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 GAIA02151STSkin · crackedDURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE RIGHT WING UPPER OUTBOARD LEADING EDGE AT WS 430 HAD A ROW OF FASTENERS WITH CRACKS RUNNING FROM HEAD HOLES AT THE NR 5 SLAT LEADING EDGE. REPAIR WAS ACCOMPLISHED IAW BOEING 727 SRM 57-30-3, FIGURE 4. TSDR GAIA02144STSkin · dentedDURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE LEFT WING NR 2 SLAT NOSE UPPER SURFACE SHOWS A LARGE DENTED AREA ON THE SKIN. REPAIR WAS ACCOMPLISHED IAW BOEING 727 SRM 57-50-3, FIGURE 4. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR GAIA02143STRib · crackedDURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE LEFT WING NR 4 SLAT INTERIOR RIB WAS CRACKED AT WS 410, OUTBOARD OF THE ACTUATOR ATTACH POINT. REPAIR WAS ACCOMPLISHED IAW BOEING 727 SRM 57-50-3, FIGURE 9. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR F3LA200200368Skin · puncturedDURING C 2 CHECK, IT WAS NOTED RT, IN BOARD FORE FLAP HAD A HOLE IN THE LOWER SURFACE. FLAP WAS REMOVED AND REPAIRED IAW SRM 51-70-10 AND REINSTALLED IAW BOEING 737 MM 27-51-07.SDR ASAA0280443Door · chafedOKC - FOUND DURING 30K-CHECK, RIGHT NR 5 SLAT TRACK DOOR CHAFED AT FORWARD END. REPLACED SLAT TRACK DOOR PER MM 27-80-01. (M)SDR ASAA0280442Panel · chafedOKC - FOUND DURING 30K CHECK, LEFT NR 3 SLAT TRACK PANEL FORWARD END IS CHAFED AT NOTCH-OUT. REPLACED SLAT TRACK DOOR PER MM 27-80-01. (M)SDR CALA0200502Slat · delaminatedINSPECTION FOUND #6 SLAT WEDGE SKIN DELAMINATED. THE #6 SLAT WAS REMOVED AND REPLACED IAW MM 27-81-01.SDR QXEA0201778Flap Track · corrodedPDX - LT WING, NR 5 FLAP TRACK, UPPER TRACK "A", HAS TWO LOCATIONS OF PITTING CORROSION. REPAIRED IAW HORIZON AIR EA 2-57-203.SDR UVV2002F00001Rib · crackedRIB HAS CRACK RADIATING THROUGH FASTENERS ATTACHING RIB TO SPAR AND A PIECE IS MISSING APPROX 6 INCHES LONG AND .2500 INCHES WIDE, CORROSION EVIDENT, POSSIBLY DUE TO INSULATION BEING WET. THIS DEFECT CAN ONLY BE SEEN IF LEADING EDGE IS DISASSEMBLED.SDR 2003UALA00243Skin · delaminatedNR 14 SLAT T/E WEDGE DELAMINATED MAJOR REPAIR ACCOMPLISHED. CORE, WEDGE AND SKIN REBUILT.SDR 2003UALA00242Skin · delaminatedNR 3 SLAT T/E WEDGE DELAMINATED MAJOR REPAIR ACCOMPLISHED. CORE, WEDGE AND SKIN REBUILT.SDR ASAA0210225Skin · wornDURING SCHEDULED C CHECK, FOUND LEADING EDGE SKIN AT NR 2 SLAT ACTUATOR CUTOUT AT WING STATION 409-447 WORN. REMOVED AND REPLACED SKIN IAW SRM.SDR ASAA0210224Structure · damagedDURING SCHEDULED C CHECK, FOUND NR5 SLAT AT WING STATION 227-329 DAMAGED. REMOVED AND REPLACED NR5 SLAT.SDR ASAA0210226Skin · wornDURING SCHEDULED C CHECK, FOUND LEADING EDGE SKIN AT NR 5 SLAT ACTUATOR AT WING STATION 399-462.5, WORN. REPAIRED SKIN IAW SRM.SDR ASAA0210231Skin · wornDURING SCHEDULED C CHECK, FOUND SKIN ON NR3 SLAT ACTUATOR CUTOUT AT WING STATION 272-313 WORN. REPAIRED SLAT SKIN IAW SRM.SDR ASAA0210241Skin · dentedDURING SCHEDULED C CHECK, FOUND NR 4 SLAT MAIN TRACK COVER AT SLAT STA 28, SLAT STA 31 DENTED. REPAIRED DENT TO ORIGINAL CONTOUR IAW EA.SDR GTIA021115Rub Strip · crackedLEFT NR 0 LEADING EDGE SLAT, OUTBOARD END RUB STRIP PANEL HAS 3 INCH CRACK ON LOWER BOTTOM CORNER THROUGH 2 EA SCREW HOLES. REMOVED PANEL AND REPAIRED AND REINSTALLED, SEALED AND SECURED.SDR DHL2002803547Plate · crackedRT INBD SLOT LE INTERNAL PLATE WITH 2 INCH CRACK IN IT STA XFS 218.000. REMOVED DAMAGED PLATE IAW SRM 57-2-0 FIG 2 FABRICATED NEW PLATE IAW SRM57-2-0 FIG. 2. CLEANED ,TREATED AND PRIMED AREA IAW SRM 51-1-8B INSTALLED NEW PLATE IAW SRM 57-2-0 FIG. 2SDR BJNA021015Skin · crackedLEFT WING NR 2 SLAT TRAILING EDGE CHAFED AND CRACKED AT OUTBOARD AUX SLAT TRACK. REPAIRED CRACKED AND CHAFED LEFT WING NR 2 SLAT TRAILING EDGE AT OUTBOARD AUX SLAT TRACK BY CUTTING OUT DAMAGED SECTION, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW B7SDR 2002UALA01627Wedge · delaminatedT/E WEDGE DELAMINATED, #2 SLAT. MAJOR REPAIR ACCOMPLISHED. AD 2002-11-02 ACCOMPLISHED. CORE, WEDGE AND SKIN REBUILT.SDR 2002UALA01626Wedge · delaminatedTRAILING EDGE WEDGE DELAMINATED, #12 SLAT MAJOR REPAIR ACCOMPLISHED. AD 2002-11-02 ACCOMPLISHED. CORE, WEDGE AND SKIN REBUILT.SDR 2002UALA01625Wedge · delaminatedDELAMINATED T/E WEDGE, #13 SLAT MAJOR REPAIR ACCOMPLISHED. AD 2002-11-02 ACCOMPLISHED. CORE, WEDGE AND SKIN REBUILT.SDR 2002UALA01860Wedge · delaminatedT/E WEDGE DELAMINATED, SLAT #11 MAJOR REPAIR ACCOMPLISHED. CORE, WEDGE AND SKIN REBUILT.SDR 2002UALA01636Wedge · delaminatedTRAILING EDGE SLAT DELAMINATED SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. CORE, WEDGE AND SKIN REBUILT.SDR A6WA200260037Tab · dentedDENT LEFT FLAP INBOARD TAB X RECEIVED CONCESSION.SDR SWAA022312Slat · delaminatedDURING SCHEDULED C4 CHECK, FOUND NR 1 L/E SLAT DELAMINATED AT INBD T/E. REMOVED AND REPLACED NR 1 L/E SLAT PER MM.SDR AWXA200201050Skin · crackedMCN - MAJOR REPAIR - DURING C-12 CHECK A 1/4 INCH CRACK WAS FOUND AT 4 EACH RIVETS AT THE LOWER TRAILING EDGE OF THE RT WING NR 6 SLAT, JUST BELOW THE INBOARD AUXILIARY TRACK WS 580. MAINTENANCE REMOVED DAMAGED AREA OF NR 6 SLAT AT LOWER TRAILING EDGE; FABRICASDR DHL2002803525Frame · crackedRT WING L/E FRAME UPPER PART AT STA 680.000 WITH 1/2 INCH CRACK IN IT. 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 AL0.032) PER SRM 57-2-0 PG9-10. CLEANED TREATED AND PRIMED PER SSDR QXEA0201703Structure · crackedCKB - RT CENTER WING LEADING EDGE HAS ALL FOUR AFT CORNERS CRACKED. REPAIRED IAW HORIZON AIR EA 6-57-63 AND EO DH8 6-57-0591.SDR DHL2002803505Frame · crackedRT WING L/E UPPER PART FRAME CRACKED 1/2 IN AT STA 649.000. REMOVED FASTNERS PER SRM 51-121 PG 1.STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10. FABRICATED REINFORCING ANGLE (2024.T3 AL 0.32) PER SRM 57-2-0 PG 9-10,51-1-21 PG 1. CLEANED TREATED AND PRIMED PER SRM SDR DHL2002803531Frame · crackedLT WING CENTRAL L/E FRAME CRACKED 1 INCH AT STA XFS 422.000. REMOVED FASTNERS PER SRM 51-1-20D PG 21. STOP DRILLED 1 INCH CRACK PER SRM 57-20 PG 9-10.FABRICATED A DOUBLER ANGLE (2024T3AL0.032) PER SRM 57-2-0 PG 9-10. CLEANED TREATED AND PRIMED PER SRM 51-1-SDR DHL2002803530Frame · crackedLT WING CENTRAL L/E FRAME CRACKED AT STA XFS 471.000. REMOVED FASTNERS PER SRM 51-1-20 PG 21. STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10. FABRICATED DOUBLER ANGLE (2024 T3 AL 0.032) PER SRM 57-2-0 PG 9-10. CLEANED TREATED AND PRIMED PER SRM 51-1-8B. INSTALLEDSDR DHL2002803526Frame · crackedRT WING L/E FRAME LOWER PART AT STA 643.000 WITH 1/2 INCH CRACK IN IT. 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 AL0.032) PER SRM 57-2-0 PG9-10. CLEANED TREATED AND PRIMED PER SRSDR DHL2002803524Frame · crackedRT WING L/E FRAME UPPER PART AT STA 649.000 WITH 1/2 INCH CRACK IN IT. REMOVED FASTNESS PER SRM 51-1-21 PG 1. STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10. FABRICATED REINFORCING ANGLE (2024.T3 AL0.032) PER SRM 57-2-0 PG9-10. CLEANED TREATED AND PRIMED PER SRMSDR DHL2002803523Frame · crackedRT WING L/E FRAME PART AT STA 607.000 WITH 1/2 INCH CRACK IN IT. REMOVED FASTNERS 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 SRM 51-SDR DHL2002803504Frame · crackedRT WING L/E FRAME UPPER PART AT STA 661.000 WITH 1/2 IN CRACK IN IT. REMOVED FASTNERS PER SRM 51-1-21 PG 1. STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10. FABRICATED REINFOCING ANGLES PER IAW SRM 57-2-0 PG 9-10. CLEANED TREATED AND PRIMED PER SRM 51-1-8B .INSTALSDR DHL2002803503Frame · crackedRT WING L/E FRAME UPPER PART AT STA 620.000, WITH 1/2 IN CRACK IN IT. REMOVED FASTNERS PER SRM 51-1-21 PG 1. STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10.FABRICATED REINFOCING ANGLES IAW SRM 57-2-0 PG 9-10.CLEANED TREATED AND PRIMED PER SRM 51-1-8B.INSTALLED NESDR DHL2002803534Frame · crackedLT WING O/B L/E FRAME AT STA XRS 603.750 WITH A 1/2 IN CRACK IN IT. STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10. FABRICATED REINFORCING ANGLE (2024T3 AL0.032) PER SRM 57-2-0 PG 9-10. CLEAND TREATED AND PRIMED PER SRM 51-1-8B. INSTALLED ANGLE PER SRM 57-2-0 SDR DHL2002803533Frame · crackedLT WING O/B L/E FRAME AT STA XRS 660.000 WITH A 1 IN CRACK IN IT. STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10. FABRICATED REINFORCING ANGLE (2024T3 AL0.032) PER SRM 57-2-0 PG 9-10. CLEAND TREATED AND PRIMED PER SRM 51-1-8B. INSTALLED ANGLE PER SRM 57-2-0 PG9-SDR DHL2002803532Frame · crackedLT WING O/B L/E FRAME AT STA XRS 616.250 WITH A 1/2 INCH CRACK IN IT. STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10. FABRICATED REINFORCING ANGLE (2024-T3 AL 0.032) PER SRM 57-2-0 PG9-10. CLEANED TREATED AND PRIMED PER SRM 51-1-8B. INSTALLED REINFORCING ANGLE PESDR DHL2002803527Frame · crackedLT WING O/B L/E FRAME UPPER PART AT STA 635.000 WITH 1/2 INCH CRACK IN IT. REMOVED FASTNERS PER SRM 51-1-21 PG 1. STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10. FABRICATED REINFORCING ANGLE (2024.T3 AL0.032) PER SRM 57-2-0 PG9-10. CLEANED TREATED AND PRIMED PERSDR DHL2002803528Frame · crackedLT WING O/B L/E FRAME UPPER PART AT STA XRS 591.250 WITH 1/2 INCH CRACK IN IT. 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 AL0.032) PER SRM 57-2-0 PG9-10.CLEANED TREATED AND PRIMED PERSDR DHL2002803517Frame · crackedLT WING O/B L/E FRAME AT STA XRS 610.000 WITH 1/2 INCH. REMOVED FASTNERS PER SRM 51-1-21 PG 9-10. FABRICATED SUPPORT ANGLE (21024 T3 AL0.032) PER SRM 57-2-0 PG 9-10. CLEANED TERATED AND PRIMED PER SRM 51-1-8B. INSTALLED SUPPORT ANGLE WITH NEW FASTNERS PERSDR DHL2002803515Frame · crackedLT WING O/B L/E FRAME AT STA XRS 672.000 WITH 1/2 INCH CRACK IN IT. REMOVED FASTNERS PER SRM 57-2-0 PG 9-10. FABRICATED SUPPORT ANGLE (2024 T3 AL0.032) PER SRM 57-2-0 PG 9-10. CLEANED TREATED AND PRIMED PER SRM 51-1-8B. INSTALLED ANGLE WITH NEW FASTNERS PSDR DHL2002803514Frame · crackedLT WING O/B L/E FRAME AT STA XRS 622.500 WITH 1/2 INCH CRACK. STOP DRILLED CRACK PER SRM 57-1-0 PG 9-10. FABRICATED REINFOCING ANGLE (2024 T3 0.032) PER SRM 57-2-0 PG 9-10. CLEANED TREATED AND PRIMED PER SRM 51-1-8B. INSTALLED REINFOCING ANGLE PER SRM 57-SDR DHL2002803512Frame · crackedLT WING CENTER L/E INTERNAL PART SHOWS FRAME CRACKED 1 INCH AT XFS 385.250. REMOVED FASTNERS PER SRM 51-1-20D PG 21. STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10. FABRICATED NEW DOUBLER ANGLE (2024T3AL0.032)PER SRM 57-2-0 PG 9-10.CLEANED TREATED NAD PRIMED IAWSDR DHL2002803511Frame · crackedLT WING CENTER L/E INTERNAL PART SHOWS FRAME WITH 2 EA CRACKS 3/4 INCH AT XFS 454.000. STOP DRILLED CRACK PER SRM57-2-0 PG 9-10. FABRICATED DOUBLER ANGLE (2024 T3 AL0.040) PER SRM 57-2-0 PG 9-10.CLEANED TERATED AND PRIMED PER SRM 51-1-8B. INSTALLED DOUBLERSDR DHL2002803510Frame · crackedLT WING CENTER L/E INTERNAL PART SHOWS FRAME CRACKED 1 INCH AT XFS 447.350. REMOVED FASTNERS PER SRM 51-1-20 D PG 21.STOP DRILLED CRACKED FRAME XFS 447.750 PER SRM 57-2-0 PG 9-10.FABRICATED DOUBLER ANGLE (2024 T3 ALO 032")PER SRM 57-20 PG 9-10.CLEANED,TREATEDSDR DHL2002803508Frame · crackedLT WING O/B L/E FRAME AT STA XRS 641.250 WITH 1/2 IN CRACK IN IT. REMOVED FASTNERS PER SRM 51-1-21 PG 1.STOP DRILLED CRACK PER SRM 57-2-0 PG9-10. FABRICATED SUPPORT ANGLE (2024.T3 AL 0.032) PER SRM 57-2-0 PG 9-10.CLEANED ,TREATED AND PRIMED PER SRM 51-1-8B. SDR DHL2002803502Frame · crackedLT WING OUTBOARD L/E FRAME AT STA XRS 585.000 WITH 1/2 IN CRACK IN IT. 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 ANGLE PER SRM 57-2
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