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.
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 AWXA200401067Wedge · debondedDURING C-14 CHECK, FOUND THE LT INBOARD MID FLAP WEDGE DISBONDED AT THE OUTBOARD END. MAINTENANCE CUTOUT DISBONDED AREA ON LT INBOARD MID FLAP WEDGE AT OUTBOARD END FROM WBL 170.5 TO WBL 175.0; FABRICATED FILLER AND REPAIR DOUBLER; BONDED REPAIR PARTS TO FLAPSDR 04FDEA02654Bracket · corrodedRT WING, I/B FLAP O/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, O/B BORE FOUND CORRODED. RT WING, I/B FLAP O/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, O/B BORE CORROSION REMOVED AND FOUND EXCEEDED LIMITS AS PER CMM 57-52-03 PAGES 442 TO 443, ORIGINAL DIAMETER=1.1SDR 04FDEA02653Bracket · corrodedRT WING, I/B FLAP O/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, I/B BORE FOUND CORRODED. RT WING, I/B FLAP O/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, I/B BORE CORROSION REMOVED AND FOUND EXCEEDED LIMITS AS PER CMM 57-52-03 PAGES 442 TO 443, ORIGINAL DIAMETER=1.1SDR 04FDEA02652Bracket · corrodedLEFT WING, I/B FLAP O/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, O/B BORE FOUND CORRODED. LEFT WING, I/B FLAP O/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, O/B BORE CORROSION. REMOVED AND FOUND EXCEEDED LIMITS AS PER CMM 57-52-03 PAGES 442-443, ORIGINAL DIAMETER=1.SDR 04FDEA02656Stop Fitting · crackedLT WING OUTBOARD FLAP INBOARD STOP FITTING FOUND CRACKED. REMOVED CRACKED FITTING AS PER SRM 51-31-01 VOL II AND INSTALLED NEW FITTING AT LEFT HAND WING OUTBOARD FLAP INBOARD AS PER SRM 51-33-01 VOL II.SDR 04FDEA02655Stop Fitting · crackedRT WING OUTBOARD FLAP INBOARD STOP FITTING FOUND CRACKED. REMOVED STOP FITTING AS PER SRM 51-31-01 VOL II AND INSTALLED NEW FITTING AT RIGHT HAND WING OUTBOARD FLAP INBOARD AS PER SRM 51-33-01 VOL II.SDR 04FDEA02651Hinge Fitting · corrodedLEFT WING INBOARD FLAP, OUTBOARD HINGE SUPPORT, PIVOT ATTACH POINT, INBOARD BORE PITTED AND CORRODED. REMOVED CORROSION, ORIGINAL DIAMETER 1.240, FINAL DIAMETER 1.2819, MATERIAL REMOVED .0419 IS BEYOND LIMITS. FABRICATED OVERSIZED BUSHING, INSTALLED AND HONESDR 04FDEA02650Hinge Fitting · corrodedRIGHT WING INBOARD FLAP OUTBOARD HINGE SUPPORT, PIVOT ATTACH POINT, INBOARD BORE CORRODED. REMOVED CORROSION, ORIGINAL DIAMETER 1.1885 FINAL DIAMETER 1.3817, FOUND TO BE OUT OF LIMITS. FABRICATED OVERSIZED BUSHING, INSTALLED AND HONED TO FINAL INSIDE DIAMETESDR 04FDEA02639Roller · corrodedLEFT WING INBOARD FLAP INBOARD TRACK 1 EACH AFT UPPER SMALL ROLLER IS PITTED. REMOVED AND REPLACED LEFT HAND INBOARD FLAP INBOARD TRACK AFT UPPER SMALL LOAD ROLLER IAW FEDEX EA> 8-5750-81449. ORIGINAL COPY OF EA 8-5750-81449 IS ATTACHED TO FEDEX N/R N00910, SDR 04FDEA02633Fitting · crackedLT WING O/B FLAP STOP FITTING FOUND CRACKED. LEFT WING O/B FLAP STOP FITTING REMOVED AND REPLACED AS PER SRM 51-33- 01 VOL II.SDR 04FDEA02623Bracket · corrodedRT WING, O/B FLAP I/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, I/B BORE FOUND CORRODED. RT WING, O/B FLAP I/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, I/B BORE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4, ORIGINAL DIAMETER=1.093 INCH, FINAL DIAMETER=1.125 INSDR 04FDEA02622Bracket · corrodedLT WING, O/B FLAP I/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, O/B BORE FOUND CORRODED. LEFT WING, O/B FLAP I/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, O/B BORE CORROSION. REMOVED AS PER CMM 20-11-02 PAGES 2-4 ORIGINAL DIAMETER=1.062 INCH, FINAL DIAMETER=1.077 INSDR 04FDEA02621Bracket · corrodedLT WING, O/B FLAP I/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, I/B BORE FOUND CORRODED. LT WING, O/B FLAP I/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, I/B BORE CORROSION. REMOVED AS PER CMM 20-11-02 PAGES 2-4 ORIGINAL DIAMETER=1.093 INCH, FINAL DIAMETER=1.096 ISDR 04FDEA02620Bracket · corrodedLT WING, O/B FLAP I/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, O/B HOLE SPOTFACE FOUND CORRODED. SNRM N0448: LT WING, O/B FLAP I/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, O/B HOLE SPOTFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4 ORIGINAL THICKNESS=0.514 INSDR 04FDEA02619Bracket · corrodedLT WING , O/B FLAP I/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, I/B HOLE SPOTFACE FOUND CORRODED. LEFT WING, O/B FLAP I/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, I/B HOLE SPOTFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4 ORIGINAL THICKNESS=0.503 INCH, MATESDR 04FDEA02618Bracket · corrodedLEFT WING - O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, O/B HOLE SPOT FACE FOUND CORRODED. LEFT WING - O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, O/B HOLE SPOT FACE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4. ORIGINAL THICKNESS=0.39SDR 04FDEA02617Bracket · corrodedLEFT WING - O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, I/B HOLE SPOT FACE FOUND CORRODED. LEFT WING - O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, I/B HOLE SPOT FACE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4. ORIGINAL THICKNESS=0.400 SDR 04FDEA02615Bracket · corrodedLEFT WING - O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, I/B BORE FOUND CORRODED. LEFT WING - O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, I/B BORE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4 ORIGINAL DIAMETER=1.062 INCH, FINAL DIAMETER=1.SDR 04FDEA02616Bracket · corrodedLEFT WING - O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, O/B BORE FOUND CORRODED. LEFT WING - O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, O/B BORE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4. ORIGINAL DIAMETER=1.062 INCH, FINAL DIAMETER=SDR SWAA042580Skin · delaminatedDURING SCHEDULED C2 CHECK, FOUND LT WING OUTBOARD T/E FOREFLAP DELAMINATED. REMOVED AND REPLACED OUTBOARD T/E FOREFLAP PER MM.SDR 04FDEA02630Hinge · corrodedRT WING- OB FLAP IB HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, OB BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.SDR 04FDEA02629Hinge · corrodedRT WING-OB FLAP IB HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, IB BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.SDR 04FDEA02628Hinge · corrodedSNRM N0456: RT WING- OB FLAP IB HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, OB HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.SDR 04FDEA02627Hinge · corrodedSNRM N0455: RT WING- OB FLAP IB HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, IB HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.SDR 04FDEA02626Hinge · corrodedSNRM N0454: RT WING- OB FLAP IB HINGE (FLAP SIDE), PIVOT ATTACH LUG, OB BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.SDR 04FDEA02625Hinge · corrodedSNRM N0453: RT WING- OB FLAP IB HINGE (FLAP SIDE), PIVOT ATTACH LUG, IB HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.SDR 04FDEA02624Hinge · corrodedRT WING-OB FLAP IB HINGE (FLAP SIDE), PIVOT ATTACH LUG, OB HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.SDR 04FDEA02614Hinge · corrodedSNRM N0442: LT WING, OB FLAP OB HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, OB BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.SDR 04FDEA02613Hinge · corrodedLT WING, OB FLAP OB HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, IB BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.SDR 04FDEA02612Hinge · corrodedLT WING, OB FLAP OB HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, OB HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.SDR 04FDEA02611Hinge · corrodedLT WING, OB FLAP OB HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, IB HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.SDR 04FDEA02610Hinge · corrodedLT WING, OB FLAP OB HINGE (FLAP SIDE), PIVOT ATTACH LUG, OB HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.SDR 04FDEA02609Hinge · corrodedLT WING - OB FLAP OB HINGE (FLAP SIDE), PIVOT ATTACH LUG, IB HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.SDR 04FDEA02608Hinge · corrodedLT WING, OB FLAP OB HINGE (FLAP SIDE), PIVOT ATTACH LUG, OB BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.SDR 04FDEA02607Hinge · corrodedLT WING, OB FLAP OB HINGE (FLAP SIDE), PIVOT ATTACH LUG, IB BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.SDR MALA040709Hinge · wornDURING C1 INSPECTION IN YYC, RT WING FLAP TAB NR 1 HINGE HAS WEAR MARKS ON SKIN BY HINGE COVER. MAINTENANCE REPAIRED IAW EO NR A57073. AIRCRAFT RETURNED TO SERVICE 9/14/04. REFER TO 409 CARD NR 187019 FOR ADDITIONAL INFORMATION.SDR 04FDEA02604Bracket · corrodedRT WING O/B FLAP O/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, O/B BORE FOUND CORRODED. RT WING O/B FLAP O/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, O/B BORE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4, ORIGINAL DIAMETER=1.062 INCH, FINAL DIAMETER=1.094 INSDR 04FDEA02603Bracket · corrodedRT WING O/B FLAP O/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, I/B BORE FOUND CORRODED. RT WING O/B FLAP O/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, I/B BORE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4, ORIGINAL DIAMETER=1.093 INCH, FINAL DIAMETER=1.125 INSDR 04FDEA02602Bracket · corrodedRT WING O/B FLAP O/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, O/B HOLE SPOTFACE FOUND CORRODED. RT WING O/B FLAP O/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, O/B HOLE SPOTFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4, ORIGINAL THICKNESS=0.502 INCH, MATERISDR 04FDEA02601Bracket · corrodedRT WING O/B FLAP O/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, I/B HOLE SPOTFACE FOUND CORRODED. RT WING O/B FLAP O/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, I/B HOLE SPOTFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4, ORIGINAL THICKNESS=0.497 INCH, MATERISDR 04FDEA02600Bracket · corrodedRT WING O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, O/B HOLE SPOTFACE FOUND CORRODED. RT WING O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, O/B HOLE SPOTFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4, ORIGINAL THICKNESS=0.408 INCH, MASDR 04FDEA02599Bracket · corrodedRT WING O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, I/B HOLE SPOT FACE FOUND CORRODED. RT WING O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, I/B HOLE SPOTFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4, ORIGINAL THICKNESS=0.392 INCHSDR 04FDEA02598Bracket · corrodedRT WING O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, O/B BORE FOUND CORRODED. RT WING O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, O/B BORE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4, ORIGINAL DIAMETER=1.062 INCH, FINAL DIAMETER=1.22SDR 04FDEA02597Bracket · corrodedRT WING O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, I/B BORE FOUND CORRODED. RT WING O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, I/B BORE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4, ORIGINAL DIAMETER=1.062 INCH, FINAL DIAMETER=1.22SDR SWAA042565Skin · delaminatedDURING SCHEDULED C3 CHECK, FOUND RT WING AFT INBOARD T/E FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR USAA050822Skin · wornMID FLAP L/E, 24 INCHES WORN. IB 24 INCHES ON THE LT OB MID FLAP L/E AT IB END. INSTALLED DOUBLER IAW SRM 57-53-01, FIG 208.SDR QXEA200400658Flap Track · crackedPDX - LEFT HAND NACELLE NR 3 OUTBOARD FLAP TRACK MOUNTING SUPPORT BEAM HAS A 1 INCH CRACK ALONG TOP ATTACH FLANGE, APPROXIMATELY 7 INCHES FROM AFT END. REPAIRED IAW HORIZON AIR EA 6-54-310 AND R/D 8/4-54-201.SDR 04FDEA02596Hinge · gougedCOMPLY WITH EA 8-5754-80608, WINGS, LEFT INBD FLAP, OUTBD HINGE BRACKET, UPSTOP MOUNT HOLE REPAIR P/N ARC 0154. COMPLIED WITH E.A.8-5754-80608.SDR 04FDEA02595Hinge · corrodedCOMPLY WITH EA 8-5750-80598, WINGS LT INBD FLAP INBD MOUNTED HINGE PIVOT BORE CORROSION REPAIR P/N ARC2512. COMPLIED WITH EA 8-5750-80598.SDR 04FDEA02594Hinge · corrodedWINGS, RT INBD FLAP AFT HINGE ASSY ARC2512,PIVOT BORE CORROSION. COMPLIED WITH E.A.8-5750-80602.
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