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 04FDEA02114Hinge · corrodedRT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT HOLE INBOARD LUG SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL THICKNESS=0.506, MATERIAL REMOVED=0.005, REMAINING THICKNESS=0.501 AND REPAIRED AS PER FEDEX EA NR 1-5Jul 19, 2004 · N613FE · Doug MD11SDR 04FDEA02113Hinge · corrodedRT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT HOLE OUTBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL DIAMETER = 1.062, FINAL DIAMETER = 1.193 AND REPAIRED AS PER EA NR 1-5750-77941. TITLE: WINGS - TRAILING EDJul 19, 2004 · N613FE · Doug MD11SDR 04FDEA02112Hinge · corrodedRT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT HOLE OUTBOARD LUG SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL THICKNESS=0.506, MATERIAL REMOVED=0.004, REMAINING THICKNESS=0.502 AND REPAIRED AS PER FEDEX EA NR 1-5Jul 19, 2004 · N613FE · Doug MD11SDR 04FDEA02111Hinge · corrodedRT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT HOLE INBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL DIA.=1.062, FINAL DIAMETER = 1.218 AND REPAIRED AS PER EA NR 1-5750-77943. TRAILING EDGE DEVICES -Jul 19, 2004 · N613FE · Doug MD11SDR 04FDEA02110Hinge · corrodedRT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT INBOARD LUG SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.Jul 19, 2004 · N613FE · Doug MD11SDR 04FDEA02109Hinge · corrodedRT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT HOLE OUTBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL DIAMETER = 1.062, FINAL DIAMETER = 1.222 AND REPAIRED AS PER EA NR 1-5750-77943. TITLE: WINGS - TJul 19, 2004 · N613FE · Doug MD11SDR 04FDEA02108Hinge · corrodedRT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT OUTBOARD LUG SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL THICKNESS=0.400, MATERIAL REMOVED=0.005, REMAINING THICKNESS=0.395 AND REPAIRED AS PER EA NR 1Jul 19, 2004 · N613FE · Doug MD11SDR 04FDEA02107Hinge · corrodedRT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), PIVOT HOLE INBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4 ORIGINAL DIAMETER = 1.093, FINAL DIAMETER = 1.096 AND REPAIRED AS PER EA NR 1-5750-77943. TITLE: WINGS - TRAILING EDGE ANDJul 19, 2004 · N613FE · Doug MD11SDR 04FDEA02106Hinge · corrodedRT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), PIVOT HOLE INBOARD LUG SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL THICKNESS=0.507, MATERIAL REMOVED=0.006, REMAINING THICKNESS=0.501, AND REPAIRED AS PER FEDEX EA NR 1-575Jul 19, 2004 · N613FE · Doug MD11SDR SWAA042025Skin · crackedRIGHT WING OUTBOARD T/E FLAP CRACKED. REPAIRED RIGHT OUTBOARD T/E FLAP PER EA.Jul 18, 2004 · N721WN · Boeing 7372T4SDR SWAA042030Skin · delaminatedDURING SCHEDULED PM CHECK, FOUND RT WING OUTBOARD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED RIGHT OUTBOARD AFT T/E FLAP PER MM.Jul 18, 2004 · N624SW · Boeing 7373H4SDR 04FDEA02105Hinge · corrodedRT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), PIVOT HOLE OUTBOARD LUG SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL THICKNESS=0.511, MATERIAL REMOVED=0.003, REMAINING THICKNESS=0.508 AND REPAIRED AS PER EA 1-5750-77943. Jul 18, 2004 · N613FE · Doug MD11SDR 04FDEA02104Hinge · corrodedRIGHT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), PIVOT HOLE OUTBOARD BORE FOUND CORRODED.Jul 18, 2004 · N613FE · Doug MD11SDR A6WA200440106Vane · chafedRIGHT INBOARD FLAP VANE AT FLAP STATION 60.005 IS CHAFED .012 INCH DEEP. PERFORMED A MAJOR REPAIR TO RIGHT INBOARD FLAP VANE BY REMOVING INBOARD END LEADING EDGE SKIN AND INSTALLING NEW LEADING EDGE SKIN, P/N 601R14303-54 IAW CRJ SRM 51-42-13. (M)Jul 17, 2004 · N429AW · Cndair CL6002B19SDR DHL2004745533Skin · puncturedDURING A C-CHECK, RT WING INBD FOREFLAP L/E WS 224 HAS A PUNCTURE AND AT WS 335 L/E HAS ONE (1) DENT. REFER TO NR 96459 FOR DENT REPAIR. CUT OUT DAMAGED AREA AND FABBED FROM 2024 T3 .050 PO 9001189 DIM 4 X 4 INCH AND 2 EA DOUBLERS FROM 2024 T3 .063 PO 900790Jul 17, 2004 · N745DH · Boeing 727224SDR 04FDEA02102Support · corrodedCOMPLY WITH EA 8-5750-80574 WINGS FLAP VANE SUPPORT CORROSION REWORK, RIGHT OUTBOARD FLAP. COMPLIED WITH EA 8-5750-80574 WINGS FLAP VANE SUPPORT CORROSION REWORK ON RIGHT O/B FLAP.Jul 17, 2004 · N359FE · Doug MD1010FSDR SWAA042020Skin · delaminatedDURING SCHEDULED A1 CHECK, FOUND LT WING OUTBOARD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED LT OUTBOARD AFT T/E FLAP PER MM.Jul 17, 2004 · N506SW · Boeing 7375H4SDR ASOA04555Guide · corrodedDURNG A C-CHECK IN YUL, THE RIGHT OUTBOARD FLAP CAM GUIDE NR 4 FROM INBOARD WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT OUTBOARD FLAP CAM GUIDE NR 4. (M)Jul 16, 2004 · N533AS · Aerosp ATR72212SDR ASOA04554Guide · corrodedDURING A C-CHECK IN YUL, THE RIGHT INBOARD FLAP CAM GUIDE NR 1 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT INBOARD FLAP CAM GUIDE NR 1 IAW AMM 20-21-12. (M)Jul 15, 2004 · N533AS · Aerosp ATR72212SDR SWAA042004Skin · delaminatedDURING SCHEDULED 1/4D CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP INBOARD END, DELAMINATED. REMOVED AND REPLACED LT OUTBOARD T/E AFT FLAP PER MM.Jul 15, 2004 · N643SW · Boeing 7373H4SDR HNAA0400067Skin · gougedDURING 20,000 HOUR INSPECTION RIGHT OUTBOARD FLAP - UPPER INBOARD SURFACE CHAFED AND GOUGED. REPAIRED PER EO 8-57-04-0476 AS A MAJOR REPAIR. DUE TO PRIOR BLENDING REPAIRS AND INABILITY TO DETERMINE REMAINING THICKNESS OF SKIN, THIS EO TRIMS OUT DAMAGE AND INJul 15, 2004 · N906HA · Dhav DHC8102SDR IXXA060133SAngle · gougedDURING ROUTINE C CHECK, FOUND RIGHT WING JOINT AREA BETWEEN INBOARD AND OUTBOARD FLAPS, AREA ON UPPER OUTBOARD FLAP ANGLE GOUGED. REMOVED DAMAGE. FABRICATED REPAIR PART. LOCATED, DRILLED TRIMMED, DEBURRED, TREATED, PRIMED, INSTALLED REPAIR PART AND NEW FASJul 14, 2004 · N605AL · Doug DC873FSDR ASOA04551Rib · crackedDURING A C-CHECK IN YUL, THE RIGHT INBOARD FLAP LEADING EDGE PICKUP RIB NR 7 FOR THE CAM GUIDE WAS FOUND TO BE CRAKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT INBOARD FLAP LEADING EDGE PICKUP RIB NR 7 FOR THE CAM GUIDE IAW SRM 51-25-03 AND 51Jul 14, 2004 · N533AS · Aerosp ATR72212SDR ASOA04552Rib · crackedDURING A C-CHECK IN YUL, THE RIGHT INBOARD FLAP LEADING EDGE PICKUP RIB NR 6 FOR THE CAM GUIDE NR 4 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND EPLACED THE RIGHT INBOARD FLAP LEADING EDGE PICKUP RIB NR 6 FOR THE CAM GUIDE NR 4 IAW SRM 51-25Jul 14, 2004 · N533AS · Aerosp ATR72212SDR UPS04242851Fairing · crackedINSPECTION TYPE: C, 7 FLAP TRACK SAILBOAT FAIRING HAS SUSPECT CRACK TO OUTER SKIN AT RIB ATTACH POINT (INDICATED ON SKIN). HFEC CONFIRMED CRACK AND MARKED END. REPAIR CARRIED OUT IAW SRM 51-40-02 FIG 1.Jul 13, 2004 · N947UP · Boeing 72725CSDR 04FDEA02070Vane · gougedCOMPLY WITH EA 8-5710-79550 WINGS REWORK OF GOUGE IN OUTBD FLAP VANE SUPPORT RIB ARB1860-3. COMPLIED WITH EA 8-5710-79550 WINGS REWORK OF GOUGE IN OUTBD FLAP VANE SUPPORT RIB ARB 1860-3 AT MAE.Jul 13, 2004 · N326FE · Doug DC1030SDR HNAA0400066Fitting · crackedOUTBOARD FLAP NR 3 FLAP TRACK ROLLER FITTING (AFT) IS BROKEN/CRACKED. UPPER ROLLER BROKEN OFF. REMOVED AND REPLACED FLAP TRACK ROLLER ASSEMBLY.Jul 13, 2004 · N906HA · Dhav DHC8102SDR UPS04242840Skin · debondedINSPECTION TYPE: C, LEFT I/B FOREFLAP I/B END & UPPER SURFACE HAS DISBOND. REPAIRED IAW SRM 51-40-20. DURING OPS CHECKS THE O/B END WAS CONTACTING THE MIDFLAP AND BINDING. FOREFLAP RESKIMMED BUT DID NOT SOLVE PROBLEM. INSTALLED FOREFLAP REMOVED FROM A/C N9Jul 12, 2004 · N947UP · Boeing 72725CSDR 04FDEA02055Hinge · corrodedRIGHT OUTBOARD FLAP, OUTBOARD HINGE (FLAP SIDE) AFT MOUNTING AREA FORWARD HOLE FOUND CORRODED. CORROSION REMOVED PER SRM 51-21-01 VOLUME II. ORIGINAL DIAMETER = 0.521, FINAL DIAMETER = 0.610. COMPLIED WITH FEDEX EA 1-5750-76755, WINGS - RIGHT OUTBOARD FLAP - Jul 12, 2004 · N606FE · Doug MD11SDR 04FDEA02044Vane · corrodedCOMPLY WITH EA 8-5750-79552 WINGS FLAP VANE SUPPORT CORROSION REWORK (RT OUTBOARD FLAP). COMPLIED WITH EA 8-5750-79552 WINGS FLAP VANE SUPPORT CORROSION REWORK, RIGHT O/B FLAP.Jul 11, 2004 · N398FE · Doug MD1010FSDR SWAA041951Skin · delaminatedDURING SCHEDULED PM CHECK, FOUND RT WING OUTBOARD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED RT OUTBOARD AFT T/E FLAP PER MM.Jul 10, 2004 · N669SW · Boeing 7373A4SDR 04FDEA02040Fitting · corrodedCOMPLY WITH EA 8-5750-79545 WINGS OUTBOARD FLAP, FLAP SPINDLE CARRIAGE SUPPORT FITTING CORROSION REPAIR, P/N ARC2177. COMPLIED WITH EA 8-5750-79545 WINGS OUTBOARD FLAP, FLAP SPINDLE CARRIAGE SUPPORT FITTING CORROSION REPAIR, P/N ARC2177.Jul 10, 2004 · N359FE · Doug MD1010FSDR 04FDEA02039Fitting · corrodedCOMPLY WITH EA 8-5750-79549 WINGS RIGHT O/B FLAP I/B HINGE LUG CORROSION REPAIR (P/N ARC1984). COMPLIED WITH EA 8-5750-79549 WINGS RIGHT OUTBD FLAP INBD HINGE LUG CORROSION REPAIR (P/N ARC1984).Jul 10, 2004 · N359FE · Doug MD1010FSDR 04FDEA02038Vane · corrodedCOMPLY WITH EA 8-5750-79551 WINGS FLAP VANE SUPPORT CORROSION REWORK (LT OUTBD FLAP). COMPLIED WITH EA 8-5750-79551 WINGS FLAP VANE SUPPORT CORROSION REWORK (LT OUTBD FLAP) AT MAE.Jul 10, 2004 · N398FE · Doug MD1010FSDR 04FDEA02035Fitting · wornRIGHT WING I/B FLAP I/B TRACK FAIRING AFT MOUNT WORN. REMOVED AND REPLACED MOUNT IAW SRM 51-33-01 AT MAE.Jul 10, 2004 · N398FE · Doug MD1010FSDR CA040827006Bolt · loose(CAN) ON A WALK AROUND INSPECTION ONE OF FOUR BOLTS FOR THE OB LT FLAP DEFECTER WAS FOUND TO HAVE BACKED OFF.Jul 9, 2004 · Emb EMB110P1SDR UPS04242701Carriage · wornATB FL 330 IN CLIMB EXPERIENCED MODERATE VIBRATION. FOUND LEFT OUTBOARD TRAILING FLAP, INBOARD TRACK AFT ROLLER CLEARANCE OUT OF TOLERANCE. REPLACED ROLLER.Jul 9, 2004 · N938UP · Boeing 727173CSDR SWAA041941Skin · delaminatedDURING SCHEDULED 1/2D CHECK, FOUND RT WING INBOARD FORE FLAP DELAMINATED. REMOVED AND REPLACED RT INBOARD FORE FLAP PER MM.Jul 9, 2004 · N349SW · Boeing 7373H4SDR UPS04242666Carriage · wornAIRFRAME HAS A VIBRATION - ATB. TE FLAP CARRIER HAS EXCESS PLAY.Jul 9, 2004 · N938UP · Boeing 727173CSDR 04FDEA02027Fitting · corrodedRT WING, INBOARD FLAP VANE TEE-FITTING INBOARD MOST AFT ATTACHING HOLE CORRODED. RT WING, INBOARD FLAP VANE TEE-FITTING INBOARD MOST AFT ATTACHING HOLE CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2 - 4. ORIGINAL DIAMETER = 0.8755 INCH, FINAL DIAMETER = 0.882 Jul 8, 2004 · N606FE · Doug MD11FSDR 04FDEA02013Hinge Bracket · corrodedLT WING OUTBOARD FLAP INBOARD AFT HINGE, INBOARD PIVOT HOLE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. ORIGINAL DIAMETER:1.093; FINAL DIAMETER: 1.096 AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76783, WINGS- LEFT AND RIGHT OUTBOARD FLJul 7, 2004 · N606FE · Doug MD11SDR 04FDEA02012Hinge Bracket · corrodedLT WING OUTBOARD FLAP INBOARD AFT HINGE, OUTBOARD PIVOT HOLE SPOT SURFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. ORIGINAL THICKNESS: 0.504; MATERIAL REMOVED 0.002"; REMAINING THICKNESS: 0.502 AND REPAIR CARRIED OUT AS PER FEDEX EA 1-Jul 7, 2004 · N606FE · Doug MD11SDR 04FDEA02011Hinge Bracket · corrodedOUTBOARD FLAP INBOARD AFT HINGE, INBOARD PIVOT HOLE SPOT SURFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. ORIGINAL THICKNESS: 0.506; MATERIAL REMOVED 0.020; REMAINING THICKNESS: 0.486 AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-767Jul 7, 2004 · N606FE · Doug MD11SDR 04FDEA02010Hinge Bracket · corrodedOUTBOARD FLAP INBOARD AFT HINGE, OUTBOARD ACTUATOR HOLE SPOT SURFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. ORIGINAL THICKNESS: 0.408; MATERIAL REMOVED 0.004; REMAINING THICKNESS: 0.404 AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-767Jul 7, 2004 · N606FE · Doug MD11SDR 04FDEA02009Hinge Bracket · corrodedOUTBOARD FLAP INBOARD AFT HINGE, INBOARD ACTUATOR HOLE SPOT SURFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. ORIGINAL THICKNESS: 0.406; MATERIAL REMOVED 0.002; REMAINING THICKNESS: 0.404 AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76Jul 7, 2004 · N606FE · Doug MD11SDR 04FDEA02008Hinge Bracket · corrodedOUTBOARD FLAP INBOARD AFT HINGE, OUTBOARD ACTUATOR HOLE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. ORIGINAL DIAMETER: 1.062"; FINAL DIAMETER: 1.189 AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76783, LEFT AND RIGHT OUTBOARD FLAP - INBJul 7, 2004 · N606FE · Doug MD11SDR 04FDEA02020Skin · damagedLEFT HAND OUTBOARD FLAP, UPPER SKIN, INBOARD SECTION, NUMEROUS DAMAGED RIVETS. REMOVED DAMAGED FASTENERS IAW DC10 SRM 51-31-01 VOL II. FABRICATED REPAIR STRAPS IAW DC10 SRM 51-20-00 VOL I AND DC10 SRM 51-21-01 VOL II. INSTALLED REPAIR STRAPS IAW DC10 SRM 57Jul 7, 2004 · N386F · Doug MD1010FSDR 04FDEA02017Wedge · dentedRIGHT HAND OUTBOARD FLAP NR 2 TRAILING EDGE STATION 556 HAS DENT OUT OF LIMITS. FABRICATED SKIN ASSEMBLY IAW DAC DWG ARC 1953 AND INSTALLED SKIN IAW DC10 SRM 51-40-02 VOL 2.Jul 7, 2004 · N323FE · Doug DC1030SDR 04FDEA02014Hinge · corrodedLEFT WING OUTBOARD FLAP INBOARD AFT HINGE, OUTBOARD PIVOT HOLE FOUND CORRODED. CORROSION REMOVED PER CMM 20-11-02, PAGES 2 - 4. ORIGINAL DIAMETER = 1.062, FINAL DIAMETER = 1.094. COMPLIED WITH FEDEX EA 1-5750-76783, WINGS - LEFT AND RIGHT OUTBOARD FLAP - INBJul 7, 2004 · N606FE · Doug MD11SDR SWAA041922Skin · delaminatedDURING SCHEDULED C2 CHECK, FOUND LT WING INBOARD T/E FORE FLAP DELAMINATED. REMOVED AND REPLACED LT INBOARD FORE FLAP PER MM.Jul 7, 2004 · N619SW · Boeing 7373H4
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