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 SWAA031051Skin · crackedDURING SCHEDULED C4 CHECK, FOUND NR 6 L/E SLAT CRACKED AT LOWER T/E AFT ROW OF FASTENERS. REPAIRED NR 6 L/E SLAT PER SWA EA.SDR AWXA200300726Skin · crackedDURING C-13 CHECK 6 EACH CRACKS WERE FOUND BETWEEN FASTENERS ON NR 4 LEADING EDGE SLAT LOWER SKIN AT SLAT ACTUATOR. MAINTENANCE CUT OUT CRACKED AREA OF LOWER SLAT SKIN; PERFORMED HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED A FILLER AND REPAIR SPLICESDR NACA20030085Hinge · corrodedLT WING KRUEGER FLAP MOUNT BRACKET HINGE ASSEMBLY CORRODED. REMOVED AND REPLACED HINGE ASSEMBLY.SDR SWAA031042Skin · crackedDURING SCHEDULED 1/4D CHECK, FOUND NR 4 L/E SLAT CRACKED ON LOWER SKIN JUST BELOW RETRACT ACTUATOR. REPAIRED NR 4 L/E SLAT PER SRM.SDR 03FDEA00706Structure · crackedRT WING- O/B FLAP L/E STOP BOLT SUPPORT ISLAND FOUND CRACKED.SDR TSAA0357117Web · corrodedCORROSION DISCOVERED ON RIGHT WING SPAR WEB AT FSS 540-552 BEHIND THE NR 6 SLAT. CUTOUT DAMAGED SECTION OF WEB. FABRICATED REPAIR PARTS AND DRILLED FASTENER HOLES. ALODINE, PRIMED AND INSTALLED REPAIR PART WET WITH FASTENERS MAKING A FAYING SURFACE SEAL. RESDR 2003UALA00435Skin · delaminatedT/E WEDGE LOWER SKIN DELAMINATED. MAJOR REPAIR ACCOMPLISHED. REMOVED, REPAIRED AND REINSTALLED T/E WEDGE, LT WING, SLAT NR 1.SDR 03FDEA00708Hinge · corrodedLT WING- O/B FLAP O/B HINGE (FLAP SIDE) LWR ATTACHING PIVOT O/B LUG HOLE FOUND CORRODED. LOWER ATTACHING PIVOT O/B LUG HOLE CORRODED AREA REPAIR CARRIED OUT AS PER FEDEX E.A. 1-5750-68412 WINGS- LT O/B FLAP- O/B HINGE AFT SUPPORT CORROSION.SDR 03FDEA00710Hinge · corrodedLT WING- O/B FLAP I/B HINGE (FLAP SIDE) LWR ATTACHING PIVOT I/B LUG HOLE FOUND CORRODED. LT WING- O/B FLAP I/B HINGE (FLAP SIDE) LWR ATTACHING PIVOT I/B LUG HOLE REPAIR CARRIED OUT AS PER FEDEX E.A. 1-5750-68413 WINGS- LT O/B FLAP- I/B HINGE AFT SUPPORT SDR MWEA030202Skin · dentedLEFT WING SLAT NR 4 LEADING EDGE APPROXIMATELY STATION XOS 467-468 HAS TWO DENTS APPROXIMATELY 1 INCH APART. FABRICATED AND INSTALLED REPAIR PART, INSTALLED UPPER SKIN FILLER, FABRICATED AND INSTALLED SPLICE DOUBLER, REMOVED AND REPLACED FASTENERS AND NR 10 BSDR GTIA030332Doubler · corrodedLEFT WING LEADING EDGE PANEL, 1118C CORROSION AT FASTENER HOLES. FABRICATED DOUBLER. INSTALLED DOUBLER.SDR DHL2003604527Frame · crackedLT WING - OUTBOARD STUB WING FORMER CRACKED 0.500 AT XS 539.000. STOP DRILLED CRACK AT XS 539.000 AND FABRICATED DOUBLER (2024-T3 0.032) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED ANGLE DOUBLER AND AREA IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER IAW SDR DHL2003604521Frame · crackedLT OUTER WING INBOARD L/E FORMER CRACKED (0.500 INCH) STA XFS 628.750. STOP DRILLED CRACK AND FABRICATED ANGLE DOUBLER (2024-T3 0.032) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10, SRM 5SDR DHL2003604525Frame · crackedLT WING INBOARD L/E FORMER AT STA XFS 691.250 CRACKED 0.500 INCH. STOP DRILLED CRACK AND FABRICATED ANGLE DOUBLER (2024-T3 0.032) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10, SRM 51-1-2SDR DHL2003604519Frame · crackedLT OUTER WING INBOARD L/E FORMER CRACKED 0.500 INCH, STA XFS 635.00. STOP DRILLED CRACK AND FABRICATED ANGLE DOUBER (2024-T3 0.032) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10, SRM 51-1SDR DHL2003604522Frame · crackedLT WING INBOARD L/E FORMER AT STA XFS 672.500 CRACKED 0.500 INCH. STOP DRILLED CRACK AND FABRICATED ANGLE DOUBLER (2024-T3 0.032) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10, SRM 51-1-2SDR DHL2003604517Frame · crackedLT WING INBOARD L/E FORMER WITH 0.500 INCH CRACK STA XFS 610.000. STOP DRILLED CRACK AND FABRICATED ANGLE DOUBLER (2024-T3 0.040) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10, SRM 51-1-2SDR DHL2003604523Frame · crackedLT OUTER WING INBOARD L/E FORMER CRACKED (0.500 INCH), STA 653.750. STOP DRILLED CRACK AND FABRICATED ANGLE DOUBLER (2024-T3 0.032) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10, SRM 51-1SDR DHL2003604520Frame · crackedLT OUTER WING INBOARD L/E FORMER CRACKED 0.500 INCH, STA XFS 641.250. STOP DRILLED CRACK AND FABRICATED ANGLE DOUBLER (2024-T3 0.032) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10, SRM 51SDR DHL2003604514Frame · crackedLT WING OUTBOARD L/E FORMER AT STA XFS 741.250 CRACKED 0.500 INCH. STOP DRILLED CRACK AND FABRICATED ANGLE DOUBLER (2024-T3 AL0.032) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10, SRM 51-SDR DHL2003604507Frame · crackedLT WING INBOARD L/E FORMER WITH 0.500 INCH CRACK STA XFS 578.750. STOP DRILLED CRACK AT STA XFS 578.750 AND FABRICATED ANGLE DOUBLER (2024-T3 0.032) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND ANGLE DOUBLER IAW SRM 51-1-8B. INSTALLED ANGLE SDR DHL2003604510Frame · crackedLT WING INBOARD L/E FORMER AT STA XFS 597.000 WITH 0.500 INCH CRACK. STOP DRILLED CRACK AND FABRICATED ANGLE DOUBLER (2024-T3 0.032) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10, SRM 51-SDR DHL2003604511Frame · crackedLT WING CTR L/E FORMER WITH 0.500 INCH CRACK IN IT, STA XS 461.372. STOP DRILLED CRACK AND FABRICATED DOUBLER ANGLE (2024-T3 AL0.040) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND DOUBLER ANGLE IAW SRM 51-1-8B. INSTALLED DOUBLER ANGLE ON LT WSDR DHL2003604513Frame · crackedLT WING CTR L/E FORMER WITH 0.500 INCH CRACK STA XS 478.897. STOP DRILLED CRACK AND FABRICATED DOUBLER ANGLE (2024-T3 AL0.032) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND DOUBLER ANGLE IAW SRM 51-1-8B. INSTALLED DOUBLER ANGLE AT XS 478.897 SDR DHL2003604504Frame · crackedLT WING CTR L/E FORMER WITH 0.500 INCH CRACK STA XS 491.193. STOP DRILLED AND FABRICATED DOUBLER ANGLE (2024-T3 0.040) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND DOUBLER ANGLE IAW SRM 51-1-8B. INSTALLED DOUBLER ANGLE ON LT WING CTR L/E FORSDR AWXA200300462Skin · crackedDURING C-17 CHECK 3 EACH 2 INCH CRACKS WERE FOUND ON NR 3 SLAT SKIN AT FASTENER HOLES ABOVE OUTBOARD AUXILIARY TRACK (HFEC VERIFIED). MAINTENANCE CUTOUT CRACKED SECTION OF NO. 3 SLAT SKIN; FABRICATED A FILLER AND SPLICE PLATE; INSTALLED REPAIR PARTS IAW B737-3SDR DHL2003801011Skin · corrodedRT OUTER WING INBOARD L/E OUTER PLATING CORRODED AT STA XW 485.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW EODHL 030405, ED 3260. REMOVED FASTENERS IAW SRM 51-1-21 PG 2. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-0 PG 16SDR DHL2003604503Frame · crackedLT WING OUTBOARD L/E FORMER AT STA XFS 835.000 CRACKED 0.500 INCH. STOP DRILLED CRACK AND FABRICATED DOUBLER ANGLE (2024-T3 AL0.032) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND DOUBLER ANGLE IAW SRM 51-1-8B. INSTALLED DOUBLER ANGLE AT XFS 8SDR DHL2003604518Frame · crackedLT WING OUTBOARD L/E FORMER AT STA XFS 722.500 CRACKED 0.500 INCH. STOP DRILLED CRACK AND FABRICATED DOUBLER ANGLE (2024-T3 AL0.032) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND DOUBLER ANGLE IAW SRM 51-1-8B. INSTALLED DOUBLER ANGLE AT XFS 7SDR DHL2003604516Frame · crackedLT WING OUTBOARD L/E FORMER AT STA XFS 735.000 CRACKED 0.500 INCH. STOP DRILLED CRACK AND FABRICATED ANGLE-DOUBLER (2024-T3 AL0.032) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10, SRM 51-SDR MEX2003145Slat · out of adjustDURING TAKE OFF THE SLAT LIGHT DISAGREE TURN ON WITH 13 DEGREES OF ADJUSTMENT ON SLATS, DISAGREE LIGHT TURN ON BEFORE V1. THE FLAP/SLAT BAR AND POSITION WERE ADJUSTED IAW MM.SDR 03FDEA00636Skin · crackedUPON REMOVAL OF RT NR 2 LEADING EDGE OUTBOARD MOST SEAL FOUND SLAT UPPER SKIN TRAILING EDGE AFT MOST HOLE CRACKED. RT WING NR 2 LEADING EDGE OUTBOARD SLAT UPPER SKIN TRAILING EDGE REMOVED AND REPLACED AS PER SRM 51-35-01 VOL. II AND DWG NRB6225.SDR CALA0300221Rib · gougedLEFT WING NUMBER TWO MID FLAP GOUGED AT MID SPAR CENTER FORE FLAP TRACK GUIDE. REPLACED RIB AT MID FLAP SPAR CENTER FORE FLAP TRACK GUIDE NUMBER TWO MID FLAP PER SRM 51-10-02.SDR DHL2003604515Frame · crackedLT WING OUTBOARD L/E FORMER AT STA XFS 866.250 CRACKED 0.500 INCH. STOP DRILLED CRACK AT XFS 866.250. FABRICATED ANGLE DOUBLER (2024-T3 0.032) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-SDR UPS03640465Skin · crackedLT WING L/E CRACK IN FIBERGLASS SKIN ON SLAT CLOSURE PANEL. FOUND S MALL DENT WITH CRACKS LOWER LEADING EDGE OF LEFT WING NEAR FUSELAGE. TRIMED DAMAGE REA OUT PER SRM 51 70 AND EO B767 5750 15568-B (AS REF FOR GAP).SDR DHL2003755006Structure · crackedRT WING L/E STA 464 APPROX HAS APPROX 5 INCH CRACK ABOVE NR 5 SLAT. CLEANED AREA OF PAINT AT STA 444 AND 454. PERFORMED DYE PENETRANT OF SUSPECTED AREAS AND CONFIRMED SKIN CRACKS AT STA 444 & 454. CUT OUT AREA SIZE 3 X 4 INCH ON STA 444 LT WING L/E AND CUT SDR DHL2003604512Frame · crackedLT WING OUTBOARD L/E FORMER AT STA XFS 797.500 CRACKED 0.500 INCH. STOP DRILLED CRACK AND FABRICATED ANGLED DOUBLER (2024-T3 0.032) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10, SRM 51-1SDR SWAA030916Structure · delaminatedDURING SCHEDULED C4 CHECK, FOUND RT INBD FOREFLAP DELAMINATED ON UPPER SURFACE. R&R RT INBD FOREFLAP PER MM.SDR A6WA200360015Skin · crackedCRACKED IN HALF ABOVE PYLON NR 2 LEADING EDGE FIXED STRUCTURE. REMOVED AND REPLACED DOUBLER, P/N HC572H1080-001. 2 INCH CRACK TO NUTPLATE. PIECE INTACT, BUT CRACKED ALL THE WAY THROUGH. CAUSE OF DAMAGE, NORMAL FATIGUE. (M)SDR 2003UALA00434Wedge · damagedHAIL DAMAGE OCCURRED TO T/E WEDGE, NR 6 SLAT. REPAIRED T/E WEDGE, SLAT NR 6.SDR 2003UALA00433Wedge · damagedHAIL DAMAGE OCCURRED TO T/E WEDGE, NR 5 SLAT. REPAIRED T/E WEDGE, SLAT NR 5.SDR 2003UALA00431Wedge · damagedHAIL DAMAGE OCCURRED TO T/E WEDGE, NR 3 SLAT. REPAIRED T/E WEDGE, SLAT NR 3.SDR 2003UALA00430Wedge · damagedHAIL DAMAGE OCCURRED TO T/E WEDGE, NR 2 SLAT. REPAIRED T/E WEDGE, SLAT NR 2.SDR 03FDEA00611Fitting · crackedLT WING L/E SLAT TRACK NR 16 INBOARD FITTING FOUND CRACKED. LT WING LEADING EDGE SLAT TRACK NR 16 INBOARD FITTING REMOVED AND REPLACED AS PER SRM 51-33-01 VOL. II AND DWG ARB2850.SDR DHL2003801027Frame · crackedLT WING OUTBOARD STUB WING FORMER CRACKED, STA XS 520.168. STOP DRILLED CRACK IAW SRM 57-2-0 PG 9-10. FABRICATED REINFORCING ANGLE (7075-T6 0.090) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED REINFORCING ANGLE IAW SRM 57-2SDR SWAA030876Skin · crackedDURING SCHEDULED 1/2D CHECK, FOUND NR 6 L/E SLAT LOWER SKIN CRACKED AT MIDDLE AUX TRACK. REPAIRED NR 6 L/E SLAT PER SRM.SDR DHL2003801021Vane · damagedLT WING L/E OUTBOARD VANE UPPER SKIN SHOWS ELONGATED HOLES AT STA XOLDI 6.224 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW EO DHL 030408, ED-3264. CUT OUT DAMAGED AREA IAW ED DHL 030408, ED-3264. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B, FABRICATED FISDR 03FDEA00468Skin · dentedRIGHT WING LEADING EDGE HAS A DENT ABOUT 6 FEET OUTBOARD OF THE FUSELAGE.SDR DHL2003801038Frame · crackedLT WING - CTR L/E FORMER WITH 2.000 INCH CRACK IN STA XFS 310.250. STOP DRILLED CRACK IAW SRM 57-2-0 PG 9-10. FABRICATED REINFORCING ANGLE (7075-T6 0.040) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED REINFORCING ANGLE IAW SDR 03FDEA00446Slat Track · wornCOMPLY WITH EA 8-2780-68790 FLIGHT CONTROLS-SLATS-REWORK OF WORN AREA ON LT WING SLAT TRACK NR 9. CLOSING ACTION ON 04/14/03. COMPLIED WITH EA 8-2780-68790 FLIGHT CONTROLS-SLAT- REWORK OF WORN AREA ON LT WING SLAT TRACK NR 9.
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