JASC 5753
Service difficulty reports · 31,513
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 IPXA12674314Wedge · dentedINSPECTION TYPE:1C, LT WING OTBD T/E FLAP T/E WEDGE UPPER SURFACE DENTED. COMPOSITE PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07 PAR 5A(1) FIG 9, REV 52.SDR IPXA12674310Fairing · delaminatedINSPECTION TYPE: 1C, LT WING INBD MAIN FLAP OTBD L/E FAIRING DELAMINATED. COMPOSITE PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-05, PAR 5A(1) FIG 5, REV 52.SDR IPXA12674307Wedge · dentedINSPECTION TYPE:1C, LT WING OTBD T/E FLAP, T/E WEDGE, UPPER SURFACE DENTED. COMPOSITE PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAC 5A(1) FIG 9, REV 52.SDR IPXA12674304Wedge · dentedINSPECTION TYPE:1C, LT WING OTBD T/E FLAP, T/E WEDGE UPPER SURFACE DENTED. COMPOSITE PERPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5A(1) FIG 9, REV 52.SDR IPXA12674292Wedge · dentedINSPECTION TYPE:1C, LT WING OTBD T/E FLAP WEDGE UPPER SURFACE DENTED. COMPOSITE PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5A(1), FIG 9, REV 52.SDR IPXA12674291Wedge · dentedINSPECTION TYPE: 1C, LT WING OTBD T/E FLAP T/E WEDGE UPPER SURFACE DENT. COMPOSITE PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5A(1) FIG 9, REV 52.SDR FDEA201207042481Skin · crackedLEFT WING INBD FLAP ASSY UPPER SURFACE MID SEGMENT STA XIFH 165, FOUND CRACKED. FOUND CRACKED. CRACKED SKIN AT LEFT HAND WING INBOARD FLAP ASSEMBLY UPPER SURFACE MID SEGMENT TRIMMED AND CARRIED OUT REPAIR AS PER SRM 57-10-00 FIGURE 85 VOLUME I REVISION 98. SDR IPXA12674325Wedge · dentedINSPECTION TYPE: 1C, LT WING OTBD T/E FLAP, T/E WEDGE DENTED. COMPOSITE PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5A (1), FIG 9, REV 52.SDR IPXA12674317Wedge · dentedINSPECTION TYPE:1C, LT WING OTBD T/E FLAP T/E WEDGE UPPER SURFACE DENTED. COMPOSITE PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5A(1), FIG 9, REV 52.SDR IPXA12674315Wedge · dentedINSPECTION TYPE: 1C, LT WING OTBD T/E FLAP, T/E WEDGE UPPER SURFACE DENTED. COMPOSITE PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5A(1), FIG 9, REV 52.SDR IPXA12674306Wedge · dentedINSPECTION TYPE: 1C, RT WING OTBD T/E FLAP, T/E WEDGE, UPPER SURFACE DENTED. COMPOSITE PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5A(1) FIG 9, REV 52.SDR IPXA12674302Wedge · dentedINSPECTION TYPE:1C, RT WING OTBD T/E FLAP, T/E WEDGE UPPER SURFACE DENTED. COMPOSITE PREPREG LAY UP REPAIR CARRIED OUT SRM 51-70-07, PAR 5A(1) FIG 9, REV 52.SDR IPXA12674300Wedge · dentedINSPECTION TYPE:1C, RT WING OTBD T/E FLAP T/E WEDGE UPPER SURFACE DENT COMPOSITE PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5A(1), FIG 9, REV 52.SDR IPXA12674295Wedge · dentedINSPECTION TYPE:1C, LT WING OTBD T/E FLAP, T/E WEDGE UPPER SURFACE DENT. COMPOSITE PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5A(1), FIG 9, REV 52.SDR IPXA12674294Wedge · dentedINSPECTION TYPE:1C, RT WING OTBD T/E FLAP, T/E WEDGE UPPER SURFACE DENT. COMPOSITE PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5A(1), FIG 9, REV 52.SDR IPXA12674293Wedge · dentedINSPECTION TYPE:1C, RT WING OTBD T/E FLAP T/E WEDGE UPPER SURFACE DENT. COMPOSITE PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5A(1), FIG 9, REV 52.SDR IPXA12674263Skin · dentedINSPECTION TYPE: 1C, RT WING OTBD FLAP UPPER FWD PANEL DENTED. METAL HOT BOND REPAIR PERFORMED IAW SRM 51-70-10-2R, REPAIR 2, FIG 201, REV 52.SDR IPXA2574205Skin · dentedRT WING T/E INBD MAIN FLAP DENTED. REMOVED DAMAGE AND REPAIRED IAW EO B757-5750-46970 ON NRC 511174.SDR UALA2012070503606Torque Tube · corrodedRT MAIN FLAP FAILSAFE TORQUE TUBE SHOWS SIGNS OF CORROSION. REPAIRED RT WING FAILSAFE TORQUE TUBE PER CMM 57-53-43.SDR UALA2012070503605Torque Tube · corrodedLEFT INBD MAIN FLAP TORQUE TUBE FAILSAFE SHOWS SIGNS OF CORROSION. REPAIRED THE FAILSAFE TORQUE TUBE PER CMM 57-53-43, REFERENCE R03846, 8130-3, 016-A004726 49. WORK WAS ACCOMPLISHED AT SFO.SDR IPXA12674321Wedge · puncturedINSPECTION TYPE: 1C, LT WING OTBD AILERON T/E WEDGE UPPER SURFACE PUNCTURED. COMPOSITE PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-05, PAR 5C, FIG 2, REV 52.SDR SWAA2012070505534Skin · delaminatedRIGHT WING OUTBOARD AFT FLAP DELAMINATED AT UPPER SURFACE. REMOVED AND REPLACED FLAP PER MM.SDR MASA2012070434962Structure · damagedLEFT INBOARD FLAP DAMAGED. REMOVED AND REPLACED LEFT INBOARD FLAP.SDR USAA2012071200019Support Fitting · corroded2S CHECK - CORROSION ON PENDULUM ASSEMBLY (MACHINED FITTING) ON RIGHT OUTBOARD FLAP OUTBOARD POSITION AT RIB 15. REPLACED PENDULUM ASSEMBLY (MACHINED FITTING) ON RIGHT OUTBOARD FLAP OUTBOARD POSITION IAW A320 SRM 51-72-11 & CMM 57-53-21.SDR WVER2012070292303Skin · dentedRT INBOARD FLAP LOWER SKIN WS 48.95 AT THE TRAILING EDGE HAS 2 DENTS IN SAME AREA 2.5 INCH BY 2.5 INCH BY .150 DEEP. THE AREA UNDER THE HINGE FAIRING IS CHAFED.SDR UALA2012070303553Skin · dentedLEFT INBD FLAP HAS BOWLING PIN SHAPED DENT 36 INCHES FROM INBOARD EDGE. DENT IS 8.50 INCHES LONG AND 7.25 INCHES WIDE AND MEASURES .25 INCHES DEEP. AFTER FURTHER EVALUATION PER MM DAMAGE IS OUT OF SERVICEABLE LIMITS. STARTED REMOVAL OF LT INBD FLAP PER AMM.SDR SWAA2012070205475Skin · delaminatedLEFT WING OUTBOARD AFT FLAP LOWER INBOARD SURFACE DELAMINATED. REMOVED AND REPLACED AFT FLAP PER AMM.SDR SWAA2012091007443Flap · chafedRIGHT WING OUTBOARD LEADING EDGE FORE FLAP INBOARD OF NR 1 AUX TRACK BULL NOSE CHAFED. REPAIRED FORE FLAP PER SRM AND AMM.SDR FDEA201206292401Hinge Fitting · damagedRT WING INBD FLAP OTBD AFT HINGE BRACKET PIVOT OTBD LUG BORE FOUND SCRATCHES. REWORKED AND FOUND EXCEED LIMIT AS PER SRM 57-52-03 REVISION 73. EXISTING HOLE DIAMETER 1.2865", REWORKED HOLE DIAMETER 1.313", MAXIMUM LIMIT DIAMETER 1.220". REPAIR ACCOMPLISSDR FDEA201206292400Hinge Fitting · damagedRT WING INBD FLAP OTBD AFT HINGE BRACKET PIVOT INBD LUG BORE FOUND SCRATCHES. REWORKED AND FOUND EXCEED LIMIT AS PER SRM 57-52-03 REVISION 73. EXISTING HOLE DIAMETER 1.228", REWORKED HOLE DIAMETER 1.250", MAXIMUM LIMIT DIAMETER 1.220". REPAIR ACCOMPLISHED ASDR FDEA201206292399Hinge Fitting · damagedLT WING INBD FLAP OTBD AFT HINGE BRACKET PIVOT INBD LUG BORE FOUND SCRATCHES. REWORKED AND FOUND EXCEED LIMIT AS PER SRM 57-52-03 REVISION 73. EXISTING HOLE DIAMETER 1.2215", REWORKED HOLE DIAMETER 1.250", MAXIMUM LIMIT DIAMETER 1.220". REPAIR ACCOMPLISSDR FDEA201206292398Hinge Fitting · damagedLT WING INBD FLAP OTBD AFT HINGE BRACKET PIVOT OTBD LUG BORE FOUND SCRATCHES. REWORKED AND FOUND EXCEED LIMIT AS PER SRM 57-52-03 REVISION 73. EXISTING HOLE DIAMETER 1.255", REWORKED HOLE DIAMETER 1.2834", MAXIMUM LIMIT DIAMETER 1.220". REPAIR ACCOMPLISHSDR 2013FA0000185Bearing · failedDURING FLIGHT, ACFT EXPERIENCED AN ASYMMETRICAL FLAP CONDITION. PROTECTION CIRCUIT WORKED APPROPRIATELY, BUT CREW NOTICED INTERFERENCE WITH AILERON, DECLARED AN EMERGENCY AND LANDED SAFELY. ON INVESTIGATION, TROUBLE WAS FOUND TO BE IN THE AFT INBD BEARING. SDR A6WA201240696Vane · chafedLEFT INBD FLAP VANE L/E CHAFED FOUR SPOTS. REPAIRED CHAFED AREAS AT OTBD AND CENTER LOCATION ON LT INBD FLAP VANE L/E IAW REO 601R-57-52-004, REV C. R & R LT INBD FLAP VANE INBD L/E SKIN IAW SRM 51-42-13.SDR AALA20120630015Skin · damagedLEFT OUTBOARD AFT FLAP LOWER SKIN TRAILING EDGE WEDGE HAS DELAMINATED DENT APPROXIMATELY 2 INCHES IN DIAMETER, 21 INCHES FROM OUTBOARD END OF FLAP AND 4.5 INCHES FROM TRAILING EDGE. REMOVED DELAMINATED SKIN AND CORE TO 0.5 DEPTH. BONDED IN NEW CORE PLUG. HOSDR DALA12002653128Flap Track · corrodedLEFT WING OUTBOARD FLAP TRACK NR 3 AND NR 4 PIVOT BOLTS HAVE CORROSION AND ARE MISSING PLATING. ACCOMPLISHED INSTALLATION OF NEW LEFT WING OUTBOARD FLAP TRACK NR 3 AND NR 4 PIVOT BOLTS ON WORKCARD NO 2750-6020RT. BOLTS REPLACED DUE TO OUT OF LIMITS IAW AMM 2SDR DALA12002643128Flap Track · corrodedRIGHT WING INBOARD FLAP TRACK NR 2 PIVOT BOLT HAS CORROSION AND MISSING PLATING. RT WING INBOARD FLAP NR 2 TRACK PIVOT BOLT REPLACED. FOUND TO BE OUT OF LIMITS IAW A319 AMM 27-54-61-220-001. INSTALLATION ACCOMPLISHED ON WORKCARD NR 2750-6010 RT. DAMAGE DIMSDR SPUY20120627022Support · corrodedRT WING REAR SPAR AREA. REAR SUPPORT TO FLAP TRACK NR 5 SHOWS CORROSION AT WS 224.50 (FWD PART).SDR QXEA2012062600553Shroud · damagedFOULING DAMAGE ON RT FLAP SHROUD. COMPLIED WITH TASK CARD RD 8/4-57-1836. COMPLIED WITH TASK CARD RD 8/4-57-1837.SDR FDEA201206262350Structure · damagedWITH INBD FLAP ASSY OTBD HINGE PIVOT BEARING REMOVED. FOUND FORWARD HINGE PIVOT HOLE INBD SPOT FACE CORROSION. REMOVED CORROSION AND FOUND WITHIN LIMIT IAW CMM 57-44-07, REV 56, ORIGINAL THICKNESS: 0.486", MATERIAL REMOVED :0.017", REMAINING THICKNESS: 0.46SDR FDEA201206252343Skin · misrepairedRT WING NR 4 SLAT AFT SURFACE STATION XOS 612, MISREPAIRED. REPAIRED IAW SRM 57-10-00 FIGURE 31, VOLUME I, REV 98. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 115.SDR SWAA2012071205774Rib · crackedRIGHT WING O/B FORE FLAP O/B HINGE RIB CRACKED AT WBL 355. REMOVED AND REPLACED RIB IAW SRM AND DWG.SDR WX0A071235Vane · chafedLEFT WING O/B FLAP CENTER VANE LEADING EDGE CHAFE. REMOVED DAMAGED AREA FABRICATED DOUBLER AND BONDED IAW MD-80 SRM 51-70-02 PARA 13.SDR V0XR20120629J0051Beam · corrodedNR 3 FLAP TRACK BEAM ON RIGHT WING IS CORRODED BEYOND SERVICEABLE LIMITS. REMOVED AND REPLACED NR 3 FLAP TRACK BEAM ON RIGHT WING IAW DHC DASH 8-200 AMM 57-50-26 & 20-16-28. (REF W/O 80064, W/C 4072)SDR REXA2012062600865Skin · dentedRIGHT OUTBOARD FLAP LOWER SKIN DENTED BETWEEN FLAP STATION 178.13 AND 226.13. REPAIRED IAW BOMBARDIER REO 601R-57-53-938.SDR CA120625006Rib · worn(CAN) ON DAILY WALK AROUND INSPECTION OF ACFT, THE LT HAND OUT BOARD FLAP WAS FOUND TO HAVE SIDE PLAY. ON CLOSER VISUAL INSPECTION THE AFT BEARING FACES ON BOTH TRACKS, IT WAS FOUND TO HAVE WORN THE RIB FACE OF THE FLAP. MEASURE OF THE WEAR FOUND TO BE .020 SDR SWAA2012062605292Flap · puncturedRIGHT WING INBOARD FORE FLAP PUNCTURED. REMOVED AND REPLACED FORE FLAP PER MM.SDR FDEA201206232316Skin · misrepairedLT WING INBD FLAP ASSY, OTBD LOWER SEGMENT UPPER SURFACE FORWARD EDGE STATION XIFH 249 MISREPAIRED. REPAIR CARRIED OUT PER SRM 57-10-00 FIGURE 85 VOLUME I REVISION 99. E.O. #8-5100-7-5001 B2 PART 2SDR FDEA201206232315Skin · misrepairedINBD LOWER SEGMENT UPPER SURFACE FORWARD EDGE STA XIFH 237 OF LT WING TE FLAP, MISREPAIRED. REPAIR CARRIED OUT PER E.A. 8-5750-160987 PART 1 STEP 2.SDR FDEA201206232314Rib · misrepairedRIB MISREPAIRED AT RT WING INBD FLAP L/E AT XIFH 240. REMOVED AND REPLACED PER E.A. 8-5750-160991.
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