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 IXXA060543SAngle · damagedDURING ROUTINE C CHECK, FOUND THREE FASTENER HEADS SHEARED ON THE RIGHT WING CENTER LEADING EDGE BOTTOM AFT OF THE END OF INBOARD SLAT. REMOVED DAMAGED ANGLE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW REPAIR PARTSSDR 03FDEA01444Structure · corrodedLT WING O/B FLAP O/B HINGE (FLAP SIDE) UPPER BORE FOUND CORRODED.SDR SWAA031956Skin · crackedDURING SCHEDULED C3 CHECK, FOUND NR 5 L/E SLAT CRACKED NEAR OUTBD END. REPAIRED NR 5 L/E SLAT PER SWA EA.SDR 03FDEA01440Structure · corrodedLT WING O/B FLAP I/B HINGE (A/C SIDE) PIVOT BEARING ATTACHMENT BORE FOUND CORRODED. LT WING O/B FLAP I/B HINGE (A/C SIDE) PIVOT BEARING ATTACHMENT BORE CORROSION REMOVED AND REPLACED AS PER EA 1-5750-72654 .SDR AMTA200301276Skin · dentedFOUND 5R SLAT L/E SKIN DENTED AT MID SECTION. REPAIRED SLAT L/E SKIN IAW SRM 57-51-00, FIG 807. (M)SDR DHL2003805587Skin · damagedLEFT WING EXTENDED L/E OUTBD VANE FWD PLATING ELONGATED HOLES AROUND STA XOLDO.67 (MAJOR REPAIR). PERFORMED MAJOR REPAIR. REMOVED FASTENERS, THE EXISTING INTERIM REPAIR AND FILLER. TRIMMED OUT THE DAMAGED SKIN AREA. PERFORMED NDT INSPECTION. CLEANED, TREASDR SWAA031908Skin · delaminatedDURING SCHEDULED D CHECK, FOUND NR 4 L/E SLAT DELAMINATED ON UPPER SURFACE OUTBD END. REPAIRED NR 4 L/E SLAT PER SRM.SDR UPS03841158Skin · crackedINSPECTION TYPE: C2, RT WING L/E SKIN IS CRACKED AT LOWER SURFACE XFS 304. STOP DRILLED CRACK, NDT VERIFIED STOP DRILL TERMINATES CRACK, FABRICATED AND INSTALLED DOUBLER IAW DC8-5720-4087-B APPX C.SDR UPS03841160Rib · crackedINSPECTION TYPE: C2, RT WING L/E LOWER RIBS ARE CRACKED AT XFS 616.25 AND XFS 622.5. STOP DRILLED CRACKS, NDT VERIFIED STOP DRILLS TERMINATES CRACKS, FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM 57-2-0 FIG 2.SDR UPS03841159Rib · crackedINSPECTION TYPE: C2, RT WING L/E LOWER RIB IS CRACKED AT XFS 772.5. STOP DRILLED CRACK, NDT VERIFIED STOP DRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM 57-2-0 FIG 2.SDR GTIA030658Rib · crackedFOUND SMALL CRACK ON INTERNAL RIB OF NR 1 L/E SLAT ON LT WING. REMOVED AND REPLACED NR 1 SLAT ON LEFT WING. (M)SDR DHL2003805581Skin · corrodedLEFT OUTER WING INBD EXTENDED L/E OUTER PLATING CORRODED AROUND STA XW 485.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR. REMOVED FASTENERS. REMOVED CORROSION. FOUND OUT OF LIMITS. CUT OUT DAMAGED AREA IAW DHL-EDT66-3, DHL-DWGT66-R03. PERFORMED NDT INSPECTISDR SWAA031882Skin · delaminatedDURING SCHEDULED C4 CHECK, FOUND NR 2 L/E SLAT DELAMINATED ON OUTBD UPPER SURFACE. REMOVED AND REPLACED NR 2 L/E SLAT PER MM.SDR DL73G030775Skin · debondedLT WING OUTBOARD FORE FLAP DISBONDED. TE WEDGE REBUILT IAW ER/A 423088-14.SDR AMTA200301277Skin · dentedFOUND 7R SLAT SKIN DENTED AT OUTBOARD LEADING EDGE. REPAIRED SLAT SKIN IAW SRM 57-51-00, FIG 807. (M)SDR AWXA200301048Door · crackedDURING C-16 CHECK A .3125 INCH CRACK WAS FOUND ON NR 5 SLAT ACTUATOR CLOSE OUT DOOR. MAINTENANCE REMOVED CLOSE OUT DOOR ON NR 5 SLAT AT WBL 435; FABRICATED A NEW REPLACEMENT CLOSE OUT DOOR PER DWG 65C26191; INSTALLED REPAIR PART IAW B737-200 SRM 51-30-02, PG. SDR AWXA200301041Skin · crackedDURING C-16 CHECK A .1250 INCH CRACK WAS FOUND ON NR 3 SLAT INBOARD MAIN TRACK CLOSE OUT DOOR AT WBL 230 LT. MAINTENANCE REMOVED AND REPLACED NR 3 SLAT INBOARD MAIN TRACK CLOSE OUT DOOR ASSEMBLY AT WBL 230 LT IAW B737-200 SRM 51-30-02, PARA B & E.SDR AWXA200301019Frame · crackedDURING C-16 CHECK A 1.75 INCH CRACK WAS FOUND ON LT WING LEADING EDGE FORMER AT WS 222.7, JUST INBOARD OF NR 1 PYLON. MAINTENANCE CUT OUT DAMAGE ON LT WING LEADING EDGE FORMER AT WS 222.7 AND PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED ASDR AWXA200301059Door · crackedDURING C-16 CHECK .1250 INCH CRACK WAS FOUND ON NR 4 SLAT ACTUATOR CLOSE OUT DOOR, WBL 279.25. MAINTENANCE REMOVED CRACKED NR 4 SLAT ACTUATOR CLOSE OUT DOOR; FABRICATED A NEW REPLACEMENT DOOR; INSTALLED REPAIR PART IAW BMM 20--050-011-2, FIG. 203.SDR AWXA200301016Skin · crackedDURING C-16 CHECK A .75 INCH CRACK WAS FOUND ON LOWER LEADING EDGE OF NR 1 KRUEGER FLAP AT L/E STA 205. MAINTENANCE BLENDED OUT CRACK ON LOWER LEADING EDGE OF NR 1 KRUEGER FLAP AT L/E STA 205 AND PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATSDR CALA0300466Skin · crackedINSPECTION FOUND NR 1 SLAT LOWER L/E SKIN CRACKED AT O/B TRACK. THERE WERE FOUR CRACKS MEASURING FROM .125 TO .25 INCH IN LENGTH. A REPAIR DOUBLER WAS INSTALLED IAW SRM 57-43-01.SDR GTIA030668Skin · lightning strikeLT WING NR 5 SLAT HAS LIGHTNING STRIKE AT INBOARD END ON TOP OF SLAT. AFTER FURTHER EVALUATION LIGHTNING STRIKE WAS FOUND TO BE CORROSION. CUT OUT DAMAGED SKIN. FABRICATED REPAIR SKIN AND DOUBLERS. INSTALLED REPAIR SKIN AND DOUBLERS. (M)SDR 03FDEA01328Hinge Fitting · damagedLT WING, IB FLAP, OB FORWARD HINGE FITTING HAS HYD ACTUATOR'S UPPER OB MOUNT LUG HOLE WITH TOOL MARK. LT WING IB FLAP OB HINGE (WING SIDE) HYD ACTUATOR ATTACHMENT OB HOLE REPAIRED IAW CMM 57-44-07.SDR 03FDEA01298Hinge Fitting · corrodedRT WING FLAP HINGE FITTING 28 WING SIDE 29 REAR SPAR LOWER MOUNT BOLT HOLE FOUND CORROSION.SDR 2003UALA00631Wedge · delaminatedT/E WEDGE DELAMINATION MAJOR REPAIR ACCOMPLISHED.REPAIRED T/E WEDGE.SDR AWXA200300877Roller · out of adjustLAX - FLIGHT CONTROL - FLT 0102 - ON TAKEOFF AT LAS EN ROUTE FOR LAX AT FLAP 1 THE AIRCRAFT HAD TENDENCY TO ROLL RIGHT, 20 DEGREES LEFT AILERON NEEDED TO HOLD WINGS LEVEL. AFTER FLAPS WERE RETRACTED ROLL TO THE RIGHT STOPPED. ON APPROCH INTO LAX AT FLAP 1 AND SDR DHL2003805582Plate · corrodedRIGHT INNER WING EXTENDED L/E SLOT UPPER PLATING CORRODED, STA XFS 207.000 AND XFS 220.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG 38. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS SDR 2003UALA00632Wedge · delaminatedT/E WEDGE DELAMINATED. T/E WEDGE REPLACED.SDR 03FDEA01208Slat Track · crackedLT WING, FOUND NR 16 SLAT TRACK INBOARD MOST FITTING WITH CRACK. CRACKED RIB ON LH WING, NR 16 SLAT TRACK INBOARD MOST FITTING REMOVED AND REPLACED AS PER SRM 51-33-01 VOL 2.SDR 03FDEA01201Bushing · wornAFTER RETRACTING FLAPS TO 2 THE RED L/E ANNUNCIATOR LIGHT REMAINED ILLUMINATED. POSITION TEST SHOWED NR 2 L/E FLAP INTRANSIT. RED TABS COMPLETED AND LIGHT WENT OUT, AFTER 1 MIN RED L/E FLAPS LIGHT ILLUMINATED AGAIN (WITH FLAPS IN THE UP POSITION). RED TABS SDR 2003UALA00719Wedge · delaminatedT/E WEDGE DELAMINATED. MAJOR REPAIR ACCOMPLISHED. REPAIRED WEDGE AND FASTENER HOLES.SDR AUS20030795Slat · wrong part(AUS) NO3 LEADING EDGE SLAT INCORRECT PART. PART NUMBER OF SLAT WAS FOR A 200 MODEL AIRCRAFT INSTEAD OF FOR A 300 MODEL. UNAPPROVED PART. PERSONNEL/MAINTENANCE ERROR.SDR SWAA031680Skin · delaminatedDURING SCHEDULED C2 CHECK, FOUND RT INBD T/E FORE FLAP DELAMINATED ON UPPER SURFACE. REMOVED AND REPLACED RT INBD T/E FORE FLAP PER MM.SDR 03FDEA01152Structure · crackedNR S-16 COMPLY WITH E.A.8-5750-70983. WINGS LEADING EDGE SLAT-NO-S SLAT TRAILING EDGE CRACK REPAIR. CLOSING ACTION ON 07/22/03 COMPLIED WITH E.A.8-5750-70983.SDR 2003UALA00601Wedge · delaminatedT/E WEDGE DELAMINATED AND SECTION HAD INFLIGHT SEPARATION. MAJOR REPAIR ACCOMPLISHED. REPLACED T/E WEDGE.SDR 2003UALA00598Wedge · delaminatedT/E WEDGE DELAMINATED, SLAT NR 9. MAJOR REPAIR ACCOMPLISHED. REMOVED, REPAIRED AND REPLACED T/E SLAT.SDR 2003UALA00587Wedge · delaminatedTRAILING EDGE WEDGE DELAMINATED, SLAT NR 6. MAJOR REPAIR ACCOMPLISHED. REMOVED , REPAIRED AND REINSTALLED TRAILING EDGE WEDGE.SDR UPS03241008Skin · crackedINSPECTION TYPE: C, SMALL CRACK 1 INCH IN LENGHT ON TAI SKIN OF NR 4 KREUGER FLAP, JUST I/B OF ACTUATOR ROD END ATTACH POINT ON FLAP. RECTIFICATION CARRIED OUT IAW UPS EO B727-5750-3082.SDR UPS03240995Skin · crackedINSPECTION TYPE: C, NR 3 SLAT OUTER SKIN CRACKED ADJACENT TO I/B HOOK ATTACH POINT. HFEC INSP CARRIED OUT AT THE ABOVE AREA IAW B727 NDTM PT 6 51-00-00. RESULT CRACK CONFIRMED & END MARKED. REPAIR CARRIED OUT IAW SRM 51-10-1, 57-50-3 & 51-30-3.SDR SWAA031562Skin · crackedDURING SCHEDULED 1/2D CHECK, FOUND NR 6 L/E SLAT CRACKED IN LOWER SKIN OUTBD EDGE. REMOVED AND REPLACED NR 6 L/E SLAT PER MM.SDR SWAA031556Skin · crackedDURING SCHEDULED SPECIAL VISIT, FOUND NR 3 L/E SLAT SKIN CRACKED AT L/E, OUTBD OF ACTUATOR. REPAIRED NR 3 L/E SLAT PER SRM.SDR 2003UALA00602Wedge · delaminatedDELAMINATION AND INFLIGHT SEPARATION OF NR 6 SLAT T/E WEDGE. MAJOR REPAIR ACCOMPLISHED. REPLACED SLAT T/E WEDGE.SDR 2003UALA00554Wedge · delaminatedTRAILING EDGE WEDGE SKIN DELAMINATED, SLAT NR 6 MAJOR REPAIR ACCOMPLISHED. REPLACED T/E WEDGE.SDR SWAA031511Skin · crackedDURING SCHEDULED C2 CHECK, FOUND NR 5 L/E SLAT CRACKED ON LOWER SKIN AT AFT RIVET ROW. REPAIRED NR 5 L/E SLAT PER SWA EA.SDR SWAA031493Skin · delaminatedDURING SCHEDULED C4 CHECK, FOUND LT INBD T/E FOREFLAP DELAMINATED ON UPPER SURFACE. REMOVED AND REPLACED LT INBD T/E FOREFLAP PER MM.SDR SWAA031489Skin · delaminatedDURING SCHEDULED C4 CHECK, FOUND NR 6 L/E SLAT T/E WEDGE DELAMINATED. REMOVED AND REPLACED NR 6 L/E SLAT PER MM.SDR DHL2003873592Skin · crackedLT OUTER WING IB EXTENDED LE LOWER PLATING CRACKED 1.000, AROUND STA. XFS.597.500 PERFORMED MAJOR REPAIR IAW EODHL-030625, ED-3457. REMOVED FASTENERS, TRIMMED OUT THE DAMAGED SKIN SEGMENT IAW EODHL-030625, ED3457. PERFORMED NDT INSPECTION IAW NDT SPM PART 6-10SDR QXEA200300810Sealant · chippedPDX - SEALANT CHIPPED AND POSSIBLE CORROSION ON FASTENER ON RIGHT LEADING EDGE UNDER SLAT. REPAIRED IAW EA R57-29 AND CRJ SRM 51-25-01.SDR DHL2003873607Vane · damagedWING VANE SLOT SHOWS HOLES ELONGATED AT XS.247.000. PERFORMED MAJOR REPAIR IAW EODHL-030627, ED-3455. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. TRIMMED OUT DAMAGED AREA IAW EODHL-030627, ED-3455. PERFORMED EDDY CURRENT INSPECTION IAW DC8 NDT SPM PART 6-10-01-001SDR AWXA200300774Skin · delaminatedDURING C-13 CHECK 19.5 INCH AREA OF THE NR 5 SLAT WAS FOUND DELAMINATED BETWEEN WS 234 AND WS 249. MAINTENANCE CUTOUT THE DAMAGED AREA OF NR 5 SLAT BETWEEN WS 234 AND WS 249; FABRICATED A FILLER AND DOUBLER; INSTALLED REPAIR IAW B737-300 SRM 51-70-10 PG 22, F
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