JASC 5753
Service difficulty reports · 31,515
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 AWXA200601052Support Fitting · crackedDURING A CHECK DISCOVERED THE LT OTBD T/E FLAP FORE FLAP CENTER TRACK, 2ND FROM OUTBOARD END SUPPORT FITTINGS, CRACKED ON THE INBOARD AND OUTBOARD HALVES. FLAP WILL BE REPLACED. NO MAJOR REPAIR FORM WILL BE COMPLETED. FLAP WAS REMOVED AND REPLACED. THE FOLLOSDR 06FDEA2413Bolt · shearedRIGHT WING TRAILING EDGE INTERIOR STRUCTURE, OUTBOARD FLAP INBOARD TRACK SUPPORT FITTING LOWER OUTBOARD ATTACH BOLT SHEARED AT AFT SPAR. COMPLIED WITH E8-5710-100781 PT 1, LOWER ATTACH STUD BOLT REPLACED. MAJOR REPAIR.SDR KCSA061186Spar · corrodedLEFT I/B MID FLAP AFT SPAR WEB HAS CORROSION.SDR KCSA061185Spar · corrodedRIGHT I/B MID FLAP AFT SPAR WEB HAS CORROSION.SDR SWAA062206Wedge · delaminatedDURING SCHEDULED 18Y CHECK, FOUND LT WING INBOARD MID FLAP T/E WEDGE OUTBOARD END DELAMINATED. REPAIRED MID FLAP WEDGE PER SRM.SDR UPS06647394Flap · delaminatedFOUND RT I/B AFT FLAP HAS 3.5" DENT WITH DELAMINATED. REPAIRED IAW 51-20-10-2 AND 51-70-10-2R.SDR QXEA200601877Skin · chafedPDX C3 - LEFT HAND OUTBOARD FLAP IS CHAFED APPROXIMATELY 10 INCHES OUTER SKIN AT STATION 263.019. REPAIRED IAW DHC-8-400 SRM 57-52-30-320-801 AND RD 8/4-57-016 AND HORIZON AIR EA 6-57-503.SDR QXEA200601709Skin · chafedPDX: C3 CHECK, - RT WING OUTBOARD FLAP, UPPER SURFACE IS CHAFED BETWEEN APPROX YW 211 AND YW 220, 15 INCHES FROM FLAP TRAILING EDGE. MAINTENANCE REPAIRED IAW Q400 SRM 57-52-30, NDTM PART 6, 51-00-01, 1-87-7A, PART 1, 51-00-04, AND HORIZON EA 6-57-502.SDR SWAA062156Flap · delaminatedDURING SCHEDULED SERVICE CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED ON T/E EDGE. REMOVED AND REPLACED RT WING FLAP PER MM.SDR C2XA06TY038Structure · gougedTYS DURING A ROUTINE 2C INSPECTION THE RT INBOARD FLAP HOLE WAS FOUNG GOUGED. MAINTENANCE REAMED HOLE FABRICATED A NEW BUSHING AND INSTALL IAW EC5750-01291. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK.SDR SWAA062141Skin · debondedDURING SCHEDULED 20Y CHECK, FOUND LT WING MID FLAP INBOARD T/E LOWER SURFACE DISBONDED. REPAIRED MID FLAP PER SRM.SDR SWAA062140Skin · debondedDURING SCHEDULED 20Y CHECK, FOUND RT WING MID FLAP INBOARD T/E LOWER SURFACE DISBONDED. REPAIRED MID FLAP PER SRM.SDR SWAA062138Skin · delaminatedDURING SCHEDULED 20Y CHECK, FOUND LT WING FORE FLAP INBOARD T/E SURFACE DELAMINATED. REPAIRED FORE FLAP PER SRM.SDR SWAA062137Arm · corrodedDURING SCHEDULED 20Y CHECK, FOUND RT WING INBOARD MID FLAP OUTBOARD CARRIAGE INBOARD ARM CORRODED. REMOVED AND REPLACED INBOARD ARM PER CMM.SDR SWAA062136Arm · corrodedDURING SCHEDULED 20Y CHECK, FOUND RT WING INBOARD MID FLAP INBOARD CARRIAGE OUTBOARD ARM CORRODED. REMOVED AND REPLACED OUTBOARD ARM PER CMM.SDR QXEA200601904Skin · chafedLEFT I/B FLAP HAS 2 CHAFE MARKS ON UPPER SURFACE. REPAIRED IAW AMM TASK 57-51-30-32-801 AND SRM 57-51-30-992-801, 51-21-10-380-801 AND SRM 51-25-10-370-801.SDR 06FDEA2370Fitting · corrodedNR 6 FLAP TRACK FORWARD FITTING IS CORRODED ON INBOARD FACE. REPAIRED PER STANDARD REWORK DRAWING SR 27-57-020A.SDR 06FDEA2369Attach Fitting · corrodedNR 1 FLAP TRACK FWD ATTACH FITTING IS CORRODED. REPAIRED PER FED EX EA 7-5740-102247.SDR 06FDEA2368Attach Fitting · corrodedNR 8 FLAP TRACK FORWARD ATTACH FITTING IS CORRODED ON INBOARD FACE. REPAIRED PER FED EX EA 7-5740-102247.SDR UPS06547161Fairing · delaminatedLEFT WING O/B FLAP INBOARD AFT FAIRING DELAMINATED, APPROX 4 INCHES FWD OF AFT EDGE. DAMAGE IS 3 X 5 INCHES. DEFERRED PER EO B757-5750-24548-A. D327577 ASSIGNED. REMOVED DAMAGE INSTALLED PLIES STARTED CURE REF SRM 51-70-05-0G COMPLETED REPAIR REF B 757 SRMSDR MWEA060068Frame · corrodedLEFT WING FIXED VANE, 4 AT STATION 80.0 ON OUTBOARD SIDE F FORMER HAS CORROSION. FABRICATED AND INSTALLED DOUBLER.SDR 06FDEA02366Skin · dentedSNRM N01911: LHW: I/B FLAP LWR SURFACE O/B SEGMENT FOUND WITH DENTS AS MARKED SNRM N01911: LHW I/B FLAP O/B SEGMENT LOWER SURFACE DENTS REPAIRED AS PER SRM 57-10-00 FIG 2 VOL I. THIS REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR 06FDEA02365Skin · dentedRHW: I/B FLAP LWR SURFACE O/B SEGMENT FOUND WITH DENTS AS MARKED. SNRM N01727: RHW I/B FLAP LOWER O/B SEGMENT SURFACE DENTS REPAIRED AS PER SRM 57-10-00 FIG 2 VOL I. THIS REPAIR CLASSIFIED MINOR PER GMM 6-2-100.SDR QXEA200601878Skin · chafedLEFT O/B FLAP IS CHAFED APPROXIMATELY 24 INCHES ON OUTER SKIN AT STA 209.019. REPAIRED IAW SRM 57-52-30-320-801 AND EA 6-57-496.SDR AWXA200601003Structure · delaminatedPHX - MAJOR REPAIR - LOG 7260237 - DURING POST FLIGHT INSPECTION CREW REPORTED FINDING THE RT TRAILING EDGE FLAP DELAMINATED. MAINTENANCE REMOVED AND REPLACED THE RT INBOARD TRAILING EDGE AFT FLAP IAW AMERICA WEST AIRLINES TASKCARD R3M27007. FLAP WAS REPAIRESDR ASAA0640709Skin · dentedRIGHT O/B AFT LEADING EDGE DAMAGED. REMOVED DAMAGED SECTION OF LEADING EDGE SKIN. REPLACED SECTION OF LEADING EDGE SKIN IAW SRM 51-40-05 AND 51-40-02.SDR 06FDEA2366Skin · dentedI/B FLAP LWR SURFACE O/B SEGMENT FOUND WITH DENTS AS MARKED.SDR 06FDEA2365Skin · dentedI/B FLAP LWR SURFACE O/B SEGMENT FOUND WITH DENTS AS MARKED.SDR 06FDEA02364Skin · dentedLHW: I/B FLAP LWR SURFACE I/B SEGMENT FOUND WITH DENTS AS MARKED, SNRM N01912: LHW I/B FLAP I/B SEGMENT LWR SURFACE DENTS REPAIRED AS PER SRM 57-10- 00 FIG 2 VOL I. THIS REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.SDR 06FDEA02363Skin · dentedRT WING: I/B FLAP LWR SURFACE I/B SEGMENT FOUND WITH DENTS AS MARKED. SNRM N01726: RT WING I/B FLAP I/B SEGMENT LOWER SURFACE DENTS REPAIRED AS PER SRM 57-10-00 FIG 2 VOL I. THIS REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.SDR CA060618002Skin · bird strikeON APPROACH, ON FLAIR AIRCRAFT HIT A BIRD. ONCE ON THE GROUND THE CREW REPORTED TO MAINTENANCE PERSONAL WHO AFTER INSPECTING THE AIRCRAFT FOUND A DENT ON THE RT FLAP BOTTOM SKIN. DUE TO THE LOCATION OF THE DENT WHICH WAS NOT COVERED UNDER SRM. SUPPORT ENGINSDR 06FDEA2364Skin · dentedI/B FLAP LWR SURFACE I/B SEGMENT FOUND WITH DENTS AS MARKED.SDR 06FDEA2363Skin · dentedI/B FLAP LWR SURFACE I/B SEGMENT FOUND WITH DENTS AS MARKED.SDR 06FDEA2319Skin · dentedRIGHT WING I/B FLAP O/B SEGMENT LOWER SURFACE FOUND DENTS. REPAIRED AS PER SRM 57 -10-00 FIGURE 2 VOLUME I. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.SDR AWXA200601038Doubler · chafedMCN - MAJOR REPAIR - NR 5926544 - DURING C-15 CHECK DISCOVERED A DOUBLER ON THE R/H OUTBOARD FOREFLAP 95" FROM THE INBOARD END, CHAFFED. MAINTENANCE REMOVED CHAFED DOUBLER ON UPPER SURFACE OF R/H OUTBOARD FOREFLAP 95" FROM INBOARD END AND BONDED FABRICATED DSDR LR7A06073Fitting · crackedDURING SCHEDULED C7 CHECK PER JOB CARD HC5712 FOUND RT OUTBOARD FLAP TRACK FITTING CRACKED AT FS 602, WL 260, OWS 241. REPLACED FITTING IAW SMP583 51-60 & 51-70.SDR 06FDEA2315Attach Fitting · corrodedCORROSION ON FWD ATTACH FITTING AT NR 3 FLAP TRACK.SDR 06FDEA2306Skin · unknownRT WING, OUTBD FLAP AT XOF 722,235 UPPER SKIN HAS A DOUBLER REPAIR (5.5" BY 2.5"). REMOVED AND REPLACED REPAIR IAW SRM 57-00-01 FIG 4. FABRICATED PART IAW SRM 57-00-01 DETAIL PART TRAVELER N01218 AND IAW SRM 57-00-01.SDR 06FDEA2297Skin · unknownLEFT WING OUTBOARD FLAP, LOWER SKIN AT STA XOF 722 HAS AN EXTERNAL DOUBLER REPAIR (23" BY 15"). REMOVED AND REPLACED REPAIR IAW SRM 57-10-00 FIG 85 SHEET 1 2 3 4 VOL 1. FABRICATED PART IAW DETAIL PART TRAVELER N01212-3 DOUBLER IAW SRM 57-10-00 FIG 85 VOL 1.SDR UIEA200600134Flap · chafedLEFT HAND OUTBOARD AFT FLAP END WEAR/CHAFE MARK. RANGING IN DEPTH FROM 0.002' TO 0.013'AND FROM 8"X1" IN DIAMETER TO 2"X1".SDR SWAA062052Skin · debondedDURING SCHEDULED 20Y CHECK, FOUND LT WING INBOARD MID FLAP LOWER SURFACE DISBONDED AT INBOARD SIDE. REPAIRED MID FLAP PER SRM.SDR SWAA062051Flap · delaminatedDURING SCHEDULED 20Y CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED AT LOWER INBOARD SIDE. REMOVED AND REPLACED AFT FLAP PER MM.SDR SWAA062040Structure · crackedDURING SCHEDULED C4 CHECK, FOUND LT WING OUTBOARD FORE FLAP CRACKED ON INBOARD SIDE. REMOVED AND REPLACED FORE FLAP PER MM.SDR SWAA062019Structure · delaminatedDURING SCHEDULED SPV CHECK, FOUND RIGHT WING OUTBOARD FORE FLAP DELAMINATED AT INBOARD SIDE. REMOVED AND REPLACED FORE FLAP PER MM.SDR SWAA062002Bearing · wornNOISE AND VIBRATION SENSED AT MID CABIN DURING FLAP RETRACTION AND EXTENSION, BETWEEN FLAP POSITION 1 AND FLAP POSITION 10. REMOVED AND REPLACED LT INBOARD FORE FLAP INBOARD ROLLER BEARINGS PER MM.SDR UPS06247382Flap Track · corrodedINSPECTION TYPE-C CORROSION IN NR 5 FLAP TRACK HOLE G. CORROSION REMOVED IAW OHM 57-40-01. MPI CARRIED OUT IAW BSOPM 20-20-0 1. BUSHING FABRICATED IAW EO 20065-042-007. STYLUS CAD PLATING CARRIED OUT IAW SOPM 20-42-10. INSTALLED BUSHING IAW SOPM 20-50-03.SDR 06FDEA2261Attach Fitting · brokenON FINAL APPROACH AS FLAPS WERE EXTENDED INCREASINGLY MORE RIGHT WING DOWN AILERON WAS NEEDED TO MAINTAIN WINGS LEVEL FLIGHT YOKE NEEDED TO BE HELD AT APPROX 30 DEGREES RIGHT WING DOWN AS PICTURED. FOUND LEFT WING INBOARD FLAP VANE IN THE RETRACTED POSITION WSDR SWAA061976Skin · crackedDURING SCHEDULED 10Y CHECK, FOUND LT WING OUTBOARD MID FLAP SKIN CRACKED AT T/E. REPAIRED MID FLAP PER SRM.SDR SWAA061973Skin · debondedDURING SCHEDULED SPV CHECK, FOUND RT WING INBOARD FORE FLAP UPPER SURFACE DISBONDED. REPAIRED FORE FLAP PER SRM.SDR PIDR2006002Skin · chafedINSPECTION NOTED A CHAFED AREA ON AN EXISTING SRM ALUMINUM REPAIR DOUBLER ON THE RIGHT WING OUTBOARD FLAP MID-FLAP LEADING EDGE 20 INCHES FROM THE INBOARD END. REPAIRED DAMAGED AREA IN ACCORDANCE WITH PACE AIRLINES REPAIR PROCEDURE REPORT EA 57-145 DATED 05/2
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