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 DL757010477Slat Track · damagedLE FLAP ASSY ON FLAP RETRACTION - DECLARED EMERGENCY AND LANDED WITH NO INCIDENT. MTC IN WORK - FOUND NR 2 LE SLAT TRACK BROKEN LOOSE ON ARRIVAL.SDR SWAA010869Skin · delaminatedDURING SCHEDULED C2 CHECK, FOUND NR 2 L/E SLAT SKIN DISBONDED. REMOVED AND REPLACED NR 2 SLAT PER MM.SDR SWAA010851Wedge · delaminatedDURING SCHEDULED C4 CHECK, FOUND LT WING NR 3 L/E SLAT T/E WEDGE DISBONDED, 75 PERCENT OF PANEL. REMOVED AND REPLACED NR 3 SLAT PER MM.SDR AWXA0001506Fitting · gougedRT WING NR 1 SLAT OUTBOARD T/E LOWER SURFACE GOUGED. REPAIRED IAW AWA ER 26-5711-01072-JS2.SDR SWAA010803Wedge · crackedDURING SCHEDULED SERVICE CHECK, FOUND NR 3 L/E SLAT CRACKED AT T/E WEDGE, 66 OUTBD FROM INBD END. REMOVED AND REPLACED NR 3 SLAT PER MM.SDR TWAA0105104Skin · dentedDURING CHECK-C MAINT ON LT WING MIDDLE OF NUMBER 4 SLAT HAD DENT FILLED WITH FILLER, 6 IN BY 4 IN. CLEANED AREA OF FILLER AND ACCOMP NDT CHECK FOR CRACKS. NO CRACKS FOUND. REFILLED AREA PER SRM 57-03 FIG 14B, SHEET 2. ALSO SRM 57-40-102 PAGE 201 FOR APPROVSDR DL72W010423Angle · crackedCOVE SKIN ATTACH ANGLE CRACKED BELOW TAI DUCT NBR 8 SLAT. REPAIR PER MM 57-54-000-8SDR SWAA010778Skin · crackedDURING SCHEDULED C4 CHECK, FOUND NR 1 L/E SLAT LOWER SKIN CRACKED AT 2 FASTENER HOLES, AFT ROW, OUTBD MAIN TRACK. REPAIRED SLAT SKIN.SDR SWAA010757Skin · crackedDURING SCHEDULED C3 CHECK, FOUND NR 2 L/E SLAT SKIN CRACKED AT 3 FASTENER HOLES ON AFT ROW. REPAIRED SKIN PER SRM.SDR SWAA010756Skin · crackedDURING SCHEDULED C3 CHECK, FOUND NR 1 L/E SLAT SKIN CRACKED AT AFT ROW OF FASTENERS, INBD OF OUTBD AUX TRACK. REPAIRED SKIN PER SRM.SDR SWAA010712Skin · crackedDURING SCHEDULED C2 CHECK, FOUND NR 6 L/E SLAT SKIN CRACKED AT LOWER AFT ROW OF FASTENERS, 24 INBD OF ACTUATOR. REPAIRED SKIN PER SRM.SDR 2001UALA00263Rib · crackedNR 6 SLAT ACTUATOR MOUNT RIBS CRACKED ON BOTH INBOARD AND OUTBOARD SIDES.SDR TWAA0104504Skin · delaminatedDURING CHECK-C MAINT ON THE RT WING THE NUMBER 8 L/E SLAT, 61 IN FROM OTBD END AND 7 IN FROM THE WEDGE T/E, HAD 3.5 BY 5.75 INCH DELAMINATION. INSTALLED 8 IN BY 8 IN METAL TO METAL HOT BOND REPAIR PER SRM 51-70-09.SDR SWAA010691Skin · crackedDURING SCHEDULED C4 CHECK, FOUND NR 2 L/E SLAT SKIN CRACKED AT 2 FASTENER HOLES, 18 OUTBD OF ACTUATOR. REPAIRED SLAT PER SRM.SDR DHL2001741509Panel · crackedNR 3 L/E SLAT ACTUATOR ROD END ATTACH AREA ADJACENT PANEL CRACKED. REMOVED INTERNAL PANEL AT NR 3 L/E SLOT ACTUATOR AS PER B 727 SRM 51-30-2. ROUTE OUT CRACK AS PER B 727 SRM 51-10-1, MAT LOSS .010. INSTALLED DOUBLER REPAIR AS PER B 727 SRM 51-40 2 FIG AT. SDR SWAA010653Skin · delaminatedDURING SCHEDULED SERVICE CHECK, FOUND NR 4 L/E SLAT DELAMINATED AT INBOARD UPPER T/E. REMOVED AND REPLACED NR 4 SLAT PER MM.SDR SWAA010664Wedge · delaminatedDURING SCHEDULED C4 CHECK, FOUND NR 4 L/E SLAT INBOARD AND NR 5 L/E SLAT OUTBOARD T/E WEDGES DELAMINATED. REPAIRED WEDGES PER SRM.SDR SWAA010641Skin · crackedDURING SCHEDULED C2 CHECK, FOUND NR 5 L/E SLAT HAS 5 SKIN CRACKS AT AFT ROW OF FASTENERS, INBOARD OF ACTUATOR. REPAIRED SLAT PER SRM.SDR SWAA010636Skin · crackedDURING SCHEDULED 1/4D CHECK, FOUND NR 6 L/E SLAT SKIN CRACKED AT OUTBOARD TRACK CUTOUT, AFT ROW OF RIVETS. REMOVED AND REPLACED NR 6 SLAT PER PER MM.SDR 2001UALA00226Rib · crackedNR 5 SLAT ACTUATOR ATTACHMENT RIBS ARE CRACKED. REPLACED RIBS PER BAC DWG 65-17276, GN MM 1-0-0-23, AND INSTALLED PER SRM 51-30-02.SDR 2001UALA00199Rib · crackedNR 6 SLAT UNDER INBOARD PANEL RIB IS CRACKED. REPAIRED SLAT RIB PER SRM 70-57-56-01-JD. INSTALLED ACCESS PANELS PER GN MM 1-0-1-2.SDR SWAA010604Skin · crackedDURING SCHEDULED 1/4D CHECK, FOUND 2 SKIN CRACKS AT NR 1 L/E SLAT FASTENER HOLES. REPAIRED SLAT PER SRM.SDR DL72W010340Attach Angle · crackedA .5 INCH VISABLE CRACK O/B END NR 2 SLAT IN COVE SKIN ATTACH ANGLE. REPAIR PER M/M 57-54-000-8.SDR DL72S010334Rib · crackedFOUND ON F1 LETTER CK, NR 6 SLAT ACTUATOR ATTACH RIBS CRACKED INBD AND OUTBD SIDES OF SLAT ACT ROD END. REPAIRED PER MM 57-54-000-8.SDR SWAA010566Skin · delaminatedDURING SCHEDULED PM CHECK, FOUND LT WING L/E OUTBD FORE FLAP DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.SDR SWAA010565Flap · brokenDURING SCHEDULED SERVICE CHECK, FOUND LT WING L/E NR 1 KRUEGER FLAP OUTBD END BROKEN AT SPRING LOADED FLAP DOOR. REMOVED AND REPLACED KRUEGER FLAP PER MM.SDR SWAA010549Rib · crackedDURING SCHEDULED C1 CHECK, FOUND LT WING L/E OUTBD KRUEGER FLAP RIB CRACKED AT THIRD RIB FROM OUTBD END. REMOVED AND REPLACED KRUEGER FLAP PER MM.SDR 2001UALA00194Slat · crackedNR 6 SLAT CRACKED UNDER ANTI-ICE DUCT. REPAIRED SLAT CRACK PER SM-OR-70-57-56-01-AR11.SDR DL72E010320Angle · crackedA .25 INCH CRACK AT FWD SIDE OF NR 6 L/E FLAP ACTUATOR MOUNT BOX O/B TRUNNION UPPER ATTACH ANGLE. REPAIRED PER MM.SDR DL72E010319Stiffener · crackedFWD SPAR STIFFENER CRACKED AT I/B SIDE OF NR 6 SLAT O/B TRACK. REPLACED STIFFENER PER MM 57-20-021-8.SDR DL72E010318Stiffener · crackedFWD SPAR VERTICAL STIFFENER CRACKED AT I/B SIDE OF NR 6 SLAT I/B TRACK. REPLACED STIFFENER PER MM 57-20-021-8.SDR 0100749868Stop · brokenDURING APPROACH WHEN SLATS EXTENDED, AIRCRAFT EXPERIENCED A ROLL TO THE LEFT AND THE SLAT DISAGREEMENT LIGHT ILLUMINATED. FOLLOWED COM PROCEDURES AND ACCOMPLISHED A SAFE NO SLAT LANDING AT JAX. MAINTENANCE FOUND THE MECHANICAL STOP ON NR 9R SLAT DOOR BROKEN SDR AWXA0001399Skin · crackedLT WING NR 3 SLAT CRACKED 2.4 INCHES LONG O/B EDGE LOWER T/E SKIN. REMOVED NR 3 SLAT O/B PANEL IAW SRM 51-40-02; REMOVED DAMAGE, INSP BY HFEC - NO CRACKS NOTED. FABED AND INSTALLED DOUBLER AND FILLER IAW SRM 51-20-05, 51-40-02 AND REINSTALLED PANEL.SDR SWAA010531Plate · delaminatedDURING SCHEDULED C1 CHECK, FOUND LT WING L/E INBD FORE FLAP REPAIR PLATE DISBONDED. REMOVED AND REPLACED FORE FLAP PER MM.SDR DL72E010301Attach Angle · crackedA .5 INCH VISIBLE CRACK AT I/B STOP ATTACH ANGLE ON NR 7 L/E SLAT. REPAIRED PER MM 57-54-000-8.SDR RRXA10777Panel · delaminatedDURING A MAINTENANCE VISIT FOUND DELAMINATION DAMAGE TO L/H WING #3 SPOILER PANEL AT #3 SPOILER, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED ARE IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 MM 27-SDR EISA20010055Web · crackedDURING ROUTINE C-CHECK INSPECTION FOUND LEFT WING NR 1 SLAT II/B WEB FOR ACTUATOR ATTACH POINT CRACKED. FABRICATED AND INSTALLED REPAIR DOUBLER, ALODINED, AND PRIMED IAW SRM 51-40-3, 51-10-2, 51-30-2, 27-81-11, SPM 20-50-01.SDR SWAA010458Slat · crackedDURING SCHEDULED 1/4D CHECK, FOUND NR 5 L/E SLAT CRACKED AT LOWER SKIN, 7 INBD OF ACTUATOR. REPAIRED SLAT PER SRM.SDR CALA0100117Skin · crackedINSPECTION FOUND LT WING NR 3 SLAT COVER SKIN CRACKED AROUND FASTENER HOLE AT WBL 254.0. THE CRACKED SKIN WAS CUT OUT. DOUBLER AND FILLER WERE INSTALLED IAW SRM 57-43-01, PAGE 216.SDR RRXA10775Panel · delaminatedDURING A MAINTENANCE VISIT FOUND DELAMINATION DAMAGE TO LT. WING #2 SPOILER PANEL AT #2 PANEL, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 MM 27-6SDR UPS01435351Structure · corrodedINSPECTION TYPE:C, RIGHT WING I/B FOREFLAP IS CORRODED BEYOND LIMITS WBL 128.4675 TO WBL 445. REMOVED AND REPLACED RIGHT I/B FOREFLAP.SDR DL72W010250Stiffener · crackedWING L/E SPAR STIFFENER CRACKED O/B SIDE NR 3 SLAT O/B TRACK. REPAIR PER M/M 57-20-21-8.SDR DL72W010249Stiffener · crackedWING L/E SPAR STIFFENER CRACKED I/B SIDE NR 3 SLAT O/B TRACK. REPAIR PER M/M 57-20-021-8.SDR SWAA010419Slat · crackedDURING SCHEDULED 1/4D CHECK, FOUND NR 2 L/E SLAT T/E SKIN CRACKED AT RIVETS HEADS, 3 INBD OF T-DUCT. REPAIRED SLAT PER SRM.SDR MWEA010149Rib · wornLEFT NR 4 SLAT OUTBOARD BUSHINGS AT THE COMMON LINK WORN. REMOVED AND REPLACED RIB.SDR 2001UALA00097Rib · crackedNR 4 SLAT OUTBOARD SIDE OF ACTUATOR ROD END ATTACH POINT INTERNAL WEB CRACKED. *S/D* REPAIRED RIB IN ACCORDANCE WITH OVERHAUL MANUAL.SDR 01FDEA00095Skin · crackedDURING ROUTINE INSP, RIGHT WING NR 5 SLAT OUTBOARD UP STOP PAD CUTOUT FOUND CRACKED. *S/D* REMOVED, REPLACED AND FAB PER IAW BAC 727 SRM 51-40-2.SDR UPS01435027Skin · crackedINSPECTION TYPE:C, RIGHT WING NR 12 K-FLAP BULLNOSE INNER SKIN IS CRACKED AT INBOARD END. REPAIRED SKIN IAW SRM 57-50-03 FIG 8.SDR 01FDEA00089Rib · crackedDURING ROUTINE INSP, NR 5 SLAT INBOARD ACTUATOR ATTACH RIB FOUND CRACKED. *S/D* BLENDED, TREATED AND PRIMED PER IAW BAC 727 SRM 57-50-1, 51-10-2.SDR DL72S011218Angle · crackedAT HMV FOUND ANGLE CRACKED UNDER I/B UP STOP NR 6 SLAT.
Back to JASC 5754