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 USAA040296Skin · delaminatedPIT - FOUND SKIN TO CORE DELAMINATED 1 INCH BY 5 INCH AREA, RT WING NR 4 SLAT OUTBOARD TRAILING EDGE. INSTALLED REPAIR CORE AND TOP DOUBLER, SEALED DOUBLER PER SRM 51-70-10. (M)SDR USAA040294Skin · delaminatedFOUND SKIN TO CORE DELAMINATION 1.5 SQUARE INCH AREA, LT WING NR 3 SLAT INBOARD END TRAILING EDGE CORNER. INSTALLED NEW CORE MATERIAL, TOP REPAIR DOUBLER, SEALED EDGE AND TOP DOUBLER PER SRM 51-70-10. (M)SDR 04FDEA01632Rib · gougedCOMPLY WITH EA 8-5710-77417 WINGS REWORK OF GOUGE IN LEADING EDGE SLAT RIB ARB1092-1. COMPLIED WITH EA 8-5710-77417 WINGS REWORK OF GOUGE IN WING LEADING EDGE SLAT RIB ARB1092-1.SDR AWXA200400658Skin · crackedLCQ - MAJOR REPAIR - DURING C-17 CHECK SEVERAL CRACKS WERE FOUND AT RIVET HOLES ON NR 4 LEADING EDGE SLAT FROM SS 28 RT TO SS 84 RT. MAINTENANCE CUT OUT DAMAGED SECTION OF NR 4 SLAT SKIN FROM SS 28 RT TO SS 84 RT; FABRICATED A FILLER AND SPLICE PLATE; INSTALLSDR 04FDEA01626Rib · crackedRT WING, SLAT TRACK NR 16 INBOARD RIB SUSPECT CRACKED.SDR 04FDEA01624Rib · gougedCOMPLY WITH EA 8-5710-77421 WINGS REWORK OF GOUGES IN NR 1 SLAT TRACK SUPPORT RIB ARB1189. COMPLIED WITH EA 8-5710-77421 WINGS REWORK OF GOUGES IN NR 1 SLAT TRACK SUPPORT RIB ARB1189.SDR SWAA041595Structure · crackedDURING SCHEDULED C2 CHECK, FOUND LT WING NR 1 L/E SLAT, CRACKED. REPAIRED L/E SLAT PER EA.SDR SWAA041594Structure · crackedDURING SCHEDULED C2 CHECK, FOUND LT WING NR 2 L/E SLAT, CRACKED. REPAIRED L/E SLAT PER EA.SDR AWXA200400610Skin · crackedMCN - MAJOR REPAIR - DURING C-15 CHECK 2 EACH CRACKS WERE FOUND EMANATING FROM STOP DRILL HOLES IN NR 4 SLAT LOWER OUTBOARD SKIN AT SS 116.75. MAINTENANCE CUT OUT CRACKED SLAT SKIN AT SS 116.75; FABRICATED A FILLER AND SPLICE PLATE; INSTALLED REPAIR PARTS IAWSDR USAA040299Skin · delaminatedPIT - FOUND SKIN AND CORE BOND HAS DELAMINATION AND KNIFE EDGE CHAFE WEAR, 5 INCHES BY 5 INCHES, LT WING NR 2 SLAT INBOARD T/E CORNER. REPLACED CORE MATERIAL, INSTALLED TOP SKIN REPLACEMENTS, SEALED AND PAINTED PER SRM 51-70-10. (M)SDR SWAA041557Wedge · delaminatedDURING SCHEDULED D-CHECK, FOUND LT WING NR 3 L/E SLAT T/E WEDGE, DELAMINATED. REPAIRED T/E WEDGE PER SRM.SDR UPS04242584Skin · crackedINSPECTION TYPE: C, NR 6 L/E FLAP CRACKED I/B OF LANDING LIGHT & JUST ABOVE BULLNOSE. FLAP REPLACED IAW MM 27-81-01.SDR ASAA0480460Skin · dentedOKC - DURING C-CHECK, FOUND LEFT WING NR 5 SLAT IS DENTED. REMOVED DAMAGED SECTION. INSTALLED FILLER AND DOUBLER PER SRM 57-03. (M)SDR UIEA200400100Channel · crackedCENTER CHANNEL CRACKED BEYOND PRIVOUS REPAIR IB HINGE ON NR 7 LE FLAP. FOUND DURING VISUAL INSPECTION. CAUSE IS UNKNOWN. LOCATION IS WING STA 944.5. CORRECTIVE ACTION REPLACED LE FLAP ASSY IAW MM.SDR USAA040297Skin · delaminatedPIT - FOUND SKIN AND CORE DELAMINATED 4 INCHES BY 4 INCHES, NR 5 SLAT OUTBOARD END TRAILING EDGE SECTION. INSTALLED NEW CORE PER SRM 51-20-10. (M)SDR USAA040298Skin · delaminatedPIT - FOUND SURFACE TO CORE DELAMINATION 3 INCHES BY 2.5 INCH AREA, NR 4 SLAT TOP SURFACE INBOARD TRAILING EDGE. INSTALLED NEW CORE AND EXT DOUBLER PER SRM 51-70-10. (M)SDR USAA040302Skin · delaminatedPIT - FOUND SKIN AND CORE 7.5 INCH BY 4.25 INCH, DELAMINATION WITH LOWER SKIN KNIFE EDGE WEAR, LT WING NR 2 SLAT OUTBOARD T/E CORNER. REMOVED DAMAGED SKIN AND CORE, REPLACED CORE AND TOP SKIN PER SRM 51-70-10. (M)SDR USAA040301Skin · delaminatedPIT - FOUND SKIN TO CORE BOND WITH 1 INCH DIAMETER AND .75 INCH DIAMETER, LEFT WING NR 2 SLAT TOP SURFACE INBOARD AND OUTBOARD T/E CORNERS. REMOVED EXT SKIN AND DAMAGED CORE, INSTALLED NEW PER SRM 51-70-10. (M)SDR AWXA200400608Skin · crackedMCN - MAJOR REPAIR - DURING C-15 CHECK 2 EACH CRACKS WERE FOUND IN NR 3 SLAT LOWER SKIN BELOW THE ACTUATOR AT SS 68.26. MAINTENANCE CUT OUT CRACKED SLAT SKIN AT SS 68.26 AND PERFORMED A HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED A FILLER SDR N150AW0002Skin · damagedLEADING EDGE OF WING DAMAGED OUTBOARD END OF THE NUMBER 5 SLAT. REPAIRED PER SRM 51-70-17.SDR SWAA041462Skin · delaminatedDURING SCHEDULED C4 CHECK, FOUND RT WING NR 5 L/E SLAT DELAMINATED. REMOVED AND REPLACED NR 5 L/E SLAT PER MM.SDR ASAA0480446Skin · gougedOKC - DURING HV-CHECK, FOUND LEFT NR 0 SLAT INBOARD UPPER SKIN IS GOUGED AT AFT CORNER. REMOVED DAMAGED SECTION AND INSTALLED DOUBLER PER SRM 57-09. (M)SDR ASAA0480444Skin · crackedOKC - DURING HV CHECK, FOUND LEFT NR 2 SLAT LOWER SURFACE SKIN IS CRACKED. REPLACED SKIN PER SRM 51-30-8. (M)SDR IXXA0400089SSkin · damagedDURING A ROUTINE C CHECK INSPECTION, FOUND LT WING OTBD FLAP L/E UPPER PART HAS INTERIM REPAIR AT XE 415.000. REPAIRS WERE ACCOMPLISHED BY PERFORMING MAJOR REPAIRS IAW DC8 SRM 57-1-0 PAGE 1, DC8 SRM 57-7-1 FIG 4. REMOVED PLATING WITH INTERIM REPAIR IAW DC8 SSDR C1HA200483006Slat · crackedNR 6 SLAT CRACK AT FASTENER HOLE AND 2 GOUGES IN WEDGE EXTRUSION. SDR SWAA041452Skin · delaminatedDURING SCHEDULED A1 CHECK, FOUND LT WING L/E NR 2 L/E SLAT DELAMINATED. REMOVED AND REPLACED NR 2 L/E SLAT PER MM.SDR 2004UALA00580Wedge · delaminatedLWR SURFACE OF TRAILING EDGE WEDGE DELAMINATED. MAJOR REPAIR ACCOMPLISHED. REPAIRED TRAILING EDGE WEDGE.SDR 04FDEA01356Support Bracket · crackedRIGHT WING NR 3 SLAT TRACK LOWER FAIRING OUTBOARD SUPPORT BRACKET IS CRACKED. REMOVED AND REPLACED SUPPORT BRACKET IAW SRM 51-31-01 AND AMM 27-80-01-4 AT MAE.SDR DHL2004754014Bracket · crackedDURING A C-CHECK, NR 5 L/E FLAP ACTUATOR TRUNNION BRACKET SUPPORT CRACK INDICATION INBOARD SIDE. REMOVED DAMAGED BRACKET AND FABBED NEW FROM 7075-T6.063 PO 900861 DIM 9.5 X 6.25 INCH IAW 727 SRM 57-20-2 FIG 1. BRACKET TREATED & PRIMED IAW 727 SRM 51-10-2 ANDSDR DHL2004754013Support Bracket · crackedDURING C-CHECK, THE FOLLOWING DISCREPANCIES WERE NOTED; NR 2 L/E FLAP ACTUATOR TRUNNION BRACKET SUPPORT IS CRACKED O/B SIDE. REMOVED DAMAGED BRACKET IAW B727 SRM 51-30-2, FABRICATED NEW BRACKET DIM 6.125 X 8.75 FROM 7075T6.063 PO 900861 IAW B727 SRM 57-20-2 FSDR 04FDEA01272Panel · crackedLEFT WING - NR 3 L/E SLAT INBOARD SIDE PANEL FOUND WITH CRACK ACROSS LIGHTENING HOLE. LEFT WING - NR 3 L/E SLAT INBOARD SIDE CRACKED PANEL REMOVED AND NEW PANEL INSTALLED AS PER SRM 51-35-01 VOL 2 & SRM 51-35-02 VOL 2.SDR DHL2004743004Rib · crackedLT WING NR 2 LEADING EDGE SLAT RIBS AT ROD END HAS 2 SMALL CRACKS. ONE ON EACH SIDE OF ROD END. REPAIRED BRACKETS IAW B-727 SRM 51-40-3, MATERIAL USED 2024T3, .051, RIVETS USED: CR3223-5-2, 10 EA, NAS 517-3-5 SCREWS, 2 EA. PO NR 400004986. .SDR 2004UALA00579Wedge · delaminatedTRAILING EDGE WEDGE DELAMINATED AT LWR INBOARD END FROM RUBBING ON LEADING EDGE WING SKIN. MAJOR REPAIR ACCOMPLISHED. REPAIRED WEDGE.SDR SWAA041382Skin · delaminatedDURING SCHEDULED 1/2D CHECK, FOUND NR 4 L/E SLAT DELAMINATED. REPAIRED NR 4 L/E SLAT PER MM.SDR DHL2004754012Actuator · crackedDURING A C-CHECK, NR 4 SLAT WS 405 INTERIOR RIBS AT ACTUATOR ATTACH INBOARD & OUTBOARD CRACKED RIBS. REMOVED NR 4 L/E SLAT IAW B727 M/M 27-81-11. REMOVED DAMAGE RIBS FROM NR 4 SLAT WS 405 INBOARD & OUTBOARD RIBS AT ACTUATOR ATTACH POINT IAW B727 SRM 51-30-2,SDR DHL2004754011Mount Bracket · crackedDURING A C-CHECK, NR 2 SLAT ACT ATTACH OUTBOARD BRACKET INSIDE PLATE HAS NEW CRACK. REMOVED CRACKED STIFFENER AND FABBED NEW FROM BAC 1503-100145, PO 3111123 DIM 9.2 X 3.5 INCHES IAW S/B 727-57-0130 REV 3 FIG 1. PART TREATED & PRIMED IAW 727 SRM 51-10-2 & ISDR UPS04242427Bracket · crackedINSPECTION TYPE: C BRACKET INSIDE NR 7 SLAT AT OB TRACK CRACKED. REPAIRED IAW SRM 57-50-3.SDR DHL2004754005Fitting · crackedDURING A C-CHECK, NR 2 SLAT WS 629 AT ATT ACT HAS INBD ATTACH FRAME CRACKED. REMOVED & REPLACED DAMAGED ATTACH FITTINGS P/N 65-17310-3, PO 4175400 & P/N 65-17310-4, PO 422356 IAW 727 SRM 51-30-2.SDR DHL2004754003Mount · crackedDURING A C-CHECK, RT WING NR 6 KRUEGER FLAP ACTUATOR MOUNT IS CRACKED AT LOWER CORNERS. REMOVED ACTUATOR MOUNT, FABRICATED REPLACEMENT PART 7075-T6, .063, PO 900861 (8 X 3 INCH) IAW B727 SRM 57-20-02 FIG 1. TREATED AND PRIMED IAW B727 SRM 51-10-02 AND INSTALSDR 04FDEA01210Bracket · crackedRT WING LEADING EDGE NR 16 SLAT TRACK ASSY INBOARD BRACKET WEB CRACKED. INBD BRACKET REMOVED AS PER SRM 51-31-01-VOL II AND INSTALLED NEW BRACKET AS PER SRM 51-33-01 VOL II & SRM 51-35-01 VOL II. CARRIED OUT OPERATION CHECK AS PER AMM 27-80-00 AND FOUND SATSDR 04FDEA01209Bracket · crackedLEFT WING LEADING EDGE NR 16 SLAT TRACK ASSY INBOARD BRACKET WEB CRACKED. RIB REMOVED AND REPLACED AS PER SRM 51-31-01 VOL II AND BUSHING REPAIR CARRIED OUT AS PER EA 1-5710-76771 - WINGS - LEADING EDGE SLAT SUPPORT NR 16 (LT) - BUSHING REPAIR.SDR SWAA041314Skin · delaminatedDURING SCHEDULED 1/2D CHECK, FOUND NR 2 L/E SLAT, OUTBOARD END DELAMINATED. REPAIRED NR 2 SLAT PER SRM.SDR SWAA041319Skin · delaminatedDURING SCHEDULED C4 CHECK, FOUND RT NR 4 L/E SLAT INBOARD END DELAMINATED. REMOVED AND REPLACED NR 4 L/E SLAT PER MM.SDR SWAA041250Wedge · delaminatedDURING SCHEDULED C4 CHECK, FOUND RT WING NR 6 L/E SLAT UPPER WEDGE PANEL DELAMINATED. REMOVED AND REPLACED NR 6 L/E SLAT PER MM.SDR SWAA041249Wedge · delaminatedDURING SCHEDULED C4 CHECK, FOUND RT WING NR 5 L/E SLAT UPPER WEDGE PANEL DELAMINATED. REMOVED AND REPLACED NR 5 L/E SLAT PER MM.SDR SWAA041248Wedge · delaminatedDURING SCHEDULED C4 CHECK, FOUND RT WING NR 4 L/E SLAT UPPER WEDGE PANEL DELAMINATED. REMOVED AND REPLACED NR 4 L/E SLAT PER MM.SDR 2004UALA00560Wedge · delaminatedTRAILING EDGE WEDGE DELAMINATED LWR INBOARD SURFACE. MAJOR REPAIR ACCOMPLISHED. REPAIRED WEDGE.SDR 04FDEA01112Structure · gougedCOMPLY WITH EA 7-5750-77346; WINGS - LEADING EDGE NR 6 SLAT TRAILING EDGE REPAIR, SLAT STA 167.9. COMPLIED WITH EA 7-5750-77346; REPAIRED NR 6 SLAT TRAILING EDGE.SDR 04FDEA001112Skin · gougedCOMPLY WITH EA 7-5750-77346; WINGS, LEADING EDGE NR 6 SLAT TRAILING EDGE REPAIR, SLAT STA 167.9. COMPLIED WITH EA 7-5750-77346; REPAIRED NR 6 SLAT TRAILING EDGE.SDR AUS20040359Skin · delaminated(AUS) RT LE SLAT T/E WEDGE DELAMINATED ON IB END UPPER FACE. AREA OF DELAMINATION APPROXIMATELY 70 SQ IN. FOUND DURING INSPECTION IAW AD/767/73.
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