JASC 5753
Service difficulty reports · 31,493
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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR SWIA2026052176785Cap · chafedDURING AUDIT OF 1C TASK CARD 57-580-302 (EXTERNAL ZONAL INSPECTION OF THE LT WING INBD FLAP, FLAP VANE, HINGE ARMS) FOUND A CHAFE ON THE FLAP VANE, LEADING EDGE AT CENTER OF VANE. INSTALLED A NEW SACRIFICIAL CAP AT CENTER OF LT WING INBD FLAP VANE CAP P/N CC6SDR VNAA202607300006Skin · damagedTEMPORARY DISPOSITION FOR BLENDED NICK/GOUGES DAMAGE TO RH INBD FLAP LOWER SKIN BTW FLS25.5-FLS36 & FRONT SPAR & T/E THE SUBJECT CONDITIONS IS STRUCTURALLY ACCEPTABLE FOR 4600 FLIGHT HOURS FROM THE TIME OF INCORPORATION OF THIS REO AT REV. PREVIOUS BLEND OUTSDR SWAA2026060205499Skin · delaminatedLH OB AFT FLAP IS DELAMINATED NEAR IB TE. PROCURED NEW LT WING OTBD AFT FLAP. REMOVAL AND INSTALLATION TO BE ACCOMPLISHED ON FAULT TTG8Q01BR3LB. PER AMM 27-51-22-401.SDR FDEA202605210626Skin · delaminatedL/H WING INB MAIN FLAP TRAILING EDGE PREVIOUS REPAIR IS DEBONDED REMOVED PREVIOUS REPAIR LOWER SKIN FOUND DEBONDED AND INSTALLED PERMANENT REPAIR AT LH WING I/B MAIN FLAP TRAILING EDGE IAW B757 SRM 57-53-01-2R, FIG 201, RPR 1, SHEET 2, DETAIL I, AND SRM 51SDR REXA2026080401476Plate · worn"INITIAL INSPECTION': WEAR ON FLAP FITTING AND PLATE SUPPORT OF ""FLAP STUB FAIRING"" 171DL AND 172DR AT RH/LH WING TRAILING EDGE. FLAP FITTING AND PLATE SUPPORT OF ""FLAP STUB FAIRING"" 171DL AND 172DR AT RH/LH WING TRAILING EDGE WERE REPLACED PER CRJ900 SRM SDR REXA2026080401475Plate · worn"INITIAL INSPECTION': WEAR ON FLAP FITTING AND PLATE SUPPORT OF ""FLAP STUB FAIRING"" 171DL AND 172DR AT RH/LH WING TRAILING EDGE. FLAP FITTING AND PLATE SUPPORT OF ""FLAP STUB FAIRING"" 171DL AND 172DR AT RH/LH WING TRAILING EDGE WERE REPLACED PER CRJ900 SRM SDR REXA2026080401474Fitting · worn"INITIAL INSPECTION': WEAR ON FLAP FITTING AND PLATE SUPPORT OF ""FLAP STUB FAIRING"" 171DL AND 172DR AT RH/LH WING TRAILING EDGE. FLAP FITTING AND PLATE SUPPORT OF ""FLAP STUB FAIRING"" 171DL AND 172DR AT RH/LH WING TRAILING EDGE WERE REPLACED PER CRJ900 SRM SDR REXA2026080401473Fitting · worn"INITIAL INSPECTION': WEAR ON FLAP FITTING AND PLATE SUPPORT OF ""FLAP STUB FAIRING"" 171DL AND 172DR AT RH/LH WING TRAILING EDGE. FLAP FITTING AND PLATE SUPPORT OF ""FLAP STUB FAIRING"" 171DL AND 172DR AT RH/LH WING TRAILING EDGE WERE REPLACED PER CRJ900 SRM SDR SWAA2026063004615Cartridge · crackedCRACKED FOUND ON RT OTBD AFT FLAP CARTRIDGE. RECEIVED A NEW AFT FLAP. NO FURTHER ACTION REQUIRED ON THIS FAULT.SDR SWAA2026063004616Rib · crackedCRACK FOUND ON RT OTBD AFT FLAP CLOSURE RIB. PROCURED NEW LT OTBD AFT FLAP. REMOVAL AND INSTALLATION TO BE ACCOMPLISHED ON FAULT TTG8Q01C9QA5. IAW AMM 27-51-22-401.SDR DALA2026052803218Vane · debondedONE DISBONDED AREA OF 1.000IN ( LENGTH) X 1.000IN (WIDTH) WAS FOUND ON FLAP VANE, ON UPPER SURFACE AT RIGHT WING. REPAIRED PER PRI 634257-14 REV 2 AND ER/A NO.634257-14 (1604178) (AIRCRAFT GROUNDED)SDR SWAA2026052704882Beam · elongatedRIGHT WING T/E BEAM 115A2759-14 HAS ELONGATED HOLES. REMOVED AND REPLACED RT WING T/E BEAM ASSY IAW DWG 115A2714, REV -, AND SRM 51-40-02. C/W MT.SDR SWAA2026052204648Skin · delaminatedRIGHT WING OTBD AFT FLAP DELAMINATED AT INBD T/E 8.5' LONG 1' WIDE. REMOVED AND REPLACED IAW AMM 27-51-22.SDR FDEA202605200623Flap · gougedGOUGE ON INBOARD FLAP LEADING EDGE AREA. RH WING (LATE FINDING) DAMAGE AT INBOARD FLAP LEADING EDGE AREA WAS REPAIRED OF RH WING. I.A.W. SRM 57-53- 01-2R REPAIR 2 FIGURE 201 REV. 94 DEC 15/2025SDR FDEA202605190780Rib · crackedLH WING CENTER FLAP RIB UPPER FLANGE FOUND 1EA CRACK AT RIB26 BETWEEN STGR2.7 AND STGR2.8 COMPLIED WITH EA 6-5750-T0377102 A P2 PERFORMED HFEC INSPECTION TO CONFIRM THE CRACK IN LH WING CENTER FLAP RIB26 UPR FLANGE BETWEEN STGR2.7 AND STGR2.8 AND REMOVEDSDR SWAA2026061104505Fairing · crackedNR 6 CANOE FAIRING CRACKED. INSIDE CENTER BOTTOM. REPAIRED PER E/A M 21-157-01063. INSPECTION C/W FOR CORRECTIVE ACTION NR 1. REPAIRED IAW E/A M 21-157-01063.SDR FDEA202605190633Rib · crackedLH WING CENTER FLAP RIB UPPER FLANGE FOUND 2EA CRACKS AT RIB13 BETWEEN STGR2.6 AND STGR2.7 & RIB15 BETWEEN STGR2.7 AND STGR2.8. COMPLIED WITH EA 6-5750-T0377102 A P2 TO REPAIR THE LH WING CENTER FLAP RIB UPPER FLANGE 2EA CRACKS AT RIB3 BETWEEN REAR SPAR ASDR FDEA202605190632Rib · crackedLH WING CENTER FLAP RIB UPPER FLANGE FOUND 2EA CRACKS AT RIB11 BETWEEN REAR SPAR AND STGR2.8 & BETWEEN STGR2.7 AND STGR2.8. COMPLIED WITH EA 6-5750-T0377102 A P2 TO REPAIR THE LH WING CENTER FLAP RIB UPPER FLANGE 2EA CRACKS AT RIB11 BETWEEN REAR SPAR AND SDR FDEA202605190631Rib · crackedLH WING CENTER FLAP RIB UPPER FLANGE FOUND 2EA CRACKS AT RIB13 BETWEEN STGR2.6 AND STGR2.7 & RIB15 BETWEEN STGR2.7 AND STGR2.8. COMPLIED WITH EA 6-5750-T0377102 A P2 TO REPAIR THE LH WING CENTER FLAP RIB UPPER FLANGE 2EA CRACKS AT RIB13 BETWEEN STGR2.6 ANSDR FDEA202605190630Rib · crackedLH WING CENTER FLAP RIB UPPER FLANGE FOUND 2EA CRACKS AT RIB19 & RIB20 BETWEEN STGR2.8 AND REAR SPAR. COMPLIED WITH EA 6-5750-T0377102 A P2 TO REPAIR THE LH WING CENTER FLAP RIB UPPER FLANGE 2EA CRACKS AT RIB19 & RIB20 BETWEEN STGR2.8 AND REAR SPAR. EA TISDR DALA2026052703188Rib · not reportedDAMAGE TOLERANCE EVALUATION ( DTE ) REQUIRED FOR REPAIR PERFORME D ON LT INBD FLAP RIB 9 LUG PER ER/A 633957-14. SECTION I IS LIMITED TO 6 MONTHS ( 182 DAYS ) FROM 15MAY26. ER/A TO BE REVISED PRIOR TO THIS LIMIT ELSE REMOVE A/C FROM SERVICE. ASSOCIATED ER/A 1SDR DALA2026051903063Hinge Fitting · corrodedCORROSION ON UPPER HOLES (2EAS) OF RH OUTBOARD WING FLAP HINGE FITTING ALSO CORROSION AND WEAR ON AFT OUTBOARD HINGE POINT (OUT FACE)OF SAME HINGE. RT OUTBOARD WING FLAP HINGE FITTING WAS REPAIRED PER CMM 27-50-5, PRI 634038-14 REV 6. & ER/A 634038-14 REV. (SDR SWAA2026061003816Wedge · debondedDEBONDED I/B MAIN FLAP TRAILING EDGE LOWER SKIN WEDGE PANEL AT RT WING. THIS REPAIR HAS BEEN ACCOMPLISHED PER SRM 57-53-01-2R-18 WITH A MINOR DEVIATION IN EXTENDED SKIN TRIM LINE CONSIDERED ACCEPTABLE AS PER EA 26-157-01381.SDR CALA2026052916638Flap Track · gougedLEFT WING OTBD MAIN FLAP NR 3 FLAP TRACK FITTING GOUGED. REMOVED NR 3 FLAP TRACK FITTING ON LT OTBD MAIN FLAP IAW ECRA 5753-02436, REPAIRED THE LT OTBD MAIN FLAP AFT NR 3 FLAP TRACK RIB WEAR DAMAGE.SDR SWAA2026051903589Cartridge · crackedLEFT OTBD FLAP, INBD CLOSURE RIB CARTRIDGE ASSY ON AFT FLAP HAS A CRACK INDICATION WHILE PERFORMING HFEC OPEN HOLE ON THE LOWER SURFACE FORWARD FASTENER HOLE. REMOVED AND REPLACED LT OTBD FLAP IAW 27-51-22. OPS CHECKS GOOD. INSPECTED PER AMM 27-51-22-401-NGSDR 1Q2R202606100004Panel · dentedLEFT INBOARD LEADING EDGE FLAP SKIN DENTED BETWEEN ST 29.00 AND 60.50. PERFORMED PERMANENT REPAIR IAW REO 670-57-52-658, REV--.SDR SWIA2026051477177Skin · dentedLEFT INBD FLAP HAD A DENT ON LOWER SKIN TRAILING EDGE, WS 104. DENT MEASURES APPROX 15L X 15W X 0030D. REPAIRED LT INBD FLAP SKIN IAW SNIEO 601R14008 S16, SRM 51-23-00 & SRM 51-42-13. COMPLETED SKYCARD 51-900-1003-SKY. NO WEIGHT CHANGE SEE CONTINUE CARD FOSDR SWIA2026051477166Spar · gougedRIGHT INBD FLAP HAS A GOUGE ON THE FWD FACE OF THE FRONT SPAR LOCATED AT WS 127.25. REMOVED GOUGE DAMAGE AND REPAIRED RT INBD FLAP IAW REO 601R-57-52-2557, REV-.SDR FDEA202605140595Skin · debondedLEFT OTBD FLAP LWR SURFACE FROM OTBD TO INBD 268 INCHES CROSS TE TO LE 10 INCHES FOUND DEBONDED. REPAIRED LH OB FLAP LWR SURFACE DISBOND AT OTEF STA 260 AS PER B777 SRM 57-53-01-2R-2 FIGURE 201-204 AND SRM 51-70-04-2R-1 AND SRM 51-70-04-2R-0 PARA 4N FIGURE SDR AALA202606116237Skin · delaminatedAIRCRAFT IN BASE MAINTENANCE: LEFT WING INBOARD AFT FLAP OUTBOARD BOTTOM CORNER SKIN DELAMINATED. REPLACED SKIN PER TI575309-601R1.SDR IPXA2026052137024Skin · debondedDEBONDED SKIN, RT WING OUTBD FLAP TE WEDGE. (REPAIR) PERFORMED NDT/UT FOR THE REWORKED AREA & PLUS 2" AROUND HEATED AREA ,PER 767 NDT MANUAL PART 1 51-01-01 REV:143 RESULT:NO DEFECT WAS FOUNDSDR SWAA2026051897807Skin · delaminatedFOUND PREVIOUS REPAIR ON RH OTBD T/E AFT FLAP DELAMINATED/COMPROMISED. 1 CIRCUMFERENCE HOLE WITH FILLED MATERIAL APPROX. 6 FROM INBD EDGE; 2.750 FROM T/E. MISSING PATCHWORK APPROX. 4.250 X 4.250.<[01] REF. TSR #2026002929. C/W EA 26-157-01277 REF. TTG8Q01C5596SDR 2026FA0000357Stiffener · shearedFLAP TRACK STIFFENERS THAT KEEP THE FLAP TRACKS STRAIGHT AND TRUE WERE FOUND TO BE SHEARED OFF AND/OR CRACKEDSDR IPXA2026051311114Fairing · crackedCRACKED SKIN, RT WING T/E NO.6 FLAP AFT FAIRING. PERFORMED NDT/UT FOR REWORKED AREA PLUS 6'' AROUND HEATED AREA IAW NTM PART1 51-01-01 REV:143. NO DEFECT FOUND.SDR AALA202606017848Skin · delaminatedAIRCRAFT IN BASE MAINTENANCE: LEFT HAND OUTBOARD TRAILING EDGE FLAP TOPSIDE DELAMINATED. REPAIRED FLAP PER CMM 57-53-08.SDR SWAA2026061596494Rub Strip · crackedNR 3 AFT FLAP FAIRING 542BB O/B RUB STRIP CRACKED. REMOVED AND INSTALLED NEW OTB RUB STRIP ON NR 3 AFT FLAP FAIRING 542BB IAW AMM 20-50-11-910-801 .SDR SWAA2026061196793Rib · crackedFOUND CRACK INDICATION BY HFEC NDT PART 6, 51-00-00 PROCEDURE 23 OF LT WING TRAILING EDGE RIB WBL 413.18. IAW EA 26-157-01239-WIP1, STEP 7. DAMAGE LOCATION 1. LENGTH APPROXIMATELY .1'. REPAIRED PER EA 26-157-01239.SDR SWAA2026052296857Cartridge · crackedCRACK INDICATION ON LT OTBD AFT FLAP INBOARD CARTRIDGE RADIUS ZONE.CRACK LENGHT 0.437 IN APPROX. LEFT WING. REPLACED INBOARD CARTRIDGE RADIUS ON OTBD AFT FLAP LT WING IAW SOPM 20-50-03; IAW AMM 27-51-22-400-801 AND IAW SRM 51-40-02FOR CARTRIDGE ASSEMBLY INSTASDR SWAA2026051896880Skin · delaminatedRH O/B AFT FLAP HAS DELAMINATION AT I/B END ALONG T/E<[01] RECIEVED NEW R/W O/B AFT FLAP. INSTALLATION OF AFT FLAP TO BE ACCOMPLISHED ON FAULT TTG8Q01BR0YJ;[02] VERIFIED CORRECTIVE ACTION STEP 1.SDR SWAA2026051896878Skin · delaminatedDURING OK TO INSTALL WAS FOUND; RH O/B AFT FLAP IS DELAMINATED AT I/B T/E UPPER SURFACE. GENERAL FAULT RESOLVED ON OTHER FAULT (FAULT WAS RESOLVED ON ANOTHER FAULT). DUPLICATE WRITE UP. AFT FLAP TO BE REPLACED ON FAULT TTG8Q01C3DBE.SDR AALA202605175691Flap Track · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON OUTBOARD ROLLER TRACK FOR LEFT HAND WING INBOARD MAIN FLAP. REPLACED TRACK PER SRM 51-40-02.SDR 2026FA0000336Stiffener · shearedFLAP TRACK STIFFENERS THAT KEEP THE FLAP TRACKS STRAIGHT AND TRUE WERE FOUND TO BE SHEARED OFF AND/OR CRACKED.SDR SWAA2026061595776Skin · delaminatedLEFT INBD MAIN FLAP OTBD T/E DELAMINATED. REMOVED AND INSTALLED A NEW LT INBD MAIN FLAP OTBD T/E IPC 27-51-11-01B, ITEM 175 IAW AMM 20-50-11-910-801.SDR SWAA2026061595777Skin · delaminatedRT INBD MAIN FLAP OTBD T/E DELAMINATED. REMOVED AND REPLACED NEW RT INBD MAIN FLAP OTBD T/E IAW AMM 20-50-11-910-801, DWG 113A2100 REV A, AND DWG 113A2100 REV B.SDR IPXA2026051439477Fairing · debondedFOUND RH WING NO.6 FLAP TRACK FWD FAIRING DISBOND (REPAIR). 1. I.A.W. 747-8F SRM 57-53-70-2R-1 REFER TO SRM 51-70-04-2R-1 AND SRM 51-30-10-0G-0 REV. 48 PERFORM REPAIR AS BELOW STEP : REMOVE THE DISBOND MATERIALS AND CLEAN. MEASURE THE DAMAGE AREA ( DIA : 2",SDR FDEA202605050562Skin · dentedDENT ON UPPER SKIN RH INB MAIN FLAP. 69" FROM OUTB EDGE UPPER SKIN RH INB MAIN FLAP. 69" FROM OUTB EDGE WAS REPAIRED IAW B767 SRM 57-53-01-2R FIG 201 REP.1 SHEET 2 REV94 DEC 15/2025SDR DALA2026050602861Skin · wornFOUND RT WING INBD FLAP AFT FLAP UPPER PANEL INBD SIDE WORN FROM FWD END 8 INCHS. REPAIRED WEAR ON RT WING I/B FLAP AFT FLAP UPPER PANEL INBD SIDE FROM FWD END 8 INCHS AS PER EARN N190DN-0009 AND SRM 51-70-10 (1576675) (AIRCRAFT GROUNDED)SDR DALA2026050502831Shaft · not reportedRIGHT WING REMOVE AND INSTALL TORQUE SHAFT 6282CM TO PERFORM REPAIR T/E OVERHANG AREA. : REMOVED AND REINSTALLED RT WING FLAP TORQUE SHAFT 6282CM IAW AMM TASK 27-54-45-000-013-A AND 27-54-45-400-013-A REV 135.00. (LP: 1577369)SDR IPXA2026070896552Fitting · gougedDURING RIG CHECK OF THE RH AFT INBD FLAP (MAIN FLAP IN EXTENDED POSTION), AFT FLAP INBD TRACK ROLLER ATTACH FITTING OUTBD FACE FOUND WITH GOUGE DAMAGE. INSTALLED INBD CARTRIDGE ASSEMBLY AT INBD FLAP RT WING IAW CMM 57-53-44 AND 57-53-43.SDR FDEA202605030534Skin · dentedFOUND LEFT WING T/E O/B FLAP I/B LOWER SURFACE 1EA DENT AT THE CROSS OTEF 127 INCHES AND T/E 10 INCHES. REPAIRED LH WING T/E O/B FLAP I/B LOWER SURFACE 1EA DENT AT OTEF STA 127 AS PER B777 SRM 57-53-01-2R-2 FIGURE 201-204 AND SRM 51-70-04-2R-1 PARA 4I FIG
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