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 2003UALA00163Wedge · damagedTRAILING EDGE WEDGE, SLAT #1A, DAMAGED IN TRANSIT. MAJOR REPAIR ACCOMPLISHED. WING SLAT #1A REPAIRED.SDR CA030419002Skin · cracked(CAN) CRACKS FOUND IN LT WING LEADING EDGE MID SECTION. CRACK IS APPROX. 10 - 15 CM VERTICAL AND IS CONNECTED TO THE RIVETS IN THE MIDDLE OF THE L.E. ASSY.IN ADDITION TO THIS CRACK, 2 SMALLER CRACKS WERE FOUND ON EACH SIDE OF THIS CRACK, BOTH OF THESE CRACKS SDR DHL2003804910Frame · crackedLT WING CTR L/E FORMER UPPER PART WITH 1.000 INCH CRACK AT STA XFS 460.250. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP DRILLED CRACK IAW SRM 57-2-0 PG 9-10. FABRICATED DOUBLER ANGLE (2024-T3 AL0.040) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IASDR DHL2003804911Frame · crackedLT WING- CTR L/E FORMER CRACKED 1.000, STA XFS 490.000. REMOVED FASTENERS IAW SRM 51-1-21 PG 1, STOP DRILLED CRACK AT STA XFS 490.000 IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER (2024-T3 AL0.040) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SDR DHL2003804883Frame · crackedLT WING CTR L/E FORMER UPPER PART WITH 1.000 INCH CRACK AT STA XFS 496.250. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP DRILLED CRACK AT STA XFS 496.250 IAW SRM 57-2-0 PG 9-10. FABRICATED DOUBLER ANGLE (2024-T3AL 0.040) IAW SRM 57-2-0 PG 9-10. CLEANED, TRSDR AWXA200300136Slat · crackedYVR - MAJOR REPAIR - DURING C-14 CHECK 5 EACH CRACKS WERE FOUND EMANATING FROM FASTENER HOLES ON THE LOWER SURFACE OF THE NO. 5 SLAT. MAINTENANCE REMOVED AND REPLACED THE NO. 5 SLAT ASSEMBLY IAW BMM 27-81-21.SDR 2003F00460Structure · corrodedAT C-CHECK, FOUND RIGHT WING LEADING EDGE NR 4 KRUEGER FLAP BULLNOSE WITH AREAS OF CORROSION ON INBOARD SIDE WS 130.7. (M)SDR DHL2003804899Frame · crackedLT WING CTR L/E FORMER LWR PART WITH CRACK AT STA XFS 297.500. STOP DRILLED CRACK IAW SRM 57-2-0 PG 9-10. FABRICATED DOUBLER ANGLE (2024-T3AL 0.040) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED DOUBLER ANGLE INNER SIDE IAW SRM 51-1-8B. INSTALLED DOUSDR DHL2003804897Frame · crackedLT WING CTR L/E FORMER UPPER PART WITH 1.000 AT STA XFS 379.000. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP DRILLED CRACK IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER (2024-T3 0.032) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW 51-1-8B. ISDR DHL2003804902Frame · crackedLT WING CTR L/E FORMER UPPER PART WITH 1.000 INCH CRACK AT STA XFS 366.500. REMOVED FASTENERS IAW SRM 51-1-21 PG 1, STOP DRILLED CRACK IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER (2024-T3 AL0.040) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAWSDR DHL2003804903Frame · crackedREMOVED FASTENERS IAW SRM 51-1-21 PG 1, STOP DRILLED CRACK IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER (2024-T3 AL0.040) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER WITH NEW FASTENERS ON LT WING CTR L/E SDR DHL2003804901Frame · crackedLT WING CTR L/E FORMER AT STA XFS 354.000 WITH 1.500 INCH CRACK. REMOVED FASTENERS IAW SRM 51-1-21 PG 1, STOP DRILLED CRACK IAW SRM 57-2-0 PG 9-10. FABRICATED DOUBLER ANGLE (2024-T3 AL0.040) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED DOUBLER ANGLE SDR DHL2003804518Frame · crackedLT WING I/B L/E FORMER CRACKED 1 IN STA XFS 603.750. REMOVED FASTNERS PER SRM 51-1-21 PG 1.STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10.FABRICATED ANGLE DOUBLER (2024.T3 AL 0.032)PER SRM 57-2-0 PG 9-10.CLEANED TREATED AND PRIMED PER SRM 51-1-8B. INSTALLED ANGLSDR P5CA0300745Seal · crackedCRACK FOUND WHILE CHECKING FLAP TO PYLON SEAL ON BACK SIDE OF NR 16 KRUEGER FLAP, RT WING, APPROX 4 INCHES INBOARD OF OUTBOARD SEAL. CRACK RUNS FROM LWR EDGE UP 12 INCHES. NR 16 KRUEGER FLAP PANEL REMOVED AND REPLACED IAW MM 27-81-01.SDR 2003UALA00133Structure · delaminatedTRAILING EDGE WEDGE SLAT NR 5 DELAMINATED. MAJOR REPAIR ACCOMPLISHED. REPAIRED RIGHT T/E IN SHOP.SDR 2003F00467Structure · crackedAT C-CHECK, FOUND CRACK ON NR 4 KRUEGER FLAP, INBOARD EDGE. (M)SDR 2003F00462Structure · crackedAT C-CHECK, FOUND CRACK ON UPPER TRAILINGE EDGE, NR 6 SLAT WS 629. TRIMMED OUT DAMAGED AREA OF TRAILING EDGE. FOUND TO BE WITHIN LIMITS. ALODINED BARE METAL AT NR 6 SLAT TRAILING EDGE WL 629. (M)SDR AWXA200300134Slat · delaminatedYVR - MAJOR REPAIR - DURING C-14 CHECK THE NO. 1 SLAT WAS FOUND DELAMINATED ON THE TRAILING EDGE WEDGE. MAINTENANCE REMOVED AND REPLACED THE NO. 1 SLAT ASSEMBLY IAW BMM 27-81-21.SDR DL767030104Wedge · debondedRIGHT WING OUTBOARD SLAT T/E WEDGE DISBONDED. REPAIRED PER ER/A 418206-14.SDR DL767030103Wedge · debondedLEFT WING OUTBOARD SLAT T/E WEDGE DISBONDED. REPAIRED PER ER/A 418205-14.SDR DHL2003804905Skin · delaminatedLT WING T/E TOP EXTERIOR SKIN SURFACE DELAMINATED (STA 5.000-47.000). CUT OUT DAMAGED AREA IAW SRM 57-2-3 PG 4 PAR 1. FABRICATED FILLER AND DOUBLER (7075-T6 AL0.032) IAW SRM 57-2-3 PG 4 PAR 11. CLEANED, TREATED AND PRIMED FILLER AND DOUBLER INNER SURFACE IASDR UPS03240102Seal · crackedINSPECTION TYPE: C&SI, NR 6 & 8 LEADING EDGE SLAT CRACK FOUND AT I/B END UNDER PORK CHOP SEAL. REPAIR CARRIED OUT IAW SRM 57-50-3 FIG 5.SDR DHL2003804874Frame · crackedRT WING CTR L/E FORMER UPPER PART AT STA XFS 372.000 WITH .500. REMOVED FASTENERS IAW SRM 51-1-21 PG 1, STOP DRILLED .500 CRACK ON CENTER L/E FORMER UPPER PART IAW SRM 57-2-0 PG 9-10. FABRICATED A DOUBLER ANGLE 2024T3 AL.032 IAW SRM 57-2-0 PG 9-10. CLEANED,SDR DHL2003804502Frame · crackedRT WING CENTER L/E FORMER UPPER PART CRACKED 1/2 IN AT XFS 422.750. REMOVED FASTENERS PER SRM 51-1-21 PG 1. STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER (2024-T3 AL 0.032) PER SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED PER SRM 5SDR UPS03540038Slat Track · damagedINSPECTION TYPE: 2C, NR 6 SLAT I/B AUX TRACK ON WING SIDE DAMAGED BY NR 2 ENGINE GENERATOR CABLES. GENERATOR CABLES DAMAGED AND TAI DUCT BUNRT THROUGH. REMOVED AND REPLACED SLAT TRACK PER M/M. SPLICED WIRES PER SRM, REPLACED TAI DUCT PER M/M.SDR DHL2003804517Frame · crackedRT WING CENTER L/E FORMER UPPER PART CRACKED 1/2 IN AT XFS 434.000. REMOVED FASTNERS PER SRM 51-1-21 PG 1.STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10. FABRICATED REINFOCING ANGLE(2024.T3 AL 0.032)PER SRM 57-2-0 PG 9-10.CLEANED TREATED AND PRIMED PER SRM 51-1-8SDR DHL2003804511Frame · crackedRT WING CENTER L/E FORMER UPPER PART CRACKED AT XFS 454.000. REMOVED FASTNERS PER SRM 51-1-21 PG 1.STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10. FABRICATED REINFOCING ANGLE (2024.T3 AL 0.032) PER SRM 57-2-0 PG 9-10.CLEANED TREATED AND PRIMED PER SRM 51-1-8B. INSSDR DHL2003804510Frame · crackedRT WING CENTER L/E FORMER LOWER PART CRACKED AT 1/2 IN STA XFS 460.000. REMOVED FASTNERS PER SRM 51-1-21 PG 1.STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10.FABRICATED REINFOCING ANGLE(2024.T3 AL 0.032)PER SRM 57-2-0 PG 9-10.CLEANED TREATED AND PRIMED PER SRM 51-1-SDR SWAA030107Skin · crackedDURING SCHEDULED D CHECK, FOUND NR 6 LE SLAT LOWER SKIN CRACKED .5 INCHES. SLAT SKIN CRACK REPAIRED PER SRM.SDR DHL2003804506Frame · crackedLT WING CENTER L/E FORMER CRACKED 1 INCH AT STA XFS 483.750 (UPPER). REMOVED FASTENERS PER SRM 51-1-21 PG 1. STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10. FABRICATED REINFORCING ANGLE (2024-T3 AL 0.032) PER SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED PER SDR DHL2003804503Frame · crackedLT WING CTR L/E FORMER UPPER PART WITH 1 INCH CRACK AT STA XFS 416.500. REMOVED FASTENERS PER SRM 51-1-21 PG 1. STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10. FABRICATED REINFORCEMENT ANGLE (2024-T3 AL 0.032) PER SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMEDSDR DHL2003804500Frame · crackedRT WING L/E INNER FORMER CRACKED 1/2 IN AT XFS 598.000. REMOVED FASTNERS PER SRM 51-1-20D PG 21,STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10.FABRICATED REINFOCING ANGLE(2024.T3 0.032. CLEANED, TREATED AND PRIMED PER SRM 51-1-8 B.INSTALLED REINFORCING ANGLE PER SSDR DHL2003804525Frame · crackedLT WING I/B L/E FORMER CRACKED 1 IN STA XFS 628.758. REMOVED FASTNERS PER SRM 51-1-21 PG 1.STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10.FABRICATED REINFOCING ANGLE (2024.T3 AL 0.032) PER SRM 57-2-0 PG 9-10.CLEANED TREATED AND PRIMED PER SRM 51-1-8B. INSTALLED ASDR DHL2003804524Frame · crackedLT OUTER WING L/E FORMER UPPER PART HAS 1 IN CRACK AT STA XFS 778.750. REMOVED FASTNERS PER SRM 51-1-21 PG 1. STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10.FABRICATED REINFOCING ANGLE (2024.T3 AL 0.032) PER SRM 57-2-0 PG 9-10.CLEANED TREATED AND PRIMED PER SRM 5SDR DHL2003804523Frame · crackedLT WING I/B L/E FORMER CRACKED 1 IN STA XFS 616.250 (LT O/B WING). REMOVED FASTNERS PER SRM 51-1-21 PG 1.STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10.FABRICATED REINFOCING ANGLE(2024.T3 AL 0.032)PER SRM 57-2-0 PG 9-10.CLEANED TREATED AND PRIMED PER SRM 51-1-8B.SDR DHL2003804522Frame · crackedLT WING I/B L/E FORMER CRACKED 1 IN STA XFS 641.250. REMOVED FASTNERS PER SRM 51-1-21 PG 1.STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10.FABRICATED REINFOCING ANGLE(2024.T3 AL 0.032)PER SRM 57-2-0 PG 9-10.CLEANED TREATED AND PRIMED PER SRM 51-1-8B. INSTALLED ANGSDR DHL2003804521Frame · crackedLT WING I/B L/E FORMER CRACKED 1 IN STA XFS 622.500. REMOVED FASTNERS PER SRM 51-1-21 PG 1.STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10.FABRICATED REINFOCING ANGLE (2024.T3 AL 0.032) PER SRM 57-2-0 PG 9-10. CLEANED TREATED AND PRIMED PER SRM 51-1-8B. INSTALLEDSDR DHL2003804520Frame · crackedLT OUTER WING L/E FORMER UPPER PART HAS A 1 IN CRACK AT STA XFS 797.500. REMOVED FASTNERS PER SRM 51-1-21 PG 1.STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10.FABRICATED REINFOCING ANGLE (2024.T3 AL 0.032) PER SRM 57-2-0 PG 9-10.CLEANED TREATED AND PRIMED PER SRM SDR DHL2003804519Frame · crackedLT WING I/B L/E FORMER CRACKED 1 IN STA XFS 653.750. REMOVED FASTNERS PER SRM 51-1-21 PG 1.STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10.FABRICATED REINFOCING ANGLE(2024.T3 AL 0.032)PER SRM 57-2-0 PG 9-10.CLEANED TREATED AND PRIMED PER SRM 51-1-8B. INSTALLED ANGLSDR DHL2003804516Frame · crackedLT WING I/B L/E FORMER CRACKED 1 IN AT XFS 610.000 (LT O/B WING). REMOVED FASTNERS PER SRM 51-1-21 PG 1.STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10.FABRICATED REINFOCING ANGLE (2024.T3 AL 0.032) PER SRM 57-2-0 PG 9-10.CLEANED TREATED AND PRIMED PER SRM 51-1-8B.SDR DHL2003804515Frame · crackedLT OUTER WING L/E FORMER LOWER PART WITH 1 IN CRACK AT STA XFS 797.500. REMOVED FASTNERS PER SRM 51-1-21 PG 1.STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10.FABRICATED REINFOCING ANGLE (2024.T3 AL 0.032) PER SRM 57-2-0 PG 9-10.CLEANED TREATED AND PRIMED PER SRM 51-SDR DHL2003804513Frame · crackedLT OUTER WING L/E FORMER UPPER PART WITH A 1 IN CRACK AT STA XFS 785.000. REMOVED FASTNERS PER SRM 51-1-21 PG 1.STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10.FABRICATED REINFOCING ANGLE(2024.T3 AL 0.032)PER SRM 57-2-0 PG 9-10.CLEANED TREATED AND PRIMED PER SRM 51-SDR DHL2003804512Frame · crackedLT OUTER WING L/E FORMER UPPER PART WITH 1 IN CRACK AT STA XFS 760.000. REMOVED FASTNERS PER SRM 51-1-21 PG 1.STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10.FABRICATED REINFOCING ANGLE (2024.T3 AL 0.032) PER SRM 57-2-0 PG 9-10. CLEANED TREATED AND PRIMED PER SRM 51SDR DHL2003804509Frame · crackedLT OUTER WING L/E FORMER UPPER PART CRACKED 1 IN AT STA XFS. 722.500. REMOVED FASTNERS PER SRM 51-1-21 PG 1.STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10.FABRICATED REINFOCING ANGLE (2024.T3 AL 0.032)PER SRM 57-2-0 PG 9-10. CLEANED TREATED AND PRIMED PER SRM 51-1-SDR DHL2003804507Frame · crackedLT OUTER WING L/E FORMER UPPER PART HAS A 1 INCH CRACK AT STA XFS 772.500. REMOVED FASTENERS PER SRM 51-1-21 PG 1. STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER (2024 T3 AL 0.032) PER SRM 57-2-0. CLEANED, TREATED AND PRIMED PER SRM SDR DHL2003804501Frame · crackedLT OUTER WING L/E FORMER UPPER PART WITH 1 INCH CRACK AT STA XFS 766.500. REMOVED FASTENERS PER SRC2 PG 1. STOP DRILLED CRACK PER SRM 57-20 PG 9-10. FABRICATED ANGLE DOUBLER (2024-T3 AL 0.032) PER SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED PER SRM 51-SDR DHL2003804514Frame · crackedLT WING INBD L/E FORMER CRACKED 1 IN AT STA XFS 597.500 (LT O/B WING). REMOVED FASTNERS PER SRM 51-1-21 PG 1.STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10.FABRICATED REINFOCING ANGLE(2024.T3 AL 0.032)PER SRM 57-2-0 PG 9-10.CLEANED TREATED AND PRIMED PER SRM 51-1-8SDR DHL2003804505Frame · crackedRT WING CENTER L/E FORMER UPPER PART CRACKED 1 INCH AT XFS 483.750. REMOVED FASTENERS PER SRM 51-1-21 PG 1. STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER (2024.T3AL 0.032) PER SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED PER SRM 51SDR EVA92012401Stringer · crackedCRACK FOUND ON RT & LT WING FIXED LE STRINGER DOUBLER AT STA XOS 906, INSTALLATION OF INTERNAL DOUBLERS AT STA XOS906 WILL REDUCE THE POTENTIALITY OF CRACK IN THIS SECTION.SDR DHL2003804504Frame · crackedLT WING CTR L/E FORMER PART WITH 2 INCH CRACK AT STA XFS 521.250. STOP DRILLED CRACK PER SRM 57-2-0. FABRICATED DOUBLER ANGLE (2024.T3 AL 0.063) PER SRM PG 9-10. CLEANED, TREATED AND PRIMED PER SRM 51-1-8B. INSTALLED DOUBLER PER SRM 57-2-0 PG 9-10.
Back to JASC 5754