(11441,'35-624A','Saab AB','SHAFT 3','C87212','D5227281320000','NA','PART ISSUE B',2,'OWED-LTA-004','','73331','','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','C66002','2019-01-25','qas_sez(a)','qas_sez(a)','D615195','2018-12-21','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','DN41092','CUSTOMER END','yes','Misc','qas_sez(a)','no','','|REFER NC NO 11424','Z3456','qas_sez|','2019-02-26|','2019-02-26',NULL,NULL,NULL,NULL,NULL,NULL),(11442,'35-603A','Saab AB','OUTER HANDLE SHAFT','B76681','D5227354020600','','PART ISSUE D',11,'OWED-LTA-004','','75703','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','yes','CORROSION OBSERVED','REFER NC NO 11424|REFER NC NO 11424|REFER NC NO 11424|REFER NC NO 11424|REFER NC NO 11424','|REFER NC NO 11424','|REFER NC NO 11424','REFER NC NO 11424','C66864','2019-01-25','qas_sez(a)','qas_sez(a)','D615195','2018-12-21','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','DN42767','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),(11443,'35A-474A','Saab AB','FRAME ASSY','','D5227338400000','','B',8,'OWED-LTA-001','','A17260','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','yes','Parts don\'t meet the flatness tolerance 0,4 mm.\r\nShould be: The parts should be in the flatness tolerance 0,4 mm.','1) Bend occurred on the part during roughing operation and was not removed in- between operations.\r\n|2) Due low thickness finish from high thickness RM the machining strategy caused the material to deform and no intermediate correction was given.\r\n|3) Intermediate correction for the bend removal and aging was not considered during the processing of these pars.\r\n|4) usually aging and intermediate distortion correction are done for the parts longer than 1m length.\r\n','|All the semi-finished parts were left for aging and intermediate distortion correction process was included. \r<br/>','|MPS amended to include the intermediate aging and intermediate distortion correction process after the roughing operation.\r<br/>','Next batched produced according to the revised process and the delta FAI was found ok. \r\n','C67537','2019-01-28','qas_sez(a)','qas_sez(a)','GLB406814','2018-12-11','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER END','yes','Misc','qas_sez(a)','no','','|Immediately collected all the parts from customer and stopped the production line and checked the machining completed parts and separated the deformed pats. \r\n','Z3456','qas_sez|','2019-04-17|','2019-04-17',NULL,NULL,NULL,NULL,NULL,NULL),(11444,'35A-474A','Saab AB','FRAME ASSY','','D5227338400000','','B',1,'1600214688','','A15876','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Parts don\'t meet the flatness tolerance 0,4 mm.\r\nShould be: The parts should be in the flatness tolerance 0,4 mm.','1) Bend occurred on the part during roughing operation and was not removed in- between operations.\r\n|2) Due low thickness finish from high thickness RM the machining strategy caused the material to deform and no intermediate correction was given.\r\n|3) Intermediate correction for the bend removal and aging was not considered during the processing of these pars.\r\n|4) usually aging and intermediate distortion correction are done for the parts longer than 1m length.\r\n','|All the semi-finished parts were left for aging and intermediate distortion correction process was included. \r<br/>','|MPS amended to include the intermediate aging and intermediate distortion correction process after the roughing operation.\r<br/>','Next batched produced according to the revised process and the delta FAI was found ok. \r\n','C66142','2019-01-28','qas_sez(a)','qas_sez(a)','GLB406814','2019-01-28','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER 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. \r\n','Z3456','qas_sez|','2019-04-17|','2019-04-17',NULL,NULL,NULL,NULL,NULL,NULL),(11445,'35A-475A','Saab AB','FRAME ASSY','','D5227338400100','','B',5,'OWED-LTA-001','','A16414','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Parts don\'t meet the flatness tolerance 0,4 mm.\r\nShould be: The parts should be in the flatness tolerance 0,4 mm.','1) Bend occurred on the part during roughing operation and was not removed in- between operations.\r\n|2) Due low thickness finish from high thickness RM the machining strategy caused the material to deform and no intermediate correction was given.\r\n|3) Intermediate correction for the bend removal and aging was not considered during the processing of these pars.\r\n|4) usually aging and intermediate distortion correction are done for the parts longer than 1m length.\r\n','|All the semi-finished parts were left for aging and intermediate distortion correction process was included. \r<br/>','|MPS amended to include the intermediate aging and intermediate distortion correction process after the roughing operation.\r<br/>','Next batched produced according to the revised process and the delta FAI was found ok. \r\n','C66470','2019-01-28','qas_sez(a)','qas_sez(a)','GLB406814','2019-01-28','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER END','yes','Misc','qas_sez(a)','no','','|Immediately collected all the parts from customer and stopped the production line and checked the machining completed parts and separated the deformed pats. \r\n','Z3456','qas_sez|','2019-04-17|','2019-04-17',NULL,NULL,NULL,NULL,NULL,NULL),(11446,'35A-475A','Saab AB','FRAME ASSY','','D5227338400100','','B',6,'1600214688','','A15865','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Parts don\'t meet the flatness tolerance 0,4 mm.\r\nShould be: The parts should be in the flatness tolerance 0,4 mm.','1) Bend occurred on the part during roughing operation and was not removed in- between operations.\r\n|2) Due low thickness finish from high thickness RM the machining strategy caused the material to deform and no intermediate correction was given.\r\n|3) Intermediate correction for the bend removal and aging was not considered during the processing of these pars.\r\n|4) usually aging and intermediate distortion correction are done for the parts longer than 1m length.\r\n','|All the semi-finished parts were left for aging and intermediate distortion correction process was included. \r<br/>','|MPS amended to include the intermediate aging and intermediate distortion correction process after the roughing operation.\r<br/>','Next batched produced according to the revised process and the delta FAI was found ok. \r\n','C66146','2019-01-28','qas_sez(a)','qas_sez(a)','GLB406814','2019-01-28','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER 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. \r\n','Z3456','qas_sez|','2019-04-17|','2019-04-17',NULL,NULL,NULL,NULL,NULL,NULL),(11447,'35A-475A','Saab AB','FRAME ASSY','','D5227338400100','','B',4,'1600214688','','A17266','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Parts don\'t meet the flatness tolerance 0,4 mm.\r\nShould be: The parts should be in the flatness tolerance 0,4 mm.','1) Bend occurred on the part during roughing operation and was not removed in- between operations.\r\n|2) Due low thickness finish from high thickness RM the machining strategy caused the material to deform and no intermediate correction was given.\r\n|3) Intermediate correction for the bend removal and aging was not considered during the processing of these pars.\r\n|4) usually aging and intermediate distortion correction are done for the parts longer than 1m length.\r\n','|All the semi-finished parts were left for aging and intermediate distortion correction process was included. \r<br/>','|MPS amended to include the intermediate aging and intermediate distortion correction process after the roughing operation.\r<br/>','Next batched produced according to the revised process and the delta FAI was found ok. \r\n','C67557','2019-01-28','qas_sez(a)','qas_sez(a)','GLB406814','2019-01-28','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER END','yes','Misc','qas_sez(a)','no','','|Immediately collected all the parts from customer and stopped the production line and checked the machining completed parts and separated the deformed pats. \r\n','Z3456','qas_sez|','2019-04-17|','2019-04-17',NULL,NULL,NULL,NULL,NULL,NULL),(11448,'35A-475A','Saab AB','FRAME ASSY','','D5227338400100','','B',3,'OWED-LTA-001','','A16415','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Parts don\'t meet the flatness tolerance 0,4 mm.\r\nShould be: The parts should be in the flatness tolerance 0,4 mm.','1) Bend occurred on the part during roughing operation and was not removed in- between operations.\r\n|2) Due low thickness finish from high thickness RM the machining strategy caused the material to deform and no intermediate correction was given.\r\n|3) Intermediate correction for the bend removal and aging was not considered during the processing of these pars.\r\n|4) usually aging and intermediate distortion correction are done for the parts longer than 1m length.\r\n','|All the semi-finished parts were left for aging and intermediate distortion correction process was included. \r<br/>','|MPS amended to include the intermediate aging and intermediate distortion correction process after the roughing operation.\r<br/>','Next batched produced according to the revised process and the delta FAI was found ok. \r\n','C66470','2019-01-28','qas_sez(a)','qas_sez(a)','GLB406814','2019-01-28','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER 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. \r\n','Z3456','qas_sez|','2019-04-17|','2019-04-17',NULL,NULL,NULL,NULL,NULL,NULL),(11449,'35A-474A','Saab AB','FRAME ASSY','','D5227338400000','','B',7,'OWED-LTA-001','','A16402','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Parts don\'t meet the flatness tolerance 0,4 mm.\r\nShould be: The parts should be in the flatness tolerance 0,4 mm.','1) Bend occurred on the part during roughing operation and was not removed in- between operations.\r\n|2) Due low thickness finish from high thickness RM the machining strategy caused the material to deform and no intermediate correction was given.\r\n|3) Intermediate correction for the bend removal and aging was not considered during the processing of these pars.\r\n|4) usually aging and intermediate distortion correction are done for the parts longer than 1m length.\r\n','|All the semi-finished parts were left for aging and intermediate distortion correction process was included. \r<br/>','|MPS amended to include the intermediate aging and intermediate distortion correction process after the roughing operation.\r<br/>','Next batched produced according to the revised process and the delta FAI was found ok. \r\n','C67537','2019-01-28','qas_sez(a)','qas_sez(a)','GLB406814','2019-01-28','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER END','yes','Misc','qas_sez(a)','no','','|Immediately collected all the parts from customer and stopped the production line and checked the machining completed parts and separated the deformed pats. \r\n','Z3456','qas_sez|','2019-04-17|','2019-04-17',NULL,NULL,NULL,NULL,NULL,NULL),(11450,'35A-474A','Saab AB','FRAME ASSY','','D5227338400000','','B',3,'1600214688','','A15879','','2019-01-28',NULL,'yes','yes','no','no','no','no','no','no','yes','Parts don\'t meet the flatness tolerance 0,4 mm.\r\nShould be: The parts should be in the flatness tolerance 0,4 mm.','1) Bend occurred on the part during roughing operation and was not removed in- between operations.\r\n|2) Due low thickness finish from high thickness RM the machining strategy caused the material to deform and no intermediate correction was given.\r\n|3) Intermediate correction for the bend removal and aging was not considered during the processing of these pars.\r\n|4) usually aging and intermediate distortion correction are done for the parts longer than 1m length.\r\n','|All the semi-finished parts were left for aging and intermediate distortion correction process was included. \r<br/>','|MPS amended to include the intermediate aging and intermediate distortion correction process after the roughing operation.\r<br/>','Next batched produced according to the revised process and the delta FAI was found ok. \r\n','C66144','2019-01-28','qas_sez(a)','qas_sez(a)','GLB406814','2019-01-28','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER 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. \r\n','Z3456','qas_sez|','2019-04-17|','2019-04-17',NULL,NULL,NULL,NULL,NULL,NULL),(11451,'35A-475A','Saab AB','FRAME ASSY','','D5227338400100','','B',12,'OWED-LTA-001','','A18638','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Parts don\'t meet the flatness tolerance 0,4 mm.\r\nShould be: The parts should be in the flatness tolerance 0,4 mm.','1) Bend occurred on the part during roughing operation and was not removed in- between operations.\r\n|2) Due low thickness finish from high thickness RM the machining strategy caused the material to deform and no intermediate correction was given.\r\n|3) Intermediate correction for the bend removal and aging was not considered during the processing of these pars.\r\n|4) usually aging and intermediate distortion correction are done for the parts longer than 1m length.\r\n','|All the semi-finished parts were left for aging and intermediate distortion correction process was included. \r<br/>','|MPS amended to include the intermediate aging and intermediate distortion correction process after the roughing operation.\r<br/>','Next batched produced according to the revised process and the delta FAI was found ok. \r\n','C69325','2019-01-28','qas_sez(a)','qas_sez(a)','GLB406814','2019-01-28','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER END','yes','Misc','qas_sez(a)','no','','|Immediately collected all the parts from customer and stopped the production line and checked the machining completed parts and separated the deformed pats. \r\n','Z3456','qas_sez|','2019-04-17|','2019-04-17',NULL,NULL,NULL,NULL,NULL,NULL),(11452,'35A-474A','Saab AB','FRAME ASSY','','D5227338400000','','B',13,'OWED-LTA-001','','A15877','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Parts don\'t meet the flatness tolerance 0,4 mm.\r\nShould be: The parts should be in the flatness tolerance 0,4 mm.','1) Bend occurred on the part during roughing operation and was not removed in- between operations.\r\n|2) Due low thickness finish from high thickness RM the machining strategy caused the material to deform and no intermediate correction was given.\r\n|3) Intermediate correction for the bend removal and aging was not considered during the processing of these pars.\r\n|4) usually aging and intermediate distortion correction are done for the parts longer than 1m length.\r\n','|All the semi-finished parts were left for aging and intermediate distortion correction process was included. \r<br/>','|MPS amended to include the intermediate aging and intermediate distortion correction process after the roughing operation.\r<br/>','Next batched produced according to the revised process and the delta FAI was found ok. \r\n','C66143','2019-01-28','qas_sez(a)','qas_sez(a)','GLB406814','2019-01-28','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER 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. \r\n','Z3456','qas_sez|','2019-04-17|','2019-04-17',NULL,NULL,NULL,NULL,NULL,NULL),(11453,'35A-475A','Saab AB','FRAME ASSY','','D5227338400100','','B',4,'OWED-LTA-001','','A17269','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Parts don\'t meet the flatness tolerance 0,4 mm.\r\nShould be: The parts should be in the flatness tolerance 0,4 mm.','1) Bend occurred on the part during roughing operation and was not removed in- between operations.\r\n|2) Due low thickness finish from high thickness RM the machining strategy caused the material to deform and no intermediate correction was given.\r\n|3) Intermediate correction for the bend removal and aging was not considered during the processing of these pars.\r\n|4) usually aging and intermediate distortion correction are done for the parts longer than 1m length.\r\n','|All the semi-finished parts were left for aging and intermediate distortion correction process was included. \r<br/>','|MPS amended to include the intermediate aging and intermediate distortion correction process after the roughing operation.\r<br/>','Next batched produced according to the revised process and the delta FAI was found ok. \r\n','C68295','2019-01-28','qas_sez(a)','qas_sez(a)','GLB406814','2019-01-28','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER END','yes','Misc','qas_sez(a)','no','','|Immediately collected all the parts from customer and stopped the production line and checked the machining completed parts and separated the deformed pats. \r\n','Z3456','qas_sez|','2019-04-17|','2019-04-17',NULL,NULL,NULL,NULL,NULL,NULL),(11454,'35A-474A','Saab AB','FRAME ASSY','','D5227338400000','','B',13,'OWED-LTA-001','','A16225','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Parts don\'t meet the flatness tolerance 0,4 mm.\r\nShould be: The parts should be in the flatness tolerance 0,4 mm.','1) Bend occurred on the part during roughing operation and was not removed in- between operations.\r\n|2) Due low thickness finish from high thickness RM the machining strategy caused the material to deform and no intermediate correction was given.\r\n|3) Intermediate correction for the bend removal and aging was not considered during the processing of these pars.\r\n|4) usually aging and intermediate distortion correction are done for the parts longer than 1m length.\r\n','|All the semi-finished parts were left for aging and intermediate distortion correction process was included. \r<br/>','|MPS amended to include the intermediate aging and intermediate distortion correction process after the roughing operation.\r<br/>','Next batched produced according to the revised process and the delta FAI was found ok. \r\n','C66460','2019-01-28','qas_sez(a)','qas_sez(a)','GLB406814','2019-01-28','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER 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. \r\n','Z3456','qas_sez|','2019-04-17|','2019-04-17',NULL,NULL,NULL,NULL,NULL,NULL),(11455,'35A-475A','Saab AB','FRAME ASSY','','D5227338400100','','B',6,'OWED-LTA-001','','A16416','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Parts don\'t meet the flatness tolerance 0,4 mm.\r\nShould be: The parts should be in the flatness tolerance 0,4 mm.','1) Bend occurred on the part during roughing operation and was not removed in- between operations.\r\n|2) Due low thickness finish from high thickness RM the machining strategy caused the material to deform and no intermediate correction was given.\r\n|3) Intermediate correction for the bend removal and aging was not considered during the processing of these pars.\r\n|4) usually aging and intermediate distortion correction are done for the parts longer than 1m length.\r\n','|All the semi-finished parts were left for aging and intermediate distortion correction process was included. \r<br/>','|MPS amended to include the intermediate aging and intermediate distortion correction process after the roughing operation.\r<br/>','Next batched produced according to the revised process and the delta FAI was found ok. \r\n','C67557','2019-01-28','qas_sez(a)','qas_sez(a)','GLB406814','2019-01-28','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER END','yes','Misc','qas_sez(a)','no','','|Immediately collected all the parts from customer and stopped the production line and checked the machining completed parts and separated the deformed pats. \r\n','Z3456','qas_sez|','2019-04-17|','2019-04-17',NULL,NULL,NULL,NULL,NULL,NULL),(11456,'35A-474A','Saab AB','FRAME ASSY','','D5227338400000','','B',4,'OWED-LTA-001','','A16398','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Parts don\'t meet the flatness tolerance 0,4 mm.\r\nShould be: The parts should be in the flatness tolerance 0,4 mm.','1) Bend occurred on the part during roughing operation and was not removed in- between operations.\r\n|2) Due low thickness finish from high thickness RM the machining strategy caused the material to deform and no intermediate correction was given.\r\n|3) Intermediate correction for the bend removal and aging was not considered during the processing of these pars.\r\n|4) usually aging and intermediate distortion correction are done for the parts longer than 1m length.\r\n','|All the semi-finished parts were left for aging and intermediate distortion correction process was included. \r<br/>','|MPS amended to include the intermediate aging and intermediate distortion correction process after the roughing operation.\r<br/>','Next batched produced according to the revised process and the delta FAI was found ok. \r\n','C66460','2019-01-28','qas_sez(a)','qas_sez(a)','GLB406814','2019-01-28','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER 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. \r\n','Z3456','qas_sez|','2019-04-17|','2019-04-17',NULL,NULL,NULL,NULL,NULL,NULL),(11457,'35A-474A','Saab AB','FRAME ASSY','','D5227338400000','','B',20,'OWED-LTA-001','','A17258','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Parts don\'t meet the flatness tolerance 0,4 mm.\r\nShould be: The parts should be in the flatness tolerance 0,4 mm.','1) Bend occurred on the part during roughing operation and was not removed in- between operations.\r\n|2) Due low thickness finish from high thickness RM the machining strategy caused the material to deform and no intermediate correction was given.\r\n|3) Intermediate correction for the bend removal and aging was not considered during the processing of these pars.\r\n|4) usually aging and intermediate distortion correction are done for the parts longer than 1m length.\r\n','|All the semi-finished parts were left for aging and intermediate distortion correction process was included. \r<br/>','|MPS amended to include the intermediate aging and intermediate distortion correction process after the roughing operation.\r<br/>','Next batched produced according to the revised process and the delta FAI was found ok. \r\n','C67537','2019-01-28','qas_sez(a)','qas_sez(a)','GLB406814','2019-01-28','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER END','yes','Misc','qas_sez(a)','no','','|Immediately collected all the parts from customer and stopped the production line and checked the machining completed parts and separated the deformed pats. \r\n','Z3456','qas_sez|','2019-04-17|','2019-04-17',NULL,NULL,NULL,NULL,NULL,NULL),(11458,'35A-475A','Saab AB','FRAME ASSY','','D5227338400100','','B',7,'OWED-LTA-001','','A15619','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Parts don\'t meet the flatness tolerance 0,4 mm.\r\nShould be: The parts should be in the flatness tolerance 0,4 mm.','1) Bend occurred on the part during roughing operation and was not removed in- between operations.\r\n|2) Due low thickness finish from high thickness RM the machining strategy caused the material to deform and no intermediate correction was given.\r\n|3) Intermediate correction for the bend removal and aging was not considered during the processing of these pars.\r\n|4) usually aging and intermediate distortion correction are done for the parts longer than 1m length.\r\n','|All the semi-finished parts were left for aging and intermediate distortion correction process was included. \r<br/>','|MPS amended to include the intermediate aging and intermediate distortion correction process after the roughing operation.\r<br/>','Next batched produced according to the revised process and the delta FAI was found ok. \r\n','C66145','2019-01-28','qas_sez(a)','qas_sez(a)','GLB406814','2019-01-28','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER 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. \r\n','Z3456','qas_sez|','2019-04-17|','2019-04-17',NULL,NULL,NULL,NULL,NULL,NULL),(11459,'35A-475A','Saab AB','FRAME ASSY','','D5227338400100','','B',6,'OWED-LTA-001','','A15619','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Parts don\'t meet the flatness tolerance 0,4 mm.\r\nShould be: The parts should be in the flatness tolerance 0,4 mm.','1) Bend occurred on the part during roughing operation and was not removed in- between operations.\r\n|2) Due low thickness finish from high thickness RM the machining strategy caused the material to deform and no intermediate correction was given.\r\n|3) Intermediate correction for the bend removal and aging was not considered during the processing of these pars.\r\n|4) usually aging and intermediate distortion correction are done for the parts longer than 1m length.\r\n','|All the semi-finished parts were left for aging and intermediate distortion correction process was included. \r<br/>','|MPS amended to include the intermediate aging and intermediate distortion correction process after the roughing operation.\r<br/>','Next batched produced according to the revised process and the delta FAI was found ok. \r\n','C66146','2019-01-28','qas_sez(a)','qas_sez(a)','GLB406814','2019-01-28','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER END','yes','Misc','qas_sez(a)','no','','|Immediately collected all the parts from customer and stopped the production line and checked the machining completed parts and separated the deformed pats. \r\n','Z3456','qas_sez|','2019-04-17|','2019-04-17',NULL,NULL,NULL,NULL,NULL,NULL),(11460,'35A-475A','Saab AB','FRAME ASSY','','D5227338400100','','B',9,'OWED-LTA-001','','A15687','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Parts don\'t meet the flatness tolerance 0,4 mm.\r\nShould be: The parts should be in the flatness tolerance 0,4 mm.','1) Bend occurred on the part during roughing operation and was not removed in- between operations.\r\n|2) Due low thickness finish from high thickness RM the machining strategy caused the material to deform and no intermediate correction was given.\r\n|3) Intermediate correction for the bend removal and aging was not considered during the processing of these pars.\r\n|4) usually aging and intermediate distortion correction are done for the parts longer than 1m length.\r\n','|All the semi-finished parts were left for aging and intermediate distortion correction process was included. \r<br/>','|MPS amended to include the intermediate aging and intermediate distortion correction process after the roughing operation.\r<br/>','Next batched produced according to the revised process and the delta FAI was found ok. \r\n','C66146','2019-01-28','qas_sez(a)','qas_sez(a)','GLB406814','2019-01-28','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER 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. \r\n','Z3456','qas_sez|','2019-04-17|','2019-04-17',NULL,NULL,NULL,NULL,NULL,NULL),(11461,'35A-475A','Saab AB','FRAME ASSY','','D5227338400100','','B',4,'OWED-LTA-001','','A18639','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Parts don\'t meet the flatness tolerance 0,4 mm.\r\nShould be: The parts should be in the flatness tolerance 0,4 mm.','1) Bend occurred on the part during roughing operation and was not removed in- between operations.\r\n|2) Due low thickness finish from high thickness RM the machining strategy caused the material to deform and no intermediate correction was given.\r\n|3) Intermediate correction for the bend removal and aging was not considered during the processing of these pars.\r\n|4) usually aging and intermediate distortion correction are done for the parts longer than 1m length.\r\n','|All the semi-finished parts were left for aging and intermediate distortion correction process was included. \r<br/>','|MPS amended to include the intermediate aging and intermediate distortion correction process after the roughing operation.\r<br/>','Next batched produced according to the revised process and the delta FAI was found ok. \r\n','C69325','2019-01-28','qas_sez(a)','qas_sez(a)','GLB406814','2019-01-28','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER END','yes','Misc','qas_sez(a)','no','','|Immediately collected all the parts from customer and stopped the production line and checked the machining completed parts and separated the deformed pats. \r\n','Z3456','qas_sez|','2019-04-17|','2019-04-17',NULL,NULL,NULL,NULL,NULL,NULL),(11462,'35A-475A','Saab AB','FRAME ASSY','','D5227338400100','','B',6,'OWED-LTA-001','','A15389','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Parts don\'t meet the flatness tolerance 0,4 mm.\r\nShould be: The parts should be in the flatness tolerance 0,4 mm.','1) Bend occurred on the part during roughing operation and was not removed in- between operations.\r\n|2) Due low thickness finish from high thickness RM the machining strategy caused the material to deform and no intermediate correction was given.\r\n|3) Intermediate correction for the bend removal and aging was not considered during the processing of these pars.\r\n|4) usually aging and intermediate distortion correction are done for the parts longer than 1m length.\r\n','|All the semi-finished parts were left for aging and intermediate distortion correction process was included. \r<br/>','|MPS amended to include the intermediate aging and intermediate distortion correction process after the roughing operation.\r<br/>','Next batched produced according to the revised process and the delta FAI was found ok. \r\n','C65527','2019-01-28','qas_sez(a)','qas_sez(a)','GLB406814','2019-01-28','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER 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. \r\n','Z3456','qas_sez|','2019-04-17|','2019-04-17',NULL,NULL,NULL,NULL,NULL,NULL),(11463,'35A-475A','Saab AB','FRAME ASSY','','D5227338400100','','B',6,'OWED-LTA-001','','A17268','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Parts don\'t meet the flatness tolerance 0,4 mm.\r\nShould be: The parts should be in the flatness tolerance 0,4 mm.','1) Bend occurred on the part during roughing operation and was not removed in- between operations.\r\n|2) Due low thickness finish from high thickness RM the machining strategy caused the material to deform and no intermediate correction was given.\r\n|3) Intermediate correction for the bend removal and aging was not considered during the processing of these pars.\r\n|4) usually aging and intermediate distortion correction are done for the parts longer than 1m length.\r\n','|All the semi-finished parts were left for aging and intermediate distortion correction process was included. \r<br/>','|MPS amended to include the intermediate aging and intermediate distortion correction process after the roughing operation.\r<br/>','Next batched produced according to the revised process and the delta FAI was found ok. \r\n','C68295','2019-01-28','qas_sez(a)','qas_sez(a)','GLB406814','2019-01-28','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER END','yes','Misc','qas_sez(a)','no','','|Immediately collected all the parts from customer and stopped the production line and checked the machining completed parts and separated the deformed pats. \r\n','Z3456','qas_sez|','2019-04-17|','2019-04-17',NULL,NULL,NULL,NULL,NULL,NULL),(11464,'35A-474A','Saab AB','FRAME ASSY','','D5227338400000','','B',1,'1600214688','','A15879','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Parts don\'t meet the flatness tolerance 0,4 mm.\r\nShould be: The parts should be in the flatness tolerance 0,4 mm.','1) Bend occurred on the part during roughing operation and was not removed in- between operations.\r\n|2) Due low thickness finish from high thickness RM the machining strategy caused the material to deform and no intermediate correction was given.\r\n|3) Intermediate correction for the bend removal and aging was not considered during the processing of these pars.\r\n|4) usually aging and intermediate distortion correction are done for the parts longer than 1m length.\r\n','|All the semi-finished parts were left for aging and intermediate distortion correction process was included. \r<br/>','|MPS amended to include the intermediate aging and intermediate distortion correction process after the roughing operation.\r<br/>','Next batched produced according to the revised process and the delta FAI was found ok. \r\n','C66144','2019-01-28','qas_sez(a)','qas_sez(a)','GLB406814','2019-01-28','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER 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. \r\n','Z3456','qas_sez|','2019-04-17|','2019-04-17',NULL,NULL,NULL,NULL,NULL,NULL),(11465,'35A-474A','Saab AB','FRAME ASSY','','D5227338400000','','B',13,'OWED-LTA-001','','A17261','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Parts don\'t meet the flatness tolerance 0,4 mm.\r\nShould be: The parts should be in the flatness tolerance 0,4 mm.','1) Bend occurred on the part during roughing operation and was not removed in- between operations.\r\n|2) Due low thickness finish from high thickness RM the machining strategy caused the material to deform and no intermediate correction was given.\r\n|3) Intermediate correction for the bend removal and aging was not considered during the processing of these pars.\r\n|4) usually aging and intermediate distortion correction are done for the parts longer than 1m length.\r\n','|All the semi-finished parts were left for aging and intermediate distortion correction process was included. \r<br/>','|MPS amended to include the intermediate aging and intermediate distortion correction process after the roughing operation.\r<br/>','Next batched produced according to the revised process and the delta FAI was found ok. \r\n','C68294','2019-01-28','qas_sez(a)','qas_sez(a)','GLB406814','2019-01-28','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER END','yes','Misc','qas_sez(a)','no','','|Immediately collected all the parts from customer and stopped the production line and checked the machining completed parts and separated the deformed pats. \r\n','Z3456','qas_sez|','2019-04-17|','2019-04-17',NULL,NULL,NULL,NULL,NULL,NULL),(11466,'35A-474A','Saab AB','FRAME ASSY','','D5227338400000','','B',9,'OWED-LTA-001','','A18655','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Parts don\'t meet the flatness tolerance 0,4 mm.\r\nShould be: The parts should be in the flatness tolerance 0,4 mm.','1) Bend occurred on the part during roughing operation and was not removed in- between operations.\r\n|2) Due low thickness finish from high thickness RM the machining strategy caused the material to deform and no intermediate correction was given.\r\n|3) Intermediate correction for the bend removal and aging was not considered during the processing of these pars.\r\n|4) usually aging and intermediate distortion correction are done for the parts longer than 1m length.\r\n','|All the semi-finished parts were left for aging and intermediate distortion correction process was included. \r<br/>','|MPS amended to include the intermediate aging and intermediate distortion correction process after the roughing operation.\r<br/>','Next batched produced according to the revised process and the delta FAI was found ok. \r\n','C69308','2019-01-28','qas_sez(a)','qas_sez(a)','GLB406814','2019-01-28','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER 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. \r\n','Z3456','qas_sez|','2019-04-17|','2019-04-17',NULL,NULL,NULL,NULL,NULL,NULL),(11467,'35A-474A','Saab AB','FRAME ASSY','','D5227338400000','','B',6,'OWED-LTA-001','','A18656','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Parts don\'t meet the flatness tolerance 0,4 mm.\r\nShould be: The parts should be in the flatness tolerance 0,4 mm.','1) Bend occurred on the part during roughing operation and was not removed in- between operations.\r\n|2) Due low thickness finish from high thickness RM the machining strategy caused the material to deform and no intermediate correction was given.\r\n|3) Intermediate correction for the bend removal and aging was not considered during the processing of these pars.\r\n|4) usually aging and intermediate distortion correction are done for the parts longer than 1m length.\r\n','|All the semi-finished parts were left for aging and intermediate distortion correction process was included. \r<br/>','|MPS amended to include the intermediate aging and intermediate distortion correction process after the roughing operation.\r<br/>','Next batched produced according to the revised process and the delta FAI was found ok. \r\n','C69308','2019-01-28','qas_sez(a)','qas_sez(a)','GLB406814','2019-01-28','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER END','yes','Misc','qas_sez(a)','no','','|Immediately collected all the parts from customer and stopped the production line and checked the machining completed parts and separated the deformed pats. \r\n','Z3456','qas_sez|','2019-04-17|','2019-04-17',NULL,NULL,NULL,NULL,NULL,NULL),(11468,'35A-475A','Saab AB','FRAME ASSY','','D5227338400100','','B',15,'OWED-LTA-001','','A17262','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Parts don\'t meet the flatness tolerance 0,4 mm.\r\nShould be: The parts should be in the flatness tolerance 0,4 mm.','1) Bend occurred on the part during roughing operation and was not removed in- between operations.\r\n|2) Due low thickness finish from high thickness RM the machining strategy caused the material to deform and no intermediate correction was given.\r\n|3) Intermediate correction for the bend removal and aging was not considered during the processing of these pars.\r\n|4) usually aging and intermediate distortion correction are done for the parts longer than 1m length.\r\n','|All the semi-finished parts were left for aging and intermediate distortion correction process was included. \r<br/>','|MPS amended to include the intermediate aging and intermediate distortion correction process after the roughing operation.\r<br/>','Next batched produced according to the revised process and the delta FAI was found ok. \r\n','C67557','2019-01-28','qas_sez(a)','qas_sez(a)','GLB406814','2019-01-28','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER 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. \r\n','Z3456','qas_sez|','2019-04-17|','2019-04-17',NULL,NULL,NULL,NULL,NULL,NULL),(11469,'35A-475A','Saab AB','FRAME ASSY','','D5227338400100','','B',2,'OWED-LTA-001','','A15686','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Parts don\'t meet the flatness tolerance 0,4 mm.\r\nShould be: The parts should be in the flatness tolerance 0,4 mm.','1) Bend occurred on the part during roughing operation and was not removed in- between operations.\r\n|2) Due low thickness finish from high thickness RM the machining strategy caused the material to deform and no intermediate correction was given.\r\n|3) Intermediate correction for the bend removal and aging was not considered during the processing of these pars.\r\n|4) usually aging and intermediate distortion correction are done for the parts longer than 1m length.\r\n','|All the semi-finished parts were left for aging and intermediate distortion correction process was included. \r<br/>','|MPS amended to include the intermediate aging and intermediate distortion correction process after the roughing operation.\r<br/>','Next batched produced according to the revised process and the delta FAI was found ok. \r\n','C66146','2019-01-28','qas_sez(a)','qas_sez(a)','GLB406814','2019-01-28','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER END','yes','Misc','qas_sez(a)','no','','|Immediately collected all the parts from customer and stopped the production line and checked the machining completed parts and separated the deformed pats. \r\n','Z3456','qas_sez|','2019-04-17|','2019-04-17',NULL,NULL,NULL,NULL,NULL,NULL),(11470,'35A-475A','Saab AB','FRAME ASSY','','D5227338400100','','B',13,'1600214688','','A17267','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Parts don\'t meet the flatness tolerance 0,4 mm.\r\nShould be: The parts should be in the flatness tolerance 0,4 mm.','1) Bend occurred on the part during roughing operation and was not removed in- between operations.\r\n|2) Due low thickness finish from high thickness RM the machining strategy caused the material to deform and no intermediate correction was given.\r\n|3) Intermediate correction for the bend removal and aging was not considered during the processing of these pars.\r\n|4) usually aging and intermediate distortion correction are done for the parts longer than 1m length.\r\n','|All the semi-finished parts were left for aging and intermediate distortion correction process was included. \r<br/>','|MPS amended to include the intermediate aging and intermediate distortion correction process after the roughing operation.\r<br/>','Next batched produced according to the revised process and the delta FAI was found ok. \r\n','C67557','2019-01-28','qas_sez(a)','qas_sez(a)','GLB406814','2019-01-28','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER 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. \r\n','Z3456','qas_sez|','2019-04-17|','2019-04-17',NULL,NULL,NULL,NULL,NULL,NULL),(11471,'35A-475A','Saab AB','FRAME ASSY','','D5227338400100','','B',2,'OWED-LTA-001','','A15392','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Parts don\'t meet the flatness tolerance 0,4 mm.\r\nShould be: The parts should be in the flatness tolerance 0,4 mm.','1) Bend occurred on the part during roughing operation and was not removed in- between operations.\r\n|2) Due low thickness finish from high thickness RM the machining strategy caused the material to deform and no intermediate correction was given.\r\n|3) Intermediate correction for the bend removal and aging was not considered during the processing of these pars.\r\n|4) usually aging and intermediate distortion correction are done for the parts longer than 1m length.\r\n','|All the semi-finished parts were left for aging and intermediate distortion correction process was included. \r<br/>','|MPS amended to include the intermediate aging and intermediate distortion correction process after the roughing operation.\r<br/>','Next batched produced according to the revised process and the delta FAI was found ok. \r\n','C65527','2019-01-28','qas_sez(a)','qas_sez(a)','GLB406814','2019-01-28','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER END','yes','Misc','qas_sez(a)','no','','|Immediately collected all the parts from customer and stopped the production line and checked the machining completed parts and separated the deformed pats. \r\n','Z3456','qas_sez|','2019-04-17|','2019-04-17',NULL,NULL,NULL,NULL,NULL,NULL),(11472,'51-145A','THE BOEING COMPANY','CLEVIS - UPPER, RH THREAD','534-20180618','112A7112-612','NA','PSDL REV B',1,'BOEING 001AA','','86172','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','CHATTERING ON THREAD','1) Improper thread formation during the thread rolling operation.|2) Thread rolling tool struck to the groove at the end of first pass.|3) Thread length was not defined.','|Removed the thread rolling tool from the part and provided the length after of the thread formation after discussion with the engineering team.','|Process is frees-ed to a fixed length of thread length.','Next batches produced found ok.','','2019-01-28','pe_sez(a)','Ravi Kumar G.B,Nagaraju P K ,Dinakar K ,','','0000-00-00','CHATTERING ON THREAD','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','yes','With Treatment','','FI','no','200MY-01','qas_sez(a)','no','','|Immediately stopped the machine and informed the engineering team and the maintenance team.','Z3456','qas|','2019-05-17|','2019-05-17',NULL,NULL,NULL,NULL,NULL,NULL),(11473,'51-183','THE BOEING COMPANY','ADAPTER, BULKHEAD - ALUMI','MA20172644','272U0021-3','NA','PSDL REV A',1,'BOEING 001Z','','85888','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Running Time Part Rotated ID and OD dig mark fond.','1) Due to Insufficient clamping force the part got rotated.|2) Chuck pressure was low.','|Increased the chuck pressure and continued the production.','|Informed the operators to not to change the chuck pressure without supervision of senior operator.','CA PA Found ok.','','2019-01-29','Narasimhamurthy(K.G.)','Anil(S)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','01','no','Misc','Narasimhamurthy(K.G.)','no','','|Immediately stopped the machine and informed the supervisor','E3456','qas|','2019-04-26|','2019-04-26',NULL,NULL,NULL,NULL,NULL,NULL),(11474,'35-604','Saab AB','SHAFT , VENT HOOKS','5084','D5227352920200','NA','PART ISSUE B',1,'OWED-LTA-004','','86416','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','OUTER DIA UNDERSIZED BY 0.12','WRONG OFFSET ENTERED DURING THE CORRECTION OF THE OUTER DIA.','|SUPERVISOR HAS TO CROSSCHECK AND ENSURE THE OPERATOR HAS ENTERED THE CORRECT OFFSET VALUE.','|SUPERVISOR HAS TO CROSSCHECK AND ENSURE THE OPERATOR HAS ENTERED THE CORRECT OFFSET VALUE.','CAPA FOUND SATISFACTORY.','','2019-01-29','Dinakar K()','Dinakar K()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Dinakar K()','no','','|OUTER DIA CHECKED AND FOUND UNDERSIZE BY 0.12MM THEN CROSS CHECKED THE OFFSET VALUE WHICH WAS FOUND WRONG AND CORRECTED THE OFFSET VALUE.','Z3456','qas_sez|','2019-02-13|','2019-02-13',NULL,NULL,NULL,NULL,NULL,NULL),(11475,'35-597','Saab AB','CORNER','755356','D5227338620200','NA','PART ISSUE B',1,'1600214688','','79698','','0000-00-00',NULL,'yes','no','yes','no','yes','no','no','no','no','profile dig upto 1mm (AT SEZ MAZZAK I-700 MACHINE) ','','','','','','2019-01-30','prodn_aero(prodn)','prodn_aero(prodn)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','no','yes','no','With Treatment','','05','no','Misc','Ravi nayak()','no','','','A3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11476,'35-598','Saab AB','CORNER','548051A','D5227338620300','NA','PART ISSUE B',1,'PA1687 LTA-1','','82635','','0000-00-00',NULL,'yes','no','yes','no','yes','no','no','no','no','Profile Dig of 1mm (AT SEZ MAZZAK I-700 MACHINE)','','','','','','2019-01-30','prodn_aero(prodn)','prodn_aero(prodn)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','no','yes','no','With Treatment','','PRODUCTION','no','Misc','Ravi nayak()','no','','','A3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11477,'47-198','GKN Aerospace Filton','BRACKET M/C','560504A3','F57555655201','NA','PART ISSUE B',1,'GKN-GS-068 PHASE2- L','','85282','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Bore over size by 0.23mm','drill was loaded in the hole mill dia 15.75 tool post|during drilling program instead of drill hole mill was runned |operator qas not aware of tool interchanged  ','|1. the tool was replaced in the correct post qa per program and run the production \r<br/>2.M00 was called in prpgram to check tool.','|1. separate tool will be used pertaining to the part\r<br/>2. dame dimension of the part will be loaded for machine easily   the available of the tool ','CA AND PA found satisfactory ','','2019-01-31','pe_sez(a)','Raghu(B)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','pe_sez(a)','no','','|1. the parts was identified and separated \r\n2. all the tool was recalled and checked once again \r\n3. NCR was raised','Z3456','qas_sez|','2019-02-13|','2019-02-13',NULL,NULL,NULL,NULL,NULL,NULL),(11478,'35-601','Saab AB','FRAME','532793B','D5227338520600','NA','PART ISSUE C',1,'OWED-LTA-001','','87353','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','BASE THICKNESS UNDER SIZE REQUIRED 1.6+/-0.2 MM MEASURED 1.2 MM','1) Due to excess bend on the part after roughing operation part lifted and resulted in thickness under-size|2) During the final pass in finishing operation due to residual stress the part is getting lifted up.|3) During aging time between the roughing and the finishing operation the material was not left in free condition (i.e. the materials were loaded one over the other).','|Informed all the operators to leave the part in free condition during the aging process. ','|Training provided to all the operators on site to avoid storage of parts one above the other during the aging operation. ','CA PA found ok.','','2019-01-31','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','08','no','Misc','Yashawantha(NH)','no','','|Immediately stopped the machine and arranged the material so that the parts are left in free condition.','E3456','qas|','2019-01-31|','2019-01-31',NULL,NULL,NULL,NULL,NULL,NULL),(11479,'56-092','GKN Aerospace Orangeburg','CLEVIS FTG FWD','279131B7','119A1215-603','NA','PSDL REV A',1,'A000047469','','86946','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','WHEN RE ENGG TIME, THE TOOL HOLDER DIG MARK ON THE FLANGE OF THE PART','PROGARAM POST ERROR IN SOLID CAM 5 AXIS','|PROGRAMM WAS RECHECKED AND CORRECTED FOR THE ERROR CAUSED','|THE PROGRAM WILL BE CROSS CHECKED BY THE SENIOR PROGRAMMER BEFORE LOADING TO THE MACHINE.\r<br/>REQUESTED FOR THE G CODE SIMULATOR.\r<br/>','CAPA FOUND SATISFACTORY','','2019-01-31','pe_sez(a)','Chethan Kumar M,','','0000-00-00','NC BY ENGG DEPT','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','3','no','i700-1','pe_sez(a)','no','','|MACHINE WAS STOPPED \r\nINFORMED TO THE PROGRAMMER','Z3456','qas_sez|','2019-02-14|','2019-02-14',NULL,NULL,NULL,NULL,NULL,NULL),(11480,'35-531A','Saab AB','SHAFT LATCH','B90458','D5227349020200','NA','PART ISSUE C',1,'OWED-LTA-002','','83188','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','FACE DIG MARK','THE OPERATOR HAS INPUT THE WRONG OFFSET VALUE.\r\n','|THE OPERATOR WAS TRAINED AND ADVISED TO DOUBLE CHECK THE INPUT VALUE IT WILL BE CROSSCHECKED BY THE SENIOR OPERATOR.','|THE OPERATOR WAS TRAINED AND ADVISED TO DOUBLE CHECK THE INPUT VALUE IT WILL BE CROSSCHECKED BY THE SENIOR OPERATOR.','CAPA FOUND SATISFACTORY.','','2019-01-31','Dinakar K()','Siddesha Y.V,Sagar C.V,Maruthi ,Dinakar K ,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','5','no','200MY-01','Dinakar K()','no','','|THE MACHINE WAS STOPPED AND INFORMED TO THE SUPERVISOR.\r\nTHE WORK OFFSET AND OTHER PARAMETERS WERE CHECKED AND FOUND THAT THE OFFSET VALUE ENTERED WAS WRONG AND CORRECTED THE VALUE.','Z3456','qas_sez|','2019-02-14|','2019-02-14',NULL,NULL,NULL,NULL,NULL,NULL),(11481,'35-227A','Saab AB','HINGE BRACKET 2','5881601 1','D576 50005 204','','D00',1,'1600223433/Forecast ','','83574','','0000-00-00',NULL,'yes','yes','yes','','','','','','','TOTAL LENGTH UNDERSIZE','PART WRONG LOADING |THERE IS NO PROPER FIXTURE TO LOCK AND IDENTIFY THE CORRECT LOADING OF THE PART.','|PART WILL BE LOCKED IN THE FIXTURE WITH TWO MORE EXTRA LOCATING PINS SO THAT PART CANNOT BE LOADED WRONGLY.','|PART WILL BE LOCKED IN THE FIXTURE WITH TWO MORE EXTRA LOCATING PINS SO THAT PART CANNOT BE LOADED WRONGLY.','FOR THE NEXT PRODUCTION BATCH THE IMPLIMENTATION OF THE ABOVE SAID ACTION WILL BE DONE AND WILL BE VERIFIED BY THE QUALITY ENGINEER. \r\n','','2019-02-01','pe_sez(a)','        Madhu Kumar N','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','03','','','','','','|MACHINE WAS STOPPED AND  INFORMED TO THE SUPERVISOR','Z3456','pe_sez|qas_sez|','2019-02-01|2019-02-13|','2019-02-13',NULL,NULL,NULL,NULL,NULL,NULL),(11482,'35-577A','Saab AB','SHAFT','C86483','D5227344120000','NA','PART ISSUE B',73,'OWED-LTA-004','','78552','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','yes','corrosion observed.','REFER NC NO 11424|REFER NC NO 11424|REFER NC NO 11424|REFER NC NO 11424|REFER NC NO 11424','|REFER NC NO 11424','|REFER NC NO 11424','REFER NC NO 11424','C70611','2019-02-01','qas_sez(a)','qas_sez(a)','GLB404928','2018-12-21','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','DN47113','Custemer 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),(11483,'35-430','Saab AB','BEAM','9274601','D522 73383 200 00','','A',12,'OWED-LTA-001','','86496','','0000-00-00',NULL,'yes','no','no','no','yes','yes','no','no','no','THICKNESS PLUS. MAXIMUM VALUE 1.8 MEASURED VALUE 1.83/1.89\r\n','1)Re-engineering process.|2)Change in tool path.|3)Finishing operation carried in one tool pass but earlier it was 2 pass.|4)Machine center changed from Mazak to HMC.','|1)Verified and changes was made in the program on the finishing operation related to tool path to avoid eliminate the stock.\r<br/>2)Training and awareness was provided to operator on checking of parts in different area of parts which will covers all the part flange/rib to ensure thickness is same in all flange/rib within the limit.\r<br/>','|1)Verified and changes was made in the program on the finishing operation related to tool path to avoid eliminate the stock.\r<br/>2)Training and awareness was provided to operator on checking of parts in different area of parts which will covers all the part flange/rib to ensure thickness is same in all flange/rib within the limit.\r<br/>','CA/PA found ok.','','2019-02-01','pe_sez(a)','Vijay Kumar H.J,Thaveni D M ,Karthik Raj T ,','','0000-00-00','THICKNESS PLUS. MAXIMUM VALUE 1.8 MEASURED VALUE 1.83/1.89\r\n','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Cancelled','no','no','no','With Treatment','','FI','yes','a51nx-01','qas_sez(a)','no','','|1)Re-Inspected all the WIP quantities.\r\n2)NCR raised for re-work process.\r\n','Z3456','qas_sez|','2019-02-12|','2019-02-12',NULL,NULL,NULL,NULL,NULL,NULL),(11484,'47-172','GKN Aerospace Filton','TEE PANEL SUPPT BEAM','2361201-2','F5755034220501','NA','PART ISSUE D',1,'GKN-GS-068 PHASE2- L','','87394','','0000-00-00',NULL,'yes','no','no','no','yes','yes','no','no','no','HOLE SIZE OVER SIZE MAXIMUM VALUE 8.08 MEASURED VALUE IS 8.15. HOLE MEASURED 0.07 PLUS ','No sufficient coolant during cutting the material |During Finish Operation ,the chips clocked in the tool|for finishing operation the stock was more due to which extra material was removed and the chips was clocked in the tooL','|M00 was added in the program during finishing to cross check if chips any in the tool and clean.\r<br/>2.the same was instructed to the operator to do .','|REFER ca','next part in this work order was setted and the hole size found within limits','','2019-02-02','pe_sez(a)','Somashekar ,Raghu B,','','0000-00-00','HOLE SIZE OVER SIZE MAXIMUM VALUE 8.08 MEASURED VALUE IS 8.15. HOLE MEASURED 0.07 PLUS ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','Slim3n-4AHS-3','qas_sez(a)','no','','|1.The tool was recalled and the cleaned thoroughly and removed the chips\r\n2.the devation part was rejected and NCR was raised','Z3456','qas_sez|','2019-04-24|','2019-04-24',NULL,NULL,NULL,NULL,NULL,NULL),(11485,'18-392B','Magellan Aerospace(Polska) Sp','END COVER','19278','D278 50167 200','','D',1,'104569','','86871','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','THICKNESS UNDER SIZE BY -0.23MM.','1)Total thickness of the part got undersize.|2) The Raw material was in the undersize to the required minimum dimension due to which the  thickness got undersized at the finishing.|3) Due to cross cutting of the RM the thickness got undersized and the operator only checked the first two pieces and since they were in nominal value he loaded the remaining pieces without inspecting.','|Checked all the finished parts and RM and continued the production since all the RM were found ok.','|Informed all the operators to check the thickness of the RM before loading to machine and return the undersized RM back to the store','CAPA found ok.','','2019-02-02','Dinakar K()','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Ravi(M)','no','','|Immediately stopped the machine and checked the total length of all the remaining RM and found Ok.\r\nChecked the finished parts and the thickness was found ok.','E3456','qas|','2019-02-07|','2019-02-07',NULL,NULL,NULL,NULL,NULL,NULL),(11486,'56A-092','','','','','','',0,'','','','','0000-00-00',NULL,'no','no','no','no','no','no','no','no','no','','','','','','','2019-02-04','select','','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Cancelled','no','no','no','','','','no','','select','no','','','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11487,'56A-092','GKN Aerospace Orangeburg','CLEVIS FTG ASSY FWD','','119A1215-601','','PSDL REV A',1,'A000047469','','A22186','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','BUSH DIAMETER OVER SIZE','No sufficient coolant during cutting the material \r\n|During Finish Operation ,the chips clocked in the tool\r\n|for finishing operation the stcok was more due to which extra material was removed and the chips was clocked in the tool \r\n|Operator didn’t notice the chipes and didn’t remove it.\r\n','|1.M00 was added in the program during finishing to cross check if chips any in the tool and clean.\r<br/>2.the same was instructed to the operator to do .\r<br/>','|REFER CA','NEXT PART IN THIS WORKORDER WAS SETTED AND THE BORE FOUND WITHIN THE LIMITS','','2019-02-04','pe_sez(a)','pe_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Assembly','','5','no','Misc','pe_sez(a)','no','M09849|BACB28AP10Z047','|1.The tool was recalled and the cleaned througly and removed the chips\r\n2.the devation part was rejected and NCR was raised\r\n','Z3456','qas_sez|','2019-04-24|','2019-04-24',NULL,NULL,NULL,NULL,NULL,NULL),(11488,'56A-092','GKN Aerospace Orangeburg','CLEVIS FTG ASSY FWD','','119A1215-601','','PSDL REV A',6,'A000047469','','A22186','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','BUSH DIAMETER OVERSIZE','REFER NCR 11487|REFER NCR 11487|REFER NCR 11487','|REFER NCR 11487','|REFER NCR 11487','REFER NCR 11487','','2019-02-04','pe_sez(a)','op_sez(s)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Assembly','','5','no','Misc','pe_sez(a)','no','M09851|BACB28AT10B047Z','|REFER NCR 11487','Z3456','qas_sez|','2019-04-24|','2019-04-24',NULL,NULL,NULL,NULL,NULL,NULL),(11489,'35-588','Saab AB','LOCK SECTOR','532747A','D5227349920200','NA','PART ISSUE C',1,'OWED-LTA-003','','82045','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','PART OD UNDER SIZE BY 0.040MM . AND ID UNDER SIZE BY 0.6MM . NOMINAL DIMENSION OF ID IS 12.7 . AND JAW MARKS FOUND ON THE PART ','THE PART WAS HELD IN THE JAW WITH MORE PRESSURE THAN THE REQUIRED.|THE OPERATOR WAS NOT AWARE OF THE CHUCK PRESSURE.','|TRAINING GIVEN TO THE OPERATORS TO CREATE AWARENESS ON THE CHUCK PRESSURE AND OTHER MACHINE PARAMETERS.','|IN FUTURE THE CHUCK PRESSURE TO BE MAINTAINED WILL BE  MENTIONED IN THE MPS.','CAPA FOUND SATISFACTORY','','2019-02-04','pe_sez(a)','Umesh B,Thaveni D M ,Sanjeev S.D,Nataraja C V,NataRaj.CV ,Nagaraju P K ,Karthik Raj T ,HariPrasad ,Diwakar R.B.,Dinakar K ,Chethan Kumar M,Anand ,','','0000-00-00','PART OD UNDER SIZE BY 0.040MM . AND ID UNDER SIZE BY 0.6MM . NOMINAL DIMENSION OF ID IS 12.7 . AND JAW MARKS FOUND ON THE PART ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','200MY-01','qas_sez(a)','no','','|THE MACHINE WAS STOPPED AND INFORMED TO THE SUPERVISOR AND THE CHUCK PRESSURE WAS CORRECTED BY THE SUPERVISOR.\r\nALL THE OTHER PARTS  OF SAME WORK ORDERS WERE CHECKED AND FOUND OK.','Z3456','qas_sez|qas_sez|','2019-02-12|2019-02-14|','2019-02-14',NULL,NULL,NULL,NULL,NULL,NULL),(11490,'56A-101','GKN Aerospace Orangeburg','CLOSEOUT RIB ASSY - AFT, ','','119A1383-602','','PSDL REV -',1,'A000047470','','A22028','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','CSK over size','1.the tool offset taken was recorded wrongly in the Log book and the same was entered into the system\r\n|2.The offset taken was not validated in with the previous one which was recorded in the log book\r\n|3.Operator entered Wrong Tool offset  in the system and did not follow the check list provided for setting.\r\n','|1.Awareness and on job training was given to all the operators on following the check list provided for doing the setting\r<br/>2.Instruction given to all the operators to get the check list approved from the supervisor and senior operators once the setting is done.\r<br/>','|refer ca','Next batched machined and CSK found within the limits .wo# A23446 ,qty 14 nos ','','2019-02-04','pe_sez(a)','pe_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Assembly','','04','no','Misc','pe_sez(a)','no','','|1.The part was rejected and internal NCR was raised.\r\n\r\n2.All the tools pertaining to the program was recalled and new offset was taken.\r\n','Z3456','qas_sez|qas_sez|','2019-05-23|2019-05-23|','2019-05-23',NULL,NULL,NULL,NULL,NULL,NULL),(11491,'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 tool down 2MM so part reject','1) Tool dropped during the running time.|2) Grip screw locking mechanism got affected due to which the tool got loose and dropped during machining.|3) Hydraulic oil flow got blocked due to which the mechanism didn\'t functioned properly ','|Scrapped the affected holder and informed the holder supplier.','|Informed all the operators and supervisors to ensure all tool holders once in a week.','CA PA found ok.','','2019-02-05','Dhananjaya(N)','        Narasimhamurthy C','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','11','','','','','','|Immediately stopped the machine and checked all the tool holders. Replaced the affected holder with new one and continued the production.','E3456','pe|qas|','2019-02-05|2019-02-05|','2019-02-05',NULL,NULL,NULL,NULL,NULL,NULL),(11492,'51A-066A','THE BOEING COMPANY','STRUT SUPPORT ASSY','','113T1958-7','','PSDL REV A',2,'BOEING 001AA','','A21947','','0000-00-00',NULL,'yes','no','yes','no','yes','no','no','no','no','Bore Oversize.','1) Ovality formation inside the bore.|2) Due to run out in the reamer ID oversized due to ovality.|3) Chips were struck inside the holder and operator did not cleaned and noticed the inside of the holder before loading the reamer to it.','|Removed all the chips from the holder and cleaned the Holding area.','|Informed the operator to clean the ID of holder during every tool change and to check the Run out of the tool after the tool change.','CA PA found ok.','','2019-02-05','Karthineyan(V.S.)','Karthineyan(V.S.)','','0000-00-00','bore over size','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Assembly','','in process','no','Misc','Karthineyan(V.S.)','no','M03806|BACB28AT06B011Z','|Immediately stopped the machine and checked the run out of the reamer and cleaned the holding area.','E3456','qas|','2019-04-26|','2019-04-26',NULL,NULL,NULL,NULL,NULL,NULL),(11493,'51-197','THE BOEING COMPANY','END FITTING-','20233630','3-48675-901','NA','PSDL REV -',1,'BOEING 001AA','','85165','','0000-00-00',NULL,'yes','no','yes','no','yes','no','no','no','no','Thread problem(ID),ID thread dig mark found because of electricity problem.','WHEN ELECTRICITY DROPPED AIR PRESSURE WILL BE LOST SO THAT TIME MACHINE WILL BE STOPED WAIL RUNNING . ','','','INFORMED TO MAINTENANCE DEPARTMENT ','','2019-02-05','Dinakar K()','Dinakar K()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','pe_sez(a)','no','','','Z3456','pe_sez|qas_sez|','2019-02-05|2019-02-13|','2019-02-13',NULL,NULL,NULL,NULL,NULL,NULL),(11494,'51-135A','THE BOEING COMPANY',' 	CLEVIS - UPPER, RH THRE','H29007','112A7112-3','NA','PSDL REV B',1,'BOEING 001AA','','87191','','0000-00-00',NULL,'yes','no','yes','no','yes','no','no','no','no','Double thread found because of electricity problem','WHEN ELECTRICITY DROPPED  AIR PRESSURE WILL BE LOST SO THAT TIME MACHINE WILL BE STOPED ','','','INFORMED TO MAINTENANCE DEPARTMENT  ','','2019-02-05','Dinakar K()','Dinakar K()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','pe_sez(a)','no','','','Z3456','qas_sez|','2019-02-13|','2019-02-13',NULL,NULL,NULL,NULL,NULL,NULL),(11495,'35-415','Saab AB','SHAFT LATCH LINK','M794860','D522 73496 200 00','','A',1,'OWED-LTA-004','','87190','','0000-00-00',NULL,'yes','no','yes','no','yes','no','no','no','no','Tool dig mark found on OD because of electricity problem.','WHEN ELECTRICITY DROPPED AIR PRESSURE WILL BE LOST AND MACHINE WILL BE STOPED  WAIL RUNNING ','','','INFORMED TO MAINTENANCE DEPARTMENT ','','2019-02-05','Dinakar K()','Dinakar K()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','pe_sez(a)','no','','','Z3456','qas_sez|qas_sez|','2019-02-13|2019-02-13|','2019-02-13',NULL,NULL,NULL,NULL,NULL,NULL),(11496,'18-075A','Magellan Aerospace Wrexham','ADAPTOR','M037890/27097','D282 50044 200PF','','A',1,'175162','','84010','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','thickness undessized.','Part not properly but to fixture. Due to burr on fixture. Operator has not effectively cleaned the fixture','||Operator has been trained to double check for burr or any other particles on the fixture.','|Feeler gauge is used to check the proper butting of the part on the fixture.','After the introduction of the feeler gauge to ensure proper butting of the part on the fixture the parts produced were checked and found ok.\r\nCAPA found satisfactory.','','2019-02-05','Dinakar K()','Manu K,Dinakar K ,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','1','no','100MY-02','Dinakar K()','no','','|Machine was stooped and informed to the supervisor.\r\nprevious produced parts were checked and found ok.','Z3456','qas_sez|','2019-02-14|','2019-02-14',NULL,NULL,NULL,NULL,NULL,NULL),(11497,'35-415','Saab AB','SHAFT LATCH LINK','M789340','D522 73496 200 00','','A',1,'OWED-LTA-004','','83881','','0000-00-00',NULL,'yes','yes','yes','','','','','','','1NO REJECTED DUE TO CUTTING TOOL PROBLEM DIA(6.2 DRLL).. ','In Op-02 drill 6.2 broken during machining|Process Knowledge on Drilling operation is not adequate|To reduce the cycle time the drilling was performed using directly Finish Drill and Hole mill.|Drilling cycle was not adopted (centre drill/Pre-drill for steel material and cylindrical part)','|Drilling Cycle was re-defined as per drilling operation for steel material','|Refer to CA','Monitored Work order 83880 ,qty 72 nos anfd found no rejection in drilling','','2019-02-05','pe_sez(a)','        Karthik Raj T ','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','07','','','','','','|1.the part was identified and rejected NCR 11479\r\n2.Drill was replaced and tool offset taken\r\n','Z3456','pe_sez|qas_sez|','2019-02-07|2019-04-02|','2019-04-02',NULL,NULL,NULL,NULL,NULL,NULL),(11498,'56-038','GKN Aerospace Orangeburg','CLOSEOUT - RIB, ANTICOLLI','421871','119A1442-604','NA','PSDL REV -',1,'LTA Orangeburg 737 W','','82911','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','8flat program profile dig mark and 6bn program dig mark and 8bn tool brocken part  base thickness - side...','m/c stop ,and old program running','|taken old program','|no dig mark on part','next part found okay','','2019-02-07','pe_sez(a)','op_sez(s)','','0000-00-00','8flat program profile dig mark and 6bn program dig mark and 8bn tool brocken part  base thickness - side...','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','op_sez(s)','no','','|machine stopped','Z3456','qas_sez|','2019-02-07|','2019-02-07',NULL,NULL,NULL,NULL,NULL,NULL),(11499,'47-188','GKN Aerospace Filton','BRKT JACK MTG (INNER)','1750033421','F5755203020101','NA','PART ISSUE A',1,'1210042824-1','','86415','','0000-00-00',NULL,'yes','no','no','no','yes','yes','no','no','no','TOOL DIG AND WALL HEIGHT UNDER SIZE BY 1.2MM ','WAIL RUNNING TOOL WAS BROKEN AND DIG MARK FOUND ON THE PART|IN PROGRAM DEPTH OF CUT WAS GIVEN 4MM SO THAT PART WAS BROKEN|DUE TO DIG MARK PART .  TOTAL HEIGHT WAS MINUS TO 1.2MM ','|1. TOOL AND HOLDER WAS REPLACED WITH NEW ONE \r<br/>2. PROGRAM WAS EDITED WITH ENGINEERING \r<br/>\r<br/> ','|1. BASED ON THE TOOL STRENGTH DEPTH OF CUT SHOULD BE GIVEN \r<br/>2. SUPERVISOR SHOULD CROSS CHECK THE PROGRAM BEFORE RUNNING ','CA & PA FOUND SATISFACTORY ','','2019-02-07','pe_sez(a)','Madhu Kumar N,Lohith K,Kiran KM,','','0000-00-00','TOOL DIG AND WALL HEIGHT UNDER SIZE BY 1.2MM ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','Slim3n-4AHS-1','qas_sez(a)','no','','|1. STOPPED THE MACHINE \r\n2. CROSS CHECKED THE PROGRAM \r\n3. INSPECTED PREVIOUS PART \r\n4. INFORMED TO SENIOR ','Z3456','qas_sez|','2019-02-13|','2019-02-13',NULL,NULL,NULL,NULL,NULL,NULL),(11500,'35-234A','Saab AB','HINGE BRACKET 5 ','2106701 3','D576 50008 209','','D00',1,'1600223433/Forecast ','','86855','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Slot over size ','1) Due to tool outrun the slot got oversize.|2) Chips got clogged between the tool pocket during the tool changed and resulted in tool run out.|3) Due to pressure drop in the flush nozzle of the machine the chips didn\'t got removed completely.','|Informed all the operator to check proper flush out of chips and machine air pressure.','|Informed the operators to check the air pressure in machine every day before starting the machine.','CA PA found ok.','','2019-02-07','Dinesh kulal()','Dinesh kulal()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','Production','no','Misc','Dinesh kulal()','no','','|Immediately stopped the machine and cleaned all the tool holding area and continued the production.','A3456','qas|','2019-02-11|','2019-02-11',NULL,NULL,NULL,NULL,NULL,NULL),(11501,'56-038','GKN Aerospace Orangeburg','CLOSEOUT - RIB, ANTICOLLI','421871','119A1442-604','NA','PSDL REV -',1,'LTA Orangeburg 737 W','','82911','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','8flat program profile dig mark and 6bn program dig mark and 8bn tool brocken part  base thickness - side...','m/c stop ,and old program running','old program taken for running','No dig mark on profile.','next part found okay','','2019-02-07','pe_sez(a)','op_sez(s)','','0000-00-00','8flat program profile dig mark and 6bn program dig mark and 8bn tool brocken part  base thickness - side...','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','op_sez(s)','no','','MACHINE STOPPED','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11502,'35A-353A','Saab AB','LIFT PIN HOUSING FWD','','423Z1124-5-52','','1',1,'LTA SAAB B787 Assemb','','A21976','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Bore over size','REFER NCR 11488|REFER NCR 11488|REFER NCR 11488','|REFER NCR 11488','|REFER NCR 11488','REFER NCR 11488','','2019-02-07','pe_sez(a)','Nagaraju P K()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','Assembly','','06','no','Misc','pe_sez(a)','no','M07880|BACB28AP20Z253','|REFER NCR 11488','Z3456','pe_sez|qas_sez|qas_sez|','2019-02-07|2019-02-07|2019-04-24|','2019-04-24',NULL,NULL,NULL,NULL,NULL,NULL),(11503,'35A-357A','Saab AB','Latch Actuator Support Fi','','423Z1225-1-50','','---',1,'LTA SAAB B787 Assemb','','A21989','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','bore Over size','No sufficient coolant during cutting the material \r\n|During Finish Operation ,the chips clocked in the tool\r\n|for finishing operation the stock was more due to which extra material was removed and the chips was clocked in the tool \r\n|Operator didn’t notice the chips and didn’t remove it.\r\n','|1.M00 was added in the program during finishing to cross check if chips any in the tool and clean.\r<br/>2.the same was instructed to the operator to do .\r<br/>','|REFER CA','NEXT PART IN THIS WORKORDER WAS SETTED AND THE BORE FOUND WITHIN LIMITS','','2019-02-07','pe_sez(a)','Nagaraju P K()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','Assembly','','06','no','Misc','pe_sez(a)','no','M03637|BACB28AT14B034Z','|1.The tool was recalled and the cleaned thoroughly and removed the chips\r\n2.the devation part was rejected and NCR was raised\r\n','Z3456','pe_sez|qas_sez|qas_sez|','2019-02-07|2019-02-07|2019-04-24|','2019-04-24',NULL,NULL,NULL,NULL,NULL,NULL),(11504,'56-006','GKN Aerospace Orangeburg','SPLICE PLATE FWD UPR','8-22-05419/26172','119A1213-604','NA','PSDL REV -',2,'LTA GKN 737 Winglet','','86246','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','during 5 axis program posting problem due to operation was shifted.','during 5 axis program cad posting problem due to operation was shifted.\r\n','inform to cad department and modify the individual programes. ','inform to cad department and modify the individual programes.','CAD DEPARTMENT SOLVED  THE PROBLEM AND NEXT BATCH PRODUCTION  FOUND OK ','','2019-02-07','pe_sez(a)','pe_sez(a)','','0000-00-00','during 5 axis program posting problem due to operation was shifted.','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','pe_sez(a)','no','','','Z3456','qas_sez|','2019-02-13|','2019-02-13',NULL,NULL,NULL,NULL,NULL,NULL),(11505,'35A-357A','Saab AB','Latch Actuator Support Fi','','423Z1225-1-50','','---',1,'LTA SAAB B787 Assemb','','A21989','','0000-00-00',NULL,'yes','no','yes','no','yes','no','no','no','no','Bush ID oversize','No sufficient coolant during cutting the material |During Finish Operation ,the chips clocked in the tool|for finishing operation the stock was more due to which extra material was removed and the chips was clocked in the tool |Operator didn’t notice the chips and didn’t remove it.','|1.M00 was added in the program during finishing to cross check if chips any in the tool and clean.\r<br/>2.The same was instructed to the operator to do .','|refer CA','Next part in this workorder was setted and the bore diameter found within the limits','','2019-02-07','Karthineyan(V.S.)','Karthineyan(V.S.)','','0000-00-00','bush id oversize','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','in process','yes','Misc','Ramesh(D)','no','M03637|BACB28AT14B034Z','|1.The tool was recalled and the cleaned thoroughly and removed the chips\r\n2.the devation part was rejected and NCR was raised','Z3456','qas_sez|qas_sez|','2019-04-16|2019-04-24|','2019-04-24',NULL,NULL,NULL,NULL,NULL,NULL),(11506,'35A-353A','Saab AB','LIFT PIN HOUSING FWD','','423Z1124-5-52','','1',1,'LTA SAAB B787 Assemb','','A21976','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Bore Undersize.','During continuous milling boring operation tool wear out occurred |Due to that tool wear out bore under-size occurred','|Every parts boring dimension is checking machining itself which is avoiding rework','|Every parts boring dimension is checking machining itself which is avoiding rework','CAPA FOUND OK','','2019-02-07','Gurukiran S(M)','Gurukiran S(M)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','in procces','yes','Misc','Gurukiran S(M)','no','M07880|BACB28AP20Z253','|The next part boring process boring dimensions to be re arranged and found ok ','Z3456','pe|qas|qas|','2019-02-08|2019-05-17|2019-05-17|','2019-05-17',NULL,NULL,NULL,NULL,NULL,NULL),(11507,'35-407','Saab AB','BEAM 3','2323601','D522 73396 200 00','','A',2,'OWED-LTA-001','','82007','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','Modeling problem','in one billet two parts are production done|because of the program mirror problem LH part production has done  ','|1. changed the program \r<br/>2. cross checking the program by supervisor      \r<br/>','|1. programmer should cross check the program before giving the  \r<br/>  program to the production.  ','next batch production found ok ','','2019-02-09','CAD(sez)','Mahesh(N)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','05','no','Misc','pe_sez(a)','no','','|1. parts inspection has been done  found the problem\r\n2.  informed to the supervisor \r\n3. checked the program \r\n4. informed to the programmer \r\n5. part rejected NCR has been raised ','Z3456','qas_sez|','2019-02-13|','2019-02-13',NULL,NULL,NULL,NULL,NULL,NULL),(11508,'35-596','Saab AB','LEVER','532795E','D5227350820300','NA','PART ISSUE C',2,'OWED-LTA-003','','80995','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Tool dig mark..','Running time tool broken.|Due to improper step over residue from the previous operation the carbide tool got broken while guiding for the next operation|chattering occurred due to worn out tool.','|Informed all the operators to Ensure the insert and cutting edges of the tools before starting the cycle.','|Tool life will be closely monitored.','CA PA found ok.','','2019-02-09','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','01','no','Misc','Prashanth Kumar(M)','no','','|Immediately stopped the machine informed the supervisor and changed the affected tools.','E3456','qas|','2019-04-23|','2019-04-23',NULL,NULL,NULL,NULL,NULL,NULL),(11509,'18-415B','Magellan Aerospace(Polska) Sp','ACTUATOR HOUSING','M084340/28588A','D278 50163 201','','D',1,'104569','','86890','','0000-00-00',NULL,'yes','yes','yes','','','','','','','running time m10 bolt broken part rotate so part reject','1) Due to excess tightening of bolt the bolt got broken and the clamping got loosed during the running time.|2) Due to manual tightening of bolt based the skill of operator the load applied on the bolt differed and resulted in excess tightening.|3) Torque limit was not set and was not practiced.','|Used new bolt and continued the production.','|1) M8 Bolt made of SS material will be dedicated for this part.\r<br/>2) Bosch Torque gun machine will be used to clamp the parts using bolts.','Threading in the fixture changed to M8 bolt immediately and torque Guns for 10 Machines has been ordered.','','2019-02-10','Anjinamurthy(H)','        Patel Appaaji','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','5','','','','','','|Ensured all the bolts for any wear or cracks and checked all the completed parts and found ok.','E3456','pe|qas|','2019-02-11|2019-02-12|','2019-02-12',NULL,NULL,NULL,NULL,NULL,NULL),(11510,'35-182B','Saab AB','EDGE HOUSING','9417060','423Z1121-5-02','','--B',1,'Forecast po for B787','','87067','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Outer profile dig up to 1mm.','','','','','','2019-02-11','Dinesh kulal()','Dinesh kulal()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','no','yes','no','With Treatment','','09','no','Misc','Dinesh kulal()','no','','','A3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11511,'18-090A','Magellan Aerospace(Polska) Sp','BUSH','1670510-3/YT2N','PID278 50164 200','','A',11,'104569','','84860','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','OD UNDER SIZE BY -0.02MM.','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.','','2019-02-12','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','03','no','Misc','Ravi(M)','no','','|Immediately stopped the machine and checked the previously running parts and separated the parts that were undersized.','E3456','qas|','2019-04-08|','2019-04-08',NULL,NULL,NULL,NULL,NULL,NULL),(11512,'47-143','GKN Aerospace Filton','STIFFENER 6 TOP SKIN','8870501-1','D57250497202','NA','PART ISSUE H',1,'GKN-GS-068 PHASE2- L','','87975','','0000-00-00',NULL,'no','yes','yes','no','no','no','yes','no','no','program problem so profile dig','1) Outer profile cut out due to program fault.|2) Outer profile line selection is wrong.|3) simulation is not done after taking the outer profile line. ','|Simulation will be done after taking the Template.  ','|Before Posting the program simulation will be done by another seiner Eng cross checked. ','CAPA found ok.','','2019-02-12','Ramesh(Poojary)','Sathisha(K.C.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','3','no','Misc','Subramanya L(Naik)','no','','|Immediately stop the machine and inform the Eng team.','E3456','qas|qas|','2019-02-15|2019-03-30|','2019-03-30',NULL,NULL,NULL,NULL,NULL,NULL),(11513,'51-041','THE BOEING COMPANY','BRACKET','741161','149A7371-9603','','PSDL REV A',1,'BOEING 001F','','72960','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Thickness 2.54mm Measured as 2.4mm to 2.3mm ','While part running time tool was broken. ','Inform to CAD CAM department change the program level after continue the production. ','Inform and training given to operator check the feed and speed every program. ','Next part found within acceptable limit. ','','2019-02-13','Murali(M)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','DN40824','POST TREATMENT','no','Misc','qas_sez(a)','no','','New tool added and continue the production. ','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11514,'51-161','THE BOEING COMPANY','MACHINED FITTING, AERIAL ','255688B4','349T2200-357','NA','PSDL REV J',1,'BOEING 001Z','','88351','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','orientation problem','the profile was machined in opposite direction in the second operation|there were no defined relation in op-01 to achieve the consistent profile in op-02|the orientation of PCD hole was not defined in op-01 with respect to the square billet,these holes were only used to orient the part in op-02.|the operator could load the part in any direction in op-02|the process was not fool proof in op-02','|1.the orientation of the square billet was defined in the MPS for op-02 \r<br/>2.the orientation of the PCD starting point was defined in op-01','|1.All the hole will be opened out during op-01 to ensure that orientation of the holes will be visible to the operator while loading it to op-02','88351-6 nos,88288-1 no machined and profile is meeting to the requirement.','','2019-02-14','CAD(sez)','CAD(sez)','','0000-00-00','.','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','05','no','Misc','pe_sez(a)','no','','|1.the next part was produced in consistent orientation in op-01.\r\n2.Next part machine, profile was checked and the part was meeting the drawing requirement','Z3456','qas_sez|','2019-02-28|','2019-02-28',NULL,NULL,NULL,NULL,NULL,NULL),(11515,'51-186','THE BOEING COMPANY','ADAPTER, BULKHEAD - ALUMI','20228749','272U0021-6','NA','PSDL REV A',1,'BOEING 001Z','','85882','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','no','supplier did measure the characteristics of the product to verify that product requirements have been met and one of the engineering specification BAC5001-14 section 8.3.1 requirement of check dimensions for the witness markings was missed to properly measure in the boeing part number 272U0021-6 work order number 85882 qty 1.','1) Witness marking done on the part was not as per the requirement.|2) The location Marking dimension mentioned in the drawing was measured deviated on the part.|3) The marking was done manually by using a marking locating tool which got rotated slightly during the marking of rotation, because of which the dimension was not achieved.|4) Operator was not aware about the rotated tool and he did not checked the dimension after the completion of operation.','|Removed the marking from the part and re-marked the witness marking with the help of the tool and re-inspected and found ok.','|Fixed the tool with clay or glue during the marking in order to avoid the rotation of the tool which carrying out the witness marking.','Next batches produced found ok.','','2019-02-14','qas_sez(a)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','DN52311','onsite','yes','Misc','qas_sez(a)','yes','','|Immediately checked the dimension of marking on all the parts in WIP and FG and found ok.','Z3456','qas_sez|','2019-06-06|','2019-06-06',NULL,NULL,NULL,NULL,NULL,NULL),(11516,'35-415','Saab AB','SHAFT LATCH LINK','M789340','D522 73496 200 00','','A',11,'OWED-LTA-004','','83880','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','OD UNDER SIZE. MINIMUM VALUE IS 22.048. MEASURED VALUE IS 21.87 TO 22.032','CLAMPING MARK WAS OBSERVED ON THE OUTER DIA FOR THE LENGTH OF 50MM AND WIDTH OF 3MM AT 3 LOCATIONS ON BOTH THE ENDS OF THE PART.|CLAMPING FORCE WAS HIGH AND THE PART WAS CLAMPPED MANUALLY BY HAND|OPERATOR WAS NOT AWARE OF THE CLAMPING MARK ON THE PART','|1.CLAMPING FORCE WAS REDUCED FOR THE REST OF THE PRODUCTION BATCH.','|1.TORQUE TOOL FOR TIGHTENING THE PART WILL BE PROCURED(DT:22.2.19)\r<br/>2.TORQUE REQUIREMENT FOR THE SPECIFIC BOLTS WILL BE DISPLAYED NEAR ALL THE MACHINE(DT:22.2.19)\r<br/>3.PROCESS WILL BE PLANNED TO TURN MILL SUCH THAT IT WILL NOT BE MACHINED IN THE VMC/HMC(DT:15.4.19) ','work orders 83883,87190 was clamped and machined using the torquing tool and found no rejection due to clamp marks and OD underside','','2019-02-14','pe_sez(a)','Vijay Kumar H.J,Ravi Kumar G.B,Nagaraju P K ,Dinakar K ,Dhanush J.K,','','0000-00-00','FIXTURE HOLDING MARK FOUND ON THE PARTS AND OD UNDER SIZE. MINIMUM VALUE IS 22.048. MEASURED VALUE IS 21.87 TO 22.032','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','a51nx-05','qas_sez(a)','no','','|1.ALL THE PARTS WAS INSPECTED FOR OD AND THE DEVIATION PARTS WAS IDENTIFIED .\r\n2.NCR WAS RAISED FOR THE NON CONFORMING PART','Z3456','|qas_sez|','2019-02-15|2019-04-02|','2019-04-02',NULL,NULL,NULL,NULL,NULL,NULL),(11517,'35-618','Saab AB','SHAFT HANDLE ','M789340','D5227348520200','','PART ISSUE C',8,'OWED-LTA-004','','84104','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','OUTER  DIAMETER UNDER SIZE NOMINAL VALVE 22.1 TOLERANCE -0.05. MEASURED VALVE 21.94 TO 22.04','Chips clotted in the tool while running the finish pass. |There was no sufficient coolant flow on tool to remove the chips during cutting|The coolant nozzle was not aligned on to the cutting tool','|Instruction given to the operator to set the coolant nozzle on to the cutting edge and check weather there is proper flow of coolant while cutting ','|Refer to CA','Next part in this work order machined and entire batch was inspected 100% and OD found within the limits.','','2019-02-15','op_sez(s)','Vijay Kumar H.J,Siddesha Y.V,Ravi Kumar G.B,Nagaraju P K ,Maruthi ,Manu K,Karthik Raj T ,HariPrasad ,Dinakar K ,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','a51nx-05','qas_sez(a)','no','','|1.The part was rejected and internal NCR was raised,\r\n2.The coolant nozzle was aligned on to cutting tool and continued production','Z3456','qas_sez|qas_sez|','2019-02-15|2019-04-17|','2019-04-17',NULL,NULL,NULL,NULL,NULL,NULL),(11518,'35-227A','Saab AB','HINGE BRACKET 2','297136','D576 50005 204','','D00',1,'1600223433/Forecast ','','87480','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Slot width over size up to 0.3mm (Because of Holder Run out)','Holder butting face damage.|Tool holder is not putting properly in the place. |Tool racks are not available sufficiently.','|Load the another tool holder before starting the process and we check run out.','|Tool holder are maintain in the rack only.','CA Pa found ok','','2019-02-15','Ravi nayak()','Ravi nayak()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','2ND','no','Misc','prodn_aero(prodn)','no','','|Immediately stopped the machine and check the tool holder run out ','A3456','qas|qas|','2019-02-19|2019-03-30|','2019-03-30',NULL,NULL,NULL,NULL,NULL,NULL),(11519,'51-087','THE BOEING COMPANY','SHEAR TIE','8-33-09781/26646','481Z2130-15','NA','NIL',1,'BOEING 001N','','84427','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Tool offset wrong.','1) Tool Offset not taken after tool trial.|2) Operator was running two machines continuously and at the same time tool trial was carried out in one machine operator removed the new tool because of poor performance of the new tool and loaded the old tool and started the  cycle.|3) operator taught that offset was taken and he only changed the insert index and continued the production due to fatigue in running two machines and multi tasking.','|1) Next time tool trial will be carried out only in the presence of supervisor.\r<br/>2) Additional operator support will be provided during the tool trial(Tool trial will not be carried out where single operator runs two machines).','|1) Cutting tool test report will be amended to include Tool offset old tool, new tool & again old tool.\r<br/>2) After tool trial single pass of the program will be run in the machine and then the z level will be measured and reported in the Cutting tool test report.','CA Pa found ok.','','2019-02-16','Gurukiran S(M)','SIDDESH ,MANJE GOWDA S,','','0000-00-00','NC','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','5','no','MakinoF3-1','Dhananjaya(N)','no','','|Immediately stopped the machine and checked the offset of the tool and found not taken and re took the tool offset, also cross checked all the other tools in machine and found ok.','E3456','qas|qas|','2019-02-16|2019-03-30|','2019-03-30',NULL,NULL,NULL,NULL,NULL,NULL),(11520,'18-709A','Magellan Aerospace Bournemouth','SHAFT ','A0154U','L57552465200','','A00',1,'425757','','86203','','0000-00-00',NULL,'yes','','yes','','yes','','','','','Dig mark occurred on part  ','During machining process dig mark occurred|Machine stopped suddenly the purpose of power cut occurred|Due to problem on UPS over heat power cut occurred|In UPS room AC was not worked properly','|AC maintenance monitoring record to be create and maintain','|AC maintenance monitoring record to be create and maintain','AC maintenance done and capa found ok. ','','2019-02-17','Raghavendra Rao(R)','        GUNDEGOWDA H.G.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','01','','','','','','|UPS and AC both was checked and maintenance carried out then after that next part was loaded','E3456','pe|qas|qas|','2019-02-18|2019-03-02|2019-03-30|','2019-03-30',NULL,NULL,NULL,NULL,NULL,NULL),(11521,'18-032A','Magellan Aerospace(Polska) Sp','BUSH','1649129-2/WXRL','PID278 50165 200','','A',3,'104569','','86647','','0000-00-00',NULL,'yes','no','no','no','yes','yes','no','no','no','ID UNDERSIZE 0.04-0.15','Rework part mixed up with finished part and reached Quality.|The parts were segregated for ID rework near the machine but were not identified with proper tag.|Due to unclear stock due to worn out insert the ID was not finished and the identification card was not put in place.|Lack of awareness.','|Immediate rework NC raised in the ERP and proper rework tag was placed.','|All the rework parts need to be immediately identified with the proper Yellow tag to distinguish them as rework.','CAPA ok.','','2019-02-18','Dinakar(K)','Dinakar(K)','','0000-00-00','NC CREATED','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Manufacture Only','','FI','yes','Misc','Narasimha Murthy(R)','no','','|Checked all the completed parts and separated the uncleared parts.','E3456','qas|','2019-04-08|','2019-04-08',NULL,NULL,NULL,NULL,NULL,NULL),(11522,'18-085A','Magellan Aerospace Wrexham','BRACKET SUPPORT','17134955-B','D579 52009 200','L168','A',24,'175154','','88243','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Part Marking date code wrong','First Off clearance was not done.|During part marking operation, old part marking program was selected instead of new one.|Both old & new part marking program are in same folder.','|From next time all the programs to be separate year wise and to be store in a required path\r<br/>During part marking process first off to carry out','|During part marking process first off to be carry out','CAPA found ok.','','2019-02-18','Anjinamurthy(H)','S. Shiva Kumar,','','0000-00-00','NC CREATE','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','','FI','yes','BMV 60-2','Santhosh Kumar.R()','no','','|The parts in wip ensures found ok','E3456','qas|qas|','2019-02-19|2019-03-30|','2019-03-30',NULL,NULL,NULL,NULL,NULL,NULL),(11523,'35-225A','Saab AB','HINGE BRACKET 1 ','1750032110','D576 50004 206','','D00',1,'1600214065','','87655','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Bore over size by 0.08 (Because of chips clot)','Insufficient coolant supply.|Chips blocked in filter.','|Clean the filter and coolant lines. ','|every week clean the filter and related connections. ','CA PA ok','','2019-02-18','Ravi nayak()','prodn_aero(prodn)','','0000-00-00','operator Name Naveen S','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Ravi nayak()','no','','|Immediately stopped the machine and inform the maintenance team.','A3456','qas|qas|','2019-02-19|2019-03-30|','2019-03-30',NULL,NULL,NULL,NULL,NULL,NULL),(11524,'18-090A','Magellan Aerospace(Polska) Sp','BUSH','1670510-3/YT2N','PID278 50164 200','','A',8,'104569','','84863','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','OD UNDER SIZE BY -0.03MM.','OD under size due to improper wear offset.|During insert change the operator did not properly calculated the wear correction and continued the production with out checking the part.|Due to improper awareness the operator did not ensured the dimension of the part machined after insert change.','|Informed the operator to continue production under senior operator supervision only.','|Informed the operators to carry out insert change and new settings only under the supervision of senior operators.','CA PA found ok.','','2019-02-18','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','03','no','Misc','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),(11525,'35-495A','Saab AB','BRACKET','802628','D5227334920200','NA','PART ISSUE B',1,'OWED-LTA-005','','87309','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','OD Digmark.','1.the tool offset taken was recorded wrongly in the Log book and the same was entered into the system|2.The offset taken was not validated in with the previous one which was recorded in the log book|3.Operator entered Wrong Tool offset  in the system and did not follow the check list provided for setting.','|1.Awareness and on job training was given to all the operators on following the check list provided for doing the setting\r<br/>2.Instruction given to all the operators to get the check list approved from the supervisor and senior operators once the setting is done.','|Refer to CA','87311	machined and  found ok ','','2019-02-18','Dinakar K()','Dinakar K ,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','1','no','100MY-02','Dinakar K()','no','','|1.The part was rejected and internal NCR was raised.\r\n2.All the tools pertaining to the program was recalled and new offset was taken.','Z3456','qas_sez|','2019-04-16|','2019-04-16',NULL,NULL,NULL,NULL,NULL,NULL),(11526,'35-415','Saab AB','SHAFT LATCH LINK','M789340','D522 73496 200 00','','A',7,'OWED-LTA-004','','83879','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','OD UNDER SIZE MINIMUM VALUE IS 22.048. MEASURED VALUE IS 22.035 TO 21.90 . AND FIXTURE HOLDING MARKS OBSERVED ON THE ALL PARTS ','CLAMPING MARK WAS OBSERVED ON THE OUTER DIA FOR THE LENGTH OF 50MM AND WIDTH OF 3MM AT 3 LOCATIONS ON BOTH THE ENDS OF THE PART.\r\nCLAMPING FORCE WAS HIGH AND THE PART WAS CLAMPPED MANUALLY BY HAND\r\nOPERATOR WAS NOT AWARE OF THE CLAMPING MARK ON THE PART\r\n','|CLAMPING FORCE WAS REDUCED FOR THE REST OF THE PRODUCTION BATCH.','|1.TORQUE TOOL FOR TIGHTENING THE PART WILL BE PROCURED(DT:22.2.19) \r<br/>2.TORQUE REQUIREMENT FOR THE SPECIFIC BOLTS WILL BE DISPLAYED NEAR ALL THE MACHINE(DT:22.2.19) \r<br/>3.PROCESS WILL BE PLANNED TO TURN MILL SUCH THAT IT WILL NOT BE MACHINED IN THE VMC/HMC(DT:15.4.19)\r<br/>','work orders 83883,87190 was clamped and machined using the torquing tool and found no rejection due\r\nto clamp marks and OD underside ','','2019-02-19','pe_sez(a)','Shivaraj K S,Ravi Kumar G.B,Pradeep B.D,Nagaraju P K ,Karthik Raj T ,Dinakar K ,','','0000-00-00','OD UNDER SIZE MINIMUM VALUE IS 22.048. MEASURED VALUE IS 22.035 TO 21.90 . AND FIXTURE HOLDING MARKS OBSERVED ON THE ALL PARTS ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','a51nx-05','qas_sez(a)','no','','|1.ALL THE PARTS WAS INSPECTED FOR OD AND THE DEVIATION PARTS WAS IDENTIFIED . 2.NCR WAS RAISED FOR THE NON CONFORMING PART','Z3456','qas_sez|qas_sez|','2019-02-20|2019-04-02|','2019-04-02',NULL,NULL,NULL,NULL,NULL,NULL),(11527,'18-104A','Magellan Aerospace Bournemouth','BODY TURNBUCKLE ','CD703094/02891A','PID575 40490 200','','E',1,'428863','','82161','','0000-00-00',NULL,'yes','no','yes','no','yes','no','no','no','no','RUNNING TIME POWER TRIP ID THREAD DIG .','Machine running time thread damage.|suddenly off the machine.|power trip.|UPS Not properly.','|Checking the all battery and correct it. ','|Maintaining the UPS & Battery .','Machines will be moved to non power problem area before 15-May-2019.','','2019-02-19','Raghavendra Rao(R)','Arun Kumar(R)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','03','no','Misc','GUNDEGOWDA(H.G.)','no','','|Checking the UPS and changing the battery. ','E3456','qas|qas|','2019-03-04|2019-03-30|','2019-03-30',NULL,NULL,NULL,NULL,NULL,NULL),(11528,'35-139','Saab AB','BCD_DR_BEAM_FTG-LWR_FWD-4','245884B2','424Z1130-13-01','7050 - T7451 ALUMINU','--B',1,'Forecast po for B787','','76022','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','STEPS OBSERVED IN HOLE.','While finishing the hole chips clocked in the tool and formed deep step in the hole|No proper coolant flow to remove the chips during machining|The coolant nozzle was not aligned with the cutting tool','|1.MOO optional stop added in the program to clean the chips after roughing operation\r<br/>2.Instruction given to the operator to clean and ensure weather any chips presence after roughing operation','|refer to CA','Next batch wo#76023 machined and found no evidence for step formation  	','','2019-02-20','qas_sez(a)','qas_sez(a)','','2019-02-20','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','DN44145','POST DN','no','Misc','qas_sez(a)','no','','|1.The part was rejected and NCR was Raised.\r\n2.The coolant nozzle was aligned with the cutting edge of the tool to remove the chip.','Z3456','qas_sez|','2019-04-16|','2019-04-16',NULL,NULL,NULL,NULL,NULL,NULL),(11529,'51A-072','THE BOEING COMPANY','BEARING ASSY','','113T1204-1','','NIL',3,'BOEING 001S','','A15482','','0000-00-00',NULL,'yes','no','no','no','no','yes','no','yes','no','Step and dent marking observed on the bearing surface and groove.','The bought out item received was found dent.|Part to part contact happened in transportation|There were no sufficient cussion in packing material','|the dent dimensions were measured and sent to the customer for approval','|Informed to the supplier to improve the packing method','Customer approved the parts and found OK','','2019-02-20','pe_sez(a)','pe_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','Assembly','','FI','no','Misc','qas_sez(a)','no','','|Informed to the supplier to improve the packing method\r\n\r\nAll the parts were inspected visually and difected parts identified and sagrgated','Z3456','qas_sez|qas_sez|','2019-03-08|2019-03-08|','2019-03-08',NULL,NULL,NULL,NULL,NULL,NULL),(11530,'51A-072','THE BOEING COMPANY','BEARING ASSY','','113T1204-1','','NIL',6,'BOEING 001S','','A20252','','0000-00-00',NULL,'yes','no','no','no','no','yes','no','yes','no','Step and dent marking observed on the bearing surface and groove.','','','','','','2019-02-20','pe_sez(a)','pe_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Cancelled','no','no','no','Assembly','','FI','yes','Misc','qas_sez(a)','no','','','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11531,'51A-072','THE BOEING COMPANY','BEARING ASSY','','113T1204-1','','NIL',6,'BOEING 001S','','A20253','','0000-00-00',NULL,'yes','no','no','no','no','yes','no','yes','no','Step and dent marking observed on the bearing surface and groove.','','','','','','2019-02-20','pe_sez(a)','pe_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Cancelled','no','no','no','Assembly','','FI','yes','Misc','qas_sez(a)','no','','','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11532,'18-210B','Magellan Aerospace Wrexham','BODY','M037880/27054','D321 40204 204','','D, ECN NR29999ST1KM15, NR29999ST2KF65, WQN DFB09775',1,'175174','','85609','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','ID DEPTH OVER SIZE.','Program mistake(ID DEPTH OVER SIZE )|Operator did not observed the program before run. ','|Revised the program & correct it. \r<br/>Saved the program after editing.','|Before the first part running we will check the program & maintain the checklist.|All the proved program will be stored and controlled by Engineering department and the same will be used for every production.','CAPA found ok.','','2019-02-20','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','01','no','Misc','Ravi(M)','no','','|Immediately stop the machine,corrected the program & run.','E3456','qas|qas|','2019-02-25|2019-03-12|','2019-03-12',NULL,NULL,NULL,NULL,NULL,NULL),(11533,'51-164','THE BOEING COMPANY','FLANGE','20233506','349T2200-50','NA','PSDL REV J',1,'BOEING 001Z','','87692','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','GROOVE WIDTH OVER SIZE MAX 3.25MM MEASURED 3.40MM','TOOL:WIDIA, \r\nINSERT:SPECIAL INSERT GRINDED TO THE REQUIREMENT OF THE DRAWING\r\nSPEED:200RPM AND FEED 0.05|CHATTERING MARKS OBSERVED IN GROOVE AND THE CHATTERING MARK WAS REMOVED MANUALLY BY USING ZERO EMERY PAPER.\r\nIDLE PASS WAS CALLED OUT TO REMOVE THE CHATTERING.\r\n|NO SUFFICIENT COOLANT TO CHIPS FLOW DUE THE CHIPS DEPOSITION THE GROVE SIZE WAS OVERSIZED.','|FURTHER PRODUCTION WAS WAS CONTINUED WITHOUT THE IDLE PASS AND CHATTERING WAS REMOVED MANUALLY.','|STANDARD TOOL BE FIXED FOR THE GROOVING OPERATION.\r<br/>CUTTING PARAMETERS TO BE FIXED.\r<br/>\r<br/>TO FIX THE CUTTING PARAMETER EFFECTIVENESS DATE IS 15/04/2019','nEXT bATCH PRODUCTION DONE AND GROOVE FOUND OK REFER WO87587','','2019-02-20','pe_sez(a)','Manu K,Dinakar K ,','','0000-00-00','GROOVE WIDTH OVER SIZE MAX 3.25MM MEASURED 3.40MM\r\n','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','200MY-01','qas_sez(a)','no','','|ALL PREVIOUSLY MACHINED PARTS WERE CHECKED AND AND GROOVE WAS FOUND OK.\r\nTHE DEVIATION PART WAS IDENTIFIED WITH A TAG AND NC WAS RAISED.\r\n','Z3456','qas_sez|qas_sez|','2019-02-22|2019-04-03|','2019-04-03',NULL,NULL,NULL,NULL,NULL,NULL),(11534,'35-415','Saab AB','SHAFT LATCH LINK','M789340','D522 73496 200 00','','A',7,'OWED-LTA-004','','83879','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','OD UNDER SIZE MINIMUM VALUE IS 22.048. MEASURED VALUE IS 22.035 TO 21.90 . AND FIXTURE HOLDING MARKS OBSERVED ON THE ALL PARTS \r\n\r\n\r\ndummy nc','CLAMPING MARK WAS OBSERVED ON THE OUTER DIA FOR THE LENGTH OF 50MM AND WIDTH OF 3MM AT 3 LOCATIONS ON BOTH THE ENDS OF THE PART.\r\nCLAMPING FORCE WAS HIGH AND THE PART WAS CLAMPPED MANUALLY BY HAND\r\nOPERATOR WAS NOT AWARE OF THE CLAMPING MARK ON THE PART\r\n|\r\nDummy nc','CLAMPING FORCE WAS REDUCED FOR THE REST OF THE PRODUCTION BATCH.','1.TORQUE TOOL FOR TIGHTENING THE PART WILL BE PROCURED(DT:22.2.19) \r<br/>2.TORQUE REQUIREMENT FOR THE SPECIFIC BOLTS WILL BE DISPLAYED NEAR ALL THE MACHINE(DT:22.2.19) \r<br/>3.PROCESS WILL BE PLANNED TO TURN MILL SUCH THAT IT WILL NOT BE MACHINED IN THE VMC/HMC(DT:15.4.19)\r<br/>','dummy nc','','2019-02-20','pe_sez(a)','Shivaraj K S,Ravi Kumar G.B,Pradeep B.D,Nagaraju P K ,Karthik Raj T ,Dinakar K ,','','0000-00-00','OD UNDER SIZE MINIMUM VALUE IS 22.048. MEASURED VALUE IS 22.035 TO 21.90 . AND FIXTURE HOLDING MARKS OBSERVED ON THE ALL PARTS ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','a51nx-05','qas_sez(a)','no','','1.ALL THE PARTS WAS INSPECTED FOR OD AND THE DEVIATION PARTS WAS IDENTIFIED . \r\n2.NCR WAS RAISED FOR THE NON CONFORMING PART\r\n','Z3456','qas_sez|','2019-02-22|','2019-02-22',NULL,NULL,NULL,NULL,NULL,NULL),(11535,'51-183','THE BOEING COMPANY','ADAPTER, BULKHEAD - ALUMI','MA20172644','272U0021-3','NA','PSDL REV A',2,'BOEING 001Z','','88170','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','THREAD NO GO GAUGE ANSWERING FULL LENTH','after thread finishing the parts was reworked on the threads.|there was light step formed on the thread angle which visually was not accpectable.|during threading operation very minor chip clocked in the insert which  rubbed along the thread and formed some minor  marks on thread|The coolant nozzle was not aligned with the insert while cutting','|The following instruction was flow down to all the operators on threading operation.\r<br/>1.To adjust coolant nozzle on to the insert to avoid chips clocking.\r<br/>2.To monitor and record the life of the threading insert.','|Refer to CA',' Wo 88782 ,Qty 7 nos was machined as per the CA and found the thread was meeting the requirement and the life of the insert was recorded and setted the frequency to 30 nos to change the insert.	','','2019-02-20','pe_sez(a)','Maruthi ,Dinakar K ,','','0000-00-00','THREAD NO GO GAUGE ANSWERING FULL LENTH','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','200MY-01','qas_sez(a)','no','','|1.After rework the parts was checked with thread gauge and found NO-GO was entering.\r\n2.NCr was raised for these parts.\r\n3.Checked the threading insert and removed the chips clocked in the insert.','Z3456','qas_sez|','2019-04-10|','2019-04-10',NULL,NULL,NULL,NULL,NULL,NULL),(11536,'35-415','Saab AB','SHAFT LATCH LINK','M794860','D522 73496 200 00','','A',2,'OWED-LTA-004','','87190','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','OD Dig mark Fund.','CLAMPING MARK WAS OBSERVED ON THE OUTER DIA FOR THE LENGTH OF 50MM AND WIDTH OF 3MM AT 3 LOCATIONS ON BOTH THE ENDS OF THE PART.|CLAMPING FORCE WAS HIGH AND THE PART WAS CLAMPPED MANUALLY BY HAND|OPERATOR WAS NOT AWARE OF THE CLAMPING MARK ON THE PART','|CLAMPING FORCE WAS REDUCED FOR THE REST OF THE PRODUCTION BATCH. ','|1.TORQUE TOOL FOR TIGHTENING THE PART WILL BE PROCURED(DT:22.2.19)\r<br/>2.TORQUE REQUIREMENT FOR THE SPECIFIC BOLTS WILL BE DISPLAYED NEAR ALL THE MACHINE(DT:22.2.19)\r<br/>3.PROCESS WILL BE PLANNED TO TURN MILL SUCH THAT IT WILL NOT BE MACHINED IN THE VMC/HMC(DT:15.4.19) ','work orders 83883,87190 was clamped and machined using the torquing tool and found no rejection due\r\nto clamp marks and OD underside ','','2019-02-21','Dinakar K()','Maruthi ,Dinakar K ,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','3','no','200MY-01','op_sez(s)','no','','|1.ALL THE PARTS WAS INSPECTED FOR OD AND THE DEVIATION PARTS WAS IDENTIFIED . 2.NCR WAS RAISED FOR THE NON CONFORMING PART ','Z3456','qas_sez|','2019-04-02|','2019-04-02',NULL,NULL,NULL,NULL,NULL,NULL),(11537,'56-104','GKN Aerospace Orangeburg','CLOSEOUT - RIB, LWR, AFT','1222701-2','119A1441-607','NA','PSDL REV -',1,'A000047470','','87888','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','THE DEEP DENT OBSERVED ON THE PART DUE TO POST PROCESS ERROR.','12R3 WALL FINISHING PROGRAM WAS CHANGED TO AVOID THE CHATTERING MARKS, STEPS AND THICKNESS OVER SIZE.|ENGINEERING POST PROCESSOR PROBLEM','|INFORMED TO THE SOFTWARE APPLICATION ENGINEER.REQUESTED FOR THE TECHNICAL SUPPORT.','|G CODE SIMULATOR WILL BE PROCURED.|Informed the operator to dry run the programm by keeping offset in z axis to conform if any G-code is missing and then run on final part','CAPA ok','','2019-02-22','CAD(sez)','CAD(sez)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','pe_sez(a)','no','','','Z3456','qas_sez|qas_sez|','2019-02-22|2019-04-16|','2019-04-16',NULL,NULL,NULL,NULL,NULL,NULL),(11538,'18-567A','Magellan Aerospace Wrexham','FITTING SPIKE AFT','503029A','L575 51783 201','','A',1,'162904','','68047','','0000-00-00',NULL,'no','no','no','no','no','no','yes','yes','no','Corrosion pit marks observed after NDT inspection','REFER NC NO 11424|REFER NC NO 11424|REFER NC NO 11424|REFER NC NO 11424|REFER NC NO 11424','|REFER NC NO 11424','|REFER NC NO 11424','REFER NC NO 11424','','2019-02-22','qas_sez(a)','qas_sez(a)','','0000-00-00','NC CREATE','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','DN52446','POST DN','no','Misc','qas_sez(a)','yes','','|REFER NC NO 11424','Z3456','qas_sez|','2019-04-16|','2019-04-16',NULL,NULL,NULL,NULL,NULL,NULL),(11539,'56-100','GKN Aerospace Orangeburg','CLOSEOUT RIB - AFT, UPR','1682402','119A1383-603','NA','PSDL REV -',1,'A000047470','','87423','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dig mark observed on wall.','Running time tool was broken|due to insufficient coolant supply.|foam was flown instead of the coolant.','|informed to the coolant supplier.','|PH level of the coolant was maintained to the required value and it was varified by the  maintainance team.','capa found ok','','2019-02-23','pe_sez(a)','Raghu B,','','0000-00-00','.','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','1','no','Slim3n-4AHS-3','pe_sez(a)','no','','|machine was stopped ','Z3456','qas_sez|qas_sez|','2019-03-14|2019-04-03|','2019-04-03',NULL,NULL,NULL,NULL,NULL,NULL),(11540,'56-098','GKN Aerospace Orangeburg','CLOSEOUT - CHORD, LWR','0054701-2','119A1381-603','NA','PSDL REV -',16,'A000047470','','88027','','0000-00-00',NULL,'yes','yes','yes','','','','','','','total thickness undersized by 1.8mm because of wrong offset taken in Z offset while setting time.','1.the tool offset taken was recorded wrongly in the Log book and the same was entered into the system|2.The offset taken was not validated in with the previous one which was recorded in the log book|3.Operator entered Wrong Tool offset  in the system and did not follow the check list provided for setting.','|1.Awareness and on job tarining was given to all the operators on following the check list provided for doing the setting\r<br/>2.Intruction given to all the operators to get the check list approved from the supervisor and senior opeartors once the setting is done','|refer to CA','wo#88028,machined and part found ok	','','2019-02-23','pe_sez(a)','        Kiran Kumar M','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','01','','','','','','|1.The part was rejected and internal NCR was raised.\r\n2.All the tools pertaining to the programm was recalled and new offset was taken.','Z3456','pe_sez|qas_sez|','2019-02-23|2019-04-16|','2019-04-16',NULL,NULL,NULL,NULL,NULL,NULL),(11541,'35-527','Saab AB','GUIDE PIN','C80552.SD4W','D522 73458 202 00','','PART ISSUE B',31,'OWED-LTA-003','','73126','','0000-00-00',NULL,'no','no','no','no','no','no','yes','yes','yes','Plating THICKNESS OVER SIZE.','Parts were rejected by customer as the parts are not suiting for assembly however the platting thickness is as per the specification.|when processing according to the standard the thickness gets naturally built up at the edges due to the high concentration of current at edges.','|Parts are sent to supplier for stripping and re-processing.','|Informed the supplier to reduce the immersion time inside the platting tank to reduce the platting thickness and to maintain the thickness to minimum side.','Fresh batches processed to new method are verified and found ok.','C70895','2019-02-26','qas_sez(a)','qas_sez(a)','mail','2019-02-01','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','DN40819','CUSTOMER END','yes','Misc','qas_sez(a)','no','','Informed to Suppler. ','Z3456','qas|','2019-04-11|','2019-04-11',NULL,NULL,NULL,NULL,NULL,NULL),(11542,'35-527','Saab AB','GUIDE PIN','C80552','D522 73458 202 00','','PART ISSUE B',18,'OWED-LTA-003','','78463','','0000-00-00',NULL,'no','no','no','no','no','no','yes','yes','yes','plating thickness over size.','Parts were rejected by customer as the parts are not suiting for assembly however the platting thickness is as per the specification.|when processing according to the standard the thickness gets naturally built up at the edges due to the high concentration of current at edges.','|Parts are sent to supplier for stripping and re-processing.','|Informed the supplier to reduce the immersion time inside the platting tank to reduce the platting thickness and to maintain the thickness to minimum side. ','Fresh batches processed to new method are verified and found ok.','C72266','2019-02-26','qas_sez(a)','qas_sez(a)','mail','2019-02-01','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','DN47795','CUSTOMER END','yes','Misc','qas_sez(a)','no','','informed to supplier.','Z3456','qas|','2019-04-11|','2019-04-11',NULL,NULL,NULL,NULL,NULL,NULL),(11543,'35-527','Saab AB','GUIDE PIN','C80552','D522 73458 202 00','','PART ISSUE B',20,'OWED-LTA-003','','73128','','0000-00-00',NULL,'no','no','no','no','no','no','yes','yes','yes','plating thickness over size.','1.Parts were rejected by customer as the parts are not suiting for assembly however the platting thickness is as per the specification.\r\n|2.when processing according to the standard the thickness gets naturally built up at the edges due to the high concentration of current at edges.\r\n','|1.Parts are sent to supplier for stripping and re-processing. \r<br/>\r<br/>','|1.Informed the supplier to reduce the immersion time inside the platting tank to reduce the platting thickness and to maintain the thickness to minimum side. \r<br/>\r<br/>\r<br/>','1.Fresh batches processed to new method are verified and found ok.\r\n','C72265','2019-02-26','qas_sez(a)','qas_sez(a)','mail','2019-02-01','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','DN40816','CUSTOMER END','yes','Misc','qas_sez(a)','no','','informed to supplier.','Z3456','qas_sez|','2019-04-16|','2019-04-16',NULL,NULL,NULL,NULL,NULL,NULL),(11544,'35-527','Saab AB','GUIDE PIN','C80552','D522 73458 202 00','','PART ISSUE B',38,'OWED-LTA-003','','78463','','0000-00-00',NULL,'no','no','no','no','no','no','yes','yes','yes','plating thickness over size.\r\n','1.Parts were rejected by customer as the parts are not suiting for assembly however the platting thickness is as per the specification.\r\n|2.when processing according to the standard the thickness gets naturally built up at the edges due to the high concentration of current at edges.\r\n','|1.Parts are sent to supplier for stripping and re-processing. \r<br/>\r<br/>','|1.Informed the supplier to reduce the immersion time inside the platting tank to reduce the platting thickness and to maintain the thickness to minimum side. \r<br/>\r<br/>\r<br/>','1.Fresh batches processed to new method are verified and found ok.\r\n','C72267','2019-02-26','qas_sez(a)','qas_sez(a)','mail','2019-02-01','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','DN47795','CUSTOMER END','yes','Misc','qas_sez(a)','no','','informed to supplier.','Z3456','qas_sez|','2019-04-16|','2019-04-16',NULL,NULL,NULL,NULL,NULL,NULL),(11545,'35-527','Saab AB','GUIDE PIN','C80552.SD4W','D522 73458 202 00','','PART ISSUE B',78,'OWED-LTA-003','','73124','','0000-00-00',NULL,'no','no','no','no','no','no','yes','yes','yes','plating thickness over size.','1.Parts were rejected by customer as the parts are not suiting for assembly however the platting thickness is as per the specification.\r\n|2.when processing according to the standard the thickness gets naturally built up at the edges due to the high concentration of current at edges.\r\n','|1.Parts are sent to supplier for stripping and re-processing. \r<br/>\r<br/>','|1.Informed the supplier to reduce the immersion time inside the platting tank to reduce the platting thickness and to maintain the thickness to minimum side. \r<br/>\r<br/>\r<br/>','1.Fresh batches processed to new method are verified and found ok.\r\n','C65342','2019-02-26','qas_sez(a)','qas_sez(a)','mail','2019-02-01','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','DN40815','CUSTOMER END','yes','Misc','qas_sez(a)','no','','informed to supplier.\r\n','Z3456','qas_sez|','2019-04-16|','2019-04-16',NULL,NULL,NULL,NULL,NULL,NULL),(11546,'35-527','Saab AB','GUIDE PIN','C80552.SD4W','D522 73458 202 00','','PART ISSUE B',19,'OWED-LTA-003','','73124','','0000-00-00',NULL,'no','no','no','no','no','no','yes','yes','yes','plating thickness over size.\r\n','1.Parts were rejected by customer as the parts are not suiting for assembly however the platting thickness is as per the specification.\r\n|2.when processing according to the standard the thickness gets naturally built up at the edges due to the high concentration of current at edges.\r\n','|1.Parts are sent to supplier for stripping and re-processing. \r<br/>\r<br/>','|1.Informed the supplier to reduce the immersion time inside the platting tank to reduce the platting thickness and to maintain the thickness to minimum side. \r<br/>\r<br/>\r<br/>','1.Fresh batches processed to new method are verified and found ok.\r\n','C65342','2019-02-26','qas_sez(a)','qas_sez(a)','mail','2019-02-01','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','DN40815','CUSTOMER END','yes','Misc','qas_sez(a)','no','','informed to supplier.\r\n','Z3456','qas_sez|','2019-04-16|','2019-04-16',NULL,NULL,NULL,NULL,NULL,NULL),(11547,'35-527','Saab AB','GUIDE PIN','C80552.SD4W','D522 73458 202 00','','PART ISSUE B',51,'OWED-LTA-003','','73123','','0000-00-00',NULL,'no','no','no','no','no','no','yes','yes','yes','plating thickness over size.\r\n','1.Parts were rejected by customer as the parts are not suiting for assembly however the platting thickness is as per the specification.\r\n|2.when processing according to the standard the thickness gets naturally built up at the edges due to the high concentration of current at edges.\r\n','|1.Parts are sent to supplier for stripping and re-processing. \r<br/>','|1.Informed the supplier to reduce the immersion time inside the platting tank to reduce the platting thickness and to maintain the thickness to minimum side. \r<br/>\r<br/>\r<br/>','1.Fresh batches processed to new method are verified and found ok.\r\n','C65340','2019-02-26','qas_sez(a)','qas_sez(a)','mail','2019-02-01','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','DN40814','CUSTOMER END','yes','Misc','qas_sez(a)','no','','informed to supplier.\r\n','Z3456','qas_sez|','2019-04-16|','2019-04-16',NULL,NULL,NULL,NULL,NULL,NULL),(11548,'35-527','Saab AB','GUIDE PIN','C80552.SD4W','D522 73458 202 00','','PART ISSUE B',44,'OWED-LTA-003','','73123','','0000-00-00',NULL,'no','no','no','no','no','no','yes','yes','yes','plating thickness over size.\r\n','1.Parts were rejected by customer as the parts are not suiting for assembly however the platting thickness is as per the specification.\r\n|2.when processing according to the standard the thickness gets naturally built up at the edges due to the high concentration of current at edges.\r\n','|1.Parts are sent to supplier for stripping and re-processing. \r<br/>','|1.Informed the supplier to reduce the immersion time inside the platting tank to reduce the platting thickness and to maintain the thickness to minimum side. \r<br/>','1.Fresh batches processed to new method are verified and found ok.\r\n','C65338','2019-02-26','qas_sez(a)','qas_sez(a)','mail','2019-02-01','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','DN40814','CUSTOMER END','yes','Misc','qas_sez(a)','no','','informed to supplier.\r\n','Z3456','qas_sez|','2019-04-16|','2019-04-16',NULL,NULL,NULL,NULL,NULL,NULL),(11549,'35-603A','Saab AB','OUTER HANDLE SHAFT','C78930.TX4W','D5227354020600','','PART ISSUE D',4,'OWED-LTA-004','','78375','','0000-00-00',NULL,'no','no','no','no','no','no','yes','yes','yes','Corrosion mark notes. ','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.','C71980','2019-02-26','qas_sez(a)','qas_sez(a)','mail','2019-02-01','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','DN44600','CUSTOMER END','yes','Misc','qas_sez(a)','no','','|Refer NC No 11424.','Z3456','qas_sez|','2019-04-16|','2019-04-16',NULL,NULL,NULL,NULL,NULL,NULL),(11550,'35-603A','Saab AB','OUTER HANDLE SHAFT','C86598.SSHF','D5227354020600','','PART ISSUE D',13,'OWED-LTA-004','','78374','','0000-00-00',NULL,'no','no','no','no','no','no','yes','yes','yes','Corrosion mark notes. ','Refer NC No 11424.|Refer NC No 11424.|Refer NC No 11424.|Refer NC No 11424.|Refer NC No 11424.','|Refer NC No 11424.','|Refer NC No 11424.','Refer NC No 11424.','C70613','2019-02-26','qas_sez(a)','qas_sez(a)','mail','2019-02-01','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','DN45824','CUSTOMER END','yes','Misc','qas_sez(a)','no','','|Refer NC No 11424.','Z3456','qas_sez|','2019-04-16|','2019-04-16',NULL,NULL,NULL,NULL,NULL,NULL),(11551,'35-603A','Saab AB','OUTER HANDLE SHAFT','C78930.TX4W','D5227354020600','','PART ISSUE D',13,'OWED-LTA-004','','78373','','0000-00-00',NULL,'no','no','no','no','no','no','yes','yes','yes','Corrosion mark notes. \r\n','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.','C70613','2019-02-26','qas_sez(a)','qas_sez(a)','mail','2019-02-01','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','DN44599','CUSTOMER END','yes','Misc','qas_sez(a)','no','','|Refer NC No 11424.','Z3456','qas_sez|','2019-04-16|','2019-04-16',NULL,NULL,NULL,NULL,NULL,NULL),(11552,'35-603A','Saab AB','OUTER HANDLE SHAFT','C78930.TX4W','D5227354020600','','PART ISSUE D',7,'OWED-LTA-004','','78372','','0000-00-00',NULL,'no','no','no','no','no','no','yes','yes','yes','Corrosion mark notes. \r\n','Refer NC No 11424.|Refer NC No 11424.|Refer NC No 11424.|Refer NC No 11424.|Refer NC No 11424.','|Refer NC No 11424.','|Refer NC No 11424.','Refer NC No 11424.','C70613','2019-02-26','qas_sez(a)','qas_sez(a)','mail','2019-02-01','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','DN44598','CUSTOMER END','yes','Misc','qas_sez(a)','no','','|Refer NC No 11424.','Z3456','qas_sez|','2019-04-16|','2019-04-16',NULL,NULL,NULL,NULL,NULL,NULL),(11553,'35-603A','Saab AB','OUTER HANDLE SHAFT','C78930.TX4W','D5227354020600','','PART ISSUE D',7,'OWED-LTA-004','','78375','','0000-00-00',NULL,'no','no','no','no','no','no','yes','yes','yes','Corrosion mark notes. \r\n','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.','C70613','2019-02-26','qas_sez(a)','qas_sez(a)','mail','2019-02-01','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','DN44600','CUSTOMER END','yes','Misc','qas_sez(a)','no','','|Refer NC No 11424.','Z3456','qas_sez|','2019-04-16|','2019-04-16',NULL,NULL,NULL,NULL,NULL,NULL),(11554,'35-479A','Saab AB','SHAFT','C78930.TX4X','D5227336520000','NA','PART ISSUE B',1,'OWED-LTA-004','','79076','','0000-00-00',NULL,'no','no','no','no','no','no','yes','yes','yes','Corrosion mark notes. ','Refer NC No 11424.|Refer NC No 11424.|Refer NC No 11424.|Refer NC No 11424.|Refer NC No 11424.','|Refer NC No 11424.','|Refer NC No 11424.','Refer NC No 11424.','C72262','2019-02-26','qas_sez(a)','qas_sez(a)','mail','2019-02-01','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','DN48058','CUSTOMER END','yes','Misc','qas_sez(a)','no','','|Refer NC No 11424.','Z3456','qas_sez|','2019-04-16|','2019-04-16',NULL,NULL,NULL,NULL,NULL,NULL),(11555,'35-479A','Saab AB','SHAFT','C78930.TX4X','D5227336520000','NA','PART ISSUE B',5,'OWED-LTA-004','','79077','','0000-00-00',NULL,'no','no','no','no','no','no','yes','yes','yes','Corrosion mark notes. ','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.','C72264','2019-02-26','qas_sez(a)','qas_sez(a)','mail','2019-02-01','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','DN48059','CUSTOMER END','yes','Misc','qas_sez(a)','no','','|Refer NC No 11424.','Z3456','qas_sez|','2019-04-16|','2019-04-16',NULL,NULL,NULL,NULL,NULL,NULL),(11556,'35-479A','Saab AB','SHAFT','C78930.TX4X','D5227336520000','NA','PART ISSUE B',16,'OWED-LTA-004','','79076','','0000-00-00',NULL,'no','no','no','no','no','no','yes','yes','yes','Corrosion mark notes. ','Refer NC No 11424.|Refer NC No 11424.|Refer NC No 11424.|Refer NC No 11424.|Refer NC No 11424.','|Refer NC No 11424.','|Refer NC No 11424.','Refer NC No 11424.','C72264','2019-02-26','qas_sez(a)','qas_sez(a)','mail','2019-02-01','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','DN48058','CUSTOMER END','yes','Misc','qas_sez(a)','no','','|Refer NC No 11424.','Z3456','qas_sez|','2019-04-16|','2019-04-16',NULL,NULL,NULL,NULL,NULL,NULL),(11557,'35-602A','Saab AB','SHAFT 1','C78776','D5227280720000','NA','PART ISSUE B',32,'OWED-LTA-004','','75851','','0000-00-00',NULL,'no','no','no','no','no','no','yes','yes','yes','plating thickness over size.','1.Parts were rejected by customer as the parts are not suiting for assembly however the platting thickness is as per the specification.\r\n|2.when processing according to the standard the thickness gets naturally built up at the edges due to the high concentration of current at edges.\r\n','|1.Parts are sent to supplier for stripping and re-processing. \r<br/>','|1.Informed the supplier to reduce the immersion time inside the platting tank to reduce the platting thickness and to maintain the thickness to minimum side. \r<br/>','1.Fresh batches processed to new method are verified and found ok.\r\n','C68090','2019-02-26','qas_sez(a)','qas_sez(a)','mail','2019-02-01','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','DN42251','CUSTOMER END','yes','Misc','qas_sez(a)','no','','informed to supplier.','Z3456','qas_sez|','2019-04-16|','2019-04-16',NULL,NULL,NULL,NULL,NULL,NULL),(11558,'35-602A','Saab AB','SHAFT 1','C78776','D5227280720000','NA','PART ISSUE B',8,'OWED-LTA-004','','78470','','0000-00-00',NULL,'no','no','no','no','no','no','yes','yes','yes','plating thickness over size.\r\n','1.Parts were rejected by customer as the parts are not suiting for assembly however the platting thickness is as per the specification.\r\n|2.when processing according to the standard the thickness gets naturally built up at the edges due to the high concentration of current at edges.\r\n','|1.Parts are sent to supplier for stripping and re-processing. \r<br/>','|1.Informed the supplier to reduce the immersion time inside the platting tank to reduce the platting thickness and to maintain the thickness to minimum side. \r<br/>','1.Fresh batches processed to new method are verified and found ok.\r\n','C69825','2019-02-26','qas_sez(a)','qas_sez(a)','mail','2019-02-01','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','DN45606','CUSTOMER END','yes','Misc','qas_sez(a)','no','','informed to supplier.\r\n','Z3456','qas_sez|','2019-04-16|','2019-04-16',NULL,NULL,NULL,NULL,NULL,NULL),(11559,'35-681','Saab AB','LATCH FORK','D91680','D5227348920600','NA','PART ISSUE D',64,'OWED-LTA-003','','86401','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Is: Hole chamfer measures 0.75mm to 0.8mm X 45 degree.\r\n\r\nShould be : Hole Chamfer should be 0.5mm (+ 0.1/ -0.2) X 45 degree.(Refer below image)\r\n','Why-1: Chamfer Oversize.|Why-2: Depth of the Chamfer Tool is increased after changing the new tool.|Why-3: Initially the part was proved with a sharp edge tool and the Program was generated according to the sharp edge tool but since the previous tool has worn out the operator has changed the new tool which was supplied with flat edge due to which the offset was varied and the depth increased.','|Informed the tooling department about the issue and ordered special tool with sharp edge(Refer Images)','|1) Spare tool with specific requirements ordered and dedicated for this particular part number.\r<br/>2) The CSK formation will be verified on a dummy material before carrying out on the Actual part.','Next batch production monitored and produced 140 No\'s out of 140 No\'s under work order  no 88099 is found ok and the production is continued to another 200No\'s under work order no 88100 in which 50No\'s manufactured are also found ok.','','2019-02-26','Anjinamurthy(H)','Anjinamurthy(H)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','yes','With Treatment','','FI','no','Misc','Yashawantha(NH)','no','','|Checked all the completed parts and segregated the deviated parts.','E3456','qas|qas|','2019-02-26|2019-03-30|','2019-03-30',NULL,NULL,NULL,NULL,NULL,NULL),(11560,'51-184','THE BOEING COMPANY','ADAPTER, BULKHEAD - ALUMI','MA20172644','272U0021-4','NA','PSDL REV A',1,'BOEING 001Z','','85887','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','yes','Problem(As Is): For P/N 272U0021-4, WO# 85887, Qty (1), One set of positioning mark and inspection mark doesn\'t meeting\r\nFigure 3 and Table V requirements. (Refer Attachment 1).\r\n\r\nRequirement(Should Be): As per BAC 5001-14 Rev (D) 8.3.1.d. (1), Apply a minimum of one witness mark to each prepared tube end before fitting installation.\r\n(1) The positioning mark and inspection mark must be in accordance with Figure 3 and Table V','Witness marking tool was not properly fixed in the tube end on OD surface.','|1) Internal meeting was conducted on 14-Feb-2019 along with Cross Functional Team (CFT), quality inspectors to discuss, identify and resolve the root cause.\r<br/>2) Removed and clean the witness marking and once again carried the marking by Bharat kumar on 14-02-2019.Reviewed the marking location and inspection results by Sr. Quality Engineer Mr. Basavaraj Kuri on 14-02-2019 found acceptable (see the attached images).\r<br/>3) Training plan to be conduct on Inspection & Positioning marking and acceptance criteria per BAC5001-14 by Quality Engineer Mr. Basavaraj kuri on 21-02-2019. \r<br/>4) Training will provide for quality engineers and inspectors on reviewing/acceptance/approval of dimensional inspection reports on 21-02-2019 by Sr. Quality engineer Mr. Basavaraj kuri and Mr. Satish Gondi.\r<br/>','|1) To fix the issue permanently new marking tool will be designed and developed which will not rotate in the end tube while marking.\r<br/>2) Training plan to be conduct on Inspection & Positioning marking and acceptance criteria per BAC5001-14 by Quality Engineer Mr. Basavaraj kuri on 19-02-2019.\r<br/>3) Training will provide for quality engineers and inspectors on reviewing/acceptance/approval of dimensional inspection reports on 21-02-2019 by Sr. Quality engineer Mr. Basavaraj kuri and Mr. Satish Gondi.','CAPA found Ok.','C75210','2019-02-26','Dharani(Shankar)','qas_sez(a)','PV1528522-00','2019-02-26','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','With Treatment','DN52968','Cust End','no','Misc','qas_sez(a)','no','','|1) Rejected one quantity which is not meeting the boeing drawing specification requirements and Internal NC was raised Refer NC number 11515 raised on 14-02-2019 by Quality engineer Bharat kumar and move the rejected part into quality clinic room.\r\n2) Immediately check the FG stock and no parts are available in FG and this is verified by quality engineer Bharat kumar on 14-02-2019.\r\n3) Re-Visual inspection carried for all the produced parts on 14-02-2019 by quality engineer Bharat kumar and all are acceptable to the drawing specification requirements.\r\n4) The above Non-conformance was discussed in quality clinic by Mr. Basavaraj Kuri with CFT team on 14-02-2019.\r\n','Z3456','qas_sez|','2019-03-02|','2019-03-02',NULL,NULL,NULL,NULL,NULL,NULL),(11561,'35A-353A','Saab AB','LIFT PIN HOUSING FWD','','423Z1124-5-52','','1',1,'LTA SAAB B787 Assemb','','A22784','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Zinc nickel plating not properly done on flange bush','Zi Ni platting peeling off from the BOM.|Improper adhesion of Platting. ','|Information provided to supplier about the issue and requested for further actions.','|All the BOI will be inspected visually before releasing to production.','CA PA found ok.','','2019-02-27','Ramesh(D)','Nithin(S)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Assembly','','procesing','no','Misc','Ramesh(D)','no','M07881|BACB28AP20Z253','|Checked all the BOI and separated the similarly affected BOI and returned back to BOI stores.','E3456','qas|','2019-04-26|','2019-04-26',NULL,NULL,NULL,NULL,NULL,NULL),(11562,'51-141A','THE BOEING COMPANY','CLEVIS - UPPER, RH THREAD','534-20180618','112A7112-610','NA','PSDL REV B',1,'BOEING 001AA','','87300','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Chattering observed inside bore','The tool was over heated which in-turn chatter marks was observed in the bore|there was not sufficient coolant flow on the tool during machining|The coolant nozzle was not adjusted on the cutting tool|Operator was not able to see the coolant since ,he part is not visible during machining','|1.Instruction given to the operator to set the coolant nozzel at roughing and check the finish of the bore and then finally finish the bore ','|refer to CA','next batch WO#87301 machined and bore found within the limits','','2019-02-27','pe_sez(a)','pe_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','','07','yes','Misc','pe_sez(a)','no','','|1.The part was rejected and internal NCR was raised\r\n2.The coolant nozzel was adjusted on to the cutting edge of the tool.','Z3456','qas_sez|','2019-04-16|','2019-04-16',NULL,NULL,NULL,NULL,NULL,NULL),(11563,'35-600','Saab AB','FRAME','532794A','D5227338520400','NA','PART ISSUE C',1,'OWED-LTA-001','','86042','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','base thickens under size by 0.24mm','The clamping of part was not clear.|Due to the warpage on part surface|Warpage was formed due to long distance of clmps in clamping method.','|100% inspection by the production team','|Clamping method is changed to avoid the warpage formation so that clamping is done clearly.','Changed clamping method verified and  next batches produced found ok.','','2019-02-28','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','5','no','Misc','Anjinamurthy(H)','no','','|All remaining parts are inspected and found okay.','E3456','pe|qas|','2019-03-04|2019-03-12|','2019-03-12',NULL,NULL,NULL,NULL,NULL,NULL),(11564,'35-473B','Saab AB','LEVER CAM','B78355 P4B6','D5227353720000','NA','PART ISSUE C',1,'OWED-LTA-003','','86617','','0000-00-00',NULL,'yes','','yes','','yes','','','','','power cut so 1 number od dig mark....','In part dig mark occurred when machine running. |machine suddenly off. |Power cut & UPS not working.|UPS Over heat AC Not working properly.','|AC Maintenance to be create &maintain.','|AC Maintenance monitoring record to be create and maintain. ','CAPA found ok.','','2019-02-28','Raghavendra Rao(R)','        Devaraj K.C.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','05','','','','','','|AC & UPS Checked-out & maintenance carried out then next part loaded. ','E3456','pe|qas|qas|','2019-03-01|2019-03-04|2019-03-05|','2019-03-05',NULL,NULL,NULL,NULL,NULL,NULL),(11565,'35-118','Saab AB','ALCD_STRUCT_INTERCOSTAL_L','9404441','423Z1178-3','7050-T7451 ALUMINUM ','--A',1,'Forecast po for B787','','76910','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','no','dummy nc','dummy nc','|dummy nc','|dummy nc','dummy nc','','2019-03-01','qas_sez(a)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','DN45292','ONSITE','no','Misc','qas_sez(a)','yes','','|dummy nc','Z3456','QAS_SEZ|','2019-03-01|','2019-03-01',NULL,NULL,NULL,NULL,NULL,NULL),(11566,'47-033A','GKN Aerospace Filton','RIB 2 INTMD','9990501 4','F5755193620002','NA','C, MIS ISSUE F',1,'GKN GS-034 KIT -2018','','86089','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','BASE THICKNESS OVER SIZE BY 0.05MM','Base thickness over size.|Tool Offset overall base is 0.05 in +side. |Base thickness is controlled that purpose prater is putting in +side because of safety purpose.   ','|Next time controlled dimensions maintaining under process.','|Ensuring the base thickens in machining using Dial gauge. ','CAPA found ok.','','2019-03-01','Dhananjaya(N)','Venkatesh R,S. Shiva Kumar,Narasimhamurthy C,Girish HP,Dileep Kumar,BHUVANAPRAKASH  J.S,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','','FI','yes','VM2-3','Nagendra(SN)','no','','|Remaining parts are checked.','E3456','qas|qas|','2019-03-04|2019-03-30|','2019-03-30',NULL,NULL,NULL,NULL,NULL,NULL),(11567,'35-473B','Saab AB','LEVER CAM','B78355 P4B6','D5227353720000','NA','PART ISSUE C',3,'OWED-LTA-003','','86615','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','3 NUMBER TOTAL LENGTH UNDER SIZE.\r\n','why1: After final machining the part profile was not fully machined due to shortage of raw materia|why2: Supplied raw material dimension was undersize|why3: The supplied raw material was in taper |why4: During raw material cutting process raw material taper occurred','|During cutting process the raw material dimension maintaining 2mm extra in all faces','|Before machining process the raw material dimension to be check ','Next batch found ok','','2019-03-01','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','01','no','Misc','Ravi(M)','no','','|Remaining parts dimension checked and found ok','E3456','qas|qas|','2019-03-19|2019-03-19|','2019-03-19',NULL,NULL,NULL,NULL,NULL,NULL),(11568,'18-285B','Magellan Aerospace Wrexham','SERRATED PLATE','29073','F57551393200','NA','A',1,'175170','','86530','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','PART DIG MARK.','1) Tool Dig mark on the part face during the final step machining.|2) Part lifted during the final pass of the tool.|3) Due to bend in the semi-finished part the clamping was not sufficient to hold the part during the machining.|4) Due to increased lead time between operations the part deformed due to creep.|5) Since the work order was released well in advance to the Schedule the part was stored in semi-finished rack after the completion of first operation.','|The clamping load was increased for this particular batch and mallet application was done to all the parts.','|Immediate production will be completed after the completion of 1st setup Ir-respective of the work order schedule.','CAPA found ok.','','2019-03-02','Anjinamurthy(H)','Punith G(S)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','05','no','Misc','Prashanth Kumar(M)','no','','|Immediately stopped the production and checked all the previously completed parts and found ok.','E3456','qas|','2019-03-05|','2019-03-05',NULL,NULL,NULL,NULL,NULL,NULL),(11569,'35-443C','Saab AB','HINGE','D83028 YNRQ','D5227338820000','NA','B',1,'OWED-LTA-002','','88269','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','Bore Diameter oversize and position shiftted','2 parts are done at a time ,one is top  and the other is bottom|both the top and bottom part was clamped in a single clamp|in op-03 the part which was clamped in the bottom side is been shifted due to weight of the part and drilling cycle.|the location of the part was only one single face and free at other side.','|1.Location Pin was provided to arrest the part in both the direction.','|Clamping Process will be changed DT:7.3.2019 and the same will be updated in MPS.','Wo# 88271 was machined ,bore and position found within the limits	','','2019-03-04','pe_sez(a)','Manu()','','0000-00-00','NC','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','05','no','Misc','pe_sez(a)','no','','|1.the part was identified and NCR raised \r\n2.Previous machined parts were inspected and found ok','Z3456','pe_sez|pe_sez|qas_sez|qas_sez|','2019-03-04|2019-03-04|2019-03-04|2019-04-16|','2019-04-16',NULL,NULL,NULL,NULL,NULL,NULL),(11570,'35-479A','Saab AB','SHAFT','C91486 WC34','D5227336520000','NA','PART ISSUE B',1,'OWED-LTA-004','','87368','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dia 9.476mm outer diameter was -0.05mm undersized.','During jaws boring process 0.05mm run out occurred on jaws bore. |That was not ensured. ','|During jaws boring process run out to be check then part production to be carry on. ','|Without run out ensuring process part wont to be produce. So run out to be ensure on log book. ','CAPA Found OK','','2019-03-04','Ravi(M)','Ugraiah()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','09','no','Misc','Sandhesh D(S)','no','','|Jaws boring process was again carried out. Then ensued the jaws run out was 0.01mm ','E3456','qas|qas|','2019-05-03|2019-05-03|','2019-05-03',NULL,NULL,NULL,NULL,NULL,NULL),(11571,'51-066A','THE BOEING COMPANY','STRUT SUPPORT ','20195373','113T1958-9','NA','PSDL REV A',1,'BOEING 001AA','','88629','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','PART DAMAGED BY CUTTING TOOL HOLDER DUE TO WRONG TOOL OFFSET ENTRY BY THE OPERATOR','IN OP-02 DIA 8 BALL NOSE,TOOL OFFSET VALUE WAS ENTERED IN MINUS (-140MM) \r\n|TOOL OFFSET WAS MANUALLY INPUTTED IN THE TOOL OFFSET','|INFORMATION GIVEN TO THE MACHINE MANUFACTURER  TO MAKE THE TOOL OFFSET TO TAKE IN POSITIVE SIDE.EVEN IF WE PUT MINUS VALUES THE MACHINE SHOULD MAKE IT ZERO.(','|1.INFORMATION GIVEN TO THE MACHINE MANUFACTURER  TO MAKE THE TOOL OFFSET TO TAKE IN POSITIVE SIDE.EVEN IF WE PUT MINUS VALUES THE MACHINE SHOULD MAKE IT ZERO.(7.3.2019)\r<br/>2.ZOLLER TOOL OFFSET VALUE SHOULD DIRECTLY TRANSFER TO MACHINE WHEN OFFSET TAKEN(UNDER DISCUSSION) (7.4.2019)','The next part in this work order was resetted by taking correct tool offset and the part found ok within the limits .all the parts was checked in CMM and all the parameters were meeting the drawing requriments.','','2019-03-05','pe_sez(a)','Umesh B,Sanjeev S.D,Diwakar R.B.,Chethan Kumar M,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','3','no','i700-5','pe_sez(a)','no','','|Stopped the machine and check the spindle by machine maintenance team (MAZAK team)\r\n\r\n8 ball TOOL WAS REPLACED AND TOOL OFFSET WAS TAKEN TO RUN THE PRODUCTION\r\n\r\nNEXT PART INSPECTED AND FOUND OK.','Z3456','qas_sez|qas_sez|','2019-03-05|2019-04-16|','2019-04-16',NULL,NULL,NULL,NULL,NULL,NULL),(11572,'35-228A','Saab AB','HINGE BRACKET 2 ','233915B8','D576 50005 205','','D00',1,'1600223433/Forecast ','','87937','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Profile width shifted by 0.5mm','THE RAW MATERIAL WHICH WAS LOADED TO MACHINING  WAS TAPER   AND NOT FULLY BUTTED TO THE VICE.|WHILE CLAMPING, THE PART WAS CLAMPED AT PEAK POINT OF THE BUTTING SURFACE AS IT WAS NOT STRAIGHT.|IT WAS NOT NOTICED BY THE OPERATOR ','|1.RAW MATERIAL WILL BE CHECKED FOR THE DIMENSION AND IF FOUND ANY TAPER OR DEVIATION ,THE RAW MATERIAL WILL BE ROUGHLY FACED FOR CLAMPING PURPOSE','|1.INSTRUCTED OPERATOR TO CHECK THE CLAMPING SURFACE AND ENSURE WEATHER IT IS BUTTED PROPERLY WILE CLAMPING THE PARTS.\r<br/>2.AFTER TIGHTENING THE PARTS DOUBLE CHECK  TO BE DONE FOR GAP IF ANY BETWEEN THE PART AND VICE USING FEELER GAUGE','ALL THE PARTS IN THIS WORK ORDER INSPECTED AND FOUND NO EVIDENCE FOR PROFILE GETTING MINUS AND THE PARTS FOUND OK TO THE DRAWING REQUIREMENT.','','2019-03-06','pe_sez(a)','pe_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','pe_sez(a)','no','','|1.THE NON CONFORMING PART WAS IDENTIFIED AND NCR RAISED.\r\n2.ALL RM IN THIS WORK ORDER  CHECKED FOR THE SIZE  AND FOUND OK ','Z3456','|','2019-03-06|','2019-03-06',NULL,NULL,NULL,NULL,NULL,NULL),(11573,'35-473B','Saab AB','LEVER CAM','B78355 P4B6','D5227353720000','NA','PART ISSUE C',1,'OWED-LTA-003','','86617','','0000-00-00',NULL,'yes','no','yes','','yes','','','','','RUNNING TIME POWER CUT  OD DIG MARK SO PART  REJECT ...','During machining process dig mark occurred|Machine stopped suddenly the purpose of power cut occurred|Due to problem on UPS over heat power cut occurred|In UPS room AC was not worked properly','|AC maintenance monitoring record to be create and maintain ','|AC maintenance monitoring record to be create and maintain ','Machines will be moved to the non power fluctuating area before 15-May-2019. ','','2019-03-06','Raghavendra Rao(R)','        GUNDEGOWDA H.G.','','0000-00-00','.','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','03','','','','','','|UPS and AC both was checked and maintenance carried out then after that next part was loaded ','E3456','pe|qas|qas|','2019-03-07|2019-03-08|2019-03-30|','2019-03-30',NULL,NULL,NULL,NULL,NULL,NULL),(11574,'35-681','Saab AB','LATCH FORK','D91680','D5227348920600','NA','PART ISSUE D',4,'OWED-LTA-003','','86402','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Dia 18.8E7 bore over size by 0.020mm to 0.040mm.','1 part running time chips present in spindle so tool run out occur |2.To give the proper training for operator while running time check the tool clamping before running |3.Monitor to check the tool-holder for bore finish tool |4.inform to all operators and check the critical dimension 1:1 ratios ','|Based on the usage of the part [Assembly Requirement], since a shaft gets into the bore, the checking method was changed and all the rejected parts were subjected to re-inspection using a GO and NOGO Plug Gage. ','|once a week clean the ATC Shutter and information pass the all 3 shift operator, \r<br/>2.TO every part setting time to check and ensure the m/c ATC arm and shutter door \r<br/>','CAPA FOUND OK ','','2019-03-07','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','Misc','Yashawantha(NH)','no','','|Stop Machine & cleam the ATC,spindle after run the production','E3456','qas|','2019-05-08|','2019-05-08',NULL,NULL,NULL,NULL,NULL,NULL),(11575,'51-195','THE BOEING COMPANY','FITTING-MONOLITHIC','236310B9','65B16000-87','NA','PSDL REV C',1,'BOEING 001Z','','87628','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','DIG MARK OBSERVED ON PROFILE INNER WALL.','In op-03 special tool, shank dia20 ,relief of 16 mm T-Slot cutter used for finishing the inner wall|The required relief was 32mm min to finish the inner wall ,but the tool has 20 mm|T-Slot cutter with 20mm relief  used to finish the inner wall instead of 32mm relief |due to less relief in the tool ,the shank of the tool rubbed on the part surface ','|Correct tool with 32mm relief T-Slot cutter used for machine next part','|1.Drawing for Special Tools will be provided to the tool manufacturer ,validated by the engineering Dept\r<br/>2.The same will inspected by the tooling dept on receipt of the tool before issuing it to production.',' Wo#87630 was machined using the required tool and found all the parameters was meeting the drawing requirements	','','2019-03-07','CAD(sez)','CAD(sez)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','CAD(sez)','no','','|1.the part was identified and NCR raised.\r\n2.Correct tool with 32mm relief T-Slot cutter used for machine next part','Z3456','pe_sez||qas_sez|','2019-03-07|2019-03-07|2019-04-16|','2019-04-16',NULL,NULL,NULL,NULL,NULL,NULL),(11576,'47-195','GKN Aerospace Filton','M/C HINGE POST 5 I/A','524201','F5755517020003','NA','PART ISSUE A',1,'GKN-GS-068 PHASE2- L','','89102','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Bore over size by 1mm.','In op-02,programm No 15 the tool was not placed in the tool magzine  as per the MPS and process|As per the process in 15th program the tool should be 12X 45 chamfer tool but was 12 flat.|The operator failed to change the tool in op-02 program no 15|All the 20 programs in op-02 was taken into DNC mode while setting the first part','|1.Tool 12 flat was removed and 12x45 chamfer tool replaced\r<br/>2.All the tool pertaining to the was recalled as per the MPS and offset taken once again','|1.For setting the first part ,Check list to check the tools as per the MPS will be given to operator to check weather all the tool has be loaded in tool magazine.\r<br/>2.Instruction given to the operator to prove the setting part by proving the  program 1 by 1 instead of combining all the programs together. ','THE CAPA taken is effective and the check list is also in place.Wo #90984 machined using the check list and found ok','','2019-03-08','pe_sez(a)','Thaveni D M()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','pe_sez(a)','no','','|1.The machine was stopped \r\n2.All the tool in the machine was recalled and checked as per the MPS and process requirement and program validated\r\n','Z3456','qas_sez|qas_sez|','2019-03-08|2019-04-16|','2019-04-16',NULL,NULL,NULL,NULL,NULL,NULL),(11577,'35-473B','Saab AB','LEVER CAM','B78355 P4B6','D5227353720000','NA','PART ISSUE C',1,'OWED-LTA-003','','86617','','0000-00-00',NULL,'yes','no','yes','','yes','','','','','RUNNING TIME POWER CUT  OD DIG MARK SO PART  REJECT','During machining process dig mark occurred|Machine stopped suddenly the purpose of power cut occurred|Due to problem on UPS over heat power cut occurred|In UPS room AC was not worked properly','AC maintenance monitoring record to be create and maintain ','AC maintenance monitoring record to be create and maintain ','','','2019-03-08','Raghavendra Rao(R)','        GUNDEGOWDA H.G.','','0000-00-00','.','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','03','','','','','','UPS and AC both was checked and maintenance carried out then after that next part was loaded\r\n','E3456','qas|','2019-03-08|','2019-03-08',NULL,NULL,NULL,NULL,NULL,NULL),(11578,'47-040A','GKN Aerospace Filton','RIB 4 INTMD','2986601 6','F5755193920102','','B, MIS ISSUE F',1,'GKN GS-034 KIT -2018','','87557','','0000-00-00',NULL,'yes','yes','yes','','','','','','','WRONG WORK OFFSET TAKEN,\r\nPART HOLE 1.0MM SHIFTED  ','WHY1: During machining process wrong offset taken|WHY2: While entering the offset value, wrong value entered','|Training will be given to the operator','|Training record to be maintain','Training verified and found ok.','','2019-03-08','Gurukiran S(M)','        Govindraju NR','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','09','','','','','','|Correct offset value entered and next part found ok','E3456','pe|qas|qas|','2019-03-09|2019-03-11|2019-03-30|','2019-03-30',NULL,NULL,NULL,NULL,NULL,NULL),(11579,'51-141A','THE BOEING COMPANY','CLEVIS - UPPER, RH THREAD','534-20180618','112A7112-610','NA','PSDL REV B',1,'BOEING 001AA','','87300','','0000-00-00',NULL,'yes','no','no','no','yes','yes','no','no','no','BORE OVALITY OBSERVED  BY 0.050MM . MAX VALUE 31.77MM MEASURED 31.82MM','Cross check the CRC value in tool offset D value|Enter the correct CRC value in tool offset D value|Enter the correct CRC value in tool offset D value','|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. ','','2019-03-09','pe_sez(a)','Thaveni D M ,Nagaraju P K ,Maruthi ,Manu K,Dinakar K ,','','0000-00-00','BORE OVALITY OBSERVED  BY 0.050MM . MAX VALUE 31.77MM MEASURED 31.82MM','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','a51nx-04','qas_sez(a)','no','','|Previous part Bore value measured and ensure','Z3456','qas_sez|','2019-04-16|','2019-04-16',NULL,NULL,NULL,NULL,NULL,NULL),(11580,'51-141A','THE BOEING COMPANY','CLEVIS - UPPER, RH THREAD','534-20180618','112A7112-610','NA','PSDL REV B',2,'BOEING 001AA','','87676','','0000-00-00',NULL,'yes','no','no','no','no','yes','no','yes','no','BORE O/S IN OVALITY 0.05 &0.07MM., MAX 31.77MM MSD AS 31.82MM &31.84MM RESPECTIVELY','Refer nc no 10806|Refer nc no 10806|Refer nc no 10806|Refer nc no 10806|Refer nc no 10806','|\r<br/>Inform to operator boring operation running before clean the tool pockets and spindle.\r<br/>Every time boring operation running clean the ATC arm. ','|\r<br/>1) M0 optional program stop was provided in the program.\r<br/>2)Training provided to all operators and supervisors for visual inspections in the intermediate CNC stop to ensure no chips in the bore and tool.\r<br/>3)The same above alert was displayed near the machine','CA/PA found satisfied. ','','2019-03-09','pe_sez(a)','Ravi Kumar G.B,Manu K,Karthik Raj T ,Dinakar K ,','','0000-00-00','BORE O/S IN OVALITY 0.05 &0.07MM., MAX 31.77MM MSD AS 31.82MM &31.84MM RESPECTIVELY','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','a51nx-04','qas_sez(a)','no','','|M0 intermediate stop or optional stop was given in the program to ensure if any chips in tools and for tool cleaning. ','Z3456','qas_sez|qas_sez|','2019-04-16|2019-04-16|','2019-04-16',NULL,NULL,NULL,NULL,NULL,NULL),(11581,'47-104','GKN Aerospace Filton','BRACKET FT4 FWD','W7764','F57550777003','NA','PART ISSUE E',1,'1210042293-1','','88574','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Running time chips clogged in reamer so part hole over size by \r\n0.2mm','1) Chips clogged in reamer.|2) In- sufficient coolant supply to the reamer.|3) Due to in-sufficient length of the coolant pipe.','|Coolant supply pipe length extended in the machine.','|MO comment given in the program to instruct the operator to ensure and adjust the sufficient length of the coolant supply pipe.','CA PA found ok','','2019-03-09','Gurukiran S(M)','Shivanand(D.B.)','','0000-00-00','Part hole over size ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','09','no','Misc','Gurukiran S(M)','no','','|Checked the previous completed parts are found ok.','E3456','qas|','2019-04-01|','2019-04-01',NULL,NULL,NULL,NULL,NULL,NULL),(11582,'56-092','GKN Aerospace Orangeburg','CLEVIS FTG FWD','745412','119A1215-603','NA','PSDL REV A',1,'A000047470','','89279','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','TOOL DIG NOTICE WHEN RE ENGG TIME','the tool was over hanged |Mimi mum clamping area for the is 30 mm ,but the operator has clamped for 20 mm|The tool offset taken was not validate and compared with the log book in which previous batch tool offset was recorded|The operator didn’t follow the Instruction given in the MPS','|1.Awareness given to operators to follow the instruction given in the MPS and to follow the check list provided for setting.\r<br/>2.Intruction given to all the operators to get the check list approved from the supervisor and senior opeartors once the setting is done.','|refer to CA','Next batch machined and part found ok within the limits.WO#90092','','2019-03-09','pe_sez(a)','Umesh B,Nataraja C V,Diwakar R.B.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','yes','With Treatment','','3','no','i700-4','pe_sez(a)','no','','|1.The part was rejected and internal NCR was raised.\r\n2.2.All the tools pertaining to the program was recalled and new offset was taken.','Z3456','pe_sez|qas_sez|','2019-03-09|2019-04-16|','2019-04-16',NULL,NULL,NULL,NULL,NULL,NULL),(11583,'51-096','THE BOEING COMPANY','U JOINT','G23552K06','65B80423-3','NA','PSDL REV -',1,'BOEING 001Y','','83350','','0000-00-00',NULL,'yes','no','no','no','yes','yes','no','no','no','TOOL DIG MARK ','the tool was over hangged |Mimimum clamping area for the is 30 mm ,but the operator has clampped for 20 mm|The tool offset taken was not validate and compared with the log book in which previous batch tool offset was recorderd|The operator didn’t follow the Instruction given in the MPS','|1.Awareness given to operators to follow the instruction given in the MPS and to follow the check list provided for setting.\r<br/>2.Intruction given to all the operators to get the check list approved from the supervisor and senior opeartors once the setting is done.','|refer to CA','Next batch machined WO# 89074 and the part found within the limits','','2019-03-11','op_sez(s)','Umesh B,Nataraja C V,Diwakar R.B.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','i700-3','qas_sez(a)','no','','|1.The part was rejected and internal NCR was raised.\r\n2.2.All the tools pertaining to the programm was recalled and new offset was taken.','Z3456','qas_sez|','2019-04-16|','2019-04-16',NULL,NULL,NULL,NULL,NULL,NULL),(11584,'51-096','THE BOEING COMPANY','U JOINT','G24840K03','65B80423-3','NA','PSDL REV -',1,'BOEING 001Y','','89074','','0000-00-00',NULL,'yes','no','no','no','yes','yes','no','no','no','TOOL DIG MARKS','1.the tool was over hanged |2.Mimi mum clamping area for the is 30 mm ,but the operator has clamped for 20 mm|3.The tool offset taken was not validate and compared with the log book in which previous batch tool offset was recorded|4.The operator didn’t follow the Instruction given in the MPS','|1.Awareness given to operators to follow the instruction given in the MPS and to follow the check list provided for setting.\r<br/>2.Intruction given to all the operators to get the check list approved from the supervisor and senior opeartors once the setting is done.','|refer to CA','WO NO 89075 PARTS MACHINED , FOUND OK AND WITHIN THE LIMITS.','','2019-03-11','op_sez(s)','Umesh B,Thaveni D M ,Nataraja C V,Diwakar R.B.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','i700-3','qas_sez(a)','no','','|1.The part was rejected and internal NCR was raised\r\n2.All the tools pertaining to the program was recalled and new offset was taken.','Z3456','qas_sez|','2019-04-16|','2019-04-16',NULL,NULL,NULL,NULL,NULL,NULL),(11585,'28-046A','Magellan Aerospace New York  Inc.','SHOULDER BOLT - DOOR MECH','G24732K04','162A3109-301','NA','PL REV B, PSDL REV A',2,'A000155382','','86226','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','no','Length should be 1.078 to 1.088 Measured value is 1.0763 to 1.077 in two nos, undersized by 0.001 to .0017 out off 100 nos,.(DWG ZONE-G-6)','WHY1: During machining process offset problem occurred|WHY2: While changing the insert offset value needs to be check, but which was not taken','|Awareness to be given on operators regarding the parts first off to be carry on every insert change','|Insert changing to be monitor and reporting on a record and first off to be carry as per that','CAPA found ok.','','2019-03-11','Nandishkumar(D.K.)','Ravindra(P)','','0000-00-00','NC CREATE','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Manufacture Only','','CUST END','yes','Misc','Ravindra(P)','yes','','|The parts which are all in FG found ok, and the machining parts to be carry first off on every insert change','E3456','qas|qas|','2019-03-11|2019-04-08|','2019-04-08',NULL,NULL,NULL,NULL,NULL,NULL),(11586,'18-412A','Magellan Aerospace Wrexham','ROD END','1649138-3/XRDK','D321 53012 200','','F01',1,'175173','','85953','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Thickness under-size.','1) Chips Clogged inside the spindle|2) Aluminum chips from the previously machined parts floated due to high spindle RPM and got stuck to the oil strains of the empty pocket.|3) No protection available to avoid floating chips from entering inside the tool pockets.','|1) Informed all the operator to clean the tool pockets and spindle during every new setups.\r<br/>2) No empty pockets will be left in the machine and the empty pockets will be loaded with dummy holders to avoid entry of chips.','|Informed the maintenance department to install a Guard for the tool pockets to completely avoid the floating chips from entering the tool pocket. ','CA PA found ok.','','2019-03-11','Subramanya L(Naik)','        Naveen Kumar KM','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','05','','','','','','|Immediately stopped the machine and cleaned the machine and checked all the tool pockets and removed the chips from them.','E3456','pe|qas|qas|','2019-03-11|2019-03-12|2019-04-23|','2019-04-23',NULL,NULL,NULL,NULL,NULL,NULL),(11587,'35-259','Saab AB','SUPPORT_DEFLECT STOP','852182-13','423Z6190-3','','--A',2,'Forecast po for B787','','85731','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Profile and CHF was shifted by 0.5mm as the B axis was tilted ','During First operation tap was broken in the part|Part was re-tapped before second operation ,During referencing of second operation B axis was not made zero.|B-Axis home position reference  was not done appropriately. Thus the tilt angle in the B-axis has affected the part flatness and chamfer.','|1.B-Axis homing and reference was taken and made zero.\r<br/>2.Further machined next part and inspected found ok.','|A-axis & B-Axis homing cycle will be added in the program by revising the program and MPS.','Effectiveness will be verified for the next batch.\r\nnext part in this work order machined by taking the CAPA in consideration and the part found ok.','','2019-03-11','pe_sez(a)','        Maruthi  D R ','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','03','','','','','','|1.the part was identified and NCR was raised.\r\n2.All the previous parts in the batch inspected and found ok.','Z3456','pe_sez|qas_sez|qas_sez|','2019-03-11|2019-03-11|2019-04-16|','2019-04-16',NULL,NULL,NULL,NULL,NULL,NULL),(11588,'35-718','Saab AB','','D86939 YQE3','D5227349320700','NA','PART ISSUE E',1,'OWED-LTA-005','','87095','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','part dig mark observed .','Part got dig mark on the bottom face.|Chips from the broken tool got located under the part during the machining and caused dig mark on the part.|Tool got broken during the machining time and the operator did not cleaned the butting faces properly before loading the next part.|During the movement of semi finished material on the fixture the broken chips got relocated in between the part and the fixture.','|Informed all the operators to lift and place the part on the fixture and not to drag on the machine surface. \r<br/>','|\r<br/>Chips and scraps from the machine bed to be cleaned once in 4 Hrs in case of bigger materials. \r<br/>','CA PA found ok.','','2019-03-13','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Prashanth Kumar(M)','no','','|Immediately stopped the machine and cleaned the complete machine bed and fixture. \r\n','E3456','qas|pe|qas|','2019-03-14|2019-05-30|2019-06-03|','2019-06-03',NULL,NULL,NULL,NULL,NULL,NULL),(11589,'35-531A','Saab AB','SHAFT LATCH','B90458','D5227349020200','NA','PART ISSUE C',1,'OWED-LTA-002','','83188','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no',' Tool dig mark on the OD','1.Groove mark observed on OD for a depth of 0.5mm and width of 0.5mm\r\n\r\n\r\n|2.Machine was emergency stopped automatically due to low air pressure |3.tool was stationary and excess material removed during the idle time.','|1. Tool was changed \r<br/>2.All the tools retaining to the program ,tool offset was reset and new offset was taken and further continued production\r<br/>','|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.\r<br/>','capa found satisfactory\r\n','','2019-03-13','pe_sez(a)','Thaveni D M ,Siddesha Y.V,Sagar C.V,Pradeep B.D,Nagaraju P K ,Maruthi ,HariPrasad ,Dinakar K ,Dhanush J.K,','','0000-00-00','DIG MARK OBSERVED ON THE OD SURFACE ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','a51nx-06','qas_sez(a)','no','','|1.Machine was stopped 2.All the tools was recalled and checked for the cutting edges and rigidity of the tool','Z3456','qas_sez|qas_sez|','2019-03-14|2019-04-03|','2019-04-03',NULL,NULL,NULL,NULL,NULL,NULL),(11590,'18-091A','Magellan Aerospace(Polska) Sp','BUSH','1649123-1/X7C7','PID278 50164 202','','A',10,'104569','','81474','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','OD UNDER SIZE BY -0.02MM.','OD under size due to improper wear offset.|During insert change the operator did not properly calculated the wear correction and continued the production with out checking the part.|Due to improper awareness the operator did not ensured the dimension of the part machined after insert change.','|Informed the operator to continue production under senior operator supervision only.','|Informed the operators to carry out insert change and new settings only under the supervision of senior operators.','CA PA Found ok.','','2019-03-14','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','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','pe|qas|','2019-03-14|2019-04-08|','2019-04-08',NULL,NULL,NULL,NULL,NULL,NULL),(11591,'35-671','Saab AB','SHAFT LEVER ','4213601','D5227346221800','NA','PART ISSUE D',1,'OWED-LTA-001','','87207','','0000-00-00',NULL,'yes','yes','yes','','','','','','','OD UNDER SIZE BY -0.03MM.','1) OD undersized by 0.030mm because the insert position change during the running of part.|2) The crack generated on the insert camp during the tightening of insert resulted in insufficient clamping force and pushed the insert from its position and the operator did not notice the Development of crack in the clamp.|3) The insert clamp used was old and the tightening force was applied manually and because of which the insert clamp cracked from the bottom and resulted in poor holding of insert. ','|1) Checked all the insert clamps in the production floor and changed all the older clamps with new ones.\r<br/>2) Information given to all the operators and supervisors to remove the insert clamp and examine them for any symptoms of crack formation or presence of crack during every setup and during every insert indexing.\r<br/>','|1) To avoid excess tightening of Insert clamp torque wrench will be implemented before 20-Apr-2019.','CA PA implementation verified and found ok.','','2019-03-14','Ravi(M)','        Ashoka R','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','03','','','','','','|1) Immediately stopped the machine and checked the clamping of the part and the insert holders and identified the looseness of insert and checked the clamping and found cracked.\r\n2) Checked all the insert clamps loaded in machine for similar issue and no defect found.','E3456','pe|qas|qas|','2019-03-15|2019-03-18|2019-03-30|','2019-03-30',NULL,NULL,NULL,NULL,NULL,NULL),(11592,'35-601','Saab AB','FRAME','800397','D5227338520600','NA','PART ISSUE C',2,'OWED-LTA-001','','87354','','0000-00-00',NULL,'yes','no','yes','no','yes','no','no','no','no','bore dia 33.335+0.025 but measure value is 33.395 ','Bore size variation.|Machine axis not come to original position.|Y-Axis backlash problem.|Maybe machine ball screw wear-out.','|1)Instead of boring bar used Reamer.\r<br/>2)Avoided axis movement.','|Introduced Hole mill cum Reamer in one tool.','CAPA found ok.','','2019-03-15','Narayanappa(G)','Vasu SN,Rajesh B D,Mohan Kumar C.M.,Manjunatha N.R.,Gajendra Singh C.,Ashith B,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','7','no','HAAS VM6','Narayanappa(G)','no','','|All previous parts are checked.','E3456','qas|qas|','2019-03-16|2019-03-30|','2019-03-30',NULL,NULL,NULL,NULL,NULL,NULL),(11593,'51-184','THE BOEING COMPANY','ADAPTER, BULKHEAD - ALUMI','MA20172644','272U0021-4','NA','PSDL REV A',1,'BOEING 001Z','','88957','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','OD Undersized by 0.4mm. ','EXCESS MATERIAL WAS REMOVED IN ROUGHING OPERATION AND NO STOCK WAS PRESENCE FOR FINISHING |SINCE THE TOOL WAS NOT DISTURBED AND WAS IN RUNNING FOR THE PREVIOUS OTHER PARTS OPERATOR REFUSED TO TAKE THE OFFSET|ROUGHING TOOL TNMG160408 , OFFSET NOT TAKEN FOR THE FIRST PART','|OPERATOR WAS INSTRUCTED FOR  THE NEW PART SETTED ALL THE TOOLS HAS TO BE RECALLED AND TOOL OFFSET TO BE TAKEN ONCE AGAIN.','|CHECK LIST FOR SETTING THE NEW PART  IS IMPLEMENTED AND WHILE SETTING THE PART OPERATOR HAS TO FILL THE CHECK LIST AND THE SAME WILL BE VALIDATED BY THE SUPERVISOR ','NEXT PART MACHINED AND OD FOUND WITHIN THE LIMITS','','2019-03-16','Dinakar K()','Maruthi ,Dinakar K ,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','3','no','200MY-01','op_sez(s)','no','','|1.THE PART WAS IDENTIFIED WITH TAGE AND NC WAS RAISED\r\n2.ALL THE TOOL WAS RECALLED AND NEW OFFSET WAS TAKEN ','Z3456','qas_sez|','2019-04-03|','2019-04-03',NULL,NULL,NULL,NULL,NULL,NULL),(11594,'51A-076','THE BOEING COMPANY','ASSY - FTG, AFT FAIRING F','','112U7625-11','','PSDL REV-',2,'BOEING 001V','','K23719','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','drilling operation done on the opposite face.(dia 0.2532 to 0.2605 inch) ','The part was butted wrongly during the drilling operation after assembly.|for LH part the reference was taken but the RH part was loaded for drilling.|the operator was not able to differentiate between LH & RH part since the parts were similar.','|\r<br/>Fool Proof Machining Fixture LH and RH will be implemented for machining.Dt:15.4.2019','|\r<br/>refer to CA ','CAPA FOUND SATISFACTORY','','2019-03-16','pe_sez(a)','pe_sez(a)','','0000-00-00','drilling the holes in opposite face.(dia 0.2532 to 0.2605 inch)','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Assembly','','FINAL INSPECTION','no','Misc','pe_sez(a)','no','87644|112U7625-13','|1.All the parts rejected and NCR raised. 2.checked the Parts in WIP if any and found no parts were in WIP.','Z3456','qas_sez|qas_sez|','2019-04-04|2019-04-16|','2019-04-16',NULL,NULL,NULL,NULL,NULL,NULL),(11595,'51A-077','THE BOEING COMPANY','ASSY - FTG, AFT FAIRING F','','112U7625-12','','PSDL REV-',2,'BOEING 001V','','K23721','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','drilling operation done on the opposite face.(dia 0.2532 to 0.2605 inch)','The part was butted wrongly during the drilling operation after assembly.|for LH part the reference was taken but the RH part was loaded for drilling.|the operator was not able to differentiate between LH & RH part since the parts were similar.','|Fool Proof Machining Fixture LH and RH will be implemented for machining.Dt:15.4.2019','|refer to CA','CAPA FOUND SATISFACTORY','','2019-03-16','pe_sez(a)','pe_sez(a)','','0000-00-00','drilling the holes in opposite face.(dia 0.2532 to 0.2605 inch)','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Assembly','','FINAL INSPECTION','no','Misc','qas_sez(a)','no','','|1.All the parts rejected and NCR raised.\r\n2.checked the Parts in WIP if any and found no parts were in WIP.','Z3456','qas_sez|qas_sez|','2019-04-04|2019-04-16|','2019-04-16',NULL,NULL,NULL,NULL,NULL,NULL),(11596,'35-159','Saab AB','FLCD_DS_DEFLECT_STOP','852710-01','423Z6187-8','','---',1,'Forecast po for B787','','86901','','0000-00-00',NULL,'yes','no','yes','no','yes','no','no','no','no','Rotary Problem','During First operation tap was broken in the part|Part was re-tapped before second operation ,During referencing of second operation B axis was not made zero.|B-Axis home position reference was not done appropriately. Thus the tilt angle in the B-axis has affected the part flatness and chamfer.','|1.B-Axis homing and reference was taken and made zero.\r<br/>2.Further machined next part and inspected found ok.','|A-axis & B-Axis homing cycle will be added in the program by revising the program and MPS. ','Effectiveness will be verified for the next batch. next part in this work order machined by taking\r\nthe CAPA in consideration and the part found ok. ','','2019-03-16','pe_sez(a)','pe_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','pe_sez(a)','no','','|1.the part was identified and NCR was raised. 2.All the previous parts in the batch inspected and found ok. ','Z3456','qas_sez|','2019-04-16|','2019-04-16',NULL,NULL,NULL,NULL,NULL,NULL),(11597,'18-411A','Magellan Aerospace Wrexham','PLUNGER','CD706803/05523A','D321 40205 200','','H01',2,'175173','','87265','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','OD THREAD PROBLEM.','Double thread formation|Operator repeated the threading cycle on the same part.|operator performed rework on the part length without proper supervision.','|Informed all the operators to use proper identification tag to identify the rework parts and inform the supervisor immediately and to carry out rework under supervisor surveillance.','|Senior operators are identified per shift and are given responsibility to monitor the rework activities that are carried out without supervisor and to stop it.','CA PA found ok.','','2019-03-18','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Ravi(M)','no','','|Immediately stopped the machine and informed the supervisor.','E3456','qas|','2019-04-23|','2019-04-23',NULL,NULL,NULL,NULL,NULL,NULL),(11598,'18-680A','Magellan Aerospace Bournemouth','BARREL-STRUT','1709084-1/ZKB8','D572 50463 200','','F',1,'425753','','88846','','0000-00-00',NULL,'yes','no','yes','no','yes','no','no','no','no','POWER CUT ID THREAD DIG MARK.','1) Grove formation in the ID thread.|2) Due to power failure the slant bed of the machine resulted in the treading tool to form grove in the part.','|UPS maintenance team was called and the UPS was inspected and found ok.','|All the machines will be shifted from the power fluctuating source to the non power fluctuating source before 15-May-2019.','CA PA ok','','2019-03-18','Raghavendra Rao(R)','Rohith(M)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','05','no','Misc','Raghavendra Rao(R)','no','','|Immediately informed the supervisor and the maintenance team about the power failure and identified the rejected part with rejection tag.','E3456','qas|qas|','2019-03-18|2019-03-30|','2019-03-30',NULL,NULL,NULL,NULL,NULL,NULL),(11599,'18-686A','Magellan Aerospace Bournemouth','FORK END OUT BD','1670508-3/YZPQ','D575 41546 202','','B',1,'425753','','88537','','0000-00-00',NULL,'yes','no','yes','no','yes','no','no','no','no','POWER CUT SO OD TURNING TOOL DIG MARK.','Dig mark on OD during spear finishing operation.|Due to power cut the slant bed to slide over the part resulting in the dig mark formation.','|Reset the machine to home and verified all the work offsets and continued the production after the return of power.','|Machines will be relocated from the power fluctuating zone to the constant power supply zone before 15-May-2019.','Initially the NCR was raised considering that the part can not meet the requirement based on the MPS, later after reviewing with the Customer drawing the part was reworked after the 2nd setup completion, the parts were reinspected and found confirming to the drawing requirement. so the part is accepted and NC is closed.','','2019-03-18','Raghavendra Rao(R)','Arun Kumar(R)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','With Treatment','','03','no','Misc','Raghavendra Rao(R)','no','','|Immediately stopped the machine and informed the supervisor and the maintenance team.','E3456','qas|','2019-03-22|','2019-03-22',NULL,NULL,NULL,NULL,NULL,NULL),(11600,'47-177','GKN Aerospace Filton','BRACKET','662152A8','F5755108720002','NA','PART ISSUE F01',1,'GKN-GS-068 PHASE2- L','','87539','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','wall thickness undersized BY 2 MM','IN OP-03 WALL FINISHING WAS DONE WITH 16 R3 INSTEAD OF 12R3|OPERATOR SELECTED 12R3 INSTEAD OF 16R3|OPERATOR DID NOT NOTIFY THE TOOL ID INPUTTED IN THE PROGRAM|OPERATOR WAS NOT AWARE  OF THE FINISHING TOOL 16R3 ','|1.FIRST PART SETTING PROCEDURE WAS RE EXPLAINED TO THE OPERATOR\r<br/>2.PREPARATION OF TOOL FOR SETTING THE FIRST PART SHOULD BE DONE IN PRIOR LOADING THE PART TO THE MACHINE.','|SUPERVISOR TO VAILDIATE THE TOOLS ACCORDING TO THE TOOL DATA AVAILABLE BEFORE LOADING TO THE MACHINE.','CAPA FOUND SATISFACTORY','','2019-03-18','pe_sez(a)','Nagaraju P K()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','pe_sez(a)','no','','|1.THE PART WAS REJECTED AND NCR WAS RAISED\r\n2.CORRECT TOOL ID WAS SETTED, OFFSET TAKEN AND CONTINUED THE PRODUCTION','Z3456','qas_sez|','2019-04-03|','2019-04-03',NULL,NULL,NULL,NULL,NULL,NULL),(11601,'35-718','Saab AB','','D87797 YQE4','D5227349320700','NA','PART ISSUE E',5,'OWED-LTA-005','','87299','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Part dig mark observed .  ','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. \r<br/>','|\r<br/>Chips and scraps from the machine bed to be cleaned once in 4 Hrs in case of bigger materials. ','Next batches found ok.','','2019-03-19','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Prashanth Kumar(M)','no','','|Immediately stopped the machine and cleaned the complete machine bed and fixture. \r\n','E3456','pe|qas|','2019-05-30|2019-06-03|','2019-06-03',NULL,NULL,NULL,NULL,NULL,NULL),(11602,'35-442B','Saab AB','HINGE','C91072','D5227338720200','NA','B',3,'OWED-LTA-002','','86691','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','wire cutting  problem. (total length problem) ','During the raw material cutting cross cut the RM.|While cutting RM is not fixed properly.|RM is not clamped properly because of clamping bolt worn out.','|before starting the cutting operation verify the clamping bolts  and RM.','|Change the clamping nut with new once in a month.','CA PA found ok.','','2019-03-19','Sunil Kumar(K.R.)','SIDDESH ,Shanmukha R,Ravi R,Praveen KR,Narasimhamurthy C,Manu HB,MANJE GOWDA S,Mallikarjuna D,Hemaprakash K V,DILIP G C ,dharshan d,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','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','Deshpande|qas|qas|','2019-03-25|2019-03-27|2019-03-30|','2019-03-30',NULL,NULL,NULL,NULL,NULL,NULL),(11603,'35-411','Saab AB','BRACKET ','2291601','D5227341120000','','A',1,'OWED-LTA-001','','88686','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Outer Profile Dig.','Tool Offset Wrong.|Tool Offset Taken.\r\nMachine Value Minus & Block Value Minus -40mm & Again Block Value Minus -40MM.','|Cross Check The another Tool offsets.','|Guide The Operator About Tool Offset.','CA PA found ok.','','2019-03-20','prodn_aero(prodn)','Manjunatha.S.T(M)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Manjunatha.S.T(M)','no','','|Immediately Stop The Machine & The Tool Offset Taken Correctly.','A3456','prodn_aero|qas|','2019-03-23|2019-04-25|','2019-04-25',NULL,NULL,NULL,NULL,NULL,NULL),(11604,'47-201','GKN Aerospace Filton','SIDE ROLLER HOUSING','3436101-3','F57953065202','NA','PART ISSUE B',1,'GS68-LTA-1-2018','','84318','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dia 12.646 TO 12.664 Measured 12.684 (20 micron over size)','chips blocked inside the bore .|Coolant flowing  insufficiency.  |Coolant motor filter blocked. ','|Maintaining the monthly once coolant filter and line.','|Maintaining the monthly once coolant filter and line.','ca pa ok','','2019-03-20','prodn_aero(prodn)','Manjunatha.D()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Manjunatha.D()','no','','|Previews parts will be checked using air gauge.\r\nClean the coolant filter. ','A3456','qas|qas|','2019-03-20|2019-03-30|','2019-03-30',NULL,NULL,NULL,NULL,NULL,NULL),(11605,'35-484','Saab AB','BRACKET STOP','531882D','D522 73363 200 00','','A',1,'OWED-LTA-004','','87483','','0000-00-00',NULL,'yes','no','yes','no','yes','no','no','no','no','Tool dig mark in the part.','When program running time tool comes down (z-side).|Machine Z-axis drive fault.','','|Check the drive cooling fan monthly and revised the maintenance check list.\r<br/>After maintenance once dry run the machine.  ','CA PA found ok.','','2019-03-20','Dinesh kulal()','prodn_aero(prodn)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Dinesh kulal()','no','','|Intimidate stop the machine and inform the maintenance team.\r\nDrive cooler fan replaced and checked out.  ','A3456','qas|qas|','2019-03-20|2019-04-25|','2019-04-25',NULL,NULL,NULL,NULL,NULL,NULL),(11606,'35-717','Saab AB','','D87797 YQE4','D5227349320600','NA','PART ISSUE E',1,'OWED-LTA-005','','87298','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','part plain face dig mark, ','Part got dig mark on the bottom face.|Chips from the broken tool got located under the part during the machining and caused dig mark on the part.|Tool got broken during the machining time and the operator did not cleaned the butting faces properly before loading the next part.|During the movement of semi finished material on the fixture the broken chips got relocated in between the part and the fixture.','|Informed all the operators to lift and place the part on the fixture and not to drag on the machine surface. \r<br/>','|Chips and scraps from the machine bed to be cleaned once in 4 Hrs in case of bigger materials. \r<br/>','CA PA found ok.','','2019-03-20','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','06','no','Misc','Yashawantha(NH)','no','','|Immediately stopped the machine and cleaned the complete machine bed and fixture. \r\n','E3456','pe|qas|','2019-05-30|2019-06-03|','2019-06-03',NULL,NULL,NULL,NULL,NULL,NULL),(11607,'51-141A','THE BOEING COMPANY','CLEVIS - UPPER, RH THREAD','H29949','112A7112-610','NA','PSDL REV B',1,'BOEING 001AA','','89005','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Core Drill Insert dig mark in the Bore inner Diameter','the tool was over hanged |Mimi mum clamping area for the is 30 mm ,but the operator has clamped for 20 mm|The tool offset taken was not validate and compared with the log book in which previous batch tool offset was recorded|The operator didn’t follow the Instruction given in the MPS','|\r<br/>1.Awareness given to operators to follow the instruction given in the MPS and to follow the check list provided for setting.\r<br/>2.Intruction given to all the operators to get the check list approved from the supervisor and senior opeartors once the setting is done.','|\r<br/>Refer to CA ',' Next batch machined and part found ok with in the limits.','','2019-03-21','pe_sez(a)','Vijay Kumar H.J,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','7','no','a51nx-04','pe_sez(a)','no','','|\r\n1.The part was rejected and internal NCR was raised. 2.2.All the tools pertaining to the program was recalled and new offset was taken. ','Z3456','qas_sez|','2019-04-16|','2019-04-16',NULL,NULL,NULL,NULL,NULL,NULL),(11608,'47-099B','GKN Aerospace Filton','BRACKET M/C TRACK 2 FWD ','02316828','F57550193001','NA','PART ISSUE H02',1,'LTA-GKN-002','','89053','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Bore ovality 0.030microns ,,','1) Part to part repeatability during the boring operation was not achieved.|2) Due to Worn out axis guide in the machine the axis repeatability was affected and resulted in the repeatability of the control features. This issue was not addressed completely during the preventive maintenance.|3) Complaint regarding the axis issue was not properly registered or communicated to the maintenance team through proper feedback format.','|Feedback form was dropped in the suggestion box to formally report the maintenance issue. ','|As per the management suggestion informed the maintenance team to address the axis issue of the machine immediately.','CA PA found ok.','','2019-03-22','Guru(Kiran)','Niranjan(Murthy)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','11','no','Misc','Guru(Kiran)','no','','|Stopped the production of the forging parts and no parts with controlled features are loaded to the machine.','E3456','qas|qas|','2019-03-22|2019-03-30|','2019-03-30',NULL,NULL,NULL,NULL,NULL,NULL),(11609,'18-391B','Magellan Aerospace(Polska) Sp','END COVER','28668803-B','D278 50166 200','','A',1,'104569','','89134','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Bore dia meter 0.2mm over size....','Bore Dia over size. |Wrong Tool off-set.|Changing the insert new one. |Because of wear-out the insert.  ','|Re set the tool offset and continue the production.','|To train up the operator. ','CA PA ok','','2019-03-22','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','01','no','Misc','Sandhesh D(S)','no','','|immediately to stop the machine and verify all the parts.   ','E3456','qas|qas|','2019-03-29|2019-03-30|','2019-03-30',NULL,NULL,NULL,NULL,NULL,NULL),(11610,'47-196','GKN Aerospace Filton','M/C HINGE POST 5 I/A','524201','F5755517020103','NA','PART ISSUE A',1,'GKN-GS-068 PHASE2- L','','87115','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','Bore over size by 0.1mm.','Bore oversize.|Double side chamfer tool shank diameter rubbed the bore diameter.|Shank relief diameter not checked by operator.','|Tool changed with Relief diameter of double side chamfer tool lesser than which was used earlier. ','|1.Awareness created among operators to chack the relief diameter before running the program.\r<br/>','WO# 89103,MACHINED AND FOUND OK ','','2019-03-22','CAD(sez)','CAD(sez)','','0000-00-00','Program Fault','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','pe_sez(a)','no','','|Since this was the first part, operator informed the supervisor about the dig mark.','Z3456','qas_sez|qas_sez|','2019-03-25|2019-04-16|','2019-04-16',NULL,NULL,NULL,NULL,NULL,NULL),(11611,'18-391B','Magellan Aerospace(Polska) Sp','END COVER','28668803-B','D278 50166 200','','A',1,'104569','','89639','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','THICKNESS UNDERSIZED UPTO 0.12mm','Due to part butting problem|Chips not removed during the part loading to machine. ','|Next part butting properly and checked by the feeler gauge and run the part thickness found OK. ','|Inform to operator every part butting properly and checked by the feeler gauge and run the part. ','Next part found ok.','','2019-03-23','Dinakar(K)','Dinakar(K)','','0000-00-00','NC CREATE','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','Misc','Manjunatha(P)','no','','|Check the previous runned parts found OK','E3456','qas|','2019-05-08|','2019-05-08',NULL,NULL,NULL,NULL,NULL,NULL),(11612,'18-392B','Magellan Aerospace(Polska) Sp','END COVER','M108410/30283','D278 50167 200','','D',1,'104569','','88413','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','TOTAL LENGTH UNDER SIZE.','The insert was found to be blunt.|Then will change the insert and re offset.|Every time to check the insert in continues production. |Every 30 pisses to change the insert. ','|Every 30 pieces to change the insert.|Every 30 pieces to change the insert.','|Every 30 pieces to change the insert.','CA PA OK','','2019-03-25','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Ravi(M)','no','','|To stop the machine and check the insert.to change the insert and continue the production.|To stop the machine and check the insert.to change the insert and continue the production.','E3456','qas|qas|qas|','2019-04-26|2019-04-26|2019-04-30|','2019-04-30',NULL,NULL,NULL,NULL,NULL,NULL),(11613,'18-032A','Magellan Aerospace(Polska) Sp','BUSH','1649129-2/WXRL','PID278 50165 200','','A',5,'104569','','86931','','0000-00-00',NULL,'no','yes','yes','no','no','no','yes','no','no','CHATTERING OBSERVED IN THE OUTER DIAMETER  ','Due to wear out of insert this error was occurred. |due tools life not monitoring','|After change insert part found OK','|1)Start monitor the tool life.\r<br/>','CAPA found OK','','2019-03-25','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','01','no','Misc','Sandhesh D(S)','no','','|Change the insert  & run the production','E3456','qas|','2019-05-08|','2019-05-08',NULL,NULL,NULL,NULL,NULL,NULL),(11614,'35-601','Saab AB','FRAME','800396','D5227338520600','NA','PART ISSUE C',1,'OWED-LTA-001','','88604','','0000-00-00',NULL,'yes','yes','yes','','no','','','','','33.353 BORE 0.1 OVER SIZE ','Bore over size.|Reamer with holder 0.06 run out.|Metal chips butting in the Tool taper.|Lot-of chips stuck on the near to spindle face.   |Because of 23 Days contentiously machine running that purpose chips are sucked.   ','|Cleaning the ATC, spindle area and all tool holder taper area and continew the production. ','|Weekly once cleaning the machine.','CA PA found ok.','','2019-03-26','Narayanappa(G)','        Rajesh B D','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','7','','','','','','|Stop the machine and checked the bore, Bore is over size that  purpose remove the part .','E3456','pe|qas|qas|','2019-03-26|2019-03-27|2019-03-30|','2019-03-30',NULL,NULL,NULL,NULL,NULL,NULL),(11615,'51-140','THE BOEING COMPANY','STRUT, FWD','H7L00/177972','112A7111-601','NA','PSDL REV -',2,'BOEING 001W','','83876','','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','','2019-03-27','pe_sez(a)','pe_sez(a)','','0000-00-00','NC CREATED','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','IN PROCESS','no','Misc','pe_sez(a)','no','','|REFER NC NO:10744','Z3456','qas_sez|','2019-03-27|','2019-03-27',NULL,NULL,NULL,NULL,NULL,NULL),(11616,'35-531A','Saab AB','SHAFT LATCH','B78267 NM2Z','D5227349020200','NA','PART ISSUE C',1,'OWED-LTA-002','','87673','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Total length 341+/-0.5 ,measures 339 i;e 2 mm minus','The process of finishing the length is not robostic|for every part the operator has to check the stock in the length and enter the value in the stopper program|while entering the total length value in the stopper programs ,the operator has entered wrong value i:e minus 2mm','|Immediately Back Stopper was provided and implemented so that operator has to just butt the part in the stopper instead of entering the length dimension in the program ','|refer to CA ','next part in the batch was machined using Back stopper and the total length measured and found\r\nwithin limits wo;87673','','2019-03-27','Dinakar K()','Manu(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','05','no','Misc','pe_sez(a)','no','','|1.the part was identified and rejected and NCR raised. 2.all the previous machined parts checked and found ok. ','Z3456','qas_sez|','2019-04-09|','2019-04-09',NULL,NULL,NULL,NULL,NULL,NULL),(11617,'56-088','GKN Aerospace Orangeburg','CHANNEL FWD','0068701-2','119A1212-601','NA','NIL',1,'A000047470','','89066','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Outer flange cut out.','Outer flange cut up to  20mm .  |Wrong tool offset.  |When setting time Operator wrong enter the offset.     |1.the tool offset taken was recorded wrongly in the Log book and the same was entered into the system\r\n2.2.The offset taken was not validated in with the previous one which was recorded in the log book|3.Operator entered Wrong Tool offset  in the system and did not follow the check list provided for setting.','|Tool offset value maintaining in Note book and after  enter the machine. |1.Awareness and on job tarining was given to all the operators on following the check list provided for doing the setting\r<br/>2.Intruction given to all the operators to get the check list approved from the supervisor and senior opeartors once the setting is done.','|Maintaining in one book and cross check every time.|REFER TO CA',' WO# 90677 MACHINED AND FOUND OK  	','','2019-03-27','pe_sez(a)','pe_sez(a)','','0000-00-00','part rejected at AC SITE ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','pe_sez(a)','no','','|Enter the correct tool offset and continue the production.  |1.The part was rejected and internal NCR was raised.\r\n2.All the tools pertaining to the programm was recalled and new offset was taken.','Z3456','qas|qas_sez|','2019-03-29|2019-04-16|','2019-04-16',NULL,NULL,NULL,NULL,NULL,NULL),(11618,'47-021B','GKN Aerospace Filton','FITTING- FWD INBD','1014901 2','F57550070200','NA','PART ISSUE C01',1,'GKN GS-034 KIT -2018','','85411','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','DIA 15.875/15.890 AND DIA 22.225/22.243 BORE NOT FINISHED AS PER DRAWING.','why1: Bore diameter undersized|why2: Boring operation was not done|why3: During boring operation the finished and unfinished parts mix-up occurred|why4: Their is no proper storage area for finished and unfinished parts','|The storage area for finished and unfinished parts to be  allocate and identify those areas','|The storage area for finished and unfinished parts to be  allocate and identify those areas','','','2019-03-27','Subramanya L(Naik)','Yogesha K,Umesha ,Eranna K,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','','FI','yes','MakinoF5-3','Nagendra(SN)','no','','|The parts under machining, Inspection found ok','E3456','qas|qas|','2019-03-27|2019-03-29|','2019-03-29',NULL,NULL,NULL,NULL,NULL,NULL),(11619,'51-151','THE BOEING COMPANY','LWR SKIN COVER','R6J13/153495','312Z3122-502','NA','NIL',1,'BOEING 001X','','84716','','0000-00-00',NULL,'no','no','no','no','yes','yes','yes','no','no','Visual Discoloration on part','Chemical mark i:e Strain marks of the chemical was left uncleaned on the part after NDT|After post cleaning the part was not cleaned thoroughly by air blower','|1.Instruction given to the operators to clean the parts thoroughly after post cleaning for 3 min .\r<br/>2.Q-Alert was displayed near the line for the same.','|Refer to CA','Next Batch received from the supplier and found no evidence for Strain marks WO: 84718	','','2019-03-27','qas_sez(a)','Shivaraj K S,Sanjeev S.D,Rajesha A.R,Maruthi  D R ,Chethan Kumar M,Anand ,','','2019-03-27','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','yes','With Treatment','DN54618','FI','no','i700-5','qas_sez(a)','no','','|1.NCR was raised and the same was shared to the Supplier.\r\n2.Part was sent back to Supplier for rework','Z3456','qas_sez|','2019-04-16|','2019-04-16',NULL,NULL,NULL,NULL,NULL,NULL),(11620,'18-157A','Magellan Aerospace Wrexham','Strap Crackstopper','8791502','D572 50203 204','ABM3 1029','L',4,'175151','','80365','','0000-00-00',NULL,'yes','','yes','','','','','yes','','RUNNING TIME VACUUM PIPE CUT SO THICKNESS UNDER SIZE 0.2','While program running time part was lifted.|Because of vacuum release. |Vacuum hose pipe is broken.  |Vacuum hose pipe struck up in machine Dore.   ','|Hose pipe arranged in proper way clamped it.','|Arranged spring type hose pipe instead of old hose pipe.  |Quality alert displayed near the machine to instruct how to handle the Vacuum hose and relevant valves.','CA PA implementation verified and found ok.','','2019-03-27','Narayanappa(G)','        Vasu SN','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','03','','','','','','|Immediately to stop the machine and reset the vacuum connection. ','E3456','pe|qas|qas|qas|','2019-03-28|2019-03-28|2019-04-01|2019-04-05|','2019-04-05',NULL,NULL,NULL,NULL,NULL,NULL),(11621,'18-117B','Magellan Aerospace Bournemouth',' 	HOUSING-OUT BD BRG','1647348-2/XBDW','PID275 40004 200','','C01',1,'428867','','81751','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dig Mark & Ovality.','Part outer profile dig and ovality.|Part flow down.|Handling problem because of at at a time pick four parts. |Part pick one place to another place then flow down in Flore. ','|Pick the single single part in one time after completing the operation taking next part.  |Pick the single single part in one time after completing the operation taking next part.  |Pick the single single part in one time after completing the operation taking next part.  |Pick the single single part in one time after completing the operation taking next part.  |Pick the single single part in one time after completing the operation taking next part.  ','|Flore mat is compulsory used.    |Flore mat is compulsory used.    |Flore mat is compulsory used.    |Flore mat is compulsory used.    |Flore mat is compulsory used.    ','CA PA Found ok.','','2019-03-28','Anjinamurthy(H)','Santhosh(RH)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','13','no','Misc','Dhananjaya(N)','no','','|Immediate remaining other parts putting in a tray. |Immediate remaining other parts putting in a tray. |Immediate remaining other parts putting in a tray. |Immediate remaining other parts putting in a tray. |Immediate remaining other parts putting in a tray. ','E3456','|||||qas|','2019-03-28|2019-03-28|2019-03-28|2019-03-28|2019-03-28|2019-04-23|','2019-04-23',NULL,NULL,NULL,NULL,NULL,NULL),(11622,'56-004','GKN Aerospace Orangeburg','GAS DUMPER FITTING','155708B1','475Z3604-19','NA','NIL',1,'A000044745','','89332','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','WIDTH 137.66 MM TO 138.174MM.\r\nMEASURED 137.46 MM UNDER SIZE BY 0.20 MM.','APPROPRIATE TOOL FOR FINISHING WAS NOT USED|SAME TOOL WAS USED FOR OTHER OPERATION MANUFACTURING|TO REDUCE THE CYCLE TIME OPERATOR USED THE SAME TOOL FOR FINISHING','|SUPERVISOR TO MONITOR THE TOOLS AS PER THE TOOL DATA SHEET PROVIDED IN THE MPS','|REFER TO CA','11 NOS FOR THE SAME WORK ORDER WAS MACHINED USING APPROPRIATE TOOL AND FOUND OK ','','2019-03-30','pe_sez(a)','Somashekar ,Raghu B,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FINAL','no','Slim3n-4AHS-3','Mahesh(N)','no','','|THE PART WAS REJECTED AND THE APPROPRIATE TOOL WAS USED FOR PRODUCTION','Z3456','pe_sez|qas_sez|qas_sez|','2019-03-30|2019-03-30|2019-04-03|','2019-04-03',NULL,NULL,NULL,NULL,NULL,NULL),(11623,'56-004','GKN Aerospace Orangeburg','GAS DUMPER FITTING','155708B1','475Z3604-19','NA','NIL',11,'A000044745','','89332','','0000-00-00',NULL,'yes','no','no','no','yes','yes','no','no','no','SLOT WIDTH 14.36 MM TO 14.56 MM. \r\n\r\n14.36 MM SLIP GAUGE NOT ANSWERING IN THE SLOT.  ','Operator  checked  the slot width during the manufacturing the batch quantity of 12 nos using the vernier calliper.|Slip gauges was not used for inspection of the slot |Work instruction calls for vernier hence operator used vernier and found ok','|1.Further for all such slot tolerance ,in MPS the measuring device like slip gauges and slot gaues will be Implemented','|Engineering to include slip gaues in MPS for slot which are having close tolerance.','All the parts was reworked and checked using slip gaues and found ok','','2019-03-30','pe_sez(a)','Somashekar ,Raghu B,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','','FINAL','yes','Slim3n-4AHS-3','Mahesh(N)','no','','|Rework NCR was raised and the parts was returned to stores for rework','Z3456','qas_sez|','2019-04-02|','2019-04-02',NULL,NULL,NULL,NULL,NULL,NULL),(11624,'35-681','Saab AB','LATCH FORK','YMS4','D5227348920600','NA','PART ISSUE D',2,'OWED-LTA-003','','88100','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Part hole chatring and hole black mark.','1) Due to broken(chipped off) edge of the drill grove formation occurred in the hole.|2) Usually the drill was used for 30 pieces as per the tool life monitoring result but this time the tool broken(chipped off) for 15th piece.|3) Due to insufficient stock for the drill the tool gets vibrated while guiding through curved surface and gets braked soon.','|Changed the cutting sequence by including 6Dia free drill before the reamer operation and continued the production.','|Changed the process by drilling a 7Dia drill and then passing 7.8Dia reamer to achieve the required dimension and finish.','CA PA found ok.','','2019-03-30','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Prashanth Kumar(M)','no','','|Immediately stopped the machine and changed the cutting sequence and checked the previously completed parts and found ok.','E3456','qas|qas|','2019-04-01|2019-04-23|','2019-04-23',NULL,NULL,NULL,NULL,NULL,NULL),(11625,'51-144','THE BOEING COMPANY','STRUT, AFT','8-27-06662','112A7111-602','NA',' PSDL REV -',2,'BOEING 001AA','','88773','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Hole position shift AT 90 DEG','the part was loaded for machining in the wrong direction in op-05|there was no any instruction flow down to the operator on which direction of the part to be loaded in op-05|operator was not aware of the relation between op-04 and op-05 and how the drill orientation is related .','|Q-Alert was displayed near the machine on which direction the parts has to loaded in op-05 and the same was instructed to all the operators.','|refer to CA','Next part in this work order was proved in front of CFT team by displaying the Q-Alert near the machine.\r\nparts were found ok and the drill was as per the requirement.','','2019-03-30','Dinakar K()','pe_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','05','no','Misc','pe_sez(a)','no','','|1.the part was rejected and NCR was raised.\r\n','Z3456','qas_sez|','2019-04-09|','2019-04-09',NULL,NULL,NULL,NULL,NULL,NULL),(11626,'56-037','GKN Aerospace Orangeburg','CLOSEOUT - RIB, ANTICOLLI','709216B6','119A1442-603','NA','PSDL REV -',1,'LTA Orangeburg 737 W','','88695','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','tool dig mark observed on the profile','THE PROGRAM 56-038_0214_6BN_R01 WAS MIRRORED FOR THE PART 56-037 FROM THE COORDINATE SYSTEM INSTEAD FROM THE PLANE.|THE PROCESS OF MIRRORING THE PROGRAM WAS ADEQUATE TO THE PROGRAMMER|THE MIRRORED PROGRAM WAS NOT VALIDATED BY THE SENIOR PROGRAMMER','|ANY PROGRAM CHANGES/RE-ENGINEERING/NEW PART  SHOULD BE REVIEWED AND VALIDATED BY THE SENIOR PROGRAMMER BEFORE TRYING IT OUT ON THE MACHINE AND SHOULD BE EVIDENT(LOG BOOK)','|REFER TO CORRECTIVE ACTION ','NEXT PART MACHINE AND ALL THE PROFILE MEASURED WITH IN THE LIMITS REFER WO#89151','','2019-03-30','CAD(sez)','CAD(sez)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','pe_sez(a)','no','','|THE PROGRAM WAS REVIEWED BY SENIOR PROGRAMMER (DILIP)DATED :19/3/19 AND THE SAME WAS EXECUTED PART FOUND ACCEPTED','Z3456','qas_sez|','2019-04-03|','2019-04-03',NULL,NULL,NULL,NULL,NULL,NULL),(11627,'35-718','Saab AB','','D87797 YQE4','D5227349320700','NA','PART ISSUE E',1,'OWED-LTA-005','','87535','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','18.8E7 BORE OVER SIZE UP TO 10 TO 20 MICRON ','Running time chips clogged in reamer so part hole over size by 0.2mm| Chips clogged in reamer|In- sufficient coolant supply to the reamer.|Due to in-sufficient length of the coolant pipe.\r\n','|Coolant supply pipe length extended in the machine.\r<br/>','|MO comment given in the program to instruct the operator to ensure and adjust the sufficient length of the coolant supply pipe.\r<br/>','Code inclusion verified and found ok.','','2019-03-30','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Yashawantha(NH)','no','','|Checked the previous completed parts are found ok','E3456','pe|qas|','2019-05-30|2019-06-03|','2019-06-03',NULL,NULL,NULL,NULL,NULL,NULL),(11628,'35-404','Saab AB','BEAM 2','2731601','D522 73392 200 01','','A',2,'OWED-LTA-005','','86450','','0000-00-00',NULL,'yes','yes','yes','','','','','','','RIB UNDERSIZED','WRONG PROGRAM CALL AND RUN IN DNC MODE|The NC program loaded second time and the cycle restarted automatically and the part got dig marked on the wall during the cutout stage.','|\r<br/>Informed all the supervisors to re-check the program before stating the production. ','|Informed the Mazak Maintenance team to address this issue in the next preventive maintenance. ','CA PA found effective. Mazak team visited the plant and resolved the issue and the problem was not\r\nrepeated. ','','2019-04-01','pe_sez(a)','        Dhanush J.K','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','01','','','','','','|\r\nStopped the machine immediately and deleted the previously copied files and reloaded the correct program once again and continued the production. ','Z3456','pe_sez|qas_sez|','2019-04-01|2019-04-12|','2019-04-12',NULL,NULL,NULL,NULL,NULL,NULL),(11629,'56-037','GKN Aerospace Orangeburg','CLOSEOUT - RIB, ANTICOLLI','534311','119A1442-603','NA','PSDL REV -',4,'LTA Orangeburg 737 W','','89151','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','PART HOLES GOT oblong WHEN DRILLING DUE TO SPRING BACK ACTION ON THE LOW THICKNESS FLANGE','During Drilling program the rib was bend and after finishing it came to the original position|Program sequence for drilling was change to avoid the chatter mark and step near the hole|Inadequate process knowledge on drilling cycle to the programmer','|Awareness on the process knowledge will be strengthen to all the programmer on the requirement of the drilling and stock required for machining','|refer to Corrective action','Enough stock was maintained to avoid bend during drilling cycle  and the part in this workorder was manufactured accordingly and holes found ok and meeting the requriment.','','2019-04-01','pe_sez(a)','Umesh B,Sanjeev S.D,Nataraja C V,Diwakar R.B.,Chethan Kumar M,Anand ,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','3','no','i700-5','pe_sez(a)','no','','|The sequence in the program was changed adding the stock in the wall thickness to avoid the bend during drilling.','Z3456','qas_sez|qas_sez|','2019-04-01|2019-04-16|','2019-04-16',NULL,NULL,NULL,NULL,NULL,NULL),(11630,'51-152','THE BOEING COMPANY','PIVOT STRAP','8-19-01482-2/23540','313Z6310-501','NA','NIL',4,'BOEING 001X','','84962','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','no','PART MARKING CONTENT ENTERED WAS WRONG AS IS 313Z6410-501 \r\nS/B 313Z6310-501','The part number entered into the part marking machine was not changed during the series run of production.|Operator failed to change the part number during the series production run since the parts were similar|Part marking operator was not able to identify the part.|No instruction was flown down from the engineering to identify the similar parts.','|1.SS sheet was flown down to the supplier to identify the similar parts .\r<br/>2.Instruction given to the supplier to follow the same during part marking process.','|Refer to CA','Next batch received for the supplier and part marking found ok .','','2019-04-02','Dharani(Shankar)','Bharath(Kumar)','','0000-00-00','NC RAISED','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','DN55719','FINAL INSPECTION','yes','Misc','Bharath(Kumar)','yes','','|1.NCR was raised and sent to the supplier.\r\n2.Supplier requested to carry out the rework at our end','Z3456','qas_sez|','2019-04-16|','2019-04-16',NULL,NULL,NULL,NULL,NULL,NULL),(11631,'56-047','GKN Aerospace Orangeburg','TIP CAP','713724B3','119A1370-603','NA','PSDL REV -',1,'A000047470','','89156','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','dig on part','','','','','','2019-04-03','pe_sez(a)','Tejas M,Somashekar ,Raghu B,Madhu Kumar N,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Cancelled','no','yes','no','With Treatment','','final','no','slim3n-5AHS-1','Mahesh(N)','no','','','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11632,'28-046A','Magellan Aerospace New York  Inc.','SHOULDER BOLT - DOOR MECH','G24732K04','162A3109-301','NA','PL REV B, PSDL REV A',1,'A000155382','','86228','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Bubbling No 19 : .3125-24UNJF-3A Thread NOGO answering','OD thread damaged.|Thread damaged during the Total length rework|Operator dropped the part on the floor after the completion of rework.|X0, Y0 reference defined in the fixture did not ensure the tapper of the fixture.','|Informed the operators to carryout the rework operations only under proper supervision.','|The hole defined for the X0, Y0 offset will be enlarged to identify the tapper on the part and to avoid entering trans in the program.','CA PA FOUND OK.','','2019-04-03','Dhananjaya(N)','Venkatesh R,Santhosh Kumar N,Ravi K,Rajesh T,Raghavendra P,Narasimhamurthy C,KRISHNAMURTHY N,GUNDEGOWDA H.G.,Devaraj K.C.,','','0000-00-00','NC CREATE','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','FI','no','Fitting','Ravindra(Kumar)','no','','|Immediately stopped the machining and carried out the rework under proper supervision.','E3456','qas|qas|','2019-04-15|2019-04-30|','2019-04-30',NULL,NULL,NULL,NULL,NULL,NULL),(11633,'35-525A','Saab AB','ROD BODY','M839130-15292','D5227333620000','NA','PART ISSUE B',4,'OWED-LTA-005','','89018','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Total length 482.60+/-0.2 ,measures 480.60 i;e 2 mm minus','The process of finishing the length is not robostic|for every part the operator has to check the stock in the length and enter the value in the stopper program|while entering the total length value in the stopper programs ,the operator has entered wrong value i:e minus 2mm','|immediately Back Stopper was provided and  implemented so that operator has to just butt the part in the stopper instead of entering the length dimension in the program','|refer to CA','next part in the batch was machined using Back stopper and the total length measured and found within limits wo;89018','','2019-04-03','Dinakar K()','pe_sez(a)','','0000-00-00','Total Length Undersized','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','09','no','Misc','pe_sez(a)','no','','|1.the part was identified and rejected and NCR raised.\r\n2.all the previous machined parts checked and found ok.','Z3456','qas_sez|','2019-04-09|','2019-04-09',NULL,NULL,NULL,NULL,NULL,NULL),(11634,'18-110A','Magellan Aerospace Bournemouth','FORK END INTERMEDIATE ','CD706650/05273A','PID575 40494 202','','J',1,'428865','','88246','','0000-00-00',NULL,'yes','yes','yes','no','','no','','','','THICKNESS UNDER SIZE ','While part running time holding bush loose.|Bush not tightened properly.|Bush holding place wear out.','|Holding bush was changed.','|Every time to complete the one thousand parts to change the holding clamp. ','CA PA FOUND OK.','','2019-04-04','Subramanya L(Naik)','        Naveen Kumar KM','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','07','','','','','','|Suddenly to stop the machine and check the holding the bush.','E3456','qas|qas|','2019-04-04|2019-04-30|','2019-04-30',NULL,NULL,NULL,NULL,NULL,NULL),(11635,'35-685','Saab AB','LATCH BRACKET','Z87G','D5227347720200','NA','PART ISSUE B',2,'OWED-LTA-005','','88925','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','length under size . disrupt the setting , the job wrong tool running ','During the setting time of final operation the operator selected the profile tool and selected the chamfer program.|Operator did not completely studied the process before starting the setting.|operator selected the profile tool immediately after looking the 6dia in the chamfer program as both the profile tool and the chamfer tool starts from 6Dia.','|Checked all the program sequence and tool no\'s with respect to the process sheet and corrected the faulty ones.','|Re-training will be given to the operator on the understanding of program sequence.','CA PA FOUND OK.','','2019-04-04','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Prashanth Kumar(M)','no','','|immediately stopped the machine, informed the supervisor and changed the tool according to the program.','E3456','qas|qas|','2019-04-11|2019-04-30|','2019-04-30',NULL,NULL,NULL,NULL,NULL,NULL),(11636,'56-089','GKN Aerospace Orangeburg','CHANNEL FWD','0068701-2','119A1212-602','NA','NIL',1,'A000047470','','88688','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','*Thickness under size by 0.3mm(AERO)\r\n \r\n\r\n\r\n','1.the tool offset taken was recorded wrongly in the Log book and the same was entered into the system|2.The offset taken was not validated in with the previous one which was recorded in the log book|3.Operator entered Wrong Tool offset  in the system and did not follow the check list provided for setting.','|Awareness and on job training was given to all the operators on following the check list provided for doing the setting\r<br/>\r<br/>2.Instruction given to all the operators to get the check list approved from the supervisor and senior opeartors once the setting is done.','|REFER TO CA','Next part in this work order was resetted and the part found within the limits','','2019-04-04','pe_sez(a)','pe_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','pe_sez(a)','no','','|1.The part was rejected and internal NCR was raised\r\n2.All the tools pertaining to the program was recalled and new offset was taken.','Z3456','qas_sez|','2019-04-16|','2019-04-16',NULL,NULL,NULL,NULL,NULL,NULL),(11637,'35-266','Saab AB','LATCH PROBE','G24701K05','424Z6101-1','','--A',1,'Forecast po for B787','','84402','','0000-00-00',NULL,'yes','no','yes','no','yes','no','no','no','no','RUNNING TIME POWER TRIP TOOL DIG MARK ON THE PART ,,,','Dig mark on OD during spear finishing operation.|Due to power cut the slant bed to slide over the part resulting in the dig mark formation.','|Reset the machine to home and verified all the work offsets and continued the production after the return of power.','|To avoid by passing of power lines due to overheating air circulation systems will be adopted.','CA PA FOUND OK','','2019-04-04','Gurukiran S(M)','MANJE(GOWDA S)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','09','no','Misc','Gurukiran S(M)','no','','|Immediately stopped the machine and informed the supervisor and the maintenance team.','E3456','qas|qas|','2019-04-05|2019-04-17|','2019-04-17',NULL,NULL,NULL,NULL,NULL,NULL),(11638,'51A-007','THE BOEING COMPANY','LOWER BEAM AFT INBD SPLIC','','315Z1304-1502','','NIL',1,'BOEING 001K','','A23511','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','GANG CHANEL AND PART RIVET HOLE POSITION WAS OFFSET BY 0.50 mm','hole co-ordinates was not maintained during the finish operation|Step notice on the datum plane for depth of 0.5 mm|while removing the step material has been removed in the datum plane ','|1.100% inspection will be done for couple of batches to the repeatability of the hole co-ordinates','|Refer to CA','Next batch produced and hole coordinates found within the limits.','','2019-04-05','pe_sez(a)','pe_sez(a)','','0000-00-00','GANG CHANEL AND PART RIVET HOLE POSITION WAS OFFSET BY 0.50 mm','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Assembly','','FI','no','Misc','qas_sez(a)','no','','|1.The parts were rejected and NCR was raised','Z3456','qas_sez|','2019-04-16|','2019-04-16',NULL,NULL,NULL,NULL,NULL,NULL),(11639,'56-106','GKN Aerospace Orangeburg','FAIRING SUPPORT - FWD','5089701-1','119A1520-603','NA','PSDL REV A',1,'A000047471','','89449','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','Wall thickness under sized','1.the tool offset taken was recorded wrongly in the Log book and the same was entered into the system|2.The offset taken was not validated in with the previous one which was recorded in the log book|3.Operator entered Wrong Tool offset  in the system and did not follow the check list provided for setting.','|1.Awareness and on job training was given to all the operators on following the check list provided for doing the setting\r<br/>2.Intruction given to all the operators to get the check list approved from the supervisor and senior opeartors once the setting is done.','|REFER CA','NEXT PART IN THIS WORK ORDER WAS RESETTED BY USING THE CHECK LIST AND HE PART FOUND OK WITH IN THE LIMITS','','2019-04-05','pe_sez(a)','pe_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','pe_sez(a)','no','','|1.The part was rejected and internal NCR was raised.\r\n2.All the tools pertaining to the program was recalled and new offset was taken.','Z3456','qas_sez|','2019-04-16|','2019-04-16',NULL,NULL,NULL,NULL,NULL,NULL),(11640,'56-104','GKN Aerospace Orangeburg','CLOSEOUT - RIB, LWR, AFT','1222701-2','119A1441-607','NA','PSDL REV -',1,'A000047470','','87889','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Total length undersized','After  roughing operation  stock was not there for finishing operation|In work offset,Z-axis was kept 5mm above the required Z0 level|Operator failed to take the correct Work Offset After trying out re-engineering program|The checklist was not filled and approved after the setting of new parts was done','|The checklist provided for setting validation  must be filled and approved by concerned supervisor or Senior operator.','|refer to CA','wo 87890 machined provided with the check list for setting.  Thickness and profile checked and found within the requirement','','2019-04-05','pe_sez(a)','pe_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','pe_sez(a)','no','','|Required Work Offset was taken before continuing the rest of the programs. The next run part was found OK.','Z3456','pe_sez|qas_sez|','2019-04-05|2019-04-08|','2019-04-08',NULL,NULL,NULL,NULL,NULL,NULL),(11641,'51-198','THE BOEING COMPANY','TENSION TUBE','F00280238-0002','251A3149-902','NA','PSDL REV-',1,'BOEING 001AA','','89574','','0000-00-00',NULL,'yes','yes','yes','','','','','','','od dig 01 no','The part was not aligned with the stopper provide for butting the part.|operator failed to butt the part with the stopper and clamped the chuck.|due to lack of  negeliancy and operator was not aware of  clamping techniques ','|On-job training was conducted  to the operator by the supervisor on the clamping techniques and other key parameters of machining. ','|refer to CA','Wo# 89574 next part machined and found no evidence of dent on the part .','','2019-04-05','Dinakar K()','        Dinakar K ','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','03','','','','','','|1.the part was rejected and ncr was raised.','Z3456','pe_sez|qas_sez|','2019-04-08|2019-04-08|','2019-04-08',NULL,NULL,NULL,NULL,NULL,NULL),(11642,'35-495A','Saab AB','BRACKET','802628','D5227334920200','NA','PART ISSUE B',2,'OWED-LTA-005','','90819','','0000-00-00',NULL,'yes','yes','yes','','','','','','','PARTS ARE ACEPTED.','Dummy NCR','|Dummy NCR','','Dummy NCR','','2019-04-08','Dinakar K()','        Dinakar K ','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','','','','','1','','','','','','|Dummy NCR','Z3456','pe_sez|qas_sez|','2019-04-08|2019-04-08|','2019-04-08',NULL,NULL,NULL,NULL,NULL,NULL),(11643,'56-109','GKN Aerospace Orangeburg','FAIRING SUPPORT - L.E., M','533664-C2','119A1541-604','NA','PSDL REV -',1,'A000047470','','89176','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','Dia 10ball nose broke in running time so tool dig mark observed on the profile.','During finish operation 10 ball nose was touching the extra material and noise was occurring|In op-02 10 Ball nose Tool was not clamped as per the requirement.|The tool offset data which was recorded in the log book was not validated and compared  at the time of setting|The tool was clamped in the collect for a 25mm length instead of 30mm','|Check list for setting the part will be updated for the tool overhang length and validation of tool offset data in the log book to compare the tool offset. ','|refer to CA','For the same workorder 89176 ,all the tools was taken from the machine and re-setting was done using the check list and machined next part.part was inspected and found ok.','','2019-04-08','pe_sez(a)','Raghu(B)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','pe_sez(a)','no','','|1.Machined was stopped and a new tool 10 ball nose  was changed \r\n2.the part was rejected and NCR was raised\r\n3.Tool offset was taken for 10 ball nose and continued the production','Z3456','qas_sez|qas_sez|','2019-04-08|2019-04-10|','2019-04-10',NULL,NULL,NULL,NULL,NULL,NULL),(11644,'51-148A','THE BOEING COMPANY','UPR SKIN COVER ','H29958-Y06','312Z3121-501','NA','NIL',1,'BOEING AC001','','89780','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','DEEP STEP MARK FOUND ON EDGES OF THE PART.','1.The material was lifted at the edges where the tool has rubbed and deep mark has formed.|2.During butting the part in the machine the part was not tighten properly.|3.Operator failed to use torque tightening method while tightening.','|1.The torque tightening process was explained to the operator on how to use the torque for different bolt sizes.\r<br/>2.The required torque for different bolt size was displayed near the machine ','|Refer to CA','CAPA FOUND SATISFACTORY','','2019-04-08','qas_sez(a)','Shivaraj K S,Maruthi  D R ,Kiran Kumar M,Anand ,','','0000-00-00','STEP MARK FOUND ON EDGES OF THE PART.','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','DN55857','FI','yes','i700-3','qas_sez(a)','no','','|1.The part was identified and rework NCR was raised\r\n2.The deep step mark was removed manually by rework procedure.','Z3456','qas_sez|','2019-04-16|','2019-04-16',NULL,NULL,NULL,NULL,NULL,NULL),(11645,'18-075A','Magellan Aerospace Wrexham','ADAPTOR','M048290/27613','D282 50044 200PF','','A',1,'175162','','90310','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','ID OVER SIZE 0.030 TO 0.035mm.','1 part 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 ','|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. ','|once a week clean the ATC Shutter and information pass the all 3 shift operator, \r<br/>2.TO every part setting time to check and ensure the m/c ATC arm and shutter door \r<br/>','CAPA FOUND OK ','','2019-04-09','Narasimhamurthy(K.G.)','Manu K,Dinakar K ,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','FI','no','200MY-02','Narasimha Murthy(R)','no','','|Stop Machine & cleam the ATC,spindle after run the production ','E3456','qas|','2019-05-08|','2019-05-08',NULL,NULL,NULL,NULL,NULL,NULL),(11646,'18-210B','Magellan Aerospace Wrexham','BODY','M037880/27054','D321 40204 204','','D, ECN NR29999ST1KM15, NR29999ST2KF65, WQN DFB09775',1,'175174','','89238','','0000-00-00',NULL,'yes','yes','yes','','','','','','','OD Thread flat','1) Insert locking screw was not tightened.|2) Operator hand tightened the screw with hand and went in search of the cutting player after getting the player he just corrected the wear offset and continued the production.|3) Operator did not practiced to clamp the insert with align key and he did not checked the tightness of the insert.|4) Operator got distracted and forgot to ensure the tightness if the insert.','|Informed all the operators to check the tightness of the insert before continuing the production.','|informed the supervisors to monitor the operator until he practices to tighten the insert with align key alone.','','','2019-04-09','Raghavendra Rao(R)','        Raghavendra P','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','7','','','','','','|Immediately stopped the machine and tightened the insert and re-took the work offset and continued the production.','E3456','pe|qas|','2019-04-16|2019-04-16|','2019-04-16',NULL,NULL,NULL,NULL,NULL,NULL),(11647,'18-780A','Magellan Aerospace Wrexham','STUD AFT HINGE','A1041Z','F57551861200','NA','PART ISSUE A',1,'RP174264','','78096','','0000-00-00',NULL,'yes','yes','yes','','','','','','','part od dige mark ','Part Accepted','|Part Accepted','|Part Accepted','Part Accepted','','2019-04-09','Ravi(M)','        Ningaraj A N','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','','','','','03','','','','','','|Part Accepted','E3456','pe|qas|','2019-05-06|2019-05-08|','2019-05-08',NULL,NULL,NULL,NULL,NULL,NULL),(11648,'18-110A','Magellan Aerospace Bournemouth','FORK END INTERMEDIATE ','CD706650/05273A','PID575 40494 202','','J',2,'428865','','88246','','0000-00-00',NULL,'yes','yes','yes','','','','','','','thread damage','1) Thread holding bush over tight|2) While clamping the part in the bush part chips struck in between the threads.|3) operator did not cleaned the bush ID completely and loaded the part and continued the production because of which the thread got damaged during the clamping of part.|4) operator did not noticed the clogging of chips inside the thread.|5) operator without informing the supervisor loaded the second part on the damaged fixture and resulted in the rejection of the second part.','|Removed all the damaged bush near the machine and scraped them.','|All the operators are instructed to completely remove the bushes from the clamp and blow air both inside and outside the bush before and after loading and removing the part.','CA PA FOUND OK.','','2019-04-09','Subramanya L(Naik)','        Shivappa M B','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','7','','','','','','|immediately stopped the production and changed the damaged bush and continued the production.','E3456','pe|qas|qas|','2019-04-11|2019-04-16|2019-04-30|','2019-04-30',NULL,NULL,NULL,NULL,NULL,NULL),(11649,'35-513','Saab AB','BRACKET','2290602','D522 73459 200 00','','A',1,'OWED-LTA-002','','87375','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1.5+/-0.2 THICKNESS UNDER SIZE UP TO 5 TO 10 MICRON','1) Thickness got undersized beyond the drawing tolerance.|2) Thickness got undersized during the polishing operation.|3) 1.5mm thickness was maintained at minimum side during the machining completion and the part was not identified and separated at that stage.|4) Due to improper clamping the face did not properly butted and resulted in thickness to the minimum side. The part was sent for polishing because of the chatter marks caused due to machining strategy.|5) Due to the negligence of the operator the operator did not ensured the tightness of the part and the did not checked the thickness immediately after the completion machining.','|Informed all the operator to check the proper tightness of the clamps before starting the cycle and also to ensure the dimensions of the part immediately after the completion of cycle and inform the supervisor if any deviation found.','|Re-fresher training is arranged for all the operators to educate them on the importance of inspecting and identifying the deviated parts before moving to next operation.','CA PA FOUND OK.','','2019-04-09','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','With Treatment','','FI','no','Misc','Yashawantha(NH)','no','','|Checked the thickness and other relevant dimensions in all the completed parts and found ok.','E3456','qas|qas|qas|','2019-04-11|2019-04-15|2019-04-30|','2019-04-30',NULL,NULL,NULL,NULL,NULL,NULL),(11650,'35-404','Saab AB','BEAM 2','2731601','D522 73392 200 01','','A',2,'OWED-LTA-005','','86450','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','Program Fault','due to programs was updated. The program was not cross verified by another personnel.|due to operator demanding the new program.|due to non-available tool cutting tool because the cutting Tool flute length was shorter than the required cutting flute length.','|Will Cross check the program by another person before posting it into the machines','|Before Posting will cross check the program by another personnel','CAPA found OK','','2019-04-10','CAD(sez)','CAD(sez)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','05','no','Misc','pe_sez(a)','no','','|Cross-checked the program again and given. Next parts were found OK.','Z3456','cam|qas_sez|','2019-07-05|2019-08-27|','2019-08-27',NULL,NULL,NULL,NULL,NULL,NULL),(11651,'35-287','Saab AB','BEAM FITTING','716847B9','424Z1139-2','','--B',1,'Forecast po for B787','','89907','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Over all height minus up to 5mm','Z0 offset wrong taken|Operator initially took the offset according to the MPS then after measuring the depth from the first cut with Vernier instead of dial he got 20-micron deviation in the result because of which he changed the Z0 offset to the bottom of the fixture and continued the production without ensuring the part.|Operator did not consult with the supervisor before correcting the error.','|Informed all the operator to follow the work instructions as per MPS and in case of any doubt should contact the respective supervisors before providing corrections.','|Informed the operators to clearly study the process sheet instructions and get the doubts clarified before starting the production.','CA PA found ok','','2019-04-10','Dinesh kulal()','Manjunatha.D()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','2ND','no','Misc','Ravi nayak()','no','','|Immediately stopped the production and discussed with the senior operator and took the offset as per the MPS and checked with dial stand and continued the production.','A3456','qas|qas|','2019-04-16|2019-04-25|','2019-04-25',NULL,NULL,NULL,NULL,NULL,NULL),(11652,'18-778A','Magellan Aerospace Wrexham','BRACKET AFT M/C','1671472-2/Y9QY','F57551860200','NA','PART ISSUE A',1,'RP174264','','89142','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Bore over size.(0.02mm)','1) Drill Chipped off.|2) Proper Guide for the drill was not available.|3) Step over was left by the previous operation tool in the axis point and was not cleared.|4) Since the dia. of the drill was near to the finish diameter and due to improper guide for the drill the bore got oversize.','|Informed the operator to scribe the sharp edge of the Step over with scribe and continue the production.','|Changed the free drill size from 15.8 to 14.5 in order to build enough stock for the finishing tool and to avoid bore oversize.','CA PA FOUND OK.','','2019-04-10','Krishna(Chowdary.G.P.)','Dinakar K()','','0000-00-00','nc','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','3','no','Misc','Dhananjaya(N)','no','','|Immediately stopped the machine and changed the drill.','E3456','qas|qas|','2019-04-15|2019-04-30|','2019-04-30',NULL,NULL,NULL,NULL,NULL,NULL),(11653,'28-028A','Magellan Aerospace New York  Inc.','BUSHING SPRING GUIDE ','NSCQCC6101','141T6274-5','','PL_A + ADCN # 3 & 4, DL_N/C',60,'A000165483','','87700','','0000-00-00',NULL,'yes','no','no','no','no','no','no','yes','no','ID  .23 Inch dia to be Dia 0.251/.252 inch as per P/O Requirement. But part manufactured to Dia .23inch.','1) a) ID not achieved according to the PO requirement.\r\nb) Parts with undersized ID dimension reached customer\r\n|2) a) Part was machined according to the Drawing requirement.\r\nb) Part was machined and inspected according to the drawing not as per Po\r\n|3) a) The MPS uploaded to the CIM Soft was according to the Drawing dimension therefore the parts were machined according to the Drawing.\r\nb) Being a usual practice the operator inspected the part as per the drawing.\r\n|4) a) MPS updated with the dimension according to the Po was not uploaded to the CIM Soft.\r\nb) Inspector was not completely aware of the Customer specific requirements.\r\n|5) a) Updated MPS (MPS/28-028A _Rev-01) was not uploaded to CIM Soft.','|Process: Availability of the updated MPS as per the FAIR / Delta FAIR documentation will be confirmed by the QAD Department before providing FAIR approval to release the production Work orders in ERP.\r<br/>Quality: Additionally, Re-fresher training will be conducted to the concern inspector about the specific requirements of the customer as per CSR-EMC-001 and also instructed them to refer the PO during the final inspection to check for any additional requirements.','|Process: Availability of the updated MPS as per the FAIR / Delta FAIR documentation will be confirmed by the QAD Department before providing FAIR approval to release the production Work orders in ERP.\r<br/>Quality: Additionally, Re-fresher training will be conducted to the concern inspector about the specific requirements of the customer as per CSR-EMC-001 and also instructed them to refer the PO during the final inspection to check for any additional requirements.','Next batches produced and shipped verified and found ok.','','2019-04-10','Nandishkumar(D.K.)','Ravindra(Kumar)','RDN-224','2019-04-09','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Manufacture Only','','Cust End','yes','Misc','Ravindra(Kumar)','yes','','|1) Parts from Work Order 87700 were returned back to the production for rework as per the CIM rework procedure.\r\n2) Checked all the other Pos from customer with the MPS for specific requirements and ensured the availability of the updated MPS in the CIM Soft and found ok. (Part Nos with similar process which are checked and confirmed 65-46358-16, 161A2303-1, & 55-3575004-00)\r\n3) Immediately uploaded the updated MPS to the CIM Soft and made it available to all concern departments.','E3456','qas|','2019-05-17|','2019-05-17',NULL,NULL,NULL,NULL,NULL,NULL),(11654,'35-623A','Saab AB','SHAFT 2','788619','D5227280820000','NA','PART ISSUE A',13,'OWED-LTA-004','','89792','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','OD UNDER SIZE 0.008MM TO 0.012MM','1) Outer diameter undersized at one region.|2) ovality formation during the machining operation.|3) Eccentricity between the machine spindle and the revolving center is shifted due to historical accidents and the deviation in the eccentricity was left non-rectified,  because of which whenever the parts are machined with center support the consistency in machining was not achieved. Due to this issue the supervisor carried out trial in other two machines in the same cell in order to support the production for urgent requirement as the part proved machine was utilized for other priority job. The remaining parts got rejected during the trial process.|4) All the machines in the cell were having the same eccentricity issue.','|Informed all the supervisors to avoid producing parts in these machines that need revolving center support until the problem is rectified.','|Informed the maintenance team about the criticality of the issue and instructed to call the Authorized service personnel to solve the issue.','CA PA FOUND OK.','','2019-04-10','Sandhesh D(S)','Veerabadraswamy TB,Narasimha Murty S,Manoj Kumar D,Arun Kumar A M,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','5','no','QT100S-5','Raghavendra Rao(R)','no','','|Immediately stopped the production and informed the project engineer about the delay in production and informed the maintenance department.','E3456','qas|qas|','2019-04-24|2019-04-30|','2019-04-30',NULL,NULL,NULL,NULL,NULL,NULL),(11655,'35-588','Saab AB','LOCK SECTOR','2322601','D5227349920200','NA','PART ISSUE C',1,'OWED-LTA-003','','88723','','0000-00-00',NULL,'yes','no','no','no','no','yes','no','yes','no','TOOL DIG ON THE PART ','Running time tool was broken|due to insufficient coolant supply.|foam was flown instead of the coolant.','|informed to the coolant supplier. ','|PH level of the coolant was maintained to the required value and it was verified by the maintenance team. ',' capa found ok ','','2019-04-10','pe_sez(a)','Thaveni D M ,Pradeep B.D,Manu K,Manu ,Karthik Raj T ,Dinakar K ,Dhanush J.K,','','0000-00-00','TOOL DIG ON THE PART ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','a51nx-01','qas_sez(a)','no','','|machine was stopped ','Z3456','qas_sez|','2019-04-12|','2019-04-12',NULL,NULL,NULL,NULL,NULL,NULL),(11656,'56-108','GKN Aerospace Orangeburg','FAIRING SUPPORT - L.E., M','2430701-3','119A1541-603','NA','PSDL REV -',1,'A000047470','','88057','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','DUMMY NCR','DUMMY NCR|DUMMY NCR|DUMMY NCR|DUMMY NCR|DUMMY NCR','|DUMMY NCR','|DUMMY NCR','DUMMY NCR','','2019-04-10','pe_sez(a)','Tejas(M)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','pe_sez(a)','no','','|DUMMY NCR','Z3456','pe_sez|pe_sez|qas_sez|','2019-04-11|2019-04-11|2019-04-16|','2019-04-16',NULL,NULL,NULL,NULL,NULL,NULL),(11657,'56-108','GKN Aerospace Orangeburg','FAIRING SUPPORT - L.E., M','2430701-3','119A1541-603','NA','PSDL REV -',1,'A000047470','','88057','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','wall thickness under size by 1.5mm','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 and profile checked and found within the requirement. ','','2019-04-10','pe_sez(a)','Tejas(M)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','pe_sez(a)','no','','Required tool Offset was taken before continuing the rest of the programs. The next run part was found OK.','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11658,'47-083B','GKN Aerospace Filton','BUSH FLANGED ','T3973','F57555530200 ','NA','PART ISSUE A',1,'LTA-GKN-002','','88652','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no',' HELICAL GROOV PITCH PROBLEM.','1) Lead undersize.|2) Operator entering the pitch value instead of the lead value.|3) Because of the work center change the operator got confused with the machine input parameters.|4) Machine up gradation is needed in the FAIR machine to finish the part without any risk.','|Corrected the pitch and lead value and continued the production.','|Chart with common and differential parameters will be prepared and displayed near the machine.','CA PA FOUND OK.','','2019-04-10','Raghavendra Rao(R)','Raghavendra Rao(R)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','05','no','Misc','Raghavendra Rao(R)','no','','|Immediately stopped the machine and changed the input values.','E3456','qas|qas|','2019-04-15|2019-04-30|','2019-04-30',NULL,NULL,NULL,NULL,NULL,NULL),(11659,'56-009','GKN Aerospace Orangeburg','SPLICE PLATE FWD LWR','17802DD','119A1214-603','NA','PSDL REV-',1,'LTA GKN 737 Winglet','','89031','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Tool Dig mark Observed','the tool was over hanged |Mimi mum clamping area for the tool is 30 mm ,but the operator has clamped for 20 mm|The tool offset taken was not fed into the system ,in return the operator has inputted the old tool offset which was recorder in log book|The operator didn’t follow the Instruction given in the MPS','|Awareness given to operators to follow the instruction given in the MPS and to follow the check list provided for setting.\r<br/>2.Instruction given to all the operators to get the check list approved from the supervisor and senior opeartors once the setting is done.','|Refer to CA','next part in this work order was re setted and the part found ok and evidence for tool dig','','2019-04-11','pe_sez(a)','Upendra N()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','pe_sez(a)','no','','|1.The part was rejected and internal NCR was raised.\r\n2.All the tools pertaining to the program was recalled and new offset was taken.','Z3456','qas_sez|','2019-04-16|','2019-04-16',NULL,NULL,NULL,NULL,NULL,NULL),(11660,'51A-071A','THE BOEING COMPANY','FITTING ASSY, OUTBD','','112T7057-4','','PSDL REV -',1,'BOEING 001AB','','A23833','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Bearing Damaged','1) During the load testing after the stacking of bearing the part was not properly loaded to the fixture.|2) The holding grove on the fixture was short because of which the part slipped during the load testing operation.','|Changed the fixture and continued the testing.','|Increased the depth of the groove in the new fixture.','Next part tested with the new fixture verified and found ok.','','2019-04-11','Ramesh(D)','Nithin(S)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Assembly','','procesing','no','Misc','Ramesh(D)','no','M06315|BACB10AB10MZ','|immediately stopped the load testing and checked the bearing of the other parts and found ok.','E3456','qas|','2019-05-17|','2019-05-17',NULL,NULL,NULL,NULL,NULL,NULL),(11661,'51-153','THE BOEING COMPANY','PIVOT STRAP','8-19-01482-2/23540','313Z6310-502','NA','NIL',1,'BOEING 001X','','84974','','0000-00-00',NULL,'yes','no','no','no','yes','yes','no','no','no','THICKNESS UNDER SIZE THE NOMINAL VALUE 6.35+/-0.25MM, IS MEASURED 5.97 TO 6.23MM AND OTHER DIMENSION NOMINAL 7.62+/-  IS MEASURED 7.25 TO 7.75 ','1.the tool offset taken was recorded wrongly in the Log book and the same was entered into the system\r\n\r\n|2.The offset taken was not validated in with the previous one which was recorded in the log book|3.Operator entered Wrong Tool offset  in the system and did not follow the check list provided for setting.|\r\n','|1.Awareness and on job training was given to all the operators on following the check list provided for doing the setting\r<br/>2.Instruction given to all the operators to get the check list approved from the supervisor and senior operators once the setting is done.','|Refer to CA','Next part in this was setted according to the check list and the thickness was found within the limits','','2019-04-11','pe_sez(a)','Karthineyan V.S.,Jayanth Babu P.S,','','0000-00-00','THICKNESS UNDER SIZE THE NOMINAL VALUE 6.35+/-0.25MM, IS MEASURED 5.97 TO 6.23MM AND OTHER DIMENSION NOMINAL 7.62+/-  IS MEASURED 7.25 TO 7.75 ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','FJV 35/60-2','qas_sez(a)','no','','|1.The part was rejected and internal NCR was raised.\r\n2.All the tools pertaining to the program was recalled and new offset was taken.','Z3456','qas_sez|','2019-04-16|','2019-04-16',NULL,NULL,NULL,NULL,NULL,NULL),(11662,'35-404','Saab AB','BEAM 2','2730601','D522 73392 200 01','','A',2,'OWED-LTA-005','','86453','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Height of the part undersized by 2.00mm','1.While part running B-axis of the machine angle was changed.|2.Due to the air pressure low.|3.By knowing air pressure down by operator stop the machine but he is re-call the program again from initial stage instead of middle of the program.','|1.Instructed to operator informed to supervisor if sudden uncontrolled issues observed.\r<br/>2.Training was provided to operator to double check before intermediate program running.\r<br/>3.Ensured the tool, air pressure and any chips observing in the fixture.\r<br/>','|1.Instructed to operator informed to supervisor if sudden uncontrolled issues observed.\r<br/>2.Training was provided to operator to double check before intermediate program running.\r<br/>3.Ensured the tool, air pressure and any chips observing in the fixture.\r<br/>','CA/PA found OK and next produce part found within the acceptable limit to the drawing.','','2019-04-12','pe_sez(a)','Dhanush(J.K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','05','no','Misc','pe_sez(a)','no','','|1.Verified and inspected previous produce parts found OK.\r\n2.Reviewed and ensured no chips sticking in the fixture free from chips.\r\n','Z3456','qas_sez|','2019-04-15|','2019-04-15',NULL,NULL,NULL,NULL,NULL,NULL),(11663,'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\r\nout and bore over size. ','A chips in boring bar holder while tool changing by CNC mode in the machine so tool becomes run out and bore over size.|operator did not notice the chips in the boring holder. |The chips was very minimal and was not visible to the operatoe.','Inform to operator boring operation running before clean the tool pockets and spindle.\r<br/>Every time boring operation running clean the ATC arm. ','\r<br/>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 ','','2019-04-12','pe_sez(a)','Thaveni D M()','','0000-00-00','Bore over size','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','05','no','Misc','pe_sez(a)','no','','M00 COMMAND intermediate stop or optional stop was given in the program to ensure if any chips in tools and for tool cleaning.','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11664,'56-094','GKN Aerospace Orangeburg','CLEVIS FTG AFT','9336446','119A1215-607','NA','PSDL REV A',1,'A000047470','','89692','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Tool dig mark on the profile for a depth of 2mm on the outer surface.','The part were loaded in the wrong pallet in Mazzak machine|during machining instead of pallet number 12 wrong pallet 32 was loaded for machining in mazzak|there was instruction for the operators for any re-engineering pallet number 32 to be used.|Operator continued the production in the same pallet number 32','|1.Pallet used for machining will be incorporated in the program with the pallet number.\r<br/>2.Instruction given to the operator to validate the pallet number recorded in the reference book at production.','|Refer CA','Next part in this work order resetting done and the part found ok and evidence of tool dig.','','2019-04-15','pe_sez(a)','        Anand ','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','05','','','','','','|1.The part is rejected and NCR was raised.\r\n2.Correct pallet was called and the part was loaded and offset was taken to continued the production','Z3456','pe_sez|qas_sez|','2019-04-16|2019-04-16|','2019-04-16',NULL,NULL,NULL,NULL,NULL,NULL),(11665,'35-159','Saab AB','FLCD_DS_DEFLECT_STOP','852710-01','423Z6187-8','','---',1,'Forecast po for B787','','86901','','0000-00-00',NULL,'yes','no','yes','no','yes','no','no','no','no','Rotary Problem,\r\nProfile and CHF was shifted by 0.5mm as the B axis was tilte','During First operation tap was broken in the part|Part was re-tapped before second operation ,During referencing of second operation B axis was not made zero|B-Axis home position reference was not done appropriately. Thus the tilt angle in the B-axis has affected the part flatness and chamfer.','1.B-Axis homing and reference was taken and made zero.\r<br/>2.Further machined next part and inspected found ok.','\r<br/>A-axis & B-Axis homing cycle will be added in the program by revising the program and MPS. ','Effectiveness will be verified for the next batch. next part in this work order machined by taking\r\nthe CAPA in consideration and the part found ok. ','','2019-04-16','pe_sez(a)','pe_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','pe_sez(a)','no','','1.the part was identified and NCR was raised. 2.All the previous parts in the batch inspected and found ok','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11666,'51-096','THE BOEING COMPANY','U JOINT','G23552K06','65B80423-3','NA','PSDL REV -',1,'BOEING 001Y','','83350','','0000-00-00',NULL,'yes','no','no','no','yes','yes','no','no','no','TOOL DIG MARK ','1.the tool was over hanged |2.Mimi mum clamping area for the is 30 mm ,but the operator has clamped for 20 mm|3.The tool offset taken was not validate and compared with the log book in which previous batch tool offset was recorded|4.The operator didn’t follow the Instruction given in the MPS\r\n','1.Awareness given to operators to follow the instruction given in the MPS and to follow the check list provided for setting.\r<br/>2.Instruction given to all the operators to get the check list approved from the supervisor and senior operators once the setting is done.','refer to CA ','WO NO 89075 PARTS MACHINED , FOUND OK AND WITHIN THE LIMITS.','','2019-04-16','op_sez(s)','Umesh B,Nataraja C V,Diwakar R.B.,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','i700-3','qas_sez(a)','no','','1.The part was rejected and internal NRC was raised.\r\n2.All the tools pertaining to the program was recalled and new offset was taken.','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11667,'35-602A','Saab AB','SHAFT 1','C78776','D5227280720000','NA','PART ISSUE B',8,'OWED-LTA-004','','78470','','0000-00-00',NULL,'no','no','no','no','no','no','yes','yes','yes','plating thickness over size.\r\n','1.Parts were rejected by customer as the parts are not suiting for assembly however the platting thickness is as per the specification.\r\n|2.when processing according to the standard the thickness gets naturally built up at the edges due to the high concentration of current at edges.\r\n','1.Parts are sent to supplier for stripping and re-processing. \r<br/>','1.Informed the supplier to reduce the immersion time inside the platting tank to reduce the platting thickness and to maintain the thickness to minimum side. \r<br/>','1.Fresh batches processed to new method are verified and found ok.\r\n','C69825','2019-04-16','qas_sez(a)','qas_sez(a)','mail','2019-02-01','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','DN45606','CUSTOMER END','yes','Misc','qas_sez(a)','no','','','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11668,'35-479A','Saab AB','SHAFT','C78930.TX4X','D5227336520000','NA','PART ISSUE B',16,'OWED-LTA-004','','79076','','0000-00-00',NULL,'no','no','no','no','no','no','yes','yes','yes','Corrosion mark notes. ','Refer NC No 11424.|Refer NC No 11424.|Refer NC No 11424.|Refer NC No 11424.|Refer NC No 11424.','Refer NC No 11424.','Refer NC No 11424.','Refer NC No 11424.','C72264','2019-04-16','qas_sez(a)','qas_sez(a)','mail','2019-02-01','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','DN48058','CUSTOMER END','yes','Misc','qas_sez(a)','no','','Refer NC No 11424.','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11669,'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','Part base thickness .05mm undersize','1.the tool offset taken was recorded wrongly in the Log book and the same was entered into the system\r\n|2.The offset taken was not validated in with the previous one which was recorded in the log book\r\n|3.Operator entered Wrong Tool offset  in the system and did not follow the check list provided for setting.\r\n|\r\n','|1.Awareness and on job tarring was given to all the operators on following the check list provided for doing the setting\r<br/>2.Instruction given to all the operators to get the check list approved from the supervisor and senior operators once the setting is done.\r<br/>','|refer to ca','next batch parts are checked and verify fund OK','','2019-04-16','pe_sez(a)','op_sez(s)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','5','no','Misc','pe_sez(a)','no','','|1.The part was rejected and internal NRC was raised.\r\n2.All the tools pertaining to the program was recalled and new offset was taken.\r\n','Z3456','qas_sez|','2019-04-17|','2019-04-17',NULL,NULL,NULL,NULL,NULL,NULL),(11670,'35-604','Saab AB','SHAFT , VENT HOOKS','2878','D5227352920200','NA','PART ISSUE B',28,'OWED-LTA-004','','81913','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Total Run out required 0.1mm, measuring 0.25mm.','\r\nThe concept of measuring the run out was not enough to the inspector|The part was not butted properly while checking the run out','1.On-Job training provided to all the inspector on checking method of GD&T parameters. ','Refer CA ','Next batch machined parts found OK. ','','2019-04-16','op_sez(s)','Sagar C.V,Dinakar K ,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','With Treatment','','FI','no','100MY-01','qas_sez(a)','no','','\r\n1.All the parts was reinspected by the senior inspector and run found within the limits. 2.Parts accepted ','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11671,'35-618','Saab AB','SHAFT HANDLE ','M794860','D5227348520200','','PART ISSUE C',1,'OWED-LTA-004','','91252','','0000-00-00',NULL,'yes','','yes','','yes','','','','','POWER CUT OD DIG MARK TIME 5:00PM AIR PRESSURE LOW .........','Due to power trip the part got rejected.|Back up UPS tripped due to excess load.','|Checked for the possibility of rework in the part and found to be not meeting the drawing requirement so rejected the part.','|New dedicated UPS backup will be installed for the Turning machines.','CAPA found ok.','','2019-04-16','pe_sez(a)','        Dinakar K ','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','no','yes','','','03','','','','','','|Informed the maintained team about the issue and after the return of power checked the machine axis and continued the production.','Z3456','pe_sez|qas_sez|qas|','2019-04-17|2019-04-17|2019-05-17|','2019-05-17',NULL,NULL,NULL,NULL,NULL,NULL),(11672,'35-618','Saab AB','SHAFT HANDLE ','M794860','D5227348520200','','PART ISSUE C',1,'OWED-LTA-004','','87202','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dig mark observed on OD','The part was not aligned with the stopper provide for butting the part.|operator failed to butt the part with the stopper and clamped the chuck.|due to lack of negeliancy and operator was not aware of clamping techniques ','|On-job training was conducted to the operator by the supervisor on the clamping techniques and other key parameters of machining. ','|refer to CA ','Next part in this work order resetted and found ok to the requirements','','2019-04-17','pe_sez(a)','pe_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','07','no','Misc','pe_sez(a)','no','','|1.the part was rejected and ncr was raised. ','Z3456','qas_sez|','2019-04-17|','2019-04-17',NULL,NULL,NULL,NULL,NULL,NULL),(11673,'51-140','THE BOEING COMPANY','STRUT, FWD','H28474','112A7111-601','NA','PSDL REV -',1,'BOEING 001AA','','88790','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','ID Dig mark for a length of 10 mm and bore oversize by 1.5mm.','the insert was not clamped properly during setting |the operator did not check weather the insert is clamped tightly|The tightening of insert in the tool is not adequate|Offset was taken in the same condition ','|1.Torque tightening method  for  insert will be implemented and the same will instructed to the operator to use. ','|refer to CA','Next part in this work order resetted and the part found ok with in the requirements.','','2019-04-17','Dinakar K()','Dinakar K ,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','1','no','200MY-01','Dinakar K()','no','','|1.The part was rejected and NCR was raised\r\n2.All the tool was recalled and checked and ensured the insert is tighten rigidly','Z3456','qas_sez|','2019-04-17|','2019-04-17',NULL,NULL,NULL,NULL,NULL,NULL),(11674,'35A-545','Saab AB','BEAM ASSY','','D522 73335 000 00','','PART ISSUE A',2,'OWED-LTA-001','','A17101','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','yes','Improper Sealant squeeze out surrounding the bushes and paint touch up done has over flow on the bushes assembled and  surrounding the rivet head and tail  ','1) The fillet sealant formation around the bush was not uniform.|2) The sealant application around the bushes and the ID of the part was not uniform.|3) Sealant application was done manually therefore there was less uniformity in the formation of the squeeze out.','|Removed the bushes applied uniform amount of sealant and re-assembled.','|Training provided to the operators to apply and ensure uniform application of sealant inside the bore and the bush.','Next Batches verified and found ok.','C67482','2019-04-17','Dharani(Shankar)','Mr.Dharani','GLB415324','2019-04-12','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER END','yes','','Dharani(Shankar)','no','','|Checked similar parts in the FG and no similar defects identified.','Z3456','qas_sez|','2019-11-26|','2019-11-26','0000-00-00','0000-00-00','0000-00-00','','',''),(11675,'35A-545','Saab AB','BEAM ASSY','','D522 73335 000 00','','PART ISSUE A',30,'OWED-LTA-001','','A17135','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','yes','Improper Sealant squeeze out surrounding the bushes and paint touch up done has over flow on the\r\nbushes assembled and surrounding the rivet head and tail','1) Fillet sealant formation around the bushes and the paint touch up was not uniform.|2) Very low amount of sealant was applied to the OD of the bushes because of which the Squeeze out was not uniform to form a uniform fillet sealant.|3) Due to manual application of sealant the uniformity varies.','|Rework NCR and Rework Work order for the returned parts were raised and the Sealant and paint touch up rework were carried out accordingly and re-inspection was carried out.','|Re-fresher training conducted and sealant applying tool is implemented to ensure uniform application sealant and uniform fillet formation.','Next batches supplied verified and found ok.','C67482','2019-04-17','Dharani(Shankar)','qas_sez(a)','GLB415324','2019-04-12','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER END','yes','Misc','Dharani(Shankar)','no','','|Immediately checked all the parts in FG and in process for similar issue and all the parts were found ok.','Z3456','qas_sez|','2019-06-05|','2019-06-05',NULL,NULL,NULL,NULL,NULL,NULL),(11676,'35A-545','Saab AB','BEAM ASSY','','D522 73335 000 00','','PART ISSUE A',8,'OWED-LTA-001','','A17136','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','yes','Improper Sealant squeeze out surrounding the bushes and paint touch up done has over flow on the\r\nbushes assembled and surrounding the rivet head and tail','1) Fillet sealant formation around the bushes and the paint touch up was not uniform.|2) Very low amount of sealant was applied to the OD of the bushes because of which the Squeeze out was not uniform to form a uniform fillet sealant.|3) Due to manual application of sealant the uniformity varies.','|Rework NCR and Rework Work order for the returned parts were raised and the Sealant and paint touch up rework were carried out accordingly and re-inspection was carried out.','|Re-fresher training conducted and sealant applying tool is implemented to ensure uniform application sealant and uniform fillet formation.','Next batches supplied verified and found ok.','C67482','2019-04-17','Dharani(Shankar)','qas_sez(a)','GLB415324','2019-04-12','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER END','yes','Misc','Dharani(Shankar)','no','','|Immediately checked all the parts in FG and in process for similar issue and all the parts were found ok.','Z3456','qas_sez|','2019-06-05|','2019-06-05',NULL,NULL,NULL,NULL,NULL,NULL),(11677,'35-717','Saab AB','','D87797 YQE4','D5227349320600','NA','PART ISSUE E',3,'OWED-LTA-005','','87534','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no',' DIA 8.1H8 BORE NOGO ANSWER  ','Running time chips clogged in reamer so part hole over size by 0.02mm|Chips clogged in reamer|In- sufficient coolant supply to the reamer|In- sufficient coolant supply to the reamer','|Coolant supply pipe length extended in the machine.\r<br/>','|MO comment given in the program to instruct the operator to ensure and adjust the sufficient length of the coolant supply pipe.','M0 Code verified in program and found ok.','','2019-04-17','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','REJECT','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','06','no','Misc','Yashawantha(NH)','no','','|Checked the previous completed parts are found ok.','E3456','pe|qas|','2019-05-30|2019-06-03|','2019-06-03',NULL,NULL,NULL,NULL,NULL,NULL),(11678,'35-193','Saab AB','INTERCOSTAL CAM HOUSING','209324B3','423Z1190-1-01','','---',3,'Forecast po for B787','','77743','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Is condition: Hole too small for JIG insertion, probably due to too much colour. In two of these parts, the\r\nhole size was measured to: 28,9 mm (1.137\"). Primer locally measured in area to 150 -200 µm\r\nShould be: 1.1500\" ± 0.0020\" (29,16 - 29,26 mm) before surface treatment.','Primer thickness over size inside of the bore.|We cannot measure the coating thickness inside of the bore.|We implement the checking Gauge for ensure the bore diameter  Before treatment & after treatment.  ','|Immediately check parts in FG no such parts found & 21 nos found in treatment house in inprocess stage so we inform to the treatment supplier for ensure the parts after treatment','|\r<br/>1)We implement the checking Gauge for ensure the bore diameter  Before treatment & after treatment.\r<br/>2)Change the Hole/bore diameter tolerance zone in MPS + side only instead of +/- for all painted holes.\r<br/>3) Raise the quality alert for ensure the checking gauge for Painted bore  \r<br/>','CAPA FOUND OK','C74440','2019-04-19','qas_sez(a)','qas_sez(a)','GLB421387,GLB421598, GLB423922','2019-04-15','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','DN49886','Custemer End','yes','Misc','qas_sez(a)','no','','|Immediately check parts in FG no such parts found & 21 nos found in treatment house in inprocess stage so we inform to the treatment supplier for ensure the parts after treatment','Z3456','qas_sez|nagendra|','2019-04-25|2019-05-03|','2019-05-03',NULL,NULL,NULL,NULL,NULL,NULL),(11679,'35-308A','Saab AB','RIB INTER 3','0448502 2','F575 54797 201 00','','SCH-ISSUE B, PART ISSUE A',2,'A330 NEO FORECAST-20','','73593','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','yes','Part marking inter changed.\r\n','These are similar parts so wrong identification in treatment house|F575 54796 201 00 & F575 54797 201 00 similar parts are sent to surface treatment in same day. |As per QAD procedure once parts received to QAD complete the inspection within 2 days & move to surface treatment so parts are inspected same day then same day sent surface treatment.','|1) The deviation part got reworked by CIM & send to customer then request to for replace & return the deviated part.\r<br/>2) Get awareness & provide the CAD sheets to receiving treatment parts inspector how to identify the similar parts.\r<br/>3) We raise the NCR our treatment supplier for CAPA.\r<br/>','|1) Avoid the same day dispatch of similar parts to treatment house.\r<br/>2) Weekly once visit to treatment house for get awareness/training for identify the similar parts/LH &                                                                     RH Parts, batch Mix up, Documentations issue etc..\r<br/>3) We are internally discuss for implementation checking JIG.\r<br/>4) Raise the quality alert.\r<br/>5) Include the similar parts identification in PSIS (Parts specific information sheet) by treatment house.  \r<br/>','CA PA found ok.','C75046','2019-04-19','qas_sez(a)','qas_sez(a)','GLB422116','2019-04-17','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','DN51919','Custemer End','yes','Misc','qas_sez(a)','no','','|Cross check in our FG all similar parts found ok but 1 part 35-306A (F575 54796 201 00) found deviation. The physically part found 35-308A (F575 54797 201 00) but part marked as 35-306A (F575 54796 201 00) so quarantine the deviated part & inform to supplier.','Z3456','nagendra|qas|','2019-05-03|2019-05-17|','2019-05-17',NULL,NULL,NULL,NULL,NULL,NULL),(11680,'35-231A','Saab AB','HINGE BRACKET 4 ','2106701 3','D576 50007 208','','E00',1,'1600223433/Forecast ','','90486','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Profile Dig mark.','1) Part loaded in wrong location.|2) Part loading location defined wrongly in the reference copy that was issued to the operator.|3) MPS was not prepared by the Person who programmed and there was no proper coordination between both.','|Changed the part camping location according to the correct MPS reference copy and continued the production.','|In future both the part programing and MPS need to be designed by the same person.','CA PA Found OK.Implementation in MPS.  ','','2019-04-19','Gurukiran S(M)','        ABHISHEK M G','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','03','','','','','','|Immediately stopped the machine and informed the Engineering team.','E3456','pe|pe|pe|qas|qas|','2019-04-20|2019-04-20|2019-04-25|2019-04-26|2019-04-30|','2019-04-30',NULL,NULL,NULL,NULL,NULL,NULL),(11681,'35-404','Saab AB','BEAM 2','2731601','D522 73392 200 01','','A',2,'OWED-LTA-005','','86450','','0000-00-00',NULL,'yes','no','no','no','no','yes','no','yes','no','Bore over size by 0.030mm .max bore size 17.018 . measured up to 17.050 ','No sufficient coolant during cutting the material and the coolant nozzel was not in line with the cutting edge\r\n|During Finish Operation ,the chips clocked in the tool\r\n|for finishing operation the stock was more due to which extra material was removed and the chips was clocked in the tool \r\n|Operator didn’t notice the chips and didn’t remove it.\r\n','|1.M00 was added in the program during finishing to cross check if chips any in the tool and clean.\r<br/>2.the same was instructed to the operator to do.\r<br/>3.Coolant nozzel was adjusted on to the cutting edge\r<br/>','','NEXT PART SETTED IN THE WORKORDER ,BORE FOUND WITHIN THE LIMITS','','2019-04-22','pe_sez(a)','Thaveni D M ,Pradeep B.D,Nagaraju P K ,Manu ,HariPrasad ,Dhanush J.K,','','0000-00-00','Bore over size by 0.030mm .max bore size 17.018 . measured up to 17.050 ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','a51nx-05','qas_sez(a)','no','','|1.The tool was recalled and the cleaned thoroughly and removed the chips\r\n2.the devation part was rejected and NCR was raised\r\n','Z3456','qas_sez|','2019-04-24|','2019-04-24',NULL,NULL,NULL,NULL,NULL,NULL),(11682,'18-392B','Magellan Aerospace(Polska) Sp','END COVER','M108410/30283','D278 50167 200','','D',1,'104569','','90576','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Thickness required 6+0.1mm, which was measures 5.76mm','1) Thickness tapper.|2) Part not butted properly.|3) Chips blocked in between the butting plane.|4) Chips sticking to the jaws because of the softness of the jaws.','|Informed the operator to clean the jaws before loading the next part.','|informed the operator to rub the jaws ID with the help of scratch bright to remove small burrs that are sticky to the jaws once in 5 pieces.','CA PA FOUND OK.','','2019-04-22','Dinakar(K)','Dinakar(K)','','0000-00-00','NC creation','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','Misc','Narasimha Murthy(R)','no','','|Checked all the previously completed parts and found ok.','E3456','qas|qas|','2019-04-26|2019-04-30|','2019-04-30',NULL,NULL,NULL,NULL,NULL,NULL),(11683,'51-198','THE BOEING COMPANY','TENSION TUBE','F00280238-0002','251A3149-902','NA','PSDL REV-',2,'BOEING 001AA','','88625','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','2 QTY REJECTED IN NDT(2mm AND 1.3mm CRACK LINEAR INDICATION OBSERVED ON TH PART SURFACE)','1.Raw material problem as it is a extrusion tube.','|NA','|NA','NA','','2019-04-22','qas_sez(a)','qas_sez(a)','','0000-00-00','2 QTY REJECTED IN NDT(2mm AND 1.3mm CRACK LINEAR INDICATION OBSERVED ON TH PART SURFACE)','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','DN54460','SECONDARY PROCESS','no','Misc','qas_sez(a)','no','','|1.Inform to the material supplier and NCR raised to RM supplier.','Z3456','qas_sez|','2019-04-24|','2019-04-24',NULL,NULL,NULL,NULL,NULL,NULL),(11684,'35-618','Saab AB','SHAFT HANDLE ','M794860','D5227348520200','','PART ISSUE C',1,'OWED-LTA-004','','87009','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Fixture impression mark found on the part and OD measured minus 0.013mm on that place   ','The torque value specified for clamping was more than adequate. |The Torque  value for clamping the part was considered for solid material and the same was used for hallow material.|The torque value for clamping the Hallow part was not defined.','|Torque value for clamping was minimized from 0.2N/M to 0.15N/M','|The process of drilling and Total length finish i:e OP-05 will be planned to finish in Turning based on the output of trials and the same will be updated in the MPS.','The process of drilling and Total length finish was carried out on dummy material in turn mill center and the hole pitch,hole diameter,hole position and total length checked and found within the drawing requirements.the same will be applied for next batch and will be updated in the MPS.','','2019-04-23','pe_sez(a)','Vijay Kumar H.J,Dinakar K ,','','0000-00-00','Fixture impression mark found on the part and OD measured minus 0.013mm on that place   ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','a51nx-02','qas_sez(a)','no','','|1.the part was identified and rejected.\r\n2.The torque value was redefined by the engineering for hallow parts','Z3456','qas_sez|qas_sez|','2019-04-23|2019-04-26|','2019-04-26',NULL,NULL,NULL,NULL,NULL,NULL),(11685,'51-168','THE BOEING COMPANY','FITTING - FUEL TRANSFER, ','405301','344T2201-971','NA','PSDL REV C',1,'BOEING 001AA','','91537','','0000-00-00',NULL,'yes','','yes','','','','','yes','','program running time tool broken so wall dig mark                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                             ','During milling operation tool dig mark occurred on part|Tool holding on holder was insufficient|Due to that tool was broken and dig mark occurred on the part','|Instructions provided to the operator regarding tool holding','|training was given and training records stored','CAPA FOUND OK','','2019-04-24','pe_sez(a)','        HariPrasad ','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','03','','','','','','|Next tool was loaded as per the required length','Z3456','pe_sez|pe|pe|qas|','2019-04-25|2019-05-17|2019-05-17|2019-05-17|','2019-05-17',NULL,NULL,NULL,NULL,NULL,NULL),(11686,'51-187','THE BOEING COMPANY','BRACKET - AFT LAIRCM COOL','484712','217T4105-762','NA','NIL',1,'BOEING 001Z','','87567','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Thread NO-GO gauge answering','The thread mill used for threading was not as per the requirement.|The shank length of the thread mill used for threading  was 21mm and the part length was 20.32 |there was no relief provided in the tool and the threading operation was done for 18mm on the part and the remaining thread was done manually by tapping method |while completing the thread manually the tap selected was wrong i:e Instead of  .1640-32UNJC-3B  , .1640-32UNJC-3A was used for manual tapping ','|Correct Thread mill tool as per the requirement (shank length 25mm) was ordered and purchased to avoid manual tapping and the thread will be finished in the machine. ','|refer CA','Work orders 89220 qty-3nos & 89265 qty-3nos was machined using new thread mill length of 25mm and the parts were found OK.','','2019-04-25','pe_sez(a)','pe_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','05','no','Misc','pe_sez(a)','no','','|1.The parts was rejected and NCR was raised.','Z3456','qas_sez|','2019-04-26|','2019-04-26',NULL,NULL,NULL,NULL,NULL,NULL),(11687,'51-187','THE BOEING COMPANY','BRACKET - AFT LAIRCM COOL','484712','217T4105-762','NA','NIL',4,'BOEING 001Z','','87571','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Thread NO-GO gauge answering','refer NCR:11686|refer NCR:11686|refer NCR:11686','|refer NCR:11686','|refer NCR:11686','refer NCR:11686','','2019-04-25','pe_sez(a)','pe_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','05','no','Misc','pe_sez(a)','no','','|refer NCR:11686','Z3456','qas_sez|','2019-04-26|','2019-04-26',NULL,NULL,NULL,NULL,NULL,NULL),(11688,'56-004','GKN Aerospace Orangeburg','GAS DUMPER FITTING','717409B7','475Z3604-19','NA','NIL',1,'A000044745','','91097','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Slot width 14.45+/-0.12mm measures oversize by 0.1/0.15mm .','Chattering marks observed during slot machining due to tool over hang|Due to vibration during finishing the slot chatter marks occured|since the clearance between the spindle,part fixture was very less the tool was over hang|The tool was clamped 5mm above the required tool length','|1.The stock was provide in slot to check the slot width and finish the slot.\r<br/>2.Additional pass was added in the program to remove material slowly by 0.1mm per side to avoid chattering marks and to control the slot ','|Refer to CA ','Next Part in this work was machined as per the CA and slot found ok with in the limits.','','2019-04-30','pe_sez(a)','Somashekar()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','pe_sez(a)','no','','|1.All the parts were checked for slot width and found ok. 2.The deviation part was identified and NCR was raised ','Z3456','qas_sez|qas_sez|','2019-05-02|2019-05-22|','2019-05-22',NULL,NULL,NULL,NULL,NULL,NULL),(11689,'35-601','Saab AB','FRAME','4213601','D5227338520600','NA','PART ISSUE C',1,'OWED-LTA-001','','83952','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','3.6MM D10 hole over size','3.8 dia tool selected instead of 3.6 Dia.|Power trip during the tool change process.|Physically 3.8 dia tool is changed in machine but not updated in machine software.','|Tool pocket replace in ATC & Spindle','|During the tools change if power trip occurs,calls the tools in spindle & confirm the tool number,tool dia,etc.','CAPA Found OK','','2019-04-30','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Prashanth Kumar(M)','no','','|Stop the machine and ensure the previous runned parts found ok','E3456','qas|qas|qas|','2019-05-02|2019-05-08|2019-05-10|','2019-05-10',NULL,NULL,NULL,NULL,NULL,NULL),(11690,'35-601','Saab AB','FRAME','521026A1','D5227338520600','NA','PART ISSUE C',1,'OWED-LTA-001','','81630','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','2.4 dia hole over size','Wrong tool selected.|During this part production 10 dia end mill loaded to machine for another part rework.|Due to communication gap between shift re-leaver for unload the 10dia end mill after rework','|Change the tool 2.4 Dia instead of 10 dia end mill.','|Inform to operator before start the production once check all tools once disturbed during production running.','CAPA Found OK','','2019-04-30','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Prashanth Kumar(M)','no','','|Check the previous parts found ok','E3456','qas|qas|','2019-05-08|2019-05-10|','2019-05-10',NULL,NULL,NULL,NULL,NULL,NULL),(11691,'35-601','Saab AB','FRAME','796718','D5227338520600','NA','PART ISSUE C',1,'OWED-LTA-001','','86482','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Base thickness undersize.','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.\r<br/>','CAPA Found OK','','2019-04-30','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Prashanth Kumar(M)','no','','|Immediately stopped the machine and arranged the material so that the parts are left in free condition.','E3456','qas|qas|','2019-05-08|2019-05-10|','2019-05-10',NULL,NULL,NULL,NULL,NULL,NULL),(11692,'35-177','Saab AB','ALCD_STRUCT_BEAM-LOWER_OU','196506B0','423Z1404-5-02','','---',1,'Forecast po for B787','','89924','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Base thickness taper  and -1mm','Fixture butting problem|Because fixture not butted properly on ZPS|It was instead butted on the clamping bolt used to clamp the ZPS to bed|used the washer for clamp the fixture. ','|Part proved by removing washer and part found okay  ','|Counter bore to be done in the fixture because bolt not clamp outside of the fixture.','CAPA FOUND OK','','2019-05-02','Dinesh kulal()','Santhosh Kumar.R()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','2','no','Misc','prodn_aero(prodn)','no','','|Part proved by removing washer and part found okay  ','A3456','qas|nagendra|qas|qas|','2019-05-02|2019-05-02|2019-05-07|2019-05-07|','2019-05-07',NULL,NULL,NULL,NULL,NULL,NULL),(11693,'56-093','GKN Aerospace Orangeburg','CLEVIS FTG FWD','282769B9','119A1215-604','NA','PSDL REV A',2,'A000047469','','88355','','0000-00-00',NULL,'yes','no','yes','no','yes','no','no','no','no','Outer profile of the part is  minus by 1.25 mm which is not meeting the drawing requirement.','Aluminum block of 180mm height was used to hold the single point system due to 5 axis machining.|The aluminum block was not rigidly clamped to the pallet.|Only 2 bolts was used to clamp the aluminum block.|The aluminum block during machining has been rotated for 2 degree in angle.','|1.The Clamping block to locate the zero point system  was changed to steel for a rigid clamping of parts.\r<br/>2.Instruction given to all concern operators not to use Aluminum block for clamping zero point system.','|Refer to CA','steel block installed and parts machined ,parts found ok to the drawing requirement.Refer Wo 89280 and 89281','','2019-05-03','pe_sez(a)','pe_sez(a)','','0000-00-00','PART  PROFILE PROBLEM','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','pe_sez(a)','no','','|1.The rejected parts were identified and internal NCR was raised.\r\n2.Checked all the parts 100% for the deviation and found no such deviation.\r\n','Z3456','qas_sez|','2019-05-03|','2019-05-03',NULL,NULL,NULL,NULL,NULL,NULL),(11694,'35-257','Saab AB','BRACKET, DEFLECTION STOP','G24973K01','423Z6187-5','','---',1,'Forecast po for B787','','90601','','0000-00-00',NULL,'yes','yes','yes','','','','','','','<dummy NC>','<dummy NC>|<dummy NC>|<dummy NC>|<dummy NC>|<dummy NC>','|<dummy NC>','|<dummy NC>','dummy ncr','','2019-05-06','pe_sez(a)','        Pradeep B.D','','0000-00-00','<dummy NC>','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','03','','','','','','|<dummy NC>','Z3456','pe_sez|qas_sez|','2019-05-06|2019-05-13|','2019-05-13',NULL,NULL,NULL,NULL,NULL,NULL),(11695,'35-257','Saab AB','BRACKET, DEFLECTION STOP','G24973K01','423Z6187-5','','---',1,'Forecast po for B787','','90601','','0000-00-00',NULL,'yes','yes','yes','','','','','','','wall chamfer dig.','1.the tool offset taken was recorded wrongly in the Log book and the same was entered into the system\r\n|2.The offset taken was not validated in with the previous one which was recorded in the log book\r\n|3.Operator entered Wrong Tool offset  in the system and did not follow the check list provided for setting.\r\n','|1.Awareness and on job training was given to all the operators on following the check list provided for doing the setting\r<br/>2.Instruction given to all the operators to get the check list approved from the supervisor and senior operators once the setting is done.\r<br/>','|refer CA','next part in this workorder was resetted and the chamfer found within the drawing requriments','','2019-05-06','pe_sez(a)','        Pradeep B.D','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','03','','','','','','|1.The part was rejected and internal NCR was raised.\r\n\r\n2.All the tools pertaining to the program was recalled and new offset was taken.\r\n','Z3456','pe_sez|qas_sez|','2019-05-06|2019-05-23|','2019-05-23',NULL,NULL,NULL,NULL,NULL,NULL),(11696,'18-090A','Magellan Aerospace(Polska) Sp','BUSH','1670510-3/YT2N','PID278 50164 200','','A',2,'104569','','88734','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','COLLAR THICKNESS UNDER SIZE -0.2MM.','dummy nc','|dummy nc','|dummy nc','dummy nc','','2019-05-06','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','03','no','Misc','Ravi(M)','no','','|dummy nc','E3456','qas|','2019-05-07|','2019-05-07',NULL,NULL,NULL,NULL,NULL,NULL),(11697,'35-630','Saab AB','SUPPORT SEAL RETAINER ','272229B6','423Z1834-1-03','NA','---',1,'Forecast po for B787','','91301','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','while part running time part lifted due bolt head broken ','Bolt head broken.|Due to Bolt over tight.|For M8 bolt torque required is 40 Nmts but it has set to 80 Nmts (M10).|Guidelines chart not observed by Operator.','|Guide lines chart provided for every machine. ','|Information given to all operators.','CA PA FOUND OK.','','2019-05-06','Gurukiran S(M)','SIDDESH()','','0000-00-00','Tool dig mark observed on wall \r\n','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','09','no','Misc','Gurukiran S(M)','no','','|immediately stop the machine and take the guide lines manual ','E3456','|','2019-05-06|','2019-05-06',NULL,NULL,NULL,NULL,NULL,NULL),(11698,'18-090A','Magellan Aerospace(Polska) Sp','BUSH','1670510-3/YT2N','PID278 50164 200','','A',1,'104569','','88731','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','OD UNDER SIZE BY -0.012MM SO PART REJECTED','Due to wear out of insert OD undersized.***\r\n','|Instructed to operator for checking wear of insert in\r<br/>regular intervals and set frequency for changing inserts.\r<br/>','|Tool life was calculated in next batch and tool life was\r<br/>mentioned that part for tool.','CAPA FOUND OK','','2019-05-07','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','03','no','Misc','Raghavendra Rao(R)','no','','|check the all previous running parts and set the frequency of changing inserts.','E3456','pe|qas|qas|','2019-05-07|2019-05-08|2019-05-08|','2019-05-08',NULL,NULL,NULL,NULL,NULL,NULL),(11699,'18-090A','Magellan Aerospace(Polska) Sp','BUSH','1670510-3/YT2N','PID278 50164 200','','A',2,'104569','','88734','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','COLLAR THICKNESS UNDER SIZE -0.2MM.','1) Thickness tapper.\r\n|2) Part not butted properly.4) Chips sticking to the jaws because of the softness of the|3) Chips blocked in between the butting plane.|4) Chips sticking to the jaws because of the softness of the jaws.','Informed the operator to clean the jaws before loading the next part. ','informed the operator to rub the jaws ID with the help of scratch bright to remove small burrs that are sticky to the jaws once in 5 pieces. ','After this preventive action no such deviation parts found.','','2019-05-07','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','03','no','Misc','Ravi(M)','no','','\r\nChecked all the previously completed parts and found ok. ','E3456','qas|qas|','2019-05-08|2019-05-08|','2019-05-08',NULL,NULL,NULL,NULL,NULL,NULL),(11700,'51-140','THE BOEING COMPANY','STRUT, FWD','H30051','112A7111-601','NA','PSDL REV -',1,'BOEING 001AA','','89768','','0000-00-00',NULL,'yes','yes','yes','','','','','','','DRILL HOLE shifted to opposite side','The part was loaded in the wrong direction|operator failed to load the part in correct direction in op-02|due to operator negelancy','|1.After loading the part the operator has to check the hole diameter using pin to ensure that the part is loaded in the correct direction.\r<br/>2.Alert will be provided in the program to check the pin','|refer CA','the above said CA was evidence in front of CFT team for the remaining qty in the work and parts found OK.Instructed the supervisor to continue the same for the next batches','','2019-05-08','Dinakar K()','        Dinakar K ','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','07','','','','','','|1.The part was rejected and NCR was raised.\r\n2.Checked the previous machined parts and found ok','Z3456','pe_sez|qas_sez|','2019-05-09|2019-05-14|','2019-05-14',NULL,NULL,NULL,NULL,NULL,NULL),(11701,'35-118','Saab AB','ALCD_STRUCT_INTERCOSTAL_L','261270B3','423Z1178-3','7050-T7451 ALUMINUM ','--A',2,'Forecast po for B787','','91338','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','CHAMFER SIZE EXCEED THAN TOLERANCE VALUE IN THE BOTH SIDES OF PART.IN FIRST PART : 1.3MM-1.7MM\r\nSECOND PART: 2.3MM-2.5MM','Part lifted while chamfering operation running.|Clamping error|Butting block lifted/tapered butting block used.','|Butting block changed and two clamping sets made.','|1)Two butting block for two sets of clamping system for initial and cutout process. Till today we are not faced this problem and our team worked for giving idea to alter the chamfering and cutout program.\r<br/>Now- After full cutout (0mm), chamfering operation will run.\r<br/>Future- First 2mm relief cutout has to be run then chamfering operation will run, after these two operations 0 .2mm full cutout has to be run.  \r<br/>These were avoiding the part lifting problem.\r<br/>2. Ready the permanent clamping block for all CRN which have same process.\r<br/>','CAPA fOUND oK','','2019-05-08','Dinesh kulal()','prodn_aero(prodn)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','2nd','no','Misc','prodn_aero(prodn)','no','','|Cross check the previous production parts found ok','A3456','qas_sez|','2019-06-08|','2019-06-08',NULL,NULL,NULL,NULL,NULL,NULL),(11702,'35-588','Saab AB','LOCK SECTOR','814285','D5227349920200','NA','PART ISSUE C',1,'OWED-LTA-003','','88726','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Fixture wrong loading so part rib dig mark    ','Fixture wrong loading so part rib dig mark  |the identification on the fixture that is front and back was defined as front and forward.|Operator by mistake loaded the fixture in the forward direction but it has to be loaded in the front direction.|Multiple of setup was done in the same fixture for this part','|1.The process was proved in a dummy material and the no of setups is be reduced.Consistent of the part will be checked and the will be updated in the process sheet.','|refer to CA','The dummy part checked for all the parameters as per the drawing and found well within the limits.','','2019-05-08','Manu()','        Manu ','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','3','','','','','','|1.The Part was rejected and NCR was raised.','Z3456','pe_sez|qas_sez|qas_sez|','2019-05-08|2019-05-27|2019-06-05|','2019-06-05',NULL,NULL,NULL,NULL,NULL,NULL),(11703,'35-147','Saab AB','CED_HINGE_FTG_AFT','716504B6','425Z0302-4','7050 T7451 Per BMS 7','--A',1,'Forecast po for B787','','89913','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Bore oversize 20 micron','Tool run out presented while bore proving .|chips present in spindle |part setting time holder not present on spindle so clean the machine bed air will be sprayed so on that time chips present on spindle .\r\n','|clean the spindle and holder ','|instruction given to the operator while doing clean the bed on that time put the holder on it .','CAPA FOUND OK','','2019-05-08','prodn_aero(prodn)','prodn_aero(prodn)','','0000-00-00','Rejected in peenya site supervisior Guru kiran','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','PROD','no','Misc','prodn_aero(prodn)','no','','|clean the spindle and prove the next part ','A3456','pe|qas_aero|','2019-05-30|2019-06-08|','2019-06-08',NULL,NULL,NULL,NULL,NULL,NULL),(11704,'51-151','THE BOEING COMPANY','LWR SKIN COVER','0-24-11163/24128','312Z3122-502','NA','NIL',3,'BOEING 001X','','91275','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','HOLE DIAMETER WAS OUT OF TOLERANCE BY 0.175MM\r\nREQUIRED 0.075MM\r\nMEASURED 0.25MM\r\n','','','','','','2019-05-09','pe_sez(a)','Shivaraj K S,Maruthi  D R ,Kiran Kumar M,Kiran KM,Chethan Kumar M,Anand ,','','0000-00-00','NC RAISED','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','no','no','yes','With Treatment','','FI','no','i700-3','qas_sez(a)','no','','','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11705,'51-153','THE BOEING COMPANY','PIVOT STRAP','8-02-01297-1/24098','313Z6310-502','NA','NIL',1,'BOEING 001X','','91420','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','SCRATCH MARK FOUND ON THE PART SURFACE,','','','','','','2019-05-10','pe_sez(a)','Karthineyan V.S.,Jayanth Babu P.S,','','0000-00-00','NC RAISED','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','','FI','yes','FJV 35/60-1','qas_sez(a)','no','','','Z3456','qas_sez|','2019-06-14|','2019-06-14',NULL,NULL,NULL,NULL,NULL,NULL),(11706,'56-108','GKN Aerospace Orangeburg','FAIRING SUPPORT - L.E., M','350922','119A1541-603','NA','PSDL REV -',2,'A000047470','','90324','','0000-00-00',NULL,'yes','no','yes','no','yes','no','no','no','no','Profile and Hole position shift due to C and A axis error','The parameter was not setted as per the requirement by the Machine OEM\'S|The parameter setted by the machine OEM was changed automatically during machining in C-Axis and A-Axis','|1.all the parameters was re-adjusted by the OEM and proved \r<br/>','|refer to CA','1.Next part in this work order was re-setted and the part found ok to the drawing requirements.\r\n2.\r\n','','2019-05-10','pe_sez(a)','pe_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','01','no','Misc','pe_sez(a)','no','','|Machined was stopped and informed to the machine OEM','Z3456','qas_sez|','2019-05-14|','2019-05-14',NULL,NULL,NULL,NULL,NULL,NULL),(11707,'35-685','Saab AB','LATCH BRACKET','Z87G','D5227347720200','NA','PART ISSUE B',1,'OWED-LTA-005','','90744','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Bore over size by 0.030mm . 							\r\n','No sufficient coolant during cutting the material and the coolant nozzel was not in line with the cutting edge 							\r\n|During Finish Operation ,the chips clocked in the tool 							\r\n|for finishing operation the stock was more due to which extra material was removed and the chips was clocked in the tool 							\r\n|Operator didn’t notice the chips and didn’t remove it. 							\r\n','|1.M00 was added in the program during finishing to cross check if chips any in the tool and clean.							\r<br/>2.the same was instructed to the operator to do.							\r<br/>','|1.Coolant nozzle was adjusted on to the cutting edge							\r<br/>','CAPA FOUND OK','','2019-05-10','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Prashanth Kumar(M)','no','','|1.The tool was recalled and the cleaned thoroughly and removed the chips 2.the devation part was rejected and NCR was raised 							\r\n','E3456','pe|pe|qas_sez|','2019-05-17|2019-05-17|2019-05-24|','2019-05-24',NULL,NULL,NULL,NULL,NULL,NULL),(11708,'55-020','Spirit AeroSystems Incorporated','WEDGE,TRAILING EDGE','716504B6','113A3511-603A','NA','PSDL REV -',1,'4501352309','','92461','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','Tool Dig Mark was evident on the part which was not meeting the Required Part configuration.','Cutting tool was broken while running the program.|The program had High cutting parameter when compared to the grade of the cutting tool|The tool grade used was not the required grade.','|The Program was changed after the recommended tool parameters and grade were entered','|The grade of the tool will be considered while programming and the tool grade will be standardized across all the machines','','','2019-05-13','CAD(sez)','                        CAD(sez)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','pe_sez(a)','no','','|Part identified as rejected.The cutting parameters for similar tools was verified and was found satisfactory to the recommended tool parameters','Z3456','qas_sez|Deshpande|cam|cam|qas_sez|','2019-05-23|2019-10-18|2019-10-24|2019-10-30|2019-11-05|','2019-11-05',NULL,NULL,NULL,NULL,NULL,NULL),(11709,'18-209B','Magellan Aerospace Wrexham','BODY','M037880/27053','D321 40204 202','','D, ECN NR29999ST1KM15, NR29999ST2KF65, WQN DFB09775',1,'175173','','91635','','0000-00-00',NULL,'yes','','yes','','yes','','','','','dig mark on part profile due to machine X axis problem.','due shift in position|machine x-axis problem|due to ball screw coupling loose','|stop the machine and machine and over to maintenance department and tight the coupling screw. ','|in time maintenance at that time check the coupling.','ca/pa found OK','','2019-05-13','Subramanya L(Naik)','        Naveen Kumar KM','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','05','','','','','','|immediate stop the machine  and check the all axis reference and check the all previous completed parts.all part found OK','E3456','pe|qas|','2019-05-14|2019-05-16|','2019-05-16',NULL,NULL,NULL,NULL,NULL,NULL),(11710,'55-006','Spirit AeroSystems Incorporated','DOUBLER','1850044650','113A3434-601A','NA','PSDL REV -',1,'4501351240','','92219','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','PROFILE POINTS MEASURED OUT OF TOLERANCE\r\nrequired .01 INCH MEASURED .0587 INCHES. ','Chattering marks observed on part.|due to tool length overhang.|Required length tool is not available','|order the new tool for required length.','|Keep ready the required tools before start the FAI proving.','Next Part found OK','','2019-05-14','Ramesh(Poojary)','Sathisha(K.C.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','01','no','Misc','Nagendra(SN)','no','','|order the new tool for required length.','E3456','qas|','2019-05-20|','2019-05-20',NULL,NULL,NULL,NULL,NULL,NULL),(11711,'35A-475A','Saab AB','FRAME ASY','','D5227338400100','','B',1,'OWED-LTA-001','','A25406','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','HELICOIL INSERT IS INSERTED IN MINUS SIDE(2 THREADS) OF FROM THE PART SURFACE ','THE ENTERY CHAMFER IN THE PART WAS LESS AND DURING HELICOIL INSERT THE INSER SKIPPED AND JUMPED TO SECOND THREAD.','|THE CHAMFER WILL BE DONE AS PER THE ASSEMBLY REQUIREMENT AND THE SAME WILL BE UPDATED IN MPS','|REFER CA','THE PART IA ACCEPCTED BY QUALITY CLINIC CFT TEAM.\r\nCHAMFER WILL BE EVIDENCE IN THE NEXT BATCH OF PRODUCTION','','2019-05-14','pe_sez(a)','pe_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','Assembly','','FI','no','Misc','qas_sez(a)','no','88542|D5227338420100','|tHE PART WAS IDENTIFIED AND MOVED TO QUALITY CLINIC FOR ACCEPTANCE','Z3456','qas_sez|','2019-05-17|','2019-05-17',NULL,NULL,NULL,NULL,NULL,NULL),(11712,'56A-092','GKN Aerospace Orangeburg','CLEVIS FTG ASSY FWD','','119A1215-601','','PSDL REV A',6,'A000047469','','A22186','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','there was an issues in form ,fit function and the parts dosent match the assembly .the profile was not matching with the mating parts.','at the detail stage itself the bore position in the parts were maintained at maximum side which after assembly was not able to give correction to achieve the position in the middle side of the tolerance as only 0.5mm stock was presence in the bush|work offset was kept 0.15mm plus side for safer side in y axis direction|since the  bore position was achieved as per  the drawing given tolerance at maximum side operator refused to make the work offset zero.','|1.All the tool offset.workoffset will be validate by the senior operators based on the results of the First off report.\r<br/>2.the same instruction has been flow down to the operators.','|refer CA','Next batch machined WO #A22339 and WO#22342 all the profile and bore position were found within the middle tolerance of the drawing requirement.','C74633','2019-05-14','Mahesh(N)','Mahesh(N)','RMS181914','2019-04-08','Parts from customer end to rework purposes','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','Customer END','yes','Misc','Mahesh(N)','no','','|1.As soon as we received the complaint ,NCr was raised in our system.\r\n2.Requested customer to send back the parts to do rework.','Z3456','qas_sez|','2019-05-23|','2019-05-23',NULL,NULL,NULL,NULL,NULL,NULL),(11713,'56A-092','GKN Aerospace Orangeburg','CLEVIS FTG ASSY FWD','','119A1215-601','','PSDL REV A',7,'A000047469','','A22339','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','REFER NCR 11712','REFER NCR 11712|REFER NCR 11712|REFER NCR 11712|REFER NCR 11712|REFER NCR 11712','|REFER NCR 11712','|REFER NCR 11712','REFER NCR 11712','C74633','2019-05-14','Mahesh(N)','Mahesh(N)','RMS181914','2019-04-08','Parts returned from customer end to rework','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','Customer END','yes','Misc','Mahesh(N)','no','','|REFER NCR 11712','Z3456','qas_sez|','2019-05-23|','2019-05-23',NULL,NULL,NULL,NULL,NULL,NULL),(11714,'56A-093','GKN Aerospace Orangeburg','CLEVIS FTG ASSY FWD','','119A1215-602','','PSDL REV A',6,'A000047469','','A22342','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','REFER NCR 11712','REFER NCR 11712|REFER NCR 11712|REFER NCR 11712|REFER NCR 11712|REFER NCR 11712','|REFER NCR 11712','|REFER NCR 11712','REFER NCR 11712','C74634','2019-05-14','Mahesh(N)','Mahesh(N)','RMS181914','2019-04-08','Parts returned from customer end to rework purposes','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','Customer END','yes','Misc','Mahesh(N)','no','','|REFER NCR 11712','Z3456','qas_sez|','2019-05-23|','2019-05-23',NULL,NULL,NULL,NULL,NULL,NULL),(11715,'56A-093','GKN Aerospace Orangeburg','CLEVIS FTG ASSY FWD','','119A1215-602','','PSDL REV A',2,'A000047469','','A22343','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','REFER NCR 11712','REFER NCR 11712|REFER NCR 11712|REFER NCR 11712|REFER NCR 11712|REFER NCR 11712','|REFER NCR 11712','|REFER NCR 11712','REFER NCR 11712','C74634','2019-05-14','Mahesh(N)','Mahesh(N)','RMS181914','2019-04-08','Parts returned from customer to rework purposes','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','Customer END','yes','Misc','Mahesh(N)','no','','|REFER NCR 11712','Z3456','qas_sez|','2019-05-23|','2019-05-23',NULL,NULL,NULL,NULL,NULL,NULL),(11716,'35-525A','Saab AB','ROD BODY','M839130-15292','D5227333620000','NA','PART ISSUE B',1,'OWED-LTA-005','','91256','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Length undersized.','1.the tool offset taken was recorded wrongly in the Log book and the same was entered into the system\r\n|2.The offset taken was not validated in with the previous one which was recorded in the log book\r\n|3.Operator entered Wrong Tool offset  in the system and did not follow the check list provided for setting.\r\n','|1.Awareness and on job training was given to all the operators on following the check list provided for doing the setting\r<br/>2.Instruction given to all the operators to get the check list approved from the supervisor and senior opeartors once the setting is done.\r<br/>','|refer ca','Next part resetted in this workorder, length and other parameters found within the limits','','2019-05-16','Dinakar K()','        Dinakar K ','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','','','','','5','','','','','','|1.The part was rejected and internal NCR was raised.\r\n2.All the tools pertaining to the program was recalled and new offset was taken.\r\n','Z3456','pe_sez|qas_sez|','2019-05-17|2019-06-05|','2019-06-05',NULL,NULL,NULL,NULL,NULL,NULL),(11717,'35-474A','Saab AB','FRAME ','814244','D5227338420000','NA','A',1,'OWED-LTA-001','','88527','','0000-00-00',NULL,'yes','yes','yes','','','','','','','tool dig mark in the part top face. ','Tool dig mark |Tool offset not done|Tool offset Missing|Two tools are loaded at a time, but only 1st tool offset was measured and 2nd tool offset was not measured.','|All tools offset was cross checked and run the program.','|Introduce the check list for first part setting.','','','2019-05-16','Narayanappa(G)','        Kammar Nagaraj','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','05','','','','','','|Immediately stop the machine ','E3456','pe|qas|nandishkumardk|','2019-05-17|2019-05-17|2019-05-17|','2019-05-17',NULL,NULL,NULL,NULL,NULL,NULL),(11718,'35-495A','Saab AB','BRACKET','802628','D5227334920200','NA','PART ISSUE B',1,'OWED-LTA-005','','91948','','0000-00-00',NULL,'yes','yes','yes','','','','','','','ID OVER SIZE ','THE FINISHED PART WAS RELOADED FOR THE BORE FINISH IN  OPERATION 03|THE SEMI FINISHED AND FINISHED PARTS WERE MIXED DURING OPERATION 3|THERE WAS NO  SEPARATE BIN TO KEEP THE SEMI FINISHED AND FINISHED PARTS NEAR THE MACHINE.','|1.THE PARTS  WERE PLACED IN TWO DIFFERENT BINS NEAR THE MACHINE ONE FOR FINISHED PARTS AND THE OTHER FOR SEMI FINISHED.\r<br/>2.IN ADDITION INSTRUCTION GIVEN TO THE OPERATOR TO CHECK THE PART AND ENSURE THE STOCK PRESENCE BEFORE LOADING IT TO THE MACHINE.','|REFER CA','NEXT BATCH MACHINED BY TAKING THE ABOVE CA IN CONSIDERATION AND THE ENTIRE BATCH FOUND OK.WO  91949 QTY 114 NOS. 	','','2019-05-17','pe_sez(a)','        Dinakar K ','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','05','','','','','','|1.ALL THE PARTS WERE INSPECTED AND SEPARATED.\r\n2.THE DEVIATION PART WAS REJECTED AND NCR WAS RAISED.\r\n','Z3456','pe_sez|qas_sez|','2019-05-18|2019-05-28|','2019-05-28',NULL,NULL,NULL,NULL,NULL,NULL),(11719,'35-588','Saab AB','LOCK SECTOR','814285','D5227349920200','NA','PART ISSUE C',1,'OWED-LTA-003','','88726','','0000-00-00',NULL,'yes','no','no','no','no','yes','no','yes','no','CHECK HOLDING MARK FOUND ON THE PART SO OD BULGE  UP TO 0.15 MM. AND ID 12.7MM +0.018MM TOLERANCE . MEASURED 0.11 UNDER SIZE IN ONE END ','the chuck clamping pressure was kept more as the clamping area was very less.|clamping pressure was not defined for less holding area.','|chuck clamping pressure will be defined based on the area of clamping and the volume of the part and the same will be displayed near the machine.','|refer to CA','Next part in this work order was machined using 20ksi pressure and no clamping marks was evidence found on part ','','2019-05-18','pe_sez(a)','Ravi Kumar G.B,Pradeep B.D,Nagaraju P K ,Manu ,Karthik Raj T ,HariPrasad ,Dinakar K ,Dhanush J.K,','','0000-00-00','CHECK HOLDING MARK FOUND ON THE PART SO OD BULGE  UP TO 0.15 MM. AND ID 12.7MM +0.018MM TOLERANCE . MEASURED 0.11 UNDER SIZE IN ONE END ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','','FI','yes','200MY-01','qas_sez(a)','no','','|1.The part was rejected and ncr was raised\r\n2.Chuck pressure was reduced to 20ksi for clamping ','Z3456','qas_sez|qas_sez|','2019-05-21|2019-06-05|','2019-06-05',NULL,NULL,NULL,NULL,NULL,NULL),(11720,'51-151','THE BOEING COMPANY','LWR SKIN COVER','0-24-11163/24128','312Z3122-502','NA','NIL',2,'BOEING 001X','','90753','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','MISMATCH  FOUND ON THE PART SURFACE.','MISMATCH FOUND ON THE PART SURFACE.|Due to vibration mismatch was formed on the part surface.|The operator has not clamped the part properly.','|operators are advised to double check the clamping.','|All operators are advised to double check the clamping.','next produced parts were found ok.','','2019-05-20','pe_sez(a)','Umesh B,Shivaraj K S,Rajesha A.R,Nataraja C V,Maruthi  D R ,Kiran Kumar M,Diwakar R.B.,Chethan Kumar M,','','0000-00-00','NC RAISED ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','With Treatment','DN58106','FI','no','PS105-01','qas_sez(a)','no','','|All the remaining parts of the  same work order are inspected and found ok','Z3456','qas_sez|','2019-09-04|','2019-09-04',NULL,NULL,NULL,NULL,NULL,NULL),(11721,'35-624A','Saab AB','SHAFT 3','C87212','D5227281320000','NA','PART ISSUE B',13,'OWED-LTA-004','','73780','','0000-00-00',NULL,'yes','no','no','no','no','no','no','yes','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','2019-05-20','qas_sez(a)','qas_sez(a)','D615195','2018-12-21','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','DN41932','cust end','yes','Misc','qas_sez(a)','no','','|Refer NC No 11424.','Z3456','qas_sez|','2019-05-20|','2019-05-20',NULL,NULL,NULL,NULL,NULL,NULL),(11722,'35-624A','Saab AB','SHAFT 3','C87212','D5227281320000','NA','PART ISSUE B',14,'OWED-LTA-004','','76292','','0000-00-00',NULL,'yes','no','no','no','no','no','no','yes','yes','CORROSION OBSERVED ','Refer NC No 11424.|Refer NC No 11424.|Refer NC No 11424.|Refer NC No 11424.|Refer NC No 11424.','|Refer NC No 11424.','|Refer NC No 11424.','Refer NC No 11424.','C67912','2019-05-20','qas_sez(a)','qas_sez(a)','D615195','2018-12-21','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','DN42635','cust end','yes','Misc','qas_sez(a)','no','','|Refer NC No 11424.','Z3456','qas_sez|','2019-05-20|','2019-05-20',NULL,NULL,NULL,NULL,NULL,NULL),(11723,'35-624A','Saab AB','SHAFT 3','C87212','D5227281320000','NA','PART ISSUE B',14,'OWED-LTA-004','','76292','','0000-00-00',NULL,'yes','no','no','no','no','no','no','yes','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','2019-05-20','qas_sez(a)','qas_sez(a)','D615195','2018-12-21','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','DN42635','cust end','yes','Misc','qas_sez(a)','no','','|Refer NC No 11424.','Z3456','qas_sez|','2019-05-20|','2019-05-20',NULL,NULL,NULL,NULL,NULL,NULL),(11724,'35-624A','Saab AB','SHAFT 3','C87212','D5227281320000','NA','PART ISSUE B',16,'OWED-LTA-004','','76293','','0000-00-00',NULL,'yes','no','no','no','no','no','no','yes','yes','CORROSION OBSERVED ','Refer NC No 11424.|Refer NC No 11424.|Refer NC No 11424.|Refer NC No 11424.|Refer NC No 11424.','|Refer NC No 11424.','|Refer NC No 11424.','Refer NC No 11424.','C71974','2019-05-20','qas_sez(a)','qas_sez(a)','D615195','2018-12-21','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','DN42636','cust end','yes','Misc','qas_sez(a)','no','','|Refer NC No 11424.','Z3456','qas_sez|','2019-05-20|','2019-05-20',NULL,NULL,NULL,NULL,NULL,NULL),(11725,'35A-660','Saab AB','ASSY IN BRACKET','','D5227335100000','','PART ISSUE A',1,'OWED-LTA-005','','K17568','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','yes','paint chip out.','Paint chip-off on the part surface|Due to improper packing method the paint layer got damaged during transit.|Parts were packed one after the other with a single layer of bubble sheet wrapped around the part due to witch the paint layer on the part got damaged during transit.|Packing trials was carried out.','|Informed all the packing individuals to pack only one part in a package. ','|Informed all the packing individuals to pack only one part in a package. ','Next batch shipments monitored and found ok. ','C68084','2019-05-20','qas_sez(a)','qas_sez(a)','mail','2019-05-01','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','cust end','yes','Misc','qas_sez(a)','no','','|Immediately informed the packing team verified the packing done to similar parts and changed the method. ','Z3456','qas_sez|qas_sez|','2019-05-20|2019-05-20|','2019-05-20',NULL,NULL,NULL,NULL,NULL,NULL),(11726,'35A-660','Saab AB','ASSY IN BRACKET','','D5227335100000','','PART ISSUE A',2,'OWED-LTA-005','','K16294','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','yes','Paint chip out.','Refer CIM Nc# 11725|Refer CIM Nc# 11725|Refer CIM Nc# 11725|Refer CIM Nc# 11725|Refer CIM Nc# 11725','|Refer CIM Nc# 11725','|Refer CIM Nc# 11725','Refer CIM Nc# 11725','C68084','2019-05-20','qas_sez(a)','qas_sez(a)','mail','2019-05-01','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','cust end','yes','Misc','qas_sez(a)','no','','|Refer CIM Nc# 11725','Z3456','qas_sez|','2019-05-20|','2019-05-20',NULL,NULL,NULL,NULL,NULL,NULL),(11727,'35A-464','Saab AB','FITTING ASSY','','D522 73408 001 00','','A',1,'OWED-LTA-001','','A16254','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','yes','Is condition: Damage in paint layer. Should be: No Damage, Continuous and covering surface\r\ntreatment all over. ','Paint chip-off on the part surface|Due to improper packing method the paint layer got damaged during transit.|Parts were packed one after the other with a single layer of bubble sheet wrapped around the part due to witch the paint layer on the part got damaged during transit.|Packing trials was carried out.','|Informed all the packing individuals to pack only one part in a package. ','|\r<br/>Informed all the packing individuals to pack only one part in a package. ','Next batch shipments monitored and found ok. ','C66472','2019-05-20','qas_sez(a)','qas_sez(a)','OF-003123','2018-07-25','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','cust end','yes','Misc','qas_sez(a)','no','','|Immediately informed the packing team verified the packing done to similar parts and changed the method. ','Z3456','qas_sez|qas_sez|','2019-05-20|2019-05-20|','2019-05-20',NULL,NULL,NULL,NULL,NULL,NULL),(11728,'35A-601','Saab AB','FRAME ASSY','','D5227338501000','','PART ISSUE C',9,'OWED-LTA-001','','A17131','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','yes','Sealant has not squeezed into enough in Anchor nut,','Refer cim Nc#11194|Refer cim Nc#11194|Refer cim Nc#11194|Refer cim Nc#11194|Refer cim Nc#11194','|Refer cim Nc#11194','|Refer cim Nc#11194','Refer cim Nc#11194','C67468','2019-05-20','qas_sez(a)','qas_sez(a)',' 	OF-003153','2018-08-30','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','cust end','yes','Misc','qas_sez(a)','no','','|Refer cim Nc#11194','Z3456','qas_sez|','2019-05-20|','2019-05-20',NULL,NULL,NULL,NULL,NULL,NULL),(11729,'35A-601','Saab AB','FRAME ASSY','','D5227338501000','','PART ISSUE C',11,'OWED-LTA-001','','A17132','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','yes','Sealant has not squeezed into enough in Anchor nut','refer cim nc# 11194|refer cim nc# 11194|refer cim nc# 11194|refer cim nc# 11194|refer cim nc# 11194','|refer cim nc# 11194','|refer cim nc# 11194','refer cim nc# 11194','C67468','2019-05-20','qas_sez(a)','qas_sez(a)',' 	OF-003153','2018-08-30','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','cust end','yes','Misc','qas_sez(a)','no','','|refer cim nc# 11194','Z3456','qas_sez|','2019-05-20|','2019-05-20',NULL,NULL,NULL,NULL,NULL,NULL),(11730,'35A-601','Saab AB','FRAME ASSY','','D5227338501000','','PART ISSUE C',13,'OWED-LTA-001','','A17133','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','yes',' Sealant has not squeezed into enough in Anchor nut','Refer CIM nc#11194|Refer CIM nc#11194|Refer CIM nc#11194|Refer CIM nc#11194|Refer CIM nc#11194','|Refer CIM nc#11194','|Refer CIM nc#11194','Refer CIM nc#11194','C67468','2019-05-20','qas_sez(a)','qas_sez(a)','OF-003153','2018-08-30','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','cust end','yes','Misc','qas_sez(a)','no','','|Refer CIM nc#11194','Z3456','qas_sez|','2019-05-20|','2019-05-20',NULL,NULL,NULL,NULL,NULL,NULL),(11731,'35A-608A','Saab AB','LEVER ASSY','','D5227335200200','','PART ISSUE C',30,'OWED-LTA-005','','A21262','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','yes','Paint application not done. ','1) Paint application inside the bore was not done.|2) The paint application requirement was not properly captured during the FAIR documentation.|3) In the previous issue the entire bore was required mashing but in the latest issue of drawing the requirement was changed to mask only to a specific length and the ECN (Engineering change note) did not demonstrated this requirement.','|Requested customer to return the parts back to CIM and the bush assembled are dis-assembled and sent to ATPL for paint application inside the bore.','|Delta FAIR carried out to capture the missed out requirement and shared to customer.','Next Batches produced verified and found ok.','C73034','2019-05-20','qas_sez(a)','qas_sez(a)','mail','2019-05-01','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','cust end','yes','Misc','qas_sez(a)','no','','|Moved all the affected parts from FG and WIP to ATPL for paint application in the masked area.','Z3456','qas_sez|','2019-06-05|','2019-06-05',NULL,NULL,NULL,NULL,NULL,NULL),(11732,'35A-608A','Saab AB','LEVER ASSY','','D5227335200200','','PART ISSUE C',24,'OWED-LTA-005','','A22880','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','yes','Paint application not done. ','1) Paint application inside the bore was not done.|2) The paint application requirement was not properly captured during the FAIR documentation.|3) In the previous issue the entire bore was required mashing but in the latest issue of drawing the requirement was changed to mask only to a specific length and the ECN (Engineering change note) did not demonstrated this requirement.','|Requested customer to return the parts back to CIM and the bush assembled are dis-assembled and sent to ATPL for paint application inside the bore.','|Delta FAIR carried out to capture the missed out requirement and shared to customer.','Next Batches produced verified and found ok.','C75623','2019-05-20','qas_sez(a)','qas_sez(a)','mail','2019-05-01','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','cust end','yes','Misc','qas_sez(a)','no','','|Moved all the affected parts from FG and WIP to ATPL for paint application in the masked area','Z3456','qas_sez|','2019-06-05|','2019-06-05',NULL,NULL,NULL,NULL,NULL,NULL),(11733,'35A-608A','Saab AB','LEVER ASSY','','D5227335200200','','PART ISSUE C',11,'OWED-LTA-005','','A21261','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','yes','Paint application not done. ','1) Paint application inside the bore was not done.|2) The paint application requirement was not properly captured during the FAIR documentation.|3) In the previous issue the entire bore was required mashing but in the latest issue of drawing the requirement was changed to mask only to a specific length and the ECN (Engineering change note) did not demonstrated this requirement.','|Requested customer to return the parts back to CIM and the bush assembled are dis-assembled and sent to ATPL for paint application inside the bore.','|Delta FAIR carried out to capture the missed out requirement and shared to customer.','Next Batches produced verified and found ok.','C73034','2019-05-20','qas_sez(a)','qas_sez(a)','mail','2019-05-01','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','cust end','yes','Misc','qas_sez(a)','no','','|Moved all the affected parts from FG and WIP to ATPL for paint application in the masked area','Z3456','qas_sez|','2019-06-05|','2019-06-05',NULL,NULL,NULL,NULL,NULL,NULL),(11734,'35A-608A','Saab AB','LEVER ASSY','','D5227335200200','','PART ISSUE C',4,'OWED-LTA-005','','A21263','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','yes','Paint application not done. ','1) Paint application inside the bore was not done.|2) The paint application requirement was not properly captured during the FAIR documentation.|3) In the previous issue the entire bore was required mashing but in the latest issue of drawing the requirement was changed to mask only to a specific length and the ECN (Engineering change note) did not demonstrated this requirement.','|Requested customer to return the parts back to CIM and the bush assembled are dis-assembled and sent to ATPL for paint application inside the bore.','|Delta FAIR carried out to capture the missed out requirement and shared to customer.','Next Batches produced verified and found ok.','C75623','2019-05-20','qas_sez(a)','qas_sez(a)','mail','2019-05-01','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','cust end','yes','Misc','qas_sez(a)','no','','|Moved all the affected parts from FG and WIP to ATPL for paint application in the masked area','Z3456','qas_sez|','2019-06-05|','2019-06-05',NULL,NULL,NULL,NULL,NULL,NULL),(11735,'35-161','Saab AB','STOP SUPPORT','854693-05','423Z6188-6','','---',2,'Forecast po for B787','','91187','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dig mark found on part.','Part not bolted before run the cut out program.|Operator does not read the program alert for bolting massage.|while this program alert machine was stopped so operator assumed as optional stop.|due to cross check the control hole diameter.','|instruct operator to check carefully before cycle start.','|3 more M00 added to cut out program before part cut out.','CAPA FOUND OK','','2019-05-21','Gurukiran S(M)','KIRAN (M V)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Gurukiran S(M)','no','','|cross checked previous production parts found ok.','E3456','qas|qas_sez|','2019-05-21|2019-05-24|','2019-05-24',NULL,NULL,NULL,NULL,NULL,NULL),(11736,'35-187','Saab AB','INTERCOSTAL_MIDSPAN_NO_1 ','599493','423Z1169-2-03','','---',1,'1600204275','','90028','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','no','DUMMY NC','DUMMY NC','|DUMMY NC','|DUMMY NC','DUMMY NC','','2019-05-21','qas_sez(a)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','DN57627','ONSITE','no','Misc','qas_sez(a)','yes','','|DUMMY NC','Z3456','qas_sez|','2019-05-21|','2019-05-21',NULL,NULL,NULL,NULL,NULL,NULL),(11737,'35A-608','Saab AB','LEVER ASSY','','D5227335200200','','PART ISSUE B',12,'1600217568','','A21282','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','yes','Paint missing inside the bore.','refer ncr #11734|refer ncr #11734|refer ncr #11734|refer ncr #11734|refer ncr #11734','|refer ncr #11734','|refer ncr #11734','refer ncr #11734','C73035','2019-05-21','qas_sez(a)','qas_sez(a)','Mail','2019-05-01','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','Cust End','yes','Misc','qas_sez(a)','no','','|refer ncr #11734','Z3456','qas_sez|','2019-06-05|','2019-06-05',NULL,NULL,NULL,NULL,NULL,NULL),(11738,'35A-474A','Saab AB','FRAME ASSY','','D5227338400000','','B',3,'OWED-LTA-001','','A22100','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','yes','Paint chip off on the edges.','1) Damage on the paint layer identified at SAAB.|2) Paint layer on the parts got damaged during the transit of the part from CIM to SAAB because of which it was not identified at CIM.|3) Due to insufficient packing material along the edges of the part the paint layer got damaged due to the part to part impact during transit handling.','|Received the parts for paint re-work from customer and carried out the rework at the affected areas.','|Additional packing between parts provided to avoid point to point contact during the transit handling.','Next shipments verified and found ok.','C74292','2019-05-21','qas_sez(a)','qas_sez(a)','OF-003653','2019-03-18','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','Cust End','yes','Misc','qas_sez(a)','no','','|Immediately checked the parts in FG And WIP for damaged paint layers and no similar damages identified, also informed the packing department about the issue and informed to provide additional packing layer between parts to avoid damages during transit handling.','Z3456','qas_sez|','2019-06-05|','2019-06-05',NULL,NULL,NULL,NULL,NULL,NULL),(11739,'35A-474A','Saab AB','FRAME ASSY','','D5227338400000','','B',1,'OWED-LTA-001','','A22101','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','yes','Paint chip off on the edges.','1) Damage on the paint layer identified at SAAB.|2) Paint layer on the parts got damaged during the transit of the part from CIM to SAAB because of which it was not identified at CIM.|3) Due to insufficient packing material along the edges of the part the paint layer got damaged due to the part to part impact during transit handling.','|Received the parts for paint re-work from customer and carried out the rework at the affected areas. ','|Additional packing between parts provided to avoid point to point contact during the transit handling.','Next shipments verified and found ok.','C74292','2019-05-21','qas_sez(a)','qas_sez(a)','OF-003653','2019-03-18','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','Cust End','yes','Misc','qas_sez(a)','no','','|Immediately checked the parts in FG And WIP for damaged paint layers and no similar damages identified, also informed the packing department about the issue and informed to provide additional packing layer between parts to avoid damages during transit handling.','Z3456','qas_sez|','2019-06-05|','2019-06-05',NULL,NULL,NULL,NULL,NULL,NULL),(11740,'56-102','GKN Aerospace Orangeburg','CLOSEOUT RIB - AFT, LWR','76536/05','119A1383-607','NA','PSDL REV -',1,'A000047470','','90436','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Running time dia 8flat end mill broken so dig mark observed on wall.','Chattering marks observed during cut out|In OP-02 ,8 flat tool was not clamped as per the program requirement|The tool was clamped 5mm above the required tool length','|After Setting all the tools,the parameters like tool length,tool cutting edge and tool offset will be validated by the senior operator and supervisor and the same will be evidence in setting checklist.','|Refer To CA','next part in this work was machined using new tool and the part found ok as per the drawing requirement.','','2019-05-21','pe_sez(a)','Maruthi  D R()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','pe_sez(a)','no','','|1.the part was rejected and NCR was raised\r\n2.The tool 8 flat was replaced and tool offset taken.','Z3456','qas_sez|','2019-05-21|','2019-05-21',NULL,NULL,NULL,NULL,NULL,NULL),(11741,'56-004','GKN Aerospace Orangeburg','GAS DUMPER FITTING','717409B7','475Z3604-19','NA','NIL',1,'A000044745','','91097','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Slot width 14.45+/-0.12mm measures oversize by 0.1/0.15mm .','Chattering marks observed during slot machining due to tool over hang|Due to vibration during finishing the slot chatter marks occured|since the clearance between the spindle,part fixture was very less the tool was over hang|The tool was clamped 5mm above the required tool length','1.The stock was provide in slot to check the slot width and finish the slot.\r<br/>2.Additional pass was added in the program to remove material slowly by 0.1mm per side to avoid chattering marks and to control the slot','Refer to CA','Next Part in this work was machined as per the CA and slot found ok with in the limits.','','2019-05-21','pe_sez(a)','Somashekar()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Cancelled','no','yes','no','With Treatment','','03','no','Misc','pe_sez(a)','no','','1.All the parts were checked for slot width and found ok.\r\n2.The deviation part was identified and NCR was raised','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11742,'35-710','Saab AB','LEVER','Z87M','D5227346621100','NA','PART ISSUE D',1,'OWED-LTA-004','','91678','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','DIG MARK OBSERVED ON PART','Running time DIA 8mm carbide end mill tool was broken.|due to over load of depth of cut|dia 8 mm flat end mill chipped out.','|cross check the previous production parts found ok.instruct operator for ensure the tools before run program.','|Add the program alert before start roughing program.','CAPA FOUND OK','','2019-05-22','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Prashanth Kumar(M)','no','','|immediate change the tool & run production','E3456','nagendra|Deshpande|qas_sez|','2019-05-25|2019-05-25|2019-05-27|','2019-05-27',NULL,NULL,NULL,NULL,NULL,NULL),(11743,'35-531A','Saab AB','SHAFT LATCH','B78267 NM2Z','D5227349020200','NA','PART ISSUE C',2,'OWED-LTA-002','','88309','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1. FOUND DEEP STEP ON THE OD SURFACE \r\n2. TOTAL LENGTH MEASURED MINUS , NOMINAL VALUE IS 341MM +/- 0.5MM . MEASURED VALUE IS 339.498 ','1.the tool offset taken was recorded wrongly in the Log book and the same was entered into the system\r\n|2.The offset taken was not validated in with the previous one which was recorded in the log book\r\n|3.Operator entered Wrong Tool offset  in the system and did not follow the check list provided for setting.\r\n','|1.Awareness and on job training was given to all the operators on following the check list provided for doing the setting\r<br/>2.Instruction given to all the operators to get the check list approved from the supervisor and senior operators once the setting is done.\r<br/>','|refer ca','Next part in this work order was resetted and the dimension found with in the limits as per the drawing','','2019-05-22','pe_sez(a)','Thaveni D M ,Ravi Kumar G.B,Manu K,Manu ,Dinakar K ,Dhanush J.K,','','0000-00-00','1. FOUND DEEP STEP ON THE OD SURFACE \r\n2. TOTAL LENGTH MEASURED MINUS , NOMINAL VALUE IS 341MM +/- 0.5MM . MEASURED VALUE IS 339.498 ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','200MY-01','qas_sez(a)','no','','|1.The part was rejected and internal NCR was raised.\r\n2.All the tools pertaining to the program was recalled and new offset was taken.\r\n','Z3456','qas_sez|','2019-06-05|','2019-06-05',NULL,NULL,NULL,NULL,NULL,NULL),(11744,'35-531A','Saab AB','SHAFT LATCH','B78267 NM2Z','D5227349020200','NA','PART ISSUE C',2,'OWED-LTA-002','','88309','','0000-00-00',NULL,'yes','no','no','no','no','yes','no','yes','no','OD MEASURED MINUS , MAX VALUE IS 18.78 MINIMUM VALUE IS 18.767,MEASURED VALUE IS 18.751 TO 18.758','1.the tool offset taken was recorded wrongly in the Log book and the same was entered into the system\r\n|2.The offset taken was not validated in with the previous one which was recorded in the log book\r\n|3.Operator entered Wrong Tool offset  in the system and did not follow the check list provided for setting.\r\n','|1.Awareness and on job training was given to all the operators on following the check list provided for doing the setting\r<br/>2.Instruction given to all the operators to get the check list approved from the supervisor and senior operators once the setting is done.\r<br/>','|refer ca','next batch machined and found ok ','','2019-05-22','pe_sez(a)','Thaveni D M ,Ravi Kumar G.B,Manu K,Manu ,Dinakar K ,Dhanush J.K,','','0000-00-00','OD MEASURED MINUS , MAX VALUE IS 18.78 MINIMUM VALUE IS 18.767,MEASURED VALUE IS 18.751 TO 17.758','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','100MY-01','qas_sez(a)','no','','|1.The part was rejected and internal NCR was raised.\r\n2.All the tools pertaining to the program was recalled and new offset was taken.\r\n','Z3456','qas_sez|qas_sez|','2019-05-22|2019-06-05|','2019-06-05',NULL,NULL,NULL,NULL,NULL,NULL),(11745,'35-146','Saab AB','CED_HINGE_FTG_FWD','716504B6','425Z0301-6','7050 - T7451 ALUMINU','--A',1,'Forecast po for B787','','92308','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','DIA 16 RIPPER TOOL DOWN AND BROKEN SO PART WALL MINUS','while first part running time tool down so dig mrk observed on part|due to tool holder problem','|Immediately change the tool holder & run the production.  ','|ensure the holder alenhead bolts are tight.','CAPA FOUND OK','','2019-05-23','Dinesh kulal()','Ravi(.S.N)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','2nd','no','Misc','prodn_aero(prodn)','no','','|Immediately change the tool holder & run the production.  ','A3456','nagendra|qas_aero|','2019-05-24|2019-06-08|','2019-06-08',NULL,NULL,NULL,NULL,NULL,NULL),(11746,'18-720A','Magellan Aerospace Wrexham','SPIGOT ','1573448-2/Q8LF','F575 51290 200','','B',1,'152089 Amnd 2','','91577','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Tool offset wrong taken\r\n','Tool dig mark .						\r\n|Tool offset not done.			|Tool offset Missing.				|Two tools are loaded at a time, but only 1st tool offset was measured and 2nd tool offset was not measured.	','|All tools offset was cross checked and run the program. ','|Introduce the check list for first part setting. 	','CAPA FOUND OK','','2019-05-23','Dhananjaya(N)','        dharshan d','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','3','','','','','','|Immediately stop the machine 				','E3456','pe|pe|qas_sez|','2019-05-23|2019-05-23|2019-05-25|','2019-05-25',NULL,NULL,NULL,NULL,NULL,NULL),(11747,'18-318A','Magellan Aerospace Wrexham','HALF CLAMP','28428474-A','D574 50551 200','DTD 5014','B01',1,'175170','','90874','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','SPOT FACE DEPTH OVERSIZED','Part not butted to fixture butting face\r\n|due to chips found on the fixture.','|stop the machine & clean the fixture before start the production','|check the part butting surface by using feeler gauge.','CAPA found ok','','2019-05-24','Anjinamurthy(H)','Ravindra(Singh R)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','7','no','Misc','Irappa(Badiger)','no','','|Cross check the previous parts found ok.','E3456','nagendra|qas_sez|qas_sez|','2019-05-24|2019-05-27|2019-05-27|','2019-05-27',NULL,NULL,NULL,NULL,NULL,NULL),(11748,'35-170','Saab AB','ALCD_STRUCT_SUPPORT-FTG_L','9366959','423Z1200-11-01','','---',1,'LTA SAAB B787 Assemb','','91513','','0000-00-00',NULL,'yes','no','yes','no','yes','no','no','no','no','9.52 holes are shifted 6MM on Y-axis.','Y-Axis offset changed upto 6mm|chips blocked on the sensor rod\r\n|telescopic wiper rubber damaged \r\n|due to y-axis continuous movement telescopic wiper rubber damaged ','|stop the machine & calls the service engineer.','|ensure the telescopic rubber while doing preventive maintenance. ','CAPA FOUND OK','','2019-05-24','Dinesh kulal()','Manjunatha.D()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','2nd','no','Misc','prodn_aero(prodn)','no','','|stop the machine & calls the service engineer.','A3456','nagendra|qas_aero|','2019-05-24|2019-06-08|','2019-06-08',NULL,NULL,NULL,NULL,NULL,NULL),(11749,'35-166B','Saab AB','HOUSING PIN ','713722B7','423Z1124-6-01','','--B',1,'1600203627','','91415','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','part wall thickness undersize by 2mm.','while first part proving time 16R3 tool loaded instead of 12R3|When editing the program wrong tool was selected.|due to miscommunication between shift operator.','|Load the correct required tool & run the production.','|While first part proving time ensure required tools are loaded in machine by using checklist provided.','CAPA FOUND OK','','2019-05-24','Dinesh kulal()','Santhosh Kumar.R()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','5TH','no','Misc','prodn_aero(prodn)','no','','|stop machine & change the tool.','A3456','nagendra|qas_aero|','2019-05-24|2019-06-08|','2019-06-08',NULL,NULL,NULL,NULL,NULL,NULL),(11750,'56-048','GKN Aerospace Orangeburg','TIP CAP','607441','119A1370-604','NA','PSDL REV -',1,'A000047470','','90385','','0000-00-00',NULL,'yes','yes','yes','','','','','','','RUNNING TIME PART LIFT','After roughing operation the part was found that the RM was not butted properly at one end |The manual hand tightening  was not done after Torque tightening by the operator |operator was in a assumption that the RM is tighten rigidly since the tightening was done by torque tightening method.','|1.the required torque to tighten M8 bolts will be re defined and fixed  as per the torque Tightening equipment so as to avoid manual tightening.\r<br/>2.The same will be update in the log.','|refer to CA','Torque tighten was redefined and the next part machined and found ok','','2019-05-24','pe_sez(a)','        Raghu B','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','01','','','','','','|1.All the previous machined parts was 100% inspected and found no evidence of extra material machined or tool dig.\r\n2.The deviation part was rejected and NCR was raised.','Z3456','pe_sez|qas_sez|qas_sez|','2019-05-24|2019-05-24|2019-06-05|','2019-06-05',NULL,NULL,NULL,NULL,NULL,NULL),(11751,'35-600','Saab AB','FRAME','796718','D5227338520400','NA','PART ISSUE C',1,'OWED-LTA-001','','88637','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','26.999 h7 hole no go pin answer,','Due to bore over size by 0.03MM to 0.04MM|While boring operation reamer tool blunt.|due to insufficiant colant supply to cutting tool edge.','|built up edges found so Polish the reamer & run the production.','|Every 100 parts cross check the reamer & adjust coolant nozzel pipe.','CAPA FOUND OK','','2019-05-24','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Prashanth Kumar(M)','no','','|Cross check the preveous production parts found ok.','E3456','qas|nagendra|','2019-06-04|2019-06-06|','2019-06-06',NULL,NULL,NULL,NULL,NULL,NULL),(11752,'56-092','GKN Aerospace Orangeburg','CLEVIS FTG FWD','241826B7','119A1215-603','NA','PSDL REV A',1,'A000047471','','90098','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Break Edge on chamfer is more and not meeting the requirements of BAC5300 ','The Chamfer tool used for break sharp edge,tool offset  was more by 1mm|The Offset was taken in Zoller and the mode was select wrongly in the zoller by the operator.|No Instruction was displayed near the Zoller machine on mode selection.','|The procedure and steps involved to take offset and mode selection for different tools  in the zoller machine  will be displayed near the zoller machine.','|Refer to CA','Next part in this batch tool offset was taken Correctly by using the correct mode in the zoller machine ,part machined and the break edges were meeting the specification of BAC5300.','','2019-05-24','pe_sez(a)','pe_sez(a)','','0000-00-00','hole chamfer  dig mark ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','With Treatment','','03','no','Misc','pe_sez(a)','no','','|1.the part was identified and Quarantine NCR was raised.\r\n2.The part was moved to Quality clinic for further discussion.\r\n3.Re-offset was taken and the same was inputted to machine.','Z3456','qas_sez|qas_sez|','2019-05-27|2019-05-27|','2019-05-27',NULL,NULL,NULL,NULL,NULL,NULL),(11753,'18-779A','Magellan Aerospace Wrexham','BRACKET AFT M/C','1671472-2/Y9QY','F57551860201','NA','PART ISSUE A',1,'RP174264','','90006','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','OUTER PROFILE DIG MARK.','Due to work offset shift in Y-axis by 3mm.|Due to wrong work offset entered by operator.|center off the job defined was wrong.','|Correct the work offset & start the production.','|1)Include the program alert in roughing program.\r<br/>2) instruct operator for cross check the work offset before start the machine.','CAPA FOUND OK','','2019-05-25','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','NC','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','3','no','Misc','Dhananjaya(N)','no','','|Stop the machine & cross check the previous production parts found OK','E3456','qas_sez|qas|qas|','2019-06-25|2019-06-28|2019-06-28|','2019-06-28',NULL,NULL,NULL,NULL,NULL,NULL),(11754,'34-069A','Magellan Aerospace Winnipeg','HINGE-L/H','G25697','400-12901-1','NA','EM104302 Iss B,EM105092 Iss H,EM104765 Iss H',1,'C81597 Rev 001','','92203','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','RIB THICKNESS UNDERSIZE BY 0.08MM ','dig mark observed on the part.|dia 5 ball nose tool broken.|material stock in radius.|dia 8 flat tool was chipped out.|used the regrinding dia 8 flat tool.','|instruct to operator for check the tools before load the machine.','|stop the using of regrinding tools for pocket roughing & use the new dia 8 flat tool for next batch.','CAPA FOUND OK','','2019-05-25','Dhananjaya(N)','Venkatesh R,Rakesh  KC,Narasimhamurthy C,Dileep Kumar,','','0000-00-00','NC RAISED BY NAVEEN BADIGERA','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','DN58509','FI','no','HAASVF2SS-2','Nagendra(SN)','no','','|Immediately change the dia 8 flat tool & run the production. ','E3456','nagendra|qas_sez|','2019-05-25|2019-05-25|','2019-05-25',NULL,NULL,NULL,NULL,NULL,NULL),(11755,'35-717','Saab AB','','D87797 YQE4','D5227349320600','NA','PART ISSUE E',1,'OWED-LTA-005','','91213','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Profile dig mark.','Running time tool broken |Insufficient coolant flow.|Coolant filter clog.|Cleaned the coolant filter. Tool changed','|while doing Preventive maintenance clean the coolant tank and motor filter ','|Operator will ensure Coolant flow before shift start. ','CA PA pound ok.','','2019-05-25','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Prashanth Kumar(M)','no','','|stop the machine and clean the filter and change the tool','E3456','pe|qas|','2019-05-30|2019-06-03|','2019-06-03',NULL,NULL,NULL,NULL,NULL,NULL),(11756,'35-419','Saab AB','BRACKET TARGET','4210601','D522 73538 201 00','','A',3,'OWED-LTA-004','','88898','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','BASE THICKNESS (-)SIDE,\r\n','1) Due to excess bend on the part after roughing operation part lifted and resulted in thickness under-size.\r\n|2) During the final pass in finishing operation due to residual stress the part is getting lifted up.\r\n|3) During aging time between the roughing and the finishing operation the material was not left in free condition (i.e. the materials were loaded one over the other).\r\n','|\r<br/>1.Informed all the operators to leave the part in free condition during the aging process.\r<br/>','|1.Training provided to all the operators on site to avoid storage of parts one above the other during the aging operation.\r<br/>','Next batches produced found ok.','','2019-05-25','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Prashanth Kumar(M)','no','','|1.immediately stopped the machine and arranged the material so that the parts are left in free condition.\r\n','E3456','pe|qas|','2019-07-01|2019-07-29|','2019-07-29',NULL,NULL,NULL,NULL,NULL,NULL),(11757,'51-151','THE BOEING COMPANY','LWR SKIN COVER','0-24-11163/24128','312Z3122-502','NA','NIL',1,'BOEING 001X','','91275','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','DEEP DIG MARK OBSERVED IN TWO HOLES','','','','','','2019-05-25','pe_sez(a)','Shivaraj K S,Maruthi  D R ,Kiran Kumar M,Kiran KM,Chethan Kumar M,Anand ,','','0000-00-00','DEEP DIG MARK OBSERVED IN TWO HOLES','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','With Treatment','','FI','no','i700-3','qas_sez(a)','no','','','Z3456','qas_sez|qas_sez|','2019-05-25|2019-05-25|','2019-05-25',NULL,NULL,NULL,NULL,NULL,NULL),(11758,'56-005','GKN Aerospace Orangeburg','SPLICE PLATE FWD UPR','0-26-09777/27577','119A1213-603','NA','PSDL REV -',1,'LTA GKN 737 Winglet','','92194','','0000-00-00',NULL,'yes','','yes','','yes','','','','','During power failure 5axis machine error,\r\ndue to tool travel in abnormal operation while i machining time. ','1) Part rejected due to wrong movement of the tool over the part.|2) The machine bed did not rotated according to the NC program after the recover of machine from power failure.|3) Due to power failure in between of machining the machine bed got locked from rotation and the operator started the cycle after the recover of power and because of which the tool moved abnormally over the part.|4) No error message regarding the axis lock was displayed as the power failure occurred during the machine bed tilting operation.','|Reset the machine axis by maintenance team and cross checked the tool offsets and continued the production.','|Next time after the power failure instructed the operators to ensure machine axis rotation as per the Program and then continue the production.','CA PA found ok.','','2019-05-28','pe_sez(a)','        Rajesha A.R','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','03','','','','','','|Immediately stopped the machine and informed the supervisor and the maintenance department about the issue.','Z3456','pe_sez|qas_sez|','2019-05-28|2019-06-06|','2019-06-06',NULL,NULL,NULL,NULL,NULL,NULL),(11759,'46-045','Mahindra Aerostructures Pvt.Ltd','BRACKET SYSTEM  ELEC','471713B','V5755893720200CM','NA','PART ISSUE A00',1,'3101472182','','92270','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','wall thickness got undersized when compared to the customer requirement.','The wall thickness was machined more than the requirement due to wrong clamping method \r\n\r\n The operator was not instructed sufficiently regarding the clamping method \r\n\r\n The clamping process was not self explanatory to the operator \r\n\r\n Fool proofing not adopted when small difference in the pitches of clamping method','Appropriate data to be provided for clamping.  \nPossible methods to be adopted to prevent small differnce occurance','Fool proofing shall be practiced while planning the process for future parts','CAPA FOUND OK','','2019-05-28','Ramesh(Poojary)','        Nandeep()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Subramanya L(Naik)','no','','Part identified as rejected.','E3456','qas|qas|Deshpande|qas|','2019-06-03|2019-06-04|2019-09-20|2019-09-23|','2019-09-23',NULL,NULL,NULL,NULL,NULL,NULL),(11760,'51-149','THE BOEING COMPANY','UPR SKIN COVER','H29958-Y05','312Z3121-502','NA','NIL',1,'BOEING 001X','','89689','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','DEEP DIG MARK FOUND IN THE HOLE','','','','','','2019-05-29','pe_sez(a)','Shivaraj K S,Maruthi  D R ,Kiran Kumar M,Chethan Kumar M,Anand ,','','0000-00-00','NC RAISED ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','no','no','no','With Treatment','DN58603','FI','yes','i700-3','qas_sez(a)','no','','','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11761,'35-443C','Saab AB','HINGE','B79882','D5227338820000','NA','B',1,'OWED-LTA-002','','88276','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','PART WAS NOT BUTT PROPERLY.','1) Part improper loaded during the second setup.|2) Part was not loaded properly by the operator.|3) During the second step part loading time the operator did not ensured proper butting of part to the wall while clamping due to which the profile got shifted.','|Informed all the operators to ensure proper butting of part before starting the cycle.','|MO code included in the program instructing the operator to ensure proper butting of part before starting the cycle.','Next part machined in this workorder and the part found ok as per the drawing','','2019-05-29','pe_sez(a)','Vijay Kumar(H.J)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','pe_sez(a)','no','','|Immediately stopped the machine and informed the supervisor checked the previously completed parts and found ok.','Z3456','qas_sez|qas_sez|','2019-05-29|2019-06-05|','2019-06-05',NULL,NULL,NULL,NULL,NULL,NULL),(11762,'35A-699','Saab AB','LEVER 3 ASSY','','D5227280900400','','PART ISSUE C',1,'OWED-LTA-005','','A25882','','0000-00-00',NULL,'no','yes','yes','yes','no','no','no','no','no','bush damaged','Protective layer on the bush damage during assembly.|Poor adhesion of protective layer to the bush.|Supplier did not ensured proper adhesion of protective layers on the bush surface.','|Rejected and returned the bush to BOI stores and returned the part back to FG.','|Informed the supplier to ensure proper adhesion of protective layer before shipping to CIM and also informed the BOI stores person to visually inspect for any damage before booking in.','CA PA found ok.','','2019-05-31','Ramesh(D)','Phaniraj(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Assembly','','procesing','no','Misc','Ramesh(D)','no','N02538|EN4535-2F04R007','|Checked all the bushes from the same batch visually for any damage to the protective layer and no parts with defect found.','E3456','qas|','2019-06-26|','2019-06-26',NULL,NULL,NULL,NULL,NULL,NULL),(11763,'35A-545','Saab AB','BEAM ASSY','','D522 73335 000 00','','PART ISSUE A',1,'OWED-LTA-001','','A25863','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','Deep scratch found on the part and the Zinc Plating is damage at that area which is visually not ok.','','','','','','2019-05-31','Dharani(Shankar)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','no','yes','no','Assembly','','FI','no','Misc','Dharani(Shankar)','no','88161|D5227347420200','','Z3456','qas_sez|','2019-05-31|','0000-00-00',NULL,NULL,NULL,NULL,NULL,NULL),(11764,'35-531A','Saab AB','SHAFT LATCH','C91277 SEQC','D5227349020200','NA','PART ISSUE C',2,'OWED-LTA-002','','91953','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','OD Under Size','1.the tool offset taken was recorded wrongly in the Log book and the same was entered into the system\r\n|2.The offset taken was not validated in with the previous one which was recorded in the log book\r\n|3.Operator entered Wrong Tool offset  in the system and did not follow the check list provided for setting.\r\n','|1.Instruction given to all the operators to get the check list approved from the supervisor and senior operators once the setting is done.\r<br/>2.Awareness and on job training was given to all the operators on following the check list provided for doing the setting\r<br/>','|refer to CA','The next part in this work order was resetted and the OD dimension was found ok within the limits','','2019-05-31','Dinakar K()','Manu K,Dinakar K ,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','3','no','200MY-02','Dinakar K()','no','','|1.The part was rejected and internal NCR was raised.\r\n2.All the tools pertaining to the program was recalled and new offset was taken.\r\n','Z3456','qas_sez|','2019-06-05|','2019-06-05',NULL,NULL,NULL,NULL,NULL,NULL),(11765,'35-602A','Saab AB','SHAFT 1','C91450 W8FG','D5227280720000','NA','PART ISSUE B',3,'OWED-LTA-004','','92011','','0000-00-00',NULL,'yes','yes','yes','','','','','','','OD UNDER SIZE','1.the tool offset taken was recorded wrongly in the Log book and the same was entered into the system\r\n|2.The offset taken was not validated in with the previous one which was recorded in the log book\r\n|3.Operator entered Wrong Tool offset  in the system and did not follow the check list provided for setting.\r\n','|1.Awareness and on job training was given to all the operators on following the check list provided for doing the setting\r<br/>2.Instruction given to all the operators to get the check list approved from the supervisor and senior operators once the setting is done.\r<br/>','|refer to ca','Next part in this work order was resetted and the OD found within the drawing limits.','','2019-05-31','Dinakar K()','        Dinakar K ','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','no','yes','','','3','','','','','','|1.The part was rejected and internal NCR was raised.\r\n2.All the tools pertaining to the program was recalled and new offset was taken.\r\n','Z3456','pe_sez|qas_sez|','2019-06-05|2019-06-05|','2019-06-05',NULL,NULL,NULL,NULL,NULL,NULL),(11766,'18-695A','Magellan Aerospace Bournemouth','HOUSING OUT B D BRG 3 ','1649705-2/XDKS','D275 56121 200','','E01, ECN NG27011ST1KA83',1,'425757','','89221','','0000-00-00',NULL,'yes','yes','yes','','','','no','','','Profile undersize.','While running time part was rotated.|clamping method is not sufficient for I-machining program.|due to reduce the cycle time used I-machining program for Roughing.','|inform to Engineering dept immediately change the program & run the production.','|Run the 2D program instead of I-machining.\r<br/>use sufficient clamping method.\r<br/>','CAPA FOUND OK','','2019-06-01','Dhananjaya(N)','        Mallikarjuna D','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','01','','','','','','|Cross check the previous production parts found OK','E3456','pe|qas|qas|','2019-06-01|2019-06-03|2019-06-04|','2019-06-04',NULL,NULL,NULL,NULL,NULL,NULL),(11767,'35-531A','Saab AB','SHAFT LATCH','C91277 SEQC','D5227349020200','NA','PART ISSUE C',2,'OWED-LTA-002','','91953','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','OD UNDER SIZE BY 0.4MM ','WRONG OFFSET VALUE ENTERED BY THE OPERATOR|THE OPERATOR WAS OPERATING TWO MACHINES DURING SAME SHIFT|DUE TO LACK OF CONCENTRATION AND NEGLIGENCE WRONG OFFSET WAS ENTERED BY THE OPERATOR.','A MESSAGE WILL  POP UP(CAUTION) SAYING OFFSET ENTERED VALUE IS CORRECT (YES OR NO)TO DOUBLE CHECK THE ENTERED VALUE IS RIGHT OR WRONG.','','CAPA FOUND SATISFACTORY.','','2019-06-03','Dinakar K()','Manu K,Dinakar K ,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','3','no','200MY-02','Dinakar K()','no','','THE MACHINE WAS STOPPED AND CHECKED THE PREVIOUS PRODUCED PARTS AND ALL PARTS FOUND OK. OFFSET VALUE WAS CROSSCHECKED AND RE INPUT THE CORRECT VALUE.','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11768,'18-090A','Magellan Aerospace(Polska) Sp','BUSH','1670511-3YT2M','PID278 50164 200','','A',3,'104569','','91042','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','OD UNDER SIZE.','1)OD Undersized -0.015mm beyond drawing limit.|2)OD undersized during the re-pass operation as the re-pass ran twice.|3)Re-pass ran twice with same -0.15 wear offset as the operator provided +0.2mm wear offset during the insert change.','|1)Changed the wear offset from +0.2mm to +0.1mm in the next part and after the completion changed the offset to -0.02mm according to the program(after considering both the pass) and found the next part OK. ','|Informed all the operator to check the relevant features after the insert change and provide of the offset accordingly with proper guidance from the supervisor or senior operators. ','CAPA found ok','','2019-06-03','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','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','qas|','2019-06-07|','2019-06-07',NULL,NULL,NULL,NULL,NULL,NULL),(11769,'56A-093','GKN Aerospace Orangeburg','CLEVIS FTG ASSY FWD','','119A1215-602','','PSDL REV A',1,'A000047470','','A26130','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','DEEP DENT MARK OBSERVED ON THE PART SURFACE','','','','','','2019-06-03','pe_sez(a)','pe_sez(a)','','0000-00-00','NC RAISED','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','no','no','no','Assembly','','INPROCESS','yes','Misc','qas_sez(a)','no','90401|119A1215-604','','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11770,'35-720','Saab AB','ROD BODY','6899','D5227333720200','NA','PART ISSUE B',1,'OWED-LTA-005','','93285','','0000-00-00',NULL,'yes','yes','yes','','','','','','','OD UNDER SIZE','1.the tool offset taken was recorded wrongly in the Log book and the same was entered into the system\r\n|2.The offset taken was not validated in with the previous one which was recorded in the log book\r\n|3.Operator entered Wrong Tool offset  in the system and did not follow the check list provided for setting.\r\n','|1.Awareness and on job training was given to all the operators on following the check list provided for doing the setting\r<br/>2.Instruction given to all the operators to get the check list approved from the supervisor and senior operators once the setting is done.\r<br/>','|refer ca','Next part in this work order was resetted and the OD found with in the drawing limits','','2019-06-03','Dinakar K()','        Manu K','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','','','','','3','','','','','','|1.The part was rejected and internal NCR was raised.\r\n2.All the tools pertaining to the program was recalled and new offset was taken.\r\n','Z3456','pe_sez|qas_sez|','2019-06-04|2019-06-05|','2019-06-05',NULL,NULL,NULL,NULL,NULL,NULL),(11771,'47-176','GKN Aerospace Filton','BRACKET','524201','F5755098420102','NA','PART ISSUE E02',1,'GKN-GS-068 PHASE2- L','','90962','','0000-00-00',NULL,'yes','yes','yes','','','','','','','CRN-47-176\r\nWO-90962\r\nNOTE- Z HEIGHT WRONG TOOL DIG MARK ON PART ','the tool was over hangged \r\n|Mimi mum clamping area for the is 30 mm ,but the operator has clamped for 20 mm\r\n|The tool offset taken was not validate and compared with the log book in which previous batch tool offset was recorders\r\n|The operator didn’t follow the Instruction given in the MPS\r\n','|1.Awareness given to operators to follow the instruction given in the MPS and to follow the check list provided for setting.\r<br/>2.Instruction given to all the operators to get the check list approved from the supervisor and senior operators once the setting is done.\r<br/>\r<br/>','|refer ca','Next batched machined and found ok as per the drawing ','','2019-06-04','pe_sez(a)','        Kiran KM','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','3','','','','','','|1.The part was rejected and internal NCR was raised.\r\n2.All the tools pertaining to the program was recalled and new offset was taken.\r\n','Z3456','pe_sez|qas_sez|','2019-06-05|2019-06-05|','2019-06-05',NULL,NULL,NULL,NULL,NULL,NULL),(11772,'56-106','GKN Aerospace Orangeburg','FAIRING SUPPORT - FWD','351531','119A1520-603','NA','PSDL REV A',1,'A000047470','','90503','','0000-00-00',NULL,'yes','yes','yes','','','','','','','LOADING  METHOD WRONG ','the fixture was loaded in the reverse direction in the pallet.|operator by mistake has loaded the fixture in the opposite direction since both the LH & RH was machined in the same fixture.|there was no fool proof method in the fixture and the fixture can be loaded in any direction ','|Fool proof method was in place.\r<br/>A hole was located in the fixture with dowel pin so that even if  operator loads the fixture in reverse side it will not butt into the pallet and zero point system. ','|Refer to CA','Next part machined in this work order by taking the above CA .Part found ok to the drawing requirements.','','2019-06-04','pe_sez(a)','        Ravi Kumar G.B','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','3','','','','','','|1.The part was rejected and NCR was raised.\r\n2.Checked All the previous machined parts and found ok','Z3456','pe_sez|qas_sez|','2019-06-05|2019-06-06|','2019-06-06',NULL,NULL,NULL,NULL,NULL,NULL),(11773,'51A-066','','','','','','',0,'','','','','0000-00-00',NULL,'no','no','no','no','no','no','no','no','no','','','','','','','2019-06-05','select','','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Cancelled','no','no','no','','','','no','','select','no','','','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11774,'51A-066A','THE BOEING COMPANY','STRUT SUPPORT ASSY','','113T1958-7','','PSDL REV A',1,'BOEING 001AA','','A26134','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','bush oversize','During bush reaming time bush oversize.|CRC correction wrong entered by the operator.|Setting time CRC wrong calculated by the operator.','|Training given to the operator on CRC calculation.','|Sandard reamer is ordered for the finish diameter to avoid entering CRC corrections in the program.','CA PA found ok.','','2019-06-05','Karthineyan(V.S.)','Karthineyan(V.S.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Assembly','','procesing','no','Misc','Karthineyan(V.S.)','no','','|Immediately stopped the machine and informed the supervisor, checked the CRC value and corrected according to the requirement.','E3456','qas|','2019-07-29|','2019-07-29',NULL,NULL,NULL,NULL,NULL,NULL),(11775,'35-443C','Saab AB','HINGE','B79882','D5227338820000','NA','B',1,'OWED-LTA-002','','88276','','2019-06-06',NULL,'yes','yes','yes','no','no','no','no','no','no','tool offset wrong','Wrong tool offset taken by the operator.|Tool offset was taken on the fixture face insteard of part face by the operator.|Operator did not refer to the MPS.','|Re-took the work offset and continued the machining.','|On spot training provided to the operator to take tool offset.','Training effectiveness verified and found ok.','','2019-06-06','pe_sez(a)','pe_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','01','no','Misc','pe_sez(a)','no','','|Immediately stopped the machine and rechecked the tool offset under supervisor surveillance.','Z3456','qas_sez|','2019-09-27|','2019-09-27',NULL,NULL,NULL,NULL,NULL,NULL),(11776,'35-583A','Saab AB','BRACKET','802628','D5227334820600','NA','PART ISSUE B',1,'OWED-LTA-005','','93570','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','DIGMARK FOUND ON OUTER DIAMETER.','The part while running OP-02 got rotated while taking cut on the material|since the part was square and the intermediate cut taken the part got rotated|Depth of cut 1.5mm was given in the roughing cycle|to minimize the cycle time in OP-02','|1.The depth of cut was reduced to 0.5mm and continued the production','|Refer To CA','Next part in this work order was  machined using 0.5mm depth of cut and the part found ok ','','2019-06-06','Dinakar K()','Dinakar K()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Dinakar K()','no','','|1.The part was rejected and NCR was raised.\r\n2.Checked the insert if any damage in the insert cutting edge and found ok','Z3456','qas_sez|','2019-06-06|','2019-06-06',NULL,NULL,NULL,NULL,NULL,NULL),(11777,'35-159','Saab AB','FLCD_DS_DEFLECT_STOP','854693-10','423Z6187-8','','---',1,'Forecast po for B787','','90626','','0000-00-00',NULL,'yes','no','no','no','yes','yes','no','no','no','SLOT DEPTH OVER SIZE, NOMINAL 4.06 MEASURED 5.62','The tool was weared out and changed in between the process|After Changing the tool,tool offset was entered wrongly in the tool geometry|Operator entered the tool offset  1mm minus in the tool geometry','|Instruction given to the operator to strictly follow the check list which is already available to avoid such Mistakes','|Checking gauge will be implementation to check the depth in OP-01 100% ','CAPA FOUND OK','','2019-06-06','pe_sez(a)','Vijay Kumar H.J,Thaveni D M ,Ravi Kumar G.B,Manu ,HariPrasad ,','','0000-00-00','SLOT DEPTH OVER SIZE, NOMINAL 4.06 MEASURED 5.62','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','a51nx-06','qas_sez(a)','no','','|1.All the previous machined parts were inspected for the deviation and found ok \r\n2.For the rejected part NCR was raised.','Z3456','qas_sez|qas_sez|','2019-06-07|2019-08-27|','2019-08-27',NULL,NULL,NULL,NULL,NULL,NULL),(11778,'35-404','Saab AB','BEAM 2','814253','D522 73392 200 01','','A',1,'OWED-LTA-005','','88955','','0000-00-00',NULL,'yes','yes','yes','','','','','','','WRONG PROGRAM SELECTION..','UNWANTED MACHINING IN 5TH SETUP OPERATIONS|3RD SETUP OPERATIONS RUN IN 5TH SETUP OPERATIONS|OPERATOR SELECT THE 3RD SETUP PROGRAM WHEN HE RUN THE 5TH SETUP|3RD AND 5TH SETUP OPERATIONS ARE IN SAME TUMB. THE WORK COORDINATES(G54)  ARE ALSO SAME. ','|THE WORK COORDINATES CHANGED IN TO 2 AS G54 AND G55. \r<br/>WORK INSTRUCTIONS ARE GIVEN THE STARTING OF THE PROGRAM.','|THE WORK COORDINATES CHANGED IN TO 2 AS G54 AND G55. \r<br/>WORK INSTRUCTIONS WILL GIVE THE STARTING OF THE PROGRAM.\r<br/>ANY DOUBT IN PROGRAM SELECTION, THE OPERATOR WILL INFORM TO THE SUPERVISOR','CA PA found ok.','','2019-06-07','op_sez(s)','        HariPrasad ','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','05','','','','','','|PRODUCTION STOPPED. THE PROBLEM ANALYZED WITH THE ENGG DEPARTMENT   ','Z3456','pe_sez|pe_sez|qas|','2019-06-11|2019-09-05|2019-09-09|','2019-09-09',NULL,NULL,NULL,NULL,NULL,NULL),(11779,'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','','','CA PA FOUND OK','','2019-06-08','Ravi nayak()','prodn_aero(prodn)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Cancelled','no','yes','no','With Treatment','','PRODUCTION','no','Misc','Ravi nayak()','no','','','A3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11780,'35-443C','Saab AB','HINGE','B79882','D5227338820000','NA','B',4,'OWED-LTA-002','','88276','','0000-00-00',NULL,'yes','no','no','no','no','yes','no','yes','no','THICKNESS MEASURED MINUS MINIMUM VALUE IS 3.61 MEASURED VALUE IS 3.512','Thickness of the part got undersized at edge area.|Due to process/Fixture issue thickness of some parts(11 out of 120 parts) in a batch found undersized at edge area.|1) The butting surface of the part is 3D but the formation of 3D surface in the fixture is not proper, due to that in some parts thickness got undersized at edge area.|2) On the butting surface area of the part a step mark is found, which is acceptable as per \"Ra\" requirement, but the same step has influence over butting of part to the fixture.','|The task is assigned to develop an improvements in the fixture and new clamping method is also inline. ','|The task is assigned to develop an improvements in the fixture and new clamping method is also inline. ','CA PA Ok.','','2019-06-10','pe_sez(a)','Vijay Kumar H.J,Upendra N ,Thaveni D M ,Ravi Kumar G.B,Nagaraju P K ,Manu ,Karthik Raj T ,HariPrasad ,Dhanush J.K,','','0000-00-00','THICKNESS MEASURED MINUS MINIMUM VALUE IS 3.61 MEASURED VALUE IS 3.512','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','','FI','yes','a51nx-06','qas_sez(a)','no','','|Inspected all the parts of the batch for similar issue and same is informed to the respective persons. ','Z3456','qas_sez|qas_sez|qas_sez|','2019-07-09|2019-09-26|2019-09-27|','2019-09-27',NULL,NULL,NULL,NULL,NULL,NULL),(11781,'51-075','THE BOEING COMPANY','BELLCRANK','E2548','252T1271-2','NA','PSDL REV -',1,'BOEING 001M','','92217','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','when machining time Part get disturbed due to low torque during tightening.','1) Hole position shifted during machining as the part lifted during the hole drilling operation.|2) Part was not clamped properly during machining.|3) Due to cross cutting of the material the part was not clamped sufficiently.','|1) Checked the available RM\'s for similar Cross cutting defects and segregated the cross catted RM and informed the supervisor.','|1) Communication provided to the supplier regarding the cross cutting of the RM.\r<br/>2) Informed all the operators to ensure the Clamping pressure and butting of the part as per MPS before starting the cycle.','Next batches verified and found ok.','','2019-06-10','pe_sez(a)','','','0000-00-00','Part rejected by Vijayakumar .HJ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','1','no','a51nx-06','HariPrasad()','no','','|Immediately stopped the machine and checked the hole position of the previously completed parts and found ok.','Z3456','qas_sez|','2019-12-05|','2019-12-05','0000-00-00','0000-00-00','0000-00-00','','',''),(11782,'56-120','GKN Aerospace Orangeburg','CLOSEOUT RIB - LWR, FWD','445511','119A1440-617','NA','PSDL REV C',1,'LTA GKN ORANGEBURG K','','93228','','0000-00-00',NULL,'yes','','yes','','','','no','yes','','PART RUNNING TIME TOOL BROKEN SO PART DIG MARK. ','Due to breakage of tool during running time the part got dent and rejected.|The cutting edges of the tool, holding length, flow of coolant and load applied to the tool during running time were not monitored during machining.','|Informed the supervisor about the tool breakage and changed the tool re-took the offset and continued the production.','|1) Production supervisors to ensure proper tool length holding, flow of cutting fluid and good condition of holders every day.\r<br/>2) Operators should verify the wear of cutting edges on the tool before start of every shift.\r<br/>3) Engineering department need to verify smooth tool path and need to avoid sudden and intensive loading of the tool during running time.\r<br/>','All the actions above need to  be monitored for one month final effectiveness will be measured on 4-Aug-2019.','','2019-06-11','pe_sez(a)','        Nataraja C V','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','03','','','','','','|Checked the previously completed parts for chattering marks and dimensional issues and all the parts found ok.','Z3456','pe_sez|qas_sez|','2019-06-12|2019-07-05|','2019-07-05',NULL,NULL,NULL,NULL,NULL,NULL),(11783,'47-173','GKN Aerospace Filton','BRACKET','524201','F5755098220002','NA','PART ISSUE F01',1,'GKN-GS-068 PHASE2- L','','90543','','0000-00-00',NULL,'yes','yes','yes','','','','','','','BORE DIAMETER OVERSIZED BY 30 MICRONS','DURING BORE FINISHING  OPERATION WHILE RE PASSING THE DIAMETER GOT OVERSIZED BY 30 MICRONS.|TO REMOVE THE 0.01MM STOCK THE OPERATOR HAS RE PASSED THE TOOL ','','|TRAINING TO BE GIVEN TO THE OPERATOR ON CORRECTION OF THE BORE BORE FINISHING OPERATION.','Boring operation done by operator is verified and found okay.','','2019-06-12','pe_sez(a)','        Madhu Kumar N','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','03','','','','','','|MACHINE WAS STOPPED AND INFORMED TO THE SUPERVISOR FOR VALIDATION.','Z3456','pe_sez|qas_sez|qas_sez|','2019-06-12|2019-06-12|2019-09-20|','2019-09-20',NULL,NULL,NULL,NULL,NULL,NULL),(11784,'28-039','Magellan Aerospace New York  Inc.','SPACER WASHER, BUSHING - ','1802720422','161A2303-1','','PL _A, PSDL_ N/C',3,'A000160675','','93193','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Total Length Required: 50.063mm/50.165mm \r\nmeasured : 50.008mm/49.993mm.','Step found on face after bore finish|Due to Boring insert wear out, burr found on chamfer so insert changed|After change of insert step found on part face|Z offset not cross checked after change of Insert.','|set the dial stand & ensure the controlled features found OK.|set the dial stand & ensure the controlled features found OK.','|Provide the checklist while insert change & ensure the offset,other parameters during production. |Provide the checklist while insert change & ensure the offset,other parameters during production. ','CAPA Found OK','','2019-06-12','Sandhesh D(S)','Sagar  GB,Dinakar K,Adithya  H N,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','FI','no','LMW LX20T-1','Ranjith(G)','no','','|Cross check the previous production runned parts found OK|Cross check the previous production runned parts found OK','E3456','||qas_sez|','2019-06-14|2019-06-14|2019-06-25|','2019-06-25',NULL,NULL,NULL,NULL,NULL,NULL),(11785,'56A-117','GKN Aerospace Orangeburg','RH ROOT FTG-UPR BLADE','','119A1210-9604','','119A1210 PSDL REV C',1,'A000049193','','A26259','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','AFTER REAMING OPERATIONS HOLE POSITION NOT ACHIVED','','','','','','2019-06-12','pe_sez(a)','NataRaj.CV()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','no','no','no','Assembly','','5','yes','Misc','pe_sez(a)','no','M07950|BACB28AP10Z039','','Z3456','qas_sez|','2019-06-12|','0000-00-00',NULL,NULL,NULL,NULL,NULL,NULL),(11787,'35-599','Saab AB','BEAM','814245','D5227338120400','NA','PART ISSUE C',1,'OWED-LTA-001','','88211','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Dia 15.877H7 bore over size by 0.12 to 0.14mm. ','Pre bore diameter had more stock|When pre bore operation running time cutting tool cutting edge shipped out|Due more the reamer got more load and take the excess material','|Instead of Endmill for pre boring operation, a Hole mill added after the drilling operations to maintain the constant for the Reamer.','|The cutting edge of the Hole mill to be ensure each and every part before the Reaming operations','CA PA Found ok.','','2019-06-12','Karthik Raj T()','Vijay Kumar H.J,Thaveni D M ,Ravi Kumar G.B,Nagaraju P K ,HariPrasad ,Dhanush J.K,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','a51nx-05','qas_sez(a)','no','','|Production stopped and produced part are checked and found ok.','Z3456','qas_sez|pe_sez|qas_sez|','2019-06-12|2019-10-17|2019-10-19|','2019-10-19',NULL,NULL,NULL,NULL,NULL,NULL),(11788,'56-115','GKN Aerospace Orangeburg','RH LOWER ARROWHEAD','657226','119A1433-9604','NA','NIL',4,'A000049193','','92199','','0000-00-00',NULL,'yes','no','no','no','yes','yes','no','no','no','profile mismatch','','','','','','2019-06-12','Mahesh(N)','Yogesh A P,Vijay Kumar H B,Vasu SN,Rajesh B D,Manjunatha N.R.,Kammar Nagaraj,Harishkumar B N,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Cancelled','no','no','no','With Treatment','DN59097','final','yes','HASS VR11','Mahesh(N)','no','','','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11789,'56-009','GKN Aerospace Orangeburg','SPLICE PLATE FWD LWR','17802DD','119A1214-603','NA','PSDL REV-',1,'LTA GKN 737 Winglet','','94199','','0000-00-00',NULL,'no','','yes','','','','yes','yes','','While trailing out with the new tool(MA FORD) dent mark found on the part.','During re engineering to reduce the cycle time and CPC(cost per component)the new tool trail out was carried out.|While new tool trailing (MA FORD) the tool got melted and due to the chips of the melted tool the deep dent mark formed on the surface of the part. ','|Due to the failure of the trailed out tool the new tool got replaced with the regular make.','|na','capa found satisfactory.','','2019-06-12','pe_sez(a)','        Rajesha A.R','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','3','','','','','','|Due to the failure of the trailed out tool the new tool got replaced with the regular make.','Z3456','pe_sez|qas_sez|','2019-06-13|2019-06-13|','2019-06-13',NULL,NULL,NULL,NULL,NULL,NULL),(11790,'56-098','GKN Aerospace Orangeburg','CLOSEOUT - CHORD, LWR','798231A7','119A1381-603','NA','PSDL REV -',1,'A000047470','','93510','','0000-00-00',NULL,'yes','yes','yes','','','','','','','PROGRAM RUNNING TIME TOOL BROKEN DUE TO WHICH DIG MARK ON THE PART  ','DUE TO THE OVERHANG LENGTH THE TOOL GOT BROKEN.|THE OPERATOR HAS NOT CROSS VERIFIED THE OVERHANG LENGTH.','|NEW TOOL WAS LOADED WITH THE CORRECT TOOL  LENGTH AND ALL THE PARTS PRODUCED WERE FOUND OK|NEW TOOL WAS LOADED WITH THE CORRECT TOOL  LENGTH AND ALL THE PARTS PRODUCED WERE FOUND OK|NEW TOOL WAS LOADED WITH THE CORRECT TOOL  LENGTH AND ALL THE PARTS PRODUCED WERE FOUND OK','|INSTRUCTION WAS GIVEN TO ALL THE OPERATORS TO CROSS CHECK ALL PARAMETERS AND DOUBLE ENSURE IT BEFORE RUNNING THE MACHINE.|INSTRUCTION WAS GIVEN TO ALL THE OPERATORS TO CROSS CHECK ALL PARAMETERS AND DOUBLE ENSURE IT BEFORE RUNNING THE MACHINE.|INSTRUCTION WAS GIVEN TO ALL THE OPERATORS TO CROSS CHECK ALL PARAMETERS AND DOUBLE ENSURE IT BEFORE RUNNING THE MACHINE.','CAPA FOUND SATISFACTORY.','','2019-06-14','pe_sez(a)','        Tejas M','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','5','','','','','','|MACHINE WAS STOPPED AND ALL PARAMETERS WERE CROSS CHECKED AND CORRECTED THE OVERHANG LENGTH.|MACHINE WAS STOPPED AND ALL PARAMETERS WERE CROSS CHECKED AND CORRECTED THE OVERHANG LENGTH.|MACHINE WAS STOPPED AND ALL PARAMETERS WERE CROSS CHECKED AND CORRECTED THE OVERHANG LENGTH.','Z3456','pe_sez||||','2019-06-17|2019-06-27|2019-06-27|2019-06-27|','2019-06-27',NULL,NULL,NULL,NULL,NULL,NULL),(11791,'35A-464','Saab AB','FITTING ASSY','','D522 73408 001 00','','A',1,'OWED-LTA-001','','A23944','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Is condition: Flange on bushing is sticking out more than 1,68 mm \r\nShould be: Flange would stick out 1,55-1,68 mm in accordance to drawing D52273408 and AIPS 01-02-019\r\n','Flange projection out of tolerance from the specification limit. |More sealant was applied in the flange of the bush, due to which the bush did not assembled properly and the bush protrusion was not measured.|Bush protrusion requirement isn\'t called in the drawing because of which both the operator and inspector didn\'t ensured the projection before the shipment.','|Bushes are removed and reassembled to meet the requirements.','|APS revised and training was given to both inspector and operators on how to inspect the bush protrusion.','Effectiveness will be measured by 23_SEP_2019','C76977','2019-06-15','Dharani(Shankar)','Dharani(Shankar)','mail','2019-06-06','W/O No A23944 33 pcs, A23946 7 pcs, A23945 13 pcs, A22517 13 pcs,W/O No A22515 1 pc, A22516 5 pcs, A22517 11 pcs,W/O No A23947 4 pcs,W/O No A24000 1 pc, A24465 3 pc,A24466 3pc, A24467 1 pc,W/O No A24469 9 pcs, A24470 7 pcs','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER END','yes','Misc','qas_sez(a)','no','','We have inspected our stock parts and are found okay. We also inspected the BOI parts they also and found within limits.|We have inspected our stock parts and are found okay. We also inspected the BOI parts they also and found within limits.','Z3456','qas_sez|','2019-08-13|','2019-08-13',NULL,NULL,NULL,NULL,NULL,NULL),(11792,'35A-600','Saab AB','FRAME ASSY','','D5227338500800','','PART ISSUE C',4,'OWED-LTA-001','','A24153','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','yes','Is condition: \r\n3 pcs with small marks, metal visible.\r\n1 pc with very thin material, 105mm x 15mm mm.\r\n\r\nShould be: Frame assy without marks and too thin material.\r\n','1)a) Due to improper handling of part during the assembly the assembly operation the paint layer got damaged and the inspection team did not identify the part during visual inspection.\r\nb) Edge breaking operation done on the part was not effective.\r\n|2) a) Due to overhanging of the part during bush and rivet assemblies the part got damaged because of miss handling.\r\nb) Edge Breaking is done manually during which the operator missed to ensure complete coverage.\r\n','|1) Instructed assembly operator to use supporting blocks to avoid overhanging of the part during assembly.\r<br/>2) Re-fresher training given to the inspection team on the identification of critical locations, and importance of visual inspection.\r<br/>3) Instructed the de burring operator to carry out de burring with a predefined path i.e. start from one point and end at the same point complete de burring one feature after other.\r<br/>','|1) Assembly table for the lengthy parts is rearranged to avoid overhanging of the part.\r<br/>2) De burring operation flow is changed so that the operator ensures complete coverage of all the features.','Next batches produced verified and found ok.','C77259','2019-06-15','Dharani(Shankar)','Dharani(Shankar)','mail','2019-06-06','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER END','yes','Misc','qas_sez(a)','no','','We have inspected our stock parts and are found okay.','Z3456','qas|','2019-07-06|','2019-07-06',NULL,NULL,NULL,NULL,NULL,NULL),(11793,'56-011','GKN Aerospace Orangeburg','SPLICE PLATE AFT LWR','8-09-08984/29248','119A1214-607','NA','PSDL REV-',1,'LTA GKN 737 Winglet','','90421','','0000-00-00',NULL,'yes','yes','yes','','','','','','','HOLE DIA OVER SIZE BY 0.8MM DUE TO THE WRONG TOOL SELECTION.','IN THE PREVIOUS SHIFT THE CRN 56-008(REAMER DIA 9.51) WAS LOADED IN THE MACHINE AND IN THE NEXT SHIFT THE CRN 56-011(REAMER DIA 8.0) WAS SUPPOSED TO BE LOADED IN PLACE OF 9.51 REAMER  IN THE MACHINE.\r\n|THE OPERATOR HAS NOT ENSURED THE REAMER SIZE BEFORE LOADING THE PART. DUE TO WHICH THE PART GOT REJECTED BECAUSE OF THE WRONG TOOL.','|THE OPERATOR WAS ADVISED TO ENSURE THE TOOLS AND READ ALL THE INSTRUCTIONS GIVEN IN THE CHECKLIST AND SIGN THE SAME  BEFORE LOADING THE PART TO THE MACHINE.','|THE OPERATOR WAS ADVISED TO ENSURE THE TOOLS AND READ ALL THE INSTRUCTIONS GIVEN IN THE CHECKLIST BEFORE LOADING THE PART TO THE MACHINE.','CAPA FOUND SATISFACTORY.','','2019-06-15','pe_sez(a)','        Rajesha A.R','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','5','','','','','','|THE PART WAS CHECKED ONCE HE NOTICED THE HOLE DIA  OVER SIZED THE OPERATOR CROSSCHECKED THE TOOLS AND THE CORRECT TOOL WAS REPLACED AND NC WAS RAISED FOR THE REJECTED PART.','Z3456','pe_sez|qas_sez|','2019-06-17|2019-06-18|','2019-06-18',NULL,NULL,NULL,NULL,NULL,NULL),(11794,'18-664A','Magellan Aerospace Bournemouth','GAMMA FITTINGS','M940330/20715','NSA840020-150','','L',7,'428939','','92747','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','no','Dent marks observed on Outer diameter of the part','','','','','','2019-06-17','qas_sez(a)','qas_sez(a)','','0000-00-00','NC CREATION','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','no','yes','no','With Treatment','DN58094','POST DN','no','Misc','qas_sez(a)','yes','','','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11795,'18-667A','Magellan Aerospace Bournemouth','GAMMA FITTINGS ','M506580','NSA840020-300','','L',1,'428939','','92725','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','no','Dent marks observed on edge of the part','','','','','','2019-06-17','qas_sez(a)','qas_sez(a)','','0000-00-00','NC CREATION','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','no','yes','no','With Treatment','DN58078','POST DN','no','Misc','qas_sez(a)','yes','','','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11796,'56-013','GKN Aerospace Orangeburg','FAIRING SUPPORT - AFT','573262','119A1521-603','NA','PSDL REV A',1,'A000043737 Rev2','','90555','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Dig mark observed on wall.','1) During part loading time the fixture slipped and dent marked formed on the part.|2) Handing of the fixture by a single operator was difficult.|3) Gross weight of the fixture and loaded part was high for a single person to handle.','|Additional support was provided to the operator to load and unload the fixture to the machine.','|1) Informed the Engineering team to consider the gross weight of fixture and part while designing new fixtures.\r<br/>2) Re-designed the fixture and removed some excess material to reduce the weight of the fixture.','New fixtures manufactured and next batch production verified and found ok.','','2019-06-17','pe_sez(a)','','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','no','','','','5','yes','','','','','|Immediately informed the supervisor and checked the fixture and part for any damage and then continued the production after confirming no defect.','Z3456','pe_sez|qas_sez|qas_sez|','2019-06-24|2019-07-12|2019-12-05|','2019-12-05','0000-00-00','0000-00-00','0000-00-00','','',''),(11797,'35-597','Saab AB','CORNER','934274 B','D5227338620200','NA','PART ISSUE B',1,'OWED-LTA-001','','88114','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Running time tool broken so dig mark on the part.','Due to increase the RPM & FEED|To reduce the cycle time|Target cycle time not achieved','|Inform to supervisor,change the FEED particular dig area.','|While FAI proving time set the RPM,FEED & stock in order to meets the target cycle time.','CAPA Found OK','','2019-06-17','Gurukiran S(M)','Manohara(M)','','0000-00-00','running time tool broken so dig mark on the part ,,','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','05','no','Misc','Gurukiran S(M)','no','','|Inform to supervisor,change the FEED particular dig area.','E3456','qas_sez|qas|qas_sez|','2019-06-19|2019-06-19|2019-06-25|','2019-06-25',NULL,NULL,NULL,NULL,NULL,NULL),(11798,'51-151','THE BOEING COMPANY','LWR SKIN COVER','0-24-11163/24128','312Z3122-502','NA','NIL',1,'BOEING 001X','','92855','','0000-00-00',NULL,'no','yes','yes','yes','no','no','no','no','no','THICKNESS UNDER SIZED DUE TO PART BEND DURING 1ST SETUP MACHINING.','THE PART GOT LIFTED DUE TO THE BEND IN THE PART THE THICKNESS GOT UNDERSIZED.|THE BEND WAS NOT CHECKED AFTER THE ROUGHING OPERATION','|INSTRUCTED THE OPERATOR TO CHECK THE PART AFTER THE ROUGHING OPERATION AND ENSURE THERE IS NO BEND IN THE PART BEFORE STARTING THE NEXT OPERATION.|INSTRUCTED THE OPERATOR TO CHECK THE PART AFTER THE ROUGHING OPERATION AND ENSURE THERE IS NO BEND IN THE PART BEFORE STARTING THE NEXT OPERATION.|INSTRUCTED THE OPERATOR TO CHECK THE PART AFTER THE ROUGHING OPERATION AND ENSURE THERE IS NO BEND IN THE PART BEFORE STARTING THE NEXT OPERATION.','|INSTRUCTED THE OPERATOR TO CHECK THE PART AFTER THE ROUGHING OPERATION AND ENSURE THERE IS NO BEND IN THE PART BEFORE STARTING THE NEXT OPERATION.|INSTRUCTED THE OPERATOR TO CHECK THE PART AFTER THE ROUGHING OPERATION AND ENSURE THERE IS NO BEND IN THE PART BEFORE STARTING THE NEXT OPERATION.|INSTRUCTED THE OPERATOR TO CHECK THE PART AFTER THE ROUGHING OPERATION AND ENSURE THERE IS NO BEND IN THE PART BEFORE STARTING THE NEXT OPERATION.','CAPA FOUND SATISFACTORY','','2019-06-18','pe_sez(a)','Maruthi  D R()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','pe_sez(a)','no','','|THE MACHINE WAS STOPPED AND PART WAS MOVED TO THE QUARENTINE AREA AND NC WAS RAISED|THE MACHINE WAS STOPPED AND PART WAS MOVED TO THE QUARENTINE AREA AND NC WAS RAISED|THE MACHINE WAS STOPPED AND PART WAS MOVED TO THE QUARENTINE AREA AND NC WAS RAISED','Z3456','|||qas_sez|','2019-06-26|2019-06-26|2019-06-26|2019-06-29|','2019-06-29',NULL,NULL,NULL,NULL,NULL,NULL),(11799,'47-098B','GKN Aerospace Filton','BRACKET M/C TRACK 2 FWD ','01117551','F57550193000','NA','PART ISSUE H02',1,'LTA-GKN-002','','91547','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Wall dig mark observed .','Due to insert screw loosing in cutter dia 40.|During the machining insert screw was loosed so operator not identified abnormal sound.','|When this abnormal sound issue noticed by operator stop the machine & inform to supervisor.','|Add M00 in program for cross check the insert screw before start machine.\r<br/>split the the roughing program.','CAPA FOUND OK','','2019-06-18','Gurukiran S(M)','Krishna(Chowdary.G.P.)','','0000-00-00','Wall dig mark observed .','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','01','no','Misc','Gurukiran S(M)','no','','|When this abnormal sound issue noticed by operator stop the machine & inform to supervisor.','E3456','qas_sez|qas|','2019-06-25|2019-06-28|','2019-06-28',NULL,NULL,NULL,NULL,NULL,NULL),(11800,'51-072','THE BOEING COMPANY','BANJO FITTING','G23991K05','113T1204-2','NA','NIL',1,'BOEING 001S','','93184','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Hole position shift by 1.0mm.','Due to wrong work offset.|Operator consider the drawing dimensions & enter the work offset.|Operator not refer the MPS.','|1)Cross check the work offset & increase the 1MM by X-axis & run the production.\r<br/>\r<br/>','|Add the massage in program before taking work offset & cross check the X-axis work offset.','CAPA FOUND OK','','2019-06-18','Gurukiran S(M)','MANJE(GOWDA S)','','0000-00-00','Hole position shift by 1.0mm','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','09','no','Misc','Gurukiran S(M)','no','','|Cross check the work offset & increase the 1MM by X-axis & run the production','E3456','qas|qas|qas|','2019-06-19|2019-06-19|2019-06-28|','2019-06-28',NULL,NULL,NULL,NULL,NULL,NULL),(11801,'56-051','GKN Aerospace Orangeburg','STIFFENER','C796751','475Z1610-100','NA','NIL',1,'A000046132','','93692','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','WIDTH 0.08 MM OVER SIZE \r\n','Due to part not butting properly|Extrusion material 90 degree angle not achieved','|Get awareness to operator when do the next batch production','|100 % check the next batch production parts,','CAPA FOUND OK','','2019-06-20','Subramanya L(Naik)','Eranna K,DILIP G C ,Balaji ,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','','FI','yes','MakinoF5-3','Narasimha Murthy(R)','no','','|Get awareness to operator when do the next batch production','E3456','qas|qas|','2019-06-25|2019-06-28|','2019-06-28',NULL,NULL,NULL,NULL,NULL,NULL),(11802,'51-127','THE BOEING COMPANY','NUT','205870B9','251W4145-2','NA','PSDL REV A',1,'BOEING 001Q','','93190','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Thread core diameter over size.','Due to thread length rework.|Thread length not achieved during first threading cycle.|Wrong offset taken in the thread mill tool by the operator.','|Re-took the tool offset in front of supervisor and continued the production after validating the offset.','|Training given to the operator and M0 comment included in the program to instruct operator to verify the tool offset before starting the cycle.','CA PA Found ok','','2019-06-20','Gurukiran S(M)','SIDDESH()','','0000-00-00','Double thread forming .','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','11','no','Misc','Gurukiran S(M)','no','','|Immediately stopped the machine and informed the supervisor and checked the offset of all the other tools.','E3456','qas|qas|','2019-06-24|2019-07-01|','2019-07-01',NULL,NULL,NULL,NULL,NULL,NULL),(11803,'35-724','Saab AB','LEVER  ','Z87L','D5227346721400','NA','PART ISSUE F',1,'OWED-LTA-001','','94174','','0000-00-00',NULL,'yes','yes','yes','','','','','','','DIA 10F/L TOOL BROKEN WHILE RUNNING AND DIG MARK FOUND ON PART..','Due to breakage of tool during running time the part got dent and rejected.|The cutting edges of the tool, holding length, flow of coolant and load applied to the tool during running time were not monitored during machining.','|Informed the supervisor about the tool breakage and changed the tool re-took the offset and continued the production.','|1) Production supervisors to ensure proper tool length holding, flow of cutting fluid and good condition of holders every day.\r<br/>2) Operators should verify the wear of cutting edges on the tool before start of every shift.\r<br/>3) Engineering department need to verify smooth tool path and need to avoid sudden and intensive loading of the tool during running time.\r<br/>','All the actions above need to be monitored for one month final effectiveness will be measured on 4-Aug-2019.','','2019-06-20','pe_sez(a)','        Karthik Raj T ','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','3','','','','','','|Checked the previously completed parts for chattering marks and dimensional issues and all the parts found ok.','Z3456','pe_sez|qas_sez|','2019-06-24|2019-07-05|','2019-07-05',NULL,NULL,NULL,NULL,NULL,NULL),(11804,'35-601A','Saab AB','FRAME','532793C','D5227338520600','NA','PART ISSUE D',4,'OWED-LTA-005','','94190','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','BASE THICKNESS - SIDE 1MM','1) Due to excess bend on the part after roughing operation part lifted and resulted in thickness under-size	|2) During the final pass in finishing operation due to residual stress the part is getting lifted up.	|3) During aging time between the roughing and the finishing operation the material was not left in free condition (i.e. the materials were loaded one over the other).		','|Informed all the operators to leave the part in free condition during the aging process. 			','|Training provided to all the operators on site to avoid storage of parts one above the other during the aging operation','CAPA FOUND OK','','2019-06-21','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Prashanth Kumar(M)','no','','|Immediately stopped the machine and arranged the material so that the parts are left in free condition. 		','E3456','qas|','2019-09-23|','2019-09-23',NULL,NULL,NULL,NULL,NULL,NULL),(11805,'53-026','Triumph Aerostructures','STRAP, LWR JOINT, TRACK 9','20161453','F5745171920100','NA','PART ISSUE A, ECN PG205026001KD08',1,'LTA TRIUMPH 2018','','93993','','0000-00-00',NULL,'yes','yes','yes','','','','','','','part bend so base thickness -0.1mm','Operator not ensure part butting by using feeler gauge.\r\n|Part bend while machining.|Due to improper clamping.','|1)Inform to supervisor & change the clamping method & run the production.\r<br/>2)Next production Part found ok','|1) Add the massage in program & include the correct clamping method in MPS.\r<br/>2) Ensure the butting face by using feeler gauge.','CA PA found ok','','2019-06-21','Dhananjaya(N)','        Narasimhamurthy C','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','3','','','','','','|Inform to supervisor & change the clamping method & run the production.','E3456','pe|qas|qas|','2019-06-22|2019-06-22|2019-07-19|','2019-07-19',NULL,NULL,NULL,NULL,NULL,NULL),(11806,'35-725','Saab AB','LEVER  ','WW4A','D5227346721500','NA','PART ISSUE F',1,'OWED-LTA-001','','92435','','0000-00-00',NULL,'yes','yes','yes','','','','','','','running time tool broken dig mark found','Due to breakage of tool during running time the part got dent and rejected.|The cutting edges of the tool, holding length, flow of coolant and load applied to the tool during running time were not monitored during machining.','|Informed the supervisor about the tool breakage and changed the tool re-took the offset and continued the production.','|1) Production supervisors to ensure proper tool length holding, flow of cutting fluid and good condition of holders every day.\r<br/>2) Operators should verify the wear of cutting edges on the tool before start of every shift.\r<br/>3) Engineering department need to verify smooth tool path and need to avoid sudden and intensive loading of the tool during running time.\r<br/>','All the actions above need to  be monitored for one month final effectiveness will be measured on 4-Aug-2019.','','2019-06-21','pe_sez(a)','        HariPrasad ','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','3','','','','','','|Checked the previously completed parts for chattering marks and dimensional issues and all the parts found ok.','Z3456','pe_sez|qas_sez|','2019-06-24|2019-07-05|','2019-07-05',NULL,NULL,NULL,NULL,NULL,NULL),(11807,'53-057','Triumph Aerostructures','FORK FITTING ','457425A','F57953444200A01','NA','PART ISSUE A',1,'LTA 4 - TRIUMPH 2018','','92886','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','BOTTOM WALL THICKNESS UNDERSIZED BY 0.13MM','DURING 90 DEGREE A AXIS ROTATION DUE TO THE VIBRATION THE WALL THICKNESS GOT UNDERSIZED.|DURING THE FIRST PART PROVING OUT THE CHATTERING MARKS WERE OBSERVED ON THE PART DUE TO THE VIBRATION WHILE AVOIDING THE MISMATCH AND CHATTERING THE PART THICKNESS GOT UNDERSIZED.|SINCE  THE CUTTING PARAMETERS WERE NOT PROPERLY ADJUSTED DURING THE FIRST PART PROVING OUT.','|THE CUTTING PARAMETERS WERE CHECKED AND ADJUSTED TO AVOID THE VIBRATION.NEXT PRODUCED PARTS WERE FOUND OK.\r<br/>AND THE CORRECTED PARAMETERS PROGRAM WAS SAVED AND INFORMED THE OPERATOR TO CROSS VERIFY ALL THE PARAMETERS BEFORE RUNNING THE FIRST PART.','|REFER CORRECTIVE ACTION.','CAPA FOUND SATISFACTORY AND ALL PRODUCED AFTER THIS BATCH WERE FOUND OK.','','2019-06-22','pe_sez(a)','Shivaraj K S,Pradeep B.D,Madhu Kumar N,Kiran KM,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','1','no','Slim3n-4AHS-4','pe_sez(a)','no','','|MACHINE WAS STOPPED AND THE CUTTING PARAMETERS WERE CHECKED AND ADJUSTED TO AVOID THE VIBRATION.','Z3456','qas_sez|','2019-06-22|','2019-06-22',NULL,NULL,NULL,NULL,NULL,NULL),(11808,'18-090A','Magellan Aerospace(Polska) Sp','BUSH','1670511-3YT2M','PID278 50164 200','','A',5,'104569','','91045','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Outer diameter was 0.15mm undersized.','1)OD Undersized -0.015mm beyond drawing limit.\r\n|2)OD undersized during the re-pass operation as the re-pass ran twice.\r\n|3)Re-pass ran twice with same -0.15 wear offset as the operator provided +0.2mm wear offset during the insert change.\r\n','|\r<br/>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.\r<br/>','|1.Informed all the operator to check the relevant features after the insert change and provide of the offset accordingly with proper guidance from the supervisor or senior operators.\r<br/>','CA PA found ok','','2019-06-22','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','03','no','Misc','Dinakar(K)','no','','|1.Immediately stopped the machine and changed the wear offset and continued the production on the next part.\r\n','E3456','pe|qas|','2019-07-01|2019-07-19|','2019-07-19',NULL,NULL,NULL,NULL,NULL,NULL),(11809,'56-121','GKN Aerospace Orangeburg','CLOSEOUT RIB - LWR, FWD','445621','119A1440-618','NA','PSDL REV C',1,'LTA GKN ORANGEBURG K','','93235','','0000-00-00',NULL,'yes','yes','yes','','','','','','','part running time drill and holemill broken hole oblong   ','Due to breakage of tool during running time the part got dent and rejected.|The cutting edges of the tool, holding length, flow of coolant and load applied to the tool during running time were not monitored during machining.','|Informed the supervisor about the tool breakage and changed the tool re-took the offset and continued the production.','|1) Production supervisors to ensure proper tool length holding, flow of cutting fluid and good condition of holders every day.\r<br/>2) Operators should verify the wear of cutting edges on the tool before start of every shift.\r<br/>3) Engineering department need to verify smooth tool path and need to avoid sudden and intensive loading of the tool during running time.\r<br/>','All the actions above need to  be monitored for one month final effectiveness will be measured on 4-Aug-2019.','','2019-06-23','pe_sez(a)','        Anand ','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','3','','','','','','|Checked the previously completed parts for chattering marks and dimensional issues and all the parts found ok.','Z3456','pe_sez|qas_sez|','2019-06-24|2019-07-05|','2019-07-05',NULL,NULL,NULL,NULL,NULL,NULL),(11810,'18-210B','Magellan Aerospace Wrexham','BODY','M022730/27066','D321 40204 204','','D, ECN NR29999ST1KM15, NR29999ST2KF65, WQN DFB09775',2,'175174','','92529','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','OD UNDER SIZE BY -0.35MM','OD measured out of bottom limit to the drawing requirement.|Due to cross cutting of the RM run-out on the OD diameter resulted in this rejection.|Operator did not ensured the run out of the part before staring the cycle.','|Informed the operator to segregate the parts with high run out(i.e. greater than 0.2mm) and continued the production.','|Run out on the RM due to cross cutting will be avoided before starting the cycle.','CA PA Ok.','','2019-06-24','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Dinakar(K)','no','','|Immediately stopped the machine and instructed the operator to check the run out of the remaining RM and checked the previously completed parts.','E3456','qas|','2019-09-30|','2019-09-30',NULL,NULL,NULL,NULL,NULL,NULL),(11811,'18-693A','Magellan Aerospace Bournemouth','HOUSING OUT BD BRG','1683197-3/ZMAN','D275 40005 200','','C01',1,'425757','','93667','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','DENT MARKS OBSERVED','TRANSACTION DENT','|AFTER REWORK PART OK','|AFTER REWORK PART OK','CA/PA FOUND OK','','2019-06-25','qas(qas)','qas(qas)','','2019-06-25','NC CREATED','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','14','no','Misc','qas(qas)','no','','|TO CHECK THE ALL  PARTS ON THIS BATCH . PARTS FOUND OK ','E3456','qas|','2019-07-02|','2019-07-02',NULL,NULL,NULL,NULL,NULL,NULL),(11812,'35-717','Saab AB','','D87797 YQE4','D5227349320600','NA','PART ISSUE E',2,'OWED-LTA-005','','91213','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Ra value required 1.6 in 18.8E7 BORE measured 2.5','1.While boring operation running time surface finish not achieved  |2.Tool chip out while running |3.improper coolant supply on inside the boring operation so cutting edge chip-out ','|1.information given to all operators and check the every part \r<br/>before removing the finish part .','|1.coolant pipe length increased and proper checking method training will be given to operators. ','CA  PA found ok','','2019-06-27','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','Ra value required 1.6 in 18.8E7 BORE measured 2.5  ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','06','no','Misc','Yashawantha(NH)','no','','|1.stop the machine and check the previous running parts, ','E3456','qas|pe|qas|','2019-06-27|2019-07-01|2019-07-19|','2019-07-19',NULL,NULL,NULL,NULL,NULL,NULL),(11813,'35-718','Saab AB','','D87797 YQE4','D5227349320700','NA','PART ISSUE E',3,'OWED-LTA-005','','91215','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Ra value required 1.6 in 18.8E7 bore measured value 3.5 ','1.While boring operation running time surface finish not achieved  \r\n|2.Tool chip out while running \r\n|3.improper coolant supply on inside the boring operation so cutting edge chip-out \r\n','|1.information given to all operators and check the every part \r<br/>before removing the finish part .\r<br/>','|1.coolant pipe length increased and proper checking method training will be given to operators.','CA PA found ok','','2019-06-27','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','06','no','Misc','Yashawantha(NH)','no','','|1.stop the machine and check the previous running parts,\r\n','E3456','pe|qas|','2019-07-01|2019-07-19|','2019-07-19',NULL,NULL,NULL,NULL,NULL,NULL),(11814,'35-718','Saab AB','','D87797 YQE4','D5227349320700','NA','PART ISSUE E',2,'OWED-LTA-005','','91215','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','DISTANCE REQUIRED 13.65+/-0.1 MM MEASURED VALUE 13.82 MM','1.While boring operation running time surface finish not achieved  \r\n|2.Tool chip out while running \r\n|3.improper coolant supply on inside the boring operation so cutting edge chip-out \r\n','|1.information given to all operators and check the every part \r<br/>before removing the finish part .\r<br/>','|1.coolant pipe length increased and proper checking method training will be given to operators.','CA PA found ok.','','2019-06-27','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','06','no','Misc','Yashawantha(NH)','no','','|1.stop the machine and check the previous running parts,\r\n','E3456','pe|pe|qas|qas|','2019-07-01|2019-07-01|2019-07-04|2019-07-19|','2019-07-19',NULL,NULL,NULL,NULL,NULL,NULL),(11815,'35-670','Saab AB','BRACKET','532729B','D5227342920700','NA','PART ISSUE E',3,'OWED-LTA-002','','92033','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','POSITION ERROR ','1) Hole position measured out of drawing requirement.|2) During machining operation the operator did not ensured the tool wear correction after insert change.|3) inadequate awareness of the operator.','|Corrected the wear offset of the tool and cross checked the wear offset and work offset of the other tools loaded in the machine under supervisor guidance and continued production.','|Training provided to the operator to check and correct the wear correction.','CA PA ok.','','2019-06-28','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','1','no','Misc','Lohith(K)','no','','|Immediately stopped the machine and corrected the wear offset and measured the previously completed parts and segregated the affected parts and identified with proper tag.','E3456','qas|','2019-09-30|','2019-09-30',NULL,NULL,NULL,NULL,NULL,NULL),(11816,'51-179','THE BOEING COMPANY','ADAPTER - FLANGED, BULKHE','20228749','272U1230-2','NA','PSDL REV B',10,'BOEING 001Z','','94389','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Drill Depth oversized by 3mm.','THE ROUGHING OPERATION WAS SPLIT INTO TWO AS THERE WAS A PROBLEM IN THE INSERT.|12 DIA TOOL WAS SUPPOSED TO BE LOADED INSTEAD 18 DIA TOOL WAS LOADED IN THE MACHINE.','|THE OPERATOR WAS STRICTLY INSTRUCTED TO FOLLOW THE PROCEDURE AND IF ANY CHANGE IN THE PROCESS IT SHOULD BE FLOWED DOWN FROM THE ENGINEERING DEPARTMENT.|THE OPERATOR WAS STRICTLY INSTRUCTED TO FOLLOW THE PROCEDURE AND IF ANY CHANGE IN THE PROCESS IT SHOULD BE FLOWED DOWN FROM THE ENGINEERING DEPARTMENT.|THE OPERATOR WAS STRICTLY INSTRUCTED TO FOLLOW THE PROCEDURE AND IF ANY CHANGE IN THE PROCESS IT SHOULD BE FLOWED DOWN FROM THE ENGINEERING DEPARTMENT.','|IN FUTURE THE TOOL LIST SHOULD BE UPDATED IN THE MPS.|IN FUTURE THE TOOL LIST SHOULD BE UPDATED IN THE MPS.|IN FUTURE THE TOOL LIST SHOULD BE UPDATED IN THE MPS.','EFFECTIVENESS WILL BE CHECKED FOR NEXT PRODUCTION BATCHES.','','2019-06-28','Narasimha Murthy (K G)','Narasimha Murthy (K G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Narasimha Murthy (K G)','no','','|THE MACHINE WAS STOPPED AND NC WAS RAISED.|THE MACHINE WAS STOPPED AND NC WAS RAISED.|THE MACHINE WAS STOPPED AND NC WAS RAISED.','Z3456','|||qas_sez|','2019-06-28|2019-06-28|2019-06-28|2019-07-01|','2019-07-01',NULL,NULL,NULL,NULL,NULL,NULL),(11817,'51-179','THE BOEING COMPANY','ADAPTER - FLANGED, BULKHE','20238533','272U1230-2','NA','PSDL REV B',30,'BOEING 001Z','','94390','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Drill Depth Oversized by 3mm.','THE ROUGHING OPERATION WAS SPLIT INTO TWO AS THERE WAS A PROBLEM IN THE INSERT.|12 DIA TOOL WAS SUPPOSED TO BE LOADED INSTEAD 18 DIA TOOL WAS LOADED IN THE MACHINE.','|THE OPERATOR WAS STRICTLY INSTRUCTED TO FOLLOW THE PROCEDURE AND IF ANY CHANGE IN THE PROCESS IT SHOULD BE FLOWED DOWN FROM THE ENGINEERING DEPARTMENT.','|IN FUTURE THE TOOL LIST SHOULD BE UPDATED IN THE MPS\r<br/>AN ALERT MESSAGE WILL BE GIVEN IN THE PROGRAM FOR CROSS CHECKING TOOLS TO BE LOADED IN THE MACHINE.','EFFECTIVENESS WILL BE CHECKED FOR NEXT PRODUCTION BATCHES.','','2019-06-28','Narasimha Murthy (K G)','Narasimha Murthy (K G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Narasimha Murthy (K G)','no','','|THE MACHINE WAS STOPPED AND NC WAS RAISED.','Z3456','qas_sez|','2019-07-01|','2019-07-01',NULL,NULL,NULL,NULL,NULL,NULL),(11818,'35-725','Saab AB','LEVER  ','Z87L','D5227346721500','NA','PART ISSUE F',2,'OWED-LTA-001','','94179','','0000-00-00',NULL,'yes','yes','yes','','','','no','','','DIA 10F/L ,6R1,6FL TOOLS BROKEN WHILE RUNNING..','Raw material have 2mm excess in Length.|When outer sizing program running time Dia 10Flat End mill got overload and broken. The follower tool Dia 6R1 and 6Flat End mill also broken and damaged the part. |The operator not observe the cutting tool Broken and uneven noise.','|The operator ensured the Raw material before the start the machining. New cutting tools replaced','|The operator ensured the Raw material before the start the machining. If he found any deviation, that Raw material send back to Store with the particular records.','CA PA ok.','','2019-06-28','Karthineyan(V.S.)','        Karthik Raj T ','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','3','','','','','','|Production Stooped. Remaining Raw materials checked.Found ok.','Z3456','pe|pe_sez|qas_sez|','2019-06-29|2019-11-19|2019-11-20|','2019-11-20',NULL,NULL,NULL,NULL,NULL,NULL),(11819,'56-107A','GKN Aerospace Orangeburg','FAIRING SUPPORT - FWD','720240B1','119A1520-604','NA','PSDL REV B',1,'LTA GKN ORANGEBURG W','','92730','','0000-00-00',NULL,'yes','yes','yes','','','','','','','running time tool broken\r\n tool dig mark ','Due to breakage of tool during running time the part got dent and rejected.|The cutting edges of the tool, holding length, flow of coolant and load applied to the tool during running time were not monitored during machining.','|Informed the supervisor about the tool breakage and changed the tool re-took the offset and continued the production.','|1) Production supervisors to ensure proper tool length holding, flow of cutting fluid and good condition of holders every day.\r<br/>2) Operators should verify the wear of cutting edges on the tool before start of every shift.\r<br/>3) Engineering department need to verify smooth tool path and need to avoid sudden and intensive loading of the tool during running time.','All the actions above need to  be monitored for one month final effectiveness will be measured on 4-Aug-2019.','','2019-06-29','Narasimha Murthy (K G)','        Chethan Kumar M','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','5','','','','','','|Checked the previously completed parts for chattering marks and dimensional issues and all the parts found ok.','Z3456','pe_sez|qas_sez|','2019-07-03|2019-07-05|','2019-07-05',NULL,NULL,NULL,NULL,NULL,NULL),(11820,'18-078A','Magellan Aerospace Wrexham','ADAPTOR ','M048350/27688','A282 50081 200PF','','A',2,'190629','','94491','','0000-00-00',NULL,'yes','yes','yes','','','','','','','ID OVERSIZE BY 0.04/0.06MM','1. DURING ID BORING OPERATION PROCESS BORE OVERSIZE OCCURRED|2. THE EXCESSIVE HEAT GENERATION AND BUILT-UP EDGES CREATED ON THE INSERT WHICH CAUSE TO REMOVAL OF THE EXCESS MATERIAL|3. THE SUFFICIENT COOLANT NOT FLOWED ON THE PART DUE TO THAT BUILT-UP EDGES AND HEAT GENERATION CREATED|4. COLLANT FILTER BLOCKED DUE TO THAT COOLANT WAS NOT FLOWED PROPERLY','|THE FILTER MAINTENANCE CARRIED OUT AND MAINTENANCE RECORD TO BE MONITOR.','|EVERY PREVENTIVE MAINTENANCE PERIOD, COOLANT TANK TO BE CLEANING AND FILTER SERVICING TO BE DONE.','capa found ok','','2019-06-30','Raghavendra Rao(R)','        KRISHNAMURTHY N','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','01','','','','','','|THE MACHINE WAS STOPPED AND INFORMED TO MAINTENANCE. THEN PARTS IN WIP AND FG FOUND OK.','E3456','pe|qas|qas|qas_sez|','2019-07-01|2019-08-20|2019-08-20|2019-08-31|','2019-08-31',NULL,NULL,NULL,NULL,NULL,NULL),(11821,'35-720','Saab AB','ROD BODY','6899','D5227333720200','NA','PART ISSUE B',1,'OWED-LTA-005','','93288','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','PITCH MEASURED UNDER SIZE. MINIMUM VALUE IS 9.9 MM MEASURED VALUE IS 9.8 MM 0.1 MEASURED MINUS ','Part total length tolerance is */- 0.2mm. But drilling point distance tolerance is */-0.1mm |when the drill operation, as per MPS. the drilling operation CNC programs drill coordinates from one face only. |If part total length with in 0.1mm tolerance, hole position distance is with in 0.1mm. If part total length above 0.1mm tolerance, hole position distance is apart from drawing dimensions.','|The part total length operations carried out along with drilling operations. the Part total length maintained with in the 0.1mm tolerance.   ','|The part total length operations will be carried out  along with drilling operations to maintain the all dimensions with in tolerance. ','CA PA ok','','2019-07-01','pe_sez(a)','Vijay Kumar H.J,Upendra N ,Manu K,Manu ,Karthik Raj T ,Dinakar K ,Ashok Kumar K,','','0000-00-00','PITCH MEASURED UNDER SIZE. MINIMUM VALUE IS 9.9 MM MEASURED VALUE IS 9.8 MM 0.1 MEASURED MINUS ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','a51nx-05','qas_sez(a)','no','','|Production Stopped. finished Parts checked.Found ok.','Z3456','pe_sez|qas_sez|','2019-11-16|2019-11-16|','2019-11-16',NULL,NULL,NULL,NULL,NULL,NULL),(11822,'56-107A','GKN Aerospace Orangeburg','FAIRING SUPPORT - FWD','720240B1','119A1520-604','NA','PSDL REV B',1,'LTA GKN ORANGEBURG W','','92730','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','PART CUT OUT TIME PART HOLE DAMAGED DUE TO M5 SCREW HEAD BROKEN','','','','','','2019-07-02','pe_sez(a)','Umesh B,Sanjeev S.D,NataRaj.CV ,Chethan Kumar M,Anand ,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','no','no','yes','With Treatment','','5','no','i700-4','pe_sez(a)','no','','','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11823,'51A-072','THE BOEING COMPANY','BEARING ASSY','','113T1204-1','','NIL',6,'BOEING 001S','','A20252','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Dents found on surface of bearing','The bought out item received was found dent.|Part to part contact happened in transportation|There were no sufficient cussion in packing material','|the dent dimensions were measured and sent to the customer for approval ','|Informed to the supplier to improve the packing method ','Customer approved the parts and found OK ','','2019-07-03','pe_sez(a)','pe_sez(a)','','0000-00-00','Dents found on bearing','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Assembly','','FI','no','Misc','qas_sez(a)','no','M03733|MS14103-6','|Informed to the supplier to improve the packing method All the parts were inspected visually and difected parts identified and sagrgated ','Z3456','qas_sez|','2019-10-17|','2019-10-17',NULL,NULL,NULL,NULL,NULL,NULL),(11824,'51A-072','THE BOEING COMPANY','BEARING ASSY','','113T1204-1','','NIL',3,'BOEING 001S','','A20253','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Dents found on surface of bearing','The bought out item received was found dent.|Part to part contact happened in transportation|There were no sufficient cussion in packing material','|the dent dimensions were measured and sent to the customer for approval ','|Informed to the supplier to improve the packing method','Customer approved the parts and found OK','','2019-07-03','pe_sez(a)','pe_sez(a)','','0000-00-00','Dents found on surface of bearing','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Assembly','','FI','no','Misc','qas_sez(a)','no','M03733|MS14103-6','|Informed to the supplier to improve the packing method All the parts were inspected visually and difected parts identified and sagrgated ','Z3456','qas_sez|','2019-10-17|','2019-10-17',NULL,NULL,NULL,NULL,NULL,NULL),(11825,'35-625','Saab AB','STOP BRACKET','788619','D5227281720000','NA','PART ISSUE A',1,'OWED-LTA-004','','92021','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Wall thickness undersized by 0.30MM\r\nDrawing required 2.40 MM but Part measures 1.91 to 2.00MM','Thickness undersized during manual rework.|Dent marks observed on the wall surface. |while loading the job, chips found in one side bottom of the job.|Improper cleaning of the butting surface.','|Instructed to clean the butting surface every time loading the part','|Instructed to clean the butting surface every time loading the part. Instructed to all the operators.','CA PA Found okay','','2019-07-04','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','Nc creation','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','Misc','Nagendra(SN)','no','','|Cleaned the fixture and checked previous parts and found okay.','E3456','qas_sez|','2019-07-09|','2019-07-09',NULL,NULL,NULL,NULL,NULL,NULL),(11826,'18-435B','Magellan Aerospace(Blackpool) Limited','MANIFOLD ','3278','PI201274609','NA','NIL',1,'Bpp-529619 amed-2','','94546','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Wrong tool selection so wall dig mark observed in part','1st part proving time wrong tool selected used 16 flat instead of 10flat. |Due to operator  negligence wrong toll selected  ','|Before part proving check list to be provided .','|Training given to operator Before run the program ensure the tool diameter twice ,\r<br/>','Next Batch Produced verified & Found Ok','','2019-07-04','Gurukiran S(M)','Niranjan(Murthy)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','05','no','Misc','Gurukiran S(M)','no','','|immediately stop the machine and change the proper corrected  tool for roughing program .','E3456','qas|qas_sez|','2019-07-05|2019-08-31|','2019-08-31',NULL,NULL,NULL,NULL,NULL,NULL),(11827,'18-090A','Magellan Aerospace(Polska) Sp','BUSH','1670513-3/Z83Q','PID278 50164 200','','A',2,'104569','','93304','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','OD UNDER SIZE BY -0.2MM.','due to wear out the insert OD under size','|change the insert and run the parts. ','|ensure the insert life and change the insert for life period. ','training providing to the operator.','','2019-07-05','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','03','no','Misc','Ravi(M)','no','','|Immediately stopped the machine and checked the previously running parts and separated the parts that were undersized. ','E3456','qas|','2019-07-24|','2019-07-24',NULL,NULL,NULL,NULL,NULL,NULL),(11828,'47-146','GKN Aerospace Filton','OUTB BTM LUG MACHINED','4892402 2','D5755024820101','NA','PART ISSUE A',2,'1210042824-1','','91583','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Bore Over Size +.008Micron to +.020Micron Ovality.','Coolant flowing to the tool tip was not in high pressure.|Small chips was blocked to the coolant vents to supply coolant with high pressure.','|while doing reaming operation to ensure the coolant pressure for every part . |while doing reaming operation to ensure the coolant pressure for every part . ','|To clean the coolant tank and coolant motor filter on every month|To clean the coolant tank and coolant motor filter on every month','CAPA FOUND OK','','2019-07-06','Ravi nayak()','Manjunatha.S.T(M)','','0000-00-00',' ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Manjunatha.S.T(M)','no','','|Stopped the machine immediately & cleaned the coolant pipe for the next part. |Stopped the machine immediately & cleaned the coolant pipe for the next part. ','A3456','||qas_aero|','2019-07-09|2019-07-09|2019-11-11|','2019-11-11',NULL,NULL,NULL,NULL,NULL,NULL),(11829,'47-167','GKN Aerospace Filton','TEE T/E RIB 2','3227601 1','F57550130200','NA','PART ISSUE D02',1,'GKN-GS-068 PHASE2- L','','92786','','0000-00-00',NULL,'yes','no','no','no','yes','yes','no','no','no','THICKNESS Oversized SIZE BY 0.12MM','Work Offset error done by the operator.|Typo error done by the operator while entering in the machine.|Operator did not cross verified the value entered by him.','|Identified part reworked and found ok.','|On Job training given to the operator on how to verify the tool offset.','Training effectiveness of the three shift operators verified and found ok.','','2019-07-06','pe_sez(a)','Raghu B,Madhu Kumar N,Kiran KM,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','With Treatment','','final','no','Slim3n-4AHS-1','Mahesh(N)','no','','|All the other parts machined verified and found ok.','Z3456','qas_sez|','2019-11-20|','2019-11-20',NULL,NULL,NULL,NULL,NULL,NULL),(11830,'35-597','Saab AB','CORNER','934275 A','D5227338620200','NA','PART ISSUE B',1,'OWED-LTA-001','','88120','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','GROOVING PROFILE MINUS UP TO 2 MM (AT SEZ MAZZAK I-700 MACHINE)','','','','','','2019-07-06','prodn_aero(prodn)','prodn_aero(prodn)','','0000-00-00','(AT SEZ MAZZAK I-700 MACHINE)','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','no','yes','no','With Treatment','','2nd','no','Misc','Ravi nayak()','no','','','A3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11831,'47-151','GKN Aerospace Filton','LWR ANGLE ATTACHMENT','1013901 5','F57254364202','NA','PART ISSUE C',1,'GKN-GS-068 PHASE2- L','','91100','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','PART WRONG LOADING ','Part wrong loaded to the machine. The rework fixture designed was also not fool proof.|Operator did not referred to the M.P.S. reference copy which was given near the machine.|Since it was a rework part the fixture was designed for one time use and the engineer did not considered the fool proofing of fixture.','|The production was continued under the presence of supervisor.','|Fool proof mistake proofing of the fixture will be ensured before issuing the fixture to production.','New fixtures manufactured verified and found okay.','','2019-07-06','pe_sez(a)','Pradeep(B.D)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','DN57693','5','no','Misc','pe_sez(a)','no','','|Immediately stopped the machine and informed the supervisor checked the previously completed parts and continued the production under supervisor presence.','Z3456','qas_sez|qas_sez|','2019-07-09|2019-09-20|','2019-09-20',NULL,NULL,NULL,NULL,NULL,NULL),(11832,'35-536','Saab AB','BRACKET','509499B','D522 73550 200 00','','PART ISSUE A',1,'OWED-LTA-002','','87330','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Part Width under size.\r\n','1.while part cutout program running time lifted .\r\n|2.part not holding properly .|3.part clamping hole thread damaged. ','|1.in fixture clamping hole enlarged and installed the Helicoil.','|1.Before loading the fixture to cross check the clamping holes \r<br/>condition ,','CAPA FOUND OK','','2019-07-08','Ravi nayak()','Manjunatha.S.T(M)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Manjunatha.S.T(M)','no','','|immediately stop the machine and change the clamp for next parts .','A3456','pe|qas_aero|qas_aero|','2019-07-09|2019-11-11|2019-11-11|','2019-11-11',NULL,NULL,NULL,NULL,NULL,NULL),(11833,'34-066A','Magellan Aerospace Winnipeg','BASE FITTING,F/D HINGE RH','G25209','400-12780-2','NA','EM104302 Iss B,EM105092 Iss H,EM104765 Iss H',1,'C81597 Rev 001','','94783','','0000-00-00',NULL,'yes','','yes','','yes','','','','','m/c y axis problem. y axis 1.40 shift','work offset wrong|after machine maintains work offset not ensured  ','|correct the work offset then run the other remaining parts.','|training providing the operator and in future ensure the work offset for after maintenance time.    ','provide the training material with sing of operator to the QAD','','2019-07-09','Dhananjaya(N)','        Venkatesh R','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','03','','','','','','|machine immediately stoped and correct the work offset    ','E3456','pe|qas|','2019-07-09|2019-07-17|','2019-07-17',NULL,NULL,NULL,NULL,NULL,NULL),(11834,'56-049A','GKN Aerospace Orangeburg','FAIRING SUPPORT - CTR, LW','567722','119A1531-603','NA','PSDL REV B',2,'LTA GKN ORANGEBURG W','','93920','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','During i-machining time part lifted.','During machining process part is lifted from the fixture.|Clamping bolt got loosen during the process.|Thread in the fixture was weared out and the operator didn\'t noticed it. ','|Rework done on the fixture threads and Helicoil is inserted.','|Instructed all operators to inspect fixture threads every time loading the part.','Effectiveness is verified on 12-AUG-2019','','2019-07-09','pe_sez(a)','Thaveni D M ,Manu ,HariPrasad ,Chetan N,Ananda M,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','1','no','a51nx-01','pe_sez(a)','no','','|Immediately inspected the previously machined parts and found okay','Z3456','qas_sez|','2019-07-11|','2019-07-11',NULL,NULL,NULL,NULL,NULL,NULL),(11835,'47-098B','GKN Aerospace Filton','BRACKET M/C TRACK 2 FWD ','01117551','F57550193000','NA','PART ISSUE H02',1,'LTA-GKN-002','','94628','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','dig mark on base of the part','fixture wrong direction  loading|after loading the fixture on the machine the engraved marking not able to see.','|engrave the part text(top and bottom) on the face of the fixture.','|change the location pin diameter ,different dia on top and bottom of the fixture locating pin. ','CA PA found ok.','','2019-07-09','Gurukiran S(M)','Shivanand(D.B.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Gurukiran S(M)','no','','|stop the machine immediately,change the direction of the fixture  ','E3456','qas|qas|','2019-07-12|2019-07-29|','2019-07-29',NULL,NULL,NULL,NULL,NULL,NULL),(11836,'18-722A','Magellan Aerospace(Blackpool) Limited','SLAVE LINK UPPER','263901/1426','PI 55-3569004-00','','PART REV PDM3',1,'BPP-529619 amed-1','','93906','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','OD REQUIRED 17.75 MM TO 18.25 MM MEASURED VALUE 17.58MM TO 17.65 MM','program altered |purpose of reducing the cycle time.','|change the program and run the old program.','|if in future any program will be change, before discussion with engineering team and all production department.','CA/PA found OK.','','2019-07-12','Ravi(M)','Madhu()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','05','no','Misc','Ravi(M)','no','','|immediately stop the machine and ensure the previous run parts.  ','E3456','qas|qas|','2019-07-16|2019-07-23|','2019-07-23',NULL,NULL,NULL,NULL,NULL,NULL),(11837,'35-404','Saab AB','BEAM 2','814254','D522 73392 200 01','','A',2,'OWED-LTA-001','','92137','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','THE TOTAL LENGTH UNDERSIZE BY 2MM.','the part was positioned with the stopper|The stopper is not the rigid one(temporary) where part  will be adjusted by using stopper and the part will be clamped in the vice.|Since the part is loaded in the vice where there is no space in the vice to fix the stopper rigidly.','|Discussed with engineering team and requested for the fixture with the permanent stopper.','|Discussed with engineering team and requested for the fixture with the permanent stopper.','The effectiveness will be checked for the next batch production.','','2019-07-13','pe_sez(a)','Vijay Kumar H.J,Upendra N ,Ravi Kumar G.B,Pradeep B.D,Nagaraju P K ,Manu ,Dhanush J.K,','','0000-00-00','Total height U/S Nominal 330.23 +/- 0.25\r\nAt measured 327.90   ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','1','no','a51nx-02','pe_sez(a)','no','','|The machine was stopped and all the parts were checked for the total length and found ok.','Z3456','qas_sez|qas_sez|','2019-07-16|2019-09-04|','2019-09-04',NULL,NULL,NULL,NULL,NULL,NULL),(11838,'56-048','GKN Aerospace Orangeburg','TIP CAP','292467B8','119A1370-604','NA','PSDL REV -',1,'A000047470','','93913','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Rib thickness under size by 0.3mm.','DUE TO THE VIBRATION IN THE PART.|THE PART WAS NOT CLAMPED PROPERLY.|THE DEPTH SCREW WAS NOT TIGHTENED PROPERLY SO PART GOT LIFTED. DURING MACHINING.','|ADVISED THE OPERATOR TO CROSS CHECK THE SCREW THREAD LENGTH AND VISUALLY CHECK THE THREAD FOR ANY WEAR OUT.','|ADVISED THE OPERATOR TO CROSS CHECK THE SCREW THREAD LENGTH AND VISUALLY CHECK THE THREAD FOR ANY WEAR OUT.\r<br/>AND CROSS CHECK THE PART WAS CLAMPED TO THE FIXTURE PROPERLY BEFORE RUNNING THE PROGRAM.','FURTHER PRODUCED PARTS OF THE SAME WORK ORDER WERE INSPECTED AND FOUND OK.','','2019-07-16','pe_sez(a)','Raghu B()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','01','no','Misc','pe_sez(a)','no','','|THE MACHINE WAS STOPPED AND INFORMED TO THE SUPERVISOR AND NC WAS RAISED.','Z3456','qas_sez|','2019-07-16|','2019-07-16',NULL,NULL,NULL,NULL,NULL,NULL),(11839,'51-130A','THE BOEING COMPANY','SPACER-POWER FEEDER CLAMP','526145-01','332W1912-103','NA','PSDL REV -',1,'BOEING 001W','','94727','','0000-00-00',NULL,'yes','yes','yes','','','','','','','RUNNING TIME PART DISLOCATED AND PROFILE DIG MARK FOUND.','','','','','','2019-07-16','pe_sez(a)','        HariPrasad ','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','','yes','','','','3','','','','','','','Z3456','pe|','2019-07-17|','0000-00-00',NULL,NULL,NULL,NULL,NULL,NULL),(11840,'18-690A','Magellan Aerospace Bournemouth','EYE END INBOARD ','CD706800/02729A','D575 41542 200','','D',1,'435247','','94377','','0000-00-00',NULL,'yes','yes','yes','','','','','','','hole pitch required 80mm measured value 86mm. ','work offset wrong|While taking offset for first part not added shank value (6mm)in work offset.|Forgot to move half of the tool radius in work offset for 12mm tool\r\n','|taken re offset and run the machine, the next part was found OK.','|message added in program, to take reference with shank half value.  ','TRAINING PROVIDED TO OPERATOR,AND CA/PA FOUND OK.','','2019-07-16','Subramanya L(Naik)','        Sundar D.K.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','7','','','','','','|immediately stoped the machine, cross checked the offset.','E3456','pe|qas|qas|','2019-07-17|2019-07-22|2019-07-31|','2019-07-31',NULL,NULL,NULL,NULL,NULL,NULL),(11841,'18-711A','Magellan Aerospace Wrexham','STUD ','1660208-3/Y5FY','D278 50006 206','','D',1,'167896','','94339','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','OD DIG MARK...','Part dig mark formed on the OD during the final finishing pass operation.|Due to low Lubricant the program sequence changed from continuous to single block for the safety purpose and the operator did not changed refilled the lubricant and continued the production as is condition due to which the tool formed a dig mark at the end of the OD.|Operator was not aware of refilling the lubricant and was not aware of the requirements of finishing cycle.','|Retrained the operator on the requirements to be followed during the finial finishing operation cycle.','|Informed the maintenance team to check and refill the lubricant regularly.','CA PA found ok.','','2019-07-17','Sandhesh D(S)','Veerabadraswamy(TB)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','03','no','Misc','GUNDEGOWDA(H.G.)','no','','|Immediately stopped the machine and refilled the lubricant to the required level and continued the production.','E3456','qas|','2019-09-30|','2019-09-30',NULL,NULL,NULL,NULL,NULL,NULL),(11842,'18-711A','Magellan Aerospace Wrexham','STUD ','1660208-3/Y5FY','D278 50006 206','','D',1,'167896','','94339','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','OD UNDER SIZE -0.01 MM   ','DURING JAWS BORING PROCESS 0.05MM  RUN OUT OCCURRED ON JAWS BORE ,THAT WAS NOT ENSURED. ','|DURING JAWS BORING PROCESS RUN OUT TO BE CHECK THEN PART PRODUCTION TO BE CARRY ON.','|WITH OUT RUN OUT ENSURING PROCESS PART WONT TO BE PRODUCE SO RUN OUT TO BE ENSURE ON LOG BOOK.','next parts produced found ok.','','2019-07-17','Sandhesh D(S)','Veerabadraswamy(TB)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','03','no','Misc','GUNDEGOWDA(H.G.)','no','','|JAWS BORING PROCESS WAS AGAIN CARRIED OUT .THEN ENSURED THE JAWS RUN OUT WAS 0.01MM.','E3456','pe|qas|','2019-07-17|2019-09-30|','2019-09-30',NULL,NULL,NULL,NULL,NULL,NULL),(11843,'35-623A','Saab AB','SHAFT 2','788619','D5227280820000','NA','PART ISSUE A',4,'OWED-LTA-004','','90656','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','OD UNDER SIZE 0.02 MM','machine LM guide way problem,','|change the machine and run the reaming parts ','|machine hand over to maintenance department. ','CA/PA found ok','','2019-07-18','Sandhesh D(S)','Arun Kumar(A M)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','05','no','Misc','GUNDEGOWDA(H.G.)','no','','|immediately stop the machine and check the all previous run part 3 parts not found OK.   ','E3456','qas|','2019-07-23|','2019-07-23',NULL,NULL,NULL,NULL,NULL,NULL),(11844,'51A-072','THE BOEING COMPANY','BEARING ASSY','','113T1204-1','','NIL',2,'BOEING 001S','','A27224','','0000-00-00',NULL,'no','yes','yes','yes','no','no','no','no','no','bearing dent mark','Dent Mark observed on the bearing after assembly.|Improper handling of bush during the assembly.|Chips available on the butting face during the bush assembly.','|Informed the operator to ensure the assembly area is completely FOD free before assembly','|Pre assembly activities (like machining) of the parts will be carried out in separate location.','Next parts produced verified and found ok.','','2019-07-18','Ramesh(D)','Yogananda(c)','','0000-00-00','bearing dent mark','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Assembly','','procesing','no','Misc','Ramesh(D)','no','M03733|MS14103-6','|Immediately stopped the assembly and checked the butting face and cleaned the chips and continued assembly.','E3456','qas|','2019-09-24|','2019-09-24',NULL,NULL,NULL,NULL,NULL,NULL),(11845,'56A-014A','GKN Aerospace Orangeburg','FAIRING SUPPORT ASSY - AF','','119A1521-602','','PSDL REV B',1,'LTA GKN ORANGEBURG W','','A27471','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Wall dig mark due to wrong loading of part','part was wrongly loaded by the operator|operator did not checked the completion of operation physically and went for next operation thinking that the current operation was completed by the previous operator.|due to the presence of multiple M00 code in the program the operator thought that the previous operation is completed and went for next setup.|single program contains two setups and operator has to reload the part after completion of first setup, for which multiple M00 was called in the program to guide the operator.','|Instructions are given to the operators for referring the given instructions every-time loading the part. ','|Program changed from two setup in one program to separate programs for two setups.','CA/PA Verified and found okay.','','2019-07-20','NataRaj.CV()','Chetan Kumar(M)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Assembly','','2','no','Misc','pe_sez(a)','no','90559|119A1521-604','|Checked the spindle run-out and continued the production, next part was inspected and found okay.','Z3456','qas_sez|qas_sez|','2019-07-22|2019-09-20|','2019-09-20',NULL,NULL,NULL,NULL,NULL,NULL),(11846,'51A-197','THE BOEING COMPANY','ROD ASSY','','6-58993-3300','','PSDL REV B',1,'BOEING 001AA','','K26796','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Thread Gauge 7/16-20UNF3 \"GO\" GAUGE  not entering in the part which in turn the female part is not getting assembled.','','','','','','2019-07-22','Dinakar K()','','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','no','yes','no','Assembly','','FI','no','','Dharani(Shankar)','no','','','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11847,'51A-197','THE BOEING COMPANY','ROD ASSY','','6-58993-3300','','PSDL REV B',2,'BOEING 001AA','','K26796','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','THE SUB ASSEMBLE PART HAS BEEN REJECTED DUE TO THREAD PROBLEM AND TO REPLACE THAT PART THE RIVET HAS TO BE REMOVED FROM THE PART.  ','','','','','','2019-07-22','qas_sez(a)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','no','yes','no','Assembly','','FI','no','Misc','Dharani(Shankar)','no','N01421|BACR15BB6D16C','','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11848,'51-128','THE BOEING COMPANY','SPACER','526145-01','332W1912-79','NA','PSDL REV -',1,'486998 MPP','','94402','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','THICKNESS UNDER SIZE BY 0.1 MM\r\nREQUIRED MIN THICKNESS 7.62MM\r\nMEASURED THICKNESS 7.51MM\r\n','1)During 12End mill running time the part dislocated.|2)Due to inadequate and insufficient clamping the part got dislocated during machining.|3)Part is held only in 5mm land on the part with a vise due to improper tightening the part got dislocated due to machine vibration.','|Ensured proper clamping of the part and ensured no tapper while clamping and continued the production.','|Instructed all the operators to ensure proper tightening of part and ensure proper butting with the help of feeler gauge before starting the cycle.','Next batch machining will be monitored for the effectiveness.','','2019-07-22','pe_sez(a)','pe_sez(a)','','0000-00-00','NC RAISED','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','yes','With Treatment','','IN PROCESS','no','Misc','pe_sez(a)','no','','|Stopped the machine and checked the Parts completed and other parts found ok and checked the offset and other machining parameters and found ok.','Z3456','qas_sez|','2019-07-25|','2019-07-25',NULL,NULL,NULL,NULL,NULL,NULL),(11849,'35A-671','Saab AB','SHAFT LEVER ASSY','','D5227346201800','','PART ISSUE D',1,'OWED-LTA-001','','A24059','','0000-00-00',NULL,'no','yes','yes','no','no','no','yes','no','no','Part damaged during assembly process','Bend in the part is found to be beyond the acceptable limits.|Improper loading of the part to the fixture.|As the operator is new to job, he did not cross checked the part while loading it to the fixture','|Training is given for the new operator and next batch of parts assembled found okay.','|Proper training will be conducted for new operators while assigning new job for them.','Next batch of parts are verified and found okay.','','2019-07-22','Ramesh(D)','Basavaraju(M)','','0000-00-00','part damaged','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Assembly','','01','no','Misc','Phaniraj(G)','no','86499|D5227346221800','|Assembly work is stopped, informed to the supervisor, an experienced operator is given for the assembly job.','E3456','ramesh|qas_sez|','2019-09-26|2019-09-27|','2019-09-27',NULL,NULL,NULL,NULL,NULL,NULL),(11850,'35A-408A','Saab AB','FRAME MID ASSY','','D522 73397 000 00','','PART ISSUE B',1,'1600214688','','A26201','','0000-00-00',NULL,'no','yes','yes','no','no','no','yes','no','no','Threads damaged','Helicoil is inserted improperly.|During the helicoil insertion process, helicoil was not aligned properly to the part but operator continued the process without noticing it.|Usage of damaged tool caused the improper alignment of the helicoil to the part.|At the beginning of operation operator did not noticed the damage in the tool.','|Operators are informed to verify the tool every-time before the beginning of assembly process.','|Operators are informed to verify the tool every-time before the beginning of assembly process.','Next batch parts assembled are verified and found okay.','','2019-07-22','Ramesh(D)','Nithin(S)','','0000-00-00','Thread damage ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Assembly','','01','no','Misc','Phaniraj(G)','no','88513|D522','|Immediately stopped the process and informed to the supervisor, the damaged tool is replaced with new one and continued the assembly process.','E3456','ramesh|qas_sez|','2019-09-26|2019-09-27|','2019-09-27',NULL,NULL,NULL,NULL,NULL,NULL),(11851,'18-210B','Magellan Aerospace Wrexham','BODY','M037950/27372','D321 40204 204','','D, ECN NR29999ST1KM15, NR29999ST2KF65, WQN DFB09775',3,'175174','','92977','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','OD UNDER SIZE BY 0.10 MM','insert wear out','|change the insert and run the parts all parts are found OK.','|monitoring the insert life and check the all parts OD in running time','training given to operators,and submit the training record.   ','','2019-07-22','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Raghavendra Rao(R)','no','','|immediately stop the machine and check the all previous completed parts were found the parts. ','E3456','qas|','2019-07-26|','2019-07-26',NULL,NULL,NULL,NULL,NULL,NULL),(11852,'47-151','GKN Aerospace Filton','LWR ANGLE ATTACHMENT','6583801 1','F57254364202','NA','PART ISSUE C',12,'GKN-GS-068 PHASE2- L','','91099','','0000-00-00',NULL,'yes','no','no','no','no','no','no','yes','no','profile increased by 3mm','','','','','','2019-07-22','qas_sez(a)','qas_sez(a)','G8D1150','2019-06-25','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','no','no','no','With Treatment','DN58406','cust end','yes','Misc','qas_sez(a)','yes','','','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11853,'47-151','GKN Aerospace Filton','LWR ANGLE ATTACHMENT','1013901 5','F57254364202','NA','PART ISSUE C',32,'GKN-GS-068 PHASE2- L','','91101','','0000-00-00',NULL,'yes','no','no','no','no','no','no','yes','no','profile increased by 3 mm','','','','','','2019-07-22','qas_sez(a)','qas_sez(a)','G8D1150','2019-06-25','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','no','no','no','With Treatment','DN58408','Cust end','yes','Misc','qas_sez(a)','yes','','','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11854,'47-151','GKN Aerospace Filton','LWR ANGLE ATTACHMENT','1013901 5','F57254364202','NA','PART ISSUE C',19,'GKN-GS-068 PHASE2- L','','91100','','0000-00-00',NULL,'yes','no','no','no','no','no','no','yes','no','profile increased by 3 mm','','','','','','2019-07-22','qas_sez(a)','qas_sez(a)','G8D1150','2019-06-25','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','no','no','no','With Treatment','DN57693','Cust end','yes','Misc','qas_sez(a)','yes','','','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11855,'56-070','GKN Aerospace Orangeburg','CARGO NET BEAM','717005B3','475Z3603-187','NA','NIL',1,'A000047052','','92606','','0000-00-00',NULL,'yes','yes','yes','','','','','','','32face mill 1mm offset entry wrong so part thickness minus side','','','','','','2019-07-22','pe_sez(a)','        Diwakar R.B.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','','yes','','','','7','','','','','','','Z3456','pe_sez|','2019-07-23|','0000-00-00',NULL,NULL,NULL,NULL,NULL,NULL),(11856,'53-049','Triumph Aerostructures','FILLER, A330/340','264005/2130','F57451527200A01','NA','PART ISSUE A, ECN PG49998ST1QR54',1,'LTA4 TRIUMPH 2018','','95389','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Thickness under size. ','RUNNING TIME PART OUT FROM CLAMPING,|IMPROPER CLAMPING METHOD. ','|CLAMP THE PART TIGHTLY,AND THE PARTS ALL ARE FOUND OK','|IN FUTURE IMPLEMENT THE WEG CLAMPING METHOD. ','CA/PA FOUND OK','','2019-07-23','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','01','no','Misc','Prashanth Kumar(M)','no','','|IMMEDIATELY STOP THE MACHINE AND ENSURE THE ALL PREVIOUS RUN PARTS ALL ARE FOUND OK. ','E3456','qas|','2019-07-26|','2019-07-26',NULL,NULL,NULL,NULL,NULL,NULL),(11857,'56-050A','GKN Aerospace Orangeburg','FAIRING SUPPORT - CTR, LW','567762','119A1531-604','NA','PSDL REV B',2,'LTA GKN ORANGEBURG W','','93921','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','position out of tolerance','Hole position out of tolerance after rework|mismatch found on the datum surface after machining|During re-engineering datum was not considered by the engineering department because of which proper stock was allocated.','|Reprogram done and the next parts found okay.|Reprogram done and the next parts found okay.|Reprogram done and the next parts found okay.|Reprogram done and the next parts found okay.','|Refresher Training will be given to all the engineers by Head engineering on parameters to be considered during programming.|Refresher Training will be given to all the engineers by Head engineering on parameters to be considered during programming.|Refresher Training will be given to all the engineers by Head engineering on parameters to be considered during programming.|Refresher Training will be given to all the engineers by Head engineering on parameters to be considered during programming.','Effectiveness will be measured on 16 August 2019','','2019-07-23','CAD(sez)','CAD(sez)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','','03','yes','Misc','CAD(sez)','no','','|Production is stooped and the same is informed to engineering department for correction of program.|Production is stooped and the same is informed to engineering department for correction of program.|Production is stooped and the same is informed to engineering department for correction of program.|Production is stooped and the same is informed to engineering department for correction of program.','Z3456','||||','2019-07-25|2019-07-25|2019-07-25|2019-07-25|','2019-07-25',NULL,NULL,NULL,NULL,NULL,NULL),(11858,'56-122','GKN Aerospace Orangeburg','CHANNEL FWD','528501','119A1212-602-4702','NA','NIL',1,'A000051447','','95299','','2019-07-20',NULL,'yes','no','yes','no','yes','no','no','no','no','hole position out by 1mm','','','','','','2019-07-23','pe_sez(a)','pe_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','no','yes','no','With Treatment','','03','no','Misc','pe_sez(a)','no','','','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11859,'18-210B','Magellan Aerospace Wrexham','BODY','M037950/27372','D321 40204 204','','D, ECN NR29999ST1KM15, NR29999ST2KF65, WQN DFB09775',1,'175174','','92975','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Bor over size (0.022mirone)','tool run out|tool run out not checked in setting time,','|in future any  setting time checked all tools run out, then run the parts,','|training providing to operators , and alarm message added in program  ','ca/pa found ok','','2019-07-23','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','5','no','Misc','Dhananjaya(N)','no','','|ensure the other dimensions of the parts ,all are found OK','E3456','qas|','2019-07-26|','2019-07-26',NULL,NULL,NULL,NULL,NULL,NULL),(11860,'35A-475A','Saab AB','FRAME ASSY','','D5227338400100','','B',1,'OWED-LTA-001','','A22207','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','PART BEND OBSERVED','','','','','','2019-07-23','Dharani(Shankar)','qas_sez(a)','','0000-00-00','NC CREATED','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','no','yes','no','Assembly','','FI','no','Misc','qas_sez(a)','no','','','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11861,'18-090A','Magellan Aerospace(Polska) Sp','BUSH','1670513-3/Z83Q','PID278 50164 200','','A',2,'104569','','93304','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','OD UNDER SIZE BY -0.2MM.','due to wear out the insert OD under size,','change the insert and run the parts.','ensure the insert life and change the insert for life period. ','training given to the operator ','','2019-07-23','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','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',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11862,'18-090A','Magellan Aerospace(Polska) Sp','BUSH','1670513-3/Z83Q','PID278 50164 200','','A',2,'104569','','93304','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','OD UNDER SIZE BY -0.2MM.','OD under size due to improper wear offset|Due to improper awareness the operator did not ensured the dimension of the part machined after insert change','after insert changing process supervisor will be again checked then run the part. ','training given to operator,','CA/PA FOUND OK','','2019-07-23','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Manufacture Only','','03','no','Misc','Ravi(M)','no','','Immediately stopped the machine and checked the previously running parts and separated the parts that were undersized. ','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11863,'35A-628A','Saab AB','LATCH FORK ASSY','','D5227349300400','','PART ISSUE C',49,'OWED-LTA-001','','A21869','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','yes','wrong bush assembled.','1) Bush interchanged by the operator during assembly.|2) The operator did not ensured the location of the bush he was supposed to install and since the outer diameter of both the bushes were same the bushes got interchanged.|3) No fool proofing method was available to avoid interchange of bushes.','|Re-assembled the bushes according to the drawing.','|1) Butting block will be marked with the profile and pin which avoids wrong bush entering into wrong flange.\r<br/>2) First off part will be given to quality for inspection and the other parts will be assembled after the final confirmation from assembly.','Next batches assembled verified and found ok.','C74294','2019-07-24','Dharani(Shankar)','Dharani(Shankar)','mail','2019-07-01','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER END','yes','Misc','qas_sez(a)','no','','|Checked all the parts in FG and found to be assembled as per the drawing.','Z3456','qas_sez|','2019-11-25|','2019-11-25','0000-00-00','0000-00-00','0000-00-00','','',''),(11864,'35A-464','Saab AB','FITTING ASSY','','D522 73408 001 00','','A',3,'OWED-LTA-001','','A22516','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Is condition:Bushing sticks out 1,80 - 1,85 mm.\r\nShould be: Between 1,55-1,68mm according to drawing D5227340800100 and AIPS 01-02-019','Flange projection out of tolerance from the specification limit.|More sealant was applied in the flange of the bush, due to which the bush did not assembled properly and the bush protrusion was not measured.|Bush protrusion requirement isn\'t called in the drawing because of which both the operator and inspector didn\'t ensured the projection before the shipment.','|Bushes are removed and reassembled to meet the requirements.','|APS revised and training was given to both inspector and operators.','\r\nEffectiveness will be measured by 23_SEP_2019\r\n','C75372','2019-07-24','Dharani(Shankar)','Dharani(Shankar)','GLB430832','2019-06-11','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER END','yes','Misc','qas_sez(a)','no','','|We have inspected our stock parts and are found okay. We also inspected the BOI parts they also and found within limits.','Z3456','qas_sez|','2019-08-13|','2019-08-13',NULL,NULL,NULL,NULL,NULL,NULL),(11865,'35A-464','Saab AB','FITTING ASSY','','D522 73408 001 00','','A',2,'OWED-LTA-001','','A23946','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Brief Description of Non Conformance:\r\nIs condition:Bushing sticks out 1,80 - 1,85 mm. Should be: Between 1,55-1,68mm according to drawing\r\nD5227340800100 and AIPS 01-02-019 ','Flange projection out of tolerance from the specification limit.|More sealant was applied in the flange of the bush, due to which the bush did not assembled properly and the bush protrusion was not measured.|Bush protrusion requirement isn\'t called in the drawing because of which both the operator and inspector didn\'t ensured the projection before the shipment.','|Bushes are removed and reassembled to meet the requirements.','|APS revised and training was given to both inspector and operators.','\r\nEffectiveness will be measured by 23_SEP_2019\r\n','C76977','2019-07-24','Dharani(Shankar)','Dharani(Shankar)','GLB430832','2019-07-11','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER END','yes','Misc','qas_sez(a)','no','','|We have inspected our stock parts and are found okay. We also inspected the BOI parts they also and found within limits.','Z3456','qas_sez|','2019-08-13|','2019-08-13',NULL,NULL,NULL,NULL,NULL,NULL),(11866,'35A-464','Saab AB','FITTING ASSY','','D522 73408 001 00','','A',2,'OWED-LTA-001','','A23944','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Brief Description of Non Conformance:\r\nIs condition:Bushing sticks out 1,80 - 1,85 mm. Should be: Between 1,55-1,68mm according to drawing\r\nD5227340800100 and AIPS 01-02-019 ','Flange projection out of tolerance from the specification limit.|More sealant was applied in the flange of the bush, due to which the bush did not assembled properly and the bush protrusion was not measured.|Bush protrusion requirement isn\'t called in the drawing because of which both the operator and inspector didn\'t ensured the projection before the shipment.','|Bushes are removed and reassembled to meet the requirements.','|APS revised and training was given to both inspector and operators.','Effectiveness will be measured by 23_SEP_2019','C76977','2019-07-24','Dharani(Shankar)','Dharani(Shankar)','GLB430832','2019-06-11','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER END','yes','Misc','qas_sez(a)','no','','|We have inspected our stock parts and are found okay. We also inspected the BOI parts they also and found within limits.','Z3456','qas_sez|','2019-08-13|','2019-08-13',NULL,NULL,NULL,NULL,NULL,NULL),(11867,'35A-464','Saab AB','FITTING ASSY','','D522 73408 001 00','','A',2,'OWED-LTA-001','','A24465','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Brief Description of Non Conformance:\r\nIs condition:Bushing sticks out 1,80 - 1,85 mm. Should be: Between 1,55-1,68mm according to drawing\r\nD5227340800100 and AIPS 01-02-019 ','Flange projection out of tolerance from the specification limit.|More sealant was applied in the flange of the bush, due to which the bush did not assembled properly and the bush protrusion was not measured.|Bush protrusion requirement isn\'t called in the drawing because of which both the operator and inspector didn\'t ensured the projection before the shipment.','|Bushes are removed and reassembled to meet the requirements.','|APS revised and training was given to both inspector and operators.','Effectiveness will be measured by 23_SEP_2019','C77857','2019-07-24','Dharani(Shankar)','Dharani(Shankar)','GLB430832','2019-06-11','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER END','yes','Misc','qas_sez(a)','no','','|We have inspected our stock parts and are found okay. We also inspected the BOI parts they also and found within limits.','Z3456','qas_sez|','2019-08-13|','2019-08-13',NULL,NULL,NULL,NULL,NULL,NULL),(11868,'35A-464','Saab AB','FITTING ASSY','','D522 73408 001 00','','A',5,'OWED-LTA-001','','A23945','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Brief Description of Non Conformance:\r\nIs condition:Bushing sticks out 1,80 - 1,85 mm. Should be: Between 1,55-1,68mm according to drawing\r\nD5227340800100 and AIPS 01-02-019 ','Flange projection out of tolerance from the specification limit.|More sealant was applied in the flange of the bush, due to which the bush did not assembled properly and the bush protrusion was not measured.|Bush protrusion requirement isn\'t called in the drawing because of which both the operator and inspector didn\'t ensured the projection before the shipment.','|Bushes are removed and reassembled to meet the requirements.','|\r<br/>APS revised and training was given to both inspector and operators.\r<br/>','\r\nEffectiveness will be measured by 23_SEP_2019\r\n','C76977','2019-07-24','Dharani(Shankar)','Dharani(Shankar)','GLB430832','2019-06-11','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER END','yes','Misc','qas_sez(a)','no','','|We have inspected our stock parts and are found okay. We also inspected the BOI parts they also and found within limits.','Z3456','qas_sez|','2019-08-13|','2019-08-13',NULL,NULL,NULL,NULL,NULL,NULL),(11869,'35A-464','Saab AB','FITTING ASSY','','D522 73408 001 00','','A',3,'OWED-LTA-001','','A24469','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Brief Description of Non Conformance:\r\nIs condition:Bushing sticks out 1,80 - 1,85 mm. Should be: Between 1,55-1,68mm according to drawing\r\nD5227340800100 and AIPS 01-02-019 ','Flange projection out of tolerance from the specification limit.|More sealant was applied in the flange of the bush, due to which the bush did not assembled properly and the bush protrusion was not measured.|Bush protrusion requirement isn\'t called in the drawing because of which both the operator and inspector didn\'t ensured the projection before the shipment.','|\r<br/>Bushes are removed and reassembled to meet the requirements.\r<br/>','|APS revised and training was given to both inspector and operators.','Effectiveness will be measured by 23_SEP_2019','C77858','2019-07-24','Dharani(Shankar)','Dharani(Shankar)','GLB430832','2019-07-11','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER END','yes','Misc','qas_sez(a)','no','','|We have inspected our stock parts and are found okay. We also inspected the BOI parts they also and found within limits.','Z3456','qas_sez|','2019-08-13|','2019-08-13',NULL,NULL,NULL,NULL,NULL,NULL),(11870,'35A-464','Saab AB','FITTING ASSY','','D522 73408 001 00','','A',5,'OWED-LTA-001','','A24000','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Brief Description of Non Conformance:\r\nIs condition:Bushing sticks out 1,80 - 1,85 mm. Should be: Between 1,55-1,68mm according to drawing\r\nD5227340800100 and AIPS 01-02-019 ','Flange projection out of tolerance from the specification limit.|More sealant was applied in the flange of the bush, due to which the bush did not assembled properly and the bush protrusion was not measured.|Bush protrusion requirement isn\'t called in the drawing because of which both the operator and inspector didn\'t ensured the projection before the shipment.','|Bushes are removed and reassembled to meet the requirements.','|APS revised and training was given to both inspector and operators.','Effectiveness will be measured by 23_SEP_2019','C76978','2019-07-24','Dharani(Shankar)','Dharani(Shankar)','GLB430832','2019-06-11','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER END','yes','Misc','qas_sez(a)','no','','|We have inspected our stock parts and are found okay. We also inspected the BOI parts they also and found within limits.','Z3456','qas_sez|','2019-08-13|','2019-08-13',NULL,NULL,NULL,NULL,NULL,NULL),(11871,'35A-464','Saab AB','FITTING ASSY','','D522 73408 001 00','','A',18,'OWED-LTA-001','','A22517','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Brief Description of Non Conformance:\r\nIs condition:Bushing sticks out 1,80 - 1,85 mm. Should be: Between 1,55-1,68mm according to drawing\r\nD5227340800100 and AIPS 01-02-019 ','Flange projection out of tolerance from the specification limit.|More sealant was applied in the flange of the bush, due to which the bush did not assembled properly and the bush protrusion was not measured.|Bush protrusion requirement isn\'t called in the drawing because of which both the operator and inspector didn\'t ensured the projection before the shipment.','|Bushes are removed and reassembled to meet the requirements.','|APS revised and training was given to both inspector and operators.','Effectiveness will be measured by 23_SEP_2019','C75372','2019-07-24','Dharani(Shankar)','Dharani(Shankar)','GLB430832','2019-06-11','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER END','yes','Misc','qas_sez(a)','no','','|We have inspected our stock parts and are found okay. We also inspected the BOI parts they also and found within limits.','Z3456','qas_sez|','2019-08-13|','2019-08-13',NULL,NULL,NULL,NULL,NULL,NULL),(11872,'35A-463','Saab AB','FITTING ASSY','','D522 73408 000 00','','A',2,'OWED-LTA-005','','A22502','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Brief Description of Non Conformance:\r\nIs condition:Bushing sticks out 1,80 - 1,85 mm. Should be: Between 1,55-1,68mm according to drawing\r\nD5227340800100 and AIPS 01-02-019 ','Flange projection out of tolerance from the specification limit.|More sealant was applied in the flange of the bush, due to which the bush did not assembled properly and the bush protrusion was not measured.|Bush protrusion requirement isn\'t called in the drawing because of which both the operator and inspector didn\'t ensured the projection before the shipment.','|Bushes are removed and reassembled to meet the requirements.','|APS revised and training was given to both inspector and operators.','Effectiveness will be measured by 23_SEP_2019','C75340','2019-07-24','Dharani(Shankar)','Dharani(Shankar)','GLB430832','2019-06-11','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER END','yes','Misc','qas_sez(a)','no','','|We have inspected our stock parts and are found okay. We also inspected the BOI parts they also and found within limits.','Z3456','qas_sez|','2019-08-13|','2019-08-13',NULL,NULL,NULL,NULL,NULL,NULL),(11873,'35A-463','Saab AB','FITTING ASSY','','D522 73408 000 00','','A',2,'OWED-LTA-005','','A22504','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Brief Description of Non Conformance:\r\nIs condition:Bushing sticks out 1,80 - 1,85 mm. Should be: Between 1,55-1,68mm according to drawing\r\nD5227340800100 and AIPS 01-02-019 ','Flange projection out of tolerance from the specification limit.|More sealant was applied in the flange of the bush, due to which the bush did not assembled properly and the bush protrusion was not measured.|Bush protrusion requirement isn\'t called in the drawing because of which both the operator and inspector didn\'t ensured the projection before the shipment.','|\r<br/>Bushes are removed and reassembled to meet the requirements.\r<br/>','|APS revised and training was given to both inspector and operators.','Effectiveness will be measured by 23_SEP_2019','C75341','2019-07-24','Dharani(Shankar)','Dharani(Shankar)','GLB430832','2019-06-11','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER END','yes','Misc','qas_sez(a)','no','','|We have inspected our stock parts and are found okay. We also inspected the BOI parts they also and found within limits.','Z3456','qas_sez|','2019-08-13|','2019-08-13',NULL,NULL,NULL,NULL,NULL,NULL),(11874,'35A-463','Saab AB','FITTING ASSY','','D522 73408 000 00','','A',3,'OWED-LTA-005','','A24041','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Brief Description of Non Conformance:\r\nIs condition:Bushing sticks out 1,80 - 1,85 mm. Should be: Between 1,55-1,68mm according to drawing\r\nD5227340800100 and AIPS 01-02-019 ','Flange projection out of tolerance from the specification limit.|More sealant was applied in the flange of the bush, due to which the bush did not assembled properly and the bush protrusion was not measured.|Bush protrusion requirement isn\'t called in the drawing because of which both the operator and inspector didn\'t ensured the projection before the shipment.','|\r<br/>Bushes are removed and reassembled to meet the requirements.\r<br/>','|APS revised and training was given to both inspector and operators.','Effectiveness will be measured by 23_SEP_2019','C77856','2019-07-24','Dharani(Shankar)','Dharani(Shankar)','GLB430832','2019-06-11','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER END','yes','Misc','qas_sez(a)','no','','|We have inspected our stock parts and are found okay. We also inspected the BOI parts they also and found within limits.','Z3456','qas_sez|','2019-08-13|','2019-08-13',NULL,NULL,NULL,NULL,NULL,NULL),(11875,'35A-463','Saab AB','FITTING ASSY','','D522 73408 000 00','','A',4,'OWED-LTA-005','','A22507','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Brief Description of Non Conformance:\r\nIs condition:Bushing sticks out 1,80 - 1,85 mm. Should be: Between 1,55-1,68mm according to drawing\r\nD5227340800100 and AIPS 01-02-019 ','Flange projection out of tolerance from the specification limit.|More sealant was applied in the flange of the bush, due to which the bush did not assembled properly and the bush protrusion was not measured.|Bush protrusion requirement isn\'t called in the drawing because of which both the operator and inspector didn\'t ensured the projection before the shipment.','|Bushes are removed and reassembled to meet the requirements.','|APS revised and training was given to both inspector and operators.','Effectiveness will be measured by 23_SEP_2019','C75341','2019-07-24','Dharani(Shankar)','Dharani(Shankar)','GLB430832','2019-06-11','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER END','yes','Misc','qas_sez(a)','no','','|We have inspected our stock parts and are found okay. We also inspected the BOI parts they also and found within limits.','Z3456','qas_sez|','2019-08-13|','2019-08-13',NULL,NULL,NULL,NULL,NULL,NULL),(11876,'35A-463','Saab AB','FITTING ASSY','','D522 73408 000 00','','A',2,'1600189916','','A25350','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Brief Description of Non Conformance:\r\nIs condition:Bushing sticks out 1,80 - 1,85 mm. Should be: Between 1,55-1,68mm according to drawing\r\nD5227340800100 and AIPS 01-02-019 ','Flange projection out of tolerance from the specification limit.|More sealant was applied in the flange of the bush, due to which the bush did not assembled properly and the bush protrusion was not measured.|Bush protrusion requirement isn\'t called in the drawing because of which both the operator and inspector didn\'t ensured the projection before the shipment.','|Bushes are removed and reassembled to meet the requirements.','|APS revised and training was given to both inspector and operators.','\r\nEffectiveness will be measured by 23_SEP_2019\r\n','C78898','2019-07-24','Dharani(Shankar)','Dharani(Shankar)','GLB430832','2019-06-11','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER END','yes','Misc','qas_sez(a)','no','','|We have inspected our stock parts and are found okay. We also inspected the BOI parts they also and found within limits.','Z3456','qas_sez|','2019-08-13|','2019-08-13',NULL,NULL,NULL,NULL,NULL,NULL),(11877,'35A-463','Saab AB','FITTING ASSY','','D522 73408 000 00','','A',3,'OWED-LTA-005','','A22608','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Brief Description of Non Conformance:\r\nIs condition:Bushing sticks out 1,80 - 1,85 mm. Should be: Between 1,55-1,68mm according to drawing\r\nD5227340800100 and AIPS 01-02-019 ','Flange projection out of tolerance from the specification limit.|More sealant was applied in the flange of the bush, due to which the bush did not assembled properly and the bush protrusion was not measured.|Bush protrusion requirement isn\'t called in the drawing because of which both the operator and inspector didn\'t ensured the projection before the shipment.','|Bushes are removed and reassembled to meet the requirements.','|APS revised and training was given to both inspector and operators.','Effectiveness will be measured by 23_SEP_2019','C76979','2019-07-24','Dharani(Shankar)','Dharani(Shankar)','GLB430832','2019-06-11','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER END','yes','Misc','qas_sez(a)','no','','|We have inspected our stock parts and are found okay. We also inspected the BOI parts they also and found within limits.','Z3456','qas_sez|','2019-08-13|','2019-08-13',NULL,NULL,NULL,NULL,NULL,NULL),(11878,'35A-463','Saab AB','FITTING ASSY','','D522 73408 000 00','','A',8,'OWED-LTA-005','','A23962','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Brief Description of Non Conformance:\r\nIs condition:Bushing sticks out 1,80 - 1,85 mm. Should be: Between 1,55-1,68mm according to drawing\r\nD5227340800100 and AIPS 01-02-019 ','Flange projection out of tolerance from the specification limit.|More sealant was applied in the flange of the bush, due to which the bush did not assembled properly and the bush protrusion was not measured.|Bush protrusion requirement isn\'t called in the drawing because of which both the operator and inspector didn\'t ensured the projection before the shipment.','|Bushes are removed and reassembled to meet the requirements.','|APS revised and training was given to both inspector and operators.','Effectiveness will be measured by 23_SEP_2019','C76979','2019-07-24','Dharani(Shankar)','Dharani(Shankar)','GLB430832','2019-06-11','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER END','yes','Misc','qas_sez(a)','no','','|We have inspected our stock parts and are found okay. We also inspected the BOI parts they also and found within limits.','Z3456','qas_sez|','2019-08-13|','2019-08-13',NULL,NULL,NULL,NULL,NULL,NULL),(11879,'35A-463','Saab AB','FITTING ASSY','','D522 73408 000 00','','A',11,'OWED-LTA-005','','A23961','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Brief Description of Non Conformance:\r\nIs condition:Bushing sticks out 1,80 - 1,85 mm. Should be: Between 1,55-1,68mm according to drawing\r\nD5227340800100 and AIPS 01-02-019 ','Flange projection out of tolerance from the specification limit.|More sealant was applied in the flange of the bush, due to which the bush did not assembled properly and the bush protrusion was not measured.|Bush protrusion requirement isn\'t called in the drawing because of which both the operator and inspector didn\'t ensured the projection before the shipment.','|\r<br/>Bushes are removed and reassembled to meet the requirements.\r<br/>','|APS revised and training was given to both inspector and operators.','Effectiveness will be measured by 23_SEP_2019','C76979','2019-07-24','Dharani(Shankar)','Dharani(Shankar)','GLB430832','2019-06-11','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER END','yes','Misc','qas_sez(a)','no','','|We have inspected our stock parts and are found okay. We also inspected the BOI parts they also and found within limits.','Z3456','qas_sez|','2019-08-13|','2019-08-13',NULL,NULL,NULL,NULL,NULL,NULL),(11880,'35A-463','Saab AB','FITTING ASSY','','D522 73408 000 00','','A',25,'OWED-LTA-005','','A24040','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Brief Description of Non Conformance:\r\nIs condition:Bushing sticks out 1,80 - 1,85 mm. Should be: Between 1,55-1,68mm according to drawing\r\nD5227340800100 and AIPS 01-02-019 ','Flange projection out of tolerance from the specification limit.|More sealant was applied in the flange of the bush, due to which the bush did not assembled properly and the bush protrusion was not measured.|\r\nBush protrusion requirement isn\'t called in the drawing because of which both the operator and inspector didn\'t ensured the projection before the shipment.\r\n','|Bushes are removed and reassembled to meet the requirements.','|APS revised and training was given to both inspector and operators.','Effectiveness will be measured by 23_SEP_2019','C77856','2019-07-24','Dharani(Shankar)','Dharani(Shankar)','GLB430832','2019-06-11','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER END','yes','Misc','qas_sez(a)','no','','|We have inspected our stock parts and are found okay. We also inspected the BOI parts they also and found within limits.','Z3456','qas_sez|','2019-08-13|','2019-08-13',NULL,NULL,NULL,NULL,NULL,NULL),(11881,'35-709','Saab AB','LEVER','D95254','D5227346621000','NA','PART ISSUE D',22,'OWED-LTA-004','','86409','','0000-00-00',NULL,'no','no','no','no','no','no','yes','yes','yes','Corrosion on Zn-plating.(Hole inside).','1) Due to improper pasivation inside the hole strain marks were formed inside the hole.|2) De greasing operation prior to the pasivation was not effective.|3) The immersion time of the part inside the de greasing tank was maintained to the minimum limit which was not sufficient for the completely removing the oil residues from the hole.','|Sent the parts back to supplier for stripping and reprocessing.','|Supplier has improved immersion time from minimum limit zone to the maximum limit zone to ensure complete removal of residues from the holes and other complicated surfaces.','Next batches processed were verified and found ok.','C76033','2019-07-24','qas_sez(a)','','mail','2019-07-24','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','DN52353','CUSTOMER END','yes','Misc','qas_sez(a)','no','','|Checked all the other parts in WIP and FG for similar issue and no similar defects identified.','Z3456','qas_sez|','2019-12-12|','2019-12-12','0000-00-00','0000-00-00','0000-00-00','','',''),(11882,'35-710','Saab AB','LEVER','D95254','D5227346621100','NA','PART ISSUE D',27,'OWED-LTA-004','','86411','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','yes','Corrosion on Zn-plating.(Hole inside)','1) Due to improper pasivation inside the hole strain marks were formed inside the hole.|2) De greasing operation prior to the pasivation was not effective.|3) The immersion time of the part inside the de greasing tank was maintained to the minimum limit which was not sufficient for the completely removing the oil residues from the hole.','|Sent the parts back to supplier for stripping and reprocessing.','|Supplier has improved immersion time from minimum limit zone to the maximum limit zone to ensure complete removal of residues from the holes and other complicated surfaces.','Next batches processed were verified and found ok.','C76034','2019-07-24','qas_sez(a)','','mail','2019-07-24','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','DN52352','CUSTOMER END','yes','Misc','qas_sez(a)','no','','|Checked all the other parts in WIP and FG for similar issue and no similar defects identified.','Z3456','qas_sez|','2019-12-12|','2019-12-12','0000-00-00','0000-00-00','0000-00-00','','',''),(11883,'35-502A','Saab AB','SHAFT CAM','B90488','D5227351220000','NA','PART ISSUE B',8,'OWED-LTA-003','','84131','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','yes','Zn-Ni Plating chip off. ','Passivation layer chipped off from the part during transit.|The packing material used for protecting the part during transit was not sufficient.|Single layer of protection was used because of which the layer got chipped off due to part to part contact during transit.','|Instructed the packing team to provide sufficient packing material to protect the parts from damages during transit.','|Double layer of protection is used to avoid damages of the parts during transit.','Next batches shipped verified and found ok.','C74568','2019-07-24','qas_sez(a)','','mail','2019-07-24','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','DN51969','CUSTOMER END','yes','Misc','qas_sez(a)','no','','|Checked all the parts in FG and ensure no similar parts are available.','Z3456','qas_sez|','2019-11-28|','2019-11-28','0000-00-00','0000-00-00','0000-00-00','','',''),(11884,'51-152A','THE BOEING COMPANY','PIVOT STRAP','8-10-07217-2/24122','313Z6310-501','NA','NIL',1,'BOEING AC001','','91409','','0000-00-00',NULL,'yes','no','no','no','no','no','no','yes','yes','Warpage and excessive gap exists common to the\r\n313Z6310-501 HS MSB box that will not allow fit up\r\non next assembly.','Profile of the part measures out of tolerance when measured by customer.|Warpage occurred on the part.|Due to  improper storage and handling of the parts during transit the warpage has occurred.','|instructed the logistics and packing team to handle and store the parts with care.','|100% inspection of parts are carried out untill packing and dispatch to ensure no parts with similar defects are shipped to customer.','Next batches shipped are verified and found ok.','C80106','2019-07-24','qas_sez(a)','','N6400031511','2019-07-19','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','DN59330','CUSTOMER END','no','Misc','qas_sez(a)','no','','|Checked all the parts in our FG for warpage using the female fixture and found ok.','Z3456','qas_sez|','2019-11-28|','2019-11-28','0000-00-00','0000-00-00','0000-00-00','','',''),(11885,'18-213A','Magellan Aerospace Wrexham','END CAP ','M055840/27373','D321 40209 200','','A, ECN NR29998ST1JA76',4,'190631','','93393','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','OD UNDER SIZE -0.1MM.','refer NC NO 11892|refer NC NO 11892|refer NC NO 11892|refer NC NO 11892','|refer NC NO 11892','|refer NC NO 11892','refer NC NO 11892','','2019-07-24','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','01','no','Misc','Ravi(M)','no','','|refer NC NO 11892','E3456','qas|','2019-07-26|','2019-07-26',NULL,NULL,NULL,NULL,NULL,NULL),(11886,'47-184','GKN Aerospace Filton','TEE T/E RIB 5B OTBD','2361201-2','F57551281203','NA','PART ISSUE D',1,'GKN-GS-068 PHASE2- L','','94674','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','DUE TO TOOL DIG MARK, PROFILE NOT  ACHIEVED.(UNDER SIZE 0.2MM)','','','','','','2019-07-24','pe_sez(a)','Chetan Kumar M,Anoop B Divekar,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','no','yes','no','With Treatment','','FI','no','Slim3n-4AHS-2','Mahesh(N)','no','','','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11887,'35A-352A','Saab AB','Lift Actuator Support Fit','','423Z1223-2-50','','---',2,'1600218100','','A13907','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Bore over size','','','','','','2019-07-25','qas_sez(a)','qas_sez(a)','','0000-00-00','NC craeted','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','no','yes','no','Assembly','','FI','no','Misc','qas_sez(a)','no','M00978|BACB28AT14B059Z','','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11888,'56-005','GKN Aerospace Orangeburg','SPLICE PLATE FWD UPR','8-18-05035-2/24299','119A1213-603','NA','PSDL REV -',1,'LTA GKN 737 Winglet','','93456','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dig mark observed on face. ','Running time tool was blunt|Due to the insufficient coolant contact to the part|Operator was not ensured the direction of coolant nozzle','|Operator was instructed to ensure the direction of nozzles while starting the cycle. Also instructed to ensure the same for all tools','|All the Operators are instructed to ensure the direction of nozzles while starting the cycle for all tools.','Next work order parts found okay.','','2019-07-25','pe_sez(a)','Pradeep(B.D)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','pe_sez(a)','no','','|Coolant nozzle was adjusted to right direction and the next part found okay.\r\n','Z3456','qas_sez|','2019-07-25|','2019-07-25',NULL,NULL,NULL,NULL,NULL,NULL),(11889,'28-027','Magellan Aerospace New York  Inc.','GUIDE ','MA20143791','141T6274-4','','PL_A + ADCN # 3 & 4, DL_N/C',1,'A000159399','','94493','','0000-00-00',NULL,'yes','yes','yes','','','','','','','OD UNDER SIZE BY -0.02MM','OVER HANGING PART |OD VARY TO ONE PART TO OTHER PART.|IN REWORK TIME PART REJECTED,','|CHANGE THE FINISHING INSERTS,AND RUN THE PARTS.','|CHANGE THE FINISHING INSERT VNMG TO CBN (SPECIAL INSERT),','IN FUTURE THIS PARTS WILL BE RUN WITH CBN INSERT.','','2019-07-25','Ravi(M)','        Ningaraj A N','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','9','','','','','','|STOP THE MACHINE AND ENSURE THE ALL PREVIOUS RUN PARTS ALL ARE FOUND OK.  ','E3456','pe|qas|','2019-07-25|2019-07-26|','2019-07-26',NULL,NULL,NULL,NULL,NULL,NULL),(11890,'35-531A','Saab AB','SHAFT LATCH','B78267 NM2Z','D5227349020200','NA','PART ISSUE C',9,'OWED-LTA-002','','88309','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no','SCRATCH MARKS OBSERVED ON THE PARTS ','1) Due to improper handling of parts scratch marks formed on the parts.|2) Protection of part during storage and handling was not adequate.|3) Protective sleeves were not available while storing and handling.','|Protective sleeves were used for all the parts in process and for the parts in transit between departments.','|Alerts displayed in all the area to use protective sleeves to avoid damages on the parts during transit.','Next batches produces and parts handling in shop floor verified and found ok.','','2019-07-25','pe_sez(a)','','','0000-00-00','SCRATCH MARKS OBSERVED ON THE PARTS ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','With Treatment','DN58366','FI','yes','a51nx-06','qas_sez(a)','no','','|Checked the similar parts in transit and found ok.','Z3456','qas_sez|','2019-12-04|','2019-12-04','0000-00-00','0000-00-00','0000-00-00','','',''),(11891,'35-720','Saab AB','ROD BODY','6899','D5227333720200','NA','PART ISSUE B',1,'OWED-LTA-005','','93287','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1. OPERATION MISSING,HOLES NOT DRILLED \r\n2. PITCH MEASURED OVER SIZE MAX 10.1MM MEASURED 10.16','when drilling time, the cutting edge of the drill is broken in middle of the part.|The operator not observed the incomplete drilling operations.\r\nafter removed the from fixture only, able to observe either drilling operation completed or not. |Part total length tolerance is */- 0.2mm. But drilling point distance tolerance is */-0.1mm|when the drill operation, as per MPS. the drilling operation CNC programs drill coordinates from one face only.|If part total length with in 0.1mm tolerance, hole position distance is with in 0.1mm. If part total length above 0.1mm tolerance, hole position distance is apart from drawing dimensions.','|1.The Drill cutting edge will be monitor with in a periodically time \r<br/>2.The part total length operations carried out along with drilling operations. the Part total length maintained with in the 0.1mm tolerance. ','|1.Each 100ns the Drill will change. same size new drill will be replace\r<br/>2.The part total length operations will be carried out  along with drilling operations to maintain the all dimensions with in tolerance.','CA PA ok','','2019-07-26','pe_sez(a)','Vijay Kumar H.J,Manu ,Dinakar K ,Chetan N,','','0000-00-00','1. OPERATION MISSING,HOLES NOT DRILLED \r\n2. PITCH MEASURED OVER SIZE MAX 10.1MM MEASURED 10.16','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','a51nx-05','qas_sez(a)','no','','|Production Stopped. finished Parts checked.All parts Found ok.','Z3456','pe_sez|qas_sez|','2019-11-16|2019-11-16|','2019-11-16',NULL,NULL,NULL,NULL,NULL,NULL),(11892,'18-213A','Magellan Aerospace Wrexham','END CAP ','M055840/27373','D321 40209 200','','A, ECN NR29998ST1JA76',4,'190631','','93393','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','OD UNDER SIZE -0.1MM.','running time parts not checked|insert wear out,','change the insert and run the machine ','check the all machined parts and ensure the insert life.','training providing to the operators and submit the training record  ','','2019-07-26','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','01','no','Misc','Ravi(M)','no','','immediately stop the machine and check the all previous run parts were 3 parts parts are not found OK ','E3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11893,'56A-014A','GKN Aerospace Orangeburg','FAIRING SUPPORT ASSY - AF','','119A1521-602','','PSDL REV B',1,'LTA GKN ORANGEBURG W','','A28082','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Hole oversize.','Hole oversize during countersink operation.|1) Countersink tool setting was note done properly.|2) Part was not properly held during the countersink operation.','|Setting of countersink part was redone and help of senior operator is also taken to ensure proper holding part  during the countersink operation.','|Development of Fixture for holding the part during countersink operation is planned.','CA PA found ok.','','2019-07-27','Ramesh(D)','Varadaraju(D)','','0000-00-00','CSK hole over size','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Assembly','','procesing','no','Misc','Ramesh(D)','no','93682|119A1521-604','|Setting of countersink part was redone and help of senior operator is also taken to ensure proper holding part  during the countersink operation.','E3456','ramesh|qas|','2019-09-26|2019-09-30|','2019-09-30',NULL,NULL,NULL,NULL,NULL,NULL),(11894,'18-209B','Magellan Aerospace Wrexham','BODY','M037880/27053','D321 40204 202','','D, ECN NR29999ST1KM15, NR29999ST2KF65, WQN DFB09775',2,'175173','','92902','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','OD UNDER SIZE O.1 MM AND DIG MARK ON OD','running time part rotate.|improper jaws boring.  ','|re boring the jaws and run the machine, all parts are found OK.','|provide the jaws boring training to operator.','ca/pa found ok','','2019-07-27','Dinakar(K)','Dinakar(K)','','0000-00-00','OD under size (-o.1)','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','DN60575','03','no','Misc','Sathish(G)','no','','|stop the machine and ensure previous run parts,','E3456','qas|','2019-07-27|','2019-07-27',NULL,NULL,NULL,NULL,NULL,NULL),(11895,'18-779A','Magellan Aerospace Wrexham','BRACKET AFT M/C','1671472-2/Y9QY','F57551860201','NA','PART ISSUE A',1,'RP174264','','94666','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','BORE DIA 10 MICRON OVER SIZED.','while running time reamer edge chip out','|change the new reamer and run the part.','|implement the boring bar method,for next batch','ca /pa found OK','','2019-07-29','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Prashanth Kumar(M)','no','','|stop the machine and ensure the all previous run parts all are found ok','E3456','qas|','2019-08-06|','2019-08-06',NULL,NULL,NULL,NULL,NULL,NULL),(11896,'35-602A','Saab AB','SHAFT 1','C91450 W8FG','D5227280720000','NA','PART ISSUE B',2,'OWED-LTA-004','','92011','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','While proving drill was broken inside the part','L/D ratio was not calculated while reprogramming the part|Part was reprogrammed to avoid the mismatch inside the hole|In the previous program drilling operation was done in two parts, i.e. half of the hole was done from onside  and the remaining half was done in next setup from the other end of the part.','|Program and tooling parameters are changed and next parts are found okay','|Program and tooling parameters are changed and next parts are found okay','Remaining parts in the same work order are found okay.','','2019-07-29','Narasimha Murthy (K G)','Maruthi()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','05','no','Misc','Narasimha Murthy (K G)','no','','|next part found okay','Z3456','qas_sez|','2019-07-31|','2019-07-31',NULL,NULL,NULL,NULL,NULL,NULL),(11897,'18-210B','Magellan Aerospace Wrexham','BODY','M037950/27372','D321 40204 204','','D, ECN NR29999ST1KM15, NR29999ST2KF65, WQN DFB09775',4,'175174','','92976','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','BORE DIAMETER WAS 0.1MM OVERZIZED.','1) Bore diameter measured oversize to the drawing requirement.|2) Offset for the boring bar taken by the operator was not correct.|3) Operator took the offset when the tool was not completely clamped.|4) lack of awareness of the operator.','|Informed all the operators to check and take offset only after the insert is completely clamped.','|Re-training given to the operator regarding the offset taking and cross checking the offset.','CA PA found ok.','','2019-07-31','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','01','no','Misc','Dinakar(K)','no','','|Immediately stopped the machine and retook the offset and continued the production.','E3456','qas|','2019-09-09|','2019-09-09',NULL,NULL,NULL,NULL,NULL,NULL),(11898,'18-210B','Magellan Aerospace Wrexham','BODY','M022730/27066','D321 40204 204','','D, ECN NR29999ST1KM15, NR29999ST2KF65, WQN DFB09775',8,'RP166211','','92525','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','OUTER DIAMETER RUN OUT PROBLEM.','1) Run out measured out of tolerance.|2) Jaws boring not done properly by the operator.|3) Operator used worn out insert to bore the Jaws.','|Informed all the operators to ensure run out of the jaws before starting the production.','|Instruction given to all the operators not to use blunt inserts during the boring operation.','CA PA found ok.','','2019-07-31','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Dinakar(K)','no','','|Immediately stopped the machine and checked the bore runout and re bored the jaws.','E3456','qas|','2019-09-09|','2019-09-09',NULL,NULL,NULL,NULL,NULL,NULL),(11899,'35-671','Saab AB','SHAFT LEVER ','533387C','D5227346221800','NA','PART ISSUE D',2,'OWED-LTA-001','','93153','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','BORE 9.98H8 NO GO ANSWER','while running insert wear out ','|for next batch check the insert tip then run the part.','|ensure insert life in next batch after ensuring the insert life change the new insert then run the part.','ca/pa found OK.','','2019-08-02','Ravi(M)','Yogesha K,Venkatesh S,Ugraiah ,Sudhakar C.M,Shanmukha R,Ningaraj A N,Manohara M,Hemaprakash K V,Hanumantha Rao,Govindraju NR,Eranna K,DILIP G C ,Basavaraja S. Jr.,Ashoka R,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','QT100S-1','Yashawantha(NH)','no','','|check the all parts in this work order all are found OK','E3456','qas|','2019-08-06|','2019-08-06',NULL,NULL,NULL,NULL,NULL,NULL),(11900,'35-481B','Saab AB','LOCK LEVER','YQE3','D5227349820100','NA','PART ISSUE C',1,'OWED-LTA-003','','94214','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','HOLE DIA 6.38H7 NO GO ANSWER','while machine ruining time chip blocked in drill. ','|remove the chips and run the parts all are found OK','|from next batch remove the chips in all parts,check the go and no go in machine only then remove the part, ','ca pa found ok','','2019-08-02','Dhananjaya(N)','Yogesha K,Venkatesh R,Veerabadraswamy TB,Sundar D.K.,Sathish G,Naveen Kumar KM,Narasimhamurthy C,GUNDEGOWDA H.G.,Dileep Kumar,Devaraj K.C.,Arun Kumar R,','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','VM2-3','Yashawantha(NH)','no','','|ensure the all parts, all are found OK.','E3456','qas|','2019-08-06|','2019-08-06',NULL,NULL,NULL,NULL,NULL,NULL),(11901,'18-213A','Magellan Aerospace Wrexham','END CAP ','21403','D321 40209 200','','A, ECN NR29998ST1JA76',3,'RP166211','','76514','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1. Step over occurred on the face\r\n2. Thread minor diameter not achieved and operation not fully completed\r\n3.Improper threading formation occurred','bore over size|chips accumulation during operation|improper flow of coolant','|coolant flow was corrected by maintenance team and next part found ok ','|coolant flow will be verified once in 15 parts and plug gauge will be implemented  for bore size verification','','','2019-08-05','Dinakar(K)','S. Shiva Kumar,Ravi M,Ravi K,Punith G S,Karibasappa G,','','0000-00-00','NC CREATION','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','ST20','Narasimha Murthy(R)','no','','|immediately stopped the machine and informed maintenance team to check the coolant flow','E3456','qas|qas|','2019-08-26|2019-08-26|','2019-08-26',NULL,NULL,NULL,NULL,NULL,NULL),(11902,'51A-052','THE BOEING COMPANY','BRACKET ASSY','','149A7371-626','','PSDL REV A',1,'BOEING 001G','','A28097','','0000-00-00',NULL,'no','no','no','no','no','yes','yes','yes','no','BMS10-11 (TYPE 1) GRADE-D PAINT AS PER BAC 5736 NOT DONE PROPERLY,','.','|.','|.','.','','2019-08-05','qas_sez(a)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','FI','yes','Misc','Dharani(Shankar)','no','90109|149A7371-9628','|.','Z3456','qas_sez|qas_sez|','2019-08-06|2019-08-06|','2019-08-06',NULL,NULL,NULL,NULL,NULL,NULL),(11903,'51A-052','THE BOEING COMPANY','BRACKET ASSY','','149A7371-626','','PSDL REV A',1,'BOEING 001G','','A28097','','0000-00-00',NULL,'no','no','no','no','no','yes','yes','yes','no','BMS10-11 (TYPE-1) GRADE-D PAINT AS PER BAC5736 NOT DONE PROPERLY,','','','','','','2019-08-06','qas_sez(a)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','no','no','no','Assembly','','FI','yes','Misc','Dharani(Shankar)','no','','','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11904,'18-411A','Magellan Aerospace Wrexham','PLUNGER','CD706804/07777A','D321 40205 200','','H01',1,'190631','','93339','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Drill broken in place of 0.374-24UNF-3B thread area.','1. During turning operation drill broken occurred |2. During operation high heat produced due to that drill broken|3. Due to insufficient amount of coolant flow heat produced','|Coolant level and flow to be monitor in daily','|Coolant check list to be maintain','CA PA found ok.','','2019-08-07','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','05','no','Misc','Ravi(M)','no','','|Coolant level corrected and coolant flow checked','E3456','qas_sez|qas|','2019-08-23|2019-09-09|','2019-09-09',NULL,NULL,NULL,NULL,NULL,NULL),(11905,'35A-545','Saab AB','BEAM ASSY','','D522 73335 000 00','','PART ISSUE A',2,'OWED-LTA-001','','A25844','','0000-00-00',NULL,'no','no','no','no','no','yes','yes','yes','no','- P108 ELECTROLYTIC ZINC-NICKEL PLATING, TYPE I OR TYPE II (CHROME III TREATMENT) : AIPS 02-04-006\r\nIN ACCORDANCE WITH CROSS-REFERENCE TN A007 10050 GOT DAMAGED.','.','|.','|.','.','','2019-08-07','qas_sez(a)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Assembly','','FI','no','Misc','Dharani(Shankar)','no','87767|D5227347420200','|.','Z3456','qas_sez|','2019-08-08|','2019-08-08',NULL,NULL,NULL,NULL,NULL,NULL),(11906,'18-213A','Magellan Aerospace Wrexham','END CAP ','M055840/27373','D321 40209 200','','A, ECN NR29998ST1JA76',1,'190631','','93398','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Thread 1.6-12UNS-3B NOGO answering','tool wear correction not given properly.|wear correction was given in the positive side with out calculating the major dia of the thread.|operator was not aware of the threading operation','|supervisor corrected wear offset and next part found ok','|wear offset and tool offset need to be verified by supervisor before starting the production ','','','2019-08-07','Dinakar(K)','Dinakar(K)','','0000-00-00','NC CREATION','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','FI','no','Misc','Narasimha Murthy(R)','no','','|immediately stop the machine and informed the supervisor and check the wear offset ','E3456','qas|qas|','2019-08-26|2019-08-26|','2019-08-26',NULL,NULL,NULL,NULL,NULL,NULL),(11907,'35A-545','Saab AB','BEAM ASSY','','D522 73335 000 00','','PART ISSUE A',1,'OWED-LTA-001','','A28401','','0000-00-00',NULL,'no','no','no','no','no','yes','yes','yes','no','- P108 ELECTROLYTIC ZINC-NICKEL PLATING, TYPE I OR TYPE II (CHROME III TREATMENT) : AIPS 02-04-006\r\nIN ACCORDANCE WITH CROSS-REFERENCE TN A007 10050 GOT DAMAGED.','.','|.','|.','.','','2019-08-07','qas_sez(a)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','Assembly','','FI','no','Misc','Dharani(Shankar)','no','','|.','Z3456','qas_sez|','2019-08-08|','2019-08-08',NULL,NULL,NULL,NULL,NULL,NULL),(11908,'35-650A','Saab AB','SHAFT','C91450 W8FG','D5227346820200','NA','PART ISSUE C',1,'PA1687 LTA-2','','95959','','0000-00-00',NULL,'yes','yes','yes','','','','','','','OD THREAD NOGO ANSWER.... ','1.tool wear correction not given properly.		|wear correction was given in the positive side with out calculating the major dia of the thread.|operator was not aware of the threading operation	','|supervisor corrected wear offset and next part found ok ','|wear offset and tool offset need to be verified by supervisor before starting the production 		\r<br/>\r<br/>Informed all the operators to check the tightness of the insert before continuing the production. 		','CAPA FOUND OK','','2019-08-07','Ravi(M)','        Ashoka R','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','7','','','','','','|immediately stop the machine and informed the supervisor and check the wear offset 				\r\n','E3456','pe|pe|qas|qas|','2019-08-12|2019-09-18|2019-09-19|2019-09-19|','2019-09-19',NULL,NULL,NULL,NULL,NULL,NULL),(11909,'35-650A','Saab AB','SHAFT','C91450 W8FG','D5227346820200','NA','PART ISSUE C',1,'PA1687 LTA-2','','95959','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Thread No-Go Gauge answered on outer dia . ','Tool wear offset correction.|Thread GO GAUGE Not answered . ','|Correct the tool wear offset then the machine.','|wear offset will always given on positive side and verify every time.  ','','','2019-08-07','Ravi(M)','Ashoka(R)','','0000-00-00','OD THREAD NOGO ANSWERED......','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','05','no','Misc','Ashoka(R)','no','','|Tool wear offset given on positive side next part found ok.','E3456','qas|','2019-08-12|','2019-08-12',NULL,NULL,NULL,NULL,NULL,NULL),(11910,'35A-599','Saab AB','BEAM ASSY','','D5227338100400','','PART ISSUE C',36,'OWED-LTA-001','','A24326','','0000-00-00',NULL,'no','no','no','no','no','no','yes','yes','yes','Ink jet part marking and lacquering  OPERATION added by the customer for assembly part.','Parts shipped to customer without ink jet marking.|Part was identified only with bag and lable.|part marking location for the ink jet marking was not defined in the drawing.','|Carried out ink jet marking on the part as per customer mail confirmation.','|Delta FAIR will be submitted for the ink jet marking of part once the drawing is revised by Customer.','Next batches shipped are marked with Ink jet marking as per mail instructions.','C77341','2019-08-08','Dharani(Shankar)','','GLB428429','2019-05-16','Ink jet part marking and lacquering  OPERATION added by the customer for assembly part.','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','Cutomer End','yes','','Dharani(Shankar)','no','','|Requested the customer to provide revised drawing to carry out the ink jet marking.','Z3456','qas_sez|','2019-11-28|','2019-11-28','0000-00-00','0000-00-00','0000-00-00','','',''),(11911,'35A-599','Saab AB','BEAM ASSY','','D5227338100400','','PART ISSUE C',10,'OWED-LTA-001','','A24327','','0000-00-00',NULL,'no','no','no','no','no','no','yes','yes','yes','Ink jet part marking and lacquering  OPERATION added by the customer for assembly part.','Parts shipped to customer without ink jet marking.|Part was identified only with bag and lable.|part marking location for the ink jet marking was not defined in the drawing.','|Carried out ink jet marking on the part as per customer mail confirmation.','|Delta FAIR will be submitted for the ink jet marking of part once the drawing is revised by Customer.','Next batches shipped are marked with Ink jet marking as per mail instructions.','C77341','2019-08-08','Dharani(Shankar)','','GLB428429','2019-05-16','Ink jet part marking and lacquering  OPERATION added by the customer for assembly part.','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER END','yes','Misc','Dharani(Shankar)','no','','|Requested the customer to provide revised drawing to carry out the ink jet marking.','Z3456','qas_sez|','2019-11-28|','2019-11-28','0000-00-00','0000-00-00','0000-00-00','','',''),(11912,'35A-599','Saab AB','BEAM ASSY','','D5227338100400','','PART ISSUE C',11,'OWED-LTA-001','','A24328','','0000-00-00',NULL,'no','no','no','no','no','no','yes','yes','yes','Ink jet part marking and lacquering  OPERATION added by the customer for assembly part.','Parts shipped to customer without ink jet marking.|Part was identified only with bag and lable.|Part marking location for the ink jet marking was not defined in the drawing.','|Carried out ink jet marking on the part as per customer mail confirmation.','|Delta FAIR will be submitted for the ink jet marking of part once the drawing is revised by Customer.','Next batches shipped are marked with Ink jet marking as per mail instructions.','C77341','2019-08-08','Dharani(Shankar)','','GLB428429','2019-05-16','Ink jet part marking and lacquering  OPERATION added by the customer for assembly part.','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','no','Assembly','','CUSTOMER END','yes','Misc','Dharani(Shankar)','no','','|Requested the customer to provide revised drawing to carry out the ink jet marking.','Z3456','qas_sez|','2019-11-28|','2019-11-28','0000-00-00','0000-00-00','0000-00-00','','',''),(11913,'35A-545','Saab AB','BEAM ASSY','','D522 73335 000 00','','PART ISSUE A',1,'OWED-LTA-001','','A28401','','0000-00-00',NULL,'no','no','no','no','no','yes','yes','yes','no','P 108 ELECTROLYTIC ZINC NICKEL PLATING TYPE 1 OR 2 AS PER (AIPS 02-04-006) GOT DAMAGED. ','','','','','','2019-08-08','qas_sez(a)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','no','yes','no','Assembly','','FI','no','Misc','Dharani(Shankar)','no','92324|D5227347420200','','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11914,'35A-545','Saab AB','BEAM ASSY','','D522 73335 000 00','','PART ISSUE A',2,'OWED-LTA-001','','A25844','','0000-00-00',NULL,'no','no','no','no','no','yes','yes','yes','no','P 108 ELECTROLYTIC ZINC NICKEL PLATING TYPE 1 OR 2 AS PER (AIPS 02-04-006) GOT DAMAGED. ','','','','','','2019-08-08','qas_sez(a)','qas_sez(a)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Open','no','yes','no','Assembly','','FI','no','Misc','Dharani(Shankar)','no','87767|D5227347420200','','Z3456',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11915,'35-443C','Saab AB','HINGE','YNRQ','D5227338820000','NA','B',2,'OWED-LTA-002','','93158','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','dig mark formed on the part due to wrong tool offset value entry','Dig mark found formed on the part|running time tool holder touched on the part|Tool was weared out, so while changing the tool, offset value entered by the operator is wrong.','|Spindle runout checked, Tool offset value checked by the zolar machine and correct value of of sett is entered and next part found okay','|a 40 mm checking master to cross check the tool of sett value physically by measuring the master is introduced.','effectiveness is measured in next batch','','2019-08-09','pe_sez(a)','Ananda(M)','','0000-00-00','Wrong tool offset so part thickness under size','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','03','no','Misc','Nagaraju P K()','no','','|Machine is stopped and informed to machine maintenance team and supervisor.','Z3456','qas_sez|','2019-08-14|','2019-08-14',NULL,NULL,NULL,NULL,NULL,NULL),(11916,'35-290','Saab AB','BEAM FITTING','599492','424Z1142-2','','--B',1,'1600177789','','92930','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Center rib dig. ','Tool offset wrong.|Tool composition wrong value entered |Training effeteness not validated.','|Tool composition value verified , next part found OK.','|Training conducted.','','','2019-08-09','Dinesh kulal()','Dinesh kulal()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','yes','no','With Treatment','','2ND','no','Misc','prodn_aero(prodn)','no','','|Suddenly to stop the machine.','A3456','qas|','2019-08-12|','2019-08-12',NULL,NULL,NULL,NULL,NULL,NULL),(11917,'18-009A','Magellan Aerospace Wrexham','Plate Cover','755666','D572 52519 200','L97 T351','A',1,'190631','','95699','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','DUMMY NC','DUMMY NC','|DUMMY NC','|DUMMY NC','DUMMY NC','','2019-08-10','Raghavendra Rao(R)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','no','With Treatment','','03','no','Misc','Raghavendra Rao(R)','no','','|DUMMY NC','E3456','qas|','2019-08-12|','2019-08-12',NULL,NULL,NULL,NULL,NULL,NULL),(11918,'46-005B','Mahindra Aerostructures Pvt.Ltd','STRAP','5181501 2','D575-40862-201','NA','F',1,'MAPL forecast 2018','','96270','','0000-00-00',NULL,'yes','','yes','','yes','','','','','Running time  machine value shifted 2mm in x axis so part profile out','Part running time X-Axis value shifted.|Machine X-axis controller error.|Controller error caused due to poor capacitor in controller system.','|OEM maintenance team was called and after verifying the capacitor was checked and replaced.','|Informed the Internal maintenance team to take additional care on controller unit during every preventive maintenance.','further machine maintenance verified and found okay.','','2019-08-10','Lohith(K)','        Madhu Kumar N','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','3','','','','','','|Immediately stopped the machine, cross checked work offset and informed to maintenance team.','Z3456','pe||','2019-08-12|2019-09-20|','2019-09-20',NULL,NULL,NULL,NULL,NULL,NULL),(11919,'18-295A','Magellan Aerospace Bournemouth','BOLT','927652/289060','PID577 56145 200','','A',1,'435247','','94532','','0000-00-00',NULL,'yes','yes','yes','','','','','','','OD UNDER SIZE 0.01MM','1. Tail stock support was not given by operator.|2. In between the cycle time OD need to be cross verified, after verification without tail stock support cycle was started.','|Tail stock support was provided to next part & then Run','|Message will be added to the program for operator awareness to provide the tail stock support.','','','2019-08-11','Raghavendra Rao(R)','        KRISHNAMURTHY N','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','11','','','','','','|Before next part running, cross check with all the machined parts as per MPS','E3456','pe|qas|','2019-08-12|2019-08-13|','2019-08-13',NULL,NULL,NULL,NULL,NULL,NULL),