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 ASAA1149627Skin · delaminatedRIGHT WING LEADING EDGE NR 6 SLAT UPPER SURFACE INBOARD END DELAMINATED. REPAIRED SLAT UPPER SURFACE INBOARD END IAW B737 400 SRM 51 70 10 REPAIR 4.SDR ASAA1149626Skin · chafedRIGHT WING LEADING EDGE NR 4 SLAT LOWER SURFACE INBOARD AFT CORNER REPAIR DOUBLER CHAFED. REPAIRED SLAT LOWER SURFACE INBOARD AFT CORNER IAW B737 400 SRM 51 70 10 REPAIR 4.SDR ASAA1149542Skin · chafedNR 3 SLAT LOWER SURFACE CHAFED INBOARD AFT CORNER. REMOVED DAMAGED SKIN SECTION FABRICATED REPAIR PARTS AND BONDED IAW B737 400 SRM 51 70 10 REPAIR 4.SDR ASAA1149397Slat · delaminatedNR 1 SLAT OUTBOARD AFT CORNER DELAMINATED. REMOVED DAMAGED SECTION FABRICATED REPAIR PARTS AND BONDED IN IAW B737 400 SRM 51 70 10 REPAIR 4.SDR ABXA2011032324Rib · crackedNR 8 SLAT OUTBOARD TRACK CUTOUT OUTBOARD L/E RIB IS CRACKED. CRACK IS .7 INCH LONG. REMOVED AND INSTALLED NEW RIB IAW B767 SRM 51-40-02. AIRCRAFT WAS GROUNDED.SDR ABXA2011032321Rib · crackedINBOARD RIB OF NR 4 SLAT INBOARD DRIVE ROD AT STA 561 HAS CRACKED CLOSE OUT PAN IN NOSE RIB AREA. REMOVED AND REPLACED RIB P/N 114T2512-9AX IAW B767 SRM 51-40-02. AIRCRAFT WAS GROUNDED.SDR UALA2011032401407Skin · damagedWING LEADING EDGE AT RT SLAT NR 3 AREA HAS A DENT OF 0.125 IN DEPTH AND A SCRATCH OF 0.500 IN BY 0.250 IN. WHILE REMOVING RT LEADING EDGE SKIN FOUND CRACK AT NR 3 SLAT STOP CUTOUT AT FASTENER HOLE. CUT OUT DAMAGE .875 INCH HOLE FOR CIRCULAR PATCH REPAIR. SKSDR UALA2011032201385Wedge · damagedFLT CREW ON WALKAROUND REPORTS METAL PROTRUDING FROM LEFT WING UPPER WINGROOT. NR 5 L/E SLAT HAS 4 X 4 INCH TEAR TO SKIN PANEL ON UPPER SURFACE ADJACENT TO TRAILING EDGE WEDGE. REMOVED NR 5 L/E SLAT FOR REPAIR TO SHOP. REPLACED LEADING EDGE SLAT NR 5 PER MMSDR SWAA112100Slat · delaminatedDURING SCHEDULED 16Y CHECK, FOUND LT WING I/B END NR 2 SLAT DELAMINATED. REPAIRED SLAT PER SRM.SDR AALA20110321AFW04Slat · damagedDAMAGE WAS FOUND TO THE NUMBER 7 SLAT OUTBOARD EDGE AT APPROXIMATE WING STATION 345 NEAR THE TRAILING EDGE. ACCOMPLISHED REPAIR PER MAJOR EA COMP-57-015661.SDR SWAA111988Skin · crackedDURING SCHEDULED 10Y CHECK, FOUND LT WING L/E NR 3 SLAT SKIN CRACKED. REMOVED AND REPLACED SKIN PER EA.SDR SWAA111987Skin · crackedDURING SCHEDULED 10Y CHECK, FOUND LT WING L/E NR 2 SLAT SKIN CRACKED. REMOVED AND REPLACED SKIN PER EA.SDR FDEA201103211093Structure · crackedWHEN REMOVING NR 7 SLAT OTBD DRIVE TRACK, INBD DRIVE TRACK DOOR FOUND INCURED DAMAGE, CRACKED. CRACKED DOOR R & R IAW AMM 20-11-00-2, REV 97. REPAIR IS CLASSIFIED AS MINOR.SDR SWAA111926Skin · crackedDURING SCHEDULED OTS CHECK, FOUND LT WING NR 3 SLAT LOWER SKIN CRACKED. REPAIRED SKIN PER SRM.SDR ABXA2011031919Rib · corrodedLEADING EDGE RIB I/B OF NR 4 SLAT I/B AUX TRACK HAS CORROSION AROUND NUT PLATES. REMOVED AND REPLACED STRUT P/N 114T2208-15AX IAW B767-200 SRM 51-40-02.SDR FDEA201103191083Structure · chafedRT WING KREUGER FLAP FOLDING NOSE OTBD EDGE, SURFACE HAS 1 IN CHAFED MARK. REPAIRED RT WING KREUGER FLAP IAW EA6-5750-145582 INSTRUCTIONS.SDR ABXA2011031823Rib · corrodedNR 10 SLAT OUTBOARD AUX TRACK INBOARD RIB IS CORRODED. REMOVED AND REPLACED RIB IAW B767 SRM 51-40-02. AIRCRAFT WAS GROUNDED.SDR AALA20110318TUL12Skin · crackedCRACK ON NUMBER 2 SLAT COVE SKIN AT OUTBOARD DRIVE TRACK. INSTALLED EXTERNAL DOUBLER PER AARD 57-43-00-4.SDR UALA2011031701293Structure · dentedBIRD STRIKE NR 3 SLAT DAMAGE. DENT STARTS AT RIB COVERING 5 RIVETS GOING 16.5 IN TOWARDS OTBD. CENTER OF DENT STARTS ON TOP AT RIVETS COVERING 10 RIVETS GOING FWD TOWARDS LEADING EDGE. RPL'D NR 3 LT SLAT.SDR CALA2011032400173Skin · delaminatedNR 10 SLAT UPPER SURFACE I/B CORNER FOUND DELAMINATED. METAL HOT BOND REPAIR PERFORMED AS PER SRM 51-70-10 REPAIR 4 FIG 202.SDR FDEA201103161024Skin · misrepairedAGING ACFT - EXISTING REPAIR FOUND AT LT NR4 SLAT INNER SKIN EXISTING REPAIR AT LT WING 4 SLAT INBD SKIN EVALUATED AND FOUND NOT IAW ANY APPROVED DATA. NR4 SLAT R & R IAW AMM 27-80-30-4, REV 69.2. COMPLIED WITH "EO 1-5100-7-5001 A5 PART 1, REPAIR CLASSIFIESDR FDEA201103161015Skin · damagedFASTENERS ON AFT SIDE OF INBD END OF RT INBD SLAT CONTACTING L/E SKIN LEAVING DEEP WEAR MARKS FROM FASTENER HEADS. REPAIR CARRIED OUT IAW SRM 57-41-12 FIG 204 SCHEME BSDR FDEA201103161014Skin · misrepairedLT NR 2 SLAT LOWER SKIN TRACK 5-6 LOCATION STATES IN RECORDS, A FLUSH REPAIR IAW SRM 57-43-11, FIG 202. AIRCRAFT PHYSICALY HAS A DOUBLER REPAIR PATCH IN THIS POSITION WHICH IS NOT IAW STATED SRM. REPAIR DOUBLER INSTALLED IAW EA6-5750-149426.SDR AALA20110316TUL06Skin · crackedCRACK ON NUMBER 2 SLAT COVE SKIN AT OUTBOARD DRIVE TRACK. INSTALLED EXTERNAL DOUBLER PER AARD 57-43-00-4.SDR SWAA111940Flap · crackedDURING SCHEDULED HC2 CHECK, FOUND RT WING KRUEGER FLAP CRACKED AT STA 196.8461. REPAIRED FLAP PER EA.SDR FDEA201103150980Skin · corrodedLT WING SLAT NR 1, UPPER SKIN T/E HAS SEVERAL CORROSION- SPOTS. REPAIRED NR1 SLAT IAW SRM 51-70-10.SDR FDEA201103150979Skin · corrodedLT WING SLAT NR 1, UPPER SKIN T/E HAS SEVERAL CORROSION- SPOTS. REPAIRED NR 1 SLAT IAW SRM 51-70-10.SDR FDEA201103140967Hinge Fitting · corrodedBOTH LT AND RT KRUEGER FLAP BULL NOSE ASSY'S HAVE SEVERELY CORRODED HINGE ARM FITTINGS. THIS IS CONSIDERED PRIMARY STRUCTURE. KRUEGER FLAP HINGE ARMS REPLACED.SDR USAA2011040591328Skin · crackedCLT - Q5/QX6 - CRACKS ON NR 1 SLAT LOWER AFT TRAILING EDGE SKIN. REPLACED NR 1 SLAT IAW B737 AMM 27-81-21-4.SDR USAA2011040491325Support Bracket · brokenCLT - Q5/QX6 - INTERNAL SUPPORT BRACKET FOR NR 4 SLAT OUTBOARD HEAT TUBE IS BROKEN. REPLACED NR 4 SLAT IAW B737 AMM 27-81-21-4.SDR DALA1123651812Wedge · dentedLT WING NR 6 SLAT UPPER WEDGE EXTERNAL SURFACE FOUND DENT MARK. METAL HOT BOND REPAIR PERFORMED AS PER SRM 51-70-10, REPAIR 4 FIG 202.SDR FOTR2102212402Skin · gougedRT WING NR 5 SLAT T/E SKIN BY INBD HOOK IS GOUGED. CLEANED AREA ON NR 5 SLAT IAW MM12-40-00, FOUND AREA OF GOUGE TO BE OUT OF LIMITS IAW SRM 57-50-1, FIG 2. FRABRICATED REPAIR PLATE FROM 7075-T6, .125 PO 90095-66, MEA 6.5 X 3.1885 IAW SRM 57-50-3, INSTALLED DSDR FOTR2102212322Fence · cracked4 SLAT FENCE CRACKED LWR DRAIN HOLE SANDED, CLEANED AND PREPPED AREA IAW SRM 51-40-9 PARA. 7. APPLIED REPAIR TO PREPPED AREA IAW SRM 51-40-9, PARA 7 AND REFINISHED SURFACE OF REPAIR IAW SRM 51-40-9, PARA 7.SDR FOTR2102212315Skin · crackedNR 2 SLAT LWR SKIN CRACKED AT INBD TRACK TO SKIN ATTACH FASTENERS. CUT OUT DAMAGED AREA DIM 3.3" X 5.55" IAW SRM 57-50-3, FIG 1. FABRICATED REPAIR DOUBLER FROM 7075T6 .080 PO 90011142 DIM 6.75" X 7.4" AND FILLER FROM 7075T6 .080 PO90011142 DIM 5.55" X 3.3" SDR CALA2011032500193Skin · crackedRT WING LEADING EDGE SLAT NR 9 I/B SURFACE SKIN FASTENER HOLE FOUND CRACK AS MARK. RT WING LEADING EDGE SLAT NR 9 I/B SURFACE SKIN REPAIRED AS PER SRM 57-43-01 REPAIR 2 FIG 201 AND HFEC NIL CRACK FOUND.SDR CALA2011032500192Skin · crackedRT WING L/E SLAT NR 9 O/B SURFACE SKIN FASTENER HOLE FOUND CRACKED AS MARKED. RT WING L/E SLAT NR 9 O/B SURFACE SKIN REPAIRED AS PER SRM 57-43-01 REPAIR 2 FIG 201 AND HFEC NIL CRACK FOUND.SDR CALA2011032500190Skin · crackedLT WING - NR 4 SLAT FWD SKIN I/B SECTION FASTENER HOLE FOUND CRACKED AS MARKED. LT WING NR 4 SLAT SKIN I/B SECTION LOCATION REPAIRED AS PER SRM 57-43-01 REPAIR 2 FIG 201 AND HFEC NIL CRACK FOUND.SDR CALA2011032500188Skin · crackedLT WING NR 3 SLAT FWD SKIN I/B SECTION FASTENER HOLE FOUND CRACKED AS MARKED. LT WING NR 3 SLAT SKIN I/B SECTION PATCH REPAIRED AS PER SRM 57-43-01 REPAIR 2 FIG 201 AND HFEC NIL CRACK FOUND.SDR SWAA111804Skin · crackedDURING SCHEDULED 24Y CHECK, FOUND LT WING NR 2 SLAT SKIN CRACKED. REPAIRED SKIN PER SRM.SDR CALA2011032500191Skin · crackedLT WING NR 3 SLAT FWD SKIN O/B SECTION FASTENER HOLE FOUND CRACKED AS MARKED. LT WING NR 3 SLAT SKIN O/B SECTION LOCATION REPAIRED AS PER SRM 57-43-01 REPAIR 2 FIG 201 AND HFEC NIL CRACK FOUND.SDR SWAA111759Skin · crackedDURING SCHEDULED 24Y CHECK, FOUND RT WING NR 5 SLAT SKIN CRACKED. REPAIRED SKIN PER MM.SDR SWAA111757Slat · delaminatedDURING SCHEDULED 24Y CHECK, FOUND RT WING NR 4 SLAT I/B END DELAMINATED. REPAIRED AFT FLAP PER SRM.SDR SWAA111687Skin · delaminatedDURING SCHEDULED 20Y CHECK, FOUND LT WING NR 4 SLAT I/B END UPPER SKIN DELAMINATED. REPAIRED SKIN PER SRM.SDR SWAA111656Slat · crackedDURING SCHEDULED MV2 CHECK, FOUND LT WING L/E NR 1 SLAT CRACKED. REPAIRED SLAT PER SRM.SDR SWAA111627Slat · delaminatedDURING SCHEDULED 24Y CHECK, FOUND RT WING NR 5 SLAT I/B END DELAMINATED. REMOVED AND REPLACED NR 5 SLAT PER MM.SDR SWAA111620Slat · delaminatedDURING SCHEDULED 16Y CHECK, FOUND RT WING NR 4 SLAT I/B END DELAMINATED. REPAIRED SLAT PER SRM.SDR SWAA111619Slat · delaminatedDURING SCHEDULED 16Y CHECK, FOUND RT WING NR 6 SLAT I/B END DELAMINATED. REPAIRED SLAT PER SRM.SDR TAMF201103110081Skin · dentedDURING C4 CHECK RT WING, SLAT NR 9, NOSE SKIN DENT AND SCRATCH REPAIR, REPAIR WAS PERFORMED WITH EWO 767-57-078.SDR SWAA111834Skin · crackedDURING SCHEDULED 22Y CHECK, RT WING NR 6 SLAT SKIN CRACKED AT OUTBOARD EDGE. REPAIRED SKIN PER SRM.SDR DALA1118529873Skin · chafedRIGHT WING NR 2 SLAT CENTER SLAT TRACK L/EDGE SKIN CHAFED I/B SIDE OF CUTOUT. BLENDED CHAFE 3"X 2". FOUND TO BE OUT OF LIMITS IAW DC9 SRM 57-01 WITH AN ORIGINAL THICKNESS .190 IAW DC9 SRM 57-31-1 AND A MAT LOSS OF .062. REMAINING THICKNESS .128 CUT OUT DAMA
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