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 DHL2003801031Frame · crackedLT WING CTR L\E FORMER CRACKED 1.000 INCH AT XS 454.000. REMOVED FASTENERS IAW SRM 51-121 PG 1. FABRICATED REINFORCING ANGLE (2024-T3 AL0.040) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED REINFORCING ANGLE WITH NEW FASTENESDR SWAA030813Skin · delaminatedDURING SCHEDULED 1/4D CHECK, FOUND NR 5 L/E SLAT OUTBOARD UPPER T/E WEDGE DELAMINATED. REPAIRED NR 5 L/E SLAT PER SRM.SDR UPS03440618Rib · corrodedINSPECTION TYPE: C LHW, NR 9 VC FLAP O/B I/B ROTARY ACTUATOR SUPPORT RIB MOUNT BOLT HOLES BORE AREA FOUND CORROSION AT HOLE NR 3 ( VIEW FROM I/B ). RIB MOUNT BOLT HOLE BORE EXCEED LIMIT AFTER CORR BLEND OUT. SUPPORT RIB REPLACED AS PER SRM 51-10-01 PAGE 8SDR UPS03840447Rib · crackedINSPECTION TYPE: C1, RT WING L/E UPPER RIB IS CRACKED AT FASTENER END AT XFS 826.750. STOP DRILLED CRACK, NDT VERIFIED STOP DRILL TERMINATES CRACK, FABRICATED AND INSTALLED STACK ANGLE DOUBLER REPAIR IAW SRM 57-2-0 FIG 2.SDR CH1A200395033Skin · crackedRT WING LE CRACKED IN UPPER SURFACE SKIN AT NR 5 SLAT INBD UPHOOK CUTOUT AFT ENDSDR CH1A200395019Skin · crackedRT WING LE CRACK IN UPPER SURFACE SKIN AT NR 5 SLAT INBD.UPHOOK CUTOUT, AT AFT END.SDR CH1A200395011Rib · crackedL/E SLAT NR 5 OUTBD SIDE OF ACTUATOR ATTACH POINT TO SLAT, CRACK IN RIB FWD END.SDR DHL2003801032Frame · crackedLT WING CTR L/E FORMER WITH 2.000 INCH CRACK AT STA XOLDI 6.225. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP DRILLED 2.000 CRACK ON LT WING CTR L/E IAW SRM 57-2-0 PG 9-10. FABRICATED A DOUBLER ANGLE (STEEL-301 0.25H-0.032) IAW SRM 57-2-0 PG 9-10. CLEANED,SDR DHL2003801060Frame · crackedLT WING CTR L/E FORMER CRACKED 0.500 INCH AT XFS 354.000. REMOVED FASTENERS IAW SRM 51-1-21 PG 1 AND SRM 51-1-20D PG 21. STOP DRILLED CRACK IAW SRM 57-2-0 PG 9-00. FABRICATED REINFORCING ANGLE (2024-T3 AL0.032) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND SDR 2003FA0000528Skin · corrodedA/C RT WING OB LE SKIN WAS SLIGHTLY DAMAGED DURING TAXING. ACCOMPLISHED REPAIR OF LE AND A/C RETURNED SERVICE. IN COURSE OF INSP, FOUND EXTENSIVE CORROSION ON RT WING SPAR CAP STIFFNER BEHIND COPILOTS SEAT. CORROSION WAS SO EXTENSIVE THAT SPAR CAP STIFFNER SDR DHL2003801054Frame · crackedRT WING CTR L/E FORMER WITH 0.500 INCH CRACK IN STA XFS 466.500. 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 IAW SRM 51-1-SDR DHL2003801053Frame · crackedRT WING CTR L/E FORMER WITH 0.500 INCH CRACK IN 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 IAW SRM 51-1-SDR DHL2003801059Frame · crackedLT WING - CTR L/E FORMER CRACKED 0.500 INCH AT XS 484.895. STOP DRILLED CRACK IAW SRM 57-2-0 PG 9-10. FABRICATED REINFORCING ANGLE (2024-T3 AL0.032) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED REINFORCING ANGLE AND NEW FASDR DHL2003801058Frame · crackedRT WING CTR L/E FORMER WITH 0.500 INCH CRACK IN STA XFS 441.561. STOP DRILLED CRACK AT STA XFS 441.561 IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER (2024-T3 AL0.032) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED ANGLE DOUBLER IAW SRM 51-1-8B. INSSDR MWEA030161Filler · crackedRIGHT WING LEADING EDGE INTERNAL, CRACK IN MILLED AREA OF INTERNAL LEADING EDGE AT WING STATION XFS112. FABRICATED AND INSTALLED FILLER, INSTALLED FASTENERS.SDR MWEA030160Skin · crackedRIGHT WING LEADING EDGE INTERNAL CRACK, LOWER AND FORWARD SURFACE. FABRICATED AND INSTALLED EXTERNAL REPAIR DOUBLER AND FILLERS.SDR DHL2003801066Frame · crackedRT WING INBOARD L/E FORMER WITH 1.000 INCH CRACK AT STA XFS 578.750. STOP DRILLED CRACK IAW SRM 57-2-0 PG 9-10. FABRICATED NEW DOUBLER (2024-T3 0.032) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED DOUBLER IAW SRM 57-2-0 PG SDR SWAA030785Skin · delaminatedDURING SCHEDULED D-CHECK, FOUND NR 2 AND NR 5 L/E SLATS DELAMINATED. REPAIRED NR 2 AND NR 5 L/E SLAT PER SRM.SDR SWAA030751Skin · delaminatedDURING SCHEDULED 1/4D CHECK, FOUND RT INBOARD FORE FLAP DELAMINATED. REMOVED AND REPLACED RT INBOARD FORE FLAP PER MM.SDR DHL2003801061Frame · crackedLT WING-CTR L/E FORMER CRACKED 0.500, STA XFS. 360.250. REMOVED FASTENERS IAW SRM 51-1-21 PG 1 SRM 51-1-20D PG 21. STOP DRILLED CRACK IAW SRM 57-2-0 PG 9-10. FABRICATED REINFORCING ANGLE (2024-T3 AL0.032) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMEDSDR TSAA0357059Skin · dentedGAINED ACCESS TO DENTED AREA. CUTOUT DAMAGE BY SLICING THE LEADING EDGE SKIN PER FIGURE 1. INSTALLED A SPLICE REPAIR AT SS205.46 AND SS 238.71. REPAIR COMPLETED IAW SRM 57-50-3, FIGURE 7 AND ECO 3354. AIRCRAFT RETURNED TO SERVICE. (M)SDR DHL2003801065Frame · crackedRT WING INBOARD L/E FORMER WITH 1.000 INCH CRACK AT STA XFS 597.500. STOP DRILLED CRACK AT STA XFS 597.500 IAW SRM 57-2-0 PG 9-10. FABRICATED REINFORCEMENT (2024-T3 0.032) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED REINFSDR 03FDEA00375Rib · damagedCOMPLY WITH EA 6-5740-68775 WINGS-RT SLAT NR 2-LEADING EDGE DAMAGE REPAIR BETWEEN RIB 2 AND RIB 3 UNDER W/O NR 13350 FEDEX N/R NR S00005. *S/D* COMPLIED WITH EA 6-5740-68775 WINGS-RT SLAT NR 2 LEADING EDGE DAMAGE REPAIR BETWEEN RIB 2 AND RIB 3. SDR QXEA0300431Structure · chafedPDX-RT SLATS CHAFING AGAINST UPPER WING SURFACE AT WS.178.00 AT INBOARD DISCONNECT SENSOR AREA. REPAIRED IAW CRJ700 SRM 51-25-26, SRM 51-00-02 AND SRM 51-25-16.SDR MWEA030157Rib · corrodedLEFT NR 0 SLAT TRACK ATTACH RIB STATION XIS40.014 HAS CORROSION IN THE HOLES FOR THE AFT ECCENTRIC'S. REMOVED CORROSION, INSTALLED BUSHING ON LEFT NR 0 SLAT DRIVE TRACK ATTACH RIB.SDR 2003UALA00467Wedge · delaminatedT/E WEDGE DELAMINATED, SLAT NR 9. MAJOR REPAIR ACCOMPLISHED. REMOVED, REPAIRED & REINSTALLED T/E WEDGE. SLAT OVERHAULED.SDR DL767030285Wedge · debondedRIGHT WING SLAT T/E WEDGE DISBONDED. REPAIRED PER ER/A 422819-14.SDR DL767030284Wedge · debondedLEFT SLAT T/E WEDGE DISBONDED. REPAIRED PER ER/A 422819-14.SDR DL767030283Wedge · debondedRIGHT WING SLAT T/E WEDGE DISBONDED. REPAIRED PER ER/A 422819-14.SDR DL767030282Wedge · debondedLEFT SLAT T/E WEDGE DISBONDED. REPAIRED PER ER/A 422819-14.SDR DL767030281Wedge · debondedSLAT T/E WEDGE DISBONDED. REPAIRED PER ER/A 422819-14.SDR 2003UALA00397Wedge · delaminatedT/E WEDGE DELAMINATED. REMOVED, REPAIRED AND REINSTALLED WEDGE, NR 12 SLAT.SDR SWAA030676Skin · crackedDURING SCHEDULED C1 CHECK, FOUND NR 6 L/E SLAT LOWER SKIN CRACKED AT AFT FASTENERS 17 INCHES FROM OTBD END. REPAIRED SLAT PER SWA EA.SDR DHL2003741543Angle · crackedDURING C-CHECK DISCREPANCY AS FOLLOWS, LT WING LEADING EDGE AT LEADING EDGE STA 130 IS CRACKED. REMOVED EXISTING FASTENERS TO GAIN ACCESS TO THE REPAIR AS PER B-727 SRM 51-30-2. CUT DAMAGED AREA AS PER B-727 SRM 51-40-3 FIG 1. FABRICATED REPAIR ANGLES MATERSDR SWAA030663Slat · delaminatedDURING SCHEDULED C2 CHECK, FOUND NR 5 L/E SLAT DELAMINATED AT OUTBOARD END. REMOVED AND REPLACED NR 5 L/E SLAT PER MM.SDR SWAA030662Slat · delaminatedDURING SCHEDULED C2 CHECK, FOUND NR 2 L/E SLAT DELAMINATED AT BOTH ENDS. REMOVED AND REPLACED NR 2 L/E SLAT PER MM.SDR 2003UALA00344Wedge · delaminatedT/E WEDGE, SLAT ASSEMBLY, DELAMINATED. MAJOR REPAIR ACCOMPLISHED. T/E WEDGE WAS REPAIRED.SDR SWAA030602Doubler · missingA 4 X 6 INCH PREVIOUS REPAIR MISSING AT NR 3 L/E SLAT UPPER SURFACE. REMOVED AND REPLACED NR 3 L/E SLAT PER MM.SDR 2003UALA00346Wedge · delaminatedT/E WEDGE DELAMINATED - NR 14 SLAT BULB SEAL CORE SECTION MISSING. MAJOR REPAIR ACCOMPLISHED. T/E WEDGE REPAIRED, INSTALLED MISSING CORE IN SEAL.SDR 2003F00409Bracket · brokenAT C-CHECK, FOUND NR 6 SLAT INBOARD FIXED LEADING EDGE CAVITY STOP BRACKET BROKEN. REPLACD NR 6 SLAT INBOARD FIXED LEADING EDGE CAVITY STOP BOLT BRACKET. (M)SDR 2003UALA00345Wedge · delaminatedT/E WEDGE DELAMINATED - NR 6 SLAT MAJOR REPAIR ACCOMPLISHED. T/E WEDGE REPAIRED.SDR AWXA200300350Skin · delaminatedDURING C-16 CHECK THE NR 3 LEADING EDGE SLAT UPPER SURFACE WAS FOUND DELAMINATED AT THE INBOARD CORNER. MAINTENANCE REMOVED THE NR 3 LEADING EDGE SLAT; PERFORMED COMPOSITE REPAIR OF THE INBOARD CORNER PER B737-300 SRM 51-70-10, FIG. 32, REPAIR 23; INSTALLED SDR AWXA200300351Skin · delaminatedDURING C-16 CHECK SEVERAL AREAS OF THE LT OUTBOARD FOREFLAP UPPER SURFACE WERE FOUND DELAMINATED AT THE INBOARD END. MAINTENANCE REMOVED AND REPLACED THE LT OUTBOARD FOREFLAP IAW BMM 27-51-37, PG. 401-407.SDR AWXA200300349Skin · delaminatedDURING C-16 CHECK THE NR 5 LEADING EDGE SLAT UPPER SURFACE WAS FOUND DELAMINATED AT THE CENTER, INBOARD & OUTBOARD CORNERS. MAINTENANCE REMOVED THE NR 5 LEADING EDGE SLAT; PERFORMED COMPOSITE REPAIR OF THE CENTER, INBOARD & OUTBOARD CORNERS PER B737-300 SRM 51SDR AWXA200300347Structure · delaminatedYVR - MAJOR REPAIR - DURING C-16 CHECK THE UPPER SURFACE OUTBOARD TRAILING EDGE OF THE NR 2 SLAT WAS FOUND DELAMINATED. MAINTENANCE REMOVED AND REPLACED NR 2 SLAT IAW BMM 27-81-21, PG. 401-419.SDR AWXA200300346Structure · delaminatedYVR - MAJOR REPAIR - DURING C-16 CHECK THE UPPER SURFACE, INBOARD CORNER OF THE NR 4 SLAT WAS FOUND DELAMINATED. MAINTENANCE REMOVED NR 4 SLAT, REPAIRED DAMAGE IAW SRM 51-70-10, FIG. 32, PG. 88I, RE-INSTALLED SLAT AND RIGGED SYSTEM IAW BMM 27-81-21, PG. 414-41SDR ASAA0310127Skin · crackedPAE - DURING C-CHECK, FOUND RIGHT WING FIXED LEADING EDGE NR 5 SLAT AT WING STATION 440 CRACKED. REMOVED DAMAGE AND INSTALLED DOUBLER PER EA. (M)SDR 2003F00458Skin · crackedAT C-CHECK, FOUND CRACK AT RT WING LEADING EDGE ABOVE NR 5 INBOARD SLAT TRACK LEADING EDGE CUTOUT UPPER RADIUS. STOP DRILLED CRACK AT RIGHT WING LEADING EDGE NR 5 SLAT TRACK CUT OUT, AT WING STATION 383. FABRICATED REPARI DOUBLER. ALODINED, PRIMED AND INSTASDR 2003F00449Retainer · crackedAT C-CHECK, FOUND CRACK AT RIGHT WING NR 5 SLAT OUTBOARD SEAL RETAINER. REMOVED AND REPLACED RIGHT WING NR 5 SLAT, OUTBOARD HOOK SEAL, UPPER LEADING EDGE WING, OUTBOARD SEAL RETAINER TRIM. (M)SDR 2003F00448Plate · crackedAT C-CHECK, FOUND CRACK AT NR 6 SLAT LOWER BACKSIDE ACTUATOR ROD END ACCESS CUTOUT SUPPORT PLATE. REMOVED DAMAGED PLATE FROM RIGHT WING NR 6 SLATE LOWER BACKSIDE SLAT ACTUATOR ROD END ACCESS CUT OUT. FABRICATED PLATE. TREATED AND PRIMED PART AND AREA. INST
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