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 GAIA04122Rib · crackedDURING C-CHECK INSPECTION FOUND NR 6 SLAT INTERIOR RIB CRACKED. REF FASI NR 86613 REMOVED AND REPLACED NR 6 SLAT INTERIOR RIB IAW SRM 57-50-2.SDR GAIA04121Skin · crackedDURING C-CHECK INSPECTION FOUND NR 5 SLAT L/E LOWER TO OB END PREVIOUS REPAIR MISS MATCH. REF FASI NR 86609, REMOVED PREVIOUS REPAIR FROM NR 5 SLAT. INSTALLED DOUBLER REPAIR IAW SRM 57-50-3, FIG 1.SDR GAIA04107Rib · crackedDURING C-CHECK INSPECTION FOUND NR 5 SLAT IB END RIB CRACKED. REF FASI NR, REMOVED, FABRICATED AND INSTALLED END RIB IAW SRM 57-50-2.SDR GAIA04095Skin · dentedDURING C-CHECK INSPECTION FOUND RT WING NR 5 SLAT L/E EXTERIOR SKIN RIPPLED AND DENTED ACROSS 2 RIB ASSY. REF FASI NR 86332, INSTALLED DOUBLER REPAIR IAW SRM 57-50-3, FIG 1.SDR GAIA04166Skin · crackedDURING C-CHECK INSPECTION FOUND RT WING NR 5 L/E SLAT LOWER SKIN CRACKED. REF FASI NR 87058, INSTALLED REPAIR DOUBLER IAW SRM 57-50-3, FIG 1.SDR GAIA04154Skin · crackedDURING C-CHECK INSPECTION, FOUND RT WING L/E AT NR 5 SLAT GUIDE CUTOUT CRACKED. REF FASI NR ACCOMPLISHED DOUBLER REPAIR IAW SRM 57-30-4.SDR USAA040803Skin · delaminatedPIT, Q5, TOP SKIN AND CORE BOND, 3.5 INCH AREA. DELAMINATION, NR 4 SLAT OB END TOP SURFACE. REMOVED DAMAGE, INSTALLED NEW CORE SECTION AND DOUBLER IAW SRM 51-70-10.SDR USAA040808Skin · delaminatedPIT, O5, TOP SKIN- CORE BOND, 2 INCH AREA. NR 4 SLAT IB END TOP SURFACE. REMOVED DAMAGED SKIN AND CORE, INSTALLED NEW CORE AND DOUBLER IAW SRM 51-70-10.SDR USAA040717Skin · chafedLOWER SKIN, 1 INCH LENGTH, CHAFE WEAR, NR 3 SLAT LOWER SURFACE TRAILING EDGE. REMOVED DAMAGED SKIN AND CORE, INSTALLED NEW DOUBLER, FILLER, NEW CORE, TOP DOUBLER, IAW SRM 51-70-10.SDR UPS04243211Skin · crackedINSPECTION TYPE: C, SUSPECT CRACK ON ANTI ICE SKIN AT I/B LOWER CORNER OF NR 3 KRUEGER FLAP. SKIN REPLACED IAW DRAWING 65-16225.SDR UPS04243210Structure · corrodedINSPECTION TYPE:C, PITTING CORROSION ON NR 3 KRUEGER FLAP BULLNOSE AT O/B LOWER MOUNT LUG. BULLNOSE REPLACED IAW OHM 57-51-21.SDR UPS04243205Skin · crackedINSPECTION TYPE:C, SUSPECT CRACK ON NR 7 SLAT OUTER SKIN AT O/B HOOK. HFEC CARRIED OUT ON SUSPECT CRACK IAW B727 NDTM 51-00-00 PT 6 FIG 4, 3 CRACKS NOTED AND MARKED ON SLAT. CRACKS FOUND TO BE CONTAINED WITHIN RIVET HOLES.SDR USAA040716Skin · delaminatedUPPER SKIN, 1.5 INCH SQ AREA DELAMINATED; NR 4 SLAT IB T/E. REMOVED DELAMINATED TOP SKIN AND CORE, INSTALLED NEW CORE, TOP DOUBLER AND REFINISHED IAW SRM 57-40-02 AND 51-70-10.SDR USAA040712Skin · delaminatedUPPER AND LOWER SKIN, 2 INCH SQUARE AREA, DELAMINATION, NR 4 SLAT CTR AREA NEAR AUX TRACK, TOP AND BOTTOM SKIN. REMOVED DELAMINATED TOP SKIN AND CORE MATERIAL. INSTALLED NEW CORE AND TOP DOUBLERS, REFINISHED IAW SRM 57-43-02.SDR UPS04843301Rib · crackedINSPECTION TYPE:C3 LEFT O/B SLOT UPPER DOOR CLOSE-OUT RIB AT I/B END BROKEN IN LOWER RADIUS. REMOVED AND REPLACED LEFT O/B SLOT CLOSE OUT RIB (PAN) IAW DC-8 SRM 51-1-21. REPAIRED LEFT O/B SLOT O/B END IAW SAA SK772-387.SDR DHL2004780505Skin · dentedDURING A "C" CHECK, NR 1 SLAT L/E SURFACE, WS 720 HAS DENT WITH CREASE. CUT OUT DING AREA NR 1 SLAT L/E SKIN APPROX 3/4 BY 1 1/4 INCH AND FABRICATED ONE DOUBLER APPROX4 3/4" BY 4 3/4" USING 2024-T3 .080 PO 9001135 IAW B727 SRM 57-50-3 FIG 1 ALODINED AND PRIMESDR DHL2004780503Rib · crackedDURING A C-CHECK THE FOLLOWING DISCREPANCIES WERE NOTED; NR 3 SLAT IB AND OB ACT. ATTACH FRAMES WS 515 ARE CRACKED IN RADIUS. STOP DRILLED CRACKS IAW SRM 57-50-3 FIG 9 ON NR 3 SLAT IB AND OB ACT. ATTACH FRAMES AT WS 515, FABRICATED REPAIR DOUBLERS FROM .032 CSDR AWXA200401046Skin · debondedDURING C-14 CHECK AN AREA OF DISBONDED SKIN WAS FOUND ON OB END OF NR 2 SLAT WEDGE BETWEEN WBL 246.0 AND WBL 254.0 LT. MAINTENANCE REMOVED PREVIOUS REPAIR, DAMAGED SKIN AND HONEYCOMB ON NR 2 SLAT; FABRICATED A FILLER AND DOUBLER; INSTALLED REPAIR PARTS IAW SRSDR USAA040718Skin · damagedTOP SKIN, CORE BOND, 1 INCH SQUARE AREA, NR 1 SLAT IB TE UPPER SURFACE. REMOVED TOP SKIN AND CORE, INSTALLED NEW CORE, TOP DOUBLER IAW SRM 51-70-10 AND 09.SDR DHL2004801535Skin · wornRT OUTBD FLAP L/E UPPER PLATING WORN AT XF 226.000 CTR PART (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1, SRM 57-7-1 FIG 4, TR NR 57-94. REMOVED WORN PLATING IAW SRM 51-1-21 PG 1, SRM 51-3-0 PG 1. FABRICATED NEW PLATING (AL 2024-T3 0.063) IAW SDR USAA040809Skin · delaminatedPIT, Q5, TOP SKIN - CORE BOND, 2 INCH AREA AT NR 5 SLAT T/E; 1 AT IB END AND 1 AT OB END. REMOVED DELAMINATED AREA, INSTALLED NEW TOP SKIN IAW SRM 51-70-10.SDR SWAA042582Skin · delaminatedDURING SCHEDULED C4 CHECK, FOUND RT WING NR 5 L/E SLAT, DELAMINATED. REPAIRED SLAT PER EA.SDR SWAA042560Stiffener · crackedDURING SCHEDULED HC2 CHECK, FOUND LEFT WING NR 1 L/E KRUGER FLAP OUTBOARD STIFFENER, CRACKED. REMOVED AND REPLACED FLAP PER MM. (M)SWAASDR CALA0400626Skin · crackedINSPECTION FOUND A 1 INCH CRACK IN NR 3 SLAT LOWER EXTERNAL SKIN AT WS 270. A REPAIR WAS INSTALLED IAW SRM 57-43-01.SDR IXXA0500020SSkin · damagedDURING A ROUTINE C CHECK INSPECTION, LT WING OUTBOARD FLAP LOWER PLATING HAS INTERIM REPAIR AT STA XF 1340.000. MAJOR REPAIR ACCOMPLISHED. REMOVED SKIN WITH INTERIM REPAIR ON IT IAW DC8 SRM 51-1-21 PG 1 DC8 SRM 51-3-0 PG1. FABRICATED NEW SKIN (AL2024130.050SDR USAA040819Skin · crackedPIT, Q5, SKIN WITH 1.2500 INCH CRACKS (3 EA). NR 1 SLAT, LOWER SURFACE AT ROW IB END 4TH RIVET. INSTALLED DOUBLER IAW SRM 57-43-01, FIG 206.SDR SWAA042507Wedge · delaminatedDURING SCHEDULED C4 CHECK, FOUND LT WING NR 2 L/E SLAT WEDGE DELAMINATED. REPAIRED NR 2 L/E SLAT WEDGE PER SRM.SDR 2004UALA00788Skin · debondedRIGHT INBOARD LEADING EDGE WEDGE DISBONDED FROM SLAT. *S/D* A SECTION OF THE NR 6 SLAT TRAILING EDGE WEDGE SEPARATED FROM THE SLAT ASSEMBLY. DURING DISASSEMBLE OF THE SLAT WEDGE FOR REPAIR, COMPONENT SHOP FOUND EVIDENCE OF CORROSION ON THE ALUMINUM HONEYCOMSDR USAA040582Skin · chippedPIT - FOUND SLAT WITH .25 INCH CHIP IN EDGE MATERIAL, NR 2 SLAT OUTBOARD OF INBOARD ALTERNATE TRACK. REMOVED DAMAGE, INSTALLED FILLER AND INTERNAL DOUBLER, NEW CORE AND TOP DOUBLER PER SRM 51-70-10. (M)SDR USAA040551Skin · crackedCLT - FOUND SLAT CRACKED.5 INCH, NR 9 SLAT COVE SKIN CRACKED AT OUTBOARD MAIN TRACK. FABRICATED NEW PANEL PER DRAWING 114N4003. (M)SDR USAA040552Skin · crackedCLT - FOUND SLAT CRACKED .75 INCH, NR 9 SLAT COVE SKIN CRACKED AT INBOARD MAIN TRACK. FABRICATED NEW PANEL PER DRAWING 114N4003. (M)SDR SWAA042424Skin · crackedDURING SCHEDULED RON, FOUND RT WING NR 6 L/E SLAT SKIN CRACKED. REPAIRED SKIN PER SRM.SDR SWAA042414Skin · crackedDURING SCHEDULED C4 CHECK, FOUND RIGHT WING NR 6 L/E SLAT SKIN CRACKED. REPAIRED RIGHT WING NR 6 L/E SLAT SKIN PER SRM.SDR SWAA042412Skin · crackedDURING SCHEDULED C1 CHECK, FOUND RT WING NR 4, 5, 6 L/E SLATS SKIN CRACKED. REPAIRED RT WING L/E SLATS SKIN PER EA.SDR CALA0400607Slat Track · crackedINSPECTION FOUND A 1.5 INCH CRACK IN NR 10 AUX TRACK SLAT CAN XOS 380.229. THE NR 10 AUX TRACK SLAT, CAN WAS REMOVED AND REPLACED IAW SRM 51-30-0 AND 51-20-0.SDR USAA040467Skin · crackedPIT - FOUND SKIN CRACKED .5 INCH, NR 6 SLAT LOWER SKIN AT O/B AUX ATTACH AREA. DOUBLER INSTALLED PER SRM 57-43-01. (M)SDR USAA040540Wedge · delaminatedCLT - FOUND WEDGE ASSEMBLY DELAMINATED 2 INCH BY 2 INCH AREA, NR 1 SLAT T/E WEDGE AT OUTBOARD AUX TRACK. INSTALLED DOUBLER PER SRM 51-70-10. (M)SDR USAA040442Attach Bracket · gougedPIT - FOUND ATTACH BRACKET GOUGED .625 INCH LONG BY .625 INCH WIDE BY .035 INCH DEEP, NR 2 SLAT ACTUATOR ATTACH BRACKET OUTBOARD SIDE INBOARD FACE. BLENDED PER TYPICAL REPAIR 57-20-0-0A. (M)SDR DHL2004745543Rib · crackedDURING A C-CHECK, NR 5 SLAT ACTUATOR ROD END O/B RIB IS CRACKED. REMOVED & REPLACED DAMAGED RIB 65-17276-9 PO 4175196 IAW 727 SRM 51-30-2 ON NR 5 SLAT O/B RIB.SDR SWAA042254Skin · delaminatedDURING SCHEDULED C4 CHECK, FOUND RIGHT WING NR 5 L/E SLAT WEDGE, DELAMINATED. REMOVED AND REPLACED NR 5 L/E SLAT WEDGE PER MM.SDR USAA040407Skin · crackedPIT - FOUND L/E SLAT CRACKED 3.5 INCHES, OUTBOARD, LOWER, TRAILING EDGE, NR 4 SLAT ASSEMBLY. INSTALLED DOUBLER PER SRM 57-43-01. (M)SDR SWAA042246Skin · delaminatedDURING SCHEDULED C4 CHECK, FOUND RIGHT WING NR 4 L/E SLAT WEDGE DELAMINATED. REMOVED AND REPLACED NR 4 L/E SLAT PER MM.SDR AMTA200400988Skin · delaminatedFOUND LEFT WING NR 3 SLAT, AFT SIDE, UPPER MID AREA HAS SEVERAL AREAS WITH DELAMINTION. REPAIRED NR 2 SLAT DELAMINATE AREA, LOWER INBOARD SURFACE IAW B757 SRM 51-70-10, REPAIR 7 FIG 16. (M)SDR DHL2004745542Support · crackedDURING A C-CHECK, NR 5 SLAT ACTUATOR ROD END I/B SUPPORT IS CRACKED. REMOVED NR 5 SLAT FOR ACCESS IAW 727 MM 27-81-11. REMOVED & REPLACED DAMAGED RIB P/N 65-17270U11 PO 4274276 IAW 727 SRM 51-30-2. REINSTALLED NR 5 SLAT IAW 727 MM 27-81-11.SDR WLDA200484Skin · puncturedDURING 4C-CHECK, WHILE PERFORMING J/C NR WA5740 FOUND A PUNCH HOLE ON RT WING LEADING EDGE SLAT NR 3 AT STA XOS435. PERFORMED REPAIR OF RT WING LEADING EDGE SLAT NR 3 IAW EGAT EI NR W2004A53B. CONDITION CHECK SATISFACTORY.SDR USAA040498Skin · delaminatedFOUND TOP SKIN/CORE BOND WITH 2 INCHES OF DELAMINATION, NR 2 SLAT TOP OUTBOARD T/E SURFACE. INSTALLED NEW CORE SECTION, TOP DOUBLER, SEAL END PER BOEING SRM 51-70-10. (M)SDR UPS04242994Rib · crackedINSPECTION TYPE: C, NR 6 SLAT I/B RIB AT ACTUATOR ROD END IS CRACKED. ROD END DISCONNECTED IAW MM 27-81-32. ROD END RIBS DERIVETED IAW SRM 51-30-02. RIBS REMOVED IAW SRM 51-30-02. ON REMOVAL O/B RIB AND CENTER CHANNEL FOUND CRACKED. NEW CENTER CHANNEL, I/SDR UPS04242964Access Panel · crackedINSPECTION TYPE: C, NR 7 SLAT INNER SKIN ACCESS PANEL, EXISTING REPAIR DOUBLER IS CRACKED. NR 7 SLAT INNER SKIN ACCESS PANEL REMOVED FOR ACCESS IAW SRM 51-30-02 & CRACKED DOUBLER REPLACED IAW SRM 51-30-02.SDR USAA040497Skin · delaminatedPIT - FOUND TOP SKIN/CORE BOND WITH DELAMINATION, 3 INCH BY 3.5 INCH AREA, NR 2 SLAT TOP SURFACE INBOARD END. REMOVED DAMAGE, INSTALLED NEW CORE SECTION, TOP DOUBLER, SEAL END PER BOEIGN SRM 51-70-10. (M)SDR SWAA042172Skin · crackedDURING SCHEDULED D-CHECK, FOUND RT WING NR 6 L/E SLAT SKIN, CRACKED. REPAIRED NR 6 L/E SLAT SKIN PER SRM.
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