|','2019-04-05|','2019-04-05',NULL,NULL,NULL,NULL,NULL,NULL),(11399,'35-601','Saab AB','FRAME','4215601','D5227338520600','NA','PART ISSUE C',3,'OWED-LTA-001','','83950','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','BASE THICKNESS (-) SIDE,','implimentation of new process|Warpage on the part after first operation|part  not butting on the fixture properly due to warpage on the part.','|Continued with old proven process','|Need to further study the operation to analyze the cause for warpage on the part.','CA PA found ok.','','2019-01-21','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','05','no','Misc','Punith G(S)','no','','|Stopped the new process,','E3456','pe|qas|','2019-01-22|2019-02-14|','2019-02-14',NULL,NULL,NULL,NULL,NULL,NULL),(11400,'56-107','GKN Aerospace Orangeburg','FAIRING SUPPORT - FWD','1217701-1','119A1520-604','NA','PSDL REV A',1,'A000047469','','85688','','0000-00-00',NULL,'yes','no','yes','no','yes','no','no','no','no','Profile mismatches occurred on bottom side of the part','Bottom surface was having mismatches|During milling operation tool tip was damaged due to that improper surface created|Tool overhanging occurred due to that vibration created and tool tip was damaged|Tool length was high which was not meeting the L/D ratio requirement','|During tool loading process message alert was created regarding required length of the tool for that operation','|Tool loading to be carry out as per the L/D ratio requirement','CAPA FOUND OK','','2019-01-21','NataRaj.CV()','Umesh B,Sanjeev S.D,Nataraja C V,NataRaj.CV ,Diwakar R.B.,Chethan Kumar M,Anand ,','','0000-00-00','MISMATCHES','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','3','no','i700-5','NataRaj.CV()','no','','|Correct length tool was loaded and finished parts found ok','Z3456','pe|qas|','2019-05-17|2019-05-17|','2019-05-17',NULL,NULL,NULL,NULL,NULL,NULL),(11401,'35-531A','Saab AB','SHAFT LATCH','B90458','D5227349020200','NA','PART ISSUE C',6,'OWED-LTA-002','','83187','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','OD UNDRE SIZE BY 0.007 MM TO 0.015 MM','TOOL OFFSET WAS TAKEN WRONG IN BETWEEN THE PRODUCTION BATCH. DUE TO INSERT WEAR OUT DURING THE PRODUCTION TOOL INSERT WEAR OUT WAS NOT MONITORING. TOOL MONITORING CHART WAS NOT HANDY. ','|AWARENESS CREATED AND ADVISED THE OPERATOR ON THE CROSS CHECKING OF THE INSERTS OFTENLY FOR THE WEAR OF THE EDGE.','||TOOL MONITORING CHART WILL BE DISPLAYED NEAR THE MACHINE.','CAPA FOUND SATISFACTORY','','2019-01-21','Dinakar K()','Dinakar K()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','10','no','Misc','qas_sez(a)','no','','|1.Machine was stopped\r\n2.All the tools was recalled and checked for the cutting edges and rigitdity of the tool','Z3456','qas_sez|','2019-02-14|','2019-02-14',NULL,NULL,NULL,NULL,NULL,NULL),(11402,'46-038B','Mahindra Aerostructures Pvt.Ltd','STRAP ','M0606B0 27777','D575-40872-201-01','NA','K02, BOM ISS J, ECN NG26090ST1KD02',1,'MAPL Extrusion LTA 2','','86318','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Part dig mark.','While running ball nose cutter, component lifted and dig mark found.','|Clamping position changed, will be closer to the operating area.','|Clamping position changed, will be closer to the operating area.\r<br/>Locating pin position rearranged.','Next batches found ok.','','2019-01-21','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Prashanth Kumar(M)','no','','|Immediately stopped the operation,\r\n','E3456','pe|qas|','2019-01-22|2019-01-24|','2019-01-24',NULL,NULL,NULL,NULL,NULL,NULL),(11403,'35-509A','Saab AB','HINGE FAIRING','530221A2','D5227339020000','NA','PART ISSUE B',1,'OWED-LTA-002','','84141','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Outer profile dig up to 0.5mm.','Part lifted during the profile cut out stage.|Due to very less thickness maintained during the leg cut out stage.|During every production the operator needs to provide .25mm wear offset in order to achieve the proper thickness in the cut out program.|since there is no proper butting of part in the previous design the part gets vibrated and lifted according to the supplied program therefore operator provides .25mm stock in overall base during every production.|`','|Temporary comment included in the program to inform the operators to ensure .25mm wear offset is taken.','|Fixture re-design to be made on or before 15-Feb-19 and Delta FAI to be carried out on or before 28-Feb-19.','CA/PA found acceptable.','','2019-01-22','Dinesh kulal()','Santhosh Kumar.R()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Dinesh kulal()','no','','|Immediately stopped the machine and provided the 0.25mm wear offset and continued the production.','A3456','qas|qas_sez|','2019-01-24|2019-05-15|','2019-05-15',NULL,NULL,NULL,NULL,NULL,NULL),(11404,'35-017','Saab AB','9901503-075','706653B3','D576 50011 200','L167','A',32,'Forecast PO-2018 A32','','81274','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','24 nos Outer profile unclear.\r\n8 nos base thickness minus.','RM cross cutting.|Cutting blade twist.   |Blade teeth wear-out. ','|Informed to operator before loading the parts to check the RM size.\r<br/>','|1)Informed to operator before loading the parts to check the RM size.\r<br/>2)Outer profile marking program added.','CAPA found ok.','','2019-01-22','Dinesh kulal()','Vinod.K(V)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','01','no','Misc','Dinesh kulal()','no','','|1)Cross check the RM size and run the M/C.\r\n2)Informed to store department.\r\n\r\n','A3456','pe|qas|','2019-01-23|2019-02-14|','2019-02-14',NULL,NULL,NULL,NULL,NULL,NULL),(11405,'35-480B','Saab AB','LOCK LEVER','D86939 YQE3','D5227349820000','NA','PART ISSUE C',1,'OWED-LTA-003','','86703','','0000-00-00',NULL,'yes','yes','yes','','','','','','','od 0.06mm -side...','Finishing insert corner wear out.|Insert life not monitoring. |previous batches we are running short qty so insert life was not monitoring.\r\n','|For this batch we have running the bulk qty and monitoring the  insert life in this batch.\r<br/> ','|1)Monitoring the insert life in this batch.\r<br/>2)Add the insert index comment in the program with qty .  ','Insert life monitoring and message displayed in program verified and found ok.','','2019-01-23','Raghavendra Rao(R)','        Devaraj K.C.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','03','','','','','','|Replace the insert and run the M/C.','E3456','|qas|','2019-01-23|2019-01-31|','2019-01-31',NULL,NULL,NULL,NULL,NULL,NULL),(11406,'51-145A','THE BOEING COMPANY','CLEVIS - UPPER, RH THREAD','534-20180618','112A7112-612','NA','PSDL REV B',1,'BOEING 001AA','','86170','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','Total length undersize by 1.5mm','During machining stage the part was shifted 1.5mm from the butting face.\r\n|Heavy depth of cut given at roughing stage with less clamping pressure.|The exact clamping pressure was not known since it was a re engineering part as trailing was carried on depth of cut 1.5mm to 3mm to reduce the cycle time.','|The clamping pressure 18bar was increased to 20bar for a rigid clamping.\r<br/>','|The clamping pressure will be defined in the mps.','as mentioned in the preventive action . calming pressure is defined in the MPS found ok','','2019-01-23','pe_sez(a)','pe_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','pe_sez(a)','no','','|The work and tool offset was rechecked and found ok.\r\nThe clamping pressure was checked and found that the pressure 18bar was was not sufficient to withstand 3mm depth of cut.\r\n','Z3456','qas_sez|qas_sez|','2019-01-28|2019-02-13|','2019-02-13',NULL,NULL,NULL,NULL,NULL,NULL),(11407,'35-600','Saab AB','FRAME','3810601','D5227338520400','NA','PART ISSUE C',1,'OWED-LTA-001','','86043','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','HOLE POSITION SHIFT 0.5MM,','1)Hole position shifted during the running time.|2) Part was not correctly located.|3) Bevel pins were not available in the fixture.|4) operator missed to insert the bevel pins before loading the material after the completion of previous part unloading.','|Informed the operator to verify the presence of bevel pin before loading the next part.','|Informed the operator to verify the presence of bevel pin before loading the next part.','CA PA Found ok','','2019-01-23','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','05','no','Misc','Punith G(S)','no','','|Immediately stopped the machine and loaded the bevel pin in the fixture and continued the production.','E3456','qas|','2019-04-05|','2019-04-05',NULL,NULL,NULL,NULL,NULL,NULL),(11408,'35-600','Saab AB','FRAME','2314601','D5227338520400','NA','PART ISSUE C',2,'OWED-LTA-001','','86039','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','BASE THICKNESS (-)SIDE,','1) Due to excess bend on the part after roughing operation part lifted and resulted in thickness under-size.|2) During the final pass in finishing operation due to residual stress the part is getting lifted up.|3) During aging time between the roughing and the finishing operation the material was not left in free condition (i.e. the materials were loaded one over the other).','|Informed all the operators to leave the part in free condition during the aging process.','|Training provided to all the operators on site to avoid storage of parts one above the other during the aging operation.','CA PA found ok.','','2019-01-23','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','05','no','Misc','Punith G(S)','no','','|immediately stopped the machine and arranged the material so that the parts are left in free condition.','E3456','qas|','2019-01-28|','2019-01-28',NULL,NULL,NULL,NULL,NULL,NULL),(11409,'51-146','THE BOEING COMPANY','REAR SPAR COVER','8-28-06662-1/29515','312Z3112-501','NA','NIL',2,'BOEING 001X','','83588','','0000-00-00',NULL,'yes','no','no','no','no','yes','no','yes','no','Bend observed in Part','Bending observed on part\r\n|Raw material sheet was having bend, which was cutting into a billets those are having bending|Due to that final finished part also having bend','|From raw material itself billets purchased and ensuring no bends','|From raw material itself billets purchased and ensuring no bends','CAPA FOUND OK','','2019-01-24','pe_sez(a)','Shivaraj K S,Rajesha A.R,Maruthi  D R ,Kiran Kumar M,Kiran KM,Chethan Kumar M,Anand ,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','DN51699','FI','no','PS105-02','qas_sez(a)','no','','|WIP Raw material and parts found ok','Z3456','pe_sez|pe|qas|','2019-01-25|2019-05-17|2019-05-17|','2019-05-17',NULL,NULL,NULL,NULL,NULL,NULL),(11410,'35-480B','Saab AB','LOCK LEVER','D86939 YQE3','D5227349820000','NA','PART ISSUE C',1,'OWED-LTA-003','','86703','','0000-00-00',NULL,'yes','yes','yes','','','','','','','RUNNING TIME 8MM DRILL CROSS..','1) Due to improper butting of the part during drilling operation tapper occurred in the hole.|2) Burr was not removed from the previous operation and the operator did not ensured the removal of the burr because he taught that there will be no error as there is a clearance of 2mm but the burr thickness was more than the clearance. ','|Instructed all the operators to remove the burr prior to any operation irrespective of the process.','|Jaws relief will be increased to 7MM and will be dedicated to the same CRN & 35-481 to avoid the similar incidence.','Jaws boring done immediately, verified the same and found ok.','','2019-01-24','Ravi(M)','        Sudhakar C.M','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','07','','','','','','|Immediately stopped the machine and checked all the completed part and found ok.','E3456','pe|qas|','2019-01-25|2019-01-25|','2019-01-25',NULL,NULL,NULL,NULL,NULL,NULL),(11411,'35A-240A','Saab AB','R/H KIT FOR ARD HINGE / J','','9901503-994','','Exhibit-B',1,'1600223433/Forecast ','','K18119','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','yes','LH PART MIX UP WITH RH KIT','1) LH Part was placed inside the RH kit box.|2) Both the Kits LH & RH kit were placed one after the other due to which the part got mixed up.|3) Initially the LH and RK kits were placed side by side but in order to make space for movement the RH kit box was moved towards the LH box without awareness.','|Informed all the inspectors to check the parts with template(jig) before packing to dispatch.','|RH kit will be taken for assembly only after completely packing the LH Kit.','','C68670','2019-01-25','qas_sez(a)','qas_sez(a)','GLB404704','2018-12-12','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUCTMER END','yes','Misc','qas_sez(a)','no','','|Immediately checked all the Kits lined up for dispatch and found ok.','Z3456','qas|','2019-02-16|','2019-02-16',NULL,NULL,NULL,NULL,NULL,NULL),(11412,'35A-474A','Saab AB','FRAME ASSY','','D5227338400000','','B',6,'OWED-LTA-001','','A15877','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','PARTS BEND SO FLATNESS OUT TOLERANCE','1) Bend occurred on the part during roughing operation and was not removed in- between operations. |2) Due low thickness finish from high thickness RM the machining strategy caused the material to deform and no intermediate correction was given. |3) Intermediate correction for the bend removal and aging was not considered during the processing of these pars.|4) usually aging and intermediate distortion correction are done for the parts longer than 1m length.','|All the semi-finished parts were left for aging and intermediate distortion correction process was included.','|MPS amended to include the intermediate aging and intermediate distortion correction process after the roughing operation.','Next batched produced according to the revised process and the delta FAI was  found ok.','C66143','2019-01-25','qas_sez(a)','qas_sez(a)','D615205','2018-12-21','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUCTMER END','yes','Misc','qas_sez(a)','no','','|Immediately collected all the parts from customer and stopped the production line and checked the machining completed parts and separated the deformed pats.','Z3456','qas|','2019-04-17|','2019-04-17',NULL,NULL,NULL,NULL,NULL,NULL),(11413,'35-182B','Saab AB','EDGE HOUSING','203993B1','423Z1121-5-02','','--B',5,'Forecast po for B787','','71414','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','yes','PAINT CHIP OUT','Paint Chipped off at edges during transit due to improper packing.','|Rework NC raised for the returned material and handed the parts to Assembly department and carried out the rework process.','|Additional bubble wrap will be included to the packing method to avoid the chip offf\'s during transit.','Next shipments verified and found ok.','C65319','2019-01-25','qas_sez(a)','qas_sez(a)','GLB390336','2018-12-07','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','DN40644','CUCTMER END','yes','Misc','qas_sez(a)','no','','|Checked all the parts in FG and requested the customer to return the affected parts back to CIM.','Z3456','qas|','2019-04-11|','2019-04-11',NULL,NULL,NULL,NULL,NULL,NULL),(11414,'35-183B','Saab AB','EDGE HOUSING','681991','423Z1121-6-02','','--B',1,'Forecast po for B787','','72358','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','yes','SCRATCH MARK OBSERVED IN BORE.','Scratch like marks visible inside the bore because of the jigging method followed by the suppplier.','|Reworked the parts in CIM as per CIM rework procedure and returned them back to SAAB.','|Informed the supplier to revise the jigging method to avoid the jigging impression on the part.','Next batch verified at CIM and found ok.','C68655','2019-01-25','qas_sez(a)','qas_sez(a)','D615209','2018-12-07','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','DN41645','CUCTMER END','yes','Misc','qas_sez(a)','no','','|Checked all the parts in FG and requested customer to return the affected parts back to CIM.','Z3456','qas|','2019-04-11|','2019-04-11',NULL,NULL,NULL,NULL,NULL,NULL),(11415,'35A-628A','Saab AB','LATCH FORK ASSY','','D5227349300400','','PART ISSUE C',1,'OWED-LTA-001','','A17218','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','yes','INSUFFICIENT SEALANT AROUND THE BUSH','Squeeze out sealant was not uniform|Manual application of Sealant','|Reworked the returned parts from SAAB as per CIM rework procedure and sent back to customer.','|After the squeeze out of sealant excess sealant will be applied around the bush.','Next batches produced verified and found ok.','C67490','2019-01-25','qas_sez(a)','qas_sez(a)','GLB405303','2018-12-28','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUCTMER END','yes','Misc','qas_sez(a)','no','','|Checked and reworded the affected parts from CIM FG.','Z3456','qas|','2019-04-11|','2019-04-11',NULL,NULL,NULL,NULL,NULL,NULL),(11416,'35A-629A','Saab AB','LATCH FORK ASSY','','D5227349300500','','PART ISSUE C',1,'OWED-LTA-001','','A17219','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','yes','INSUFFICIENT SEALANT AROUND THE BUSH','Squeeze out sealant was not uniform|Manual application of Sealant','|Reworked the returned parts from SAAB as per CIM rework procedure and sent back to customer. ','|After the squeeze out of sealant excess sealant will be applied around the bush.','Next batches produced verified and found ok.','C67492','2019-01-25','qas_sez(a)','qas_sez(a)','D615206','2018-12-21','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUCTMER END','yes','Misc','qas_sez(a)','no','','|Checked and reworded the affected parts from CIM FG. ','Z3456','qas|','2019-04-11|','2019-04-11',NULL,NULL,NULL,NULL,NULL,NULL),(11417,'35A-629A','Saab AB','LATCH FORK ASSY','','D5227349300500','','PART ISSUE C',1,'OWED-LTA-001','','A17220','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','yes','INSUFFICIENT SEALANT AROUND THE BUSH ','Squeeze out sealant was not uniform|Manual application of Sealant','|Reworked the returned parts from SAAB as per CIM rework procedure and sent back to customer.','|After the squeeze out of sealant excess sealant will be applied around the bush.','Next batches produced verified and found ok.','C67493','2019-01-25','qas_sez(a)','qas_sez(a)','D615206','2018-12-21','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUCTMER END','yes','Misc','qas_sez(a)','no','','|Checked and reworded the affected parts from CIM FG.','Z3456','qas|','2019-04-11|','2019-04-11',NULL,NULL,NULL,NULL,NULL,NULL),(11418,'35A-355A','Saab AB','Pull Lift Actuator Suppor','','423Z1224-3','','---',2,'787 Forecast','','A15435','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','yes','BARE METAL OBSERVED.','Scratch like marks visible inside the bore because of the jigging method followed by the supplier.','|Reworked the parts in CIM as per CIM rework procedure and returned them back to SAAB.','|Informed the supplier to revise the jigging method to avoid the jigging impression on the part.','Next batch verified at CIM and found ok.','C67320','2019-01-25','qas_sez(a)','qas_sez(a)','GLB391214','2018-12-10','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUCTMER END','yes','Misc','qas_sez(a)','no','','|Checked all the parts in FG and requested customer to return the affected parts back to CIM','Z3456','qas|','2019-04-11|','2019-04-11',NULL,NULL,NULL,NULL,NULL,NULL),(11419,'35-261','Saab AB','RODEND','SH0582A4-H10','424Z3411-2','','--B',46,'1600177789','','69431','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','yes','SCRATCHES OBSERVED ON OD & CORROSION OBSERVED','Scratch like marks visible inside the bore because of the jigging method followed by the supplier.','|Reworked the parts in CIM as per CIM rework procedure and returned them back to SAAB.','|Informed the supplier to revise the jigging method to avoid the jigging impression on the part.','Next batch verified at CIM and found ok.','C65192','2019-01-25','qas_sez(a)','qas_sez(a)','GLB391041','2018-12-21','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','DN37891','CUSTOMER END','yes','Misc','qas_sez(a)','no','','|Checked all the parts in FG and requested customer to return the affected parts back to CIM.','Z3456','qas|','2019-04-11|','2019-04-11',NULL,NULL,NULL,NULL,NULL,NULL),(11420,'35-599','Saab AB','BEAM','7443601','D5227338120400','NA','PART ISSUE C',1,'OWED-LTA-001','','84423','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','HOLE DIA 15.9H7 OVERSIZE. deep catering marks found in the close tolerance bore  ',' work center changed from MAZAK I700 to HMC\r\n |parameters related to HMC program not validated ','|1. standard parameters will be updated in the program.\r<br/>2. supervisor has to verify the parameters before loading the progress on to the machine ','|ensuring the parameters before running the program. and making the standard parameters  ','CA & PA found satisfactory ','','2019-01-25','Nagaraju P K()','Thaveni D M ,Ravi Kumar G.B,Pradeep B.D,Nagaraju P K ,HariPrasad ,Dhanush J.K,','','0000-00-00','RE ENGG PART','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','3','no','a51nx-03','pe_sez(a)','no','','|1. informed to the supervisor and parameters like feed and speed are verified \r\n2. the feed rate reduced and maintained to the machine requirement  ','Z3456','qas_sez|','2019-02-13|','2019-02-13',NULL,NULL,NULL,NULL,NULL,NULL),(11421,'35-531A','Saab AB','SHAFT LATCH','C90596','D5227349020200','NA','PART ISSUE C',35,'OWED-LTA-002','','75910','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','yes','CORROSION OBSERVED','REFER NC NO 11424|REFER NC NO 11424|REFER NC NO 11424|REFER NC NO 11424|REFER NC NO 11424','|REFER NC NO 11424','|REFER NC NO 11424','REFER NC NO 11424','C68696','2019-01-25','qas_sez(a)','qas_sez(a)','D615215','2018-12-21','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','DN45504','CUSTOMER END','yes','Misc','qas_sez(a)','no','','|REFER NC NO 11424','Z3456','qas_sez|','2019-02-26|','2019-02-26',NULL,NULL,NULL,NULL,NULL,NULL),(11422,'35-531A','Saab AB','SHAFT LATCH','C90596','D5227349020200','NA','PART ISSUE C',8,'OWED-LTA-002','','73920','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','yes','CORROSION OBSERVED ','REFER NC NO 11424|REFER NC NO 11424|REFER NC NO 11424|REFER NC NO 11424|REFER NC NO 11424','|REFER NC NO 11424','|REFER NC NO 11424','REFER NC NO 11424','C68270','2019-01-25','qas_sez(a)','qas_sez(a)','D615195','2018-12-21','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','DN44173','CUSTOMER END','yes','Misc','qas_sez(a)','no','','|REFER NC NO 11424','Z3456','qas_sez|','2019-02-26|','2019-02-26',NULL,NULL,NULL,NULL,NULL,NULL),(11423,'35-531A','Saab AB','SHAFT LATCH','C90596','D5227349020200','NA','PART ISSUE C',7,'OWED-LTA-002','','75910','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','yes','CORROSION OBSERVED','REFER NC NO 11424|REFER NC NO 11424|REFER NC NO 11424|REFER NC NO 11424|REFER NC NO 11424','|REFER NC NO 11424','|REFER NC NO 11424','REFER NC NO 11424','C68695','2019-01-25','qas_sez(a)','qas_sez(a)','D615195','2018-12-21','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','DN45504','CUSTOMER END','yes','Misc','qas_sez(a)','no','','|REFER NC NO 11424','Z3456','qas_sez|','2019-02-26|','2019-02-26',NULL,NULL,NULL,NULL,NULL,NULL),(11424,'35-577A','Saab AB','SHAFT','C84690','D5227344120000','NA','PART ISSUE B',30,'OWED-LTA-004','','78761','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','yes','CORROSION OBSERVED','1) Same grade and different tools are used but bench work is carried out in the same location.\r\n2)  Fixture material was not prevented from corrosion causing agents.\r\n3) Rust preventive oil was used in between operations but was not effective.\r\n4) Wrapped in plastic covers and protected with Bubble and Foam wraps to prevent damages.\r\n5) Spray rinse method is used but was not effective.\r\n6) Improper cleaning on parts.\r\n7) Passivation layer was damaged|1) Different zones for bench working(de-burring) of different material was not alloted.\r\n2) Usually fixtures are preveserved with the help of Rust preventive oil(PX-24) which was less effective for fixtures stored long time.\r\n3) Rust preventive oil previously used was not good in eliminating the moisture content from the part surface.\r\n4) Plastic covers being non breathable caused built up of moisture content inside the cover which resulted in the initiation of corrosion before passivation.\r\n5) Complete 360degree rinsing of cylindrical parts was not effectively possible when the parts are suspended individually in side the spray rinse tank.\r\n6) Few parts / top portion parts were jigged using SS wire was above the rinsing nozzole level/ height.\r\n7) Parts surfaces were rubbibg/contacting during and after the passivation process.|1) There was no occurance of similar issue before.\r\n2) Previous rust preventive oil used to loose its rust prevention properties with 3 to 4 days where as the oil stays on the part for a week or more therefore it became hard to predict the cause of corrosion.\r\n5) Since the parts are suspended from the hanger with wires there and were not attached to any rotary actions comlpete rinsing(360 degree) cleaning was not effectively possible.\r\n6) There was no level indicator marked at the jigging/ loading station.\r\n7) There was no sufficient gap between part to part during movement of parts from each stage(During wagon movement and other andling}|6) The level indicator sticker provided was fallen down and the same was not noticed.\r\n7) Operator had not followed the material handling instructions as per SOP-PRD-09 during processing and there was no pictorial representation.|6) It was an adhessive sticker and not a permanent marking','|1) There was no occurance of similar issue before.\r<br/>2) Previous rust preventive oil used to loose its rust prevention properties with 3 to 4 days where as the oil stays on the part for a week or more therefore it became hard to predict the cause of corrosion.\r<br/>3) Rust preventive oil previously used was not good in eliminating the moisture content from the part surface.\r<br/>4) Plastic covers being non breathable caused built up of moisture content inside the cover which resulted in the initiation of corrosion before passivation.\r<br/>5) Since the parts are suspended from the hanger with wires there and were not attached to any rotary actions comlpete rinsing(360 degree) cleaning was not effectively possible.\r<br/>6) It was an adhessive sticker and not a permanent marking.\r<br/>7) Operator had not followed the material handling instructions as per SOP-PRD-09 during processing and there was no pictorial representation.','|Ensure proper handling of parts always and verify during internal Quality aduit. \r<br/>Process audit checklist will be amended and the process audit frequency will be increased.','next batch found ok.','C68720','2019-01-25','qas_sez(a)','qas_sez(a)','D615195','2018-12-21','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','DN45530','CUSTOMER END','yes','Misc','qas_sez(a)','no','','|FG checking and defect parts send to salt spray test. ','Z3456','qas_sez|','2019-02-26|','2019-02-26',NULL,NULL,NULL,NULL,NULL,NULL),(11425,'35-577A','Saab AB','SHAFT','C84690','D5227344120000','NA','PART ISSUE B',38,'OWED-LTA-004','','78760','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','yes','CORROSION OBSERVED','Refer NC No 11424.|Refer NC No 11424.|Refer NC No 11424.|Refer NC No 11424.|Refer NC No 11424.','|Refer NC No 11424.','|Refer NC No 11424.','Refer NC No 11424.','C68720','2019-01-25','qas_sez(a)','qas_sez(a)','D615195','2018-12-21','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','DN45529','CUSTOMER END','yes','Misc','qas_sez(a)','no','','|Refer NC No 11424.','Z3456','qas_sez|qas_sez|','2019-02-26|2019-02-26|','2019-02-26',NULL,NULL,NULL,NULL,NULL,NULL),(11426,'35-577A','Saab AB','SHAFT','C84690','D5227344120000','NA','PART ISSUE B',7,'OWED-LTA-004','','78763','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','yes','CORROSION OBSERVED','Refer NC No 11424.|Refer NC No 11424.|Refer NC No 11424.|Refer NC No 11424.|Refer NC No 11424.','|Refer NC No 11424.','|Refer NC No 11424.','Refer NC No 11424.','C68722','2019-01-25','qas_sez(a)','qas_sez(a)','D615195','2019-01-25','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','DN45532','CUSTOMER END','yes','Misc','qas_sez(a)','no','','|Refer NC No 11424.','Z3456','qas_sez|qas_sez|qas_sez|','2019-02-26|2019-02-26|2019-02-26|','2019-02-26',NULL,NULL,NULL,NULL,NULL,NULL),(11427,'35-577A','Saab AB','SHAFT','C84690','D5227344120000','NA','PART ISSUE B',55,'OWED-LTA-004','','78764','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','yes','CORROSION OBSERVED','Refer NC No 11424.|Refer NC No 11424.|Refer NC No 11424.|Refer NC No 11424.|Refer NC No 11424.','|Refer NC No 11424.','|Refer NC No 11424.','Refer NC No 11424.','C68722','2019-01-25','qas_sez(a)','qas_sez(a)','D615195','2018-12-21','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','DN45533','CUSTOMER END','yes','Misc','qas_sez(a)','no','','|Refer NC No 11424.','Z3456','qas_sez|','2019-02-26|','2019-02-26',NULL,NULL,NULL,NULL,NULL,NULL),(11428,'35-577A','Saab AB','SHAFT','C84690','D5227344120000','NA','PART ISSUE B',25,'OWED-LTA-004','','78759','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','yes','CORROSION OBSERVED','Refer NC No 11424.|Refer NC No 11424.|Refer NC No 11424.|Refer NC No 11424.|Refer NC No 11424.','|Refer NC No 11424.','|Refer NC No 11424.','Refer NC No 11424.','C68719','2019-01-25','qas_sez(a)','qas_sez(a)','D615195','2018-12-21','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','DN45528','CUSTOMER END','yes','Misc','qas_sez(a)','no','','|Refer NC No 11424.','Z3456','qas_sez|','2019-02-26|','2019-02-26',NULL,NULL,NULL,NULL,NULL,NULL),(11429,'35-577A','Saab AB','SHAFT','C84690','D5227344120000','NA','PART ISSUE B',66,'OWED-LTA-004','','78762','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','yes','CORROSION OBSERVED','REFER NC NO 11424|REFER NC NO 11424|REFER NC NO 11424|REFER NC NO 11424|REFER NC NO 11424','|REFER NC NO 11424','|REFER NC NO 11424','REFER NC NO 11424','C68721','2019-01-25','qas_sez(a)','qas_sez(a)','D615195','2018-12-21','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','DN45531','CUSTOMER END','yes','Misc','qas_sez(a)','no','','|REFER NC NO 11424','Z3456','qas_sez|','2019-02-26|','2019-02-26',NULL,NULL,NULL,NULL,NULL,NULL),(11430,'35-577A','Saab AB','SHAFT','C84690','D5227344120000','NA','PART ISSUE B',6,'OWED-LTA-004','','78762','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','yes','CORROSION OBSERVED','REFER NC NO 11424|REFER NC NO 11424|REFER NC NO 11424|REFER NC NO 11424|REFER NC NO 11424','|REFER NC NO 11424','|REFER NC NO 11424','REFER NC NO 11424','C68722','2019-01-25','qas_sez(a)','qas_sez(a)','D615195','2019-01-25','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','DN45531','CUSTOMER END','yes','Misc','qas_sez(a)','no','','|REFER NC NO 11424','Z3456','qas_sez|','2019-02-26|','2019-02-26',NULL,NULL,NULL,NULL,NULL,NULL),(11431,'35-624A','Saab AB','SHAFT 3','C87212','D5227281320000','NA','PART ISSUE B',7,'OWED-LTA-004','','73779','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','yes','CORROSION OBSERVED','REFER NC NO 11424|REFER NC NO 11424|REFER NC NO 11424|REFER NC NO 11424|REFER NC NO 11424','|REFER NC NO 11424','|REFER NC NO 11424','REFER NC NO 11424','C66807','2019-01-25','qas_sez(a)','qas_sez(a)','D615195','2018-12-21','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','DN41535','CUSTOMER END','yes','Misc','qas_sez(a)','no','','|REFER NC NO 11424','Z3456','qas_sez|','2019-02-26|','2019-02-26',NULL,NULL,NULL,NULL,NULL,NULL),(11432,'35-624A','Saab AB','SHAFT 3','C87212','D5227281320000','NA','PART ISSUE B',3,'OWED-LTA-004','','76292','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','yes','CORROSION OBSERVED','REFER NC NO 11424|REFER NC NO 11424|REFER NC NO 11424|REFER NC NO 11424|REFER NC NO 11424','|REFER NC NO 11424','|REFER NC NO 11424','REFER NC NO 11424','C68777','2019-01-25','qas_sez(a)','qas_sez(a)','D615195','2018-12-21','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','DN42635','CUSTOMER END','yes','Misc','qas_sez(a)','no','','|REFER NC NO 11424','Z3456','qas_sez|','2019-02-26|','2019-02-26',NULL,NULL,NULL,NULL,NULL,NULL),(11433,'35-603A','Saab AB','OUTER HANDLE SHAFT','B76681','D5227354020600','','PART ISSUE D',4,'OWED-LTA-004','','75702','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','yes','CORROSION OBSERVED','REFER NC NO 11424|REFER NC NO 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