JASC 5753

Service difficulty reports · 31,521

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

Query with SQL
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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR SWAA042307Skin · debondedDURING SCHEDULED C2 CHECK, FOUND LT WING T/E AFT FLAP DISBONDED. REMOVED AND REPLACED T/E FLAP ASSY PER MM.Aug 9, 2004 · N353SW · Boeing 7373H4SDR 04FDEA02406Hinge · corrodedLEFT WING, INBOARD FLAP OUTBOARD AFT HINGE INBOARD PIVOT HOLE FLANGE CORRODED. CORROSION REMOVED PER CMM 57-52-03.Aug 9, 2004 · N578FE · Doug MD11SDR 04FDEA02405Hinge · corrodedLEFT WING, INBOARD FLAP OUTBOARD AFT HINGE INBOARD PIVOT HOLE CORRODED. CORROSION REMOVED AND FOUND EXCEEDED LIMITS PER CMM 57-52-03. CORROSION REMOVED AND FOUND EXCEEDED LIMITS PER CMM 57-52-03Aug 9, 2004 · N578FE · Doug MD11SDR 04FDEA02404Hinge · corrodedRT WING, INBOARD FLAP, OUTBOARD AFT HINGE OUTBOARD PIVOT HOLE FLANGE CORRODED. CORROSION REMOVED PER CMM 57-52-03. FOUND EXCEEDED LIMITS ORIGINAL THICKNESS = 0.562, MATERIAL REMOVED = 0.002, REMAINING THICKNESS = 0.560 COMPLIED WITH FEDEX EA 1-5750-76810, Aug 9, 2004 · N578FE · Doug MD11SDR 04FDEA02403Hinge · corrodedRT WING, INBOARD FLAP, OUTBOARD AFT HINGE OUTBOARD PIVOT HOLE CORRODED. CORROSION REMOVED PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL DIAMETER = 1.187 FINAL DIAMETER = 1.327 COMPLIED WITH FEDEX EA 1-5750-76810, WINGS - LT AND RT INBOARD TRAILING EDGE FLAP HINGE BRAug 9, 2004 · N578FE · Doug MD11SDR 04FDEA02402Hinge · corrodedRIGHT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE OUTBOARD ACTUATOR ROD END ATTACHING HOLE FLANGE CORRODED.Aug 9, 2004 · N578FE · Doug MD11SDR 04FDEA02401Hinge · corrodedRIGHT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE OUTBOARD ACTUATOR ROD END ATTACHING HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.Aug 9, 2004 · N578FE · Doug MD11SDR CA041108006Mount · loose(CAN) MOUNTING STUD NUTS ON FLAP MOTOR BACKED OFF TO THE POINT WHERE THE DRIVE COUPLING DISENGAGED BETWEEN THE FLAP MOTOR AND THE ACTUATOR.Aug 7, 2004 · Cessna 208SDR SWIA200413676Flap Track · wornAFTER TAKEOFF SELECTED FLAPS UP AND RECEIVED FLAP DISAGREEMENT. REMOVED AND REPLACED RT IB FLAP OB TRACK AND ALL ROLLERS ON RT IB FLAP IAW 27-50-02, OPERATIONAL CHECKS GOOD.Aug 7, 2004 · N582SW · Emb EMB120ERSDR SWAA042247Skin · delaminatedDURING SCHEDULED C4 CHECK, FOUND LEFT WING OUTBOARD T/E FORE FLAP DELAMINATED. REMOVED AND REPLACED LEFT OUTBOARD T/E FORE FLAP PER MM.Aug 6, 2004 · N360SW · Boeing 7373H4SDR 04FDEA02390Hinge · corrodedRT WING OUTBOARD FLAP INBOARD AFT HINGE WITH ACTUATOR ROD END ATTACHING HOLE OUTBOARD CORRODED. CORROSION REMOVED PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL THICKNESS = 0.395 MATERIAL REMOVED = 0.002 REMAINING THICKNESS = 0.393 COMPLIED WITH FEDEX EA 1-5750-7Aug 6, 2004 · N578FE · Doug MD11SDR 04FDEA02389Hinge · corrodedRT WING, OUTBOARD FLAP - INBOARD AFT HINGE WITH ACTUATOR ROD END ATTACHING HOLE INBOARD FLANGED CORRODED. CORROSION REMOVED PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL THICKNESS = 0.411 MATERIAL REMOVED = 0.005 REMAINING THICKNESS = 0.406 COMPLIED WITH FEDEX EA 1-Aug 6, 2004 · N578FE · Doug MD11SDR 04FDEA02388Hinge · corrodedRT WING OUTBOARD FLAP INBOARD AFT HINGE WITH ACTUATOR ROD END ATTACHING HOLE OUTBOARD CORRODED. CORROSION REMOVED PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL DIAMETER = 1.062 FINAL DIAMETER = 1.221 COMPLIED WITH FEDEX EA 1-5750-76807, WINGS - LT AND RT OUTBOARAug 6, 2004 · N578FE · Doug MD11SDR 04FDEA02387Hinge · corrodedRT WING, OUTBOARD FLAP - INBOARD AFT HINGE WITH ACTUATOR ROD END ATTACHING HOLE OUTBOARD CORRODED. CORROSION REMOVED PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL DIAMETER = 1.062 FINAL DIAMETER = 1.223 COMPLIED WITH FEDEX EA 1-5750-76807, WINGS - LT AND RT OUTBOARD Aug 6, 2004 · N578FE · Doug MD11SDR 04FDEA02386Hinge · corrodedRT WING OUTBOARD FLAP INBOARD AFT HINGE WITH PIVOT HOLE INBOARD FLANGE CORRODED. CORROSION REMOVED PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL THICKNESS = 0.497 MATERIAL REMOVED = 0.012 REMAINING THICKNESS = 0.485 COMPLIED WITH FEDEX EA 1-5750-76807, WINGS - LAug 6, 2004 · N578FE · Doug MD11SDR 04FDEA02385Hinge · corrodedRT WING OUTBOARD FLAP INBOARD AFT HINGE WITH PIVOT HOLE INBOARD CORRODED. CORROSION REMOVED PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL DIAMETER = 1.093 FINAL DIAMETER = 1.189 COMPLIED WITH FEDEX EA 1-5750-76807, WINGS - LT AND RT OUTBOARD FLAP - INBOARD HINGE BRAAug 6, 2004 · N578FE · Doug MD11SDR 04FDEA02384Hinge · corrodedRIGHT WING, OUTBOARD FLAP - INBOARD AFT HINGE WITH PIVOT HOLE OUTBOARD FLANGE CORRODED. CORROSION REMOVED PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL THICKNESS = 0.508 MATERIAL REMOVED = 0.002 REMAINING THICKNESS = 0.506 COMPLIED WITH FEDEX EA 1-5750-76807, WINGS Aug 6, 2004 · N578FE · Doug MD11SDR 04FDEA02383Hinge · corrodedRT WING, OB FLAP, IB AFT HINGE WITH PIVOT HOLE, OB CORRODED.**** S/D COMING ****Aug 6, 2004 · N578FE · Doug MD11SDR UPS04243001Skin · delaminatedINSPECTION TYPE: C, DELAM ON RT IB FORE FLAP UPPER SURFACE AT IB END. RT IB FLAP REPLACED REPLACED IAW MM27-51-01.Aug 5, 2004 · N945UP · Boeing 72722CSDR UPS04243000Skin · delaminatedINSPECTION TYPE:C LT IB AFT FLAP LWR SKIN DELAMINATION AT IB END AND BELOW NR 7 CARRIAGE. AFT FLAP REMOVED IAW MM 27-51-02. NEW AFT FLAP INSTALLED IAW MM 27-51-02.Aug 5, 2004 · N945UP · Boeing 72722CSDR 04FDEA02381Hinge Bracket · corrodedLT WING, OB FLAP, IB AFT HINGE WITH ACTUATOR ROD END ATTACHING OB HOLE CORRODED. CORROSION REMOVED PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL DIAMETER = 1.062. FINAL DIAMETER = 1.203. COMPLIED WITH FEDEX EA 1-5750-76807, LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINAug 5, 2004 · N578FE · Doug MD11SDR 04FDEA02380Hinge Bracket · corrodedLT WING, OB FLAP, IB AFT HINGE WITH ACTUATOR ROD END ATTACHING HOLE IB CORRODED. CORROSION REMOVED PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL THICKNESS = 0.412" MATERIAL REMOVED = 0.003. REMAINING THICKNESS = 0.409. COMPLIED WITH FEDEX EA 1-5750-76807, LEFT AND Aug 5, 2004 · N578FE · Doug MD11SDR 04FDEA02379Hinge Bracket · corrodedLT WING, OB FLAP, IB AFT HINGE WITH ACTUATOR ROD END ATTACHING T IB HOLE CORRODED. CORROSION REMOVED PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL DIAMETER = 1.062. FINAL DIAMETER = 1.199. COMPLIED WITH FEDEX EA 1-5750-76807, LEFT AND RIGHT OUTBOARD FLAP - INBOARD HIAug 5, 2004 · N578FE · Doug MD11SDR 04FDEA02378Hinge Bracket · corrodedLT WING, OB FLAP, IB AFT HINGE WITH PIVOT IB HOLE FLANGE CORRODED. CORROSION REMOVED PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL THICKNESS = 0.502. MATERIAL REMOVED = 0.015. REMAINING THICKNESS = 0.487. COMPLIED WITH FEDEX EA 1-5750-76807, LEFT AND RIGHT OUTBOARD FAug 5, 2004 · N578FE · Doug MD11SDR 04FDEA02377Hinge Bracket · corrodedLT WING, OB FLAP, IB AFT HINGE WITH PIVOT HOLE IB CORRODED. CORROSION REMOVED PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL DIAMETER = 1.093 FINAL DIAMETER = 1.148. COMPLIED WITH FEDEX EA 1-5750-76807, LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE Aug 5, 2004 · N578FE · Doug MD11SDR 04FDEA02375Hinge Bracket · corrodedLT WING, OB FLAP IB AFT HINGE OB PIVOT HOLE FOUND CORRODED. CORROSION REMOVED PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL DIAMETER = 1.062 FINAL DIAMETER = 1.095. COMPLIED WITH FEDEX EA 1-5750-76807, LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODAug 5, 2004 · N578FE · Doug MD11SDR 04FDEA02382Hinge · corrodedLT WING, OB FLAP, IB AFT HINGE WITH ACTUATOR ROD END ATTACHING HOLE OB HOLE CORRODED. *** S/D COMING ****Aug 5, 2004 · N578FE · Doug MD11SDR 04FDEA02369Hinge · corrodedLT WING, OB FLAP, OB AFT HINGE WITH IB PIVOT HOLE CORRODED**** S/D COMING ****Aug 5, 2004 · N578FE · Doug MD11SDR ASOA04637Guide · corrodedDURING A C-CHECK IN YUL, THE LEFT OUTBOARD FLAP NR 6 CAM GUIDE WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT OUTBOARD FLAP NR 6 CAM GUIDE IAW AMM 20-21-12. (M)Aug 4, 2004 · N530AS · Aerosp ATR72212SDR USAA040408Skin · debondedPIT - FOUND AFT FLAP DISBONDED 12 INCHES LONG BY 4 INCHES AREA, RIGHT OUTBOARD TRAILING EDGE OF AFT FLAP CENTER SECITON OF FLAP. REMOVED AND REPLACED PER MM 27-51-39. (M)Aug 4, 2004 · N780AU · Boeing 7374B7SDR P5CA0401158Fairing · delaminatedFIX FAIRING NR 4 FLAP HAS AREA OF DELAMINATION. REMOVED DAMAGED AREA & BONDED PER SRM 51-40-15.Aug 4, 2004 · N920FT · Boeing 747249FSDR SWIA200413678Flap Track · crackedDISCOVERED CRACK ON THE FLAP TRACK (NEXT TO ROLLER) IMMEDIATELY OB OF THE NR 1 ENGINE NACELLE. REPLACED LT OB FLAP IB ROLLER BRACKET WITH SERVICEABLE UNIT. OPERATIONAL CHECK GOOD.Aug 4, 2004 · N58733 · Emb EMB120ERSDR COMA0460439Skin · gougedRT IB FLAP LOWER SKIN GOUGE JUST AFT OF MAIN TIRE. IAW REO 601R-57-51-058.Aug 4, 2004 · N821CA · Cndair CL6002B19SDR ASOA04632Guide · corrodedDURING A C-CHECK IN YUL, THE RIGHT INBOARD FLAP NR 1 CAM GUIDE AT RIB 4 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT INBOARD FLAP NR 1 CAM GUIDE AT RIB 4 IAW AMM 20-21-12. (M)Aug 3, 2004 · N530AS · Aerosp ATR72212SDR ASOA04636Guide · corrodedDURING A C-CHECK IN YUL, THE RIGHT OUTBOARD FLAP NR 4 CAM GUIDE AT RIB 17 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT OUTBOARD FLAP NR 4 CAM GUIDE AT RIB 17 IAW AMM 20-21-12. (M)Aug 3, 2004 · N530AS · Aerosp ATR72212SDR ASOA04633Guide · corrodedDURING A C-CHECK IN YUL, THE RIGHT INBOARD FLAP NR 2 CAM GUIDE AT RIB 5, AND THE RIGHT INBOARD FLAP NR 3 CAM GUIDE AT RIB 6 WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT INBOARD FLAP NR 2 CAM GUIDE AT RIB 5, AND THE RIGHTAug 3, 2004 · N530AS · Aerosp ATR72212SDR ASOA04634Guide · corrodedDURING A C-CHECK IN YUL, THE RIGHT OUTBOARD FLAP NR 2 CAM GUIDE AT RIB 15 WAS FOUND TO BE CORRODED LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT OUTBOARD FLAP NR 2 CAM GUIDE AT RIB 15 IAW AMM 20-21-12. (M)Aug 3, 2004 · N530AS · Aerosp ATR72212SDR ASOA04635Guide · corrodedDURING A C-CHECK IN YUL, THE RIGHT OUTBOARD FLAP NR 3 CAM GUIDE AT RIB 16 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT OUTBOARD FLAP NR 3 CAM GUIDE AT RIB 16 IAW AMM 20-21-12. (M)Aug 3, 2004 · N530AS · Aerosp ATR72212SDR SWAA042215Skin · delaminatedDURING SCHEDULED C2 CHECK, FOUND LEFT WING INBOARD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED INBOARD AFT T/E FLAP PER MM.Aug 3, 2004 · N637SW · Boeing 7373H4SDR ASOA04629Guide · corrodedDURING A CHECK IN YUL, THE NR 2 CAM GUIDE OUTBOARD ON THE LEFT OUTBOARD FLAP WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE NR 2 CAM GUIDE OUTBOARD ON THE LEFT OUTBOARD FLAP IAW AMM 20-21-12. (M)Aug 2, 2004 · N530AS · Aerosp ATR72212SDR ASOA04628Guide · corrodedDURING A C-CHECK IN YUL, THE NR 3 AND 4 CAM GUIDES OUTBOARD ON THE LEFT INBOARD FLAPS WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE NR 3/4 CAM GUIDES OUTBOARD ON THE LEFT INBOARD FLAP IAW AMM 20-21-12. (M)Aug 2, 2004 · N530AS · Aerosp ATR72212SDR ASOA04630Guide · corrodedDURING A C-CHECK IN YUL, THE NR 5 AND 6 CAM GUIDES OUTBOARD ON THE LEFT INBOARD FLAP AS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE NR 5 AND 6 CAM GUIDES OUTBOARD ON THE LEFT INBOARD FLAP IAW AMM 20-21-12. (M)Aug 2, 2004 · N530AS · Aerosp ATR72212SDR P5CA0401162Fairing · delaminatedDELAMINATION ON SEVERAL AREA OF NR 3 FLAP TRACK, AFT FAIRING RT WING. REMOVED DAMAGE AREA & REBONDED PER SRM 51-40-15.Aug 2, 2004 · N920FT · Boeing 747249FSDR 04FDEA02354Fitting · corrodedLT WING, OB FLAP OB HINGE FORWARD FITTING AFT. IB HOLE FOUND CORRODED. CORROSION REMOVED PER SRM 51-21-01 VOLUME II. ORIGINAL DIAMETER = 0.442, FINAL DIAMETER = 0.502 COMPLIED WITH FEDEX EA 1-5750-80364, WINGS - TRAILING EDGE FLAPS - LEFT OUTBOARD FLAP - HIAug 2, 2004 · N578FE · Doug MD11FSDR 04FDEA02353Fitting · corrodedLT WING, OB FLAP OB HINGE FORWARD FITTING MIDDLE. OB HOLE FOUND CORRODED. CORROSION REMOVED PER SRM 51-21-01 VOLUME II. ORIGINAL DIAMETER = 0.457, FINAL DIAMETER = 0.517 COMPLIED WITH FEDEX EA 1-5750-80364, WINGS - TRAILING EDGE FLAPS - LEFT OUTBOARD FLAP -Aug 2, 2004 · N578FE · Doug MD11FSDR 04FDEA02352Fitting · corrodedLT WING, OB FLAP OB HINGE FORWARD FITTING. FORWARD IB HOLE FOUND CORRODED. CORROSION REMOVED PER SRM 51-21-01 VOLUME II. ORIGINAL DIAMETER = 0.442, FINAL DIAMETER = 0.502. COMPLIED WITH FEDEX EA 1-5750-80364, WINGS - TRAILING EDGE FLAPS - LEFT OUTBOARD FLAP Aug 2, 2004 · N578FE · Doug MD11FSDR 04FDEA02351Hinge · corrodedLT WING, OB FLAP IB HINGE FORWARD FITTING FORWARD. IB HOLE FOUND CORRODED. CORROSION REMOVED PER SRM 51-21-01 VOLUME II. ORIGINAL DIAMETER = 0.567, FINAL DIAMETER = 0.627. COMPLIED WITH FEDEX EA 1-5750-80364, WINGS - TRAILING EDGE FLAPS - LEFT OUTBOARD FLAP Aug 2, 2004 · N578FE · Doug MD11SDR 04FDEA02334Bracket · corrodedRT WING, IB FLAP OB HINGE (FLAPSIDE) PIVOT HOLE NR 1 IB BORE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEEDED LIMITS AS PER CMM 57-52-03.Aug 1, 2004 · N607FE · Doug MD11SDR 04FDEA02333Bracket · corrodedRT WING, IB FLAP OB HINGE (FLAPSIDE) PIVOT HOLE NR 1 OB BORE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEEDED LIMITS AS PER CMM 57-52-03.Aug 1, 2004 · N607FE · Doug MD11SDR USAA040410Skin · gougedPIT - FOUND LEFT OUTBOARD FOREFLAP GOUGED, .3125 INCH WIDE BY .15 INCHE DEEP BY 2.5 INCH LONG, 30 INCHES FROM OUTBOARD END OF TOP SKIN, LEFT OUTBOARD FOREFLAP. DEFECTIVE PART REPLACED WITH IDENT PART NR PER MM 27-51-37-4. (M)Jul 31, 2004 · N340US · Boeing 737301
Back to JASC 5753