JASC 5753

Service difficulty reports · 31,521

Reports filed under 5753 · Trailing Edge Flaps, newest first.

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duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE jasc_code = '5753'
  ORDER BY difficulty_date DESC"

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SDR 04FDEA01298Hinge · corrodedLT WING O/B FLAP O/B HINGE (FLAP SIDE), I/B ACTUATOR ATTACHMENT BORE FOUND CORRODED. I/B ACTUATOR ATTACHMENT BORE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4 FIG 1. ORIGINAL DIAMETER: 1.063, FINAL DIAMETER: 1.190. REPAIRED AS PER EA 1-5750-76671, LT OMay 18, 2004 · N609FE · Doug MD11SDR 04FDEA01297Hinge · corrodedLT WING O/B FLAP O/B HINGE (FLAP SIDE), O/B ACTUATOR ATTACHMENT BORE FOUND CORRODED. O/B ACTUATOR ATTACHMENT BORE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4 FIG 1. ORIGINAL DIAMETER: 1.063, FINAL DIAMETER: 1.190. REPAIRED AS PER EA 1-5750-76671. LT May 18, 2004 · N609FE · Doug MD11SDR 04FDEA01296Support · corrodedARC1496 FLAP VANE SUPPORT CORROSION REWORK IAW EA 8-5750-77409. COMPLIED WITH EA 8-5750-77409 WINGS ARC1496 FLAP VANE SUPPORT CORROSION REWORK AT MAE.May 18, 2004 · N68056 · Doug DC1010SDR 04FDEA01295Hinge · corrodedLT WING O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN I/B ATTACHMENT SPOTFACE FOUND CORRODED. PIVOT PIN I/B ATTACHMENT SPOTFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4 FIG 1. ORIGINAL THICKNESS OF LUG: 0.494, MATERIAL REMOVED: 0.004, REMAINING THICKNESMay 18, 2004 · N609FE · Doug MD11SDR 04FDEA01294Hinge · corrodedLT WING O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN O/B ATTACHMENT SPOTFACE FOUND CORRODED. PIVOT PIN O/B ATTACHMENT SPOTFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4 FIG 1. ORIGINAL THICKNESS OF LUG: 0.503, MATERIAL REMOVED: 0.002, REMAINING THICKNESMay 18, 2004 · N609FE · Doug MD11SDR 04FDEA01293Hinge · corrodedLT WING O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN O/B ATTACHMENT BORE FOUND CORRODED. PIVOT PIN O/B ATTACHMENT BORE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4 FIG 1. ORIGINAL DIAMETER: 1.063, FINAL DIAMETER: 1.095. REPAIRED AS PER EA 1-5750-76670. LTMay 18, 2004 · N609FE · Doug MD11SDR 04FDEA01292Hinge · corrodedLEFT WING O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN I/B ATTACHMENT BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4 FIG 1. ORIGINAL DIAMETER: 1.093, FINAL DIAMETER: 1.125. REPAIRED AS PER EA 1-5750-76670. LT O/B FLAP - I/B FLAP SIDE HMay 18, 2004 · N609FE · Doug MD11SDR 04FDEA01291Hinge · corrodedLT WING O/B FLAP I/B HINGE (FLAP SIDE), O/B ACTUATOR ATTACHMENT BORE FOUND CORRODED. O/B ACTUATOR ATTACHMENT BORE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4 FIG 1. ORIGINAL DIAMETER: 1.063, FINAL DIAMETER: 1.1895. REPAIRED AS PER EA 1-5750-76670. LT May 18, 2004 · N609FE · Doug MD11SDR DL764040449Bushing · wornWHEN FLAPS DOWN LINKAGE ON THE RIGHT OUTBOARD FLAP INBOARD TRACK WAS FOUND LOOSE. SEVERAL WORN AND FLAT BUSHINGS ON THE CARRIAGE ASSY. REPAIRED OR REPLACED DAMAGED PARTS.May 18, 2004 · N832MH · Boeing 767432ERSDR 04FDEA01290Hinge · corrodedLT WING O/B FLAP I/B HINGE (FLAP SIDE), I/B ACTUATOR ATTACHMENT BORE FOUND CORRODED. LT WING O/B FLAP I/B HINGE (FLAP SIDE), I/B ACTUATOR ATTACHMENT BORE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4 FIG 1. ORIGINAL DIAMETER: 1.063, FINAL DIAMETER: 1.1May 18, 2004 · N609FE · Doug MD11SDR 04FDEA01289Hinge · corrodedLEFT WING O/B FLAP I/B HINGE (FLAP SIDE), O/B ACTUATOR ATTACHMENT SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4 FIG 1. ORIGINAL LUG THICKNESS: 0.403, MATERIAL REMOVED: 0.005, REMAINING THICKNESS OF LUG: 0.398 REWORKED AREA REPAIRMay 18, 2004 · N609FE · Doug MD11SDR 04FDEA01288Hinge · corrodedLT WING O/B FLAP I/B HINGE (FLAP SIDE), I/B ACTUATOR ATTACHMENT SPOTFACE FOUND CORRODED. SPOTFACED, CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4 FIG 1. ORIGINAL THICKNESS OF LUG: 0.405, MATERIAL REMOVED: 0.002, REMAINING THICKNESS OF LUG: 0.403. REWORMay 18, 2004 · N609FE · Doug MD11SDR UNI2004F00000Flap Track · corrodedUPON PERFORMANCE OF INSPECTION OPERATION MD OF MFG MM, SEVERE EXFOLIATION, CORROSION WAS FOUND ON BOTH OB FLAP TRACKS. AREAS ON FLAP TRACK WHERE CORROSION WAS DISCOVERED INCLUDE: AFT RECESSED WEB AREA AND ADJACENT UPPER AND LOWER PORTIONS OF TRACK. CONTRIBUMay 17, 2004 · N127HA · Cessna 208BSDR ASAA0480428Wedge · gougedDURING HV CHECK, FOUND RIG WING INBOARD FLAP, INBOARD WEDGE LOWER SURFACE IS GOUGED. REMOVED DAMAGE AND INSTALLED REPAIR DOUBLER IAW 57-03. (M)May 17, 2004 · N979AS · Doug MD83SDR 04FDEA01282Stop Fitting · crackedRIGHT WING - OUTBOARD FLAP STOP FITTING FOUND CRACKED. RIGHT WING - OUTBOARD FLAP STOP FITTING REMOVED AND REPLACED AS PER SRM 51-31-01 VOL 2 AND SRM 51-35-01 VOL 2.May 17, 2004 · N609FE · Doug MD11SDR 04FDEA01281Stop Fitting · crackedLEFT WING - OUTBOARD FLAP STOP FITTING FOUND CRACKED. LEFT WING - OUTBOARD FLAP STOP FITTING REMOVED AND REPLACED AS PER SRM 51-31-01 VOL 2 AND SRM 51-35-01 VOL 2.May 17, 2004 · N609FE · Doug MD11SDR SWAA041405Flap · delaminatedDURING SCHEDULED PM CHECK, FOUND RIGHT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED RIGHT T/E AFT FLAP PER MM.May 17, 2004 · N629SW · Boeing 7373H4SDR SWAA041395Flap · delaminatedLEFT WING INBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED T/E AFT FLAP PER MM.May 16, 2004 · N328SW · Boeing 7373H4SDR 04FDEA01278Hinge · corrodedC/W EA8-5740-77406, RIGHT INBOARD FLAP, AFT HINGE ASSY ARC 2512, PIVOT BORE CORROSION. COMPLIED WITH EA 8-5740-77406 RIGHT INBOARD FLAP, AFT HINGE ASSY, PIVOT BORE CORROSION CW PT1 ONLY.May 16, 2004 · N68051 · Doug DC1010SDR DL76G040441Fitting · corrodedDURING PSV IN ATLANTA, FOUND HOLES CORRODED WHILE ACCOMPLISHING ME 02 OF EA 01-085672-12 AD, REV C. REPAIRED PER ERA 089397-14MA REVISION A, REPAIR NR 4.May 16, 2004 · N152DL · Boeing 7673P6SDR 04FDEA01271Fitting · corrodedLEFT O/B FLAP NR 3 VANE FITTING FWD BOLT HOLE HAS CORROSION. AFT BOLT HOLE BUSHING IS CORRODED AND FITTING HAS NUMEROUS AREAS OF CORROSION. RECEIVED NEW NR 3 VANE FITTING TO BE INSTALLED ON WORK CARD E8-5750-7- 5000 PT 3 AT MAE.May 15, 2004 · N68056 · Doug DC1010SDR DL76G040440Fitting · corrodedDURING PSV IN ATLANTA, FOUND A HOLE CORRODED WHILE ACCOMPLISHING ME 02 OF EA 01-085672-12 AD, REV C. REPAIRED PER ERA 089397-14MA REVISION A, REPAIR NR 1.May 15, 2004 · N152DL · Boeing 7673P6SDR GTIA040624Vane · corrodedFOUND INBOARD FLAP VANE OF OUTBOARD FLAP HAS CORROSION AND MISSING SCREW. REMOVED DAMAGED AREA. SKIN ALTERNATE ID 2024T81 SUBSTITUATION FOR 2075T6- .016 HOT BONDED REPAIR. (M)May 14, 2004 · N802NK · Doug DC983SDR 04FDEA01268Hinge · corrodedCOMPLY WITH EA 8-5740-77404 WINGS - LEFT INBOARD FLAP - AFT HINGE ASSY ARC2512 PIVOT BORE CORROSION. COMPLIED WITH EA 8-5740-77404 WINGS - LEFT INBOARD FLAP AFT HINGE ASSY ARC 2512 PIVOT BORE CORROSION AT MAE.May 14, 2004 · N68056 · Doug DC1010SDR AUS20040484Flap Track · fod(AUS) PASSENGER REPORTED RAG SEEN IN WING TRAILING EDGE. INVESTIGATION FOUND RAG LOCATED ON AREA OF LT WING REAR SPAR ABOVE NR 3 FLAP TRACK. THE RAG WAS NOT INTERFERING WITH ANY AIRCRAFT SYSTEM. FOD PERSONNEL/MAINTENANCE ERROR.May 13, 2004 · Boeing 737*SDR IXXA0400086SSkin · wornDURING A ROUTINE C CHECK INSPECTION, FOUND RT OUTBD FLAP UPPER SKIN HAS INTERIM REPAIR AT STA XF 282.000. REPAIRS WERE ACCOMPLISHED BY PERFORMING MAJOR REPAIRS IAW DC8 SRM 51-1-0 PG 1 DC8 SRM 57-7-1 PG 2 FIG 4. REMOVED RT OUTBD FLAP FWD UPPER PLATING WITH IMay 13, 2004 · N830BX · Doug DC871FSDR 04FDEA01250Flap Track · wornLEFT INBOARD FLAP VANE NR 2 TRACK HAS DEEP WEAR MARKS ON LOWER & UPPER SURFACE. REPLACED NR 2 LEFT I/B TRACK TO BE INSTALLED ON EO 8-5750-7-5002 AT MAE.May 13, 2004 · N68056 · Doug DC1010SDR A6WA200460015Flap Track · wornNR 2 FLAP TRACK, WEAR FOUND ON NR 2 LT LOWER ROLLER THAT MEASURES .033 INCHES DEEP. REQUESTED REPAIR FROM BAE SYSTEMS REF AVMAX FAX 607-1907002. MAINTENANCE REMOVED LOWER CARRIAGE NR 2 LEFT. ROLLERS REPLACED IAW CMM 57-50-22. CARRIAGE REINSTALLED IAW AMM 2May 12, 2004 · N607AW · Bag BAE146200ASDR AWXA200400537Skin · delaminatedMCN - MAJOR REPAIR - DURING C-03 CHECK FOUND THE RT INBOARD FLAP DELAMINATED AT THE LOWER INBOARD SURFACE, 7 INCHES OUTBOARD OF RIB 1, WS 700 RIGHT. MAINTENANCE CUT OUT DELAMINATED AREA OF RT INBOARD FLAP LOWER SKIN AT RIB 1, WS 700 RT; FABRICATED A CORE FILLMay 12, 2004 · N636AW · Airbus A320231SDR DL73S040430Skin · delaminatedNR 2 AFT FLAP AFT SKIN SEPARATED/DELAMINATED AT IB END. REPAIRED IAW SRM 51-40-20 FIG 10.May 12, 2004 · N305DL · Boeing 737232SDR 04FDEA01247Carriage · corrodedRIGHT O/B FLAP BOTH I/B AND O/B CARRIAGES HAVE CORROSION IN ROLLER MOUNT HOLES. REPLACED I/B AND O/B ROLLER CARRIAGES TO BE INSTALLED ON EO 8-5750-7-5000 AT MAE.May 12, 2004 · N68051 · Doug DC1010SDR 04FDEA01230Flap Track · wornRIGHT O/B FLAP NR 3 VANE TRACK TOP PLATING IS WORN. REPLACED TRACK TO BE INSTALLED ON W/C E 8-5750-7-5000 AT MAE.May 12, 2004 · N68056 · Doug DC1010SDR 04FDEA01229Flap Track · wornLEFT WING O/B FLAP NR 3 TRACK TOP COATING IS WORN. REPLACED TRACK TO BE INSTALLED ON W/C 8-5750-7-5000 PT 3 AT MAE.May 12, 2004 · N68056 · Doug DC1010SDR 04FDEA01228Flap Track · gougedLEFT WING O/B FLAP NR 4 TRACK HAS GOUGE. REPLACED TRACK TO BE INSTALLED ON W/C 8-5750-7-5000 PT 3 AT MAE.May 12, 2004 · N68056 · Doug DC1010SDR 04FDEA01227Flap Track · gougedRIGHT O/B FLAP NR 1 VANE TRACK HAS GOUGE. REPLACED TRACK TO BE INSTALLED ON W/C E 8-5750-7-5000 PT 4 TA MAE.May 12, 2004 · N68056 · Doug DC1010SDR 04FDEA01226Flap Track · wornRIGHT O/B FLAP NR 2 VANE TRACK TOP PLATING IS WORN. REPLACED TRACK TO BE INSTALLED ON W/C E 8-5750-7-5000 PT 4 AT MAE.May 12, 2004 · N68056 · Doug DC1010SDR 04FDEA01225Flap Track · gougedRIGHT O/B FLAP NR 4 TRACK HAS GOUGE. REPLACED TRACK TO BE INSTALLED ON W/C E 8-5750-7-5000 PT 4 AT MAE.May 12, 2004 · N68056 · Doug DC1010SDR 04FDEA01224Flap Track · gougedLEFT WING O/B FLAP NR 2 TRACK HAS GOUGE. REMOVED AND REPLACED TRACK TO BE INSTALLED ON W/C 8-5750-7-5000 PT 3 AT MAE.May 12, 2004 · N68056 · Doug DC1010SDR 04FDEA01223Stop Fitting · wornRIGHT INBOARD FLAP STOP PAD FITTING FWD OF O/B HINGE FASTENER HOLES ELONGATED AND WORN. REPLACED ANTI FRICTION UPSTOP PAD IAW MM 20-50-02-2 AT MAE.May 12, 2004 · N68056 · Doug DC1010SDR DHL2004754006Structure · delaminatedDURING A C-CHECK, THE FOLLOWING DISCREPANCIES WERE NOTED; RT WING OUTBD AFT FLAP SHOW SPOTS 2 EA OF DISBOND OF WBL 279 & WBL 395. T/E UPPER SIDE. CUT OUT DELAMINATED AREAS AT RT OUTBD AFT FLAP APPROX 1.25 X 10 INCH AND 1.5 X 1.5 INCH. APPLIED ADHESIVE PRIMERMay 11, 2004 · N754DH · Boeing 727223SDR SWAA041345Skin · delaminatedDURING SCHEDULED 1/4D CHECK, FOUND RT WING INBOARD FORE FLAP DELAMINATED. REPAIRED RT WING INBOARD FORE FLAP PER SRM.May 11, 2004 · N693SW · Boeing 737317SDR SWAA041344Skin · delaminatedDURING SCHEDULED 1/4D CHECK, FOUND RT WING INBOARD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED INBOARD AFT FLAP PER MM.May 11, 2004 · N693SW · Boeing 737317SDR 04FDEA01220Spindle · corrodedRIGHT O/B FLAP I/B ROLLER SPINDLE WORN AND HAS CORROSION. REMOVED AND REPLACED SPINDLE IAW W/C E 8-5750-7-5000 AT MAE.May 11, 2004 · N68051 · Doug DC1010SDR 04FDEA01189Hinge Bracket · corrodedRIGHT AFT (FLAP SIDE) O/B FLAP O/B HINGE - O/B ACTUATOR LUG HOLE CORRODED. RIGHT AFT (FLAP SIDE) O/B FLAP O/B HINGE - O/B ACTUATOR LUG HOLE CORROSION REMOVED AS PER SRM 51-21-01 VOL 2. ORIG DIA 1.062 INCH, FINAL DIA 1.189 INCH AND REPAIRED AS PER FEDEX EA May 10, 2004 · N597FE · Doug MD11SDR 04FDEA01202Hinge · corrodedRIGHT AFT (FLAP SIDE) O/B FLAP I/B HINGE, O/B PIVOT BORE SPOTFACE FOUND CORRODED. RT AFT (FLAP SIDE) O/B FLAP I/B HINGE, O/B PIVOT BORE SPOTFACE CORROSION REMOVED AS PER SRM 51-21-01 VOL. II. ORIGINAL THICKNESS: 0.503 MATERIAL REMOVED: 0.002 REMAINING THICKMay 10, 2004 · N597FE · Doug MD11SDR 04FDEA01201Hinge · corrodedRT AFT (FLAP SIDE) O/B FLAP I/B HINGE, O/B PIVOT BORE HOLE FOUND CORRODED. RT AFT (FLAP SIDE) O/B FLAP I/B HINGE, O/B PIVOT BORE HOLE CORROSION REMOVED AS PER SRM 51-21-01 VOL II. ORIG DIA 1.062, FINAL DIA 1.094. REPAIRED AS PER EA 1-5750-75954, LT AND RT OMay 10, 2004 · N597FE · Doug MD11SDR 04FDEA01200Hinge · corrodedRIGHT AFT (FLAP SIDE) O/B FLAP I/B HINGE, I/B PIVOT BORE SPOTFACE FOUND CORRODED. RT AFT (FLAP SIDE) O/B FLAP I/B HINGE, I/B PIVOT BORE SPOTFACE CORROSION REMOVED AS PER SRM 51-21-01 VOL. II. ORIGINAL THICKNESS: 0.487 MATERIAL REMOVED: 0.003 REMAINING THICKNEMay 10, 2004 · N597FE · Doug MD11SDR 04FDEA01199Hinge · corrodedRT AFT (FLAP SIDE) O/B FLAP I/B HINGE, I/B PIVOT BORE HOLE FOUND CORRODED. RT AFT (FLAP SIDE) O/B FLAP I/B HINGE, I/B PIVOT BORE HOLE CORROSION REMOVED AS PER SRM 51-21-01 VOL. II. ORIGINAL DIAMETER: 1.093 FINAL DIAMETER: 1.126 AND REPAIRED AS PER FEDEX EMay 10, 2004 · N597FE · Doug MD11SDR 04FDEA01198Hinge · corrodedRIGHT AFT (FLAP SIDE) O/B FLAP I/B HINGE, O/B ACTUATOR LUG SPOTFACE FOUND CORRODED. RT AFT (FLAP SIDE) O/B FLAP I/B HINGE, O/B ACTUATOR LUG SPOTFACE CORROSION REMOVED AS PER SRM 51-21-01 VOL. II. ORIGINAL THICKNESS: 0.410 MATERIAL REMOVED: 0.004 REMAININGMay 10, 2004 · N597FE · Doug MD11SDR 04FDEA01197Hinge · corrodedRIGHT AFT (FLAP SIDE) O/B FLAP I/B HINGE, O/B ACTUATOR LUG HOLE FOUND CORRODED. RT AFT (FLAP SIDE) O/B FLAP I/B HINGE, O/B ACTUATOR LUG HOLE CORROSION REMOVED AS PER SRM 51-21-01 VOL. II. ORIGINAL DIAMETER: 1.062 FINAL DIAMETER: 1.189 AND REPAIRED AS PER FEDEMay 10, 2004 · N597FE · Doug MD11
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