JASC 5754
Service difficulty reports · 17,344
Reports filed under 5754 · Leading Edge Devices, 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 = '5754' 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 = '5754' 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 USAA2011010790120Skin · crackedCLT - Q1 - MAJOR REPAIR - CRACKS ON NR 6 SLAT LEADING EDGE SKIN APPROX 40 INCHES OUTBOARD OF INBOARD EDGE. REPLACED NR 6 SLAT IAW JOB CARD 03C40227004 & B737 AMM 57-54-00.SDR FDEA201012314787Skin · damagedLT WING NR 2 SLAT LOWER SURFACE FSS 635 WEDGE PUNCTURED REPAIRED NR2 SLAT LOWER WEDGE PUNCTURE IAW SRM 51-70-10, REPAIR 2. MAJOR REPAIR.SDR IPXA11564060Wedge · chafedINSPECTION TYPE:C2, NR8 SLAT CHAFED LOWER SURFACE T/E AT INBD MAIN TRACK LOCATION. REPAIRED NR8 SLAT T/E WEDGE ASSY IAW SRM 57-43-02-1A1, FIG101, SRM57-43-02-0I-1, SRM51-70-10-2R, SRM57-43-02-1A-1 FIG 101, SHT 3 AND 4, NOTE M.SDR USAA2011010390027Skin · crackedCLT - MAJOR REPAIR - Q1 CHECK - NR 2 SLAT LOWER SKIN CRACKED. REPLACED NR 2 SLAT IAW B737 AMM 2761-21-4.SDR USAA2011010390026Skin · crackedCLT - MAJOR REPAIR - Q1 CHECK - NR 3 SLAT LOWER SKIN CRACKED. REPLACED NR 3 SLAT IAW B737 AMM 2761-21-4.SDR USAA2011010390025Wedge · debondedPHX - MAJOR REPAIR - B1 CHECK - NR4634051, LEFT WING NR 1 SLAT AFT TRAILING EDGE WEDGE HAS AREA OF DISBOND. REPLACED LEFT WING NR 1 SLAT IAW B737 AMM 27-81-21.SDR DALA1053560909Rib · crackedDURING HMV4, FOUND LT WING NR4 SLAT CUTOUT RIB IS CRACKED. ACCOMPLISHED PERMANENT REPAIR IN COMPLIANCE WITH ER/A 472719-14MA AND DWG AMR0957267. TAGGED AND EDGE SEALED REPAIR IAW DPS 900-5-1 NR 04.SDR USAA2010122793242Skin · damagedCLT- MAJOR REPAIR - C4 CHECK - NR 03C40057003/013, RIGHT WING NR 4 SLAT HAS A PREVIOUS REPAIR DISBONDED ON THE UPPER SUFRACE AT THE INBOARD TRAILING EDGE. REPAIRED NR 4 SLAT UPPER SKIN AT THE INBOARD TRAILING EDGE I/A/W B737 SRM 51-70-10.SDR SWAA107934Slat · delaminatedDURING SCHEDULED 26Y CHECK, FOUND NR 2 L/E SLAT DELAMINATED AT UPPER INBD EDGE. REMOVED AND REPLACED SLAT ASSY PER MM.SDR SWAA107931Skin · crackedDURING SCHEDULED 26Y CHECK, FOUND NR 3 L/E SLAT LOWER SKIN CRACKED. REMOVED AND REPLACED SLAT ASSY PER MM.SDR SWAA107930Skin · crackedDURING SCHEDULED 26Y CHECK, FOUND NR 1 L/E SLAT LOWER SKIN CRACKED. REMOVED AND REPLACED SLAT ASSY PER MM.SDR SWAA108009Slat · delaminatedDURING SCHEDULED 26Y CHECK, FOUND NR 2 L/E SLAT DELAMINATED AT UPPER SKIN. REMOVED AND REPLACED SLAT PER MM.SDR DALA1107390175Skin · dentedLT WING NR 6 SLAT OTBD UPPER SURFACE FOUND DENTED AS MARKED. DENTED UPPER SURFACE REPAIRED PERMANENT IAW SRM 57-43-01, FIG 201.SDR SWAA107970Slat · crackedDURING SCHEDULED SPV CHECK, FOUND NR 6 L/E SLAT CRACKED AT OUTBD END. REPAIRED SLAT PER SRM.SDR MALA100204Skin · damagedROUTINE-900, LT SLAT, INBD, HAS DAMAGE TO T/E 87.25" FROM INBD EDGE FROM SCREW STICKING UP. THERE ARE GOUGES IN THE TOP WING SURFACE 18" AFT. COMPLIED WITH BLENDING, NDT AN TOUCH UP IAW REO 690-57-40-007.SDR DALA1102100197Wedge · deformedLT WING NR 4 SLAT WEDGE AREA INBD EDGE FOUND DEFORMED. METAL HOT BOND REPAIR PERFORMED IAW SRM 51-70-10. REPAIR 4, FIG 202 AND SRM 57-43-02 REPAIR 1, FIG 201.SDR SWAA107902Skin · delaminatedDURING SCHEDULED 24Y CHECK, FOUND NR 4 L/E SLAT DELAMINATED AT T/E. REPAIRED SLAT PER SRM.SDR SWAA107901Skin · crackedDURING SCHEDULED 24Y CHECK, FOUND NR 5 L/E SLAT SKIN CRACKED AT T/E. REPAIRED SKIN PER SRM.SDR DALA1102110197Skin · delaminatedRT WING OTBD FLAP L/E MID AREA FOUND DELAMINATED. COMPOSITE PREPREG HOT BOND REPAIR CARRIED OUT AT DELAMINATED AREA IAW SRM 57-53-01, REPAIR 1 AND SRM 51-70-05, FIG 5.SDR SWAA107742Skin · crackedDURING SCHEDULED 24Y CHECK, FOUND LT WING NR 1 SLAT LOWER SKIN CRACKED AT I/B END. REPAIRED SKIN PER SRM.SDR FDEA201012124644Skin · dentedNR4 SLAT T/E OTBD SIDE LWR SURFACE HAS A DENT. REPAIRED NR4 SLAT T/E IAW SRM 51-70-10, SLAT NR4 PN: 114N4005-159, SN : A1-0144, DAMAGE WAS REPAIRED ON LOWER SKIN APPROX 2" FROM OTBD END, FINAL DIMENSION OF REPAIR IS 3" IN DIAMETER. F-5740-146203 GENERATED FSDR SWAA107785Skin · crackedDURING SCHEDULED HC2 CHECK, FOUND RT WING NR 5 SLAT LOWER SKIN CRACKED. REPAIRED SKIN PER SRM.SDR DALA1135001608Skin · delaminatedRT INBD FLAP OTBD L/E FAIRING FOUND DELAMINATED. COMPOSITE PREPREG HOT BOND REPAIR CARRIED OUT AT DELAMINATED AREA AS PER SRM 57-53-01 REPAIR 1 AND SRM 51-70-05 FIG 5.SDR USAA2010121393031Skin · crackedCWF - MAJOR REPAIR - C1 - CRACK ON NR 2 SLAT UPPER SURFACE TRAILING EDGE 16 INCHES FROM INBOARD EDGE OF SLAT. REPAIRED NR 2 SLAT UPPER SURFACE TRAILING EDGE 16 INCHES FROM INBOARD EDGE OF SLAT IAW A330 SRM 57-40-00.SDR USAA2010121393027Wedge · delaminatedCLT - C6 - MAJOR REPAIR - AREA OF DISBONDING ON NR 5 SLAT TRAILING EDGE WEDGE AT CENTER OF UPPER SKIN. REPAIRED NR 5 SLAT TRAILING EDGE WEDGE AT CENTER OF UPPER SKIN IAW B737 SRM 51-70-10.SDR SWAA107665Wedge · delaminatedDURING SCHEDULED 20Y CHECK, FOUND LT WNG NR 2 SLAT O/B TRAILNG EDGE WEDGE DELAMINATED. REPAIRED WEDGE PER SRM.SDR SWAA107660Wedge · delaminatedDURING SCHEDULED 18Y CHECK, FOUND RT WING NR 4 SLAT T/E WEDGE DELAMINATED AT O/B END. REPAIRED WEDGE PER SRM.SDR SWAA107659Wedge · delaminatedDURING SCHEDULED 18Y CHECK, FOUND RT WING NR 5 SLAT T/E WEDGE DELAMINATED AT I/B END. REPAIRED WEDGE PER SRM.SDR AALA20101206TUL04Skin · crackedCRACK FOUND IN COVE SKIN OF THE NUMBER 2 SLAT. DAMAGE IS LOCATED TWO FASTENERS ABOVE THE FIRST AUXILIARY ARM. INSTALLED EXTERNAL DOUBLER PER AARD 57-43-00-4.SDR SWAA107536Wedge · delaminatedDURING SCHEDULED 16Y CHECK, FOUND RT WING NR 5 SLAT O/B CORNER T/E WEDGE DELAMINATED. REPAIRED NR 5 SLAT PER MM.SDR AALA20101202TUL03Skin · corrodedDEEP BLEND ON NUMBER 7 SLAT UPPER SKIN (MKD). REMOVED CORRODED AREA AND INSTALLED FLUSH DOUBLER PER AARD 57-43-00-1.SDR SWAA107434Skin · crackedDURING SCHEDULED 10Y CHECK, FOUND LT WING NR 2 L/E SLAT LOWER SKIN CRACKED. REPAIRED SLAT SKIN PER EA.SDR SWAA107419Skin · delaminatedDURING SCHEDULED 16Y CHECK, FOUND RT WING NR 6 SLAT SKIN O/B EDGE DELAMINATED. REPAIRED SKIN PER SRM.SDR SWAA107380Skin · delaminatedDURING SCHEDULED 16Y CHECK, FOUND RT WING NR 6 SLAT SKIN I/B EDGE DELAMINATED. REPAIRED SKIN PER SRM.SDR SWAA107379Skin · delaminatedDURING SCHEDULED 16Y CHECK, FOUND RT WING NR 4 SLAT SKIN I/B EDGE DELAMINATED. REPAIRED SKIN PER SRM.SDR SWAA107486Wedge · delaminatedDURING SCHEDULED HC2 CHECK, FOUND RT WING NR 5 SLAT I/B END T/E WEDGE DELAMINATED. REPAIRED WEDGE PER SRM.SDR AALA20101201TUL02Skin · corrodedNUMBER 1 SLAT SKIN INBOARD MAIN TRACK ATTACH FITTING AREA CORRODED. REMOVED DAMAGED AREA AND INSTALLED DOUBLER PER AARD 57-43-00-1.SDR SWAA107507Skin · gougedDURING SCHEDULED 2HC2 CHECK, FOUND RT WING NR 6 I/B SLAT CAN LOWER SURFACE GOUGED. REMOVED AND REPLACED SLAT CAN PER SRM.SDR USAA2010120292788Panel · missingPHX - WALKAROUND - MAJOR REPAIR - INSPECTION PANEL MISSING ON FORWARD LEADING EDGE SLAT ON LEFT WING AT SLAT STA 356. REPAIRED FORWARD LEADING EDGE SLAT ON LEFT WING AT SLAT STA 356 IAW B737 SRM 57-43-01.SDR AALA20101129TUL09Slat · damagedRIGHT WING NUMBER 5 SLAT DAMAGED ON LEADING EDGE FROM BIRD STRIKE. INSTALLED FLUSH DOUBLER REPAIR ON RIGHT WING NUMBER 5 SLAT LEADING EDGE PER SRM 57-42-01-2R-5.SDR SWAA107315Skin · delaminatedDURING SCHEDULED HC2 CHECK, FOUND RT WING NR 5 SLAT O/B END UPPER SURFACE DELAMINATED. REMOVED AND REPLACED NR 5 SLAT PER MM.SDR ASMF201012003Skin · crackedCAPTAIN REPORTED A BIRD STRIKE IN RT WING DURING LANDING. ACFT WAS SENT TO THE HANGAR AND MX PERFORMED A BIRD STRIKE INSP IAW 05-51-18 DETECTING CRACK IN THE L/E SLAT NR 6; SO IT WAS REPLACED IAW MM 27-81-54, TESTED CORRECT.SDR USAA2010120192718Wedge · delaminatedCLT - C2 - MAJOR REPAIR - DELAMINATION ON LOWER SIDE OF NR 5 SLAT WEDGE 16 INCHES OUTBOARD FROM INBOARD END. REPAIRED NR 5 SLAT WEDGE IAW B757 SRM 51-70-10.SDR USAA2010112992680Slat · delaminatedPHX - MAJOR REPAIR - B CHECK - 2 X 6.25 INCHES DELAMINATED SECTION 18 INCHES FROM OUTBOARD END OF NR 1 SLAT. REPLACED NR 1 SLAT IAW B737 AMM 27-81-21 AND 27-81-00-5.SDR USAA2010112992679Slat · delaminatedPHX - MAJOR REPAIR - B CHECK - 20 X 3 INCHES AND 6 X 5.5 INCHES DELAMINATED CENTER SECTION OF NR 3 SLAT. REPLACED NR 3 SLAT IAW B737 AMM 27-81-21 AND 27-81-00-5.SDR FDEA201011264493Skin · damagedRT WING NR 10 L/E SLAT T/E LOWER SURFACE PUNCTURED. REPAIRED RT WING NR 10 SLAT T/E WEDGE IAW SRM 51-70-10. MAJOR REPAIR.SDR FDEA201011264491Skin · delaminatedNR5 SLAT T/E LOWER SURFACE OTBD CORNER SIDE DELAMINATED. REPAIRED NR 5 SLAT IAW SRM 51-70-06. MAJOR REPAIR.SDR FDEA201011234469Skin · corrodedRT WING NR9 L/E SLAT, OTBD AREA, CORROSION RUNS UNDER BOTH FASTENERS. ACCOMPLISHED EA F-5740-141230; WING L/E SLAT NR9, NOSE SKIN CORROSION REPAIR. REF. FAA FORM 8100-9, DATED 11/12/2010. REPAIR ACCOMPLISHED ON SLAT ASSY. PN; 141N4003- 174, SN; A2-0122. COSDR UALA2010111904275Wedge · delaminatedNR 9 SLAT WEDGE DELAMINATED AT IB TRACK AREA. TEMP INJECTION REPAIR ACP AND ULTRASONIC VERIFIED NO DISBOND. REMOVED THE SLAT, BONDING REPAIRED PER SRM. TOUCH UP PAINT PER AMM. REINSTALLED THE SLAT PER AMM. ADJUSTED AND OPS TEST OKAY.SDR FDEA201011184421Wedge · chafedNR 6 SLAT T/E WEDGE UNDER SKIN HAS CHAFE MARKS, REPAIRED NR6 SLAT T/E IAW SRM 51-70-10 IAW SRM 57-43-02. DAMAGE WAS LOCATED AT STA 177.5, APPROX 3" FWD OF T/E. REF EA F-5750-143211. CLASSIFIED CAT "A" MAJOR REPAIR.
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