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.

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. TOct 24, 2002 · N936PG · Boeing 727225SDR 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)Oct 24, 2002 · N936PG · Boeing 727225SDR 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)Oct 24, 2002 · N936PG · Boeing 727225SDR 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.Oct 23, 2002 · N313FL · Boeing 737300SDR 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)Oct 22, 2002 · N976AS · Doug DC983SDR 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)Oct 22, 2002 · N976AS · Doug DC983SDR CALA0200502Slat · delaminatedINSPECTION FOUND #6 SLAT WEDGE SKIN DELAMINATED. THE #6 SLAT WAS REMOVED AND REPLACED IAW MM 27-81-01.Oct 21, 2002 · N13113 · Boeing 757224SDR 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.Oct 19, 2002 · N364PH · Dhav DHC8202SDR 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.Oct 18, 2002 · N405JW · Amd FALCON20C5SDR 2003UALA00243Skin · delaminatedNR 14 SLAT T/E WEDGE DELAMINATED MAJOR REPAIR ACCOMPLISHED. CORE, WEDGE AND SKIN REBUILT.Oct 17, 2002 · N769UA · Boeing 777222SDR 2003UALA00242Skin · delaminatedNR 3 SLAT T/E WEDGE DELAMINATED MAJOR REPAIR ACCOMPLISHED. CORE, WEDGE AND SKIN REBUILT.Oct 17, 2002 · N769UA · Boeing 777222SDR 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.Oct 14, 2002 · N747AS · Boeing 7372X6CSDR ASAA0210224Structure · damagedDURING SCHEDULED C CHECK, FOUND NR5 SLAT AT WING STATION 227-329 DAMAGED. REMOVED AND REPLACED NR5 SLAT.Oct 14, 2002 · N747AS · Boeing 7372X6CSDR 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.Oct 14, 2002 · N747AS · Boeing 7372X6CSDR ASAA0210231Skin · wornDURING SCHEDULED C CHECK, FOUND SKIN ON NR3 SLAT ACTUATOR CUTOUT AT WING STATION 272-313 WORN. REPAIRED SLAT SKIN IAW SRM.Oct 14, 2002 · N747AS · Boeing 7372X6CSDR 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.Oct 14, 2002 · N747AS · Boeing 7372X6CSDR 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.Oct 14, 2002 · N825NK · Doug DC983SDR 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. 2Oct 12, 2002 · N803DH · Doug DC873SDR 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 B7Oct 9, 2002 · N233TM · Boeing 737282SDR 2002UALA01627Wedge · delaminatedT/E WEDGE DELAMINATED, #2 SLAT. MAJOR REPAIR ACCOMPLISHED. AD 2002-11-02 ACCOMPLISHED. CORE, WEDGE AND SKIN REBUILT.Oct 8, 2002 · N769UA · Boeing 777222SDR 2002UALA01626Wedge · delaminatedTRAILING EDGE WEDGE DELAMINATED, #12 SLAT MAJOR REPAIR ACCOMPLISHED. AD 2002-11-02 ACCOMPLISHED. CORE, WEDGE AND SKIN REBUILT.Oct 8, 2002 · N769UA · Boeing 777222SDR 2002UALA01625Wedge · delaminatedDELAMINATED T/E WEDGE, #13 SLAT MAJOR REPAIR ACCOMPLISHED. AD 2002-11-02 ACCOMPLISHED. CORE, WEDGE AND SKIN REBUILT.Oct 8, 2002 · N769UA · Boeing 777222SDR 2002UALA01860Wedge · delaminatedT/E WEDGE DELAMINATED, SLAT #11 MAJOR REPAIR ACCOMPLISHED. CORE, WEDGE AND SKIN REBUILT.Oct 7, 2002 · N769UA · Boeing 777222SDR 2002UALA01636Wedge · delaminatedTRAILING EDGE SLAT DELAMINATED SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. CORE, WEDGE AND SKIN REBUILT.Oct 7, 2002 · N769UA · Boeing 777222SDR A6WA200260037Tab · dentedDENT LEFT FLAP INBOARD TAB X RECEIVED CONCESSION.Oct 4, 2002 · N612AW · Bac 146300ASDR 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.Oct 2, 2002 · Boeing 7372H4SDR 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; FABRICAOct 1, 2002 · N322AW · Boeing 7373G7SDR 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 SSep 29, 2002 · N803DH · Doug DC873SDR 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.Sep 29, 2002 · N407QX · Bombdr DHC8401SDR 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 Sep 29, 2002 · N803DH · Doug DC873SDR 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-Sep 27, 2002 · N803DH · Doug DC873SDR 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. INSTALLEDSep 27, 2002 · N803DH · Doug DC873SDR 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 SRSep 27, 2002 · N803DH · Doug DC873SDR 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 SRMSep 27, 2002 · N803DH · Doug DC873SDR 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-Sep 27, 2002 · N803DH · Doug DC873SDR 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 .INSTALSep 27, 2002 · N803DH · Doug DC873SDR 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 NESep 27, 2002 · N803DH · Doug DC873SDR 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 Sep 26, 2002 · N803DH · Doug DC873SDR 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-Sep 26, 2002 · N803DH · Doug DC873SDR 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 PESep 26, 2002 · N803DH · Doug DC873SDR 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 PERSep 26, 2002 · N803DH · Doug DC873SDR 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 PERSep 26, 2002 · N803DH · Doug DC873SDR 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 PERSep 26, 2002 · N803DH · Doug DC873SDR 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 PSep 26, 2002 · N803DH · Doug DC873SDR 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-Sep 26, 2002 · N803DH · Doug DC873SDR 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 IAWSep 26, 2002 · N803DH · Doug DC873SDR 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 DOUBLERSep 26, 2002 · N803DH · Doug DC873SDR 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,TREATEDSep 26, 2002 · N803DH · Doug DC873SDR 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. Sep 26, 2002 · N803DH · Doug DC873SDR 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 57-2Sep 24, 2002 · N803DH · Doug DC873
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