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--
-- Table structure for table `nc4qa`
--

CREATE TABLE `nc4qa` (
  `recnum` int(11) DEFAULT NULL,
  `refnum` varchar(20) DEFAULT NULL,
  `customer` varchar(255) DEFAULT NULL,
  `partname` varchar(25) DEFAULT NULL,
  `bachnum` varchar(20) DEFAULT NULL,
  `partnum` varchar(20) DEFAULT NULL,
  `matl_spec` varchar(20) DEFAULT NULL,
  `issues_ps` varchar(255) DEFAULT NULL,
  `qty` int(11) DEFAULT NULL,
  `ponum` varchar(20) DEFAULT NULL,
  `part_sl_num` varchar(20) DEFAULT NULL,
  `wonum` varchar(20) DEFAULT NULL,
  `dcnum` varchar(20) DEFAULT NULL,
  `dcdate` date DEFAULT NULL,
  `traceability_recnum` varchar(30) DEFAULT NULL,
  `dim_deviation` varchar(5) DEFAULT NULL,
  `man` varchar(5) DEFAULT NULL,
  `inprocess` varchar(5) DEFAULT NULL,
  `mat_deviation` varchar(5) DEFAULT NULL,
  `machine` varchar(5) DEFAULT NULL,
  `final_insp` varchar(5) DEFAULT NULL,
  `other_deviation` varchar(5) DEFAULT NULL,
  `method` varchar(5) DEFAULT NULL,
  `cust_end` varchar(5) DEFAULT NULL,
  `description` text,
  `root_cause` text,
  `corrective_action` text,
  `preventive_action` text,
  `effectiveness` text,
  `cofcnum` varchar(20) DEFAULT NULL,
  `create_date` date DEFAULT NULL,
  `super_name` varchar(100) DEFAULT NULL,
  `oper_name` varchar(255) DEFAULT NULL,
  `cust_ncno` varchar(100) DEFAULT NULL,
  `cust_ncdate` date DEFAULT NULL,
  `remarks` text,
  `formatnum` varchar(255) DEFAULT NULL,
  `formatrev` varchar(255) DEFAULT NULL,
  `rm_cost` decimal(10,2) DEFAULT NULL,
  `currency` char(10) DEFAULT NULL,
  `status` char(30) DEFAULT NULL,
  `accepted` varchar(5) DEFAULT NULL,
  `rejected` varchar(5) DEFAULT NULL,
  `quarantined` varchar(5) DEFAULT NULL,
  `wotype` varchar(45) DEFAULT NULL,
  `dn_num` varchar(45) DEFAULT NULL,
  `stagenum` varchar(30) DEFAULT NULL,
  `rework` char(5) DEFAULT NULL,
  `mc_name` varchar(100) DEFAULT NULL,
  `created_by` varchar(30) DEFAULT NULL,
  `onsite` char(5) DEFAULT NULL,
  `assy_grn` varchar(255) DEFAULT NULL,
  `immediate_corrective_action` text,
  `siteid` varchar(45) DEFAULT NULL,
  `modified_by` text,
  `modified_date` text,
  `close_date` date DEFAULT NULL,
  `acknowledgement_date` date DEFAULT NULL,
  `response_date_cust` date DEFAULT NULL,
  `response_date` date DEFAULT NULL,
  `nc_mode` varchar(255) DEFAULT NULL,
  `cim_nc_status` varchar(20) DEFAULT NULL,
  `cust_nc_status` varchar(20) DEFAULT NULL,
  KEY `ind_nc4qa_wonum` (`wonum`),
  KEY `ind_refnum` (`refnum`),
  KEY `ind_create_date` (`create_date`)
) ENGINE=InnoDB DEFAULT CHARSET=latin1;

--
-- Dumping data for table `nc4qa`
--

INSERT INTO `nc4qa` VALUES (1,'18-001A','Magellan Aerospace W','BRACKET SUPPORT - LH','54213','D361 50110 200 01','s80','a',2,'RM83631','nil','485','nil','2007-07-24','nil','','yes','yes','','','','','','','Tool dig mark 1 no\r\nthickness undersize 1 no','rrrrrrr2','Need correction','ppppppp2','DUMMY NC','nil',NULL,'','','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'$','Closed','','','','','','0','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(3,'18-032A','Magellan Aerospace B','BUSH','027354','D278 50165 200','','',30,'RM358377','-','376','','0000-00-00','','yes','yes','yes','no','no','no','no','no','no','','DUMMY NC','DUMMY NC','DUMMY NC','DUMMY NC','',NULL,'Anjinamurthy(H)','        ','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'$','Closed','','yes','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(4,'18-190A','Magellan Aerospace B','BUSH HINGE BRKT FWD','0804401698','L575 52329 200','BS 23','',4,'RM365245 Amnd 1','','1570','','0000-00-00','','yes','yes','yes','no','no','no','no','no','no','BORE TO BE CHANGED','DUMMY NC  ','DUMMY NC','DUMMY NC','DUMMY NC','',NULL,'Anjinamurthy(H)','        ','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'$','Closed','','yes','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(5,'18-217A','Verdict Aerospace Co','BUSH SLIDING CON DRIVEN','CD712400','PIL579 51151 200','S145','A00',3,'55551','','1952','','0000-00-00','','yes','yes','yes','no','no','no','no','no','no','1)Total length: 28.74 to 28.94 measures 28.50 to 28.64mm.\r\n\r\n2)Bore dia 25.40 to 25.433 measures 25.438 to 25.441\r\n\r\n\r\n','1)Operator has not butted the part properly\r\n2)During FAI proving out this deviation occured.','1)Instructed Operator to butt the part properly before machining the part.\r\n2)Instructed Operator to take care during FAI proving of parts.','1)Instructed Operator to butt the part properly before machining the part.\r\n2)Instructed Operator to take care during FAI proving of parts.','Further produced parts found O.K.','','2009-04-11','Dinakar.K','Dinakar.K','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(6,'33-012','Norcot Engineering L','JACK BRACKET 1','306191-1B1','D576 50009 200','7050 T7651 ABM3 1030','C00',2,'20561','NA','2081','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Rib thickness 3.8mm measured 3.3mm','The 3d face was unable to check correctly, hence this deviation occured','Corrected the tool offset accordingly to acheive the required 3d face within the tolerance.','Suggested for checking fixture to check the COS points during operation itself.','Further produced parts found OK','','2009-04-23','Krishna(Chowdary.G.P.)','Rangaswamy()','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(7,'18-219A','Verdict Aerospace Co','BUSH SLIDING DRIVEN ECC','CD712400','PIL579 51156 200','S145','A00',3,'55551','','1954','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','1)Tool dig mark noticed. \r\n2)Bore over size by 10 micron.','1)During power failure tool dig mark occured on part.\r\n2)Since the part was produced for the first time,during FAI this deviation occured.','1)Power failure could not be predicted,\r\n2)Care shall be taken to avoid such deviation during FAI.','1)Process shall be made correctly during FAI.','Next produced parts were found O.K.','','2009-04-26','Dinakar.K','Dinakar.K','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(8,'28-004','Ellanef Manufacturin','PIN',' 91047','161A2332-1','15-5PH per AMS5659','NA',2,'98436 Rel-0','','2008','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','1)Dig mark noticed on OD of dia 1.8660/1.8650','Tool offset not taken properly  by operator.','Instruction given to operator while taking offset crosscheck once again before running job.','Process is changed for next batch for avoid taking workoffset for every peice.','Shall be derived during next batch production','','2009-04-27','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(9,'18-208A','Verdict Aerospace Co','SPRING RETAINER','638857','PID321 40203 220','S98','L',2,'55568','','1879','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1)Bore measures over size by 4 to 5 micron locally.','During production batch machining of 100 nos, this deviation of 4 to 5 micron occured on 2nos.','Took extra care while Checking of bores with more precision.','Care shall be taken during inspecting bores with high precision.','Further produced parts were found O.K','','2009-04-27','Dinakar.K','Rajesh.T ','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(11,'18-097A','Magellan Aerospace B','PLATE','39064','PID282 50100 200','L168','A',18,'RM365291','','1988','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1) thread damage noticed.','During tapping manually by the fitter this deviation occured.','Instruction given to fitter to take care while manuall tapping to avoid this deviation.','Planned for this operation in CNC machine.','CA/PA Found satisfactory.','','2009-04-27','Dinakara(G)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(12,'18-175A','Magellan Aerospace B','BRKT MTG HINGE FWD','8404101','PIL575 55449 201','ABM3 - 1029','A00',1,'RM365233 Amend 1','','1987','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Bore: dimensions dia 19.05/19.071 measures 19.074 to 19.076mm','Cutter compensation not adjusted properly.','Instructions given for operator to take care while adjust cutter compensation.','For next batch planned for reamer to avoid such deviation.','Shall be derived after next batch production','','2009-04-27','','','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'$','Closed','','yes','','','','0','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(13,'01-080','HAL-Helicopter','ARIS BEAM - LH','H918-44/07','201X 533H 6100 305','3.1354.T351','PS 23939, 24322, 30408, 31922, 33225, 33846',1,'5553055','','2025','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Tool dig mark noticed on the flat side rib by 1mm','One of the inserts of Dia 25 tipped cutter broke down while running and dig mark appeared on the part. Tool was older and insert seating was weak.\r\n','Tool replaced.','New tool is replaced.','Further produced parts were found O.K','','2009-04-27','','','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'$','Closed','','yes','','','','0','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(14,'18-223A','Verdict Aerospace Co','BUSH','CD744010','PIL579 51177 200','S145','A00',6,'55551','','1966','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Outer diameter: dia12.666 to 12.684 measures dia12.661,***','Since the part was produced for the first time,during FAI this deviation occured','Care shall be taken to avoid such deviation during FAI','Process shall be made correctly during FAI.','Shall be derived after next batch production.','','2009-04-27','Dinakar.K','Dinakar.K','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(15,'01-080','HAL-Helicopter','ARIS BEAM - LH','H918-44/07','201X 533H 6100 305','3.1354.T351','PS 23939, 24322, 30408, 31922, 33225, 33846',1,'5553055','','2025','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Tool dig mak noticed on th part','Operator did not take the offset correctly','Instructed Operator to take the tool offset correctly','Instructed Operator to take the tool offset correctly','further produced parts found ok','','2009-04-27','Vishwanath(P)','Vishwanath(P)','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(16,'18-106A','Magellan Aerospace B','EYE END INBOARD','590431','PID575 41542 200','S98','D',1,'RM365154 Amnd 1','','2022','','0000-00-00',NULL,'yes','no','yes','no','yes','no','no','no','no','Thread damage noticed.','Power failure during the machining operation caused this deviation.','Could not predict the power failure during operation.','Could not predict the power failure during operation.','Remaining parts produced were found O.K.','','2009-04-27','Dinakar.K','Parmesh & Ramesh Bandagi','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(17,'18-221A','Verdict Aerospace Co','PIN CON N/DRIVEN','CD712400','PIL579 51163 200','S145','A00',9,'55551','','1963','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','Bore dia15.00mm measures 15.40 to 15.50mm','Since the part is produced for the first time this deviation occured.','Process change is requested to the process planning department.','Process change is requested to the process planning department.','Shall be derived after next batch production.','','2009-04-27','','',NULL,NULL,NULL,'F8003-S','Rev 0 dt 8/1/2009',NULL,NULL,'Closed',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(18,'18-202A','Magellan Aerospace W','ANGLE CLEAT','158385','D572 59281 200','ABM3 - 1029','A',5,'RM90868','','1933','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Thickness: dimension 3.5mm measures 3.05 to 3.10mm.','Wrong offset of tool taken by operator.insted of moving 60mm down from fixture top, operator made rotary center as Z0.','Instruction given to operator to take the offset correctly.','Feed back form is attached to process sheet requesting to mention the Z0 referance in the process sheet.','Shall be derived after next batch production.','','2009-04-27','Dinakara(G)','Dinakara(G)','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(19,'18-001A','Magellan Aerospace W','BRACKET SUPPORT - LH','96913012','D361 50110 200 01','ABM3 - 1029','A',1,'RM90857','','1809','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1) Hole diameter: dia3.20 measures 3.40mm.','HSS drill bit was used to drill the hole,operator did not notice the runout of drill bit.','Instruction given to operator for checking whether the tool is mounted properly without runout.','Planned to use CARBIDE drill instead of HSS drill.','Shall be derived after next batch production','','2009-04-27','Dinakara(G)','Dinakara(G)','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(20,'18-199A','Magellan Aerospace W','ANGLE CLEAT','158385','D572 59282 200','ABM3 - 1029','A',3,'RM90868','','1924','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1)To a depth 0.5mm tool dig mark noticed in 1no.\r\n\r\n2)Total Length: dimension 30.0mm measures 29.60mm.','1) Dia 5 flat e/m broken during cut-out and tool dig mark occured.\r\n2) Due to run out the tool dia 5 flat which was held in collet this deviation occured.','1)Tool is replaced and instructed operator to check the tool periodically during production.\r\n2) Collet holder replaced with hydraulic holder to avoid runout.','1)Instructed operator to check the tool periodically during production.\r\n2) Collet holder replaced with hydraulic holder to avoid runout.','Further produced parts were found O.K.','','2009-04-27','Dinakara(G)','Dinakara(G)','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(23,'18-104A','Magellan Aerospace B','BODY TURNBUCKLE','027952','PID575 40490 200','S80','E',1,'RM365144 Amnd 1','','1980','','0000-00-00',NULL,'yes','no','yes','no','yes','no','no','no','no','Thread NOGO Gauge answered in LH side.','During final cut of threading operation power failed, when the same cut passed  again the thread nogo answered.','Power failure unpredictable.','Power failure unpredictable.','Further produced parts were found O.K.','','2009-04-27','Dinakar.K','x','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(24,'18-213A','Verdict Aerospace Co','END CAP','48468','PID321 40209 200','L168','A',3,'55568','','1873','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','1) 45deg hole not achived as per drawing.','While drilling using the jig this deviation occured.','Planned to machine the 45 deg hole on the machine itself.','Planned to machine the 45 deg hole on the machine itself.','Further produced parts were found O.K.','','2009-04-27','Dinakara(G)','Dinakara(G)','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(25,'18-006A','Magellan Aerospace W','COVER PLATE','5578702 3','D572 52516 200 01','L97 - T351','A',1,'rm90854','','1897','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no',' Tool dig mark noticed to a depth of 0.5mm.','Dia 8 flat E/M broken during machining and dig mark occured.','Tool replacsd and instructed operator to check the tool peridically.','Instructed operator to check the tool peridically.','Further produced parts were found O.K.','','2009-04-27','Dinakara(G)','Dinakara(G)','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(26,'18-049A','Magellan Aerospace B','CLEAT RH','1866601','PIL575 52505 201','ABM3 1029 7010','A00',1,'RM365124','','1833','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Tool dig mark noticed to a deapth of 0.5mm.','while machining firstoff peice workoffset was not taken properly.','Instruction given to operator to take the workoffset correctly.','Suggested to process planning dept to incorporate the position of the workoffset in process sheet.','Shall be derived after next batch production.','','2009-04-27','Dinakara(G)','Dinakara(G)','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(27,'18-197A','Magellan Aerospace W','ANGLE CLEAT','179125','D572 59284 200','ABM3 - 1029','A',1,'RM90868','','1926','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no',' 1) Tool dig mark noticed.','During machining tool broken,hence this deviation occured.','Instructed operator to check the tool periodically during machining batch quantity.\r\n','Program changed with less depth of cut and feed.','Further produced parts were found O.K.','','2009-04-27','Dinakara(G)','Dinakara(G)','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(28,'18-049A','Magellan Aerospace B','CLEAT RH','0748501','PIL575 52505 201','ABM3 1029 7010','A00',1,'RM365124','','1832','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','Tool dig mark noticed to a depth of 1mm and length under size by nominal.','Program was not correct, hence this deviation occured.','Instructed Programmer to ensure the correct program is given to manufacture the part.','Took backup of the corrected program for further batch parts machining.','Further produced parts were found O.K.','','2009-04-27','','','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'$','Closed','','yes','','','','0','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(29,'18-044A','Magellan Aerospace B','ANGLE ATCH RSPAR UPR - LH','352672A0','PIL575 52440 200','ABM3 1029 7010','A00',1,'RM365124','','1861','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','1) Tool dig mark noticed to a deapth of 2mm.','Tool broken during machining and dig mark occured on the part.','Tool replaced and instructed operator to check the tool periodically during production.','Instructions given to the operator to check the tool periodically during production and to change the tool if it is wornout.','Further produced parts were found O.K.','','2009-04-27','Dinakara(G)','Dinakara(G)','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(30,'18-049A','Magellan Aerospace B','CLEAT RH','1866601','PIL575 52505 201','ABM3 1029 7010','A00',1,'RM365124','','2007','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','Thickness: 2.50+/-0.25 measures 2.15 to 2.20mm.','Method of clamping was not correct hence this deviation occured.','Requested process planning Dept to change the clamping method.','Next batch of production shall be carried out with new clamping method.','Shall be derived after next batch production','','2009-04-27','','','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'$','Closed','','yes','','','','0','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(31,'18-122A','Magellan Aerospace B','FORKEND ASSEMBLY','614122','PID572 50462 201','S98','J01',7,'RM365139 Amnd 1','','1606','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1) Bore: dia15.895+0.018 measures dia15.922 to 15.938','operator not checked bore every peice and he has not checked stock for boring bar in regural intervals.','Instruction given to operator for checking bore for every peice and checking stock at regular intervals.','Instruction given to operator for checking bore for every peice and checking stock at regular intervals.','Shall be derived after next batch production.','','2009-04-27','Dinakara(G)','Dinakara(G)','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(32,'18-121A','Magellan Aerospace B','BARREL - STRUT','583915','PID572 50463 201','S98','F',3,' RM365136 Amnd 1','','1844','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','1) In dia 4.88 hole tool dig mark noticed.\r\n\r\n2) in dia 1.6 hole drill bit broken and clogged into the hole.\r\n\r\n','1) Dia 4.88 drill bit broken while drilling.\r\n2) Dia 1.6 drill bit broken while drilling.','Drills replaced and instructions given to the operator to check the drill bits periodically during batch production.','instructions given to the operator to check the drill bits periodically during batch production.','Further produced parts were found O.K.','','2009-04-27','Dinakara(G)','Dinakara(G)','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(33,'18-105A','Magellan Aerospace B','FORKEND ASSEMBLY','614122','PID572 50462 200','S98','J01',1,'RM365139 Amnd 1','','1635','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','1) Key way machined wrong side (opposite)','Operator loaded the job in wrong direction.','Instructed operator to check whether the part is loaded correctly as per process sheet before machining the part.','Instructed operator to check whether the part is loaded correctly as per process sheet before machining the part.','Further produced parts were found O.K.','','2009-04-27','Dinakara(G)','Dinakara(G)','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Select','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(34,'18-198A','Magellan Aerospace W','ANGLE CLEAT','126661','D572 59283 200','ABM3 - 1029','A',2,'RM90868','','1927','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','1) Tool dig mark noticed to a deapth of 3mm.\r\n\r\n2) Length: 30.0mm measurs 28.90 to 28.95\r\n\r\n\r\n                                             date:04-04-09','1) Dia 5 flat e/m broken during cut-out and tool dig mark occured.\r\n2) Due to run out the tool dia 5 flat which was held in collet this deviation occured.','1)Tool is replaced and instructed operator to check the tool periodically during production.\r\n2) Collet holder replaced with hydraulic holder to avoid runout.','1)Instructed operator to check the tool periodically during production.\r\n2) Collet holder replaced with hydraulic holder to avoid runout.','Further produced parts were found O.K.','','2009-04-27','Dinakara(G)','Dinakara(G)','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(35,'18-152A','Magellan Aerospace W','CLEAT','140543','F572 54597 202','ABM3 - 1029','E',2,'RM90864','','1800','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','1) Thickness:2.50mm measurs 2.05 to 2.10mm.','Operator did not check the stock before giving final cut.','Instructed operator to ensure enough stock is available to give final cut.','Instructed operator to ensure enough stock is available to give final cut.','Further produced parts were found O.K.','','2009-04-27','Dinakara(G)','Dinakara(G)','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(36,'18-097A','Magellan Aerospace B','PLATE','39064','PID282 50100 200','L168','A',1,'RM365291','','1221','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','1) Dia 5.50 hole measures plus side is dia 5.80.','Due to run out in the drill this deviation is occured.','Instructed operator to ensure whether the drill is held properly without run out and also to ensure the drill angle is correct.','Carbide drill is being used and collet holder is replaced with hydraulic holder.','Further produced parts were found O.K.','','2009-04-27','Kumar(K.S.)','Lokesh(B.D.)','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'$','Closed',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(37,'30-025','Gardner Aerospace Bu','RIB CLOSING INBOARD - RH','6708501 03','L575 54754 201','ABM3 1029','A, ECN: SG60049U03JA06',1,'CON0009715','','1971','','0000-00-00',NULL,'yes','no','yes','no','yes','no','no','no','no','1) Web and Flage thickness reduced by 0.3 to 0.5 gradually.\r\n\r\n\r\n\r\n\r\n','Machine bed is taper by 0.6mm','Informed to service personnel to correct the bed allignment.','Expecting clearance from service personnel.','Shall be derived after getting clearance from Service Personnel.','','2009-04-27','','','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'$','Closed','','yes','','','','0','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(38,'30-002','Gardner Aerospace Bu','CHANNEL TRAILING EDGE - R','240747-1A1','L575 51740 201','ABM3 1029','A, ECN:PG60049E01KB91',1,'CON0009715','','1659','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','1) Web thickness: web thickness measures 0.8 to 1.2mm insted of 1.8mm locally.\r\n\r\n\r\n\r\n                                         date:08-04-09','Operator did not enter the tool length compensation \"H\" value correctly, hence this deviation occured.','Instructed Operator to be cautious while entering compensations in machine.','Pasted a caution notice on the Machine on how to enter \"H\" value in machine.','Further produced parts were found O.K.','','2009-04-27','Kumar(K.S.)','PAVAN KUMAR (S.K.)','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'$','Closed',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(39,'23-027','Goodrich Aerospace','REINFORCEMENT PLATE','50416-1','7712500-8054','7075-T6511 AMS QQ A-','TR IP 7712500-8054 REV 02',1,'CRGL14416-03-09','','2028','','0000-00-00',NULL,'yes','no','no','no','no','yes','no','yes','no','1) Holes position in zone TRIP measures 0.025\" for 0.010\" for all the holes. thickness 0.1220/0.1420\" measures 0.1208/0.1210\"\r\n\r\n\r\n','Since the RM is extrusion,the material after declamping this deviation accured.','Suggested to QAD inspector to clamp at the same positions which was made while machining.','Suggested to QAD inspector to clamp at the same positions which was made while machining.','Shall be derived after next batch production.','','2009-04-27','Krishna(Chowdary.G.P.)','Krishna(Chowdary','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'$','Closed','','yes','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(40,'23-047','Goodrich Aerospace','PLATE','57111-1','7712501-822','7075-T6511 AMS-QQ-A-','TR IP 7712501-822 REV 02',1,'CRGL14416-02-09','','2042','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no',' 1)web: dig mark noticed at web thickness.(base)','While operator was taking tool length offset this dig mark occured.and machine was not having handwheel difficult to take offset.','Instructed  operator to take care while taking tool length offset.','Requested for commissioning  handwheel on machine to avoid such mistakes.','Further produced parts were found O.K. Expected to incorporate handwheeel in the machine.','','2009-04-27','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'$','Closed','','yes','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(41,'23-086','Goodrich Aerospace','BASE','402543A3','A800268-812','7050T7451 IAW AMS405','ECN 71347 (2 Sheets)',1,'CRGL14435-FI','','1876','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1)Hole diameter dia 0.3747/0.3753\" measures dia 0.3758/0.3760\"\r\n\r\n\r\n\r\n','Quite difficult to analyze,the reamer was checked on a dummy block and found correct,but when the same was run on the job this deviation occured.','Scraped the reamer a new reamer was ordered for machining next batch of parts.','New reamer was ordered for machining next batch of parts.','Shall be derived after next batch production.','','2009-04-27','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'$','Closed','','yes','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(42,'23-086','Goodrich Aerospace','BASE','402543A3','A800268-812','7050T7451 IAW AMS405','ECN 71347 (2 Sheets)',1,'CRGL14435-FI','','1876','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','1) dia0.219/0.227\" in zone D12 measures dia0.2510','During clamping hole drilling fitter used wrong size drill and hence this deviation occured.','Inculuded clamping hole drilling on the CNC machine itself instead of drilling it on drilling machine.','Inculuded clamping hole drilling on the CNC machine itself instead of drilling it on drilling machine.','Further produced parts were found O.K.','','2009-04-27','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'$','Closed','','yes','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(43,'18-108A','Magellan Aerospace B','FORK END OUT BD','619171','PID575 41546 200','S80','B',4,'RM365147 Amnd 1','','2029','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1) Bore: dia11.0+0.018 measures 11.021 to 11.025mm.','operator not checked bore every peice and he has not checked stock for boring bar in regural intervals.','Instruction given to operator for checking bore for every peice and checking stock at regular intervals.','Instruction given to operator for checking bore for every peice and checking stock at regular intervals.','Shall be derived after next batch production','','2009-04-27','Dinakara(G)','Dinakara(G)','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(44,'23-041','Goodrich Aerospace','PLATE','266500','7712501-814','7075-T651 IAW AMS-QQ','TR IP 7712501-814 REV 03',1,'CRGL14416-04-09','','1999','','0000-00-00',NULL,'yes','no','no','no','no','yes','no','yes','no','Dimension 1.695 -0.015 measures 1.6614 to 1.6732\r\n\r\n\r\n\r\n','Setting block was set for X axis ref,however pieces having excess material got cleared during machining operation, this piece was not having enough stock for final operation.','Instructed operator to adjust the Y axis ref for pieces which have minimum stock.','Suggested to process planning to increase the RM size in width for further batches.','Shall be derived after next batch production.','','2009-04-27','Siddalinga(Tambake)','Venkatesh(B)','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'$','Closed',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(45,'23-083','Goodrich Aerospace','BRACKET','267892','A400129-801','7075-T651- IAW- AMS-','ECN 63701',1,'CRGL14435-01-09','','2046','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','1) Dig mark noticed on top face.','During cutout machining part lifted up and dig mark occured on the part.','Instructed operator to ensure wheather the part is clamped rigidly.','Instructed operator to ensure wheather the part is clamped rigidly.','Further produced parts were found O.K.','','2009-04-27','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'$','Closed','','yes','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(46,'18-106A','Magellan Aerospace B','EYE END INBOARD','590431','PID575 41542 200','S98','D',1,'RM365154 Amnd 1','','2100','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Total length drawing dimension 101.0 measures 99.7mm.','while running piece came out side from the jaws(1mm). because of insert problem and chuck pressure low','new insert changed and chuck pressure adjusted.','Chuck pressure updated in process sheet.','Further Pieces manufactured and found within tolerance','','2009-04-27','Dinakar.K','Parmesh K','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(47,'18-121A','Magellan Aerospace B','BARREL - STRUT','583915','PID572 50463 201','S98','F',1,' RM365136 Amnd 1','','2038','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Outer diameter dia32.0 measures dia31.20mm.','while rough tool running the dia undersize.','Instructed operator to ensure enough stock is there before running final pass.','While approaching finish dimension semifinish cut should be given prior to final cut to ensure correct dimension is acheived.','Further produced parts were found O.K.','','2009-04-27','Dinakar.K','Parmesh K','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(48,'18-211A','Verdict Aerospace Co','PLUNGER','694000','PID321 40205 200','S80','H01',1,'55568','','1889','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Thread NOGO Gauge answered.','During production batch running of 100nos, this deviation occured for 1no.','Instructed operator to check the dimensions prior to giving final cut during threading operation.','Instructed operator to check the dimensions prior to giving final cut during threading operation.','Further produced parts were found O.K.','','2009-04-27','Dinakar G','Dinakar G',NULL,NULL,NULL,'F8003-S','Rev 0 dt 8/1/2009',NULL,NULL,'Closed',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(49,'18-006A','Magellan Aerospace W','COVER PLATE','127155 / 03','D572 52516 200 01','L97 - T351','A',2,'rm90854','','2093','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','1) profile shifted from center axis by 1mm.','Mis-interpretation of work offset by operator.in 1st su and 2nd su operator has centerlized work piece for X0 Y0 insted of moving from locating hole.','Work offset corrected and instructed operator to understand the process correctly before taking work offset.','A note is included in the process sheet to dial the locating hole and to move towards center by 60mm and make X0 Y0.','Further produced parts were found O.K.','','2009-04-27','Dinakara(G)','Dinakara(G)','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(50,'23-060','Goodrich Aerospace','BASE ASSY','269268','7718152-815','7075-T7351 PER QQ-A-','ECN 102246 (3 Sheets)',1,'CRGL14435-01-09','','2107','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Width size less by 1mm.','While machining a batch of 250 nos setting block was set for X axis ref,however pieces having excess material got cleared during final operation,this piece was not having enough stock for final operation.','Instructed operator to adjust the X axis ref for pieces which have minimum stock.','Suggested to process planning to increase the RM size in width for further batches.','Shall be derived after next batch production.','','2009-04-28','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'$','Closed','','yes','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(52,'33-006','Norcot Engineering L','HINGE BRACKET 3','253234 A','D576 50006 200','7050 T7651 ABM3 1030','C00',1,'20562','','2179','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','BORE: Bore measures plus side by 0.2 in one side','Operator not take care while doing boring operation and this deviation accured.','Training given to operator to how to set the boring bar and instruction given to take care while doing firstoff.','next all parts coming ok.','Next batch found satisfactory.','','2009-05-06','Krishna','Girish prasad','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','','yes','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(51,'18-121A','Magellan Aerospace Bournemouth','BARREL - STRUT','583915','PID572 50463 201','S98','F',4,' RM365136 Amnd 1','','2038','','0000-00-00',NULL,'yes','no','yes','no','yes','no','no','no','no','Sub : 1) Thread damage noticed in 2 no’s \r\n      2) Drill bit broken in 2 no’s (dia 1.5)','1) Thread damage (tool dig mark)because of power trip or failure.','Power failure unpredictable.','Power failure unpredictable.','RC/CA/PA TO BE ENTERED','','2009-05-06','Dinakar.K & Dinaker. G','Parmesh K &','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(53,'28-002','Ellanef Manufacturing Corporation','LOWER LINK','91119','161A6104-4','15-5PH CRES Steel Pl','NA',1,'98515 Rel-0','','2036','','0000-00-00',NULL,'yes','no','yes','no','yes','no','no','no','no','1) chamfer diameter oversize, chf 0.5mm plus on one side.','tool offset changed in tool no. 2 and 4 while running continous production in intervals.','instructed to operator to dont use tool no. 2 and 4 and message putted on machine.\r\n','informed to BFW person to attend the problem.','RC/CA/PA TO BE ENTERED','','2009-05-07','Anjinamurthy(H)','Anjinamurthy(H)','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'$','Closed','','yes','','Manufacture Only','','03','','Misc',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(54,'18-108A','Magellan Aerospace Bournemouth','FORK END OUT BD','633077','PID575 41546 200','S80','B',2,'RM365147 Amnd 1','','2276','','0000-00-00',NULL,'yes','no','yes','no','yes','no','no','no','no','1)Thread damage noticed in 01 no.\r\n2) Thickness Dimension 4.24+/-0.3 measures 3.46/3.64 in 01 no.','1)Due to sudden power failure, thread damaged.\r\n2)Cutter radius compensation not entered correctly by the Operator.','1. Sudden power failure occured hence thread damage occured\r\n2. Corrected Cutter radius compensation','1.Power failure unpredictable\r\n2. Instructed Operator to enter correct Cutter radius compensation','CA/PA Found satisfactory.','','2009-05-11','Dinakar.G','Parmesh & Ramesh Bandagi','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(55,'23-027','Goodrich Aerospace','REINFORCEMENT PLATE','57110-1','7712500-8054','7075-T6511 AMS QQ A-','TR IP 7712500-8054 REV 02',3,'CRGL14416-03-09','','2268','','0000-00-00',NULL,'yes','no','no','no','no','yes','no','yes','no','1)Drawing calls position tolerance 0.010\" (Excluding bonus tolerance of 0.006\")but part measures 0.027\" / 0.032\".','RM is extrusion and it has BEND & TWIST therefore this deviation occured.Due to Urgency in dispatch we taken risk and manufactured.','Instructed Operator to check whether bend or twist is found on RM before taking for machining.','From next batch taken care that if material is not BEND & TWIST then only machine the parts.','CA/PA found satisfactory.','','2009-05-11','Dayananda','Dayananda','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'$','Closed','','yes','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(56,'18-108A','Magellan Aerospace Bournemouth','FORK END OUT BD','633077','PID575 41546 200','S80','B',1,'RM365147 Amnd 1','','2030','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Thread effective diameter undersize.\r\nThread dia: 13.053 to 13.134 measured value is 12.98 to 12.99.','While changing new tip this deviation occured.','Instructed operator to change the offset value to get correct dimension','Instructed operator to approach the final cut after checking the part during semifinishing cut.','CA/PA Found satisfactory.','','2009-05-13','Dinakar.K','Parmesh & Ramesh Bandagi','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(57,'18-110A','Magellan Aerospace Bournemouth','FORK END INTERMEDIATE','625707','PID575 40494 202','S80','J',2,'RM365150','','2066','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Thread effective diameter undersize. \r\n1)Thread dia: 13.053to13.134 measured value is 13.00 in 1no.\r\n2)Thread damage noticed in 1 no.','power failure 1no. next piece had loaded and the thread cycle runned but the thread dia had undersize. \r\n','for the next job offset have taken in plus side.','instruction given to operator that if power goes take the offset in plus side.','RC/CA/PA TO BE ENTERED','','2009-05-13','Dinakar.K','Ramesh Bandagi','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(58,'18-001A','Magellan Aerospace Wrexham','BRACKET SUPPORT - LH','2849331C1','D361 50110 200 01','ABM3 - 1029','A',1,'RM90857','','2085','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Tool dig mark noticed on hole of Dia7.937.','Drill broken while drilling the part.','Instructed Operator to check the sharpness and drill grinding of the part before using it.','Instructed Operator to check the sharpness and drill grinding of the part before using it.','FOUND OK.','','2009-05-13','Dinakar.G','Nagaraj','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(59,'18-006A','Magellan Aerospace Wrexham','COVER PLATE','1780401-3','D572 52516 200 01','L97 - T351','A',1,'rm90854','','2095','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Hole: Dia6.35 / 6.40 measures, dia6.43 pin gauge entering.','Operator used 6.4 reamer instead of 6.35 reamer.','Instructed operator to check tool dimension before loading tool.','Tool eching done for avoding such mistakes.','RC/CA/PA TO BE ENTERED','','2009-05-13','Dinakara(G)','Dinakara(G)','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(60,'18-006A','Magellan Aerospace Wrexham','COVER PLATE','8579403-3','D572 52516 200 01','L97 - T351','A',1,'rm90854','','2096','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','1) Thickness: Base thickness 4.0mm+0.3/-0.2, measures 3.63 to 3.67\r\n2) 7.0mm+0.3/-0.2 measures 6.67.','tool offset not taken properly by operator.','instructed to operator to check tooloffset onceagain before running job.','presetting block planned.','RC/CA/PA TO BE ENTERED','','2009-05-13','Dinakara(G)','Dinakara(G)','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(61,'18-110A','Magellan Aerospace Bournemouth','FORK END INTERMEDIATE','625707','PID575 40494 202','S80','J',1,'RM365150','','1932','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Bore: Bore over size by 3 to 4micron and also feed lines noticed.','due to wear of insert feed lines noticed.','instructed to operator to change inserts regular intervals.','planned for reamer.','RC/CA/PA TO BE ENTERED','','2009-05-13','Dinakara(G)','Dinakara(G)','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(62,'18-006A','Magellan Aerospace Wrexham','COVER PLATE','127155 / 03','D572 52516 200 01','L97 - T351','A',2,'rm90854','','2093','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Base Thickness: base thickness reduced by 1mm.','Wrong tool offset entered by Operator','Tool offset corrected.','Warned operator to work seriously and to cross check off set. and also tool pre setter is planned.','RC/CA/PA TO BE ENTERED','','2009-05-13','Dinakara(G)','Dinakara(G)','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(63,'18-205A','Magellan Aerospace Wrexham','JOINT PLATE','025962 / 001','D572-59095-200-01','ABM3-1029','C01',2,'RM90867','','2078','','0000-00-00',NULL,'no','no','yes','yes','no','no','no','yes','no','raw material stock less for 2nd sup (part length will be reduced after finish the part by 1mm)','while cutting raw material, length undersize.','instructed to fitter while cutting care to be take.','instructed to fitter while cutting care to be take.','Next batch found satisfactory.','','2009-05-13','Dinakara(G)','Dinakara(G)','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(64,'18-087B','Magellan Aerospace Wrexham','PLATE SEALING ASSY','7984401-1','D572 52914 200 01','ABM3 1029','B',2,'RM90855','','2035','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dig mark: tool dig mark noticed on the out side profile by 1mm.','coolant not adjusted propely due to this tool broken.','instructed to operator adjust coolant for every tool.','instructed to operator adjust coolant for every tool.','CA/PA Found satisfacory.','','2009-05-13','Dinakara(G)','Dinakara(G)','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(65,'18-087B','Magellan Aerospace Wrexham','PLATE SEALING ASSY','268039','D572 52914 200 01','ABM3 1029','B',4,'RM90855','','1816','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Groove: dig mark noticed on inside groove width 6.27/6.40 measures plus by 2mm.','Operator used wrong tool 8r0.8 instead of 6r0.4.','Instructed operator to use right tool as per process sheet.','Instructed operator to croscheck whether right tool is used before running job.','CA/PA Found satisfacory.','','2009-05-13','Dinakara(G)','Dinakara(G)','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(66,'33-011','Norcot Engineering Limited','HINGE BRACKET 5','253234 C','D576 50008 201','7050 T7651 ABM3 1030','C00',3,'20562','','2267','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Bore oversize by 30 microns.Dia 22.225 / 22.246 measured value is 22.250 to 22.290.','In between production running this deviation occured.','Instruction given to operator to take care while doing boring operation and changed the insert and all parts coming ok.\r\n','Instruction given to operator to take care while doing boring and check the boring bar insert at reguler interval','RC/CA/PA TO BE ENTERED','','2009-05-13','Krishna(Chowdary.G.P.)','Krishna','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'$','Closed','','yes','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(67,'18-086B','Magellan Aerospace Wrexham','PLATE SEALING','268038','D572 52913 200 01','ABM3 1029','B',3,'RM90855','','2034','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Out side chamfer tool dig mark noticed in 1no.\r\nTotal length undersize, 170+0.3/-0.3 measured value 169.66 169.67 in 2no\'s.','operator used damaged holder due to hold the tool, hence runout of tool became more.','Damaged holder scrapped and instructed operator to check before loading tool.','Damaged holders are srcapped.','CA/PA Found satisfacory.','','2009-05-13','Dinakara(G)','Dinakara(G)','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(68,'18-121A','Magellan Aerospace Bournemouth','BARREL - STRUT','509259','PID572 50463 201','S98','F',2,' RM365136 Amnd 1','','786','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','1)Drill bit broken in 1no\r\n2) Hole oblonged in Dia4.88 hole.','1) drill bit not grinded properly due to this drill bit broken.\r\n2) drill bit not grinded properly.','drill bit proved for dummy peice and then runned for orginal peice.','drill bit proved for dummy peice and then runned for orginal peice.','RC/CA/PA TO BE ENTERED','','2009-05-13','Dinakara(G)','Dinakara(G)','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(69,'18-118A','Magellan Aerospace Bournemouth','BEARING HOUSING','674211','PID275 40005 200','S130','C01',2,'RM365159 Amnd 1','','1603','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1) Outer diameter: dia44.405/44.420 measures 44.38 to 44.39','while contenious running suddenly the od diameter have gon undersize.there was no material stock for finish tool.','for every 5pieces after od roughing the operator checks at the machine it self.','for every 5pieces after od roughing the operator checks at the machine it self.','RC/CA/PA TO BE ENTERED','','2009-05-13','Dinakar.K','Vikram E','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(70,'18-097A','Magellan Aerospace Bournemouth','PLATE','45559A','PID282 50100 200','L168','A',2,'RM365291','','2024','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','1) Tool dig mark noticed on profile in 1no\r\n\r\n2) NO GO answered (10x32 unf Thread)in 1no','1) \r\n2) This operation done in tapping m/c and then manually done this operation.','Instructed to fitter care to be taken while doing operation manually.','Planned to do tapping operation on cnc m/c.','CA/PA Found satisfactory.','','2009-05-13','Dinakara(G)','Dinakara(G)','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(71,'34-007','BRISTOL AEROSPACE LIMITED','CLIP UPPER CUTTER WSPS','245642','446 83029 1 901','17-4PH/AMS 5528','B, ECN 39968 Iss-A',1,'B62472','','1902','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Hole: hole dia4.83/4.87 measures 4.90 pin gauge entering.','drill bit not grinded properly.','drill bit proved in dummy peice and then runned in orginal peice.','drill bit proved in dummy peice and then runned in orginal peice','RC/CA/PA TO BE ENTERED','','2009-05-13','Anjinamurthy(H)','Anjanamurthy','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'$','Closed','','yes','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(72,'18-105A','Magellan Aerospace Bournemouth','FORKEND ASSEMBLY','590431','PID572 50462 200','S98','J01',2,'RM365139 Amnd 1','','2015','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Bore Dia 14.308+0.018 measures 0.2mm in one piece plus and 2mm plus on another piece.','Operator did not adjust the boring bar correctly','Instructed Operator to ensure currect adjustment of boring bar before machining the bore.','Planned for machgining with Reamers','CA/PA Found satisfactory.','','2009-05-13','Dinakar.G','Sunil kumar','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(73,'18-111A','Magellan Aerospace Bournemouth','BODY TURNBUCKLE INTMD','625720','PID575 41544 200','S80','A',1,'RM365149 Amnd 1','','2023','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1) hole: dia6.0+0.12 measures 6.20 pin gauge entering.','drill centeraid was incurrect so drill dia had oversize','centeraid have been set for an dummy piece and then proved to the job.','in future further setup first we proved centeraid to an dummy piece.','CA/PA Found satisfactory.','','2009-05-13','Dinakar.K','Ramesh Bandagi','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(74,'18-107A','Magellan Aerospace Bournemouth','LINK ASSY','112','PID574 50553 200','DTD5014','A',5,'RM365142 Amnd 1','','2175','','0000-00-00',NULL,'yes','no','yes','no','yes','no','no','no','no','Bore dia15.870+0.015 measures 15.892 to 15.901','while proving reamer in bmv 60-2, 5 nos. rejeected.','this job then loaded in bmv 45-2 and all jobs found ok.','Here after this job will be machined only on bmv 45-2.','CA/PA Found satisfactory.','','2009-05-13','Pandurang','Diwakar.R.B','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(75,'18-112A','Magellan Aerospace Bournemouth','BODY TURNBUCKLE INNER','659414','PID575 41541 200','S80','A',3,'RM365153 Amnd 1','','2187','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Bore: bore dia12.70+0.018 measures 12.723 to 12.740','operator not checked stock for bore regular intervals.','instructed operator for checking stock for bore regular intervals.','planned for reamer for next batch.','RC/CA/PA TO BE ENTERED','','2009-05-13','Dinakara(G)','Dinakara(G)','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(76,'18-086B','Magellan Aerospace Wrexham','PLATE SEALING','6150401','D572 52913 200 01','ABM3 1029','B',1,'RM90855','','2033','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','1) Tool dig mark noticed on out side diameter.',' Due to improper clamping during cutout xtra material rotated and tool broke down resulting in dig mark on outer surface.Threads were worn in fixture.','Retapping done.','New fixture is done for next batches.','CA/PA Found satisfacory.','','2009-05-13','Dinakara(G)','Dinakara(G)','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(77,'18-116A','Magellan Aerospace Bournemouth','ASSEMBLY FORK END','46079','PIF575 51377 200','L168','A',4,'RM365155 Amnd 1','','2121','','0000-00-00',NULL,'yes','no','no','no','no','yes','no','yes','no','1) Bore 12.00+0.018 measures 12.016 to 12.029','Bore finishing was being done by interpolation as a result of which in some pieces ovality was coming.','Reamer for dia 12 H7 is used and interpolation method was dropped.','Reamer for dia 12 H7 is used and interpolation method was dropped.','RC/CA/PA TO BE ENTERED','','2009-05-13','Dinakara(G)','Dinakara(G)','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(78,'18-198A','Magellan Aerospace Wrexham','ANGLE CLEAT','888417','D572 59283 200 01','ABM3 - 1029','A',1,'RM90868','','2142','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Hole oblong noticed on dia4.0mm hole.','Centering was not proper as a result after dia 4 drill hole was oblong.','Centering deapth adjusted.',' Center drill deapth altered and instructions given to operator to check centering before dilling.','Further produced parts were found O.K','','2009-05-13','Dinakara(G)','Dinakara(G)','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(79,'18-117A','Magellan Aerospace Bournemouth','HOUSING-OUT BD BRG','662385','PID275 40004 200','S130','C01',5,'RM365157','','2064','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','Bore Dia 66.675 to 66.705 measures 66.712 to 66.735','During machining ID Bore ovality occured when clamping, hence this deviation occured.','Rubber pad inserted in the step bore during clamping to avoid ovality of bore during machining.','Rubber pad inserted in the step bore during clamping to avoid ovality of bore during machining.','Further machined parts are found O.K','','2009-05-13','Dinakar.G','Narashima Murthy & Vikram','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(80,'18-078A','Magellan Aerospace Wrexham','ADAPTOR','257068','D282 50081 200',' L111 T6','NIL',1,'','','1781','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Tool dig mark noticed on Threads.','Operator did not butt the job properly, hence this deviation occured.','Ensured the butting of the job is done correctly.','Instructed Operator to butt the job correctly.','CA/PA Found satisfactory.','','2009-05-14','Dinakar.K','Nithin','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(81,'18-078A','Magellan Aerospace Bournemouth','ADAPTOR','257068','D282 50081 200',' L111 T6','NIL',15,'','','1223','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','1) Spot face not carried out as per dwg (depth more)in 6no,s\r\n2) Tool dig mark noticed in 2no\'s\r\n3) Thread damage noticed in 4no\'s\r\n4) Outer diameter measures under size in 3no\'s','1.Program error caused the deviation\r\n2.Program error caused the deviation\r\n3.Attempted to reduce cycle time this deviation occured.\r\n4.Attempted to reduce cycle time this deviation occured.','1.Programer Corrected the program to derive the correct depth at the spot face area\r\n2. Operator took the offset wrongly\r\n3.Care taken during machining after changing cutting parameters.\r\n4.Care taken during machining after changing cutting parameters.\r\n','1.Programer Corrected the program to derive the correct depth at the spot face area\r\n2. Operator took the offset wrongly\r\n3.During attempting cycle time reduction care to be taken to acheive correct dimensions on the part.\r\n4.During attempting cycle time reduction care to be taken to acheive correct dimensions on the part.\r\n','Further produced parts found OK','','2009-05-14','Dinakara(G)','Dinakara(G)','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(82,'18-078A','Magellan Aerospace Wrexham','ADAPTOR','256413','D282 50081 200',' L111 T6','NIL',3,'','','2132','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','1) Outer diameter measures under size by 0.5mm in 2no\'s\r\n2) Thickness under size 3.9 measures 3.15 in 1no.','1) This deviation occured because X-offset was not entered correctly.\r\n2) Butting not done properly','1. Instructed Operator to take the X-offset correctly.\r\n2. Instructed Operator to butt the job properly.\r\n','1.Instructed Operator to check the offset before machining the job.\r\n2.Instructed Operator to crosscheck whether the job is butted properly to the jaws face.','CA/PA Found satisfactory.','','2009-05-14','Dinakar.K','Parmesh & Ramesh Bandagi','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(83,'18-091A','Magellan Aerospace Bournemouth','BUSH','659416','PID278 50164 202','S80','A',7,'RM365162 Amnd 1','','1644','','0000-00-00',NULL,'yes','no','yes','no','yes','no','no','no','no','Outer diameter measures under size by 5 to 8microns.','In DX-200(2)  outer dia was giving ovality hence the OD was undersize.','','','RC/CA/PA TO BE ENTERED','','2009-05-14','Dinakar.K','Parmesh & Ramesh Bandagi','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(84,'33-002','Norcot Engineering Limited','HINGE BRACKET','219021 B','D576 50004 200','7050 T7651 ABM3 1030','C00',1,'20562','','2264','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','Wall thickness 3.125+/-0.125 measures 1.0mm','Operator taken wrong workoffset and this deviation accured.\r\ndue to not avialable of process sheet operator not understand process written in referance book and taken wrong work offset.','Cross check the workoffset in CAD CAM and taken new workoffset and machined, then all parts coming ok.','Request to CAD CAM to prepare process sheet.','RC/CA/PA TO BE ENTERED','','2009-05-14','Krishna(Chowdary.G.P.)','Krishna','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'$','Closed','','yes','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(85,'18-102A','Magellan Aerospace Bournemouth','BARREL-STRUT','583915','PID572 50463 200','S98','F',1,' RM365136 Amnd 1','','1843','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Bore dia 24.5 +0.2 measured value is 25.46/25.48.','Tool radius offset was not given correctly by the Operator','Corrected the offset value','Instructed Operator to check the offset values entered before machining the part.','CA/PA Found satisfactory.','','2009-05-14','Dinakar.K','x','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(86,'23-026','Goodrich Aerospace','REINFORCEMENT PLATE','57110-1','7712500-8053','7075-T6511 / AND 101','TR IP 7712500-8053 REV 01',2,'CRGL14416-03-09','','2108','','0000-00-00',NULL,'yes','no','no','no','no','yes','no','yes','no','Hole position out of tolerance:Hole position 0.010\" measures 0.004\"/0.018\".','Due to BEND & TWIST in RM this deviation accured.','From next batch check the BEND & TWIST then only machine the part.','From next batch check the BEND & TWIST then only machine the part.','CA/PA found satisfactory.','','2009-05-15','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'$','Closed','','yes','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(87,'18-082A','Magellan Aerospace Wrexham','STUD PLATE - LH','0141302','D278 50007 200 01','ABM3 1029','D01',1,'RM90860','','2154','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dig mark noticed on top face.','Tool fell down on part and dig mark appeared on the part.\r\nWhen operato tried to remove the tool from spindle it slipped out of his hand and fell down on part.','Warned operator to handle the tools and parts properly.','Warned operator to handle the tools and parts properly','found ok.','','2009-05-16','panduranga','Nagaraj K S','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(88,'18-112A','Magellan Aerospace Bournemouth','BODY TURNBUCKLE INNER','659414','PID575 41541 200','S80','A',1,'RM365153 Amnd 1','','2208','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Bore dia12.7 / 12.718 measures 12.725 to 12.728','Not tightening the screw of boring bar after giving correction.','Screw tightened and instruction given to operator to cross check whether screw is tightened or not.','Instruction given to operator to cross check whether screw is tightened or not.','CA/PA Found satisfactory.','','2009-05-17','Dinakar.G','Lokesh.B.D','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(89,'33-015','Norcot Engineering Limited','JACK BRACKET 2','306191 1A1','D576 50010 201','7050 T7651 ABM3 1030','C00',4,'20562','','2311','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','1) Radius: Tool dig mark witnessed on R4 and base thickness 3.825+/-0.125 measures 3.65 locally in 1no.\r\n2) Major tool dig mark noticed on the top profile in 1no.\r\n3) Bore measures plus side by 12microns.\r\n4) tool dig mark noticed in the place of bore to','1)Tool comeout from holder while running and dig mark noticed.\r\n2),4)These two parts are due.\r\n3)Operator not given correction boring bar properly and found deviation.','1)Changed the holder and all parts coming ok.(holder made scrap).\r\n2),4)\r\n3)Instruction given to operator to take care while doing boring operation.\r\n','1)Checked all the holders and found ok.  \r\n2),4)\r\n3)Instruction given to operator to take care while doing boring operation.','Next batch found satisfactory.','','2009-05-17','Krishna(Chowdary.G.P.)','Girish(Prasad P)','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','','yes','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(90,'33-014','Norcot Engineering Limited','JACK BRACKET 2','306191 1A1','D576 50010 200','7050 T7651 ABM3 1030','C00',1,'20562','','2310','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','COS points measures minus side by 0.1mm on both sides.','Operator not taken correct workoffset and this deviation accured in firstoff part.','Correct the workoffset and all parts coming ok.','training given infront of machine to operator and also instruction given to him to take care while taking workoffset.','RC/CA/PA TO BE ENTERED','','2009-05-17','Krishna(Chowdary.G.P.)','Krishna','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'$','Closed','','yes','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(91,'18-117A','Magellan Aerospace Bournemouth','HOUSING-OUT BD BRG','662385','PID275 40004 200','S130','C01',2,'RM365157','','2280','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','1)Major dig mark noticed on outside profile in 01 no.\r\n2)OD 69.95/69.97 measures 69.933/69.947 in 01 no.','1. Job slipped from the jaws due to wear in roughing inserts.\r\n2. Ovality occured during machining the part.','1. Changed the wornout inserts \r\n2. Used rubber pad at ID and clamped the part for avoiding ovality on OD\r\n','1. Check the wearout of the tool tips periodically.\r\n2. Use rubber pad at ID and clamped the part for avoiding ovality on OD\r\n','CA/PA Found satisfatory.','','2009-05-17','Dinakar.K','Narashima Murthy & Vikram','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(92,'18-211A','Verdict Aerospace Components Ltd.','PLUNGER','694000','PID321 40205 200','S80','H01',1,'55568','','2189','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Outside thread NOGO gauge entering.','Operator did not set the threading tool properly','Instructed Operator to set the threading tool correctly','Instructed Operator to set the threading tool correctly','Further produced parts found OK','','2009-05-17','Dinakar(K)','Nithin(S)','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(93,'18-111A','Magellan Aerospace Bournemouth','BODY TURNBUCKLE INTMD','659414','PID575 41544 200','S80','A',1,'RM365149 Amnd 1','','2207','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1) Dent mark noticed on top profile up to 1mm.\r\n2) Major tool dig mark noticed in slot.','Tool broken during machining.\r\nJOb fell down from hand and dent mark appeared.','Tool replaced.\r\nInstructed oprator to handle the job carefully.','Instructions given to operator to observe the tool and to change if necessary.','CA/PA Found satisfactory.','','2009-05-18','Dinakar.G','Thirthappa  & Sunil Kumar & Mohan kumar','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(94,'18-110A','Magellan Aerospace Bournemouth','FORK END INTERMEDIATE','657212','PID575 40494 202','S80','J',1,'RM365150','','2200','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','1) Major tool dig mark witnessed upto 2mm deapth and 5mm width.','Tool broken during machining.','Tool replaced','Instruction given to oprator to observe cutter and to replace if necessary.','RC/CA/PA TO BE ENTERED','','2009-05-19','Dinakar.G','Thirthappa','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(95,'18-110A','Magellan Aerospace Bournemouth','FORK END INTERMEDIATE','657212','PID575 40494 202','S80','J',4,'RM365150','','2200','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Bore: 1) dai14.2875+0.018 measures plus side by 14.3085 to 14.316 in 2no,s\r\n2) dai14.2875+0.018 measures plus side by 14.3115 to 14.313 in 2no,s\r\n','1) Operator did not set the boring tool correctly\r\n2) Operator did not set the boring tool correctly','1)Instructed Operator to set the boring tool correctly','1)Instructed Operator to set the boring tool correctly','Further produced parts founf OK','','2009-05-19','Dinakara(G)','Theerthappa(K.N.)','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'$','Closed','','yes','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(96,'18-033A','Magellan Aerospace Bournemouth','CARRIER SEAL - LH','0729405-2','PID575 55658 200','L97 T351','C',1,'RM364965','','2332','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Tool dig mark noticed at the end of groove for 1mm depth.','Operator tried to take T-slot tool up when power failure happened and machine was restarted. The toolwas inside thr groove.','Instructions given to operator in such cases to unclamp the tool from holder first and then to take spindle to safe position for refferencing.','Instructions given to operator in such cases to unclamp the tool from holder first and then to take spindle to safe position for refferencing.','Next parts found ok.','','2009-05-20','Dinakar.G','Divakar S','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(97,'01-305','HAL-Helicopter','FRAME # 9 (TAIL CONE)','H918-23/07','201C 533H 6211 201','3.1354.T351','NIL',1,'5553091','','2232','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no',' Tool dig mark noticed on outside profile.( 3mm rib opend out)','Operator did not enter the offset value correctly for the program which clears extra material leftover.','Instructed Operator to take the offset value correctly, and cross check whether the taken offset is correct.','Change requested to CAD/CAM to edit the program which shall clear the extra material.','RC/CA/PA TO BE ENTERED','','2009-05-21','viswanath','venkatesh B I','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'$','Closed',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(98,'23-122','Goodrich Aerospace','REAR HOUSING EFB 10.4','610292','08720-0087-0003','6061-T651','NA',2,'395924','','2319','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','<b>Root Cause:</b><br>\r\n    <textarea name=\"root_cause\" rows=6 cols=60 value=\"\">\">    </td>\r\n</tr>\r\n<tr bgcolor=\"#FFFFFF\">\r\n    <td bgcolor=\"#FFFFFF\" colspan=6><span class=\"heading\"><b>Root Cause:<\" style=\";background-color:#DDDDDD;\"\" style=\";background-c','','1)Wrong workoffset taken by operator and this deviation occured. \r\n2)butting of the job not done properly and pocket shifted.','1)Instruction given to operator to take care while taking workoffset and loading the part.','CA/PA found satisfactory.','','2009-05-21','Krishna(Chowdary.G.P.)','Basvaraj','','0000-00-00','<b>Root Cause:</b><br>\r\n    <textarea name=\"root_cause\" rows=6 cols=60 value=\"\">\">    </td>\r\n</tr>\r\n<tr bgcolor=\"#FFFFFF\">\r\n    <td bgcolor=\"#FFFFFF\" colspan=6><span class=\"heading\"><b>Root Cause:<\" style=\";background-color:#DDDDDD;\"\" style=\";background-color:#DDDDDD;\" readonly=\"readonly\"><span class=\"heading\"><b>Root Cause:</b><br>\r\n    <textarea name=\"root_cause\" rows=6 cols=60 value=\"\">\">    </td>\r\n</tr>\r\n<tr bgcolor=\"#FFFFFF\">\r\n    <td bgcolor=\"#FFFFFF\" colspan=6><span class=\"heading\"><b>Root Cause:<\" style=\";background-color:#DDDDDD;\" readonly=\"readonly\">    <td bgcolor=\"#FFFFFF\" colspan=6><span class=\"heading\"><b>Root Cause:</b><br>\r\n    <textarea name=\"root_cause\" rows=6 cols=60 value=\"\">\">','F8003-S','Rev 0 dt 8/1/2009',0.00,'$','Closed','','yes','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(99,'18-098A','Magellan Aerospace Bournemouth','SEAT VALVE','B4356','PID282 50060 204','L109 T4','D',2,'RM365292','','2283','','0000-00-00',NULL,'yes','no','yes','no','yes','no','no','no','no','Hole dia4.83 measures over size and dia5.0 pin gage entering and it should be within dia4.87','While running 2 nd piece wrong tool change by machine instead of dia 4.83 drill dia 5 e/m called hence hole oversize..','Machine switched off and on.Cross checked all tools reference once again.','Informed to Service personnel','next batch found satisfactory.','','2009-05-22','panduranga','anjina murthy','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','','yes','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(100,'18-106A','Magellan Aerospace Bournemouth','EYE END INBOARD','590431','PID575 41542 200','S98','D',2,'RM365154 Amnd 1','','2258','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','1)Dia31.02 +0.025 measures dia31.100 in 1 no.\r\n2)Thickness undersize drawing dimension 11.1mm measures 10.58 to 9.38 in 1no.','1)Locking screw was not locked properly as threads worn.hence bore got oversize .\r\n2)Wrong tool offset','1)Screw replaced \r\n2)Work offset corrected.','1)Instructions given to operator to check whether loking screw is in good condition.\r\n2)Instructions given to operator to check  tool offset twice. PRESETTER is ordered to avoid this problem.','Further produced parts were found O.K.','','2009-05-22','Dinakar.G','Sathish.Y.R','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(101,'18-113A','Magellan Aerospace Bournemouth','ADJUSTER','629913','PID575 40496 200','S80','G',2,'RM365151 Amnd 1','','2115','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','1) Dia 1.15 hole drilled extra in 1no.\r\n2) dia 1.15 broken and clogged.','Fitter wrongly drill the hole on the piece.','Instructed Operator to ensure the drilling is performed at right position.','Instructed Operator to ensure the drilling is performed at right position.','Next batch found ok.','','2009-05-23','Nagaraj T','Erappa','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(102,'23-087','Goodrich Aerospace','BASE','346241','A800321-812','7050-T7451-IAW-AMS 4','ECN 71642',1,'CRGL14435-03-09','','2009','','0000-00-00',NULL,'no','yes','yes','no','no','no','yes','no','no','Dig mark observed at the base(Datum A)at zone C8.','tool inserts broken while running and dig mark noticed on face.','Changed the insert and screw.','Instruction given to operator to check the inserts and screws condition and then only load the tool.','CA/PA found satisfactory.','','2009-05-23','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'$','Closed','','yes','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(103,'18-104A','Magellan Aerospace Bournemouth','BODY TURNBUCKLE','027799','PID575 40490 200','S80','E',7,'RM365144 Amnd 1','','1892','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','1) Dia 3mm hole is done on both sides, but should be on one side only in 04nos.\r\n2) .5000\" 20-UNJF 3B LH Nogo gauge enters through full thread & damaged.','1)As pin was not entering completely, deapth of drill was increased by 5mm and drill touched the inner thrad at bottom side.\r\n2)while running,insert tip had broken and changed the insert took 0.1mm in plus side instead of 0.2mm so for this nogo gauge ente','1)Drill replaced and deapth corrected.\r\n2)so that for next job 0.2mm have been taken in plus side.','1)Instructions given to operator to change the drill but not the deapth.\r\n2)i have given training to operator at the spot itself.','Next batch found ok.','','2009-05-26','Dinakar.G',' Sunil Kumar','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','','yes','','','','0',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(104,'18-090A','Magellan Aerospace Bournemouth','BUSH','631516','PID278 50164 200','S80','A',2,'RM365162 Amnd 1','','2212','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','1)Dig mark observed on OD in 01 no.\r\n2) OD 39.964/39.980mm measures 39.95/39.96 in 01 no.','1)job slipped from the jaws.\r\n2)while contonious running od gone undersize.','1)to control the cycle time for one and half minitue so the spindle speed and feed was more, so job slipped. \r\n2)934Nos production quantity.','Instructed operator to hold the part correctly','Further produced parts found O.K','','2009-05-26','Dinakar(K)','Narasimha(Murthy R)','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'$','Closed','','yes','','','','0',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(105,'18-123A','Magellan Aerospace Bournemouth','FORK END OUT BD','633077','PID575 41546 202','S80','B',1,'RM365147 Amnd 1','','2349','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','bore: bore measures plus side by 0.02 to 0.03mm','Wrong setting of boring bar. Stock was only 0.08mm and operator while setting gave more correction.','Given correction corrected.','On line training given to operator and instucted him to check the given correction and confirm before machining.','Shall be derived after next batch production','','2009-05-27','Dinakar.G','Thirthappa & Mohan Kumar','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(106,'33-003','Norcot Engineering Limited','HINGE BRACKET 1','317180 2A1','D576 50004 201','7050 T7651 ABM3 1030','C00',1,'20562','','2339','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','slot width: 23.0+/-0.03 measures 23.50','While running production in between 1 no this deviation accured.unable to judge the root cause.','Very difficult to analyse that this is a operator problem or tool problem or machine problem.changed the tool and runned and next part found OK. problem is under opservation.','Very difficult to analyse that this is a operator problem or tool problem or machine problem.changed the tool and runned and next part found OK. problem is under opservation','Next batch found satisfactory.','','2009-05-27','Krishna C','Lokesh.B.D & Girish Prasad & Srinivas.S.N','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','','yes','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(107,'18-113A','Magellan Aerospace Bournemouth','ADJUSTER','644826','PID575 40496 200','S80','G',2,'RM365151 Amnd 1','','2278','','0000-00-00',NULL,'yes','no','yes','no','yes','no','no','no','no','Thread damage noticed.','While running threadind operation power failure 2times.','power fail will not control.','power fail will not control.','Next further part found ok.','','2009-05-27','Dinakar.K','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(108,'33-006','Norcot Engineering Limited','HINGE BRACKET 3','317180 2A1','D576 50006 200','7050 T7651 ABM3 1030','C00',2,'20562','','2388','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','1)Tool dig mark noticed on COS surface upto a deapth of 5mm in 1no.\r\n2) Major tool dig mark noticed on top profile to a deapth of 1mm.','1)Operator taken wrong workoffset and dig mark noticed.\r\n\r\n','1) training given infront off the machine to operator and instruction given to take care while taking tool offset.','1) next all batch parts coming ok.','*','','2009-05-28','Krishna C','Krishna','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'$','Closed','','yes','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(109,'18-101A','Magellan Aerospace Bournemouth','TUBE-STRUT','51186','PID572 50464 202','T45','F',1,'RM365135 Amnd 1','','2114','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','A quantity of 1 part has been found to have deep scores on the outside surface and has been assessed as being scrap. RDN 00504 Date:21/05/09','1) It might be happend in the packing.\r\n2) It maight be happend in the raw material stage it self.\r\n3) In Final inspection did not noticed.','instructed to concerned personal to handle carefully.','same as above.','CA/PA found satisfacory.','C1102','2009-05-29','Avinash.R.J','Muniyappa','RDN00504','2009-05-21','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','','yes','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(110,'01-244','HAL-Helicopter','SWASH PLATE MAST','H918-101/07','201P 623H 1200 254','7075 T73','PS 25169, 26167, 31270',1,'5553108','','1214','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','Major tool dig mark noticed on datum \'D\' and dimension 166.5-0.1 measures 163.0 at one place.','Improper clamping.While reworking, the part was direcly clamped on the bed with less butting area.So part rotated and major dig mark appeared on the datum D.','Fixture is used to clamp the cylinder so that clamping area is more and rigid.','Fixture is used to clamp the cylinder so that clamping area is more and rigid.','Further produced parts were found O.K','','2009-06-01','panduranga','anjina murthy','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(111,'18-211A','Verdict Aerospace Components Ltd.','PLUNGER','694000','PID321 40205 200','S80','H01',6,'55568','','2345','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','1) Tap broken and clogged at inside the hole in 2no\'s\r\n2) Drill bit broken in 2nos.\r\n3) Thread nogo answered due to oversize in 2no\'s.','1. During tapping operation the tap broken.\r\n2. Drill was wornout hence the drill was broken\r\n3. During tapping operation chips clogged and thread oversize occured','1. Changed new TAP for further pieces machining\r\n2. Instructed Operator to check the sharpness of the drill periodically.\r\n3. Instructed operator to adjust the coolant to flush the chips.','1. Tap should be changed after machining a defined batch qty.\r\n2. Instructed Operator to check the sharpness of the drill periodically.\r\n3.Instructed operator to adjust the coolant to flush the chips.','Further produced parts were found O.K.','','2009-06-01','viswanath','Narayan and Gajendra','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','','yes','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(112,'18-211A','Verdict Aerospace Components Ltd.','PLUNGER','694000','PID321 40205 200','S80','H01',5,'55568','','2189','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','1) OD undersize 9.965/9.975 measures 9.958/9.961 in 1no.\r\n2) dia8.50 hole oversize by 8.90 in 3no\'s.\r\n3) dia1.60 drill bit broken and clogged in side the hole.','1)od had been measured in plus side to control in drawing dimension again repass had been left,so the od undersize.','1)close tolerance.','','Next batch found ok.','','2009-06-01','Dinakar.K & viswanath','Narayan and Gajendra','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','','yes','','','','0',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(113,'18-105A','Magellan Aerospace Bournemouth','FORKEND ASSEMBLY','590431','PID572 50462 200','S98','J01',6,'RM365139 Amnd 1','','2178','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1)Keyway wrongside in 1 no.\r\n2)Tool dig mark noticed on 14.308 bore.\r\n3)Dia 14.308+0.018 measures 14.331 to 14.334 bore oversize in 3no\'s\r\n4)Dia 15.895+0.018 measures 15.919 to 15.923 bore oversize in 3no\'s','1) piece loaded wrongly.\r\n2)Dia 8 flat broken while roughing the bore as it was blunt.\r\n3)&4) Wrong correction given by the oprator .','1)piece loade correctly, operator was instructed to ensure that part is loaded correctly before machining.\r\n2)tool replaced.\r\n3)&4) Right correction given.','1)Separate fixture will be done for this part so that location matches to this part only.\r\n2)Instructions given to operator to check the tool periodically and to change the tool if necessary.\r\n3) & 4) On job training is provided to operator.','CA/PA Found satisfactory.','','2009-06-03','Dinakar G','Basvaraj and mohan and Thirthappa','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(114,'01-238','HAL-Helicopter','HINGE FITTING','H918-205/06','201Z 521H 3263 203','17734.4','PS 27010 30444',2,'','','2320','','0000-00-00',NULL,'no','yes','no','no','no','yes','yes','no','no',' 1)Parts not received in final inspection.','Parts produced almost 2 years back, and at the time of dispatch this year 2 parts are missing.','It is made mandatory for every department to count the parts as per W/O and make sure that recieved qty matches to W/O.','It is made mandatory for every department to count the parts as per W/O and make sure that recieved qty matches to W/O.','Next batch we have received correctly. ','','2009-06-03','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'$','Closed','','','yes','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(115,'23-033','Goodrich Aerospace','REINFORCEMENT PLATE','50416-1','7712500-80054','7075-T6511 / AND 101','TR IP 7712500-80054 REV 01',3,'CRGL14416-03-09','','2480','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','Hole Position Ø0.01(M) A B C measures 0.009/0.01588.','Due to bend and twist in RM this deviation accured.','Before loading the part checked the twist and then machined the part by taking workoffset (Y-AXIS)for every part.','Before loading the part checked the twist and then machined the part by taking workoffset (Y-AXIS)for every part.','CA/PA found satisfactory.','','2009-06-05','Krishna(Chowdary.G.P.)','Diwakar R B','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'$','Closed','','yes','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(116,'23-029','Goodrich Aerospace','REINFORCEMENT PLATE','266583','7712500 8106','7075-T651','TR IP 7712500-8106 REV 01',4,'CRGL14416-04-09','','2494','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','1)Dimension 3.504 +/-.03 measures 3.4418 and 11.607 +/-.03 measures 11.5540 in 02nos.\r\n2) Dig mark observed on top face near holes.','Operator calling wrong prg and this deviation occured.','instruction given to operator to take care while calling prg.Read and understand properly the process sheet then machine the parts.','Taking all prg backups from machine and only running prgs are given to operators to avoid such mistakes.','CA/PA Found satisfactory.','','2009-06-08','Pandurang',' Naveen','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(117,'33-015','Norcot Engineering Limited','JACK BRACKET 2','306191 1A1','D576 50010 201','7050 T7651 ABM3 1030','C00',2,'20562','','2385','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Bore oversize dia 30.1625/30.1875 measures 30.23 & finish not good in 2no\'s.','Boring bar long adapter used for boring operation and repeatablity not coming and for 2 nos this deviation occured.','Setup changed and removed adapter from boring bar and found all remaining parts coming ok.','Given feedback form to CAD CAM to make note in process sheet that boring operation done in small legth boring bar only.','Further produced parts found O.K','','2009-06-08','Krishna C','lokesh B.D','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'$','Closed','','yes','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(118,'18-007A','Magellan Aerospace Wrexham','COVER PLATE ASSY','127155 03','D572 52517 200 01','L97 - T351','A',1,'rm90854','','2228','','0000-00-00',NULL,'no','yes','yes','yes','no','no','no','no','no','First setup thickness undersize 2.0 mm.','the material recived was having more bend and to achieve the required flatness the operator errored while giving the workoffset.','instructed to operator while doing this job bend is to be checked.','instructed to operator before loading job material bend is to be check.','Further produced parts were found O.K','','2009-06-08','Dinakar G','Diwakar.S','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(119,'18-119A','Magellan Aerospace Bournemouth','HOUSING OUT B D BRG 3','CB882330','PID275 40011 200','S130','D01',2,'RM365160 Amnd 1','','2347','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1)Tool dig mark on undercut in ID in 1no.\r\n2)Scraches on OD radius & 1.5thickness face in 1no.','tool offset not taken properly due to this deviztion occurs.','instruction given to operator for crosschecking offset onceagain before giving cut.','instruction given to operator for crosschecking offset onceagain before giving cut.','Next batch found ok.','','2009-06-09','Dinakar K','Narashima Murthy','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','','yes','','','','0',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(120,'18-123A','Magellan Aerospace Bournemouth','FORK END OUT BD','690634','PID575 41546 202','S80','B',1,'RM365147 Amnd 1','','2350','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Tool dig mark on sphere.','As internal threads of bush were worn in which the part was held rotated while facing was under process.','Bush replaced.','Instructions were given to operator to check bush and replace if necessary at regular intervals.','CA/PA Found satisfactory. ','','2009-06-09','Dinakar G','Mohan kumar.C.M','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(121,'18-102A','Magellan Aerospace Bournemouth','BARREL-STRUT','583915','PID572 50463 200','S98','F',1,' RM365136 Amnd 1','','2260','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Dia 1.5 hole oblong & 1.5 drill bit brocken.','while running dia 1.5 drill bit broken.','instruction given to operator for changing drill for every 20 nos.','instruction given to operator for changing drill for every 20 nos.','CA/PA Found satisfactory.','','2009-06-09','Dinakar G','Thirthappa & Mohan Kumar','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(122,'33-014','Norcot Engineering Limited','JACK BRACKET 2','306191 1A1','D576 50010 200','7050 T7651 ABM3 1030','C00',1,'20562','','2384','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Rib thickness undersize 10.7 +/-0.25 measures 10.40 & slot width oversize 27.85 +/-0.25 measures 28.40.','Operator not entered correct trans value and this deviation occured.','training given to operator to how to give trans.','Requested  CAD/CAM to change the prg to CRC prg to avoid the manual mistakes.','Next batch found satisfactory.','','2009-06-09','Krishna C','Nagraj Nadiger','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','','yes','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(123,'18-008A','Magellan Aerospace Wrexham','COVER PLATE','6306402-1','D572 52518 200 01','L97 - T351','A',1,'RM90858','','2353','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','1) Dimension 1.0 x 45 degree measures 1.65/1.70 x 45 degree.','cutter radius compensation not entered properly.','CRC Value corrected and instructed operator to take care while entering compensation value.','Requested CAD/CAM to change programe for next batch without crc.','Further produced parts were found O.K','','2009-06-09','Pandurang','Manjunath.N.R','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(124,'23-077','Goodrich Aerospace','EDGE TEE','266218','7716254-801','7075-T7351 PER AMS 4','ECN 55880',1,'CRGL14435-02-09','','2367','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dig mark observed at zone B9 and thickness 0.160\" +/-.01 measures 0.1450\".','Fixture tap wearout and not clamped properly,operator not check butting face and this deviation occured.\r\n','Fixture tap hole corrected and clamped then part butted currectly.','Instruction given to operator that check tap holes properly then only load the fixture.and every part check butting face with FEALLER GUAGE.\r\nInform to CAD CAM to put note in process sheet that every piece should check butting.','Further machined parts were found O.K','','2009-06-10','Pandurang','Naveen B S','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(125,'18-098A','Magellan Aerospace Bournemouth','SEAT VALVE','B4356','PID282 50060 204','L109 T4','D',2,'RM365292','','2283','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','1)Thickness 3.25 +0.3/-0.2 measures 3.0 to 3.02 & slot depth oversize 0.9/1.0 measures 1.05 to 1.07 in 2no.','1)due to bend in material thikness undersize.\r\n2)crc not adjusted properly.','1)instruction given to operator for cheking bendness of the material before running job.\r\n2)in program mentioned crc value.','1)instruction given to operator for cheking bendness of the material before running job.\r\n2)in program mentioned crc value.','CA/PA Found satisfactory.','','2009-06-10','Pandurang','Siddaramappa','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(126,'18-121A','Magellan Aerospace Bournemouth','BARREL - STRUT','583915','PID572 50463 201','S98','F',6,' RM365136 Amnd 1','','2261','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1)Thread NOGO answered in 5nos.\r\n2)Dia 1.5 hole oblonged in 1no.','1)during setting 2no reject(Vikram)(Narasimha Murthy).\r\nwhile contenious running 3no\'s reject.','1)further currect setting had done.\r\nfor every each piece had checked in machine its self.','1)training have given to the operator at the spot.','RC/CA/PA TO BE ENTERED','','2009-06-10','Dinakar.K & Dinakar.G','Mohan kumar.C.M & Vikram & Narasimha Murthy','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(127,'18-205A','Magellan Aerospace Wrexham','JOINT PLATE','025962 / 001','D572-59095-200-01','ABM3-1029','C01',2,'RM90867','','2361','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','While cutting operation raw material undersize.','Fitter did not cut the raw material correctly.','instruction given for fitter while cutting care should be taken.','instruction given for fitter while cutting care should be taken.','Next batch found satisfactory.','','2009-06-11','Nagaraj','Rajesh','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(128,'18-207A','Magellan Aerospace Wrexham','JOINT PLATE','025962 / 001','D572 59094 203 01','ABM3-1029','D01',2,'RM90867','','2553','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','1)Tool dig mark on outside profile 1.0mm depth in 1no.\r\n2)Thickness undersize 4.0+0.3/-0.2 measures 3.50 to 3.70 in 1no.','1) while running tool broken.\r\n2) due to bend in material thickness undersize.','1) feed reduced for that cutter and next peices found ok.\r\n2) after removing bend next peices are machined and found ok.','same will be carried for next batches.','Next batch found ok.','','2009-06-13','Dinakar G','Lohith','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','','yes','','','','0',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(129,'30-017','Gardner Aerospace Burnley Limited','FRAME OUTBD RIB IFS - LH','47433014','L575 51896 200','ABM3 1029','A, ECN:PG60621001JA01',1,'CON0009715','','1665','','0000-00-00',NULL,'yes','no','no','no','no','no','no','yes','yes','Score marks in various pockets, not removed after machining. Burrs present in two pockets,not removed after machining.Inspection failur & failur to deliver conforming parts.','1) 100% visual inspection not carried out by QAD\r\n2) Visual inspection not done by production team.\r\n3) The special tool used to scan the negative draft has gone under size, there by not clearing the material.','1) QAD shall ensure 100% visual inspection and the same shall be mentioned in the quality plan.\r\n2) operators shall be educated on visual inspection and the same shall be recorded in the stage inspection report.\r\n3) Engineering shall look into improving t','Same as above','Found satisfacory.','C927','2009-06-16','Avinash.R.J','Prakash.C.B','Mail on 15/06/09','2009-06-15','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','yes','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(130,'30-018','Gardner Aerospace Burnley Limited','FRAME OUTBD RIB IFS - RH','47433013','L575 51896 201','ABM3 1029','A, ECN:PG60621001JA01',1,'CON0009715','','1667','','0000-00-00',NULL,'yes','no','no','no','no','no','no','yes','yes','We have received  rib from CIM, L575 51896 201, which have a score mark in one pocket on each rib, see attachment SNV31103. As can be seen from the attachments, the score mark is in the corresponding pocket in each rib & in the same position.',') In final inspection visualy did not noticed the score marks.\r\n2) production personnel did not noticed the score marks.\r\n3) In FAI part score marks in fillet radius smoothened in bench work.\r\n4) After FAI clearence CAD/CAM department has to pass the info','1) For future batches CAD/CAM department will take care in toolings to avoid the score marks and same information will be incorporated in the process sheet.\r\n2) Visual inspection will be incorporated in our quality plan.\r\n','Same as above','RC/CA/PA found satisfacory.','C928','2009-06-16','Avinash.R.J','Prakash.C.B','Mail on 15/06/09','2009-06-15','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','yes','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(131,'18-107A','Magellan Aerospace Bournemouth','LINK ASSY','112','PID574 50553 200','DTD5014','A',3,'RM365142 Amnd 1','','2275','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','1)Chamfer oversize & thickness 8.30/8.70 measures 7.1/7.8 in 1no.\r\n2)Dia 6.20/6.30 OD bend noticed in 2no.','1)wrong tool selection.\r\n2)due to wrong clamping piece have been found bend.','1)correct tool given and next peices found ok.\r\n2)clamping area space was less.','1)separate tool kept for that job.\r\n2)training given to the operator.','CA/PA Found satisfactory.','','2009-06-16','Dinakar.K & Dinaker. G','Mohan kumar.C.M& Rajesh.T','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(132,'18-214A','Verdict Aerospace Components Ltd.','SPECIAL WASHER','631551','PID321 40210 202','S98','E01',11,'55568','','1955','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1)width 2.0+/-0.3 measures 1.56 to 2.6 in 4nos.\r\n2)length 7.90/8.20 measures 7.78 to 7.84 in 7nos.','while broaching operation carring this deviation occurs.','broachig tool changed and next peices found ok.','new process done for next batch.','Next batch found ok.','','2009-06-16','Stalin','Ravindra sing and Suresh','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','','yes','','','','0',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(133,'18-215A','Verdict Aerospace Components Ltd.','ROD END ASSMY - MALE','631551','PID321 53012 200','S98','F01',6,'55568','','1853','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1)Tool dig mark on threads in 1no.\r\n2)Keyway depth oversize in 1no.\r\n3)Bore oversize & feedline noticed in 4nos.','1) power failure while thread machining.\r\n2) while adjusting keyway depth one no. rejected.\r\n3) while adjusting bore finsh this deviation occurs.','2)keyway depth adjusted and next peices found ok.\r\n3)RPM and FEED adjusted and next peices found ok.','boring insert grade changed for next batch.','ca/pa found satisfactory.','','2009-06-17','Pandurang','Divakar R.B and Nagaraj.K.S','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(134,'33-006','Norcot Engineering Limited','HINGE BRACKET 3','317180 1A1','D576 50006 200','7050 T7651 ABM3 1030','C00',1,'20577','','2414','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Dia22.225H7 measures 10micron plus by nominal.','Very difficult to analyse that this is a operator problem or tool problem or machine problem.problem is under opservation','Very difficult to analyse that this is a operator problem or tool problem or machine problem. problem is under opservation','Very difficult to analyse that this is a operator problem or tool problem or machine problem. problem is under opservation','RC/CA/PA TO BE ENTERED','','2009-06-18','krishna','Srinivas S.N,Lokesh B.D,Girishprasad','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'$','Closed','','yes','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(135,'33-007','Norcot Engineering Limited','HINGE BRACKET 3','253234A','D576 50006 201','7050 T7651 ABM3 1030','C00',1,'20577','','2416','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Slot Width: 23.09+0.03/-0.03 measures 23.15 to 23.17','Very difficult to analyse that this is a operator problem or tool problem or machine problem.changed the tool and runned and next part found OK. problem is under opservation','Very difficult to analyse that this is a operator problem or tool problem or machine problem.changed the tool and runned and next part found OK. problem is under opservation','Very difficult to analyse that this is a operator problem or tool problem or machine problem.changed the tool and runned and next part found OK. problem is under opservation','Next batch found satisfactory.','','2009-06-18','krishna','Srinivas S.N,Lokesh B.D,Girishprasad','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','','yes','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(136,'33-014','Norcot Engineering Limited','JACK BRACKET 2','313443 1B1','D576 50010 200','7050 T7651 ABM3 1030','C00',1,'20577','','2431','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Width: dimension 94.0 +/-0.3 measures 93.0 in the place of taper rib to a length of 10mm on both sides.','while running production tool come out from holder due to dia 12.5 collet putedd for dia 12 tool therefore tool come out from holder and taper rib measures minus side.','Changed the holder and then all parts machined ok.','Instruction given to all three operators to put collects for required dia only.','Next batch found satisfactory.','','2009-06-19','Krishna C','Rangaswamy','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','','yes','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(137,'18-103A','Magellan Aerospace Bournemouth','HEADED BUSH','027952','PID572 50465 200','S80','A',3,'RM365138 Amnd 1','','2566','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1)Bore oversize 9.525/9.540 measures 9.542 to 9.546.','1)during setting 3no\'s rejected due to tolerance 0.015 so there where no bore gauge.','1)to check bore dia air gauge had been set.','1)training have given to the operator.','CA/PA Found satisfacory.','','2009-06-24','Dinaker  K','Paramesh K&Ramesh Bandagi','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(138,'18-197A','Magellan Aerospace Wrexham','ANGLE CLEAT','147596','D572 59284 200 01','ABM3 - 1029','A',1,'RM90868','','2496','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Thickness min 5.6 -0/+0.3 measures 5.48/5.59 & stepmark on outside face.','Wrong referencing of A-axis ,After power failure when machine was switched on operator referenced 4th axis in wrong method.','REference corrected and on job training provided to operator regarding 4th axis referencing.','REference corrected and on job training provided to operator regarding 4th axis referencing.','Next further production batch found ok.','','2009-06-24','Panduranga','Naveen.B.S','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(139,'33-011A','Norcot Engineering Limited','HINGE BRACKET 5','219242 A','D576 50008 201','7050 T7651 ABM3 1030','C00',1,'20562','','2584','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Cos rib measures minus side by 2mm to depth of 20mm.','In tapping operation part butted in one face and tapping and location hole is done, but due to variation in RM size hole and tap shifted and after machining 2su rib thickness measures minus side.','Taking workoffset for every part and then all production parts coming ok.','Instruction given to operator to inspect the part correctly and check the RM size for every part and then put a location hole and tap.\r\ninform to CAD CAM to put note on process sheet.','Next batch found satisfactory.','','2009-06-24','Krishna C','Basvaraj.','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','','yes','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(140,'23-075','Goodrich Aerospace','EDGE TEE','266219','7716204-801','7075-T7351 PER AMS 4','ECN 55818',1,'CRGL14435-02-09','','2454','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dig mark observed at the radius .09\" throughout the length on both sides of the rib at zone E1.','Wrong tool offset taken by operator.','Tool off set corrected.','Instructed operator to take work offset correctly and check twice before starting machining.','CA/PA Found satisfactory.','','2009-06-24','Panduranga','Siddaramappa','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(141,'18-162A','Magellan Aerospace Bournemouth','STRUT AFT INNER - RH','A349852','F574 50156 207 47','J4374','E',1,'RM365294 Amnd 1','','2608','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Hole pitch shifted by 0.3 to 0.7mm on dia 2.4mm hole.','1) it was happend due to drill bit overhang. drill bit holded in drill chuck and it\'s not holded properly.','1) drill chuck replaced with new one.','1) to be check the run out of drill chuck before machining.','CA/PA found satisfactory.','','2009-06-24','Vishwanath','        Ghajendra Singh','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'$','Closed','','yes','','','','0',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(142,'18-090A','Magellan Aerospace Bournemouth','BUSH','224880','PID278 50164 200','S80','A',10,'RM358398','','999','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1)Dia 39.964/39.980 measures 39.955 to 39.959 in 8no\'s\r\n2)Tool dig mark on OD in 2no.','1)Operator did not take the offset correctly.\r\n1)Operator did not take the offset correctly.','1)Instructed Operator to take the offset correctly\r\n2)Instructed Operator to take the offset correctly','1)Instructed Operator to take the offset correctly\r\n2)Instructed Operator to take the offset correctly','Further produced parts found OK','','2009-06-24','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'$','Closed','','yes','','','','0',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(143,'18-104A','Magellan Aerospace Bournemouth','BODY TURNBUCKLE','629913','PID575 40490 200','S80','E',4,'RM365144 Amnd 1','','2316','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1)RH thread NOGO answered in 1no.\r\n2)LH thread NOGO answered in 3no.','1)Operator did not give the tool offet correctly\r\n)Operator did not give the tool offet correctly','1)Instructed Operator to take the tool offset correctly\r\n2)Instructed Operator to take the tool offset correctly','1)Instructed Operator to take the tool offset correctly\r\n2)Instructed Operator to take the tool offset correctly','Further produced parts found OK','','2009-06-25','Dinakar(K)','Narasimha(Murthy R)','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'$','Closed','','yes','','','','0',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(144,'18-091A','Magellan Aerospace Bournemouth','BUSH','659416','PID278 50164 202','S80','A',7,'RM365162 Amnd 1','','2282','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','OD undersize & ovality 45.964/45.980 measures 45.948 to 45.992.','Operator did not take the tool offset correctly','Instructed operator to take the tool offset correctly','Instructed operator to take the tool offset correctly','Further produced parts found OK','','2009-06-25','Dinakar(K)','Rajesh(T)','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(145,'18-105A','Magellan Aerospace Bournemouth','FORKEND ASSEMBLY','590431','PID572 50462 200','S98','J01',3,'RM365139 Amnd 1','','2438','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Bore 15.895+0.018 measures 15.918 to 15.920 in 3nos.','Operator did not set the boring tool correctly','Corrected the boring tool setting','Instructed the Operator to set the boring tool correctly','Further produced parts found OK','','2009-06-25','Dinakar(K)','Narasimha(Murthy R)','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(146,'18-122A','Magellan Aerospace Bournemouth','FORKEND ASSEMBLY','614122','PID572 50462 201','S98','J01',1,'RM365139 Amnd 1','','1637','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Tool dig mark noticed on spher.','while running job rotated.','instruction given to operator for doing proper tight. ','instruction given to operator for doing proper tight','CA/PA Found satisfactory.','','2009-06-25','Dinakar G','Sathish.Y.R','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(147,'18-122A','Magellan Aerospace Bournemouth','FORKEND ASSEMBLY','590431','PID572 50462 201','S98','J01',2,'RM365139 Amnd 1','','2439','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1)Bore 15.895+0.018 measures 15.918/15.923 & ovality 20 micron in 1no.\r\n2)Bore 14.308+0.018 measures 14.331/14.336 in 1no.','while adjusting boring bar this deviation occurs.','instruction given for operator while adjusting boring bar care should be take.','instruction given for operator while adjusting boring bar care should be take.','CA/PA Found satisfactory.','','2009-06-25','Dinakar G','Mohan Kumar & Sunil Kumar','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(148,'18-119A','Magellan Aerospace Bournemouth','HOUSING OUT B D BRG 3','CB894702','PID275 40011 200','S130','D01',2,'RM365160 Amnd 1','','2452','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','1)Tool dig mark on face in 1no.\r\n2)5 deg angle undercut oversize & stepmark noticed in 1no.','1) Tool broken during machining\r\n2) Operator did not take the offset correctly','1) Replaced with a new tool\r\n2) corrected the offset ','1)Instructed the Operator to check the sharpness of the tool periodically\r\n2) Instructed the Operator to take the offset correctly','Further produced parts found OK','','2009-06-26','Dinakar(K)','Paramesh(K)','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'$','Closed','','yes','','','','0',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(149,'18-282A','Magellan Aerospace Bournemouth','FUNK PINS','583915','PIA572 43263 200','S98','H',2,'RM368853','','2551','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Inside bore ovality & taper.','difficult to analyze the root cause, it might have occured due to high clamping pressure','Slightly reduced the clamping pressure','Instructed Operator to select correct claming pressure for holding the job','Further produced parts found OK','','2009-06-28','Dinakar(K)','Ramesh(S. Bandagi)','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(150,'18-283A','Magellan Aerospace Bournemouth','FUNK PINS','583915','PIA572 43263 202','S98','H',2,'RM368853','','2552','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Inside bore ovality & taper.','it might have occured due to high clamping pressure  \r\n\r\n','Slightly reduced the clamping pressure','Instructed Operator to select correct claming pressure for holding the job  \r\n','Further produced parts found OK ','','2009-06-28','Dinakar(K)','Paramesh(K)','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(151,'18-121A','Magellan Aerospace Bournemouth','BARREL - STRUT','583915','PID572 50463 201','S98','F',1,' RM365136 Amnd 1','','2549','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Dia 1.5 drill bit brockened.','while running dia 1.5 drill bit broken.','instruction given for operator changing drill for every 20 nos.','instruction given for operator changing drill for every 20 nos','NEXT BATCH FOUND.\r\n','','2009-06-28','Dinakar G','Thirthappa & Mohan Kumar & Sunil Kumar','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(152,'18-111A','Magellan Aerospace Bournemouth','BODY TURNBUCKLE INTMD','686194','PID575 41544 200','S80','A',3,'RM365149 Amnd 1','','2628','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1)Thread damage noticed in 1no.\r\n2)Slot width oversize in 2mm.','1) while runnig power failure.\r\n2) this job already rejected for bore oversize but we are used this job for setting antoher job.','instruction given for operator while adjusting boring bar care should be take. ','instruction given for operator while adjusting boring bar care should be take. ','CA/PA Found satisfactory.','','2009-06-28','Dinakar K & Dinakar G','Thirthappa  & Sunil Kumar & Nithin','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(153,'18-086B','Magellan Aerospace Wrexham','PLATE SEALING','283407','D572 52913 200 01','ABM3 1029','B',2,'RM90855','','2662','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Tool dig mark noticed on out side profile to a deapth of 0.5 to 1.0mm.','while running inserts losened due to this dig mark occurs.','instruction given to operator to check inserts tightness at regular intervals.','instruction given to operator to check inserts tightness at regular intervals','CA/PA Found satisfactory.','','2009-06-29','panduranga','Naveen.B.S','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(154,'18-178A','Magellan Aerospace Bournemouth','DOUBLER LOWER MID RIB','445821A2','PIF574 51070 200','L165','A',1,'RM365240 Amnd 1','','2572','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Tool dig mark noticed on face.','while drilling in jig boring operator putted hole in wrong co ordinate.','instructed to operater while drilling care should be take and next peices found ok.','for next batch jig is planned.','Next batch found ok.','','2009-06-30','Dinakar G','Jayaram','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','','yes','','','','0',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(155,'30-010','Gardner Aerospace Burnley Limited','RIB CLOSING OUTBOARD - RH','8788501 01','L575 51826 201','ABM3 1029','B, ECN:PG69999001JK19',1,'PRO0016034-S11','','2535','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Slot was done opposite side at one end','Operator loaded the part opposite side for machining the slot.','Instructed Operator to read the process sheet and load the part correctly','Instructed Operator to read the process sheet and load the part correctly','Futher produced parts found ok.','','2009-06-30','Stalin','Ravinder Singh','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'$','Closed',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(156,'18-107A','Magellan Aerospace Bournemouth','LINK ASSY','1243','PID574 50553 200','DTD5014','A',1,'RM365142 Amnd 1','','2634','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Bore 15.870/15.885 measures 15.905/15.912.','while setting reamer this deviation occurs.','reamer setted and next peices found ok.','reamer will be proved for dummy peices.','CA/PA Found satisfactory.','','2009-06-30','Dinakar G','Thirthappa','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(157,'34-018','BRISTOL AEROSPACE LIMITED','BRACKET, STRUT-L/H','A8107A','400-12609-1-905','4340 Steel Per SAE-A','ECN: 39611 Iss A, ECN 39840 Iss B',1,'B70996','','3170','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','Out side profile not done correct (out side diameter)','NC program not correctly made.','Program was made again correctly','Insruction given to programmer to run the NC dat verifier to ensure right toolpath is generated.','Next batch found ok','','2009-06-30','Mahesh.B.T','Girish','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','','yes','','','','0',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(158,'33-011A','Norcot Engineering Limited','HINGE BRACKET 5','253234 B','D576 50008 201','7050 T7651 ABM3 1030','C00',1,'20577','','2619','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Bore over size: Bore measures dia22.225/22.246 measures 22.2560 in one side and chttering mark witnessed.','While doing firstoff part given 0.2 cut for boring bar and this deviation accured.','instruction given to operator to take care while doing boring operation and give only 0.1 max cut on every pass.\r\n','Instruction given to all three operators to give only 0.1 max cut to boring operation on every pass.','Next batch found satisfactory.','','2009-06-30','krishna',' Lokesh B.D','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','','yes','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(159,'33-005','Norcot Engineering Limited','HINGE BRACKET 2','314321 1C1','D576 50005 201','7050 T7651 ABM3 1030','C00',1,'20577','','2478','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Tool dig mark witnessed to a deapth of 3mm at the place of 10mm rib.','While taking work offset in 2 su shank touches the part and dig mark noticed on rib.','Instruction given to operator to take care while taking workoffset.','Instruction given to operator to take care while taking workoffset.','Next batch found satisfactory.','','2009-06-30','krishna','Lokesh B.D','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','','yes','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(160,'33-011A','Norcot Engineering Limited','HINGE BRACKET 5','219242 A','D576 50008 201','7050 T7651 ABM3 1030','C00',1,'20577','','2585','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Bore oversize, dia 22.225/22.246 measures 22.262 in one direction.','While running boring operation power tripped and boring bar repassed then hole hovality coming.','Instruction given to all, If power tripped then take reading backside in boring bar and urjust the bore onceagain. ','Instruction given to all ,If power tripped then take reading backside in boring bar and urjust the bore onceagain. ','Further produced parts found O.K','','2009-07-01','krishna','Lokesh.B.D & Girish Prasad & Srinivas.S.N','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','','yes','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(161,'23-083','Goodrich Aerospace','BRACKET','267892','A400129-801','7075-T651- IAW- AMS-','ECN 63701',2,'CRGL14435-01-09','','2289','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','1) Dig mark observed on the taper surface in 01 no.\r\n2) Rib thickness 2 x .100 +/-.01 at zone D4 measures .0815 on one side.','1),2) In between production 2 parts lifted up fron fixture while machining and above deviation accored.','1),2)Instruction given to operator to clamp properly and once again crosscheck before machining.','1),2)Instruction given to operator to clamp properly and once again crosscheck before machining.','Further produced parts found O.K.','','2009-07-01','Krishna','Ranga Swamy','','0000-00-00','','F8003-S','Rev 0 dt 8/1/2009',0.00,'','Closed','','yes','','','','0',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(162,'18-066A','Magellan Aerospace Bournemouth','ANGLE LOWER F R S - RH','274316','PIL575 53374 201','ABM3 1029 7010','B00',1,'RM365128','','2562','','0000-00-00',NULL,'no','no','yes','no','yes','no','yes','no','no','Tool dig mark witnessed on out side profile (top radius) to a deapth of 10mmx10mm.','while runnig long program in harddisk some time line jumping happen same problem occur for this job.','program splitted and runned for further peices.','program splitted for long programs.','Further produced parts found O.K.','','2009-07-02','Dinakar.G','Lohith.K','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'','Closed','','yes','','','','0',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(163,'23-079','Goodrich Aerospace','EDGE TEE','4464603','7716304-801','7075-T7351 PER AMS 4','ECN 55882',2,'CRGL14435-02-09','','2674','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dimension 0.23\" +/-0.010 zone D3 measures 0.1988 in 01 no. and .2125/.2165 in 01 no.','Dia 20 tipped cutter held in the collet holder loosened and hence thickness got under sized.After observing this deviation in 1st piece tool reloaded and tightened properly but for next piece same deviation occured.','Replaced with a new holder.','That particular holder is scrapped & Replaced with a new holder..','Further produced parts found O.K','','2009-07-03','Pandurang','Manjunath','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(164,'23-087','Goodrich Aerospace','BASE','346231','A800321-812','7050-T7451-IAW-AMS 4','ECN 71642',2,'CRGL14435-03-09','','2589','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','1)Dig mark observed at face at zone F5 in 01 no.\r\n2)Hole position .01(M) A B C meausres .0150 in 01 no.\r\n','1) \r\n2)During production pallet problem accored and part thickness minus side. and this deviation accored.','1)\r\n2)Planned to run only in single pallet without changing the pallet.','pallet servicing done.','CA/PA found satisfactory.','','2009-07-04','Mahesh B T,Krishna','Pandith, Prakash','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(165,'18-120B','Magellan Aerospace Bournemouth','HOUSING OUT B D BRG 3','CB882330','PID275 56121 200','S130','E01, ECN No: NG27011ST1KA83',2,'','','2547','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','1) ID oversize and it\'s 66.675/66.705 measures 66.80 with step mark witnessed in 1no\r\n2) OD undersize dia71.951/71.970 measures 71.920 to 71.932 in 1 no.','Due to jaws run out ovality occured during machining.','Re machined jaws id to get concentric holding.','For the first piece keep in plus side and check it out and maintain the dimension as required.','Further produced parts found O.K.','','2009-07-04','Dinakar.K','Narashima Murthy','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'','Closed','','yes','','','','0',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(166,'18-106A','Magellan Aerospace Bournemouth','EYE END INBOARD','590431','PID575 41542 200','S98','D',2,'RM365154 Amnd 1','','2708','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Bore over size and Dia 31.020+0.025 measures 31.049 to 31.056','while setting boring bar 2 nos rejected.','Instruction given to operator while setting boring bar keep stock and check repeatability.','Instruction given to operator while setting boring bar keep stock and check repeatability','Shall be derived upon next batch production.','','2009-07-04','Dinakar.G','Sunil kumar & thirthappa','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(167,'18-078A','Magellan Aerospace Wrexham','ADAPTOR','256413','A282 50081 200PF',' L111 T6','A',4,'PRP91227 Amendment 1','','2262','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1)Spot space area 2mm tool dig mark noticed in 2no.\r\n2)OD undercut dia 0.1mm undersize in 2no.  ','1)while running tool loosened from the holder.\r\n2)Rework in profile length & undercut program problem.\r\n','1)tool holder changed and instruction given to operator for proper clamping of tool.\r\n2)Program correction given in next peice.','1)1)tool holder changed and instruction given to operator for proper clamping of tool.\r\n\r\n2)Instruction given to Operator to check the size of the undercut','Shall be derived upon next batch production','','2009-07-05','pandurang & Dinakar K','Dinakar K&Naveen','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(168,'18-110A','Magellan Aerospace Bournemouth','FORK END INTERMEDIATE','657212','PID575 40494 202','S80','J',1,'RM365150','','2671','','0000-00-00',NULL,'yes','no','yes','no','yes','no','no','no','no','Thread damage noticed (one full thread chip out)','Due to power failure this deviation occured.','Power failure unknown.','Power failure unknown.','Due to unexpected power failure this deviation has occured.','','2009-07-08','Dinakar.k','Narashima Murthy','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(169,'33-015','Norcot Engineering Limited','JACK BRACKET 2','306191 1A1','D576 50010 201','7050 T7651 ABM3 1030','C00',1,'20577','','2433','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','Tool dig mark noticed to 8x2x30mm in controlled inside slot.','NC Program was done for dia 16 bn but program identified as dia 20F, hence deviation occured.','Instructed programmer to identify the program correctly.','Instructed programmer to identify the program correctly.','Further produced parts found O.K.','','2009-07-08','Mahesh.B.T','Mahesh.B.T','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'','Closed','','yes','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(170,'18-151A','Magellan Aerospace Wrexham','CLEAT','2646401','F572 54614 202 01','ABM3 - 1029','E',3,'RM90864','','2529','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Thickness 2.5 +0.3/-0.2 measures 1.95 to 2.90\r\n','Operator did not butt the job properly, hence this deviation occured.','Instruction given to operator to ensure whether the job is set properly.','Instruction given to operator to ensure whether the job is set properly.','Further produced parts found O.K.','','2009-07-08','Stalin','        Ravindra singh & Suresh','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(171,'18-106A','Magellan Aerospace Bournemouth','EYE END INBOARD','590431','PID575 41542 200','S98','D',1,'RM365154 Amnd 1','','2022','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Bore,thickness,undercut&thread is rust noticed.','rust proof oil not putted due to this rust occured.','instruction given to operator for putting oil after machining.','instruction given to operator for putting oil after machining','','','2009-07-10','Dinakara.G','Mohan kumar.C.M','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(172,'18-247A','Magellan Aerospace Bournemouth','BUTTSTRAP LOW RS4X13600','278831','L575 50179 200','ABM3 1029','A00',1,'RM366521','','2857','','0000-00-00',NULL,'no','yes','yes','yes','no','no','no','no','no','Raw material length undersize by 6mm even though machining operation carried out but part doesnot meet draewing requirement.  ','Neither supervisor nor operator check the required size of RM before loading the part.','Instructed Supervisor & Operator to check the blank preparation size when receiving the material from stores.','Check up with CAD/CAM for correctr size of RM required for producing the part.','Shall be updated upon next batch production.','','2009-07-10','Panduranga','Siddaramappa','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(173,'18-084A','Magellan Aerospace Wrexham','BRACKET SUPPORT','M122420','D579 52008 200 01','L168','C01',1,'RM90861','','2463','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Base thickness 4.0mm measures 3.0mm.','Operator did not take the offset correctly','','Instruction given for operator to take the offset correctly and ensure whether the offset taken is correct','Further produced parts found O.K.','','2009-07-13','Dinakar.G','divakar.s','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(174,'18-083A','Magellan Aerospace Wrexham','STUD PLATE - RH','2933502','D278 50007 201 01','ABM3 1029','D01',2,'RM90860','','2604','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Depth 3.15/3.10 measures 3.25 to 3.23 and also it\'s not reworkable.','Wrong tool offset, 12R0.8 cutter provided was worn and it was replaced and after taking the reference operator forgot to zero the z work offset which was kept for old tool.','Offset corrected and instructed operator to check the wear values and offset values after changing the tool.','Offset corrected and instructed operator to check the wear values and offset values after changing the tool.','Further produced parts found O.K.','','2009-07-13','panduranga','Naveen B S','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(175,'18-078A','Magellan Aerospace Wrexham','ADAPTOR','256413','A282 50081 200PF',' L111 T6','A',2,'PRP91227 Amendment 1','','2685','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Tool dig mark witnessed to a depth of 2mm near to spot face.','Component not tighted properly due to this while runnig component rotated.','Instruction given to operator tighten the clamps properly.','Instruction given to operator tighten the clamps properly.','Further produced parts found O.K.','','2009-07-13','Pandurang','Naveen','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(176,'18-249A','Magellan Aerospace Bournemouth','BUTTSTRAP LOW RS4X500','1591601','PIL575 50181 200','ABM3 1029','A00',1,'RM366521','','2862','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Hole size dia5.60 insted of dia5.10 at 2 places','Drillbit runout caused this deviation.','Instructed to hold the dril bit and ensure there is no runout and then machine the job.','Instructed to hold the dril bit and ensure there is no runout and then machine the job.','Further produced parts found O.K','','2009-07-14','Panduranga','Manjnatha','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(177,'18-209A','Verdict Aerospace Components Ltd.','BODY ASSEMBLY','9866','PID321 40204 202','L168','D',1,'55568','','2703','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Thickness 8.3+/-0.1 measures 8.10 to 8.12 & bore chamfer oversize.','Operator did not take the tool offset properly.','instruction given for operator for taking proper tool offset.','instruction given for operator for taking proper tool offset.','Further produced parts found O.K','','2009-07-17','Dinakar G','Thirthappa','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(178,'18-213A','Verdict Aerospace Components Ltd.','END CAP','48469','PID321 40209 200','L168','A',4,'55568','','2682','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1)Thread damage & thread gauge tight in 1no\'s.\r\n2)4.9 hole oblonged & 4.90 hole 45deg +/-30\' measures 45.70 one side & other side 44.32 in 1 no.  ','1)Drill bit grinding not correct.','Instruction given for operator while putting new drill prove on dummy peice.','Instruction given for operator while putting new drill prove on dummy peice','Further produced parts found O.K','','2009-07-17',' Dinakar G','Thirthappa&mohankumar','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(179,'18-215A','Verdict Aerospace Components Ltd.','ROD END ASSMY - MALE','631551','PID321 53012 200','S98','F01',1,'55568','','2681','','0000-00-00',NULL,'yes','no','yes','no','yes','no','no','no','no','Thrad damage noticed.','Due to power failure thread damage occured.','Sudden power failure unknown','Sudden power failure unknown','Further produced parts found O.K.','','2009-07-19','Dinakar.k','Narashima Murthy','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(180,'35-004','Saab AB','HINGE BRACKET 2','317180 2A1','D576 50005 200','7050 T7651 ABM3 1030','C00',1,'1600028482','','2823','','0000-00-00',NULL,'yes','no','yes','no','yes','no','no','no','no','Slot width 23.09+/-0.03 measures 23.19.','While running production in between 1 no. slot width problem.','It is a machine problem and in under observation. and also inform to machine manufacturer to slove the problem.','It is a machine problem and in under observation. and also inform to machine manufacturer to slove the problem','CA/PA Found satisfactory.','','2009-07-20','Krishna C','Nagaraj Nadiger','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(181,'35-012','Saab AB','JACK BRACKET 1','313443 1B1','D576 50009 200','7050 T7651 ABM3 1030','C00',1,'1600028482','','2897','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Bore Dia 30.163/30.187 measures over size by 30.217','While running boring operation power tripped and again repassed boring cut and bore measures oversize.','Instruction given to operator to if power cut in between boring pass again repassed in stock (take boring bar reading back)and then check the dia then arjust boring bar and finish.','Instruction given to operator to if power cut in between boring pass again repassed in stock (take boring bar reading back)and then check the dia then arjust boring bar and finish.','Further produced parts found O.K','','2009-07-23','Krishna C','Dhanjaya','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(182,'23-042','Goodrich Aerospace','REINFORCEMENT PLATE','57111-1','7712501 815','7075-T6511 / BAC1503','TR IP 7712501-815 REV 02',1,'CRGL14416-02-09','','2808','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Chamfer in zone 1E 0.04 x 0.04/ 0.06 x 0.06 measures 0.1 x 0.1.','Operator not located properly in fixture and this deviation Occured.','Instruction given to operator to take care while loading the part in fixture and once again crosscheck the butting and locating of part.','Instruction given to operator to take care while loading the part in fixture and once again crosscheck the butting and locating of part.','Further produced parts found O.K','','2009-07-24','Krishna C','Nagaraj K S','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(183,'18-091A','Magellan Aerospace Bournemouth','BUSH','659416','PID278 50164 202','S80','A',2,'RM365162 Amnd 1','','2960','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','1)Dig mark noticed on OD to a depth of 1mm.\r\n2)OD ovality & undersize 45.964/45.980 measures 45.954 to 46.02 in 1no.','1)job sliped from the jaws.','1)jaws had re bored for further jobs.','1)for every 50nos once jaws will be re bore and training given to the operetor.','Further produced parts found O.K','','2009-07-28','Dinakar.k','Narashima Murthy & Vikram','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(184,'35-012','Saab AB','JACK BRACKET 1','313443 1B1','D576 50009 200','7050 T7651 ABM3 1030','C00',2,'1600028484','','3013','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Bore: bore dia30.165/.185 measures 30.197 on both sides in one no. 2) tool dig mark noticed to a deapth of 1mm in one side.','1)while running production power fail when taking boring cut and this deviation accured. \r\n2)while running production power fail when taking boring cut and this deviation occured.','1)power fail is not avioded.\r\n2)power fail is not avioded.','1)power fail is not avioded.\r\n2)power fail is not avioded.','Further produced parts found O.K.','','2009-08-03','Krishna(Chowdary.G.P.)','Dhananjaya(N)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(185,'18-107A','Magellan Aerospace Bournemouth','LINK ASSY','112','PID574 50553 200','DTD5014','A',1,'RM358384','','856','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','The required measurment at drawing map reference C4 should measure 6.20mm - 6.35mm but this part actually measures 6.05mm in the middle section only. This has only appeared on qty 1 out of a batch of 30','Compensation error with the tool might have occured for this and in parallel as this particular place as mentioned is assumed to be small, may have slipped the inspector putting the instrument at this area.','100% inspection introduced for this part at the machining stage itself. This was evident with the 200no\'s dispatched subsequently and no such problem was noticed.','same as above.','NEXT BATCH FOUND SATISFACTORY.','C356','2009-08-07','Avinash(R.J.)','Muniyappa(N)','RDN00432','2009-01-07','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(186,'18-176A','Magellan Aerospace Bournemouth','BUSH FLANGED','G7959H3552','PIF321 50037 200','DTD 197','A',3,'RM358210','','703','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','These 10 parts have the helix going in the wrong direction.','1)Drawing misinterpreted.','1)Program changed and correct part were dispatched 2 times.','Instructed Inspector to check the part correctly by interpretation with the drawing before dispatching it to the Customer','NEXT BATCH FOUND SATISFACTORY..','C94','2009-08-07','Avinash(R.J.)','Muniyappa(N)','RDN00446','2009-01-26','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(187,'18-176A','Magellan Aerospace Bournemouth','BUSH FLANGED','G7959H3552','PIF321 50037 200','DTD 197','A',7,'RM358210','','710','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','These 10 parts have the helix going in the wrong direction.','1) Drawing misinterpreted.','1) Programme changed and correct part were dispatched 2 times','Instructed Inspector to check the part correctly by interpretation with the drawing before dispatching it to the Customer ','NEXT BATCH FOUND SATISFACTORY.','C94','2009-08-07','Avinash(R.J.)','Muniyappa(N)','RDN00446','2009-01-26','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(188,'18-060A','Magellan Aerospace Bournemouth','TOP SKIN STIFFENER 3 - LH','8086501','PIL575 53251 200','ABM3 1029','A00',1,'RM358373','','1257','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','Qty 1 part has been identified as having the flange thickness undersize or without fettle allowance incorporated.','flange thickness undersize may the cause for rejection. Request to get the part back for further analysis.','Has introduced 100% inspection of these at all stages to ensure there is no reoccurrence of this','','NEXT BATCH FOUND SATISFACTORY.','C491','2009-08-07','Avinash(R.J.)','Muniyappa(N)','RDN00451','2009-01-29','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(189,'18-160A','Magellan Aerospace Bournemouth','STRUT FWD INNER - RH','A349849','F574 50155 201','J4374','B01',8,'RM365235 Amnd 1','','1398','','0000-00-00',NULL,'yes','no','no','no','no','no','no','yes','yes','Qty 8 parts have been identified as having significant corrosion on the surfaces. we belive that this is due to the packing used (polythene) causing chlorine to leach into the aluminium and corrode the surface.','this is due to the polythene sheet wrapped on to the material first and later the brown sheet instead of only the brown sheet.','The parts shall only be wrapped in the brown sheet provided with the PX24','','NEXT BATCH FOUND SATISFACTORY.','C546','2009-08-07','Avinash(R.J.)','Muniyappa(N)','RDN00464','2009-02-23','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(190,'18-161A','Magellan Aerospace Bournemouth','STRUT AFT INNER - LH','A349853','F574 50156 206 47','J4374','E',3,'RM365294 Amnd 1','','1539','','0000-00-00',NULL,'yes','no','no','no','no','no','no','yes','yes','Qty 8 parts have been identified as having significant corrosion on the surfaces. we belive that this is due to the packing used (polythene) causing chlorine to leach into the aluminium and corrode the surface.','This is due to the polythene sheet wrapped on the material first and later the brown sheet instead of only the brown sheet.','the parts shall only be wrapped in the brown sheet provided with the px24','','NEXT BATCH FOUND SATISFACTORY.','C633','2009-08-07','Avinash(R.J.)','Muniyappa(N)','RDN00465','2009-02-23','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(191,'18-162A','Magellan Aerospace Bournemouth','STRUT AFT INNER - RH','A349853','F574 50156 207 47','J4374','E',4,'RM365294 Amnd 1','','1540','','0000-00-00',NULL,'yes','no','no','no','no','no','no','yes','yes','Qty 4 parts have been identified as having significant corrosion on the surfaces. we belive that this is due to the packing used (polythene) causing chlorine to leach into the aluminium and corrode the surface.','This is due to the polythene sheet wrapped on to the material first and later the brown sheet instead of only the brown sheet','The parts shall only be wrapped in the brown sheet provided with the px24','','NEXT BATCH FOUND SATISFACTORY.','C634','2009-08-07','Avinash(R.J.)','Muniyappa(N)','RDN00466','2009-02-23','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(192,'18-163A','Magellan Aerospace Bournemouth','STRUT MID RIB - LH','A349808','PIF574 50160 200','J4374','B02',8,'RM365238 Amnd 1','','1404','','0000-00-00',NULL,'yes','no','no','no','no','no','no','yes','yes','Qty 8 parts have been identified as having significant corrosion on the surfaces. we belive that this is due to the packing used (polythene) causing chlorine to leach into the aluminium and corrode the surface.','This is due to the polythene sheet wrapped on to the material first and later the brown sheet instead of only the brown sheet.','the parts shall only be wrapped in the brown sheet provided with the px24.','same as above','NEXT BATCH FOUND SATISFACTORY.','C549','2009-08-07','Avinash(R.J.)','Muniyappa(N)','RDN00467','2009-02-23','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(193,'18-164A','Magellan Aerospace Bournemouth','STRUT MID RIB - RH','A349809','PIF574 50160 201','J4374','B02',7,'RM365238 Amnd 1','','1405','','0000-00-00',NULL,'yes','no','no','no','no','no','no','yes','yes','Qty 7 parts have been identified as having significant corrosion on the surfaces. we belive that this is due to the packing used (polythene) causing chlorine to leach into the aluminium and corrode the surface.','this is due to the polythene sheet wrapped on to the material first and later the brown sheet instead of only the brown sheet.','the parts shall only be wrapped in the brown sheet provided with the px24','same as above.','NEXT BATCH FOUND SATISFACTORY.','C550','2009-08-07','Avinash(R.J.)','Muniyappa(N)','RDN00468','2009-02-23','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(194,'18-163A','Magellan Aerospace Bournemouth','STRUT MID RIB - LH','A349809','PIF574 50160 200','J4374','B02',7,'RM365238 Amnd 1','','1541','','0000-00-00',NULL,'yes','no','no','no','no','no','no','yes','yes','Qty 7 parts have been identified as having significant corrosion on the surfaces. we belive that this is due to the packing used (polythene) causing chlorine to leach into the aluminium and corrode the surface.','This is due to the polythene sheet wrapped on to the material first and later the brown sheet instead of only the brown sheet.','The parts shall only be wrapped in the brown sheet provided with the px24','','Next batch found satisfactory.','C635','2009-08-07','Avinash(R.J.)','Muniyappa(N)','RDN00469','2009-02-23','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(195,'18-159A','Magellan Aerospace Bournemouth','STRUT FWD INNER - LH','A349849','F574 50155 200','J4374','B01',1,'RM365235 Amnd 1','','1537','','0000-00-00',NULL,'yes','no','no','no','no','no','no','yes','yes','Qty 1 part have been identified as having significant corrosion on the surfaces. we belive that this is due to the packing used (polythene) causing chlorine to leach into the aluminium and corrode the surface.','This is due to the polythene sheet wrapped on to the material first and later the brown sheet instead of only the brown sheet.','This is due to the polythene sheet wrapped on to the material first and later the brown sheet instead of only the brown sheet.','The parts shall only be wrapped in the brown sheet provided with the px24','Next batch found satisfactory.','C631','2009-08-07','Avinash(R.J.)','Muniyappa(N)','RDN00470','2009-02-23','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(196,'18-160A','Magellan Aerospace Bournemouth','STRUT FWD INNER - RH','A349849','F574 50155 201','J4374','B01',1,'RM365235 Amnd 1','','1538','','0000-00-00',NULL,'no','no','no','no','no','no','no','no','yes','Qty 1 part have been identified as having significant corrosion on the surfaces. we belive that this is due to the packing used (polythene) causing chlorine to leach into the aluminium and corrode the surface.','This is due to the polythene sheet wrapped on to the material first and later the brown sheet instead of only the brown sheet.','The parts shall only be wrapped in the brown sheet provided with the px24','','Next batch found satisfactory.','C632','2009-08-07','Avinash(R.J.)','Muniyappa(N)','RDN00471','2009-02-23','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','no','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(197,'18-159A','Magellan Aerospace Bournemouth','STRUT FWD INNER - LH','A349851','F574 50155 200','J4374','B01',10,'RM365235 Amnd 1','','1397','','0000-00-00',NULL,'no','no','no','no','no','no','no','no','yes','Qty 10 parts have been identified as having significant corrosion on the surfaces. we belive that this is due to the packing used (polythene) causing chlorine to leach into the aluminium and corrode the surface.','This is due to the polythene sheet wrapped on to the material first and later the brown sheet instead of only the brown sheet.','The parts shall only be wrapped in the brown sheet provided with the px24','','Next batch found satisfactory.','C545','2009-08-07','Avinash(R.J.)','Muniyappa(N)','RDN00463','2009-02-23','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(198,'28-017','Ellanef Manufacturing Corporation','LOWER LINK UNASSEMBLED','93218','161W6005 2','PER BMS 7-240 TYPE-I','B',3,'100581 Rel-0','','3110','','0000-00-00',NULL,'no','no','yes','no','yes','no','yes','no','no','1) Bore Diameter .8125/.8132 measures .8162 in 01 nunber,.8148 in 01 number.\r\n2)Dig mark observed in the pocket.','due to m/c problem (tool offset was getting altered for each piece) 3 nos were rejected.','informed to BFW service person for service m/c.','BFW has corrected the root cause by altering the necessary parameters in the machine.   ','CA/PA Found satisfactory.','','2009-08-07','Dinakara(G)','Nagaraj(G. Nadiger)','','0000-00-00','one no. rejected by Basavaraj (S jr) but it is also m/c problem.','F8003-S','Rev 0 dt 8-1-2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(199,'23-119','Goodrich Aerospace','PROFILE D','4772777','A872316-8206','7055 T76511','ECN 89524',2,'CRGL14435-03-09','','2204','','0000-00-00',NULL,'yes','no','no','no','no','no','no','yes','yes','Parts were damaged before chemical finish was applied.','1)While handling the part damage may have occured.\r\n2) Visual inspection not carriedout properly.','1) parts will be handeled properly and visual inspection will be improved.','same as above','CA/PA Found satisfactory.','C1319','2009-08-07','Avinash.R.J','Pradeep Kumar','QN-4138267','2009-07-31','','F8003-S','Rev 0 dt 8-1-2009',0.00,'','Closed','yes','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(200,'18-119A','Magellan Aerospace Bournemouth','HOUSING OUT B D BRG 3','CB894702','PID275 40011 200','S130','D01',1,'RM365160 Amnd 1','','2928','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dig mark on ID undercut 5 deg angle.','The rejection happened while attempting to take out the job from the fixture. Instead of removing the fixture to get the job release, the operator deviated from this procedure by using unconventional method and thus resulting in rejection.','Instructed the operator to follow the standard removal procedure','A standard work instruction shall be prepared to avoid recurrence. ','CA/PA Found satisfactory.','','2009-08-09','Dinakara(G)','Sunil(Kumar K.R.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(201,'18-123A','Magellan Aerospace Bournemouth','FORK END OUT BD','697907','PID575 41546 202','S80','B',4,'RM365147 Amnd 1','','2959','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1)Bore oversize dia 11.000+0.018 measures 11.023to11.026 in 2nos.\r\n2)Thickness undersize drawing dim 18+0.3/-0.2 measures 17.10 in 1no.\r\n3)Tool dig mark on radius profile at 3.mm depth in 1no. ','1) stock not checked at regular intervals.\r\n2) seating of insert not done properly. \r\n3) while running component rotated.','1) Changes in the quality plan in process sheet to check the stock at defined intervals .\r\n2) instruction given for operator proper seating of insert.\r\n3) instruction given for operator for proper tight.','1) instruction given for operator stock checking at regular intervals.\r\n2) instruction given to operator to ensure proper seeting of insert.\r\n3) instruction given to operator to ensure for proper tightness of the job in the fixture.','CA/PA Found satisfactory.','','2009-08-09','Dinakara(G)','Mohan(Kumar C.M.)','','0000-00-00','Sunil Kumar K.R and Mohan kumar also responsible because it rejected in final inspection.','F8003-S','Rev 0 dt 8-1-2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(202,'18-121A','Magellan Aerospace Bournemouth','BARREL - STRUT','583915','PID572 50463 201','S98','F',7,' RM365136 Amnd 1','','2867','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dia 4.90 holes center shift 0.3mm & pin not entered through.','The information to check this parameter is missing in the process sheet. Based on the other information given in the process sheet, first off clearence was given. With regard to the process deviation, setting not done properly.','Resetting done and next peices were found ok.','Instructed the operator to set the job properly.','NEXT BATCH FOUND.\r\n','','2009-08-09','Dinakara(G)','Theerthappa(K.N.)','','0000-00-00','inspector Nandish kumar K not inspected first off properly due to this 7 Nos. rejected.','F8003-S','Rev 0 dt 8-1-2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(203,'18-107A','Magellan Aerospace Bournemouth','LINK ASSY','1243','PID574 50553 200','DTD5014','A',6,'RM365142 Amnd 1','','2663','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','1)OD undersize 6.20/6.35 measures 5.80 & step observed in 3no.\r\n2)chf 0.5x45 deg oblong in 1no.\r\n3)Bore oversize 15.870+0.015 measures 15.888 to 15.891 in 2no.','2) tool offset not taken properly. The tool was offset by 0.5 mm unnecessarily by operator who assumed that the tool was a double sided chamfer tool while the actual tool insert issued was single sided chamfer tool.\r\n3) while proving new reamer 2 nos. rej','2) instruction given for operator for taking proper tool offset and has been warned to run the program as per the instructions.\r\n3) Reamer proved and next peices found ok.','2) Pre setter implemented.\r\n3) The reamer shall be proved on dummy material with similar charecteristics as that of the job thus reducing the possibilities of rejections on original material.\r\n\r\n','CA/PA Found satisfactory.','','2009-08-09','Dinakara(G)','Mohan(Kumar C.M.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(204,'18-121A','Magellan Aerospace Bournemouth','BARREL - STRUT','583915','PID572 50463 201','S98','F',2,' RM365136 Amnd 1','','2866','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1)Thread gauge Nogo answered in 1 no.\r\n2)Dia 1.5mm hole oversize & oblong in 1no.','1) Thread was damaged due to wear out of inserts. The operator intended to rework the damaged thread resulting in non conformance of ID.\r\n2) HSS drill was not properly ground.','1)Insert was worn out at that stage which was replaced for the next job.\r\n2) Drill was replaced.','1) The block holding the tool shall be set by the Supervisor for every batch which is expected to extend the tool life and reduce these type of non conformances.\r\n2) Henceforth, drills shall be proved on dummy blocks before cutting on the actual material.','NEXT BATCH FOUND.\r\n','','2009-08-09','Dinakar(K)','Paramesh(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(205,'18-117A','Magellan Aerospace Bournemouth','HOUSING-OUT BD BRG','662385','PID275 40004 200','S130','C01',1,'RM365157','','2860','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','OD undersize 69.950/69.970 measures 69.920 to 69.950\r\n','The OD was in plus side (ovality). At the time of production, the jobs when inspected by QC were within acceptable limits. However during final inspection, ovality was notices on may pieces. This perticular job got rejected while re-working.','for further pieces the required tolerance was maintained.','Engineering / QC to advice. ','CA/PA Found satisfatory.','','2009-08-09','Dinakar(K)','Vikram(E)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(206,'18-104A','Magellan Aerospace Bournemouth','BODY TURNBUCKLE','027952','PID575 40490 200','S80','E',1,'RM365144 Amnd 1','','2874','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Thread gauge Nogo answered LH side.\r\n','Threading insert broken while running so nogo gauge answered.','Insert changed for next piece. ','for every 20no\'s inserts will be checked. QC needs to advice which charecteristic of the thread has deviated.','CA/PA Found satisfactory.','','2009-08-09','Dinakar(K)','Paramesh(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(207,'18-105A','Magellan Aerospace Bournemouth','FORKEND ASSEMBLY','590431','PID572 50462 200','S98','J01',2,'RM365139 Amnd 1','','2177','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Bore oversize 14.308+0.018 measures 14.328 to 14.335.','The probable reason for this rejection might be due to wrong setting of the inserts in the boring bar.','The rest of the parts in this batch have been found to conforming to the actual requirement after correcting the setting.','Training program has been initiated to avoid recurrence.','CA/PA Found satisfactory.','','2009-08-09','Dinakara(G)','Sunil(Kumar K.R.)','','0000-00-00','Other probable operators: Thirthappa K N, Mohan kumar C M','F8003-S','Rev 0 dt 8-1-2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(208,'18-111A','Magellan Aerospace Bournemouth','BODY TURNBUCKLE INTMD','686194','PID575 41544 200','S80','A',1,'RM365149 Amnd 1','','2709','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Tool dig mark on radius profile & inside slot.','Dia 12 end mill got cut while performing the operation.','Replaced the tool with a new cutter. Rest of the parts in the batch have been found conforming.','The end mill has been now replace with insert head type tool which should reduce this type of non conformance.','CA/PA Found satisfactory.','','2009-08-09','Dinakara(G)','Theerthappa(K.N.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(209,'18-108A','Magellan Aerospace Bournemouth','FORK END OUT BD','690634','PID575 41546 200','S80','B',4,'RM365147 Amnd 1','','2664','','0000-00-00',NULL,'yes','no','no','no','yes','yes','no','no','no','Bore oversize 11.00+0.018 measures 11.024 to 11.035','Spindle bearing had worn out.','Replaced the bearings with new ones.','Replaced the bearings with new ones.','CA/PA Found satisfactory.','','2009-08-09','Dinakara(G)','Dinakara(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(210,'18-112A','Magellan Aerospace Bournemouth','BODY TURNBUCKLE INNER','686194','PID575 41541 200','S80','A',1,'RM365153 Amnd 1','','2710','','0000-00-00',NULL,'yes','no','yes','no','yes','no','no','no','no','Bore oversize 12.70+0.018 measures 12.743','Spindle bearings had worn out.','Replaced the spindle bearings with new one.','Replaced the spindle bearings with new one.','CA/PA Found satisfactory.','','2009-08-09','Dinakara(G)','Dinakara(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(211,'18-105A','Magellan Aerospace Bournemouth','FORKEND ASSEMBLY','590431','PID572 50462 200','S98','J01',1,'RM365139 Amnd 1','','2667','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Bore oversize 15.895+0.018 measures 15.928','The boring  tool was not set correctly by the operator','Instructed the operator to set the boring tool correctly','Instructed Operator to Check the bore with a semifinish cut and then measure and finally give the final finish cut. ','Further produced parts found OK','','2009-08-09','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(212,'18-122A','Magellan Aerospace Bournemouth','FORKEND ASSEMBLY','723001','PID572 50462 201','S98 FHT','J01',11,'RM365139 Amnd 1','','3056','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','1)Total length undersize 1.2mm in 9nos & thread effective dia undersize Nominal Dim 13.053/13.134 measures 12.99 to 13.0 in 1no.\r\n2)14.287 Bore chamfer oversize Drg Dim 0.45/0.65 x45deg measures 1.02 to 1.06 in 1no.','1)Operator did not take the tool offset correctly\r\n2) wrong radius offset given','1)Instructed Operator to take the work offset correctly\r\n2)Instructed Operator to enter the radius offset correctly','1)Instructed Operator to take the work offset correctly\r\n2)Instructed Operator to enter the radius offset correctly','Further produced parts found OK','','2009-08-10','Dinakar(K)','Narasimha(Murthy R)','','0000-00-00','Supervisor name:Dinakar G & Dinakar K \r\nNote:Production supervisor select the correct operator name','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(213,'18-176A','Magellan Aerospace Bournemouth','BUSH FLANGED','0804401257','PIF321 50037 200','DTD 197','A',1,'RM365319 Amendment 1','','2868','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','ID oversize out of tolerance 20 microns.','Improper bore setting','Boring bar was reset in minus side and next pieces in the batch were found conforming.','for further batches, bore setting will be taken in minus side.','CA/PA Found satisfactory.','','2009-08-10','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(214,'35-012','Saab AB','JACK BRACKET 1','313443 1B1','D576 50009 200','7050 T7651 ABM3 1030','C00',1,'1600028482','','2897','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','2nd time NCR raised. NCR no.00181','same as NCR no.00181','same as NCR no.00181','same as NCR no.00181','refer 00181','','2009-08-10','Krishna(Chowdary.G.P.)','Dhananjaya(N)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(215,'30-019','Gardner Aerospace Burnley Limited','PANEL UNDERWING LH','8043501 1','L575 58277 200','ABM3 1029','A00, ECN:PG64785001JA38',2,'PRO0015262','','2076','','0000-00-00',NULL,'yes','no','no','no','no','no','no','yes','yes','2 off countersinks have been produced at the wrong angle,should be 100 degrees','Supplied model was not with countersink holes. These holes were added with the given co-ordinates. Since these are at three-dimensional surface, error occured during validation & not noticed. Same model transferred to QC and hence got accepted in final in','Reworked at Gardner, Burnley, UK.','Model corrected, validated.  Re-FAIR to this extent shall be carried out in next batch and detail report shall be submitted','CA / PA Found satisfacory.','C1198','2009-08-10','Avinash R J','Prakash C B','2009/10','2009-08-10','','F8003-S','Rev 0 dt 8-1-2009',0.00,'','Closed','yes','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(216,'34-024','BRISTOL AEROSPACE LIMITED','STRUT PLUG R.H. THREAD','8090595','400-12615-2-905','4130 Bar Stock per M','',1,'B70996','','2639','','0000-00-00',NULL,'yes','no','no','no','no','yes','no','yes','no','Dimension 1.85 +/-.03 measures 1.8132.','Program mistake','Corrected the program','Instructed the programmer to check the program before using it on the part','Further produced parts found OK','','2009-08-11','Mahesh(B.T.)','GIREESH.K.(KULKARNI)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(217,'34-024','BRISTOL AEROSPACE LIMITED','STRUT PLUG R.H. THREAD','8090595','400-12615-2-905','4130 Bar Stock per M','',1,'B70996','','2639','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Dimension .630/.635 measures .6355.','Carbide boring tool was used to carry out ID turning. The tool that was pre-grinded was used to machine the part. It was later found that the corner radius was not checked and a wrong tool offset was entered assuming a different value.','The tool radius shall be input after inspecting the corner radius on the profile projector prior to machining the next batch.','Instruction has been put in the NC program to check the corner radius on the profile projector before entering the tool offset.','CA/PA Found satisfactory.','','2009-08-11','Dinakar(K)','Rajesh(T)','','0000-00-00','First Article','F8003-S','Rev 0 dt 8-1-2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(218,'18-083A','Magellan Aerospace Wrexham','STUD PLATE - RH','2933502','D278 50007 201 01','ABM3 1029','D01',3,'RM90860','','3096','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','Thickness 6.95/7.05 measures 6.85 to 6.90 locally.','Due to problem in method of clamping, the non conformance resulted.','The clamps have been replaced with changes in design to ensure bend piece butts properly.','Same as corrective action.','CA/PA Found satisfactory.','','2009-08-13','Dinakara(G)','Diwakar(S)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(219,'18-075A','Magellan Aerospace Wrexham','ADAPTOR','18882/011','D282 50044 200PF',' L111 T6','A',1,'PRP91227 Amendment 1','','3184','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','First peice program prooved 1no rejection& undercut dia undersize 0.04,threads chattering observed.','while prooving new program 1st piece rejected.','for next piece program corrected and next piece found ok.','The program is freezed and a back up has been taken.','CA/PA Found satisfactory.','','2009-08-19','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(220,'18-082A','Magellan Aerospace Wrexham','STUD PLATE - LH','0141302','D278 50007 200 01','ABM3 1029','D01',1,'RM90860','','2601','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Slot width over size 13.75/14.0 measures 14.90 & radius groove shifted.','CRC not properly entered by the operator.','Correct CRC value was entered and first off was proved.','Operator was warned not to repeat mistake of this nature.','CA/PA Found satisfactory.','','2009-08-19','Panduranga(G)','Naveen(B.S.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(221,'18-078A','Magellan Aerospace Wrexham','ADAPTOR','18883/012','A282 50081 200PF',' L111 T6','A',1,'PRP91227 Amendment 1','','3090','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Total length & width undersize in 1mm per side.','Operator who was supposed to enter 2 CRC values (D1 and D2), entered only one value which resulted in rejection of the component.','CRC values were entered later which resulted in obtaining conforming parts.','Message will be incorporated in the program to prompt input of both the CRC values.','CA/PA Found satisfactory.','','2009-08-19','Dinakara(G)','Lohith(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(222,'18-002A','Magellan Aerospace Wrexham','BRACKET SUPPORT - RH','719228A9','D361 50110 201 01','ABM3 - 1029','A',1,'RM90857','','2938','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Tool dig mark on dia7.937/7.959 near the bore in 2mm depth.','Tool broken during machining','Changed a new tool','Instructed Operator to check the sharpness of the tool periodically','Further produced parts found OK','','2009-08-19','Dinakara(G)','Girish(Prasad P)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(223,'18-077A','Magellan Aerospace Wrexham','COUPLING','18011/011','D282 50075 200PF',' L111 T6','A',1,'PRP91020 Amendment 1','','3008','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Total length 23.0+/-0.3 measures 22.50 to 23.22.','Operator has errored in giving the work offset.','Work offset was input for the second which has resulted in obtaining conforming parts.','Online training imparted on the operator to help avoid these kind of mistakes.','CA/ PA FOUND SATISFACTORY','','2009-08-19','Dinakar(K)','Nithin(S)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(224,'18-076A','Magellan Aerospace Wrexham','COUPLING','3259181','D282 50074 200PF',' L111 T6','A',1,'PRP91227 Amendment 1','','2890','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Tool dig mark on OD & face in 5mm depth.','while running job slipped from the jaws which might be result of excessive cutting parameters','For next piece, jaws were  bored and further operations were continued.','Cutting parameters have been reduced. ','CA/PA Found satisfactory','','2009-08-19','Dinakar(K)','Ramesh(S. Bandagi)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(225,'18-202A','Magellan Aerospace Wrexham','ANGLE CLEAT','351118A5','D572 59281 200 01','ABM3 - 1029','A',5,'RM90868','','3106','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','1)Raw material thickness undersize machining not done in 5nos.','Dimensions are not consistent as the process requires change in fixtures and programs.','Re-engineering in progress.','Re-engineering in progress.','After Re-Engineering parts found satisfactory.','','2009-08-20','Panduranga(G)','Siddaramappa()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(226,'18-197A','Magellan Aerospace Wrexham','ANGLE CLEAT','2709501','D572 59284 200 01','ABM3 - 1029','A',18,'RM90868','','3103','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1)Thickness u/s 5.60+0.3/-0.2 measures 5.25 to 5.30 in 7nos.\r\n2)Hole pitch oversize 72 +/-0.3 measures 72.60 in 11nos.','Dimensions are not consistent as the process requires change in fixtures and programs.','Re-engineering in progress. ','Re-engineering in progress. ','Further batch found ok.','','2009-08-20','Panduranga(G)','Siddaramappa()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(227,'18-198A','Magellan Aerospace Wrexham','ANGLE CLEAT','2709501','D572 59283 200 01','ABM3 - 1029','A',4,'RM90868','','3104','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Hole pitch undersize 22+/-0.3 measures 22.58 to 22.60 & 71+/-0.3 measures 70.60.','Dimensions are not consistent as the process requires change in fixtures and programs.','Re-engineering in progress.','Re-engineering in progress.','Further produced parts were found O.K','','2009-08-20','Panduranga(G)','Siddaramappa()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(228,'18-078A','Magellan Aerospace Wrexham','ADAPTOR','18883/012','A282 50081 200PF',' L111 T6','A',1,'PRP91227 Amendment 1','','2997','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Tool dig mark on near the spot space in 3mm depth.','After the electric power failed and returned, the operator had to ensure that the tool be carefully withdrawn away from the job which he failed to do.','Operator instructed to follow the standard procedure in these type of situations.','Same as above.','Next part found satisfactory.','','2009-08-20','Dinakara(G)','Sathish(Y.R.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(229,'18-088A','Magellan Aerospace Wrexham','PLATE SEALING','025962/001','D572 52998 200 01','ABM3 1029','A',2,'RM90859','','3010','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Tool dig mark on OD in 2 to 4mm depth.','Operator has butt the raw material which is a deviation from the instructions given in the process sheet. In other words, wrong clamping has tken place.','The problem analyzed by the supervisor who demonstrated the proper way of clamping the job. Further pieces were found conforming to the limits.','Training given to the operator on clamping method.','CA/PA Found satisfactory.','','2009-08-20','Dinakar(K)','Manjunath(K.N.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(230,'23-032','Goodrich Aerospace','REINFORCEMENT PLATE','57110-1','7712500-80053','7075-T6511 IAW AMS-Q','TR IP 7712500-80053 REV 01',1,'CRGL14416-03-09','','3156','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Rib thickness undersize 0.122/0.142 measures 0.1078 to 0.1314.','Clamps were bent due to which it was not possible to constain the job\'s movement properly.','New clamps were manufactured and are currently in use. No non conformance has occured since then.','Washers have been introduced on the clamping process to avoid recurrence.','CA/PA Found satisfactory.','','2009-08-20','Krishna(Chowdary.G.P.)','Prakash(Acharya)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(231,'28-007','Ellanef Manufacturing Corporation','SHAFT SUPPORT/LEVER','93034','251A1747-1','6Al-4V per MIL-T-904','N/C',5,'99457 Rel-1','','2942','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Dimension Ø .7494/.7497 measures Ø .7483/.7490 in 05 nos.','Probable reasons are:\r\n1)while running, piece turned due to insufficient clamping force.\r\n2) Dry run period might have been short.','Turning pass program has been altered which incorporates extended dry run period.','Turning pass program has been altered which incorporates extended dry run period.','CA/PA Found satisfactory.','','2009-08-21','Dinakar(K)','Vikram(E)','','0000-00-00','vikram.e and narshimamurthy.r','F8003-S','Rev 0 dt 8-1-2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(232,'28-003','Ellanef Manufacturing Corporation','PIN-ATTACHMENT WALKING BE','92668','161A7305-1','15-5PH per AMS5659','PL-Rev-NC, PSDL Rev-A, APO 28-003 Rev-0',1,'99574 Ch-4 Rel-1','','2912','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Dimension Ø 1.1160/1.1180 measures Ø 1.1185/1.1194 in 01 no.','The impact was due to milling operation that was carried out after turning which resulted in this deviation.','Sufficient stock is being left along ID and is cleared in the final operation after milling.','The process has been corrected to avoid recurrance.','CA/PA Found satisfactory.','','2009-08-21','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(233,'30-030','Gardner Aerospace Burnley Limited','PANEL UNDERWING RH','8043501 1','L575 58278 200','ABM3 1029','A00, ECN:PG64785001JA37',3,'PRO0016034-S7','','2838','','0000-00-00',NULL,'yes','no','no','no','no','no','no','yes','yes','1)three off parts received with the outer face of component not polished leaving machine lines evident and also causing the countersinks to be too deep.\r\n2) the squre cut outs in vertical flanges are being left with sharp edges.','We did not perform the polishing operation as drawing calls machined features to be per ABP 6-3345 which states that 0.13 surface mismatch is acceptable and surface finish 3.2 was met.','1) the part will be polished in the mentioned area.\r\n2) Re-FAI will be submitted in the next batch.','1) Same information will be incorporated in the process sheet.','next batch found satisfacory.','C1600','2009-08-26','Avinash.R.J','Prakash.C.B','2009/11/12','2009-08-22','','F8003-S','Rev 0 dt 8-1-2009',0.00,'','Closed','yes','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(234,'30-035','Gardner Aerospace Burnley Limited','RIB 1 OFW - LH','722726A7','L575 41326 200','ABM3 1029','A, ECN:PG69050001JA03',2,'','','3249','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','Tool dig mark noticed to a deapth of 2mm at the end of cone.','while running dia 16f cutout program, at last pass extra material getting vibrated to avoide this,operator given manual cut.','instruction given to every operator that they should not edit or run the manual programs.as well as instruction sheet attached to the every machine.','Instead of dia 16F outer cut-out program,Dia 12F new program introduced.','ca pa foundsatisfactory.','','2009-08-26','Siddalinga(Tambake)','Gajendra Singh(C.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(235,'23-075','Goodrich Aerospace','EDGE TEE','266218','7716204-801','7075-T7351 PER AMS 4','ECN 55818',1,'CRGL14435-02-09','','3319','','0000-00-00',NULL,'yes','no','yes','no','yes','no','no','no','no','Dimension .160+/-0.01\" in zone 2c-2,measures 0.1442.','While running production dia 6 ballnose cutter offset down and runned prg then this deviation accured.','Every tool offset checked at every tool change and completed production.','Instruction given to maintance dept. and also machine manufacturer to slove the problem.','CA/PA Found satisfactory.','','2009-08-28','Krishna(Chowdary.G.P.)','Diwakar(R.B.)','','0000-00-00','Superviser name:krishna c','F8003-S','Rev 0 dt 8-1-2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(236,'18-111A','Magellan Aerospace Bournemouth','BODY TURNBUCKLE INTMD','686194','PID575 41544 200','S80','A',43,'RM365149 Amnd 1','','2709','','2009-08-05',NULL,'yes','yes','no','no','no','no','no','no','yes','A qty of 43 parts have been identified as having the    3/4-16 UNJF 3B internal thread oversize(Fails on \'No Go\'of screw plug gauge). These parts cannot be reworked.\r\nCim Batch No:686194\r\nCim WO No:2709\r\n\r\n','Since this did have passed our inspection, it appers the problem with the checking gauge with us.','The gauge was scrapped & replaced with new one.','Procedure to check the gauge with 3-pin method introduced. Separate gauges for production & final inspection made available & in control of QC. Each time gauge drawn to be checked with the 3-pin method & to ascertain the values before using.','Next batch found satisfactory.','C1721','2009-08-28','Avinash(R.J.)','Muniyappa(N)','RDN 00558','2009-08-27','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(237,'18-111A','Magellan Aerospace Bournemouth','BODY TURNBUCKLE INTMD','686194','PID575 41544 200','S80','A',39,'RM365149 Amnd 1','','2709','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Internal thread 3/4-16 UNJF 3B thread gauge \'No Go\'answered.','Part not clamp correctly,while threading part might be shake.','For next part clamping method is corrected.','In future will be taken care.','CA/PA Found satisfactory','','2009-08-28','Dinakar(K)','Paramesh(K)','','0000-00-00','Supervisor Name:Dinakar K\r\nOperator Name:Paramesh K & Ramesh S Bandagi.','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(238,'18-283A','Magellan Aerospace Bournemouth','FUNK PINS','583915','PIA572 43263 202','S98','H',1,'RM368853','','2734','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dimension .7454/.7470\" measures .7430\"(18.88mm) in 01 no.','Due to insert wear out.','For next part insert changed.','Before starting the operation will cross check inserts.','CA/PA Found satisfactory.','','2009-08-28','Dinakar(K)','Nithin(S)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(239,'18-006A','Magellan Aerospace Wrexham','COVER PLATE','270132/051','D572 52516 200 01','L97 - T351','A',1,'rm90854','','3209','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Rib thickness 1.00mm undersize as per drawing dimensions.','Wrong tool was loaded by the operator assuming that only CRC program existed while the program actually consisted of both CRC and centreline.','Request to provide program consisting of only CRC program has been made.','Care shall be taken to avoid to club both centreline and CRC program during genaration of NC programs.','CA/PA Found satisfactory.','','2009-08-29','Dinakara(G)','Diwakar(S)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(240,'18-210A','Verdict Aerospace Components Ltd.','BODY ASSEMBLY','9866','PID321 40204 204','L168','D',3,'55568','','3174','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Bore dia 19.0 +0.021 measures 19.022 to 19.025.','Due to wrong adjustment in boring bar.','next part adjusted & cross check several times backclase of the boring bar.','In future will be taken care.','','','2009-08-29','Dinakara(G)','Sunil(Kumar K.R.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(241,'23-093','Goodrich Aerospace','FITTING','714993A3','A806819-801','7050 T7451 AMS 4050','ECN 83059',1,'CRGL14435-03-09','','2016','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Hole diameter 0.93/0.1030 zone D13 measures 0.1130','While doing firstoff, the operator loaded the drill in drill chuck without checking the runout in drill chuck.','Runout corrected and drilled in dummy block and then all holes have come within permissible limits.','Instruction given to operator to check the drill runout and also drill and check in dummy block each time while loading the drill in the chuck.','CA/PA Found satisfactory.','','2009-08-29','Krishna(Chowdary.G.P.)','Naveen(B.S.)','','0000-00-00','sup:krishna','F8003-S','Rev 0 dt 8-1-2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(242,'35-002','Saab AB','HINGE BRACKET 1','317180 1A1','D576 50004 000 01','7050 T7651 ABM3 1030','C00',1,'1600028484','','3069','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Bore Diameter:dia22.225+0.021 measures dia22.40','While running in production power fail in between boring cut and repassed again and this deviation occured.','Instruction given to operator not to re-pass the cut when power fails.','In these cases, the part will be finished in jig boring machine.','CA/PA Found satisfactory.','','2009-08-29','Krishna(Chowdary.G.P.)','Lokesh(B.D.)','','0000-00-00','sup:krishna','F8003-S','Rev 0 dt 8-1-2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(243,'35-008','Saab AB','HINGE BRACKET 4','317180 1A1','D576 50007 000 01','7050 T7651 ABM3 1030','D00',1,'1600028485','','3077','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Slot Width: 23.09+/-0.03 measures 23.155 to 23.162','yet to be filled, due to problem under observation.','yet to be filled, due to problem under observation.','yet to be filled, due to problem under observation.','Please review the CA/PA/ROOT CAUSE','','2009-09-01','Krishna(Chowdary.G.P.)','Nagaraj(G. Nadiger)','','0000-00-00','sup:krishna chowdry','F8003-S','Rev 0 dt 8-1-2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(244,'23-077','Goodrich Aerospace','EDGE TEE','4464601','7716254-801','7075-T7351 PER AMS 4','ECN 55880',1,'CRGL14435-02-09','','3358','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dimension .160+/-.01\" in zone 2B2 measures .140.','Due to cutter problem,while running tool getted down.','For next part cross check the tool compansation.','Same as above.','CA/PA Found satisfactory.','','2009-09-02','Krishna(Chowdary.G.P.)','Nagaraju(K.S.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(245,'23-060','Goodrich Aerospace','BASE ASSY','20107961','7718152-815','7075 T73511 AMS QQ-A','ECN 102246 (3 Sheets)',3,'CRGL14435-01-09','','3316','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Dimension .2550/.2650\" measures .2680\" in 03 nos.','Operator not entered the correct offset in the machine','corrected the entry in the machine for correct offset','Instructed Operator to take care while entering offsets in machine','Further produced parts found OK','','2009-09-03','Krishna(Chowdary.G.P.)','S. Shiva(Kumar)','','0000-00-00','Supervisor-Krishna C','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(246,'18-279A','Verdict Aerospace Components Ltd.','DOOR OUTER TYPE 23','255971B','PIL572 53721 200','ABS 5032 A055','B00',1,'','','3324','','0000-00-00',NULL,'yes','no','no','no','no','yes','no','yes','no','CSK dia 12.90/13.06 (22 holes) out of tolerance 9 holes measures 13.13 to 13.65','Due to method.presently we don\'t have counter sink gauge to check the counter sink depth.','To avoid this problem made a simple counter sink pin gauge.\r\nAs well as changed the process.','In future over come this problem,ordered counter sink depth gauge.','Next batch found satisfactory.','','2009-09-05','Tharanj R(Pandit)','Krishna(Chowdary.G.P.)','','0000-00-00','Operator:Stalin & Jayaram','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(247,'18-121A','Magellan Aerospace Bournemouth','BARREL - STRUT','583915','PID572 50463 201','S98','F',2,' RM365136 Amnd 1','','2866','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1)Thread gauge Nogo answered in 1 no.\r\n2)Dia 1.5mm hole oversize & oblong in 1no.','1)while thread running insert broken so nogo gauge answered.','1)furthre inset change for next piece. ','1)for every 20no\'s inserts will be checked. ','NEXT BATCH FOUND.\r\n','','2009-09-09','Dinakar(K)','Narasimha(Murthy R)','','0000-00-00','Supervisor Name:Dinakar K & Dinakar G\r\nOperator Name:','F8003-S','Rev 0 dt 8-1-2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(248,'18-194A','Magellan Aerospace Wrexham','M/C BRACKET','158385','D572 59092 200 01','ABM3 - 1029','A',8,'RM90866','','3410','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','hole pitch 19.0 measures 18.61/18.63 and 45.0 measures 44.62/44.64 ','Wrong work offset taken','corrected the work offset','Instructed Operator to take the offset correctly','Further produced parts found OK','','2009-09-11','Dinakara(G)','Theerthappa(K.N.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(249,'23-029','Goodrich Aerospace','REINFORCEMENT PLATE','266583','7712500 8106','7075 T651 AMS-QQ-A-2','TR IP 7712500-8106 REV 01',1,'CRGL14416-04-09','','3395','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Dimension dia 0.2500/0.2540 measures 0.2550(6.48) in one hole.','Tool was having runout','Held the tool properly without runout','Instructed the Operator to hold the tool properly without runout','Further produced parts found OK','','2009-09-14','Krishna(Chowdary.G.P.)','S. Shiva(Kumar)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(250,'23-032','Goodrich Aerospace','REINFORCEMENT PLATE','57110-1','7712500-80053','7075-T6511 IAW AMS-Q','TR IP 7712500-80053 REV 01',16,'CRGL14416-03-09','','3156','','0000-00-00',NULL,'no','yes','no','no','no','no','yes','no','yes','The parts dispatched are not 7712500-80053 and are some other parts.','A possibility might be that the paperwork might have got mixed up while packing.','An inspection stage has been set up after the parts are packed to ensure availability of correct paperwork pertaining to the parts','The corrective action has been implemented on all the parts on order from Goodrich Cargo.It has been agreed to monitor the corrective action taken from the date of receipt of this complaint. A member each from packing and QC has been assigned to ensure conformance to the expectations and the chief Customer contact shall evaluate the effectiveness. \r\n\r\n','CA/PA Found satisfactory.','C1836','2009-09-17','Ashoka()','Raghu(J)','3005455','2009-09-11','','F8003-S','Rev 0 dt 8-1-2009',0.00,'','Closed','yes','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(251,'35-012','Saab AB','JACK BRACKET 1','313443 1B1','D576 50009 200','7050 T7651 ABM3 1030','C00',1,'1600028482','','2897','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','3rd time NCR raised.','same as NCR no.00181\r\n\r\n','same as NCR no.00181','same as NCR no.00181','Refer 00181','','2009-09-17','Krishna(Chowdary.G.P.)','Dhananjaya(N)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(252,'18-068A','Magellan Aerospace Bournemouth','ANGLE SHROUD ATCH MID UPR','227734','PIL575 55179 201','ABM3 1029','A00',1,'RM365128','','3235','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Thickness undersize,Drg Dim 8.0+0.3/-0.2 measures 7.60 to 7.80','Refer NC number 00253','Refer NC number 00253','Refer NC number 00253','Next production batch found ok.','','2009-09-18','Dinakara(G)','Lohith(K)','','0000-00-00','Note:Production supervisor select the correct operator name.','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(253,'18-225A','Magellan Aerospace Bournemouth','CLAMP BLOCK','2319316','D282 50123 204','NYLON 66','A',4,'RM366515','','3348','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1)Tool dig mark on 12.7 hole in 3nos.\r\n2)Total length undersize in 0.6mm in 1no.','1)Wrong selection of the drill,drill were chip out.\r\n2)Due to wrong CRC given,instead of dia 12 operator given dia 11.7.','1)New carbide drill used & problem solved.\r\n2)Training given to operator how to give the CRC to the cutter & what are the care should be taken CRC prgrams.','Planning to avoid such a problem,instead of CRC programs center line programs should use.','CA/PA Found satisfactory.','','2009-09-18','Dinakara(G)','Diwakar(S)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(254,'18-051A','Magellan Aerospace Bournemouth','CLEAT RH','177477','PIL575 52551 201','ABM3 1029','A00',1,'RM365124','','3222','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Thickness undersize Drg Dim 2.50+/-0.25 measures 2.20 to 2.25','It is happened in fitting,without checking the dimension he made polishing. ','He is trained,what are the care should taken before polishing the parts.','Same as above','CA/PA Found satisfactory.','','2009-09-18','Nagaraju(T)','Irappa(Badiger)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(255,'18-098A','Magellan Aerospace Bournemouth','SEAT VALVE','B6352','PID282 50060 204','L109 T4','D',1,'RM365292','','3322','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Inside radius & flat area sharp edge not done & 0.2mm material cut.','operator did not take the work offset correctly','corrected the work offset','Instructed the Operator to take the offset correctly','Further produced parts found OK','','2009-09-18','Dinakara(G)','Diwakar(R.B.)','','0000-00-00','Note:Production supervisor select the correct operator name. ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(256,'18-098A','Magellan Aerospace Bournemouth','SEAT VALVE','B4356','PID282 50060 204','L109 T4','D',1,'RM365292','','2424','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Dia 4.826/4.876 in one hole oversize,measures 4.90to4.91 pin enters.','Drill bit runout caused the deviation','Removed the tool and reclamped the tool without runout','Instructed the operator to check the tool runout before machining','Further produced parts found OK','','2009-09-18','Dinakara(G)','Manjunath(K.N.)','','0000-00-00','Note:Production supervisor select the correct operator name. ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(257,'18-111A','Magellan Aerospace Bournemouth','BODY TURNBUCKLE INTMD','698428','PID575 41544 200','S80 FHT','A',1,'RM365149 Amnd 1','','3446','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dia 6.00 hole 0.5mm shifted from the center point of the part.','Due to runout of the tool this deviation occured','Removed the tool and clamped the tool again without runout','Instructed Operator to check the tool runout before clamping the tool','Further produced parts found OK','','2009-09-18','Dinakar(K)','Ramesh(S. Bandagi)','','0000-00-00','Note:Production supervisor select the correct operator name. ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(258,'18-105A','Magellan Aerospace Bournemouth','FORKEND ASSEMBLY','723001','PID572 50462 200','S98 FHT','J01',2,'RM365139 Amnd 1','','3055','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','1)Thread damege in 1no.\r\n2)Key way width oversize 0.1mm in 1no.','1)Tool wornout and caused damage\r\n2)Tool offset wrongly taken','1)changed the tool\r\n2)corrected the tool offset','1) Instructed Operator to check the sharpness of the tool periodically\r\n2)corrected the tool offset','Further produced parts found OK','','2009-09-18','Dinakara(G)','Nagaraj(G. Nadiger)','','0000-00-00','Supervisor name:Dinakar G & Dinakar K\r\nNote:Production supervisor select the correct operator name. ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(259,'18-109A','Magellan Aerospace Bournemouth','NUT SLIM 3/4 UNJF','690634','PID575 40498 200','S80 FHT','D01',3,'RM365152 Amnd 1','','3351','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Dent marks on thread, gauge not answered.','Operator did not notice the tool wearout','changed the tool','Instructed the Operator to check the sharpness of the tool periodically','Further produced parts found OK','','2009-09-18','Dinakar(K)','Nithin(S)','','0000-00-00','Note:Production supervisor select the correct operator name. ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(260,'18-110A','Magellan Aerospace Bournemouth','FORK END INTERMEDIATE','698277','PID575 40494 202','S80 FHT','J',1,'RM365150','','3178','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','OD undersize 0.6mm.','Operator did not take the offset correctly','Corrected the offset','Instructed the Operators to take the offset correctly','Further produced parts found OK','','2009-09-18','Dinakar(K)','Paramesh(K)','','0000-00-00','Note:Production supervisor select the correct operator name. ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(261,'18-090A','Magellan Aerospace Bournemouth','BUSH','625728','PID278 50164 200','S80 FHT','A',1,'RM365162 Amnd 1','','3182','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','OD undersize, Drg Dim 39.964/39.980 measures 39.950 to 39.965','OD undersize, Drg Dim 39.964/39.980 measures 39.950 to 39.965. because of insert wear out.','not applicable.because rejected piece was last piece.','will be taken care for next batch.','CA/PA Found satisfactory.','','2009-09-18','Dinakar(K)','Vikram(E)','','0000-00-00','Narasimha Murthy R and Vikram E.','F8003-S','Rev 0 dt 8-1-2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(262,'18-105A','Magellan Aerospace Bournemouth','FORKEND ASSEMBLY','590431','PID572 50462 200','S98','J01',1,'RM365139 Amnd 1','','2667','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Bore oversize 15.895+0.018 measures 15.928','Spindle bearings had worn out. Piece rejected while first off proving.','Replaced the spindle bearings with new one.','Replaced the spindle bearings with new one.','CA/PA Found satisfactory.','','2009-09-18','Dinakara(G)','Dinakara(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(263,'18-118A','Magellan Aerospace Bournemouth','BEARING HOUSING','694006','PID275 40005 200','S130 FHT','C01',4,'RM365159 Amnd 1','','3245','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','1)Tool dig mark on Undercut Groove 1.0mm Depth in 3nos.\r\n2)Length undersize 0.5mm undersize,Drg Dim 36.0 measures 35.48 to 35.52 in 1no.','1)while setting chuck pressure 3 nos. rejected.','chuck pressure seteed for next peices and whole batch found ok.','setted pressure is updated in process sheet.','RC/CA/PA TO BE ENTERED.','','2009-09-18','Dinakar(K)','Narasimha(Murthy R)','','0000-00-00','1)\r\n2)Ramesh S. Bandagi and Paramesh K. 1no\'','F8003-S','Rev 0 dt 8-1-2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(264,'18-075A','Magellan Aerospace Wrexham','ADAPTOR','18882/011','D282 50044 200PF',' L111 T6','A',3,'PRP91227 Amendment 1','','3369','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Tool dig mark on out side Profile in 2mm depth.','Operator did not take the offset correctly','corrected the offset value ','Instructed the Operator to take the offset correctly','Further produced parts found OK','','2009-09-18','Dinakara(G)','Diwakar(S)','','0000-00-00','Note:Production supervisor select the correct operator name. ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(265,'18-123A','Magellan Aerospace Bournemouth','FORK END OUT BD','697907','PID575 41546 202','S80 FHT','B',1,'RM365147 Amnd 1','','3058','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Dia 6.0mm hole depth oversize Drg Dim 20+/-0.3 measures 21.10.','offset not taken properly.','offset taken properly.','training given to take offset properly.','CA/PA Found satisfactory.','','2009-09-18','Dinakar(K)','Rajesh(T)','','0000-00-00',' ','F8003-S','Rev 0 dt 8-1-2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(266,'18-119A','Magellan Aerospace Bournemouth','HOUSING OUT B D BRG 3','CB894702','PID275 40011 200','S130 FHT','D01',1,'RM365160 Amnd 1','','3337','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','OD undersize,Drg Dim 71.950/71.970 measures 71.926 to 71.932.','WRONG TOOL COMPENSTAION GIVEN BY OPERATOR','CORRECTED THE TOOL COMPENSATION','INSTRUCTED THE OPERATORS TO TAKE THE TOOL COMPENSATION CORRECTLY','FURTHER PRODUCED PARTS FOUND OK','','2009-09-18','Dinakar(K)','Narasimha(Murthy R)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(267,'18-108A','Magellan Aerospace Bournemouth','FORK END OUT BD','697907','PID575 41546 200','S80 FHT','B',1,'RM365147 Amnd 1','','3139','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Bore shift in 2.9 mm, Dra Dim 75.0+/-0.3 measures 77.90.','Operator has taken the work offset wrongly','corrected the work offset','Instructed the operator to take the work offset correctly','Further produced parts found OK','','2009-09-18','Dinakara(G)','Theerthappa(K.N.)','','0000-00-00','Note:Production supervisor select the correct operator name. ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(268,'18-107A','Magellan Aerospace Bournemouth','LINK ASSY','1243','PID574 50553 200','DTD 5014','A',4,'RM365142 Amnd 1','','3092','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1)Bore oversize,Drg Dim 15.870+0.015 measures 15.890 to 15.897 in 2no.\r\n2)OD undersize,Drg Dim6.20/6.35measures6.10 to 6.15 in 2no. ','1)Boring tool was set wrong\r\n2)wrong clamping.','1) corrected the boring tool setting\r\n2)proper clamping done.','1)Instructed the operator to set the boring tool properly\r\n2)training given for clamping.','Further produced parts found OK','','2009-09-18','Dinakar(K)','Mohan(Kumar C.M.)','','0000-00-00','Supervisor name:Dinakar G\r\nSupervisor name:Dinakar K  operator name;Mohan Kumar C.M.\r\n','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(269,'18-086B','Magellan Aerospace Wrexham','PLATE SEALING','275616','D572 52913 200 01','ABM3 1029','B',1,'RM90855','','3155','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dia 10.0mm hole shifted 2.0mm length.','Operator took wrong offset','Corrected the offset','Instructed Operator to take the offset correctly','further produced parts found OK','','2009-09-18','Dinakara(G)','Diwakar(S)','','0000-00-00','Note:Production supervisor select the correct operator name','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(270,'18-187A','Magellan Aerospace Bournemouth','BUSH','0805406211','PIL575 50337 200','B23','B00',1,'RM365243 Amnd 1','','3341','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','OD undersize Drg Dim dia43.759/43.775 measures 43.746 to 43.755','wrong offset taken','corrected the offset','Instructed the operator to take the offset correctly','Further produced parts found OK','','2009-09-18','Dinakar(K)','Mohan(Kumar C.M.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(271,'18-117A','Magellan Aerospace Bournemouth','HOUSING-OUT BD BRG','662385','PID275 40004 200','S130 FHT','C01',5,'RM365157','','3244','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','OD undersize Drg Dim 69.951/69.970 measures 69.930 to 69.953 ','Operator entered the tool offset wrongly','corrected the tool offset','Instructed the operator to take the tool offset correctly','Further produced parts found OK','','2009-09-18','Dinakar(K)','Narasimha(Murthy R)','','0000-00-00','Note:Production supervisor select the correct operator name','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(272,'18-086B','Magellan Aerospace Wrexham','PLATE SEALING','283407','D572 52913 200 01','ABM3 1029','B',1,'RM90855','','3154','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Tool dig mark on outside profile in3mm depth.','Tool broken during machining','changed the tool','Instructed Operator to ensure the sharpness of the tool','Further produced parts found OK','','2009-09-18','Dinakara(G)','Nagaraju(K.S.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(273,'18-088A','Magellan Aerospace Wrexham','PLATE SEALING','025962/001','D572 52998 200 01','ABM3 1029','A',1,'RM90859','','3365','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Inside face dig mark & thickness undersize 2mm depth.','while running job sliped.','jaws rebore has been done.','for next  every 5pices cross chuck  the chuck pressur.','CA/PA Found satisfactory.','','2009-09-18','Dinakar(K)','Nithin(S)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(274,'18-112A','Magellan Aerospace Bournemouth','BODY TURNBUCKLE INNER','686194','PID575 41541 200','S80 FHT','A',1,'RM365153 Amnd 1','','3140','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Bore 12.700+0.018 measures 12.723 to 12.725.','Boring tool was not set correctly','corrected the boring tool setting','Instructed Operator to take care while setting the boring tool','Further produced parts found o.k','','2009-09-18','Dinakara(G)','Sunil(Kumar K.R.)','','0000-00-00','Note:Production supervisor select the correct operator name','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(275,'18-111A','Magellan Aerospace Bournemouth','BODY TURNBUCKLE INTMD','625720','PID575 41544 200','S80 FHT','A',1,'RM365149 Amnd 1','','3142','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dia 6.00 hole 0.5mm shifted from the center point of the part. Dia 3.0 hole notdone.','x axies offset not taken properly.','offset taken properly.','x offset value has been saved.','CA/PA Found satisfactory.','','2009-09-18','Dinakar(K)','Ramesh(S. Bandagi)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(276,'18-097A','Magellan Aerospace Bournemouth','PLATE','45559B','PID282 50100 200','L168','A',1,'RM365291','','3246','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Outside profile flat area. 1.0 x45deg chf observed & tool dig mark noticed.','Wrong tool selected by the operator','Instructed operator to select correct tool','Instructed operator to select correct tool','further produced parts found OK','','2009-09-18','Dinakara(G)','Diwakar(S)','','0000-00-00','Note:Production supervisor select the correct operator name','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(277,'35-008','Saab AB','HINGE BRACKET 4','328472/1A1','D576 50007 000 01','7050 T7651 ABM3 1030','D00',1,'1600028485','','3483','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Slot width oversize,23.09+/-0.03 measures 23.50','offset wrongly taken','corrected the offset','Instructed operator to take the offset correctly','Further produced parts found OK','','2009-09-18','Krishna(Chowdary.G.P.)','Basavaraju(S. Sr.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(278,'23-076','Goodrich Aerospace','EDGE TEE','4464601','7716205-801','7075-T7351 PER AMS 4','ECN 55879',1,'CRGL14435-02-09','','3431','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dimension .445\" +/-.01(11.30+/-0.250) measures .4180\"(10.60).','Operator did not take the tool offset correctly','corrected the offset','Instructed the operator to enter the offset correctly','Further produced parts found OK','','2009-09-20','Krishna(Chowdary.G.P.)','Dhananjaya(N)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(279,'18-113A','Magellan Aerospace Bournemouth','ADJUSTER','644826','PID575 40496 200','S80 FHT','G',80,'RM365151 Amnd 1','','2278','','2009-06-05',NULL,'yes','yes','no','no','no','no','no','no','yes','A quantity of 80 parts with your batch number 644826 & WO No 2278 have been found to have the external threads oversize. ','These parts are being checked with three pin method. Upon gettig this NCR it was found that the one mm diameter pins were worn out by 0.08 to 0.1 mm by which the reading recorded were found to be correct and dispatched.','Pins replaced. Customer has advised to rework these at their end to acceptable limits.','Two sets of three pin gauges are made one for quality and one for production. both shall be under the control of quality that shall be checked for the pin diameter before being issued or used.   ','Next batch found satisfactory.','C1292','2009-09-20','Avinash(R.J.)','Muniyappa(N)','RDN 00520','2009-07-06','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(280,'18-105A','Magellan Aerospace Bournemouth','FORKEND ASSEMBLY','546134','PID572 50462 200','S98 FHT','J01',43,'RM358383','','1027','','2008-11-26',NULL,'no','no','no','yes','no','no','no','yes','yes','1)A quantity of 34 parts has been found to have the hardness values below the required standard.The limits for this material are 360-410 HV and these components measured 270-279HV.These parts connot be progressed and have to be scrapped.\r\n2)A quantity of 8 parts has been found to have the hardness values higher then the required standard.The limits for this material are 360-410 HV and these components measured 422-448HV.These parts connot be progressed and have to be scrapped.\r\n3)A quantity of 1 part has been found to have the hardness value below the required standard.The limits for this material are 360-410 HV and these components measured 306HV.These parts connot be progressed and have to be scrapped.\r\n\r\n\r\n','The parts PID572-50462-200 and PID572-50463-201 as referred in the above three RDNs are made of S98 material. The same diameter is being procured for other parts but with S80 material as per the requirements. The report as per RDNs calls for the material','1)Stores advised not to issue parts for production with same diameter of two different specifications and to issue the material upon first operation in turning being complete after which such instances cannot occur as the material comes to turning for first operation.\r\n2)Clear instructions put on the turning centers machining these parts advising them not to take two parts of same diameter and different specification for machining even though Stores commits error and issue them at once.\r\n3)The raw materials available in stores against these part numbers were checked for the material hardness and they were found to be complying with the required parameters. The analysis of the test carried out is enclosed with this.','1)There exist two different Storing areas of raw material with two different entries. Insstructions are given, to store the S98 and S80 materials from the receipt stage itself in separate and in each store to avoid further possible mix up.\r\n2)Since the mentioned parts are regular requirements, dedicated racks within the Stores are kept for each part number with the S80 in one store and S98 in the other.','Next batch found satisfactory.','C348,C1135,C1398','2009-09-20','Avinash(R.J.)','Muniyappa(N)','00554,00555,00556','2009-08-11','1)RDN No:00554,WO No:1027,Qty:34no\'s.\r\n2)RDN No:00555,WO No:786,Qty:8no\'s.\r\n3)RDN No:00556,WO No:2549,Qty:1no.\r\nAll the above three RDNs refers to the same problem of hardness with the values measuring higher or lower to that of the required values. Hence the root cause, corrective and preventive action are analized and answered as common.','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(281,'35-012','Saab AB','JACK BRACKET 1','325526 1A1','D576 50009 000 01','7050 T7651 ABM3 1030','C00',1,'1600028485','','3327','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','top intersection point, it looks likeradius instead of sharp edge by 1mm.','While running production power tripped(running dia 12 ball 3D finish prg)and dig mark opserved on 3D rib. ','Inform to machine manufactured to avoid such problem, because power fail is not predectible','Machine manufacturer observed the problem and change the machine parameter such that when power tripped the \"Z\" axis moving in plus side.','CA/PA Found satisfactory.','','2009-09-21','Krishna(Chowdary.G.P.)','Girish(Prasad P)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(282,'35-010','Saab AB','HINGE BRACKET 5','328471/1C1','D576 50008 000 01','7050 T7651 ABM3 1030','C00',2,'1600028485','','3488','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','1)Bore measures over size by 0.005 to 0.007mm in 1no.\r\n2) Tool dig mark noticed to 1mm in the place of R20.','1) Boring tool setting done wrongly\r\n2) Tool offset wrongly taken','1) Corrected the boring tool setting\r\n2) Corrected the offset taken','1)Instructed operator to set the boring tool correctly\r\n2)Instructed operator to set the offset correctly ','Further produced parts found OK','','2009-09-23','Krishna(Chowdary.G.P.)','Lokesh(B.D.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(283,'35-012','Saab AB','JACK BRACKET 1','313443 1B1','D576 50009 000 01','7050 T7651 ABM3 1030','C00',6,'1600028480','','2818','','0000-00-00',NULL,'yes','no','no','no','no','no','no','yes','yes','The reason behind the suspecion of mis-orientation is that after anodizing of the parts, a grainning appears in different tones of grey on the surface.','The raw material dimensions for the above mentioned parts is 105 GF x 150 x 150.  All the parts till date have been verified for the longitudinal grain flow direction but not verified for the longitudinal traverse grain direction.','1) To enable the Customer to check the LT at their end since they were not checked, details of the previous supplied parts were sent. This consisted of: a) Dispatch details to Saab for the above 4-brackets from the 09th of July 2009 to 30th September 2009.  b) Dispatch details of these 4-brackets to Norcot Engineering (earlier Customer) from 01st February to 30th June 2009. \r\n2) The 4-parts 40-nos each ready for dispatch during end September withhold till further concurrence from the Customer. \r\n3) Stores person trained for the GF, LT and ST directions with a detailed drawing in place.\r\n \r\n4) Further production of these 4-parts withhold and no material issued \r\n5) The other 10-part numbers in WIP were cross verified for this LT direction jointly from Stores and QC.  Upon physical verification, it was found that these were correct and in place to the requirements.  ','1.	After the training to the Stores personnel and ensuring that the requirement are fully understood, hence forth it is decided that the Stores shall cross verify, mark suitably and then issue to the Production.\r\n2.	Detail drawing explaining the GF, LT and ST are put in the stores at the issue point along with the necessary photographs as attached.\r\n3.	To ensure the correct loading of the part the raw materials hence forth shall be marked as ‘F’ in paint upon checking for the GF and LT.  This F shall give indication to the Operator of loading direction. This shall be carried out by the Stores before issue of the raw material to the production.  The same method shall be adhered to all the 14-parts in this package.  Please find attached photographs evidencing the same.\r\n4.	The first operation of the process sheet to evidence this is amended accordingly.  Please find the same attached.\r\n5.	Raw material suppliers are instructed to mark the LT direction on the material before dispatch from the next coming dispatch during end of October 2009.\r\n6.	From the subsequent purchase orders for the materials it is instructed to the Material Planning to include this in the order as mandatory.\r\n','Further produced parts found O.K','C1503','2009-10-04','Avinash(R.J.)','Prakash(C.B.)','Mail on 28/09/2009','2009-09-28','Effected part numbers with details.\r\n1) D576 50009 000 01\r\n2) D576 50009 001 01\r\n3) D576 50010 000 01\r\n4) D576 50010 001 01\r\n','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(284,'28-016','Ellanef Manufacturing Corporation','STOP FITTING','94738','161A6119-1','15-5PH per AMS5659','NA',1,'99934 Rel-1','','3564','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dig mark observed in the width.','Wrong tool offset taken by operator','corrected the tool offset','Instructed operator to take the offset correctly','Further produced parts found OK','','2009-10-06','Stalin(G)','Ravindra(Singh R)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(285,'23-075','Goodrich Aerospace','EDGE TEE','266218','7716204-801','7075-T7351 PER AMS 4','ECN 55818',1,'CRGL14435-02-09','','3583','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Total width measures 2mm undersize.','Part not clamped properly.','Informed to operator to check the clamp before running the program.','Process explained to avoid such mistakes.','Next production parts found satisfactory.','','2009-10-07','Krishna(Chowdary.G.P.)','Manjunath(K.N.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(286,'30-025','Gardner Aerospace Burnley Limited','RIB CLOSING INBOARD - RH','722727 A5','L575 54754 201','ABM3 1029','A, ECN: SG60049U03JA06',2,'PRO0016034-S4','09-10','3313','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','Parts rejected due to wrong hole co-ordinates (Machining completed in Sl.no.01 & 1st set up completed in sl.no.02)','Hole co-ordinates taken from L57554754 200 LH model supplied by the customer.','Hole co-ordinates taken from L57554754 201 RH model supplied by the customer and RE-FAIR carried out for the same.','parts will be machined with no non-conformances.','','','2009-10-08','Avinash(R.J.)','Prakash(C.B.)','','0000-00-00','Parts rejected due to wrong hole co-ordinates','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(287,'23-042','Goodrich Aerospace','REINFORCEMENT PLATE','50418-1','7712501 815','7075-T6511 IAW AMS-Q','TR IP 7712501-815 REV 02',1,'CRGL14416-02-09','','3717','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','total width 1.470\" +/-.03 (29.14+/-.76) measures 1.04\" (26.14).','face butting not done properly.','For next piece operator made butting properly.','operator instructed & guided, how to butt & HOW TO CLAMP.','CA/PA Found satisfactory.','','2009-10-12','Krishna(Chowdary.G.P.)','Diwakar(R.B.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(288,'23-043','Goodrich Aerospace','REINFORCEMENT PLATE','50418-1','7712501-816','7075-T6511 IAW AMS-Q','TR IP 7712501-816 REV 03',1,'CRGL14416-02-09','','3719','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','wall thickness (.125)\"(3.175 mm) measure .0810\"(2.082 mm).','face butting not done properly. ','For next piece operator made butting properly.','operator instructed & guided, how to butt & HOW TO CLAMP. ','CA/PA Found satisfactory.','','2009-10-12','Krishna(Chowdary.G.P.)','Diwakar(R.B.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(289,'23-043','Goodrich Aerospace','REINFORCEMENT PLATE','57111-1','7712501-816','7075-T6511 IAW AMS-Q','TR IP 7712501-816 REV 03',1,'CRGL14416-02-09','','3720','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Base thickness 0.052/0.072(1.32/1.83)measures 0.045(1.14).','Operator did not take the tool offset correctly.','Corrected the tool offset.','Instructed the operator to take the offset correctly.','Futher produced parts found ok.','','2009-10-12','Krishna(Chowdary.G.P.)','Manjunath(K.N.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(290,'28-007','Ellanef Manufacturing Corporation','SHAFT SUPPORT/LEVER','92491','251A1747-1','6Al-4V per MIL-T-904','N/C',1,'99457 Rel 2','','3130','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Dimension .7494/.7497(19.035/19.042) measures .7490(19.027).','Operator did not take the offset correctly','Instructed operator to take the offset correctly','Instructed operator to take the offset correctly','Further produced parts found OK','','2009-10-14','Dinakar(K)','Rajesh(S)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(291,'18-062A','Magellan Aerospace Bournemouth','STIFFENER -2 LH','226041','PIL575 53253 200','ABM3 1029','A00',1,'RM365127','','3471','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Tool dig mark noticed on flange thickness 3.20 in depth of 6mm.','Operator did not take the offset correctly','Instructed operator to take the offset properly','Instructed operator to take the offset properly','Further produced parts found OK','','2009-10-19','Dinakara(G)','Satish(Kumar)','','0000-00-00','Note:Production supervisor select the correct operator name ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(292,'18-062A','Magellan Aerospace Bournemouth','STIFFENER -2 LH','184534','PIL575 53253 200','ABM3 1029','A00',1,'RM365127','','3470','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Thickness & length undersize,Thickness 3.0 +0.13/-0.08 measures 2.80/2.86 & length 35.0 +/-0.3 measures 34.58/34.72.','Operator did not take the offset correctly','Instructed operator to take the offset correctly\r\n','Instructed operator to take the offset correctly\r\n','Further produced parts found OK','','2009-10-19','Dinakara(G)','Satish(Kumar)','','0000-00-00','Note:Production supervisor select the correct operator name ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(293,'18-098A','Magellan Aerospace Bournemouth','SEAT VALVE','B6353','PID282 50060 204','L110','D',1,'RM365292','','3516','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Slot width oversize 0.8/0.9 measures 1.0/1.10','Tool runout caused the deviation','removed the tool and reclamped the tool without runout','Instructed operator to clamp the tool without runout','Further produced parts found OK','','2009-10-19','Dinakara(G)','Diwakar(S)','','0000-00-00','Note:Production supervisor select the correct operator name ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(294,'18-110A','Magellan Aerospace Bournemouth','FORK END INTERMEDIATE','698428','PID575 40494 202','S80 FHT','J',3,'RM365150','','3645','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Bore oversize & Width undersize.Bore 14.287+0.018 measures 28.308 / 28.313 in 2no & width 28.10+/-0.3 measures 27.70 in 1no.','Bore oversize occured due to wrong offset given\r\nWidth under size occured due to tool wear','Instructed operator to take correct offset\r\nInstructed operator to check the tool wear','Instructed operator to take correct offset\r\nInstructed operator to check the tool wear','Further produced parts found Ok','','2009-10-19','Dinakara(G)','Sunil(Kumar K.R.)','','0000-00-00','Note:Production supervisor select the correct operator name ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(295,'30-010','Gardner Aerospace Burnley Limited','RIB CLOSING OUTBOARD - RH','722725 A9','L575 51826 201','ABM3 1029','B, ECN:PG69999001JK19',1,'PRO0016034-S7','','3502','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Part has been rejected due to material loaded wrongly by the operator on machine. ','The operator has loaded the material wrongly without refer the process sheet on the machine after first setup.','The operator instucted  to refer the process sheet strictly in every setup before load the raw mateial on the machine.','The care will be taken to control the mistakes for the future quantities.','Further produced parts found ok.','','2009-10-21','Siddalinga(Tambake)','Padmanabha(K)','','0000-00-00','Part has been rejected due to material loaded wrongly on machine. ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(296,'30-010','Gardner Aerospace Burnley Limited','RIB CLOSING OUTBOARD - RH','722725 A9','L575 51826 201','ABM3 1029','B, ECN:PG69999001JK19',1,'','','3509','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','part has been rejected due to material loeaded wrongly on the machine.  ','The operator has loaded the material wrongly without refer the process sheet on the machine after\r\nfirst setup. ','The operator instucted to refer the process sheet strictly in every setup before load the raw\r\nmateial on the machine. ','The care will be taken to control the mistakes for the future quantities.','Next produced part found satisfacory.','','2009-10-21','Siddalinga(Tambake)','Padmanabha(K)','','0000-00-00','part has been rejected due to material loeaded wrongly on the machine.  ','F8003-S','Rev 0 dt 8-1-2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(297,'35-003','Saab AB','HINGE BRACKET 1','219021 B','D576 50004 001 01','7050 T7651 ABM3 1030','C00',1,'1600028483','','3044','','0000-00-00',NULL,'yes','yes','no','no','no','no','no','no','yes','one part D576 50004 200 Hinge 1 Assy is marked as right performed article.Marking D576 50004 201.After inspection is has been shown that the article is produced as a left part.','1) it might be a chances of mix up ( left hand and right hand)','we have arranged the separate tray for each code to avoid the mix up.','same as above.','Further dispatched parts found O.K.','C1667','2009-10-21','Avinash(R.J.)','Prakash(C.B.)','SCAR No.1291/2009','2009-10-18','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(298,'23-077','Goodrich Aerospace','EDGE TEE','6267601','7716254-801','7075-T7351 PER AMS 4','ECN 55880',1,'CRGL14435-02-09','','3778','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Dimension .225\"(5.715mm)+/-.01(0.250mm) in zone 2C9 measures .2080\"(5.280).','Due to tool compensation problem.','Will be taken care in future.','Will be taken care in future.','CA/PA Found satisfactory.','','2009-10-22','Krishna(Chowdary.G.P.)','Manjunath(K.N.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(299,'23-078','Goodrich Aerospace','EDGE TEE','6267601','7716255-801','7075-T7351 PER AMS 4','ECN 55881',1,'CRGL14435-02-09','','3779','','0000-00-00',NULL,'yes','no','yes','no','yes','no','no','no','no','Dimension .160\"(4.064mm) +/-.01\"(.250mm) measures .1420\"(3.6mm)','Due to machine problem.','Informed to service engineer & requested to rectify this problem as well as solve it.','Same as above.','Next part found satisfactory.','','2009-10-22','Krishna(Chowdary.G.P.)','Manjunath(K.N.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(300,'23-027','Goodrich Aerospace','REINFORCEMENT PLATE','57110-1','7712500-8054','7075-T6511 IAW AMS-Q','TR IP 7712500-8054 REV 02',1,'CRGL14416-03-09','','3677','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Hole Position .010\"(.250mm) measures .0180/.020\"(.45/.50). ','Due to RM bend and Twist hole position not achieved.','RM bend cant avoided.','RM bend cant avoided.','Next part found satisfactory.','','2009-10-23','Krishna(Chowdary.G.P.)','Rangaswamy()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(301,'18-113A','Magellan Aerospace Bournemouth','ADJUSTER','671608','D575 40496 200','S80 FHT','G',8,'RM365151 Amnd 1','','3475','','0000-00-00',NULL,'yes','no','no','no','no','yes','no','yes','no','ID thread damage & spoilled in center of the part.','Due to shrinkage in the 2nd set up it was happend.\r\nthread tapping time this prolem occur.','to be stabilize the process.','every batch supporting bush newly prepared.','Next batch found ok. ','','2009-10-24','Nagaraju(T)','Nagaraju(T)','','0000-00-00','Note:Production supervisor select the correct operator name ','F8003-S','Rev 0 dt 8-1-2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(302,'18-113A','Magellan Aerospace Bournemouth','ADJUSTER','671608','D575 40496 200','S80 FHT','G',10,'RM365151 Amnd 1','','3526','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','ID thread damaged in center of the part.','Due to shrinkage in the 2nd set up it was happend.\r\nthread tapping time this prolem occur.','to be stabilize the process.','every batch supporting bush newly prepared.','Next batch found ok.','','2009-10-24','Nagaraju(T)','Nagaraju(T)','','0000-00-00','Note:Production supervisor select the correct operator name ','F8003-S','Rev 0 dt 8-1-2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(303,'18-121A','Magellan Aerospace Bournemouth','BARREL - STRUT','687946','D572 50463 201','S98 FHT','F',3,' RM365136 Amnd 1','','3579','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1)Thread gauge NOGO answered in 2nos.\r\n2)Dia 1.50 hole oblong in 1no.','1)Tool wear was not entered properly\r\n2)Drill broken during machining','1)Instructed operator to enter the tool wear correctly\r\n2)Instructed operator to check the sharpness of the drill before using it','1)Instructed operator to enter the tool wear correctly\r\n2)Instructed operator to check the sharpness of the drill before using it','Further produced parts found OK','','2009-10-24','Dinakar(K)','Nithin(S)','','0000-00-00','Note:Production supervisor select the correct operator name ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(304,'18-118A','Magellan Aerospace Bournemouth','BEARING HOUSING','694006','D275 40005 200','S130 FHT','C01',3,'RM365159 Amnd 1','','3494','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1)Tool dig mark noticed on bore in 5mm depth in 1no.\r\n2)Dia 39.0 -0.25 measures 38.52 to 38.64 in 2nos.','1)Operator did not give the offset correctly\r\n2) Tool setting not done properly','1) Instructed operator to give the correct offset in the machine\r\n2) Instructed operator to set the tool and check whether set correctly','1) Instructed operator to give the correct offset in the machine\r\n2) Instructed operator to set the tool and check whether set correctly','Further produced parts found OK','','2009-10-24','Dinakar(K)','Ramesh(S. Bandagi)','','0000-00-00','Note:Production supervisor select the correct operator name ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(305,'18-119A','Magellan Aerospace Bournemouth','HOUSING OUT B D BRG 3','CB894702','D275 40011 200','S130 FHT','D01',1,'RM365160 Amnd 1','','3535','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','OD dia 71.951/71.970 measures 71.945 to 71.955 & feed lines existed, surface finish not maintained.','Due to new trial basis tool used,tool it self plus side.','After operation we come to known that,it is due to tool.so replaced the tool.next part get without deviation.','Same as above.','Next part found satisfactory.','','2009-10-24','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(306,'18-226A','Magellan Aerospace Bournemouth','BRKT - NUT RETAINER','4345888','F572 53828 200','L168','A',1,'RM366515','','3522','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Thickness undersize,dimension 7.5 +0.3/-0.2 measures 7.24 to 7.28.','Might be happened in sizing.','Will cross check the required dimensions before taking to the CNC operation.','Will be taken care.','Next part found satisfactory.','','2009-10-24','Dinakara(G)','Dinakara(G)','','0000-00-00','Note:Production supervisor select the correct operator name ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(307,'18-104A','Magellan Aerospace Bournemouth','BODY TURNBUCKLE','654734','D575 40490 200','S80 FHT','E',1,'RM365144 Amnd 1','','3519','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Thread gauge LH side NOGO answered.','Piece not clamp correctly & chuck pressure is above 20KG.therefore NOGO answered','next piece was clamped correctly & chuck pressure adjusted.','Will be taken care.','Next batch found ok.','','2009-10-24','Dinakar(K)','Ramesh(S. Bandagi)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(308,'18-111A','Magellan Aerospace Bournemouth','BODY TURNBUCKLE INTMD','696913','D575 41544 200','S80 FHT','A',1,'RM365149 Amnd 1','','3568','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','ID thread damaged in center of the part.','Due to part holding problem.','It was rectified in final part & final stage.So next batch will taken care.','will be taken care.','Next part found satisfactory.','','2009-10-24','Dinakar(K)','Dinakar(K)','','0000-00-00','Note:Production supervisor select the correct operator name ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(309,'18-110A','Magellan Aerospace Bournemouth','FORK END INTERMEDIATE','698277','D575 40494 202','S80 FHT','J',1,'RM365150','','3449','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Second operation OD undersize 0.5mm,12.70-0.21 measures 12.04 to 12.05.','Refer NC number 00308.','Refer NC number 00308.','Refer NC number 00308.','Further produced parts found OK.','','2009-10-24','Dinakar(K)','Dinakar(K)','','0000-00-00','Note:Production supervisor select the correct operator name ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(310,'18-105A','Magellan Aerospace Bournemouth','FORKEND ASSEMBLY','723001','D572 50462 200','S98 FHT','J01',1,'RM365139 Amnd 1','','3517','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Bore ovality & oversizein 0.02mm.','Due to boring bar problem.','Boring bar servicing done.','Will be taken care.','Next part found satisfactory.','','2009-10-24','Dinakara(G)','Dinakara(G)','','0000-00-00','Note:Production supervisor select the correct operator name ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(311,'18-112A','Magellan Aerospace Bournemouth','BODY TURNBUCKLE INNER','696913','D575 41541 200','S80 FHT','A',2,'RM365153 Amnd 1','','3544','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1)ID thread flat GO gauge not enters in 1no.\r\n2)Hole Dia 3.0 +0.12 measures 3.20 pin enters.','1)In future will be taken care.\r\n2)In future will be taken care.','1)In future will be taken care.\r\n2)In future will be taken care.','1)In future will be taken care.\r\n2)In future will be taken care.','CA/PA Found satisfactory.','','2009-10-24','Nagaraju(T)','Nagaraju(T)','','0000-00-00','Note:Production supervisor select the correct operator name 2)Fitting superviser:Nagaraju T & oprator:Nataraj','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(312,'28-016','Ellanef Manufacturing Corporation','STOP FITTING','94738','161A6119-1','15-5PH per AMS5659','NA',3,'99934 Rel-1','','3564','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Dia 9.525/9.540 measures 9.538 to 9.546.','due to runout in tool hole oversize.','instructed to operator for checking runout tool before giving cut or check on extra material first.','instructed to operator for checking runout tool before giving cut or check on extra material first.','found ok.','','2009-10-24','Dinakara(G)','Dinakara(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(313,'18-090A','Magellan Aerospace Bournemouth','BUSH','625728','D278 50164 200','S80 FHT','A',1,'RM365162 Amnd 1','','3574','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','OD 39.964/39.980 measures 39.948 to 39.958','Refer Non Conformance Number 00312.','Refer Non Conformance Number 00312.','Refer Non Conformance Number 00312.','Refer Non Conformance Number 00312.','','2009-10-24','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(314,'18-035A','Magellan Aerospace Bournemouth','BRACKET','86633012','D579 50131 202','ABM3 1029','H02',1,'RM365134','','3468','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Tool dig mark noticed on radius to a deapth 4mm. ','Due to insert problem.','New inserts was loaded & problem were solved.','Same as above.','Next batch found ok.','','2009-10-24','Dinakara(G)','Anjinamurthy(H)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(315,'18-106A','Magellan Aerospace Bournemouth','EYE END INBOARD','723001','D575 41542 200','S98 FHT','D',1,'RM365154 Amnd 1','','3480','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Bore shifted,dim 80.0+/-0.3 measures 82.02 ','Due to operator error.He was not taken reference properly.','Strictly instructed to operator to avoid such kind of mistakes.','To take X0Y0 reference,touch probe provided to the operator.','','','2009-10-24','Dinakara(G)','Dinakara(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(316,'18-211A','Verdict Aerospace Components Ltd.','PLUNGER','694000','D321 40205 200','S80-FHT','H01',7,'55568','','3400','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1)Dia 9.965/9.975 measures 9.93 to 9.95 in 3nos.\r\n2)ID thread tap brockenned in 1no.\r\n3)ID thread drill bit brockenned in 1no.\r\n4)ID dia oversize in 1no.\r\n5)ID thread damaged in 1no ','1)Due to close tolerance.\r\n2,3,4,5)Will be taken care.','1)Will be taken care.\r\n2,3,4,5)Will be taken care.','1)Will be taken care.\r\n2,3,4,5)Will be taken care.\r\n','CA/PA Found satisfatory.','','2009-10-24','Dinakara(G)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(317,'18-122A','Magellan Aerospace Bournemouth','FORKEND ASSEMBLY','723001','D572 50462 201','S98 FHT','J01',5,'RM365139 Amnd 1','','3518','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1)Bore 14.308+0.018 measures 14.337 to 14.339 in 3nos.\r\n2)Bore 15.895+0.018 measures 15.919 to 920 in 1no.\r\n3)Thickness 6.0+0.3/-0.2 measures 4.0 to 4.01 in 1no.','WILL BE TAKEN CARE IN FUTURE.','WILL BE TAKEN CARE IN FUTURE.','WILL BE TAKEN CARE IN FUTURE.','Next part found satisfactory.','','2009-10-24','Dinakara(G)','Dinakara(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(318,'18-108A','Magellan Aerospace Bournemouth','FORK END OUT BD','697907','D575 41546 200','S80 FHT','B',5,'RM365147 Amnd 1','','3436','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1)Chamfer oversize, 0.5/0.75x45deg measures 1.2x45 in 1no.\r\n2)Slot width oversize 9.53+0.3-0.0 measures 9.85 to 10.0 in 1no.\r\n3)Hole oversize dia6.0+0.12 measures 6.20 to 6.23 in 2nos.\r\n4)Hole depth oversize 20.0+/-0.3 measures 22.10 in 1no.','WILL BE TAKEN CARE IN FUTURE.','WILL BE TAKEN CARE IN FUTURE.','WILL BE TAKEN CARE IN FUTURE.','next part found satisfactory.','','2009-10-28','Dinakara(G)','Dinakara(G)','','0000-00-00','Note:Production supervisor select the correct operator name','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(319,'35-002','Saab AB','HINGE BRACKET 1','328471/1A1','D576 50004 000 01','7050 T7651 ABM3 1030','C00',1,'1600029510','','3570','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Bore oversize,Dia 22.225 +0.021 measures 22.57.',' When boring operation running operator not given correct CRC value for roughing operation(pre bore operation)and this deviation accured.  ',' Inform to operator to take care while running boring operation. And crocess check when entering CRC values.',' Next all boring operation parts found correct.','CA/PA Found satisfactory.','','2009-10-28','Krishna(Chowdary.G.P.)','Lokesh(B.D.)','','0000-00-00','Note:Production supervisor select the correct operator name','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(320,'18-116A','Magellan Aerospace Bournemouth','ASSEMBLY FORK END','49628','F575 51377 200','L168','A',1,'RM365155 Amnd 1','','3465','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Center of the part one thread damage.','Threading tool running time power tripping insert brocken thread dig mark noticed.','WILL BE TAKEN CARE IN FUTURE.','WILL BE TAKEN CARE IN FUTURE.','CA/PA Found satisfatory.','','2009-10-28','Dinakar(K)','Dinakar(K)','','0000-00-00','Note:Production supervisor select the correct operator name','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(321,'18-030A','Magellan Aerospace Bournemouth','PIN','579901','D278 50156 200','S130 FHT','A',55,'RM365133 Amnd 1','','3549','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Total length undersize,5.50/5.60 measures 5.28 to 5.48.','Operator did not butt the pieces in the fixture properly','Instructed Operator to butt the pieces correctly in order to get the dimension correct','Instructed Operator to butt the pieces correctly in order to get the dimension correct','Further produced parts found OK','','2009-10-28','Stalin(G)','Pinto(N.L.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(322,'18-215C','Verdict Aerospace Components Ltd.','ROD END ASSMY - MALE','631551','D321 53012 200','S98','F01',14,'55568','','2958','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Bore oversize & surface finish in bore not maintained as per drawing calls.','Due to process error.','Process has been changed.','Same as above.','ca/pa found satisfactory.','','2009-10-28','Dinakara(G)','Dinakara(G)','','0000-00-00','Note:Production supervisor select the correct operator name','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(323,'18-087B','Magellan Aerospace Wrexham','PLATE SEALING ASSY','277474','D572 52914 200 01','ABM3 1029','B',1,'RM90855','','3553','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Outside profile undersize & tool dig mark noticed.','Due to improper clamping made by operator.','Strictly instructed to operator,to avoid manual mistakes.','Same as above.','CA/PA Found satisfacory.','','2009-10-28','Dinakara(G)','Diwakar(S)','','0000-00-00','Note:Production supervisor select the correct operator name ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(324,'18-085A','Magellan Aerospace Wrexham','BRACKET SUPPORT','M122420','D579 52009 200 01','L168','A',3,'RM90861','','3648','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Thickness 3.0 +0.3/-0.2 measures 2.30 to 3.40','Refer Non Conformance Number 00323.','Refer Non Conformance Number 00323.','Refer Non Conformance Number 00323.','Next batch found ok.','','2009-10-28','Dinakara(G)','Theerthappa(K.N.)','','0000-00-00','Note:Production supervisor select the correct operator name ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(325,'18-075A','Magellan Aerospace Wrexham','ADAPTOR','18882/011','D282 50044 200PF',' L111 T6','A',3,'PRP91227 Amendment 1','','3559','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1)Bore oversize, dia 45.41/45.46 measures 45.48 to 45.51 in 1no.\r\n2)OD undersize, dia 48.23/48.36 measures 48.15 to 48.17 in 1no.\r\n3)4Holes radius is oversize in 2mm depth & outside profile chf is done but drawing not calls for chf in 1no. ','1)Refer Non Conformance number 00330.\r\n2)Refer Non Conformance number 00330.\r\n3)Will be taken care.','1)Refer Non Conformance number 00330.\r\n2)Refer Non Conformance number 00330.\r\n3)Will be taken care.','1)Refer Non Conformance number 00330.\r\n2)Refer Non Conformance number 00330.\r\n3)Will be taken care.','Next part found satisfactory.','','2009-10-28','Dinakar(K)','Narasimhamurthy(K.G.)','','0000-00-00','Note:Production supervisor select the correct operator name ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(326,'18-082A','Magellan Aerospace Wrexham','STUD PLATE - LH','2933502','D278 50007 200 01','ABM3 1029','D01',1,'RM90860','','3093','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Tool dig mark on slot & depth oversize 2mm.','Piece holding problem.','Next piece job holding made correct.','Strictly instructed to operator before loading the part should cross check fixture screws & holding devices.','found ok.','','2009-10-28','Dinakara(G)','Anjinamurthy(H)','','0000-00-00','Note:Production supervisor select the correct operator name ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(327,'18-082A','Magellan Aerospace Wrexham','STUD PLATE - LH','0142302','D278 50007 200 01','ABM3 1029','D01',2,'RM90860','','3556','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','1)Thickness undersize in 20mm length 0.5mm minus in 1no.\r\n2)Thickness 6.95/7.05 opposite side in part in 1no.','Refer Non Conformance Number 00326.','Refer Non Conformance Number 00326.','Refer Non Conformance Number 00326.','refer Ncr 00326','','2009-10-28','Dinakara(G)','Anjinamurthy(H)','','0000-00-00','Note:Production supervisor select the correct operator name ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(328,'18-078A','Magellan Aerospace Wrexham','ADAPTOR','18883/012','A282 50081 200PF',' L111 T6','A',3,'PRP91227 Amendment 1','','3558','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','1)Thread NOGO answered in 1no.\r\n2)Tool dig mark on OD in 1mm depth & bore oversize in dia 2mm in 2no.','1)Due to machine problem.When power failure,axis get shifted.\r\n2)Due to machine problem.','Called to service engineer,to solve this problem.they tried their level best.','Same as above.','Next part found satisfactory.','','2009-10-28','Dinakar(K)','Dinakar(K)','','0000-00-00','Note:Production supervisor select the correct operator name ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(329,'18-210A','Verdict Aerospace Components Ltd.','BODY ASSEMBLY','9866','D321 40204 204','L168','D',1,'55568','','3560','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Bore dia 19.0 +0.021 measures 19.050.','while adjusting boring bar one no. rejected.','instruction given for operator while adjusting boring bar care to be take while giving corrections.','reamer will be planned for next batch.','','','2009-10-28','Dinakara(G)','Suresh(K.R.)','','0000-00-00','Note:Production supervisor select the correct operator name ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(330,'18-208A','Verdict Aerospace Components Ltd.','SPRING RETAINER','638857','D321 40203 220','S98','L',1,'55568','','3561','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Bore 17.51/17.53 measures 17.533 to 17.538.','Due to insert wear out.Number of batch quantity was 300.\r\nWe were changing insert for 50numbers.','New insert loaded.remaining components get without deviation. ','Know we decided to change insert after 40numbers instead of 50numbers.','CA/PA Found satisfactory.','','2009-10-28','Dinakar(K)','Narasimhamurthy(K.G.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(331,'23-117','Goodrich Aerospace','PROFILE A','4772777','A872316-8200','7055 T76511','ENC 89521',3,'CRGL14435-03-09','','3667','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Total length undersize, 12.7359/12.7759 measures 12.6965.','Due to wrong tool reference taken.','Will be taken care in future.','To solve this problem,tool pre-setter has been introduced.','CA/PA Found satisfactory.','','2009-10-28','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','Note:Production supervisor select the correct operator name ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(332,'18-084A','Magellan Aerospace Wrexham','BRACKET SUPPORT','M122420','D579 52008 200 01','L168','C01',65,'RM90861','','3398','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Hole pitch undersize,19.0 +/-0.3 measures 18.42 to 18.54','setting not done properly and first part not checked properly.','warning given to operator for proper setting and first part inspection.','warning given to operator for proper setting and first part inspection','Next batch found ok.','','2009-10-28','Dinakara(G)','Sunil(Kumar K.R.)','','0000-00-00','Another Operator:Dhananjaya','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(333,'18-035A','Magellan Aerospace Bournemouth','BRACKET','86633012','D579 50131 202','ABM3 1029','H02',44,'RM365134','','3468','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Grain flow direction opposite side.','Stores personnel did not check the RM for correct grainflow on the RM','Instructed Stores personnel to check the RM for correct grainflow on the RM before issuing it to production','Instructed Stores personnel to check the RM for correct grainflow on the RM before issuing it to production','Further produced parts found OK.','','2009-10-28','Dayananda(K.G.)','Venugopal(N)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(334,'34-022','BRISTOL AEROSPACE LIMITED','BUSHING','G14742','400-12614-1-905','17-4PH Stainless Ste','EM 104302 Iss. A, EM 105092 Iss. C',2,'B70996','','3791','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Step observed on the face in 01no. Outer diameter .6235/.6240\"(15.834/15.849mm) in zone C-1 measures .6210-15.774mm) in 01no.','Due to poor clamping.','Next piece clamping made correct & butting also given.','Same as above.','next part found ok','','2009-10-28','Dinakar(K)','Nithin(S)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(335,'18-121A','Magellan Aerospace Bournemouth','BARREL - STRUT','687946','D572 50463 201','S98 FHT','F',4,' RM365136 Amnd 1','','3579','','2009-10-10',NULL,'yes','yes','no','no','no','no','no','no','yes','A qty of 4 parts Cim WO No 3579 Batch No 687946 have been identified as having the 1/2\"-20 UNJF 3B Left Hand thread oversize.These parts cannot be reworked and are therefore scarp. ','','','','Inspection method changed to check the effective diameter with thread pitch micrometer. \r\nNext batch found satisfactory.','C2198','2009-11-04','Avinash(R.J.)','Muniyappa(N)','RDN 00576','2009-11-03','','F8003-S','Rev 0 dt 8-1-2009',0.00,'','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(336,'30-009','Gardner Aerospace Burnley Limited','RIB CLOSING OUTBOARD - LH','722725 A9','L575 51826 200','ABM3 1029','B, ECN:PG69999001JK19',1,'PRO0016097-S3','','3501','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','At zone 1C4,the tool dig of arc length 16.24mm and depth 13.55mm noticed on 2 mm thick inner flange.','while running roughing program,suddenly power tripped.  might be dig mark occured.','machine were surviceing done.','there is no preventive action.','please review the PA','','2009-11-09','Siddalinga(Tambake)','Padmanabha(K)','','0000-00-00','At zone 1C4,the tool dig of arc length 16.24mm and depth 13.55mm noticed on 2 mm thick inner flange.','F8003-S','Rev 0 dt 8-1-2009',742.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(337,'30-014','Gardner Aerospace Burnley Limited','FRAME GEAR RIB IFS - RH','336220A9','L575 51890 201','ABM3 1029','B, ECN:PW69999001JB47, PG60049M01JA73',1,'PRO0016097-S4','','3888','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Outer Flange thickness 2+0.2/-0.1 mm measures 1.96 mm to 1.35 mm','while setting  2su operator should take care regarding straight dialing & bore dialing.he did a mistake in straight dialing,hence the above result found.','Operator were strictly warned & suggested to avoid manual mistake. if same mistakes happened,he will be turminated from his job.','After several warning he made a mistake & he was turminated from his job.','CA/PA Found satisfacory.','','2009-11-09','Siddalinga(Tambake)','Padmanabha(K)','','0000-00-00','Outer Flange thickness 2+0.2/-0.1 mm measures 1.96 mm to 1.35 mm','F8003-S','Rev 0 dt 8-1-2009',848.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(338,'23-095','Goodrich Aerospace','BRACKET','266238','A877940-8204','7075 T7351 AMS QQ-A-','ECN 90701 (2 Sheets) Rev B',2,'CRGL14435-03-09','','3956','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dig mark observed on the face in 01no.diameter .2520/.2598\"(6.4/6.6) measures .2677\"(6.68) in 01no.','While running program part come out from vice and dig mark observed on face.','1)Checked clamping condition in vice with another part and conformed the clamping regidity,and found OK.\r\n2)Further parts observed the cutting force on part when roughing operation running also checked spindle force, and found OK.\r\n3)Inform to operator to clamp properly and crosscheck once.','Further parts coming OK','CA/PA Found satisfactory.','','2009-11-12','Krishna(Chowdary.G.P.)','Shivashankar(H.G.)','','0000-00-00','Other operators are Nagaraju K S, Manjunath K N,      Diwakar R B','F8003-S','Rev 0 dt 8-1-2009',37.10,'$','Closed','','yes','','','','0',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(339,'23-076','Goodrich Aerospace','EDGE TEE','4464601','7716205-801','7075-T7351 PER AMS 4','ECN 55879',1,'CRGL14435-02-09','','3932','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no',' DImension 1.778 +/-0.250 measures 0.660/1.790.',' While running roughing and base finish operation in 1stSU tool running Z axis minus 0.3mm and this deviation accured.   ','1) Immidatly checked all parts thickness, and also after completed 1st operation parts step thickness checked and found all OK.\r\n2) checked all tool offset and found OK.\r\n3) Plan to check every tool offset regurly when tool change and then only run the program. ','1) Further all parts coming OK.\r\n2) Observed Z axis problem and found OK.','CA/PA Found satisfactory.','','2009-11-16','Krishna(Chowdary.G.P.)','Diwakar(R.B.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',37.30,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(340,'18-119A','Magellan Aerospace Bournemouth','HOUSING OUT B D BRG 3','CB894702','D275 40011 200','S130 FHT','D01',4,'RM365160 Amnd 1','','3967','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','OD undersize 71.950 / 71.970 measures 71.920 to 71.945','overality problem at dx-200-3.','machine changed at dx-200-1.','further will be loaded in dx-200-1 only.','CA/PA Found satisfactory.','','2009-11-16','Dinakar(K)','Nithin(S)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',87.20,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(341,'18-204A','Magellan Aerospace Wrexham','CLEAT RH','158385','D572 59294 201 01','ABM3 - 1029','A',1,'RM90869','','3923','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Hole pitch undersize 13.5+/-0.3 measures 13.01 to 13.04 ','Will be taken care in future.','Will be taken care in future.','Will be taken care in future.','Next part found satisfactory.','','2009-11-16','Dinakara(G)','Dinakara(G)','','0000-00-00','Note:Production supervisor select the correct operator name ','F8003-S','Rev 0 dt 8-1-2009',21.80,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(342,'18-204A','Magellan Aerospace Wrexham','CLEAT RH','158385','D572 59294 201 01','ABM3 - 1029','A',1,'RM90869','','3922','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Hole diameter oversize 4.0+0.12 measures 4.25 to 4.26','drill bit not grinded properly due to this hole oversize.','drillbit changed and proved on dummy peice then putted on original part.','dill bit will be proved on dummy peice first.  ','CA/PA Found Satisfactory.','','2009-11-16','Dinakara(G)','Manjunatha(N.R.)','','0000-00-00','Note:Production supervisor select the correct operator name ','F8003-S','Rev 0 dt 8-1-2009',21.80,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(343,'18-152A','Magellan Aerospace Wrexham','CLEAT','2709501','F572 54597 202 01','ABM3 - 1029','E',3,'RM90864','','3904','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Thickness undersize 2.50+0.3/-0.2 measures 2.25 to 2.28','Due to holding problem.','New fixture made to solve this problem.','Same as above.','CA/PA Found Satisfactory.','','2009-11-16','Stalin(G)','Ravindra(Singh R)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',65.40,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(344,'18-085A','Magellan Aerospace Wrexham','BRACKET SUPPORT','M122420','D579 52009 200 01','L168','A',2,'RM90861','','3919','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','1)Tool dig mark on face in 1no.\r\n2)Hole pitch oversize, 19.0+/-0.3 measures 18.55 to 18.58in 1no.','Refer NC number 00338','Refer NC number 00338','Refer NC number 00338','Next part found satisfactory.','','2009-11-16','Dinakara(G)','Dinakara(G)','','0000-00-00','Note:Production supervisor select the correct operator name ','F8003-S','Rev 0 dt 8-1-2009',12.10,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(345,'18-104A','Magellan Aerospace Bournemouth','BODY TURNBUCKLE','029839','D575 40490 200','S80 FHT','E',4,'RM365144 Amnd 1','','3968','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Thread gauge NOGO answered & one no thread damage in center of the part.','Refer Non Conformance number 00403','Refer Non Conformance number 00403','Refer Non Conformance number 00403','Next batch found ok.','','2009-11-16','Dinakar(K)','Vikram(E)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(346,'18-075A','Magellan Aerospace Wrexham','ADAPTOR','18882/011','D282 50044 200PF',' L111 T6','A',8,'PRP91227 Amendment 1','','3907','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1)OD(undercut & infront of thread land)undersize & step mark noticed.Drawing dim dia 48.23/48.36 measures 48.10 to 48.20 in 7nos.\r\n2)Tool dig mark & same OD undersize 48.02to48.10 measures in 1no.','1)In future will be taken care.','1)In future will be taken care.','1)In future will be taken care.','Next part found satisfactory.','','2009-11-16','Dinakar(K)','Dinakar(K)','','0000-00-00','Note:Production supervisor select the correct operator name ','F8003-S','Rev 0 dt 8-1-2009',173.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(347,'18-087B','Magellan Aerospace Wrexham','PLATE SEALING ASSY','277474','D572 52914 200 01','ABM3 1029','B',4,'RM90855','','3917','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Thread gauge NOGO answered  & 2 to 3 thread damage.','In urgency he made a mistake.','He was strictly instructed by supervisor.Mistake were corrected & next part come without deviation.','Same as above','CA/PA Found satisfacory.','','2009-11-16','Nagaraju(T)','Nagaraju(T)','','0000-00-00','Thread gauge NOGO answered  & 2 to 3 thread damage.','F8003-S','Rev 0 dt 8-1-2009',36.40,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(348,'18-091A','Magellan Aerospace Bournemouth','BUSH','693277','D278 50164 202','S80 FHT','A',17,'RM365162 Amnd 1','','4071','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','OD undersize 45.964/45.980 measures 45.952 to 45.963','Refer Non Conformance Number 00340','Refer Non Conformance Number 00340','Refer Non Conformance Number 00340','Next part found satisfactory.','','2009-11-16','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(349,'23-042A','Goodrich Aerospace','REINFORCEMENT PLATE','57111-1','7712501-815','7075-T6511 IAW AMS-Q','TR IP 7712501-815 REV 02',1,'CRGL14416-02-09','','4113','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dimension 1.470\" +/- .03(37.34 +/-.760)meausres 1.4295/1.4380\"(36.32/36.52).','Due to setting problem as well as cutter problem.','Problem was rectified & Sorted out.','No need.','Next batch found satisfactory.','','2009-11-24','Krishna(Chowdary.G.P.)','Manjunath(K.N.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(350,'23-043A','Goodrich Aerospace','REINFORCEMENT PLATE','57111-1','7712501-816','7075-T6511 IAW AMS-Q','TR IP 7712501-816 REV 03',1,'CRGL14416-02-09','','4114','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dimension 1.470\"+/-.03(37.34 +/-.76) meausres 1.4325/1.4340\'(36.38/36.42).','Refer Non Conformance Number 00349.','Refer Non Conformance Number 00349.','Refer Non Conformance Number 00349.','Next batch found satisfactory.','','2009-11-24','Krishna(Chowdary.G.P.)','Manjunath(K.N.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(351,'23-085','Goodrich Aerospace','BASE','267852','A800268-811','7050 T7451 AMS 4050','ECN 71347 (2 Sheets)',1,'CRGL14435-03-09','','3613','','0000-00-00',NULL,'no','no','yes','no','no','no','yes','yes','no','Hole mill broken in the hole.','While running production holemill broken in part.','Holemill running from ages and process,parameters proved,then also problem coming.First time this problem facing.We predict the chips clocking in hole or collent not sufficient for holemill and tool broken for this reasons.','New holemill placed and inform to operator to check the parameter and collent for tool and will monitor in next batch production.\r\nNext batch production done and not get any problem in holenill(WO no.        )','CA/PA found satisfactory.','','2009-11-27','Krishna(Chowdary.G.P.)','Girish(Prasad P)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',6.10,'$','Closed','','yes','','','','0','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(352,'34-013','BRISTOL AEROSPACE LIMITED','STAND-FF L/H UPPER','47372','400-12603-1-905','17-4PH Stainless Ste','',1,'B70996','','2505','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','Hole shifted by 3mm.','Due to method.','After completion of CNC operation,finishing hole is done in jig boring.To come out this problem Method changed such away that all operation will complete in CNC only.','Same as above','Next part found satisfactory.','','2009-11-29','Dinakara(G)','Jayarama(M.B.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(353,'18-076A','Magellan Aerospace Wrexham','COUPLING','3344198','D282 50074 200PF',' L111 T6','A',1,'PRP91227 Amendment 1','','3889','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Tool dig mark on dia 5.50 hole in 1mm depth. ','This problem occurs due to wrong tool compansation.','Tool compansation made correct & next part get without deviation.','Introduced tool pre setter to take tool compansation.','CA/ PA fOUND SATISFACTORY','','2009-11-29','Dinakara(G)','Dinakara(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',173.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(354,'18-202A','Magellan Aerospace Wrexham','ANGLE CLEAT','351118A5','D572 59281 200 01','ABM3 - 1029','A',5,'RM90868','','4176','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Tool dig mark on face in first operation stage.','tool offset not taken properly so dig mark found on part.','instructed to operator for crosschecking offset after rough cut.','instructed to operator for crosschecking offset after rough cut.','Further parts found satisfactory.','','2009-11-29','Dinakara(G)','Dinakara(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',109.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(355,'18-097A','Magellan Aerospace Bournemouth','PLATE','50308A','D282 50100 200','L168','A',1,'RM365291','','4126','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Groove width oversize in 3.27/3.40 measures 4.60 to 4.63.','program there for 2.24mm insert but 3mm insert loaded to tool and run the job. ','next piece insert changed 2.24mm insert.','note have given to program itself that 2.24mm insert should use for the groving.','CA/PA Found satisfactory.','','2009-11-29','Dinakar(K)','Ramesh(S. Bandagi)','','0000-00-00','Note:Production supervisor select the correct operator name ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(356,'18-098A','Magellan Aerospace Bournemouth','SEAT VALVE','B6353','D282 50060 204','L110','D',1,'RM365292','','4188','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Tool dig mark on outside profile & total length undersize in 2mm.','Refer NC number 00338','Refer NC number 00338','Refer NC number 00338','','','2009-11-29','Dinakara(G)','Dinakara(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',250.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(357,'18-195A','Magellan Aerospace Wrexham','M/C BRACKET LH','179124','D572 59093 200 01','ABM3 - 1029','A',2,'RM90866','','4174','','0000-00-00',NULL,'yes','no','no','no','no','yes','no','yes','no','Hole pitch undersize 19.+/-0.3 measures 18.60 to 18.62.','Due to process problem.','Feed back given to CAD-CAM department.','For next batch process will changed.','next batch found satisfacory.','','2009-11-29','Dinakara(G)','Dinakara(G)','','0000-00-00','Note:Production supervisor select the correct operator name ','F8003-S','Rev 0 dt 8-1-2009',43.60,'$','Closed','','yes','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(358,'18-087B','Magellan Aerospace Wrexham','PLATE SEALING ASSY','277477','D572 52914 200 01','ABM3 1029','B',2,'RM90855','','4040','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Tool dig mark on top face & extra hole to be done in top face.','Tool dig mark on top face & extra hole to be done in top face.','Refer NC number 00338','Refer NC number 00338','Refer 00338','','2009-11-29','Dinakara(G)','Diwakar(R.B.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',72.70,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(359,'18-098A','Magellan Aerospace Bournemouth','SEAT VALVE','B6353','D282 50060 204','L110','D',1,'RM365292','','3766','','0000-00-00',NULL,'no','no','yes','yes','no','no','no','yes','no','Part rust & machined finish not good as per drawing.  ','Due to coolant problem.','Collant was replaced.For finishing new inserts loaded.','For come out such problems. collant level & its concentration will monitor periodically.','CA/PA Found satisfactory.','','2009-11-29','Dayananda(K.G.)','Dinakara(G)','','0000-00-00','Note:Production supervisor select the correct operator name ','F8003-S','Rev 0 dt 8-1-2009',250.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(360,'35-012','Saab AB','JACK BRACKET 1','325526 1A1','D576 50009 000 01','7050 T7651 ABM3-1030','C00',1,'1600028485','','3810','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Tool dig mark on profile in 2mm depth.','Refer NC number 00338','Refer NC number 00338','Refer NC number 00338','refer 00338','','2009-11-29','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',53.80,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(361,'18-159A','Magellan Aerospace Bournemouth','STRUT FWD INNER - LH','A349851','F574 50155 200','J4374','B01',1,'RM365235 Amnd 1','','3642','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Tool dig mark on face in 4mm depth.','This is due to operator mistake.Proper clamping not done.','This problem were come to supervisor knoweldge,he suggested to operator & shown how to clamp.','For next batch new fixture will incorporate for this operation.','further batches components found satisfactory.','','2009-11-29','Siddalinga(Tambake)','Gajendra Singh(C.)','','0000-00-00','Note:Production supervisor select the correct operator name ','F8003-S','Rev 0 dt 8-1-2009',65.70,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(362,'18-163A','Magellan Aerospace Bournemouth','STRUT MID RIB - LH','A349808','F574 50160 200','J4374','B02',1,'RM365238 Amnd 1','','3531','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Thickness 2.40+0.3/-0.2 measures 1.82 to 1.92.','REFER NC number 00361','REFER NC number 00361','REFER NC number 00361','further batches found sdatisfactory.','','2009-11-29','Siddalinga(Tambake)','Rakeshbabu(V)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',68.30,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(363,'18-159A','Magellan Aerospace Bournemouth','STRUT FWD INNER - LH','A349851','F574 50155 200','J4374','B01',1,'RM365235 Amnd 1','','3930','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Total length undersize 10mm.','Refer NC number 00361','Refer NC number 00361','Refer NC number 00361','Same as NC:00361.','','2009-11-29','Siddalinga(Tambake)','        Gajendra Singh(C.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',65.70,'$','Closed','','yes','','','','0',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(364,'18-122A','Magellan Aerospace Bournemouth','FORKEND ASSEMBLY','723001','D572 50462 201','S98 FHT','J01',4,'RM365139 Amnd 1','','3744','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Bore 15.895 +0.018 measures 15.915 to 16.02.','Due to wrong adjustment in boring bar.','Proper training give to the opertor regarding the boring bar funtions.','In future will be taken care.','CA/PA Found satisfactory.','','2009-11-29','Dinakara(G)','Sunil Kumar(K.J.)','','0000-00-00','Note:Production supervisor select the correct operator name ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(365,'18-123A','Magellan Aerospace Bournemouth','FORK END OUT BD','706845','D575 41546 202','S80 FHT','B',1,'RM365147 Amnd 1','','3915','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Tool dig mark on sphere in 3mm depth.','Refer NC number 00338','Refer NC number 00338','Refer NC number 00338','Refer NC number 00338','','2009-11-29','Dinakara(G)','Dinakara(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',40.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(366,'18-108A','Magellan Aerospace Bournemouth','FORK END OUT BD','706845','D575 41546 200','S80 FHT','B',4,'RM365147 Amnd 1','','3738','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1)Dia 12.70 undersize before threading operation in 1no.\r\n2)Bore 11.00+0.018 measures 11.05 to 11.08 ','1)Due to drill problem.\r\n2)Due to operator mistake.because boring bar adjustment not done properly.','1)will be taken care in future.\r\n2)Proper training given to operator regarding boring bar adjustment.','Same as the above.','CA/PA Found satisfactory.','','2009-11-29','Dinakara(G)','Mohan(Kumar C.M.)','','0000-00-00','Note:Production supervisor select the correct operator name ','F8003-S','Rev 0 dt 8-1-2009',40.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(367,'05-179','HAL-Aircraft','TRAVERSE BEAM - LH','XP50644/1-08-A320','D521-10353-200-00-E0','7175 T 7351','NA',3,'C/146/ES/COMP','','3761','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','RH Hole co ordinates noticed in LH Parts.','This is happened due to wrong jig used by fitter. ','After come to the knowledge.LH jig used to the LH part.problem was sorted out.','**Required JIG will provide.\r\nFitter was strictly instructed & warned,it should not happened in future,if happened will terminated from his job.','next part found satisfactory.','','2009-11-29','Nagaraju(T)','Rajesh(T)','','0000-00-00','RH Hole co ordinates noticed in LH Parts.','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(368,'18-102A','Magellan Aerospace Bournemouth','BARREL-STRUT','687946','D572 50463 200','S98 FHT','F',2,' RM365136 Amnd 1','','3946','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no',' ID thread NOGO answered. ','Thread guage not checked.','Instruction given to the all operators that,if any threading operation, should check thread with the help of calibrated thread gauges.','Suggested to the production supervisors provide necessary gauges or tools which are require for the production. ','CA/PA Found satisfactory.','','2009-11-30','Dinakar(K)','Narasimhamurthy(K.G.)','','0000-00-00','Operator Name;Rajesh T. Narasimha Murthy R. Nithin S.','F8003-S','Rev 0 dt 8-1-2009',32.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(369,'18-105A','Magellan Aerospace Bournemouth','FORKEND ASSEMBLY','723001','D572 50462 200','S98 FHT','J01',2,'RM365139 Amnd 1','','3743','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Bore 14.308+0.018 measures 14.310 to 14.334 in 1no & Bore 15.895+0.018 measures 15.909 to 15.920.','Due to the boring bar problem.','Boring bar was serviced & error in boring bar was corrected.','All boring bar will cross check before taking to the operation.','CA/PA Found satisfactory.','','2009-11-30','Dinakara(G)','Dinakara(G)','','0000-00-00','Note:Production supervisor select the correct operator name ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(370,'05-088','HAL-Aircraft','TRAVERSE BEAM - RH','XP50644/1-08-A320','D521-10353-201-00-E0','7175 T 7351','NA',1,'C/146/ES/COMP','861','3755','2235','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Over all Flange height reduced by 4 mm.Due to operator mistake.','In 1st set up outer cut out not done for full depth but it should be happened.operator made a mistake in 2nd su.In 2nd su he want to remove extra material so he kept -4mm in work offset.','Corrected for next part.','In future will be taken care.','parts found satisfactory after  corrections done in work offset.','','2009-12-02','Siddalinga(Tambake)','Gajendra Singh(C.)','','0000-00-00','Over all Flange height reduced by 4 mm.','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(371,'18-104A','Magellan Aerospace Bournemouth','BODY TURNBUCKLE','029839','D575 40490 200','S80 FHT','E',4,'RM365144 Amnd 1','','3968','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Thread gauge NOGO answered & one no thread damage in center of the part.\r\n','due to centeried problem.\r\ndue to cutting pass more no of pass 50.\r\nThreading insert broken while running so nogo gauge answered','for next piece centeried had been set.\r\nno of pass had reduiced for 30 pass.\r\nInsert changed for next piece','for dummy piece centeried has set.\r\nfor 30 no\'s pass program had been set.\r\nfor every 15no\'s inserts will be checked. ','CA/PA Found satisfactory.','','2009-12-03','Dinakar(K)','Vikram(E)','','0000-00-00','Operator Name;Paramesh K. Vikram E. Ramesh S. Bandagi','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(372,'34-005','BRISTOL AEROSPACE LIMITED','DEFLECTOR WIPERPOST WSPS','349321','446 83031 1 901','7075-T651','D, EM101307 Iss AU',1,'B62472 Rev-09','','4262','','0000-00-00',NULL,'no','yes','yes','no','no','no','yes','no','no','Dig mark noticed on the top of the wall.','Refer Non Conformance number 00414.','Refer Non Conformance number 00414.','Refer Non Conformance number 00414.','Next part found satisfactory.','','2009-12-04','Krishna(Chowdary.G.P.)','Siddaramappa()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(373,'34-028','BRISTOL AEROSPACE LIMITED','BUSHING AFT MOUNT','E81166','400-12628-1-905','AMS-QQ-S-763 321 CRE','EM 104302 Iss. A, EM 105092 Iss. C, ECN: 39029 Is',2,'B70996','','3793','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Thread Depth out of tolerance by 0.5 to 1.0 mm.','Due to operator mistake.','Instructed to operator before starting threding operation should ensure the tool offset.','Introduced tool pre-setter.','CA/PA Found satisfactory.','','2009-12-04','Nagaraju(T)','Irappa(Badiger)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(374,'18-180A','Magellan Aerospace Bournemouth','PLATE RETAINING','966A/E','F575 55077 200','S524','A',1,'RM365240 Amnd 1','','2286','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Outside & inside profile undersize in 2mm. ','This problem occurs due to operator used damaged collet holder.while running program cutter has runout.','Replaced the damaged collet holder.next part found correct.','Instructed to operator before starting job setting should observe required holders & cutters are in good condition.If any problems found inform to supervisors.','CA/PA found satisfactory.','','2009-12-06','Dinakara(G)','        Sathish(Y.R.)','','0000-00-00','Outside & inside profile undersize in 2mm. ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(375,'18-153A','Magellan Aerospace Wrexham','BRACKET','343504A7','F579 52514 200 48 01','ABM3-1029','A',1,'RM90862','','4057','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Base radius R3.0 undersize measured 0.4mm.','Due to wrong tool selection from ATC.','Reruired tool loaded & next part comes without deviation.','In future will be taken care before running on part.','found ok','','2009-12-06','Krishna(Chowdary.G.P.)','Prakash(Acharya)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(376,'18-284A','Magellan Aerospace Bournemouth','SPINDLE FOR CLACK ALVES O','029109','A281-40019-200','S80 FHT','A',15,'RM368854','','2735','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1)Hole pitch 2.286/2.540 measures 1.98 to 2.25 in 12nos.\r\n2)Hole 1.62+0.12 measures 1.72 to 1.75 & hole oblong in 3nos.','1)Due to part bend,\r\n2)Due to drill runout.','1)In future before loading the RM to the machine.if bend observed in raw material,will be removed.\r\n2)will be taken care.','Same as above','Next part found satisfactory.','','2009-12-06','Stalin(G)','Mohan(E)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(377,'18-105A','Magellan Aerospace Bournemouth','FORKEND ASSEMBLY','723001','D572 50462 200','S98 FHT','J01',2,'RM365139 Amnd 1','','3742','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','1)One thread damage in center of the part in 1no.\r\n2)Keyway opposite side in 1no.','1)While removing from fixture it is happened.\r\n2)Job Wrong loaded by operator. ','1)Taken care for next part.\r\n2)Instructed to operator regarding the job loading & unloading. ','Same as Above.','CA/PA Found satisfactory.','','2009-12-06','Dinakara(G)','Dinakara(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(378,'18-116A','Magellan Aerospace Bournemouth','ASSEMBLY FORK END','49628','F575 51377 200','L168','A',4,'RM365155 Amnd 1','','3746','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1)Bore 12.00+0.018 measures 12.019 to 12.025 in 2nos.\r\n2)Thread effective dia 13.093/13.174 measures 12.95 to 13.04 in 2nos.','Refer Non Conformance Number 00409','Refer Non Conformance Number 00409','Refer Non Conformance Number 00409','Refer NCR00409','','2009-12-06','Dinakara(G)','Dinakara(G)','','0000-00-00','1)Bore 12.00+0.018 measures 12.019 to 12.025 in 2nos.\r\n2)Thread effective dia 13.093/13.174 measures 12.95 to 13.04 in 2nos.','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(379,'18-091A','Magellan Aerospace Bournemouth','BUSH','693277','D278 50164 202','S80 FHT','A',17,'RM365162 Amnd 1','','4071','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','OD 45.964/45.980 measures 45.950 to 45.966','Refer NC number 00404','Refer NC number 00404','Refer NC number 00404','RC/CA/PA TO BE ENTERED','','2009-12-06','Dinakar(K)','Dinakar(K)','','0000-00-00','OD 45.964/45.980 measures 45.950 to 45.966','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(380,'18-121A','Magellan Aerospace Bournemouth','BARREL - STRUT','687946','D572 50463 201','S98 FHT','F',11,' RM365136 Amnd 1','','4087','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','ID Thread gauge NOGO answered.','Refer Non Conformance Number 00404','Refer Non Conformance Number 00404','Refer Non Conformance Number 00404','Refer NCR00404','','2009-12-06','Dinakar(K)','Dinakar(K)','','0000-00-00','ID Thread gauge NOGO answered.','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(381,'18-118A','Magellan Aerospace Bournemouth','BEARING HOUSING','725059','D275 40005 200','S130 FHT','C01',1,'RM365159 Amnd 1','','3999','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Thread effective dia 45.942/46.036 measures 45.913 to 45.92','Refer Non Conformance Number 00404','Refer Non Conformance Number 00404','Refer Non Conformance Number 00404','RC/CA/PA TO BE ENTERED','','2009-12-06','Dinakar(K)','Dinakar(K)','','0000-00-00','Thread effective dia 45.942/46.036 measures 45.913 to 45.92','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(382,'18-121A','Magellan Aerospace Bournemouth','BARREL - STRUT','687946','D572 50463 201','S98 FHT','F',20,' RM365136 Amnd 1','','3947','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','ID Thread gauge NOGO answered.','Refer Non Conformance Number 00404','Refer Non Conformance Number 00404','Refer Non Conformance Number 00404','RC/CA/PA TO BE ENTERED.','','2009-12-06','Dinakar(K)','Dinakar(K)','','0000-00-00','ID Thread gauge NOGO answered.','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(383,'18-001A','Magellan Aerospace Wrexham','BRACKET SUPPORT - LH','719228A9','D361 50110 200 01','ABM3-1029','A',1,'RM90857','','4048','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Bore 7.937/7.959 is in feedlins observed  & oversize. Then 1x45 deg chf is done, so Drg not calls for chf. ','This problem occurs due to insert chipout.','New insert loaded & there is no deviation get for next part.','For every operator instructed to check inserts after every 5 components.','CA/PA Found satisfactory.','','2009-12-07','Dinakara(G)','Dinakara(G)','','0000-00-00','Bore 7.937/7.959 is in feedlins observed  & oversize. Then 1x45 deg chf is done, so Drg not calls for chf. ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(384,'18-208A','Verdict Aerospace Components Ltd.','SPRING RETAINER','638857','D321 40203 220','S98','L',2,'55568','','3869','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Bore 17.51/17.53 measures 17.533 to 17.536.','Refer NC number 00305.','Refer NC number 00305.','Refer NC number 00305.','Refer NCR00305','','2009-12-07','Dinakar(K)','Dinakar(K)','','0000-00-00','Note:Production supervisor select the correct operator name ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(385,'18-111A','Magellan Aerospace Bournemouth','BODY TURNBUCKLE INTMD','696913','D575 41544 200','S80 FHT','A',1,'RM365149 Amnd 1','','3955','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Thraed damaged & nogo answered.','Refer Non Conformance Number 00403','Refer Non Conformance Number 00403','Refer Non Conformance Number 00403','Refer NCR00403','','2009-12-07','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(386,'18-112A','Magellan Aerospace Bournemouth','BODY TURNBUCKLE INNER','696913','D575 41541 200','S80 FHT','A',4,'RM365153 Amnd 1','','3991','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','ID dia oversize before threading operation.','Refer Non Conformance Number 00405','Refer Non Conformance Number 00405','Refer Non Conformance Number 00405','Refer NCR00405','','2009-12-07','Dinakar(K)','Dinakar(K)','','0000-00-00','ID dia oversize before threading operation.','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(387,'18-152A','Magellan Aerospace Wrexham','CLEAT','2709501','F572 54597 202 01','ABM3-1029','E',3,'RM90864','','3903','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Thickness 2.50+0.3/-0.2 measures 2.15 to 2.25.','Refer Non Conformance Number 00393','Refer Non Conformance Number 00393','Refer Non Conformance Number 00393','Next production batch found ok.','','2009-12-07','Stalin(G)','Ravindra(Singh R)','','0000-00-00','Thickness 2.50+0.3/-0.2 measures 2.15 to 2.25.','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(388,'18-119A','Magellan Aerospace Bournemouth','HOUSING OUT B D BRG 3','CB894702','D275 40011 200','S130 FHT','D01',4,'RM365160 Amnd 1','','4079','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1)ID & OD ovality in (-)0.010mm (+)0.005mm in 3nos.\r\n2)1.5 thickness undersize, measures 0.5 to 0.6 in 1no.','Refer Non Conformance Number 00416','Refer Non Conformance Number 00416','Refer Non Conformance Number 00416','Next part found satisfactory.','','2009-12-07','Dinakar(K)','Dinakar(K)','','0000-00-00','1)ID & OD ovality in (-)0.010mm (+)0.005mm in 3nos.\r\n2)1.5 thickness undersize, measures 0.5 to 0.6 in 1no.','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(389,'18-078A','Magellan Aerospace Wrexham','ADAPTOR','18883/012','A282 50081 200PF',' L111 T6','A',5,'PRP91227 Amendment 1','','4086','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Undercut dia & infront of thread dia undersize 2.399/2.404\" measures 2.3940. ','Insert Broker','Insert changed','Insert to be changed for every 100 NOs. ','Further produced parts found OK.','','2009-12-07','Dinakar(K)','op(op)','','0000-00-00','Note:Production supervisor select the correct operator name ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(390,'18-122A','Magellan Aerospace Bournemouth','FORKEND ASSEMBLY','723001','D572 50462 201','S98 FHT','J01',4,'RM365139 Amnd 1','','4077','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1)Bore 15.895+0.018 measures 15.919 to 15.925 in 3nos.\r\n2)Thread damaged in 1no.','Refer Non Conformance Number 00416','Refer Non Conformance Number 00416','Refer Non Conformance Number 00416','refer 00416','','2009-12-07','Dinakara(G)','Dinakara(G)','','0000-00-00','1)Bore 15.895+0.018 measures 15.919 to 15.925 in 3nos.\r\n2)Thread damaged in 1no.','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(391,'18-226A','Magellan Aerospace Bournemouth','BRKT - NUT RETAINER','4345888','F572 53828 200','L168','A',2,'RM366515','','3525','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','1)Tool dig mark on face in 1no.\r\n2)Inside profile oversize & profile not done in 1no.','Refer Non Conformance Number 00406','Refer Non Conformance Number 00406','Refer Non Conformance Number 00406','Next part found satisfactory.','','2009-12-07','Dinakara(G)','Dinakara(G)','','0000-00-00','1)Tool dig mark on face in 1no.\r\n2)Inside profile oversize & profile not done in 1no.','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(392,'18-101A','Magellan Aerospace Bournemouth','TUBE-STRUT','56000','D572 50464 202','T45','F',1,'RM365135 Amnd 1','','4076','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Total length undersize Dim 211.0+/-0.4 measures 210.02.  ','Due to part butting problem.part was not butted properly by operator.','Next piece made correct.','To avoid these kind of problems,instructed to operator after loading the part should check material is sufficient or not for the finish part.','CA/PA Found satisfactory.','','2009-12-07','Dinakar(K)','Dharanishankar()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(393,'18-030A','Magellan Aerospace Bournemouth','PIN','579901','D278 50156 200','S130 FHT','A',31,'RM365133 Amnd 1','','4129','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Total length undersize,5.50/5.60 measures 5.28 to 5.48.','Due to operator mistake.','Adviced to prevent such mistakes in future.','Adviced to prevent such mistakes in future.','CA/PA Found satisfactory.','','2009-12-07','Stalin(G)','Pinto(N.L.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(394,'18-114A','Magellan Aerospace Bournemouth','NUT SLIM 1/2 UNJF - LH','694000','D575 40499 200','S80 FHT','D01',1,'RM365152 Amnd 1','','3863','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Dia 1.15 hole near dig mark. ','This is due to manual mistake.','Taken care for next component.','To over come this kind of manual mistakes, desided to hole deburring should be done in machine.So procured BOSCH make multi purpose drilling & deburring machine.','CA/PA Found satisfactory.','','2009-12-07','Nagaraju(T)','Irappa(Badiger)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(395,'34-027','BRISTOL AEROSPACE LIMITED','SPACER','8971641','400-12618-1-905','4340 Steel Per SAE-A','EM 104302 Iss. A, EM 105092 Iss. C',1,'B70996','','3856','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','ID oversize 0.04mm out of tolerance.','Due to process problem.','Feed back given to CAD-CAM department regarding the process error.','Feed back accepted by the CAD-CAM department & process has been changed.','CA/PA Found satisfactory.','','2009-12-07','GIREESH.K.(KULKARNI)','Dinakara(G)','','0000-00-00','FAI Prooving part.','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(396,'18-213A','Verdict Aerospace Components Ltd.','END CAP','48469','D321 40209 200','L168','A',1,'55568','','4084','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','OD undersize 0.5mm.','Due to wrong compansation of the inserted tool.','Next piece tool compansation made correct & problem sorted out.','Will be taken care.','CA/PA Found satisfactory.','','2009-12-07','Dinakar(K)','Dinakar(K)','','0000-00-00','Note:Production supervisor select the correct operator name ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(397,'18-211A','Verdict Aerospace Components Ltd.','PLUNGER','694000','D321 40205 200','S80-FHT','H01',5,'55568','','4081','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','1)OD dia17.446/17.464 measures 17.435 to 17.439 in 2nos & dia 9.965/9.975 measures 9.950 to 9.958 in 2nos. \r\n2)Dia 8.5 hole in drill bit brocken in 1no.','1)Refer NC number 00305.\r\n2)Due to tool over hang.','1)Refer NC number 00305.\r\n2)Next piece tool was set as per required length.','1)Refer NC number 00305.\r\n2)In future will be taken care.','Next part found satisfactory.','','2009-12-07','Dinakar(K)','Dinakar(K)','','0000-00-00','Note:Production supervisor select the correct operator name ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(398,'18-209A','Verdict Aerospace Components Ltd.','BODY ASSEMBLY','9866','D321 40204 202','L168','D',2,'55568','','4162','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','1)Dia 3.20 hole oblong measures 4.20dia in 1no.\r\n2)Dia 50.0 OD undersize in 2mm in 1no.\r\n','1)Due to drill over hang.\r\n2)Due to holding problem,holding pressure is low but speed is high SO above deviation occur.','1)Short carbide drill introduced to avoid hole oblong.\r\n2)Holding problem was sorted out & suitable parameter set to avoid the above problem','Same as above','Next part found satisfactory.','','2009-12-07','Dinakara(G)','Paramesh(K)','','0000-00-00','2)Supervisor Name:Dinakara(k)\r\n2)Operator Name  :Paramesh(k)','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(399,'18-108A','Magellan Aerospace Bournemouth','FORK END OUT BD','706845','D575 41546 200','S80 FHT','B',4,'RM365147 Amnd 1','','3738','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1)Bore 11.0+0.018 measures 11.023 to 11.026 in 3nos.\r\n2)Dia12.7 undersize in before threading operation in 1no.','1)Due to reamer runout.\r\n2)Due to drill problem.','1)Problem rectified & replace the reamer.\r\n2)New carbide drill replaced.','Will be taken care.','CA/PA Found satisfactory.','','2009-12-07','Dinakara(G)','Dinakara(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(400,'18-075A','Magellan Aerospace Wrexham','ADAPTOR','257067','D282 50044 200PF',' L111 T6','A',1,'PRP91227 Amendment 1','','4085','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Thread gauge NOGO answered in full thread.','while running thread were damage.','next piece taken care.','before threading operation,we will cross check threading insert is OK or NOT.','CA/PA Found satisfactory.','','2009-12-07','Dinakar(K)','Narasimhamurthy(K.G.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(401,'18-118A','Magellan Aerospace Bournemouth','BEARING HOUSING','725059','D275 40005 200','S130 FHT','C01',3,'RM365159 Amnd 1','','3867','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Thraed damaged in 1no,& thickness 1.5+0.3/-0.2 measures 1.05 to 1.23 in 2nos.','due to wrong refarence, it was happend.','operator instructed and trained.','same as above.','RC/CA/PA TO BE ENTERED','','2009-12-07','Dinakar(K)','Narasimhamurthy(K.G.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(402,'34-031','BRISTOL AEROSPACE LIMITED','PIN, SHEAR, ACCESS DOOR','4EE6','400-12748-1-905','303 CRES AMS 5640','EM 104302 Iss. A, EM 105092 Iss. CEM 104302 Iss.',1,'B70996','','3796','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Hexagon face in dig mark noticed.','Refer Non Conformance Number 00406','Refer Non Conformance Number 00406','Refer Non Conformance Number 00406','Next part found satisfactory.','','2009-12-07','Dinakara(G)','Diwakar(S)','','0000-00-00','FAI prooving part.','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(403,'18-104A','Magellan Aerospace Bournemouth','BODY TURNBUCKLE','654734','D575 40490 200','S80 FHT','E',3,'RM365144 Amnd 1','','4075','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Thread NOGO gauge answered.','In setting, nogo gauge answered due to wrong refarence.','operator instructed and trained.','same as above.','Next part found satisfactory.','','2009-12-07','Dinakar(K)','Rajesh(T)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(404,'18-113A','Magellan Aerospace Bournemouth','ADJUSTER','671608','D575 40496 200','S80 FHT','G',7,'RM365151 Amnd 1','','3748','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Thread LH gauge NOGO answered in 3nos,& ID thread damaged in 4nos.','Due to shrinkage in the 2nd set up it was happend.','to be stabilize the process.','to be stabilize the process.','Next part found satisfactory.','','2009-12-07','Dinakar(K)','Narasimha(Murthy R)','','0000-00-00','Note:Production supervisor select the correct operator name','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(405,'18-113A','Magellan Aerospace Bournemouth','ADJUSTER','694002','D575 40496 200','S80 FHT','G',13,'RM365151 Amnd 1','','3749','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','ID Thread NOGO answered in 5nos, & inside thread chf oversize 2mm in 1no,& thread damaged in 7 nos.','Due to shrinkage in the 2nd set up it was happend.','To be stabilize the process.','To be taken.','Next part found satisfactory.','','2009-12-07','Dinakar(K)','Narasimha(Murthy R)','','0000-00-00','Nithin.S and Rajesh.T both are held responsible.','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(406,'18-111A','Magellan Aerospace Bournemouth','BODY TURNBUCKLE INTMD','696913','D575 41544 200','S80 FHT','A',1,'RM365149 Amnd 1','','3990','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Tool dig mark on near the bore. ','Due to operator mistake he was not taken tool reference.','Instructed & shown how to take tool reference.','Introduced tool pre setter, to avoid such kind of mistakes.','CA/PA Found satisfactory.','','2009-12-07','Dinakara(G)','Dinakara(G)','','0000-00-00','Tool dig mark on near the bore. ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(407,'18-106A','Magellan Aerospace Bournemouth','EYE END INBOARD','723001','D575 41542 200','S98 FHT','D',2,'RM365154 Amnd 1','','3745','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Bore 31.02+0.25 measures 31.050 to 31.053','Refer Non Conformance Number 00411','Refer Non Conformance Number 00411','Refer Non Conformance Number 00411','','','2009-12-07','Dinakara(G)','Dinakara(G)','','0000-00-00','Bore 31.02+0.25 measures 31.050 to 31.053','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(408,'18-107A','Magellan Aerospace Bournemouth','LINK ASSY','1244','D574 50553 200','DTD 5014','A',5,'RM365142 Amnd 1','','3750','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1)Bore 15.870+0.015 measures 15.889 to 15.892 in 4nos.\r\n2)Part is brockened in two pieces in 1no.','while improoving the process, it was happend.','process stablized with special tool .','SAME AS ABOVE.','CA/PA Found satisfactory.','','2009-12-07','Dinakara(G)','Dinakara(G)','','0000-00-00','1)Bore 15.870+0.015 measures 15.889 to 15.892 in 4nos.\r\n2)Part is brockened in two pieces in 1no.','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(409,'18-097A','Magellan Aerospace Bournemouth','PLATE','50308A','D282 50100 200','L168','A',1,'RM365291','','3747','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Thread gauge NOGO answered in full depth.','After pre drilling operation hole got ovality,so thread is not form uniformaly.so Thread gauge NOGO answered in full depth. ','For next piece suitable drill loaded & cross checked the threaded hole.problem were sorted out.','Same as above','CA/PA Found satisfactory.','','2009-12-07','Dinakara(G)','Dinakara(G)','','0000-00-00','Thread gauge NOGO answered in full depth.','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(410,'18-090A','Magellan Aerospace Bournemouth','BUSH','697431','D278 50164 200','S80 FHT','A',2,'RM365162 Amnd 1','','4222','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','OD 39.964/39.980 measures 39.957 to 39.960.','In large production quantity it was happend in b/w the process. Due to insert wear.','corrective action not required.','same as above.','Next part found satisfactory.','','2009-12-07','Dayananda(K.G.)','Shantala Devi(V)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(411,'18-282A','Magellan Aerospace Bournemouth','FUNK PINS','583915','A572 43263 200','S98','H',17,'RM368853','','2733','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1)OD 17.350/17.388 measures 17.308 to 17.348 in 4nos.\r\n2)Hole pitch oversize in 5nos.\r\n3)ID 7.93+0.15 measures 8.0 to 8.11 in 2nos.\r\n4)Hole 3.58+0.12 measures 3.73 to 3.75 in 6nos.','while improoving the process, it was happend.','process stablized with special tool','same as aboue.','Next part found satisfactory.','','2009-12-07','Dinakar(K)','Dinakar(K)','','0000-00-00','Note:Production supervisor select the correct operator name','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(412,'18-117A','Magellan Aerospace Bournemouth','HOUSING-OUT BD BRG','662385','D275 40004 200','S130 FHT','C01',5,'RM365157','','4078','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','ID & OD ovality means ID oversize & OD undersize.','Refer Non Conformance number 00411','Refer Non Conformance number 00411','Refer Non Conformance number 00411','Refer NCR00411','','2009-12-07','Dinakar(K)','Dinakar(K)','','0000-00-00','Note:Production supervisor select the correct operator name','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(413,'35-013','Saab AB','JACK BRACKET 1','330707-1B1','D576 50009 001 01','7050 T7651 ABM3-1030','C00',1,'PA1217','','4107','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Tool down 0.65 height undersize.','Refer Non Conformance Number 00414','Refer Non Conformance Number 00414','Refer Non Conformance Number 00414','Refer 00414','','2009-12-07','Krishna(Chowdary.G.P.)','Basavaraja(S. Jr.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(414,'35-006','Saab AB','HINGE BRACKET 3','328471/1C1','D576 50006 000 01','7050 T7651 ABM3-1030','C00',1,'PA1217','','4134','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Tool down 0.65 height undersize. ','this cause occure due to machine problem.while running dia 10ballnose rib top finish, z-axis down upto 0.65mm.','we called service engineer to rectify this problem but this problem was not sorted out till the date by service personal.','we made some periodic check list like,\r\n1)move all the axis indivisually over the full range TO & FRO, twice and check for any jork vibrations,rubbibg noice etc.\r\n2)check input voltage it should be within 400-420Volts.','CA/PA Found satisfactory.','','2009-12-07','Krishna(Chowdary.G.P.)','Dhananjaya(N)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(415,'18-101A','Magellan Aerospace Bournemouth','TUBE-STRUT','56000','D572 50464 202','T45','F',32,'RM365135 Amnd 1','','4420','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Inner diameter 28.5+0.1/-0.1 measures 29.50 in all the parts in one side','1)By mistake insted of 29.50 he reads 28.50 and written in the stage inspection report and given the clearance for production.\r\n2) For sampling inspection operator did not check the parts but written the stage inspection report (1st off coppied)','Operator and Inspector seriously instructed.','GO and NOGO gauge is made to check that dimension.','CA/PA Found satisfactory.','','2009-12-10','Dinakar(K)','Nithin(S)','','0000-00-00','Dharani shanker is held responsible for this rejection','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(416,'34-020','BRISTOL AEROSPACE LIMITED','BRACKET, AFT MOUNT-APU','47372','400-12611-1-905','17-4PH Stainless Ste','EM 104302 Iss. A, EM 105092 Iss. C, ECN: 39936 Is',1,'B70996','','3783','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Bore Diameter 15.875mm +/-.1270,measures 16.02mm.','This problem occur due to cutter radius compansation problem.','Operator clearly instructed & trained regarding CRC programs by Supervisor.','We are trying to adopt center line programs.','Next batch found ok','','2009-12-11','Dinakara(G)','Manjunatha(N.R.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(417,'23-075','Goodrich Aerospace','EDGE TEE','4464603','7716204-801','7075 T7351 AMS 4078','ECN 55818',1,'CRGL14435-02-09','','4320','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Thickness undersize 3.81/4.31 measures 3.50 to 3.60.','REFER Non Conformance Number 00414','REFER Non Conformance Number 00414','REFER Non Conformance Number 00414','CA/PA Found satisfactory.','','2009-12-15','Krishna(Chowdary.G.P.)','Manjunath(K.N.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(418,'08-001','Infotech HAL Limited','PLATINE','2551501','8004224Y00','2024 T351','Nil',1,'IHL/PO/09-10/010','','4478','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','Dimension 5.0 + .0120 meassures 9.5mm.','the program was made to finish the Dim 5.0 +0.012 with cutter radius compensation, but that option was not enabled & verified when the program was posted.so the program shiftted by 4.5mm. ','Rectivied the program error & corrected.\r\nIn the next piece this Dim maintained as per the tolerence','when giving the cutter radius compensation program it should be verified before post the program.','Next batch found satisfactory.','','2009-12-18','Mahesh(B.T.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(419,'28-005','Ellanef Manufacturing Corporation','SHOULDER BOLT','95410','162A3109-1','15-5PH per AMS5659','NA,PL Rev-A, DL Rev-',4,'99937 Rel-1','','4224','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Drill broken in 04nos.','It happened because of improper drill loaded to the drill check.Drill runout was more.','Carbide drill was introduced and loaded to the collet holder.','Informed to the operator,if they are loading any drill for any components should check,\r\n(1) Sharpness of the drill.\r\n(2) Run-out of the drill.etc','found ok','','2009-12-22','Dinakara(G)','Manjunatha(N.R.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(420,'28-006','Ellanef Manufacturing Corporation','SHOULDER BOLT','95755','162A3109 2','15-5PH per AMS5659','A',10,'99939 Rel-1','','4225','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Drill cut in 05nos and step observed on OD in 05nos.','Refer Non Conformance number 00419.','Refer Non Conformance number 00419.','Refer Non Conformance number 00419.','Refer 00419','','2009-12-22','Dinakara(G)','Manjunatha(N.R.)','','0000-00-00','05nos rejection is towards Dinakar.K','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(421,'35-011','Saab AB','HINGE BRACKET 5','330705 2A1','D576 50008 001 01','7050 T7651 ABM3-1030','C00',3,'PA1217','','4581','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','1) Wall thickness 10.15 +/-0.25 measures 9.66 in one no.\r\n2) Dia22.236(H7) measures 22.70 in 2 no\'s.','1)Tool length compensation problem.\r\n2)Boring bar problem.','1)Tool length compensation made correct.\r\n2)Servicing has to be done.','Same as above.','ca/pa found satisfactory.','','2009-12-31','Krishna(Chowdary.G.P.)','Nagaraj(G. Nadiger)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(422,'35-009','Saab AB','HINGE BRACKET 4','317180 2B1','D576 50007 001 01','7050 T7651 ABM3-1030','D00',1,'PA1217','','4375','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','bore dia22.225 (H7) measures 22.50','Due to boring bar problem.Boring bar repeatability is not good.','Boring bar fine adjustment done.Found next piece correct.','All boring bar servicing tobe done.','CA/PA Found satisfactory.','','2009-12-31','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(423,'05-088','HAL-Aircraft','TRAVERSE BEAM - RH','XP50644/1-08-A320','D521-10353-201-00-E0','7175 T 7351','NA',1,'C/146/ES/COMP','','4665','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','Major tool dig mark noticed to a depth of 5mm and length 60mm ( out side 2mm rib).',' New process was introduced to reduce the cycle time.In program header G43(ie,TOOL LENGTH COMPENSATION)was missing,so dia60 cutter digged in rapidly.','Now new process planning was dropped.Jobs are running in old process.','Planning to incorporate fanuc(control)header & footer into the CIMATRON SOFTWARE. ','parts found satisfactory.','','2010-01-01','Siddalinga(Tambake)','Narayanappa(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(424,'18-081A','Magellan Aerospace Bournemouth','RIB # 14 AFT - RH','334593 1E1','L575 52364 201','ABM3-1029','E00',1,'RM365131','','4610','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Major tool dig mark noticed on contour rib and material was chip out at the vertical rib.','Due to operator error.For RH part VMC-70L bed tapped hole doe\'s not suit sufficiently,so operator anti clockwise rotated bed to clamp the job,after completion of the clamping he should rotate the bed for it\'s original possition but he did not done.He called the tool from ATC, when M6 command is activated bed came it\'s original possition in that time accident occurs between job & rotary column.','For next part rotary was not disturbed,as per regular process job loaded & next piece found OK.','Will be taken care in future.','Next batch found satisfactory.','','2010-01-01','Krishna(Chowdary.G.P.)','Girish(Prasad P)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(425,'35-005','Saab AB','HINGE BRACKET 2','335084','D576 50005 001 01','7050 T7651 ABM3-1030','C00',1,'PA1217','','4521','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','tool dig mark noticed in b/w slot to a length of 50mmx2mm in zig zag manner.','Due to machine problem.','machine ATC servicing has been done.','still under observation.','Next part found satisfactory.','','2010-01-03','Krishna(Chowdary.G.P.)','Nagaraj(G. Nadiger)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(426,'35-006','Saab AB','HINGE BRACKET 3','328471/1B1','D576 50006 000 01','7050 T7651 ABM3-1030','C00',2,'','','4014','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','1) base thickness 3.4 +/-0.25 measures 2.9 in 1no.\r\n2) web thickness 10.15 +/-0.25 measures 9.84mm in 1no.','Butting problem. part not butted properly to dovel pins and above deviations accured.','correction has been done.next piece found without deviation.','Inform to operator to crosscheck the butting with feeler guage and then start the prg.','CA/PA Found satisfactory.','','2010-01-03','Krishna(Chowdary.G.P.)','Nagaraj(G. Nadiger)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(427,'30-013','Gardner Aerospace Burnley Limited','FRAME GEAR RIB IFS - LH','2248791B1','L575 51890 200','ABM3-1029 T7651','A, ECN:PW69999001JB47, PG60049M01JA73',1,'','','4744','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Base thickness redused by 2.0 mm in all pockets.','Dia 25R2 Tool length compensation problem.','All the tool removed from ATC.tool length cross checked.','Will be taken care in future.','cross checked 3 to 4 production batches and found satisfactory.','','2010-01-06','Siddalinga(Tambake)','Venkatesh(B)','','0000-00-00','Base thickness redused by 2.0 mm in all pockets.','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(428,'28-004','Ellanef Manufacturing Corporation','PIN','95753','161A2332-1','15-5PH per AMS5659','NA',1,'','','4484','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','ID MEASURES 0.350 mm OUT OF TOLERANCE.','While running insert broken then broken insert rubbed to the ID & get plus side.','New insert loaded & runned next part.next part get with out deviation.','not required.','CA/PA Found satisfactory.','','2010-01-07','Dinakar(K)','Narasimha(Murthy R)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(429,'28-003','Ellanef Manufacturing Corporation','PIN-ATTACHMENT WALKING BE','G14939K04','161A7305-1','15-5PH per AMS5659','PL-Rev-NC, PSDL Rev-A, APO 28-003 Rev-0',2,'100436 Ch-03, Rel-01','','4272','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','ID measures .0250mm out of tolerance in 01no. and step in the bore in 01 no.','While reworking, it was happened.','Clearly checked the stock & rework done for remaining parts.','Will be taken care.','CA/PA Found satisfactory.','','2010-01-08','Dinakar(K)','Narasimha(Murthy R)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(430,'34-004','BRISTOL AEROSPACE LIMITED','MOUNTING TEE MLG CUTTER W','MA008081400','446 83054 2 901','7075-T651','A, EM101307 Iss AU, ECN 39892 Iss A, ECN 39965 Iss',1,'B62472 Rev-09','','4619','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','1)Dig mark at the base.\r\n2)all holes looks like oval shape.','Due to process problem.','new process adopted.','new process adopted.','Next batch found ok','','2010-01-08','Krishna(Chowdary.G.P.)','Girish(Prasad P)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(431,'34-003','BRISTOL AEROSPACE LIMITED','MOUNTING TEE MLG CUTTER W','MA008081400','446 83054 1 901','7075-T651','A, EM101307 Iss AU, ECN 39892 Iss A, ECN 39965 Iss',1,'B62472 Rev-09','','4618','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','Radius not formed in the part.','Refer Non Conformance number 00430.','Refer Non Conformance number 00430.','Refer Non Conformance number 00430.','Next batch found ok\r\n','','2010-01-08','Krishna(Chowdary.G.P.)','Girish(Prasad P)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(432,'28-007','Ellanef Manufacturing Corporation','SHAFT SUPPORT/LEVER','93034','251A1747-1','6Al-4V per MIL-T-904','N/C',8,'99457 Rel-03','','3528','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','1) Step on OD witnessed in 6no\'s\r\n2) OD undersize in 02no\'s.','1)while running in mass production,insert were blented,it happned.\r\n2)OD has close tolerence(ie,+/- 0.003).','1)Old insert replaced.\r\n2)New process adopted.','Will be taken care.','CA/PA Found satisfactory.','','2010-01-08','Dinakar(K)','Ramesh(S. Bandagi)','','0000-00-00','other operators\r\n1) Bharath\r\n2) Narashima murthy.K.G','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(433,'18-272A','Magellan Aerospace Bournemouth','BUTTSTRAP UPP RS4X8700','277477','L575 54369 201','ABM3 1029','A00',1,'RM368750','','4245','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Tool dig mark on 6.70 hole in depth of 5mm. ','It happened due to manual mistake. ','Will be taken care.','Planning to deburr the holes in machine with the help of chamfer tools.','Next batch found ok.','','2010-01-11','Siddalinga(Tambake)','Nagaraju(T)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(434,'35-004','Saab AB','HINGE BRACKET 2','335084','D576 50005 000 01','7050 T7651 ABM3-1030','C00',1,'PA1217','','4845','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Tool dig mark noticed to a depth of 10mm and 40mm width.','While programming tool was sellected wrongly. Dia 16 selected instead of Dia 12 & it was not cross verified with verifier.','Corrected the program and next part coming ok.','Before giving the program to the production, program will be cross checked with verifier.','CA/PA Found satisfactory.','','2010-01-12','Mahesh(B.T.)','Mahesh(B.T.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(435,'23-034A','Goodrich Aerospace','PLATE','396452','7712501-803','7075 T6 AMS-QQ-A-250','TR IP 7712501-803 REV 03',1,'CRGL14416-04-09','','4437','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Hole oversize by ','This is happened due to the holder.Operator were loaded thread damaged holder, while running tool get vibrated & hole become over size.','Holder were replaced.','Suggested to the production supervisors provide necessary gauges or tools which are require for the production. ','CA/PA Found satisfactory.','','2010-01-14','Krishna(Chowdary.G.P.)','Diwakar(S)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(436,'23-035A','Goodrich Aerospace','PLATE','396452','7712501-804','7075 T6 AMS-QQ-A-250','TR IP 7712501-804 REV 03',1,'CRGL14416-04-09','','4438','','0000-00-00',NULL,'no','yes','yes','no','no','no','yes','no','no','Dig Mark on the base.','It was happened due to improper clamping.','For next piece proper claming made & all dimension found satisfactory.','Instructed to operator ensure that clamping should be proper before run the programs.','Next production parts found satisfactory.','','2010-01-14','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(437,'30-021','Gardner Aerospace Burnley Limited','RIB 3 OFW - RH','8048502 03','L575 54203 201','ABM3-1029 T7651','B, ECN:PG69999001JP97',1,'PRO0016172','','3598','','0000-00-00',NULL,'yes','no','no','no','no','no','no','yes','yes','surface finish too rough where shown in attached photo (note:this is not acceptable as edge is mating face please dress to 32 microns-perdwg requirment)','polishing not carraiedout.','all the parts which are ready for shipment and parts which are in inspection will be recalled and shall be dressed in the area as indicated above so as to achive the surface finish called out in the drawing.','cim tools shall ensure that the surface roughness is maintained as per the drawing requirment by hand polishing wherever it is not possible to achive the same in the CNC machine for all the parts.','Next batch found satisfacory.','C2236','2010-01-14','Avinash(R.J.)','Prakash(C.B.)','2009-23','2009-12-15','reject no: 2009-23\r\nreceived by mail ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(438,'18-227A','Magellan Aerospace Bournemouth','CLAMP STRIP BTM','1526401','L572 51299 200','ABM3-1029','A00',1,'RM366521','','4448','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Tool dig mark noticed in depth of 1mm.','Due to operator mistake.he was kept 1mm in work offset(X-axis),before run the program he should cross check the work offset but he did not done so part get dig mark.','For next part cross checked the work offset & runned the program.so next piece found OK.','Training given to the operator regarding the jobs & what are the precaution has to be taken to avoid such kind of problems.','CA/PA Found satisfactory.','','2010-01-16','Krishna(Chowdary.G.P.)','Diwakar(R.B.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(439,'28-006','Ellanef Manufacturing Corporation','SHOULDER BOLT','95619 ','162A3109 2','15-5PH per AMS5659','NA',2,'99939 Ch-04 Rel-1 -S','','4640','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','OD measures undersize by 0.1mm.','It is happened due to insert problem.New insert loaded but operator was not cross checked whether insert properly seatted or not.','For next piece supervisor  loaded the insert properly & cross checked dimension for several components and found within tolerance.  ','Proper training given to the operators regarding the above NC.','CA/PA Found satisfactory.','','2010-01-18','Dinakar(K)','Nithin(S)','','0000-00-00','RM COST NOT AVAILABLE.','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(440,'23-029','Goodrich Aerospace','REINFORCEMENT PLATE','266583','7712500-8106','7075 T651 AMS-QQ-A-2','TR IP 7712500-8106 REV 01',1,'CRGL14416-04-09','','4571','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dig mark noticed on the face.','Due to tool length compensation problem.Operator has taken wrong tool length compensation.','Training given to the operator regarding tool length compensation.','Same as above.','CA/PA Found satisfactory.','','2010-01-18','Dayananda(K.G.)','Tharanj R(Pandit)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(441,'23-029','Goodrich Aerospace','REINFORCEMENT PLATE','266583','7712500-8106','7075 T651 AMS-QQ-A-2','TR IP 7712500-8106 REV 01',1,'CRGL14416-04-10','','4862','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dig mark observed on the rib','Refer Non Conformance number 00440.','Refer Non Conformance number 00440.','Refer Non Conformance number 00440.','Refer NCR00440','','2010-01-18','Dayananda(K.G.)','Tharanj R(Pandit)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(442,'23-075','Goodrich Aerospace','EDGE TEE','4464602','7716204-801','7075 T7351 AMS 4078','ECN 55818',1,'CRGL14435-02-09','','4657','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Inner Diameter 1.154\" +/-.01\" measures 1.181\".','It was happened in fitting.where fitter want to match the tool mark he used the polishing wheel.Before polishing he should check the dimension but it was not happened so ID dimension enlarged.','Instruction given to all the fitter before polishing the job refer the drawing or process sheet & check the dimension, polish the part as required.','Same as above.','CA/PA Found satisfactory.','','2010-01-18','Nagaraju(T)','Ravikumar(L)','','0000-00-00','Other operator is Shiva Kumar','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(443,'23-108','Goodrich Aerospace','REAR HOUSING EFB 10.4','622921A','08720-0087-0002','6061 T651 ASTM-B209','NA',1,'395924','','4518','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dimension 10.470\" +/-.0050 measures 10.4610\" and       7.670\" +/- .0050 measures 7.620\".','After completion of all three setup,we observed in between two rib dimension is less.after analys we come to conclusion that two ribs were get bend.','Since This is last piece for this batch so cross checked all the previous parts in this batch and all the previus parts met the requirements.','This part has center line program.To come out of this problem\r\ndecided to maintain the dimension between the ribs with the help of CRC program.And will be implemented for next batch onwards.','CA/PA found satisfactory.And further batch quantity found satisfactory.','','2010-01-18','Krishna(Chowdary.G.P.)','Manjunatha(N.R.)','','0000-00-00','Other Operators are Diwakar S and Siddramappa.','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(444,'34-043A','BRISTOL AEROSPACE LIMITED','DEFLECTOR, VENT WSPS ','418619A3','429-83051-1-905','7050-T7451 per AMS40','EM: 101307, EM: 105092, EM: 101657',1,'','','4785','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','Rib thickness 5.08mm min measures 4.65 to 4.80mm on both ribs to a deapth of 20mm and width 20mm.','For the height of 70mm with 5mm thickness rib, it will vibrated when finishing the ribs.so programm has been made to finish the ribs in roughing stage itself & runned smoothly upto 10mm depth.after that ribs vibrated due to less strenghtning. ','In roughing program kept 1mm stock on ribs then one more programm added to finish the ribs.','Same as above.','Next batch found ok','','2010-01-19','Mahesh(B.T.)','Lohith(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(445,'01-313','HAL-Helicopter','SWASH PLATE MAST','H918-192/06','201C 623H 1200 201','7075 T73','NA',1,'5553306','01','4308','2252','2010-01-21',NULL,'yes','no','yes','no','no','no','no','yes','no','1)81.0 +0.05mm measures 81.40\r\n2)44.0 -0.05mm measures 43.922/44.075\r\n3)15(typ) measures 14.60\r\n4)Small dent mark noticed on dia83.0\r\n5)0.1max mismatch for dia83.0 is 0.150(detailX)\r\n6)Hole position 0.03 measures 0.041,0.026,0.009,0.012\r\n7)Hole position 0.02 measures 0.008,0.032,0.032,0.030\r\n8)Dimension 147 +0.05 measures 147.22','1)To improve the finish programe was regenareted.\r\n2)It was happend due to new programe.','1)new program was made to correct the deviations.','1)the part to be checked with stock in the part , so that to ensure the part is within the specification.','Further produced parts found O.K','','2010-01-20','Mahesh(B.T.)','Mahesh(B.T.)','','2010-01-20','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','','yes','','','0',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(446,'35-007','Saab AB','HINGE BRACKET 3','335084','D576 50006 001 01','7050 T7651 ABM3-1030','C00',1,'PA1217','','4670','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','Major tool dig mark witnessed on top profile upto 4mm on full length.','This is happened due to programmer mistake.As per tool path generation guidelines,which tool they select to generate tool path program name should be same for that tool.In this case what happened is programmer generated with dia 12f endmill ie,inside the program name is 30_007_0214_12F & given for dia 16f endmill ie, out side program name is 30_007_0214_16F.So operator seen at out side program name & selected 16F,runned the program.','Programmer was rectified the problem and sorted out for next part.','Before upload the programs to machine should cross check program name inside & out side.','CA/PA Found satisafactory','','2010-01-21','Mahesh(B.T.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(447,'30-020','Gardner Aerospace Burnley Limited','RIB 3 OFW - LH','334659','L575 54203 200','ABM3-1029 T7651','B, ECN:PG69999001JP97',1,'PRO0016489-S2','','5138','','0000-00-00',NULL,'yes','no','yes','no','yes','no','no','no','no','Rib thickness 2.0 mm measures 1.4 mm to 1.5mm at all corner radious on top flange.','Happened due to machine spindle problem. There was a abnormal sound in spindle & informed to service personnel.Still there was sound in the spindle even after machine repaired by service personnel.He came again and rectified the real problem that the spindle motor problem.','spindle motor will be replaced.Untill that machine will be in idle condition.','Machine won\'t be runned if any abnormal sound observesd.','Part found satisfactory after machine repair.','','2010-01-29','Siddalinga(Tambake)','Gajendra Singh(C.)','','0000-00-00','Rib thickness 2.0 mm measures 1.4 mm to 1.5mm at all corner radious on top flange.','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(448,'30-016','Gardner Aerospace Burnley Limited','FRAME MID RIB IFS - RH','453552 A2','L575 51892 201','ABM3-1029 T7651','A, ECN:PG60049M01JA74',1,'PRO0016513-S2','','5001','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Crack of length about 40mm noticed on 2 mm thick outer flange. ','Crack developed when removing the lug forcely in fitting.','Right work Instuction given to the fitting  personnels strictly.','New saw cutter procured to remove the lugs to avoid the recurrence.','CA/PA Found satisfactory.','','2010-01-31','Nagaraju(T)','Ravikumar(L)','','0000-00-00','Crack of length about 40mm noticed on 2 mm thick outer flange. ','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(449,'23-034A','Goodrich Aerospace','PLATE','396452','7712501-803','7075 T6 AMS-QQ-A-250','TR IP 7712501-803 REV 03',1,'CRGL14416-04-09','','4437','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','dia 6.451/6.35 measures 6.51','It was happened due to carbide drill problem.After completion of the part operator checked the hole with pin gauge,where NOGO pin answered. ','New carbide drill loaded for next part & checked with pin gauge holes were with in the tolerence.','Decided to change the drill after 50numbers.','CA/PA Found satisfactory.','','2010-02-03','Krishna(Chowdary.G.P.)','Diwakar(R.B.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(450,'23-035A','Goodrich Aerospace','PLATE','396452','7712501-804','7075 T6 AMS-QQ-A-250','TR IP 7712501-804 REV 03',1,'CRGL14416-04-09','','4438','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Tool dig mark noticed in the out side profile and it looks like hole.','While running outer cutout prg part moved dig mark noticed.','Clamped fermly for next part and found OK.','Instruction given to operator to clamp and check once doing production job.','Further produced parts found OK.','','2010-02-03','Krishna(Chowdary.G.P.)','Diwakar(S)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(451,'23-082','Goodrich Aerospace','HOUSING','408130A3','7878053-801','7050 T7451 AMS 4050','ECN 100934 (2 Sheets), PL (2 Sheets) Rev D',2,'CRGL14435-FI-10','','4857','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','1)Depth oversize .0400/.0450 inch measures .0510/.0622 ','It was happened because of machine problem,it was occured in second hole first hole was within tolerence.\r\nAfter completion of first hole(this hole operation was in 90deg position) tool sent to the ATC,another tool was completes its operation.For 270deg position, tool length was changed what it had before.','Rectified the problem all tools removed from ATC & ATC was cleaned.Reloaded all the tools and cross checked tool lengt.we found good result.','We informed to service personnel regarding this problem.\r\nwe are waiting for feed back.','CA/PA found satisfactory.','','2010-02-03','Krishna(Chowdary.G.P.)','Anjinamurthy(H)','','0000-00-00','1no\'s rejected for fitting operator raghu','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(452,'35-002','Saab AB','HINGE BRACKET 1','335085','D576 50004 000 01','7050 T7651 ABM3-1030','C00',2,'PA1217','','5017','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Bore measures over size and it looks like oval shape. ','It was happened due to butting problem.Butting was provided for job butting & it helps to the job in rigid condition.Threads were damaged in butting bolts so clamping become poor.While pre drilling hole becomes oval shape.','Immediately changed the butting bolts.we were ensured that clamping becomes rigid.This problem was sorted out for next parts.','We decided to change butting bolts periodically.','CA/PA Found satisfactory.','','2010-02-05','Krishna(Chowdary.G.P.)','Dhananjaya(N)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(453,'35-004','Saab AB','HINGE BRACKET 2','328472 1A1','D576 50005 000 01','7050 T7651 ABM3-1030','C00',1,'PA1217','','4844','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Tool dig mark witnessed on top profile upto 10mm insted of R25.','Operator did not take the offset correctly','Instructed Operator to take the offset correctly','Instructed Operator to take the offset correctly','Further produced parts found OK','','2010-02-05','Mahesh(B.T.)','Basavaraju(S. Sr.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(454,'35-006','Saab AB','HINGE BRACKET 3','328471/1B1','D576 50006 000 01','7050 T7651 ABM3-1030','C00',1,'','','4014','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Bore measures plus side and base thickness 3.40+/-0.25 measures 2.90','Please Refer NC number 00452.','Please Refer NC number 00452.','Please Refer NC number 00452.','Refer NCR00452','','2010-02-05','Krishna(Chowdary.G.P.)','Dhananjaya(N)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(455,'18-079A','Magellan Aerospace Bournemouth','TOP SKIN STIFFENER 3 - RH','269521','L575 53251 201','ABM3-1029','A00',1,'RM358373','','4656','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','tool dig mark noticed to a depth of 0.5mm on back face.','It was happened due to wrong tool length compensation taken by operator.','Tool pre setter was introduced to avoid such kind of operator mistakes.','Proper training given to the operator regarding tool pre-setter.','CA/PA Found satisfacory.','','2010-02-05','Dinakara(G)','Diwakar(S)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(456,'18-262A','Magellan Aerospace Bournemouth','BUTTSTRAP UPP RS4X10880','288054','L575 53342 201','ABM3-1029','A00',1,'RM366521','','4756','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Base thickness 4.5mm measures minus side by 0.4mm','Refer NC number 00455','Refer NC number 00455','Refer NC number 00455','Next batch found ok.','','2010-02-05','Dinakara(G)','Diwakar(R.B.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(457,'18-185A','Magellan Aerospace Bournemouth','BUSH','0804401698','L575 50327 200','BS 23','B00',27,'RP371247 Amnd 1','','4962','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Bore measures plus side by 5 to 8micron.','During machining ID Bore ovality occured when clamping, hence this deviation occured.','Rubber pad inserted in the step bore during clamping\r\nto avoid ovality of bore during machining.','Rubber pad inserted in the step bore during clamping\r\nto avoid ovality of bore during machining.','CA/PA Found satisfactory.','','2010-02-05','Dinakar(K)','Rajesh(T)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(458,'18-105A','Magellan Aerospace Bournemouth','FORKEND ASSEMBLY','723001','D572 50462 200','S98 FHT','J01',1,'RM365139 Amnd 1','','4345','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Bore 14.308+0.018 measures 14.332, plus by 0.006micron.','It was happened due to bore-gauge setting mistake done by the operator.','Proper training given to the operators by the supervisor.\r\nregarding instruments,GD&T functions.','Same as above.','CA/PA Found satisfactory.','','2010-02-05','Dinakara(G)','Sunil(Kumar K.R.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(459,'18-121A','Magellan Aerospace Bournemouth','BARREL - STRUT','687946','D572 50463 201','S98 FHT','F',3,' RM365136 Amnd 1','','4220','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','1/2 x 20 unjf pp - LH NOGO gauge not answering.','It was happened because of insert wear out.After 2piece rejection job setting & spindle centering cross verified, there is no problem in both.It might be a insert sitting problem.','New insert loaded and further components found with in limits.','Operator instructed by supervisor,after 30numbers new insert should be loaded.','RC/CA/PA TO BE ENTERED.','','2010-02-05','Dinakar(K)','Nithin(S)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(460,'18-120B','Magellan Aerospace Bournemouth','HOUSING OUT B D BRG 3','CB 869392','D275 56121 200','S130 FHT','E01, ECN No: NG27011ST1KA83',1,'RM365160 Amnd 1','','4186','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Tool dig mark witnessed on out side profile to the 30mm.','Refer NC number 00455','Refer NC number 00455','Refer NC number 00455','Next part found satisfactory.','','2010-02-05','Dinakara(G)','Dinakara(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(461,'18-121A','Magellan Aerospace Bournemouth','BARREL - STRUT','184582','D572 50463 201','S98 FHT','F',4,' RM365136 Amnd 1','','4642','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Thread NOGO gauge answered.','Please Refer NC number 00459.','Please Refer NC number 00459.','Please Refer NC number 00459.','RC/CA/PA TO BE ENTERED.','','2010-02-05','Dinakar(K)','Bharath(R)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(462,'18-105A','Magellan Aerospace Bournemouth','FORKEND ASSEMBLY','723001','D572 50462 200','S98 FHT','J01',1,'RM365139 Amnd 1','','4344','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','dia14.308 bore over size by 0.007mm.','Dia14.308 bore over size by 0.007mm,because of boring bar re-pass.In first pass of boring bar operator found bore in under size.so he re-passed the boring bar.','We checked several times boring bar repeatability on dummy piece untill it show correct reading.we found small error in boring bar.All boring bars sent to the servicing.','We decided to send all boring bars to servicing, twice in a year.','CA/PA Found satisfactory.','','2010-02-05','Dinakara(G)','Mohan(Kumar C.M.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(463,'18-151A','Magellan Aerospace Wrexham','CLEAT','2709501','F572 54614 202 01','ABM3-1029','E',1,'RM90864','','4528','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Thickness 2.50 measures 2.10mm.','Please Refer NC number 00455.','Please Refer NC number 00455.','Please Refer NC number 00455.','Same as NC:00455.','','2010-02-05','Dinakara(G)','        Dinakara(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(464,'18-213A','Verdict Aerospace Components Ltd.','END CAP','48469','D321 40209 200','L168','A',1,'55568','','3877','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dia1.60 drill broken and dig mark witnessed.','It was happened due to drill was not tightned properly.Shank diameter was small it is difficult to tight.','New carbide drill was loaded with shank dia 3mm.As compare to the cutting dia shank dia should be more,it is helpful to tight properly.','Same as above.','CA/PA Found satisfactory.','','2010-02-05','Dinakara(G)','Dinakara(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(465,'18-095A','Magellan Aerospace Bournemouth','BUSH','3186170R','D282 50232 200','L168','A',2,'RM365288 Amnd 1','','4505','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','1) Dent mark witnessed in one no.\r\n2) dia1.60 hole done opposite side.','It was perfectly operator mistake.','Srictly instruction given to the operator,regarding job seriousness,value of the parts & time.','Same as above.','CA/PA Found satisfactory.','','2010-02-05','Dinakara(G)','Dinakara(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(466,'18-041A','Magellan Aerospace Bournemouth','EDGE BEAM BRACKET 2 - RH','334864A6','L575 52324 201','ABM3-1029','A00',1,'RP371764','','4997','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Bore 12.70mm measures over size by 0.012 to 0.013mm.','Please Refer NC number 00462.','Please Refer NC number 00462.','Please Refer NC number 00462.','','','2010-02-05','Dinakara(G)','Sunil(Kumar K.R.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(467,'18-087B','Magellan Aerospace Wrexham','PLATE SEALING ASSY','285272','D572 52914 200 01','ABM3-1029','B',4,'RP96869','','4719','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Base thickness 11 & 17 measures minus side by 1mm.','Please Refer NC number 00455.','Please Refer NC number 00455.','Please Refer NC number 00455.','Refer 00455','','2010-02-05','Dinakara(G)','Dinakara(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(468,'18-098A','Magellan Aerospace Bournemouth','SEAT VALVE','B6353','D282 50060 204','L110','D',1,'RP372014','','4697','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Instead of dia4.83/4.876, dia4.90 pin gauge entering.','It was happened due to wrong identification of drill.Operator loaded dia 4.9drill instead of dia4.85 he was not seen engraving.','Dia4.85 drill loaded & found further components within limits.','Instructed to operator before loading the tools should ensure that loading tool is correct or not.','CA/PA Found satisfactory.','','2010-02-05','Dinakara(G)','Mohan(Kumar C.M.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(469,'18-200A','Magellan Aerospace Wrexham','ANGLE CLEAT LH','183962','D572 50744 200 01','ABM3-1029','A',1,'RP96947','','4766','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Instead of dia4.0/4.12, 4.27 pin entering.','Please Refer NC number 00468.','Please Refer NC number 00468.','Please Refer NC number 00468.','Further produced parts were found O.K','','2010-02-05','Dinakara(G)','Dinakara(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(470,'18-119A','Magellan Aerospace Bournemouth','HOUSING OUT B D BRG 3','CB894702','D275 40011 200','S130 FHT','D01',1,'RP371240','','4882','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Thickness 5.0+0.3/-0.2 measures 4.60 / 4.65','Please Refer NC number 00455.','Please Refer NC number 00455.','Please Refer NC number 00455.','Next batch found ok.','','2010-02-05','Dinakara(G)','Dinakara(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(471,'18-111A','Magellan Aerospace Bournemouth','BODY TURNBUCKLE INTMD','696913','D575 41544 200','S80 FHT','A',1,'RP371230','','4167','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','3/4 x 16unjf - 3B NOGO gauge answered.','Please Refer NC number 00459.','Please Refer NC number 00459.','Please Refer NC number 00459.','Refer NCR00459','','2010-02-05','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(472,'18-085A','Magellan Aerospace Wrexham','BRACKET SUPPORT','M122420','D579 52009 200 01','L168','A',2,'RP96874 Amendment 1','','4695','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Instead of dia4.12, 4.15 pin gauge entering.','Please Refer NC number 00449.','Please Refer NC number 00449.','Please Refer NC number 00449.','Next batch found ok.','','2010-02-05','Dinakara(G)','Manjunatha(N.R.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(473,'23-108','Goodrich Aerospace','REAR HOUSING EFB 10.4','632161','08720-0087-0002','6061 T651 ASTM-B209','NA',1,'416660','','4969','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dimension 7.67+/-0.005 measures 7.66 & 10.47+/-0.005 measures 7.461.','It was last piece for the batch qty.It was happened due to bend occured in job.If bend occurs it is difficult to remove the bend.','Extra clamps introduced to avoid bend and Feed back given to CAD-CAM department regarding this issue.We got possitive response from them.They made small correction in program sequence.','Extra clamps will be provided and the corrected program will be run for the future batches.','CA/PA found satisfactory.','','2010-02-05','Krishna(Chowdary.G.P.)','Nagaraju(K.S.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(474,'18-056A','Magellan Aerospace Bournemouth','TOP SKIN STIFFENER 1 - LH','6705301','L575 53249 200','ABM3 - 1029','A00',1,'RP371766','','1454','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Flange thickness 3.0 measures 2.30 / 2.70mm.','Please Refer NC number 00455.','Please Refer NC number 00455.','Please Refer NC number 00455.','Further batches found satisfactory.','','2010-02-05','Dinakara(G)','Dinakara(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(475,'18-123A','Magellan Aerospace Bournemouth','FORK END OUT BD','706845','D575 41546 202','S80 FHT','B',1,'RP371229','','4676','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Bore 11.00 / 11.018 measures 11.023','Please Refer NC number 00458.','Please Refer NC number 00458.','Please Refer NC number 00458.','further parts found ok.','','2010-02-05','Dinakara(G)','Dinakara(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(476,'18-123A','Magellan Aerospace Bournemouth','FORK END OUT BD','706845','D575 41546 202','S80 FHT','B',1,'RP371229','','4675','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Bore 11.00 / 11.018 measures oversize as 11.023 / 11.025','Please Refer NC number 00462.','Please Refer NC number 00462.','Please Refer NC number 00462.','CA/PA Found satisfactory. ','','2010-02-05','Dinakara(G)','Dinakara(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(477,'18-198A','Magellan Aerospace Wrexham','ANGLE CLEAT','2725501','D572 59283 200 01','ABM3-1029','A',9,'RP96879 Amend1','','4770','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Tool dig mark witnessed on out side profile.','Wrong tool offset given','corrected the offset','Instructed operator to give the offset value correctly','Further produced parts found Ok','','2010-02-05','Dinakara(G)','Diwakar(S)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(478,'18-186A','Magellan Aerospace Bournemouth','BUSH','0811420017','L575 50336 200','B23','B00',2,'RP371247 Amnd 1','','4963','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','1) Bore measures over size by 0.008mm.','Operator did not enter the tool wear value correctly','Corrected the tool wear value','Instructed Operator to enter the tool wear value correctly','Further produced parts found Ok','','2010-02-05','Dinakar(K)','Narasimhamurthy(K.G.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(479,'18-110A','Magellan Aerospace Bournemouth','FORK END INTERMEDIATE','M72615','D575 40494 202','S80 FHT','J',1,'RP371231','','4932','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Bore measures 0.3mm over size.','Boring tool not set properly','Boring tool was set correctly','Instructed operator to set the boring tool correctly','Further produced parts found OK','','2010-02-05','Dinakar(K)','Narasimha(Murthy R)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(480,'18-198A','Magellan Aerospace Wrexham','ANGLE CLEAT','276012','D572 59283 200 01','ABM3-1029','A',2,'RP96879 Amend1','','4408','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Width 30.0mm measures 29.43 / 29.30mm.','Operator wrongly entered the offset','Corrected the offset value','Instructed the operator to enter the offset value correctly','Further produced parts found OK','','2010-02-05','Dinakara(G)','Girish(Prasad P)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(481,'18-106A','Magellan Aerospace Bournemouth','EYE END INBOARD','723001','D575 41542 200','S98 FHT','D',2,'RP371236','','4654','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','1) Bore over size in one no.\r\n2) tool dig mark witnessed in one no.','1) Boring tool not set correctly\r\n2) Operator entered wrong offset','1) corrected the boring tool setting\r\n2) corrected the entry of the offset','1)Instructed the Operator to check the set the boring tool correctly\r\n2)Instructed the Operator to enter the offset correctly\r\n','Further produced parts found OK','','2010-02-06','Dinakar(K)','Narasimha(Murthy R)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(482,'18-211A','Verdict Aerospace Components Ltd.','PLUNGER','694000','D321 40205 200','S80-FHT','H01',3,'55568','','4535','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','1) Thread damage noticed in 2no,s\r\n2) OD measures under size by 0.04mm.','1)power failure during machining\r\n2)Operator did not take tool offset correctly','1) Power failure un predictable\r\n2) CORRECTED THE TOOL OFFSET','1) Power failure un predictable\r\n2) Instructed the operator to take the tool offset correctly','Further produced parts found OK','','2010-02-06','Dinakar(K)','Paramesh(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(483,'18-078A','Magellan Aerospace Wrexham','ADAPTOR','251538','A282 50081 200PF',' L111 T6','A',1,'RP97165','','4704','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Stepped OD thickness 3.0mm measures 1.5mm in roughing stage.','Operator did not take the work offset correctly','Instructed Operator to take the work offset correctly','Instructed Operator to take the work offset correctly','Further produced parts found OK','','2010-02-06','Dinakar(K)','Ramesh(S. Bandagi)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(484,'18-009A','Magellan Aerospace Wrexham','COVER PLATE ASSY','2147354-08','D572 52519 200 01','L97 - T351','A',1,'RP96872','','5005','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Instead of dia7.50 / 7.75, dia7.76 pin gauge entered.','Drill run out caused the deviation','Changed the drill and clamped the drill without runout ','Instructed operator to check the drill for runout before using it on the part','Further produced parts found OK','','2010-02-06','Dinakara(G)','Basavaraju(B)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(485,'18-215C','Verdict Aerospace Components Ltd.','ROD END ASSMY - MALE','631551','D321 53012 200','S98','F01',8,'55568','','4714','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','1) Bore dia19.00/19.021 measures dia19.023 / dia19.026 in 5no,s\r\n2) chf over size by 0.5mm in one no.\r\n3) Thread damage noticed in 2no,s','1) boring tool offset not set correctly\r\n2) tool offset wrongly given\r\n3) power failure during threading operation','1) corrected the boring tool offset\r\n2) corrected chf tool offset\r\n3) power failure unpredictable','1) Instructed operator to give the boring tool offset correctly\r\n2) Instructed operator to give correct chf tool offset\r\n3) power failure unpredictable','Further produced parts found OK','','2010-02-06','Dinakar(K)','Nithin(S)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(486,'18-122A','Magellan Aerospace Bournemouth','FORKEND ASSEMBLY','723001','D572 50462 201','S98 FHT','J01',4,'RP371227','','4653','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Bore over size by 0.005 / 0.008mm.','Boring tool offset wrongly given','corrected the Boring tool offset ','Instructed operator to give the boring tool offset correctly','Further produced parts found OK','','2010-02-06','Dinakar(K)','Ramesh(S. Bandagi)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(487,'18-214A','Verdict Aerospace Components Ltd.','SPECIAL WASHER','631551','D321 40210 202','S98','E01',1,'55568','','4537','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Step noticed in dia9.60 hole.','Drill worn out caused the deviation','changed the drill witha new one','Instructed operator to check the sharpness of the drill before use','Further produced parts found OK','','2010-02-06','Dinakara(G)','Girish(Prasad P)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(488,'18-182A','Magellan Aerospace Bournemouth','SCREWED BUSH','G5172H3017','A284 40011 200','DTD 197','A',1,'RM365241 Amnd 1','','4522','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','1) Dia1.31 hole over size in 3no,s\r\n2) Thread damage witnessed in 1no.','1) Drill runout caused the deviation\r\n2) power failure while machining','1)changed with a new drill bit\r\n2)power failure unpredictable','1)Instructed operator to check the runout of the drill before using it\r\n2)power failure unpredictable','Further produced parts found OK','','2010-02-06','Dinakar(K)','Vikram(E)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(489,'28-002','Ellanef Manufacturing Corporation','LOWER LINK','95754','161A6104-4','15-5PH CRES Steel','NA',4,'99933 Ch-02 Rel-01-S','','5029','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','1) Bore(h7) over size by 0.2mm to 0.3mm in 2no,s\r\n2) Tool dig mark witnessed in top face in 2no,s','1)Boring tool was not set correctly\r\n2)Tool offset not entered correctly','1)boring tool set correctly\r\n2)corrected tool offset','1)Instructed operator to set the boring tool correctly\r\n2)Instructed operator to to enter the tool offset value correctly\r\n','Further produced parts found OK','','2010-02-06','Siddalinga(Tambake)','Sunil(Kumar K.R.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(490,'18-030A','Magellan Aerospace Bournemouth','PIN','579901','D278 50156 200','S130 FHT','A',24,'RP371769','','4130','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Total length 5.50/5.60 measures 5.21 to 5.47','Pieces were not butt properly and clamped','pieces were butt properly and clamped correctly','Instructed operator to ensure whether the pieces are butt properly before machining','Further produced parts found OK','','2010-02-06','Stalin(G)','Pinto(N.L.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(491,'18-035A','Magellan Aerospace Bournemouth','BRACKET','722725 A9','D579 50131 202','ABM3 1029','H02',1,'RP371770','','4673','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Hole pitch 20.0+/-0.3 measures 19.66 / 19.67','During drilling the drill runout caused the deviation','1) changed with a new drill\r\n','Instructed operator to check the runout of the drill before using it on part','Further produced parts found OK','','2010-02-06','Dinakara(G)','Diwakar(R.B.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(492,'18-113A','Magellan Aerospace Bournemouth','ADJUSTER','694002','D575 40496 200','S80 FHT','G',4,'RM365151 Amnd 1','','4123','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','1) Dia1.15 drill bit broken in 1no\r\n2) Thread NOGO gauge answered in 3no,s.','1) Drill bit broken\r\n2) TOOL WEAR NOT GIVEN CORRECTLY','1)CHANGED WITH THE NEW DRILL\r\n2)INSTRUCTED OPERATOR TO ENTER THE TOOL WEAR CORRECTLY','1) Instructed operator to check the sharpness of the drill before use.\r\n2) INSTRUCTED OPERATOR TO ENTER THE TOOL WEAR CORRECTLY','Further produced parts found OK','','2010-02-06','Dinakar(K)','Paramesh(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(493,'18-033A','Magellan Aerospace Bournemouth','CARRIER SEAL - LH','1838503-3','D575 55658 200','L97 T351','C',1,'RM364965','','4573','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Base thickness 1.6 measures 1.30','TOOL OFFSET WRONGLY ENTERED','CORRECTED THE TOOL OFFSET','Instructed Operator to enter the tool offset correctly','Further produced parts found OK','','2010-02-06','Dinakara(G)','Lokesh(B.D.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(494,'18-034A','Magellan Aerospace Bournemouth','CARRIER SEAL - RH','1838501-3','D575 55658 201','L97 T351','C',1,'RM364965','','4574','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Total thickness 6.9+/-0.3 measures 6.5 for the full length.','Operator entered the tool length offset wrongly','corrected the tool length offset','Instructed operator to enter the tool length offset correctly','Further produced parts found OK','','2010-02-06','Dinakara(G)','Sathish(Y.R.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(495,'18-252A','Magellan Aerospace Bournemouth','BUTTSTRAP INBD FIXED PNL','453640 A5','L575 52464 201','ABM3-1029','A00',1,'RM366521','','4511','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dia 6.60 hole formed as oblong with dig mark witnessed.','Drill broken during drilling operation','changed with a new drill bit','Instructed operator to check the sharpness of the drillbit before using','Further produced parts found OK','','2010-02-06','Dinakara(G)','Lokesh(B.D.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(496,'18-155A','Magellan Aerospace Wrexham','BRACKET','343504A7','F579 53174 200 47 01','ABM3-1029','B',1,'RM90863','','4531','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Insted of dia 5.50 / 5.62, dia5.63 pin gauge entering.','Drill bit runout caused the deviation','Changed the drill bit with new one','Instructed operator to check the runout of drill before using it','Further produced parts found Ok','','2010-02-06','Dinakara(G)','Theerthappa(K.N.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(497,'18-085A','Magellan Aerospace Wrexham','BRACKET SUPPORT','M122420','D579 52009 200 01','L168','A',2,'RM90861','','4436','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','1) Hole pitch 19.0mm measures 18.65 to 18.67 in 1no.\r\n2) Base thickness 3.0 +0.3/-0.2 measures 2.60/2.90 in 1no.','1)& 2) Work offset taken wrongly\r\n ','corrected the work offset','Instructed operator to take the work offset correctly','Further produced parts found OK','','2010-02-06','Dinakara(G)','Diwakar(R.B.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(498,'05-088','HAL-Aircraft','TRAVERSE BEAM - RH','XP50644/1-08-A320','D521-10353-201-00-E0','7175 T 7351','NA',1,'C/146/ES/COMP','897','5260','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Major tool dig mark witnessed on ellipse cutout.','Before to run the small pocket cut-out should apply external clamps.But it was not happened.Their is a \'M0\'with massage in program & clearly mentioned \"APPLY EXTERNAL CLAMPS\".Perfectly it is operator mistake,he was not seen any massage he just pressed the \"cycle start button\".','Information given to the CAD-CAM department regarding this problem.They react possitively and altered program sequence.After this correction we found better result.','Instructed to the operator should read the massages carefully if their is a \"M0\" OR \"M01\".','parts found satisfactory after correction. ','','2010-02-09','Siddalinga(Tambake)','Satheesha(H.K.)','','0000-00-00','Actual operator is Satheesh.H.K','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(499,'18-089B','Magellan Aerospace Wrexham','PLATE SEALING ASSY','122889/001','D572 52999 200 01','ABM3-1029','B',60,'RP96872','','5273','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Dia 2.46/2.56 holes oversize, measured value is 2.57 to 2.58.','Drill runout caused the deviation','changed the drill with new one','Instructed operator to check the runout of the drill before using it','Further produced parts found OK','','2010-02-10','Dinakara(G)','Manjunath(K.N.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(500,'18-113A','Magellan Aerospace Bournemouth','ADJUSTER','685001','D575 40496 200','S80 FHT','G',6,'RM365151 Amnd 1','','4124','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','1/2 x 20 UNJF NOGO answering.','Machine tap clogged with chips hence this deviation occured','Cleaned the tap and adjusted the coolant to flush the chips off the tap','Instructed operater to clean the tap frequently and adjust the coolant properly','Further produced parts found OK','','2010-02-10','Dinakara(G)','Mohan(Kumar C.M.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(501,'18-113A','Magellan Aerospace Bournemouth','ADJUSTER','685001','D575 40496 200','S80 FHT','G',3,'RM365151 Amnd 1','','4421','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','ID thread NOGO gauge answering.','Machine tap clogged with chips hence this deviation occured','Cleaned the tap and adjusted the coolant to flush the chips off the tap','Instructed operater to clean the tap frequently and adjust the coolant properly','Further produced parts found OK','','2010-02-10','Dinakara(G)','Basavaraja(S. Jr.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(502,'35-006','Saab AB','HINGE BRACKET 3','4227401','D576 50006 000 01','7050 T7651 ABM3-1030','C00',1,'PA1217','','4316','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Bore 22.225 / 22.246 measures 22.263 / 22.266','While running production bore measures out of tol in between.','Checked for another 05 parts and found OK. ','Assuming that chips clocked in tip and this deviation occured.Instruction given to operator to avoid chips clocking to tool by arjusting coolent. ','Further produced parts found OK.','','2010-02-10','Krishna(Chowdary.G.P.)','Dhananjaya(N)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(503,'18-111A','Magellan Aerospace Bournemouth','BODY TURNBUCKLE INTMD','696913','D575 41544 200','S80 FHT','A',1,'RM365149 Amnd 1','','4237','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Tool dig mark witnessed inside the slot upto 0.5mm.','due tool brocken in running.','Replace the brocken tool with new one,next part found ok.','Advise to operators to change the tool in proper intervals of time.','CA/PA Found satisfactory.','','2010-02-11','Dinakara(G)','Dinakara(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(504,'18-078A','Magellan Aerospace Wrexham','ADAPTOR','251538','A282 50081 200PF',' L111 T6','A',3,'PRP91227 Amendment 1','','4315','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Rib thickness 3.81 measures minus by 0.3 to 0.6mm.','Tool offset wrongly entered','Corrected the tool offset','Instructed the operator to take the tool offset correctly','Further produced parts found Ok ','','2010-02-11','Dinakara(G)','Diwakar(S)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(505,'18-198A','Magellan Aerospace Wrexham','ANGLE CLEAT','276012','D572 59283 200 01','ABM3-1029','A',6,'RM90868','','4180','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','1) Major tool dig mark witnessed in 1no.\r\n2) Width under size 30.0mm measures 29.63 to 29.69 in 5no,s','setting not done properly due to this dimension undersize.','resetting done and next parts found ok.','on training on m/c given for operator for setting that part.','Further produced parts found O.K','','2010-02-11','Dinakara(G)','Theerthappa(K.N.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(506,'18-087B','Magellan Aerospace Wrexham','PLATE SEALING ASSY','277477','D572 52914 200 01','ABM3-1029','B',4,'RM90855','','4456','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Hole dia 2.46/2.56, NOGO answereing.','without checking runout for drill operator run the part due to this hole oversize.','instruction given for operator before running job put drill on dummy peice.','same as above','CA/PA Found satisfacory.','','2010-02-11','Dinakara(G)','Dinakara(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(507,'18-088A','Magellan Aerospace Wrexham','PLATE SEALING','025962/001','D572 52998 200 01','ABM3-1029','A',1,'RP96873 Amendment 1','','4405','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Tool dig mark witnessed on OD upto 10mm.','while running peice came outside from the jaws.','chuck pressure increased and next parts found ok.','same as abone.','CA/PA Found satisfactory.','','2010-02-11','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(508,'18-201A','Magellan Aerospace Wrexham','ANGLE CLEAT RH','1049401','D572 50744 201 01','ABM3-1029','A',3,'RM90865','','4410','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dimension 17.30+/-0.2 shifted by 0.5mm.','wrong offset taken by operator','retaking the work offset ,next job found ok','training given to operator,keeping observetion on him for 10 days,found ok.','','','2010-02-11','Dinakara(G)','Dinakara(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(509,'23-095','Goodrich Aerospace','BRACKET','266238','A877940-8204','7075 T7351 AMS QQ-A-','ECN 90701 (2 Sheets) Rev B',2,'CRGL14435-03-09','','3956','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','1) Tool dig mark witnessed in the outside profile in 1no.\r\n2) Hole diameter 0.2520 / 0.2598 measures 0.2622 in 1no.','1) Part not clamping correctly in vice(wedge clamp vice)and while running part lifted and digmark coming.\r\n2) Refer NCR no.00537','1) Instructio given to operator to crosschech tighting while doing clamping.\r\n\r\n2)','1) Instructio given to operator to crosschech tighting while doing clamping.\r\n\r\n2)Refer NCR no.00537','CA/PA Found satisfactory.','','2010-02-11','Krishna(Chowdary.G.P.)','Rangaswamy()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(510,'30-003','Gardner Aerospace Burnley Limited','RIB 3 AFT OFW - LH','224879 1B1','L575 51776 200','ABM3-1029 T7651','A, ECN:PG60049N01JA69',2,'PRO0016513-S2','','4864','','0000-00-00',NULL,'yes','no','no','no','no','no','no','yes','yes','parts are being delivered with mismatches in the back face,see attached photos.mismatch needs to be lightly blended, no mismatches allowed through holes.','parts were not polished as per customer suggestion.','parts will be polished and maintained to drawing.','parts will be produced as per customer requirments from next shipment.','Further produced parts found O.K','C2941','2010-02-14','Avinash(R.J.)','Prakash(C.B.)','2010-2','2010-02-03','Disposition: parts were reworked at customer end & accepted.( this SRN related to various earlier deliveries, customer not mentioned the batch)','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(511,'18-161B','Magellan Aerospace Bournemouth','STRUT AFT INNER - LH ','A440028','F574 50156 206 47','J4423','E',2,'RP372017','','5224','','0000-00-00',NULL,'yes','no','no','no','no','no','no','yes','yes','A quantity of 2 parts do not meet the 0.15mm Flatness requirement stated on condition of supply drawing issue B.','Drawing calls 0.15 flatness: This note as mentioned in the COS was missed by Engineering and Quality Departments.','Corrective Action:  Reworked one part in fitting and show cased the same to Customer.  Acceptance was taken','Preventive Action:  In the process sheet an additional operation instructing to carry out this flatness in Fitting is added.','Next batch found satisfactory.','C3152','2010-02-14','Avinash(R.J.)','Muniyappa(N)','RDN00608','2010-02-10','Parts were reworked at customer end and accepted.','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(512,'18-161B','Magellan Aerospace Bournemouth','STRUT AFT INNER - LH ','A440028','F574 50156 206 47','J4423','E',2,'RP372017','','5224','','0000-00-00',NULL,'yes','no','no','no','no','no','no','yes','yes','A quantity of 2 parts have mismatch reference drawing location B5.  See attached photo’s','Drawing calls 0.15 flatness: This note as mentioned in the COS was missed by Engineering and Quality Departments','Corrective Action:  Reworked one part in fitting and show cased the same to Customer.  Acceptance was taken','Preventive Action:  In the process sheet an additional operation instructing to carry out this flatness in Fitting is added.','Next batch found satisfactory.','C3153','2010-02-14','Avinash(R.J.)','Muniyappa(N)','RDN00609','2010-02-10','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(513,'18-162B','Magellan Aerospace Bournemouth','STRUT AFT INNER - RH ','A440028','F574 50156 207 47','J4423','E',5,'RP372017','','5225','','0000-00-00',NULL,'yes','no','no','no','no','no','no','yes','yes','A quantity of 5 parts do not meet the 0.15mm Flatness requirement stated on condition of supply drawing issue B.','Drawing calls 0.15 flatness: This note as mentioned in the COS was missed by Engineering and Quality Departments','Corrective Action:  Reworked one part in fitting and show cased the same to Customer.  Acceptance was taken','Preventive Action:  In the process sheet an additional operation instructing to carry out this flatness in Fitting is added.','Next batch found satisfactory.','C3154','2010-02-14','Avinash(R.J.)','Muniyappa(N)','RDN00610','2010-02-10','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(514,'18-162B','Magellan Aerospace Bournemouth','STRUT AFT INNER - RH ','A440028','F574 50156 207 47','J4423','E',5,'RP372017','','5225','','0000-00-00',NULL,'yes','no','no','no','no','no','no','yes','yes','A quantity of 5 parts do not meet the 0.15mm Flatness requirement stated on condition of supply drawing issue B.','Drawing calls 0.15 flatness: This note as mentioned in the COS was missed by Engineering and Quality Departments','Corrective Action:  Reworked one part in fitting and show cased the same to Customer.  Acceptance was taken','Preventive Action:  In the process sheet an additional operation instructing to carry out this flatness in Fitting is added.','Next batch found satisfactory.','C3155','2010-02-14','Avinash(R.J.)','Muniyappa(N)','RDN00611','2010-02-10','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(515,'30-024','Gardner Aerospace Burnley Limited','RIB CLOSING INBOARD - LH','6708501 02','L575 54754 200','ABM3-1029 T7651','A, ECN: SG60049U03JA06',1,'PRO0016034-S12','','2538','','0000-00-00',NULL,'yes','no','no','no','no','no','no','yes','yes','Part does not confirm to drawing requirments.refer attached CMM report.','1) we considered tolerance of +/-0.25 instead of +/-0.125\r\n2) due to clamping method used while machining the part.','1) Reviewed our CMM report and found within limits as per specified tolerance.\r\n2) we will amend the CMM program to correct the tolerance.\r\n3) Vaccum fixture improved toolins to be implemented for further batches.','Vaccum fixture to be implemented.','CA/PA Found satisfactory.','C1444','2010-02-15','Avinash(R.J.)','Prakash(C.B.)','SCAR 2446','2010-02-12','Mail received on 12/02/10, for refarence see attached photos on mail','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(516,'30-025','Gardner Aerospace Burnley Limited','RIB CLOSING INBOARD - RH','6708501 05','L575 54754 201','ABM3-1029 T7651','A, ECN: SG60049U03JA06',1,'PRO0016097-S4','','3586','','0000-00-00',NULL,'yes','no','no','no','no','no','no','yes','yes','Part does not confirm to drawing requirments.','1) we considered tolerance of +/-0.25 instead of +/-0.125 2) due to clamping method used while machining the part.','1) Reviewed our CMM report and found within limits as per specified tolerance.\r\n2) we will amend the CMM program to correct the tolerance.\r\n3) Vaccum fixture improved toolins to be implemented for further batches.','Vaccum fixture to be implemented.','CA/PA Found satisfactory.','C2342','2010-02-15','Avinash(R.J.)','Prakash(C.B.)','SCAR 2447','2010-02-12','Mail received on 12/02/10, for refarence see attached photos on mail.','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(517,'30-009','Gardner Aerospace Burnley Limited','RIB CLOSING OUTBOARD - LH','8788501 07','L575 51826 200','ABM3-1029 T7651','B, ECN:PG69999001JK19',1,'PRO0016034-S4','','2983','','0000-00-00',NULL,'yes','no','no','no','no','no','no','yes','yes','Part does not confirm to drawing requirments.','1) we considered tolerance of +/-0.25 instead of +/-0.125 2) due to clamping method used while machining the part.','1) Reviewed our CMM report and found within limits as per specified tolerance.\r\n2) we will amend the CMM program to correct the tolerance.\r\n3) Vaccum fixture improved toolins to be implemented for further batches.','Vaccum fixture to be implemented.','CA/PA Found satisfactory.','C1924','2010-02-15','Avinash(R.J.)','Prakash(C.B.)','SCAR 2448','2010-02-12','Mail received on 12/02/10, for refarence see attached photos on mail.','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(518,'30-010','Gardner Aerospace Burnley Limited','RIB CLOSING OUTBOARD - RH','722725 A9','L575 51826 201','ABM3-1029 T7651','B, ECN:PG69999001JK19',1,'PRO0016097-S3','','3802','','0000-00-00',NULL,'yes','no','no','no','no','no','no','yes','yes','part does not meet drawing requirments','1) we considered tolerance of +/-0.25 instead of +/-0.125 2) due to clamping method used while machining the part.','1) Reviewed our CMM report and found within limits as per specified tolerance.\r\n2) we will amend the CMM program to correct the tolerance.\r\n3) Vaccum fixture improved toolins to be implemented for further batches.','Vaccum fixture to be implemented.','CA/PA Found satisfactory.','C2291','2010-02-15','Avinash(R.J.)','Prakash(C.B.)','SCAR 2449','2010-02-12','Mail received on 12/02/10, for refarence see attached photos.','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(519,'28-003','Ellanef Manufacturing Corporation','PIN-ATTACHMENT WALKING BE','G14939K02','161A7305-1','15-5PH per AMS5659','PL-Rev-NC, PSDL Rev-A, APO 28-003 Rev-0',2,'100436 Ch-03 Rel-01 ','','5115','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','ID measures 0.1mm out of tolerance in 01no.break sharp edges on holes measures 0.5mm out of tolerance.','while runing it measures 0.1 out of tolarence.','resetting done, next part found ok.','proper instructions given to operator to cheek tool & tool inserts.','CA/PA Found satisfactory.','','2010-02-16','Dinakar(K)','Dinakar(K)','','0000-00-00','01 no. is rejected in turning and 01 no. is rejected in milling.','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(520,'34-019','BRISTOL AEROSPACE LIMITED','BRACKET, STRUT-R/H','A8107A','400-12609-2-905','4340 Steel Per SAE-A','EM 104302 Iss. A, EM 105092 Iss. C, ECN:39611 Iss',1,'B70996','','5356','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','Bore 15.895 -0/+0.01 measures 15.915','improper method for make the bore.','changed the method,then part found ok','training given to oparator.','CAPA FOUND SATSIFACTORY','','2010-02-17','Mahesh(B.T.)','Jayarama(M.B.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(521,'34-019','BRISTOL AEROSPACE LIMITED','BRACKET, STRUT-R/H','A8107A','400-12609-2-905','4340 Steel Per SAE-A','EM 104302 Iss. A, EM 105092 Iss. C, ECN:39611 Iss',1,'B70996','','4937','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','bore 16+0.05 measures 16.0mm.','improper method of clamping.','changed the method,then part found ok','plan for proper method.','Nxex batch found ok','','2010-02-17','Mahesh(B.T.)','Jayarama(M.B.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(522,'34-019','BRISTOL AEROSPACE LIMITED','BRACKET, STRUT-R/H','A8107A','400-12609-2-905','4340 Steel Per SAE-A','EM 104302 Iss. A, EM 105092 Iss. C, ECN:39611 Iss',1,'B70996','','5188','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','bore 15.895 +0.01 measures 15.915','refer ncr 521','refer ncr 521','refer ncr 521','Next batch found ok','','2010-02-17','Mahesh(B.T.)','Jayarama(M.B.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(523,'18-061A','Magellan Aerospace Bournemouth','STIFFENER -1','0005101','L575 53252 200','ABM3-1029','A00',2,'RP371767','','4685','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','Web thickness 3.0 +0.13/-0.08 measures 2.85/2.90mm.','due to vibration while running the part web thickness measures 2.85/2.9.','change the method for machining,than found ok','plan fixture for next batch.','CA/PA Found satisfactory.','','2010-02-17','Dinakara(G)','Dinakara(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(524,'18-061A','Magellan Aerospace Bournemouth','STIFFENER -1','0005101','L575 53252 200','ABM3-1029','A00',1,'RM358373','','4684','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','Web thickness 3.0 +0.13/-0.018 measures 2.87/2.88mm.','not suficient holding','intraduse M10 bolt hole & bolted the part.then it found ok','plan fixture for next batch.','CA/PA Found satisfatory.','','2010-02-17','Dinakara(G)','Dinakara(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(525,'18-009A','Magellan Aerospace Wrexham','COVER PLATE ASSY','2147354-08','D572 52519 200 01','L97 - T351','A',4,'RP96872','','5239','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','1) Major tool dig mark witnessed in the outside profile up to 1mm ( in place of OD )\r\n2) Tool dig mark witnessed in hole in 1no.\r\n3) counet sink over size by 2mm in 1no.\r\n4) Chf existing 2 sides insted of 1 side in 1no.','1.not proper holding the fixture.\r\n2.-----------\"-----------------\r\n3.wrong tool offset taken by operator.\r\n4.wrong loading of part.','resetting the fixture & job ,then next part found ok.','proper instrutions given to operator,found ok.','Next batch found satisfactory.','','2010-02-17','Dinakara(G)','Dinakara(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(526,'18-246A','Magellan Aerospace Bournemouth','BUTTSTRAP LOW RS4X13100','4431602','L575 50178 201','ABM3-1029','A00',1,'RM366521','','5406','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','Major tool dig mark witnessed in the place of radius upto 1mm depth for the full length.','Tool offset mistaken by operator.','Reset the tool again ,next part found ok.','training given to the operator,observe for 10 days found ok.','found ok.','','2010-02-17','Dinakara(G)','Dinakara(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(527,'18-034A','Magellan Aerospace Bournemouth','CARRIER SEAL - RH','1839501 2','D575 55658 201','L97','C',1,'RP371763','','5154','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','Slot over size NOGO gauge entered.','wrong cutter radius copensetion given by operator.','Readjust the copensetion,then part found ok.','proper instructions given to operator,found ok','Next production batch found ok.','','2010-02-17','Dinakara(G)','Dinakara(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(528,'18-003A','Magellan Aerospace Wrexham','BRACKET SUPPORT','284063C','D361 50111 200 01','ABM3-1029','A',1,'RP96871 Amendment1','','5058','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','1x45deg chf existed instead of removing burrs in 1hole.','programe mistake','change the programe,then found ok.','proper instructions to programer.found ok.','CA/PA Found satisfactory.','','2010-02-17','Tharanj R(Pandit)','Tharanj R(Pandit)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(529,'18-107A','Magellan Aerospace Bournemouth','LINK ASSY','1243','D574 50553 200','DTD 5014','A',1,'RM365142 Amnd 1','','4274','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','OD 6.17 measures 6.20 / 6.35 at 1plc.','tool offset not taken properly.','tool offset changed and next parts found ok.','instruction given for operator while giving cut crosscheck tooloffset.','CA/PA Found satisfactory.','','2010-02-17','Dinakar(K)','Ashith(B)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(530,'18-088A','Magellan Aerospace Wrexham','PLATE SEALING','122889/001','D572 52998 200 01','ABM3-1029','A',2,'RP96873 Amendment 1','','5270','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','Hole dia6.35/6.40 measures 6.44 (nogo entered)','due to driil over size.','for next job ,changed the drill. Then prat found ok','instructed to operator to check driil size every time.','CA/PA Found satisfactory.','','2010-02-17','Dinakara(G)','Dinakara(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(531,'18-235A','Magellan Aerospace Bournemouth','BUTTSTRAP UPP RS4X12600','2934501','L575 50172 200','ABM3-1029','A00',1,'RM366521','','4972','','0000-00-00',NULL,'yes','no','no','no','no','yes','no','yes','no','Base thickness 2.85/3.15 measures 2.50/2.80mm','Due to bend after operation 01,In operation 03 when base thickness prg running base thick measures minus in center of part.  ','Checked all parts which completed operation 01 and found Ok.After operation 03 base thickness coming OK.','Planned to clamp in HYDRAULIC VICE insted of using WEDGE CLAMP to avoid bend.','Further produced parts found OK.','','2010-02-17','Krishna(Chowdary.G.P.)','Diwakar(R.B.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(532,'18-275A','Magellan Aerospace Bournemouth','BUTTSTRAP','288054','L575 55778 200','ABM3 -1029','A00',1,'RM368750','','4615','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','Base thickness measures under size by 0.02/0.03mm.','Tool offset not taken correctly and this deviation occured.','Tool offset corrected and next part found OK.','Need training for operator due to new employee for the company and training given in machine and also observed while he taking workoffset.','After observing of 02 weeks he can able to take all work offset indivisually.','','2010-02-17','Krishna(Chowdary.G.P.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(533,'18-295A','Magellan Aerospace Bournemouth','BOLT','212880','D577 56145 200','S80','A',9,'RP372021','','4849','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','1) Thread effective dia 18.141/18.225 measures 18.10/18.13 in 3nos.\r\n2) Dia20.959/20.980 measures 20.948/20.956 in 3no\'s\r\n3) Dia22.184/22.205 measures 22.167/22.179 in 3no\'s','1) while adjusting tooloffset 3 nos. rejected.\r\n2) &3) due to wear of inserts od undersize.','1) instruction given to operator for cross check tooloffset onceagaing before leaving cut.\r\n2) & 3) instruction given to operator for crosschecking inserts regular interval.','1) & 2) & 3) same as above','CA/PA Found satisfactory.','','2010-02-17','Dinakar(K)','Vikram(E)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(534,'18-103A','Magellan Aerospace Bournemouth','HEADED BUSH','029275','D572 50465 200','S80','A',8,'RP371226','','5100','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','ID measures under size by 0.02/0.03mm.','while running insert wear out.','insert changed and next peices found ok.','instruction given to operator for checking at regular intervals.','CA/PA Found satisfacory.','','2010-02-17','Dinakar(K)','Narasimha(Murthy R)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(535,'18-103A','Magellan Aerospace Bournemouth','HEADED BUSH','029275','D572 50465 200','S80','A',5,'RP371226','','5099','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','Inner diameter 9.525/9.540 measures 9.542 to 9.550','while running ID measures over size.','Resetting the boring tool,next part found ok.','training given to the operator,found ok','CA/PA Found satisfacory.','','2010-02-17','Dinakar(K)','Nithin(S)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(536,'18-113A','Magellan Aerospace Bournemouth','ADJUSTER','685001','D575 40496 200','S80 FHT','G',6,'RP371232','','5042','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','1) Under cut dia16.66/16.82 measures 17.50mm.\r\n2) ID thread damage noticed in 3no\'s\r\n3) total length: 37.50+0.3/-0.2 measures 37.20','1) & 3) while adjusting tooloffset it will happen.\r\n\r\n2) while running insertsbroken.','1) & 3) instruction given to operator care should be take before giving cut.\r\n\r\n2) instruction given to operator change inserts when it wear out.','same as above.','Further produced parts found OK','','2010-02-18','Dinakar(K)','Ashith(B)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(537,'23-089','Goodrich Aerospace','BASE','522702','A800345-801','7050 T7451 AMS 4050','ECN 78386 (2 Sheets)',1,'CRGL14435-03-10','','5258','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','ID oversize,dia 9.398 to 9.652 measures 9.740.','While running production batch reamer hole measures out off tol up to 2mm depth in hole(6mm deep hole). other side in same part same hole coming ok evan this hole running completion of deviated hole. Suspect that chips clocked in reamer may be this deviation coming.','Coolent arjusted throughly and next part coming.','Taken care to avoid chips clocking in tool.(Arjust coolent properly)','Next part found satisfactory.','','2010-02-19','Krishna(Chowdary.G.P.)','Shivashankar(H.G.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(607,'35-012','Saab AB','JACK BRACKET 1','282520','D576 50009 000 01','7050 T7651 ABM3-1030','C00',1,'PA1217','','5295','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Tool dig mark witnessed on top profile (R25) UPTO 2MM depth.','Program changed due to cycle time reduction then programmer selected wrong tool and dig mark observed. ','Program regenerated and checked and next part coming ok.','Instruction given to programmer to cross check the programme and verify with verifier(In softwear) and given to production.','CA/PA Found satisfactory.','','2010-02-26','Mahesh(B.T.)','Mahesh(B.T.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(608,'35-015','Saab AB','JACK BRACKET 2','296731','D576 50010 001 01','7050 T7651 ABM3-1030','C00',1,'PA1217','','5298','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Tool dig mark noticed on out side profile up to 1mm.','While running production operation 07 roughing prg dia 16 ripper cutter used and given 5mm DOC with high feed.After running smothly tool broken and dig mark coming on outer profile.','Tool changed and decrease the feed (20%)and running the production.','Tool life calculated and instruction given to operator to cross check the tool tip regularly. ','CA/PA Found satisfactory.','','2010-02-26','Krishna(Chowdary.G.P.)','Dhananjaya(N)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(733,'23-060','Goodrich Aerospace','BASE ASSY','20106013','7718152-815','7075 T73511 AMS QQ-A','ECN 102246 (3 Sheets)',3,'CRGL14435-01-09','','4648','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','1)Bore oversize,12.693/12.707 measures 12.714 to 12.717 in 2no.\r\n2)Tool dig mark in bore in depth of 0.5mm in 1no.  ','1)Reworked reamer ie newely coated reamer used directly to part due to past dimension achived in this reamer was good and 2 parts running directly then this deviations coming.\r\n2)While running reamer power cutoff and 0.5 dig mark observed in bore.','1) After running 2 parts,from next part required diameter is achived and all this production batch parts coming ok. \r\n2) Power fail is not predictible.','1) Information given to cutter manufacture to make coating with between required tolearance.\r\n2) Power fail is not predictible.','Next part found satisfactory.','','2010-03-01','Krishna(Chowdary.G.P.)','Rangaswamy()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1074,'35-036','Saab AB','PANEL LANDING LH','47383014','L574 55122 200','ABM3 1029','A00',4,'PA1226-1 Amnd1','','5214','','0000-00-00',NULL,'no','yes','no','yes','no','yes','no','no','no','Raw Material Thickness used is 45mm which should have been less than or equal to 40mm.','Parts manufactured only for dimensional clearances and to stablize process.  ','Informed to costomer to scrap the parts after inspection.','Ordered 40mm (rooling dim 40mm) thick material for next production batch.','Further produced parts found OK.','','2010-03-05','Dayananda(K.G.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1075,'35-050','Saab AB','PANEL LANDING LH','47383014','L574 55150 200','ABM3 1029','A00',2,'PA1226-1 Amnd1','','5213','','0000-00-00',NULL,'no','yes','no','yes','no','yes','no','no','no','Raw Material Thickness used is 45mm which should have been less than or equal to 40mm.','Parts manufactured only for dimensional clearances and to stablize process.  ','Informed to costomer to scrap the parts after inspection.','Ordered 40mm (rooling dim 40mm) thick material for next production batch.','Further produced parts found OK.','','2010-03-05','Dayananda(K.G.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1076,'35-020','Saab AB','PANEL LANDING','583810103','L574 55128 200','ABM3 1029 7010/7050-','A00',2,'PA1226-2 Amd1','','5209','','0000-00-00',NULL,'no','yes','no','yes','no','yes','no','no','no','Raw Material Thickness used is 45mm which should have been less than or equal to 40mm.','Parts manufactured only for dimensional clearances and to stablize process. ','Informed to costomer to scrap the parts after inspection.','Ordered 40mm (rooling dim 40mm) thick material for next production batch.','Further produced parts found OK.','','2010-03-05','Dayananda(K.G.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1077,'35-037','Saab AB','PANEL LANDING RH','47383014','L574 55122 201','ABM3 1029','A00',4,'PA1226-1 Amnd1','','5215','','0000-00-00',NULL,'no','yes','no','yes','no','yes','no','no','no','Raw Material Thickness used is 45mm which should have been less than or equal to 40mm.','Parts manufactured only for dimensional clearances and to stablize process.  ','Informed to costomer to scrap the parts after inspection.','Ordered 40mm (rooling dim 40mm) thick material for next production batch.','Further produced parts found OK.','','2010-03-05','Dayananda(K.G.)','Krishna(Chowdary.G.P.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1078,'18-116A','Magellan Aerospace Bournemouth','Fork End','1340','F575 51377 200','L168','A',0,'RP371771','','5803','','0000-00-00',NULL,'yes','yes','yes','','','','','','','','','','','','','2010-03-06','Dinakar(K)','        Paramesh(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','no','no','yes','','','0','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1079,'18-116A','Magellan Aerospace Bournemouth','Fork End','1340','F575 51377 200','L168','A',0,'RP371771','','5803','','0000-00-00',NULL,'yes','yes','yes','','','','','','','','','','','','','2010-03-06','Dinakar(K)','        Paramesh K','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1080,'35-002','Saab AB','HINGE BRACKET 1','335085','D576 50004 000 01','7050 T7651 ABM3-1030','C00',0,'PA1217','','5656','','0000-00-00',NULL,'yes','yes','yes','','','','','','','','','','','','','2010-03-06','Krishna(Chowdary.G.P.)','        Basavaraja S. Jr.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','','','','0',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1081,'35-002','Saab AB','HINGE BRACKET 1','335085','D576 50004 000 01','7050 T7651 ABM3-1030','C00',0,'PA1217','','5656','','0000-00-00',NULL,'yes','yes','yes','','','','','','','','','','','','','2010-03-06','Krishna(Chowdary.G.P.)','        Basavaraja S. Jr.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1082,'35-002','Saab AB','HINGE BRACKET 1','335085','D576 50004 000 01','7050 T7651 ABM3-1030','C00',0,'PA1217','','5656','','0000-00-00',NULL,'yes','yes','yes','','','','','','','dummy','','','','','','2010-03-06','Krishna(Chowdary.G.P.)','        Basavaraja S. Jr.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1083,'18-097A','Magellan Aerospace Bournemouth','PLATE','50023B','D282 50100 200','L168','A',0,'RP372013','','5778','','0000-00-00',NULL,'yes','yes','yes','','','','','','','','','','','','','2010-03-06','Dinakar(K)','        Ashith B','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1084,'18-107A','Magellan Aerospace Bournemouth','Link Body','M993350','D574 50553 200','DTD 5014','A',0,'RP371771','','5802','','0000-00-00',NULL,'yes','yes','yes','','','','','','','','','','','','','2010-03-06','Dinakar(K)','        Ashith B','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1085,'18-097A','Magellan Aerospace Bournemouth','PLATE','50023B','D282 50100 200','L168','A',0,'RP372013','','5778','','0000-00-00',NULL,'yes','yes','yes','','','','','','','','','','','','','2010-03-06','Dinakar(K)','        Narasimhamurthy K.G.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1086,'18-283A','Magellan Aerospace Bournemouth','FUNK PINS','213776','A572 43263 202','S98','H',0,'RP372020','','5637','','0000-00-00',NULL,'yes','yes','yes','','','','','','','','','','','','','2010-03-06','Dinakara(G)','        Nithin S','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1087,'18-182A','Magellan Aerospace Bournemouth','SCREWED BUSH','G5172H3017','A284 40011 200','DTD 197','A',8,'RM365241 Amnd 1','','5639','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Piece Rotated. ','Due improper claming parts are rotated during the Machining.','Instructed operator to put the proper clamping and ensure the clamping before run the art.','Instructed operator to put the proper clamping and ensure the clamping before run the art.','Found ok.','','2010-03-06','Kumar(K.S.)','        Sathisha K.C.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1088,'18-038A','Magellan Aerospace Bournemouth','Edge Beam Bracket','334864A6','L575 52323 200','ABM3-1029','A00',0,'RP371764','','5682','','0000-00-00',NULL,'yes','yes','yes','','','','','','','','','','','','','2010-03-06','Dinakara(G)','        Manjunatha N.R.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1089,'18-067A','Magellan Aerospace Bournemouth','ANGLE SHROUD ATCH MID UPR','128271','L575 55179 200','ABM3-1029','A00',0,'','','5350','','0000-00-00',NULL,'yes','yes','yes','','','','','','','','','','','','','2010-03-06','Dinakara(G)','Lohith K','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1090,'18-052A','Magellan Aerospace Bournemouth','CLEAT','1070601','L575 52577 200','ABM3-1029','A00',0,'RP371765','','5787','','0000-00-00',NULL,'yes','yes','yes','','','','','','','','','','','','','2010-03-06','Dinakara(G)','        Srinivasa S.N.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1091,'18-052A','Magellan Aerospace Bournemouth','CLEAT','7202101','L575 52577 200','ABM3-1029','A00',0,'RP371765','','5788','','0000-00-00',NULL,'yes','yes','yes','','','','','','','','','','','','','2010-03-06','Dinakara(G)','        Srinivasa S.N.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1092,'18-053A','Magellan Aerospace Bournemouth','CLEAT','1070601','L575 52577 201','ABM3-1029','A00',0,'RP371765','','5794','','0000-00-00',NULL,'yes','yes','yes','','','','','','','','','','','','','2010-03-06','Dinakara(G)','        Srinivasa S.N.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1093,'18-053A','Magellan Aerospace Bournemouth','CLEAT','7202101','L575 52577 201','ABM3-1029','A00',0,'RP371765','','5795','','0000-00-00',NULL,'yes','yes','yes','','','','','','','','','','','','','2010-03-06','Dinakara(G)','        Srinivasa S.N.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1094,'18-052A','Magellan Aerospace Bournemouth','CLEAT','7202101','L575 52577 200','ABM3-1029','A00',0,'RP371765','','5788','','0000-00-00',NULL,'yes','yes','yes','','','','','','','','','','','','','2010-03-06','Dinakara(G)','        Srinivasa S.N.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1095,'18-053A','Magellan Aerospace Bournemouth','CLEAT','7202101','L575 52577 201','ABM3-1029','A00',0,'RP371765','','5795','','0000-00-00',NULL,'yes','yes','yes','','','','','','','','','','','','','2010-03-06','Dinakara(G)','        Srinivasa S.N.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1096,'18-283A','Magellan Aerospace Bournemouth','FUNK PINS','213776','A572 43263 202','S98','H',0,'RP372020','','5637','','0000-00-00',NULL,'yes','yes','yes','','','','','','','','','','','','','2010-03-06','Dinakar(K)','        Narasimha Murthy R','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1097,'18-116A','Magellan Aerospace Bournemouth','Fork End','1340','F575 51377 200','L168','A',0,'RP371771','','5803','','0000-00-00',NULL,'yes','yes','yes','','','','','','','','','','','','','2010-03-06','Dinakar(K)','        Ramesh S. Bandagi','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1098,'18-193A','Magellan Aerospace Bournemouth','BUSH FLANGED','G2685C1283','L575 52508 200','B23','B00',0,'RP371247 Amnd 1','','5797','','0000-00-00',NULL,'yes','yes','yes','','','','','','','','','','','','','2010-03-06','Dinakar(K)','        Ramesh S. Bandagi','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','','','','','0',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1099,'18-182A','Magellan Aerospace Bournemouth','SCREWED BUSH','G5172H3017','A284 40011 200','DTD 197','A',0,'RM365241 Amnd 1','','5639','','0000-00-00',NULL,'yes','yes','yes','','','','','','','','','','','','','2010-03-06','Kumar(K.S.)','        Satheesha H.K.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1100,'30-005','Gardner Aerospace Burnley Limited','RIB 2A FWD OFW - LH','8068501 01','L575 51777 200','ABM3-1029 T7651','A, ECN: PG60049N01JA85',1,'','','5755','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Side positive wall rib measures -0.05 to -0.1mm out of talarence.','Due to vibration while running the positive wall.','Informed to CAD department to change the cutting parameters for rib machining.','Standardised the parameters for rib machining.','NEXT BATCH FOND SATISFACORY.','','2010-03-06','Kumar(K.S.)','Satheesha H.K.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','','yes',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1101,'30-005','Gardner Aerospace Burnley Limited','RIB 2A FWD OFW - LH','8068501 01','L575 51777 200','ABM3-1029 T7651','A, ECN: PG60049N01JA85',1,'','','5754','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Side positive wall rib measures -0.05 to -0.1mm out of talarence.','Due to vibration while running the positive wall.','Informed to CAD department to change the cutting parameters for rib machining.','Standardised the parameters for rib machining.','CA/PA Found satisfacory.','','2010-03-06','Kumar(K.S.)','Satheesha H.K.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','','yes','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1102,'18-038A','Magellan Aerospace Bournemouth','Edge Beam Bracket','334864A6','L575 52323 200','ABM3-1029','A00',0,'RP371764','','5682','','0000-00-00',NULL,'yes','yes','yes','','','','','','','','','','','','','2010-03-06','Dinakara(G)','        Siddaramappa ','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1103,'18-038A','Magellan Aerospace Bournemouth','Edge Beam Bracket','334864A6','L575 52323 200','ABM3-1029','A00',0,'RP371764','','5681','','0000-00-00',NULL,'yes','yes','yes','','','','','','','','','','','','','2010-03-06','Dinakar(K)','        Siddaramappa ','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1104,'07-001','HAL-NASIK','WALL 1 ROOT PART - RH','A/SU/4587/08','11.2000.2.101.001','V95pchT2','NIL',0,'NK/M/2513(3131)/MP/O','','5765','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Dig marks noticed in ribs corners.','Wrong program given by programer.','Immideately inform to Cad_cam department to check the program and currect the wrong program. ','Instructed programer to check the programe in software simulation and gauge check before given to production.','Found satisfactary.','','2010-03-06','Kumar(K.S.)','Narayanappa G','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','','','','0',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1105,'07-002','HAL-NASIK','WALL 1 ROOT PART - LH','A/SU/4582/08','11.2000.2.101.002','V95pchT2','NIL',0,'NK/M/2513(3131)/MP/O','','5766','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Dig marks noticed in ribs corners.','Wrong program given by programer.','Immideately inform to Cad_cam department to check the program and currect the wrong program. ','Instructed programer to check the programe in software simulation and gauge check before given to production.','CA/PA found Satisfactory .','','2010-03-06','Kumar(K.S.)','Narayanappa G','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','yes','no','','','','0',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1106,'18-052A','Magellan Aerospace Bournemouth','CLEAT','7202101','L575 52577 200','ABM3-1029','A00',0,'RP371765','','5788','','0000-00-00',NULL,'yes','yes','yes','','','','','','','','','','','','','2010-03-06','Krishna(Chowdary.G.P.)','        Girish Prasad P','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1107,'18-053A','Magellan Aerospace Bournemouth','CLEAT','7202101','L575 52577 201','ABM3-1029','A00',0,'RP371765','','5795','','0000-00-00',NULL,'yes','yes','yes','','','','','','','','','','','','','2010-03-06','Krishna(Chowdary.G.P.)','        Girish Prasad P','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1108,'18-054A','Magellan Aerospace Bournemouth','CLEAT','190735','L575 52580 200','ABM3-1029','A00',0,'RP371765','','5342','','0000-00-00',NULL,'yes','yes','yes','','','','','','','','','','','','','2010-03-06','Krishna(Chowdary.G.P.)','                Girish Prasad P','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1109,'18-055A','Magellan Aerospace Bournemouth','CLEAT','190735','L575 52580 201','ABM3-1029','A00',0,'RP371765','','5343','','0000-00-00',NULL,'yes','yes','yes','','','','','','','','','','','','','2010-03-06','Krishna(Chowdary.G.P.)','                Girish Prasad P','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1110,'18-197A','Magellan Aerospace Wrexham','ANGLE CLEAT','336220A9','D572 59284 200 01','ABM3-1029','A',0,'RP96879 Amend1','','5744','','0000-00-00',NULL,'yes','yes','yes','','','','','','','','','','','','','2010-03-06','Dinakara(G)','                Theerthappa K.N.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1111,'18-194A','Magellan Aerospace Wrexham','M/C BRACKET','336220A9','D572 59092 200 01','ABM3-1029','A',0,'RP96879 Amend1','','5751','','0000-00-00',NULL,'yes','yes','yes','','','','','','','','','','','ok','','2010-03-06','Dinakara(G)','                Siddaramappa ','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1112,'18-197A','Magellan Aerospace Wrexham','ANGLE CLEAT','336220A9','D572 59284 200 01','ABM3-1029','A',0,'RP96879 Amend1','','5744','','0000-00-00',NULL,'yes','yes','yes','','','','','','','','','','','','','2010-03-06','Dinakara(G)','                Siddaramappa ','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1113,'18-197A','Magellan Aerospace Wrexham','ANGLE CLEAT','336220A9','D572 59284 200 01','ABM3-1029','A',0,'RP96879 Amend1','','5744','','0000-00-00',NULL,'yes','yes','yes','','','','','','','','','','','','','2010-03-06','Dinakara(G)','        Theerthappa K.N.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1114,'18-283A','Magellan Aerospace Bournemouth','FUNK PINS','213776','A572 43263 202','S98','H',0,'RP372020','','5637','','0000-00-00',NULL,'yes','yes','yes','','','','','','','','','','','','','2010-03-06','Dinakar(K)','        Rajesh T','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1115,'18-283A','Magellan Aerospace Bournemouth','FUNK PINS','213776','A572 43263 202','S98','H',0,'RP372020','','5637','','0000-00-00',NULL,'yes','yes','yes','','','','','','','','','','','','','2010-03-06','Dinakar(K)','        Rajesh T','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1116,'18-193A','Magellan Aerospace Bournemouth','BUSH FLANGED','G2685C1283','L575 52508 200','B23','B00',0,'RP371247 Amnd 1','','5797','','0000-00-00',NULL,'yes','yes','yes','','','','','','','','','','','','','2010-03-06','Dinakar(K)','        Vikram E','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1117,'18-193A','Magellan Aerospace Bournemouth','BUSH FLANGED','G2685C1283','L575 52508 200','B23','B00',0,'RP371247 Amnd 1','','5797','','0000-00-00',NULL,'yes','yes','yes','','','','','','','','','','','','','2010-03-06','Dinakar(K)','        Vikram E','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1118,'18-209A','Verdict Aerospace Components Ltd.','BODY ASSEMBLY','1276','D321 40204 202','L168','D',0,'57266','','5810','','0000-00-00',NULL,'yes','yes','yes','','','','','','','','','','','','','2010-03-06','Dinakar(K)','        Vikram E','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1119,'30-006','Gardner Aerospace Burnley Limited','RIB 2A FWD OFW - RH','8068501 01','L575 51777 201','ABM3-1029 T7651','A, ECN:PG60049N01JA85',1,'','','5756','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Web thickess measures -0.1 in the portion of 50mm in one pockect.','Bottom face not butting due to bend in material.','Put extra clamp for proper butting the bottom face.','Plane to intraduce sufficient clamps to hold the job.','CA/PA Found satisfactory.','','2010-03-06','Kumar(K.S.)','Gajendra Singh C.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','no','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1120,'30-023','Gardner Aerospace Burnley Limited','RIB 4 OFW - RH','722727A5','L575 54204 201','ABM3-1029 T7651','B, ECN:PG69999001JP98',0,'PRO0016489-S2','','5823','','0000-00-00',NULL,'yes','yes','yes','','','','','','','All corner rib measers -0.1mm out of tolarene.','Due to holder run out.','Replace the tool holder & defect holder was scraped.','Checked & ensured that the old tool holders are in working condition.','CA/PA Found satisfactory.','','2010-03-06','Kumar(K.S.)','Gajendra Singh C.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','','yes','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1121,'18-038A','Magellan Aerospace Bournemouth','Edge Beam Bracket','334864A6','L575 52323 200','ABM3-1029','A00',0,'RP371764','','5681','','0000-00-00',NULL,'yes','yes','yes','','','','','','','','','','','','','2010-03-06','Dinakara(G)','        Anjinamurthy H','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1122,'18-038A','Magellan Aerospace Bournemouth','Edge Beam Bracket','334864A6','L575 52323 200','ABM3-1029','A00',0,'RP371764','','5680','','0000-00-00',NULL,'yes','yes','yes','','','','','','','','','','','','','2010-03-06','Dinakara(G)','        Anjinamurthy H','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1123,'18-038A','Magellan Aerospace Bournemouth','Edge Beam Bracket','334864A6','L575 52323 200','ABM3-1029','A00',0,'RP371764','','5679','','0000-00-00',NULL,'yes','yes','yes','','','','','','','','','','','','','2010-03-06','Dinakara(G)','        Anjinamurthy H','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1124,'35-002','Saab AB','HINGE BRACKET 1','335085','D576 50004 000 01','7050 T7651 ABM3-1030','C00',0,'PA1217','','5656','','0000-00-00',NULL,'yes','yes','yes','','','','','','','dummy','','','','','','2010-03-06','Krishna(Chowdary.G.P.)','        Basavaraja S. Jr.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1125,'18-039A','Magellan Aerospace Bournemouth','Edge Beam Bracket','334864A6','L575 52323 201','ABM3-1029','A00',0,'RP371764','','5684','','0000-00-00',NULL,'yes','yes','yes','','','','','','','','','','','','','2010-03-06','Dinakara(G)','        Anjinamurthy H','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1126,'35-002','Saab AB','HINGE BRACKET 1','335085','D576 50004 000 01','7050 T7651 ABM3-1030','C00',0,'PA1217','','5656','','0000-00-00',NULL,'yes','yes','yes','','','','','','','dummy','','','','','','2010-03-06','Krishna(Chowdary.G.P.)','        Basavaraja S. Jr.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1127,'35-002','Saab AB','HINGE BRACKET 1','335085','D576 50004 000 01','7050 T7651 ABM3-1030','C00',0,'PA1217','','5656','','0000-00-00',NULL,'yes','yes','yes','','','','','','','dummy','','','','','','2010-03-06','Krishna(Chowdary.G.P.)','        Basavaraja S. Jr.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1128,'35-002','Saab AB','HINGE BRACKET 1','335085','D576 50004 000 01','7050 T7651 ABM3-1030','C00',0,'PA1217','','5656','','0000-00-00',NULL,'yes','yes','yes','','','','','','','dummy','','','','','','2010-03-06','Krishna(Chowdary.G.P.)','        Dhananjaya N','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1129,'35-002','Saab AB','HINGE BRACKET 1','335085','D576 50004 000 01','7050 T7651 ABM3-1030','C00',0,'PA1217','','5656','','0000-00-00',NULL,'yes','yes','yes','','','','','','','dummy','','','','','','2010-03-06','Krishna(Chowdary.G.P.)','        Dhananjaya N','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1130,'35-002','Saab AB','HINGE BRACKET 1','335085','D576 50004 000 01','7050 T7651 ABM3-1030','C00',0,'PA1217','','5656','','0000-00-00',NULL,'yes','yes','yes','','','','','','','dummy','','','','','','2010-03-06','Krishna(Chowdary.G.P.)','        Dhananjaya N','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1131,'35-002','Saab AB','HINGE BRACKET 1','335085','D576 50004 000 01','7050 T7651 ABM3-1030','C00',0,'PA1217','','5656','','0000-00-00',NULL,'yes','yes','yes','','','','','','','dummy','','','','','','2010-03-06','Krishna(Chowdary.G.P.)','        Basavaraja S. Jr.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1132,'35-002','Saab AB','HINGE BRACKET 1','335085','D576 50004 000 01','7050 T7651 ABM3-1030','C00',0,'PA1217','','5656','','0000-00-00',NULL,'yes','yes','yes','','','','','','','dummy','','','','','','2010-03-06','Krishna(Chowdary.G.P.)','        Basavaraja S. Jr.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1133,'35-002','Saab AB','HINGE BRACKET 1','335085','D576 50004 000 01','7050 T7651 ABM3-1030','C00',0,'PA1217','','5656','','0000-00-00',NULL,'yes','yes','yes','','','','','','','dummy','','','','','','2010-03-06','Krishna(Chowdary.G.P.)','        Basavaraja S. Jr.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1134,'18-107A','Magellan Aerospace Bournemouth','Link Body','M993350','D574 50553 200','DTD 5014','A',0,'RP371771','','5802','','0000-00-00',NULL,'yes','yes','yes','','','','','','','','','','','','','2010-03-07','Dinakar(K)','        Ashith B','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1135,'18-209A','Verdict Aerospace Components Ltd.','BODY ASSEMBLY','1276','D321 40204 202','L168','D',0,'57266','','5810','','0000-00-00',NULL,'yes','yes','yes','','','','','','','','','','','','','2010-03-07','Dinakara(G)','        Paramesh K','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1136,'18-210A','Verdict Aerospace Components Ltd.','BODY ASSEMBLY','1276','D321 40204 204','L168','D',0,'57266','','5812','','0000-00-00',NULL,'yes','yes','yes','','','','','','','','','','','','','2010-03-07','Dinakara(G)','        Paramesh K','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1137,'18-039A','Magellan Aerospace Bournemouth','Edge Beam Bracket','334864A6','L575 52323 201','ABM3-1029','A00',0,'RP371764','','5684','','0000-00-00',NULL,'yes','yes','yes','','','','','','','','','','','','','2010-03-07','Dinakara(G)','        Manjunatha N.R.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1138,'18-209A','Verdict Aerospace Components Ltd.','BODY ASSEMBLY','1276','D321 40204 202','L168','D',1,'57266','','5810','','0000-00-00',NULL,'yes','yes','yes','','','','','','','peice damage.','RUNNING TIME INSERT BROKEN SO 1no,REJECTED.','insert change & running.','every 20 numbers one time insert checking.','CA/PA found satisfactory.','','2010-03-08','Dinakar(K)','        Ramesh S. Bandagi','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1139,'35-014','Saab AB','JACK BRACKET 2','296731','D576 50010 000 01','7050 T7651 ABM3-1030','C00',1,'PA1217','','5297','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Out side profile minus by 1mm. (COS points)','Due to part not butted properly to butting face in boring operation therefore this deviation coming.','Instruction given to operator to take care while clamping and cross check once that part is butted properly.','Feeler guage given to oprator to cross check the butting face for every part while doing boring operation and also instruction sheet placed in front of machine to avoid such human error.','Further produced parts found OK.','','2010-03-09','Krishna(Chowdary.G.P.)','Srinivasa(S.N.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1140,'35-008','Saab AB','HINGE BRACKET 4','292537','D576 50007 000 01','7050 T7651 ABM3-1030','D00',1,'PA1217','','5647','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Wall thickness 3.2mm measures 1mm near to slot.','Y ref not taken correctly and after roughing operation found wrong work workoffset and part wall thick meaasures minus side.','Y workoffset correct and continued production.','Instruction given to operator to take care while doing firstoff and crosscheck once.','Further produced parts found OK.','','2010-03-09','Krishna(Chowdary.G.P.)','Dhananjaya(N)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1141,'35-015','Saab AB','JACK BRACKET 2','301752C','D576 50010 001 01','7050 T7651 ABM3-1030','C00',1,'PA1217','','5528','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Tool dig mark witnessed on out side profile to a depth of 1mm.','While running production tool broken and dig mark observed.','Cutter changed and parameter reduced and running production.','Instruction given to operator to monitor the tool life and replace after running know nos of parts produced. ','Further production batch found OK.','','2010-03-09','Krishna(Chowdary.G.P.)','Srinivasa(S.N.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1142,'35-014','Saab AB','JACK BRACKET 2','301752B','D576 50010 000 01','7050 T7651 ABM3-1030','C00',1,'PA1217','','5526','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Tool dig mark witnessed on out side profile upto 3mm for the full length.','Tool broken and dig mark observed on profile. ','Tool changed and continued production.','Taken care to avoid tool broken.','further produced parts found OK.','','2010-03-09','Krishna(Chowdary.G.P.)','Girish(Prasad P)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1143,'18-098A','Magellan Aerospace Bournemouth','SEAT VALVE','B6353','D282 50060 204','L110','D',1,'RP372014','','5451','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Tool dig mark witnessed on out side profile up to 2mm.','operator not putted bolts before cutting operation.','warning given to operator for puttin bolts before cutout.','message added in program one more time for putting clamps.','CA/PA Found satisfactory.','','2010-03-09','Dinakara(G)','Siddaramappa()','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1144,'18-083A','Magellan Aerospace Wrexham','STUD PLATE','315926','D278 50007 201','ABM3-1029','D01',1,'RM90860','','4557','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Base thickness minus by 0.3mm.','Operator did not butt the job properly','Instructed Operator to butt the job properly and clamp','Instructed Operator to butt the job properly and clamp','Further produced parts found OK','','2010-03-09','Dinakara(G)','Lohith(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1145,'18-117A','Magellan Aerospace Bournemouth','HOUSING-OUT BD BRG','662385','D275 40004 200','S130 FHT','C01',1,'RM365157','','4269','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','OD 69.95/69.97 MEASURES DIA69.93 AND BORE MEASURES PLUS SIDE BY 20MICRON.','part rotate while running due insuficient tight for part,','for next part will hold at suficient tight & part found ok.','instructed to operator to check tightness for every pice.','CA/PA Found satisfatory.','','2010-03-09','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1146,'18-216A','Verdict Aerospace Components Ltd.','PIN HINGE CON DRIVEN','A4004A','L579 51150 200','S145 FHT','A00',2,'57249','','5235','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Dia 4.0 hole center distance shift by 0.5to0.6mm.','while maching part rotate due to insuficient holding.','chaning clamping method,found ok','checking clamping for every part','Next part found satisfactory.','','2010-03-09','Dinakara(G)','Dinakara(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1147,'18-104A','Magellan Aerospace Bournemouth','BODY TURNBUCKLE','654734','D575 40490 200','S80 FHT','E',7,'RM365144 Amnd 1','','4233','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','1) ID thread damage noticed in 2no\'s\r\n2) RH thread NOGO gauge not answered in 5no\'s','1) Power failure during machining caused the deviation\r\n2) Threading tool not set correctly','1) power failure unpredictable\r\n2) Threading tool setting done correctly','1) power failure unpredictable\r\n2) Instructed operator to set the threading tool properly','Further produced parts found OK','','2010-03-09','Dinakar(K)','Narasimhamurthy(K.G.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1148,'18-215C','Verdict Aerospace Components Ltd.','ROD END ASSMY - MALE','631551','D321 53012 200','S98-FHT','F01',3,'57257','','4459','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Thread effective dia 8.71/8.76 measures 8.65/8.70mm.','due iserts wear.','inserts change,next parts found ok.','instructed to oparetor to check the inserts for regular intervals.','ca/pa found satisfactory.','','2010-03-09','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1149,'18-049A','Magellan Aerospace Bournemouth','CLEAT','1866601','L575 52505 201','ABM3-1029','A00',1,'RM365124','','4381','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Thickness 2.5 +/-0.25 measures 2.20 to 2.25mm.','Butting problem','butting properly,next part found ok','instructed to operator by supervisor,found ok','Further produced parts found OK','','2010-03-09','Dinakara(G)','Dinakara(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1150,'18-194A','Magellan Aerospace Wrexham','M/C BRACKET','336220A9','D572 59092 200 01','ABM3-1029','A',7,'RP96879 Amend1','','5751','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Thickness 5.10mm minimum measures 5.02 to 5.08mm.','Holding problem.','proper holding for next parts ,found ok','plane for proper holding.','Next further production batch found ok.','','2010-03-09','Dinakara(G)','Dinakara(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1151,'18-110A','Magellan Aerospace Bournemouth','FORK END INTERMEDIATE','195650','D575 40494 202','S80 FHT','J',1,'RP371231','','5580','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Thread damage witnessed in 1no.','Power failure during machining.','Power failure unpredictable.','Power failure unpredictable.','Further produced parts found ok.','','2010-03-09','Dinakar(K)','Paramesh(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1152,'18-003A','Magellan Aerospace Wrexham','BRACKET SUPPORT','47383013','D361 50111 200','ABM3-1029','A',2,'RP96871 Amendment1','','5468','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Tool dig mark witnessed in the rib upto 0.5mm.','OParetor did not take the offset correctly.','Corrected the tool offset.','Instructed the operstor to take the tool offset correctly. ','Further produced parts found ok.','','2010-03-09','Dinakara(G)','Manohara(M)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1153,'18-075A','Magellan Aerospace Wrexham','ADAPTOR','18882/011','D282 50044 200PF',' L111 T6','A',3,'RP97166','','4856','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','1) Tool dig mark noticed in the square for 1no.\r\n2) OD 48.23/48.36 measures 48.10 in 2no\'s.','1) Tool brocken during machining.\r\n2) Tool tip chipoff ,hence deviation occured.','1) Changed the  new tool.\r\n2) Changed the insert. ','Instructed the operator to chek the sharpness of the tool. ','Further produced parts found ok.','','2010-03-09','Dinakar(K)','Narasimhamurthy(K.G.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1154,'18-185A','Magellan Aerospace Bournemouth','BUSH','F1041F7517','L575 50327 200','B23','B00',2,'RP371247 Amnd 1','','5616','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','Bore over size: dia21.00 to 21.02 measures 21.030 to 21.031mm.','During setting the boring tool this deviation occured.','Insrtucted the operator to set the boring tool correctly.','Insrtucted the operator to set the boring tool correctly.','Further produced parts found ok.','','2010-03-09','Dinakar(K)','Nithin(S)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1155,'18-077A','Magellan Aerospace Wrexham','COUPLING','3259181','D282 50075 200PF',' L111 T6','A',1,'PRP91020 Amendment 1','','4307','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Height 23.0mm measures 22.60mm.','OParetor did not butt the job properly.','Instructed the operator to butt the job properly.','Instructed the operator to butt the job properly.','Further produced parts found ok.','','2010-03-09','Dinakar(K)','Ashith(B)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1156,'18-193A','Magellan Aerospace Bournemouth','BUSH FLANGED','G2685C1283','L575 52508 200','B23','B00',1,'RP371247 Amnd 1','','5797','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Bore dia20.00/20.021 measures 20.031mm.','During boring tool setting this deviation occured.','Istructed the operator to set the boring tool correctly.','Istructed the operator to set the boring tool correctly.','Further produced parts found ok.','','2010-03-09','Dinakar(K)','Narasimha(Murthy R)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1157,'18-110A','Magellan Aerospace Bournemouth','FORK END INTERMEDIATE','698428','D575 40494 202','S80 FHT','J',1,'RM365150','','4386','','0000-00-00',NULL,'yes','no','yes','no','yes','no','no','no','no','Thread damage noticed in 1no.','Power failure during machining caused the deviation','Power failure unpredictable','Power failure unpredictable','Further produced parts found OK','','2010-03-10','Dinakar(K)','Paramesh(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1158,'18-039A','Magellan Aerospace Bournemouth','Edge Beam Bracket','334864A6','L575 52323 201','ABM3-1029','A00',2,'RP371764','','5683','1','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','Bore measures over size by 5 to 20micron.','Boring tool not set properly','Instructed the operator to set the boring tool correctly','Instructed the operator to set the boring tool correctly','Further produced parts found OK','','2010-03-10','Dinakara(G)','Jayarama(M.B.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1159,'01-319','HAL-Helicopter','FRAME #7 TOP','H918-86/08','201S 533H 6221 201','LN 9073 - 3.1354 T 3','DRN STP2590 ISS A',1,'','','5695','','0000-00-00',NULL,'yes','','yes','','','','','yes','','Web opened out.','Since the base thickness was only 2mm ,due to vibration while machining this deviation occured.','Approach point of 40 dia tool was wrong in NC program.Informed to CAD-CAM department to modify the NC program.','25 Dia cutter will be placed in place of 40 dia cutter.','CA/PA Found satisfactory.','','2010-03-12','Kumar(K.S.)','Satheesha H.K.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1160,'18-295A','Magellan Aerospace Bournemouth','BOLT','212880','D577 56145 200','S80','A',1,'RM369940','','5898','','0000-00-00',NULL,'yes','yes','yes','','','','','','','bore dig mark.','countine running 115 nos after runnig time toool damage . so bore damage.','new  tool added.','after 100nos tool changed.','Further produced parts found O.K','','2010-03-19','Dinakar(K)','Vikram E','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1161,'23-029','Goodrich Aerospace','REINFORCEMENT PLATE','729140100','7712500-8106','7075 T651 AMS-QQ-A-2','TR IP 7712500-8106 REV 01',1,'CRGL14416-04-10','','5928','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1)2x 6.858 thickness +.750/-.750 measure 5.867','while removing extra lugs at ends this deviation occured','Instructed fitter to take care while removing extra lugs','Instructed fitter to take care while removing extra lugs','CA/PA Found satisfactory.','','2010-03-20','Nagaraju(T)','Raghu(J)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1162,'23-086','Goodrich Aerospace','BASE','267852','A800268-812','7050 T7451 AMS 4050','ECN 71347 (2 Sheets)',1,'CRGL14435-03-10','','5864','','0000-00-00',NULL,'yes','','yes','','','','','yes','','* Dia 11.11 remer problem. Remer running time one side bore + side [+0.10]. So one piece reject.','Due to reamer problem this deviation coming.','Production stoped and immediately ordered new reamer. ','After received new reamer,Reamer run out checked and proved in dummy part.\r\nAfter proving production continued.','Next part found satisfactory.','','2010-03-20','Krishna(Chowdary.G.P.)','Girish Prasad P','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1163,'18-077A','Magellan Aerospace Wrexham','COUPLING','3344198','D282 50075 200PF',' L111 T6','A',1,'RP97167','','6012','','0000-00-00',NULL,'yes','yes','yes','','','','','','','O.D minus','Program mistake for 1 number rejected','program corrected.','program saved.','CA/ PA FOUND SATISFACTORY','','2010-03-22','Dinakar(K)','Ashith B','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1164,'18-039A','Magellan Aerospace Bournemouth','Edge Beam Bracket','334864A6','L575 52323 201','ABM3-1029','A00',1,'RP371764','','6019','','0000-00-00',NULL,'yes','yes','yes','','','','','','','Base thickness under size.','Due to part butting not properly.','Next part butting properly then checked by the feeler gauge.','Instructed operator to every part butting properly and checked by the feeler gauge.','CA/PA found satisfactory.','','2010-03-22','Dinakara(G)','        Lohith K','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1165,'18-106A','Magellan Aerospace Bournemouth','EYE END INBOARD','723001','D575 41542 200','S98 FHT','D',2,'RP371236','','6069','','0000-00-00',NULL,'yes','yes','yes','','','','','','','peice damage','Jaws problem peice shifted.','change the jaws.','jaws sepperate.','','','2010-03-22','Dinakar(K)','Narasimhamurthy K.G.','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1166,'01-319','HAL-Helicopter','FRAME #7 TOP','H918-86/08','201S 533H 6221 201','LN 9073 - 3.1354 T 3','DRN STP2590 ISS A',1,'','','5695','','0000-00-00',NULL,'yes','no','yes','no','no','no','no','yes','no','Tool dig mark witnesed in the base.','Since the base thickness was only 2mm ,due to vibration while machining this deviation occured.','Inform to CAD-CAM department to analise the problem.','Programe is changed dia 40cutter to dia 25 and aproch point to avaid the vibration.','CA/PA Found satisfactory.','','2010-03-22','Kumar(K.S.)','Satheesha(H.K.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1167,'30-031','Gardner Aerospace Burnley Limited','RIB 2A AFT LH','8046501 01','L575 58376 200','ABM3-1029 T7651','A,ECN: PG617330066JA02',1,'','','5960','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','tool dig mark witnessed on the top face.','operator enter wrong tool offset value in the machine.','Corrected the tool offset value which was wrongly entered.','Instructed to operator to take the tool offset correctly.','Futher produced parts found ok.','','2010-03-22','Kumar(K.S.)','Sathisha(K.C.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1168,'18-085A','Magellan Aerospace Wrexham','BRACKET SUPPORT','M122420','D579 52009 200','L168','A',1,'RM90861','','4054','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','dia 4.40 pin nogo gauge enters.','Due to drill runout this deviation occured.','REmoved the drill , reclamped the driil without runout.','Instructed the operator to hold the drill without runout.','Furter produced parts found ok.','','2010-03-22','Dinakara(G)','Dinakara(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1169,'18-084A','Magellan Aerospace Wrexham','BRACKET SUPPORT','M122420','D579 52008 200','L168','C01',1,'RM90861','','4444','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','instead of dia4.0 hole 4.30 pin gauge entering.','Wrong section of drill bit caused the deviation.','Changed the drill bit.','Instructed the operator to check the drill size before using it.','Further produced parts found ok.','','2010-03-22','Dinakara(G)','Mohan(Kumar C.M.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1170,'18-084A','Magellan Aerospace Wrexham','BRACKET SUPPORT','M122420','D579 52008 200','L168','C01',1,'RM90861','','4017','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Thickness under size by 0.2mm','while doing facing in conventional milling machine operator not given correct tool movement.','warning given to operator take care while giving cut.','same as above.','Next part found satisfactory.','','2010-03-22','Stalin(G)','Suresh(K.R.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1171,'18-106A','Magellan Aerospace Bournemouth','EYE END INBOARD','723001','D575 41542 200','S98 FHT','D',1,'RM365154 Amnd 1','','4236','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','thread damage noticed in 1no.','while running thread operation power failured.','','','','','2010-03-22','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1172,'18-202A','Magellan Aerospace Wrexham','ANGLE CLEAT','276012','D572 59281 200 01','ABM3-1029','A',1,'RM90868','','4431','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','hole over size and it looks like oval shape.','drill runout not cross checked operator.','instructed to operator for checking runout before putting on part and then prove the drill on extra material.','instructed to operator for checking runout before putting on part and then prove the drill on extra material.','Further batches found satisfactory.','','2010-03-22','Dinakara(G)','Anjinamurthy(H)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1173,'18-211A','Verdict Aerospace Components Ltd.','PLUNGER','694000','D321 40205 200','S80-FHT','H01',7,'55568','','3562','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','1) dia9.965/9.975 measures 9.958/9.962 in 2no\'s\r\n2) ID thread damage noticed in 1no.\r\n3) dia 17.446/17.464 measures 17.438/17.440 in 4no\'s.','1) & 3) refer ncr 1180\r\n2) while running drill blent due to this thread damage.','1) & 3) refer 1180\r\n3) drill changed.','1) & 3) refer 1180\r\n3) drill grade chnged for next batch.','CA/PA Found satisfatory.','','2010-03-22','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1174,'18-197A','Magellan Aerospace Wrexham','ANGLE CLEAT','276012','D572 59284 200 01','ABM3-1029','A',8,'RM90868','','4178','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','Hole pitch under size by 0.3mm.','due to wrong setting this deviation occurs.','once again resetting done and next peices found ok.','on training given on machine for setting that part.','Next production part found satisfactory.','','2010-03-22','Dinakara(G)','Theerthappa(K.N.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1175,'18-214A','Verdict Aerospace Components Ltd.','SPECIAL WASHER','631551','D321 40210 202','S98','E01',7,'55568','','2137','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','7.90/8.20 length under size.','while improper broaching of parts this deviation occurs.','instruction given for operator care should be take while broach because it is mannual movement.','same as above.','Next part found satisfactory.','','2010-03-22','Stalin(G)','Suresh(K.R.)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1176,'18-295A','Magellan Aerospace Bournemouth','BOLT','212880','D577 56145 200','S80','A',7,'RP372021','','5184','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','1) OD 22.184/22.205 MEASURES 22.163 / 22.181 IN 7NO\'S.\r\n2) 1X30 CHF MEASURES 1.60X30 IN 1NO.','1) refer ncr 1180.','1) refer ncr 1180.','1) refer ncr 1180.','CA/PA Found satisfactory.','','2010-03-22','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1177,'18-078A','Magellan Aerospace Wrexham','ADAPTOR','18883/012','A282 50081 200PF',' L111 T6','A',2,'RP97165','','5287','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1) BOR DIA58.115/58.16 MEASURES DIA58.19/58.20 IN 1NO.\r\n2) TOOL DIG MARK NOTICED ON OD.','1) refer NCR 1180\r\n2) while running peice came outside from jaws.','1) refer NCR 1180\r\n2) jaws pressure increased next peices found ok.',' 1) refer NCR 1180\r\n 2) same as above.','Next part found satisfactory.','','2010-03-22','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1178,'18-104A','Magellan Aerospace Bournemouth','BODY TURNBUCKLE','029839','D575 40490 200','S80 FHT','E',6,'RP371228','','4703','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1) 1/2X20 unjf - 3B nogo gauge answereing in 1no(LH side).\r\n2) 1/2x20 unjf - 3B LH nogo gauge answereing in 4no\'s\r\n3) 1/2x20 unjf - 3B thread damage noticed in 1no.','1) &2) refer NCR1180\r\n2) while running power failure.','1) & 2)refer NCR1180','10 &2) refer NCR1180','Next part found satisfactory.','','2010-03-22','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1179,'18-084A','Magellan Aerospace Wrexham','BRACKET SUPPORT','M122420','D579 52008 200','L168','C01',1,'RP96874 Amendment 1','','5264','','0000-00-00',NULL,'yes','yes','yes','no','no','no','no','no','no','1) tool dig mark noticed on side face upto 2mm depth.','while machining part is declamped from the vice, so dig mark found in side face.','re setting the  with proper holding,found ok','instructed to operator to hold the job properly,and tightly.','Next part found satisfactory.','','2010-03-22','Dinakara(G)','Dinakara(G)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','','0',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),(1180,'18-102A','Magellan Aerospace Bournemouth','BARREL-STRUT','184582','D572 50463 200','S98 FHT','F',4,'RP371225','','5456','','0000-00-00',NULL,'yes','yes','no','no','no','yes','no','no','no','1) NOGO gauge answered in 2no\'s.\r\n2) Total length under size in 2no\'s.','1) while giving tooloffset correction this deviation occur.\r\n2)tool offset not taken properly.','1) and 2) instruction given to operator while giving corection care to be take.','same as above.','Next part found satisfactory.','','2010-03-23','Dinakar(K)','Dinakar(K)','','0000-00-00','','F8003-S','Rev 0 dt 8-1-2009',0.00,'$','Closed','','yes','','','',NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL,NULL),