JASC 5754
Service difficulty reports · 17,348
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 P5CA9500530Bracket · corrosionCORROSION ON U-CHANNEL FAIRING ON HINGE BRACKET, INBOARD HINGE OF NR 14 LEADING EDGE FLAP. MANUFACTURED BRACKET PER BOEING SRM 51-20-01, INSTALLED PER 51-30-02.SDR DL72W952933Angle · crackedAT HMV, NR 4 SLAT ANGLE FOR CLOSEOUT PANEL CRACKED AT FWD LOWER EDGE AT RIB NR 12 AND NR 13. REPAIRED PER MM 57-54-0.SDR P5CA9500584Fitting · corrodedCORROSION IN BOTH HINGES FITTING SIDES RIGHT WING KRUGER LEADING EDGE FLAP NR 15. MANUFACTURED PLATE SUPPORT PER 51-20-01, INSTALLED PER 51-30-02.SDR CAL950589Rib · corrodedGSO - INSPECTION FOUND THE OUTBOARD RIB/WEB AND BOLT HOLE BUSHINGS CORRODED AT THE NR 3 LEADING EDGE SLAT OUTBOARD TRACK TO SLAT ATTACH POINT. THE CORROSION WAS CLEANED UP AND REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 57-50-3 AND SRM 51-30-2. (X)SDR CAL950588Intercostal · crackedGSO - THE NR 6 SLAT INTERIOR HAD TWO EACH INTERCOSTALS CRACKED AT INBOARD SLAT TRACK ATTACH FITTING. EACH CRACK WAS APPROXIMATELY .50 INCH LONG. A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-30-2 AND SRM 57-50-3. (X)SDR CAL950586Intercostal · crackedGSO - INSPECTION FOUND A .75 INCH CRACK IN INTERCOSTAL OF NR 2 SLAT INBOARD SLAT TRACK, AT SLAT TRACK ATTACH FITTING AREA. THE CRACK WAS STOP-DRILLED. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 57-30-3 AND SRM 51-30-2. (X)SDR 95FDEA00864Skin · corrodedCORROSION (75C002-00) NR 1 K-FLAP DATA PLATE. REPAIRED CORROSION DAMAGE AT NR 1 K-FLAP DATA PLATE AND RELOCATED DATA PLATE IAW FEDEX SRM 57-50-3 AND SRM 27-57-010.SDR DL72S952856Angle · crackedCOVE SKIN ANGLE CRACKED UNDER NR 3 SLAT TAI DUCT. FOUND DURING B-2 LTR CK. REPAIRED PER 57-54-0, PAR 2.SDR DL76S952822Te Wedge · delaminatedDURING SHOP INSPECTION, SLAT PANEL WAS FOUND WITH T/E WEDGE DELAMINATED. REPLACED WEDGE PER SRM 57-43-37.SDR DL757952834Skin · delaminatedDURING SHOP INSPECTION, NR 9 SLAT PANEL WAS FOUND WITH DELAMINATION TO T/E WEDGE. REPAIRED PER SRM 57-42-03.SDR DL72S952979Rib · crackedAT HMV, NR 4 SLAT, NR 18 RIB WAS FOUND CRACKED, REPAIRED PER MM 57-54-0, PG 807.SDR DL72L952839Angle · crackedNR 2 SLAT COVE SKIN ANGLE BELOW TAI DUCT CRACKED, FOUND AT B2 LTR CK. REPAIRED PER MM 57-54-0.SDR SWAA950500Te Skin · crackedDURING SCHEDULED D-CHECK, FOUND NR 3 SLAT CRACKED AT T/E SKIN O/B OF ACTUATOR AND NR 4 SLAT CRACKED AT LOWER T/E SKIN, I/B OF ACTUATOR. REPAIRED PER BOEING DRAWING 65C30133 AND BOEING STRUCTURAL REPAIR MANUAL.SDR DL757952841Te Wedge · delaminatedDURING INSP, THE T/E WEDGE ON NR 3 SLAT WAS FOUND TO BE DELAMINATED. THE WEDGE WAS REPLACED PER SRM 57-43-02.SDR DL72S952821Angle · crackedFOUND DURING A-1 LETTER CHECK, NR 2 L/E SLAT COVE SKIN ANGLE CRACKED AT TAI DUCT. REPAIRED PER MM 57-54-0 PAR 5A.SDR DL72S952820Rib · crackedFOUND DURING A-1 LETTER CHECK, NR 2 L/E SLAT L/E RIB CRACKED, .5 INCH I/B OF ACTUATOR MOUNT. REPAIRED PER MM 57-54-0 PAR 3.SDR DL72S952819Angle · crackedFOUND DURING A-1 LETTER CHECK, NR 2 L/E SLAT COVE SKIN ANGLE CRACKED AT I/B STOP PAD. REPAIRED PER MM 57-54-0 PAR 12.SDR DL757952774T/E Wedge · delaminatedDURING SHOP INSPECTION, NR 3 L/E SLAT WAS FOUND WITH DELAMINATION DAMAGE TO T/E WEDGE. REPLACED WEDGE PER SRM 57-43-02 FIG 202.SDR DL72S953890Heat Shield · crackedDURING SHOP INSPECTION, NR 3 L/E SLAT WAS FOUND WITH CRACK IN HEAT SHIELD AT RIVETS BETWEEN RIBS NR 5, 6, 7, 10 AND 11. REPAIRED PER MM 57-54-0 FIG 814.SDR DL72S953889Ribs · crackedDURING SHOP INSPECTION, NR 3 L/E SLAT WAS FOUND WITH CRACKING IN THE I/B AND O/B SUPPORT RIBS, FOR BOTH I/B AND O/B SLAT TRACK ATTACH FITTINGS. ACCOMPLISHED REPAIRS PER MM 57-54-0.SDR DL72S953888Ribs · crackedDURING SHOP INSPECTION, NR 3 L/E SLAT WAS FOUND WITH RIBS NR 11 AND NR 13 CRACKED. REPAIRED PER MM 57-54-0.SDR DL72W952861Rib · crackedDURING SHOP INSPECTION, NR 3 SLAT PANEL WAS FOUND WITH L/E RIB NR 17 CRACKED. REPAIRED PER MM 57-54-00 FIG 809.SDR DL72W952782Rib · crackedDURING SHOP INSPECTION, NR 3 L/E SLAT WAS FOUND WITH SUPPORT RIB NR 9 CRACKED. REPAIRED PER SRM 57-54-0 FIG 805.SDR DL72W952753L/E Rib · crackedA .5 INCH CRACK ON NR 4 SLAT L/E RIBS AT I/B AND O/B SIDES OF TRACK. FOUND DURING A-2 LETTER CHECK. REPAIRED PER MM 57-54-0.SDR USAA950889Web · crackedPIT - DURING Q-3/CX-2 INSPECTION, FOUND .75 INCH CRACK IN WEB OF RHS FLAP AT XFS341. INSTALLED .090 INCH FILLER AND .063 INCH 7075T6 DOUBLER PER SRM 57-01 AND USAIR EA 30788. (M)SDR UPS203641Stiffener · crackedWHILE IN C-CHECK, MAINTENANCE FOUND CRACKED STIFFENER R/W L/E NR 6 SLAT I/B TRACK I/B SIDE LOWER END SLAT STA 135.5. REPAIRED IAW SRM 51-30-2, 51-10-2, M/M 28-11-21, 36-00-01, OHM 20-50-01.SDR P5CA9500105Te Fiber · deterioratedRIGHT WING NR 25 LEADING EDGE FLAP VARIABLE CAMBER TRAILING EDGE FIBER IS DETERIORATED. REPAIRED PER BOEING SRM 51-40-09.SDR DL757952740Skin · dentedDURING LETTER CHECK FROM SCHEDULED MTC, INSTALLED PERMANENT REPAIR FOR DENT ON NR 9 L/E SLAT, PER SRM 57-43-02.SDR DL72W952977Rib · crackedNR 7 SLAT CRACK IN LOWER END OF AFT FLANGE ON SLAT RIB 6 FROM INBD END. INSTALLED REPAIR DOUBLERS PER MM 57-54-0. FOUND AT HMV.SDR DL767953118Skin · delaminatedNR 12 SLAT T/E WEDGE HAS TEMPORARY REPAIR 7 INCHES FROM O/B END. N/R NR 896, CHANGED WEDGE PER CMM 57-43-41. N/R NR 7738, T/E WEDGE DENTED 40 INCHES FROM O/B END UPPER SURFACE. CHANGED WEDGE PER CMM 57-43-41. REPAIRS ACCOMPLISHED AT SHOP VISIT.SDR DL72W952999Ribs · crackedAT HMV, FOUND NR 6 SLAT RIBS 8, 9, 11, 14, 15, 18, 19 CRACKED. INSTALLED REPAIRS ON ALL RIBS PER MM 57-54-0, FIG 814.SDR DL72W952998Angle · crackedAT HMV, FOUND NR 7 SLAT ANGLE CRACKED ON LWR TE IB OF TRACK. FABRICATED AND INSTALLED NEW ANGLE PER MM 57-54-0, PG 812.SDR DL72W952976Rib · crackedNR 5 SLAT CRACKED AT LOWER END OF AFT FLANGE ON RIB 19. REMOVED DAMAGE AND INSTALLED REPAIR DOUBLER PER MM 57-54-0, PG 818 AND PG 819. FOUND AT HMV.SDR DL72W952855Angle · crackedNR 1 L/E SLAT CRACKED, .25 INCH CRACK IN ANGLE ON LOWER T/E 7 INCHES FROM I/B END. REPAIRED PER MM 57-54-0, FOUND AT HMV.SDR DL72W952847Panel · crackedAT HMV, FOUND .5 INCH CRACK IN I/B UPPER CORNER OF WEB CUTOUT FOR FWD END OF ANTI-ICE DUCT OF NR 1 SLAT PANEL. STOP DRILLED CRACK, FABRICATED DOUBLER PER M/M 57-54-0.SDR DL757952754Te Wedge · delaminatedDURING HMV NR 7 SLAT T/E WEDGE WAS FOUND TO HAVE DELAMINATION ON THE T/E WEDGE 33 FROM THE I/B END.SDR DL757952681Panel · delaminatedDURING SHOP INSPECTION, SLAT PANEL WAS FOUND WITH T/E WEDGE DELAMINATED. WEDGE WAS REPLACED PER SRM 57-43-02.SDR DL72W952687Rib · crackedFOUND DURING E-2 LETTER CHECK, NR 4 L/E SLAT L/E RIB CRACKED I/B OF ACTUATOR ROD END AND RIB CRACKED O/B OF ACTUATOR ROD END. REPAIRED PER MM 57-54-0 PAR 3.SDR DL72E952881Rib · crackedDURING SHOP INSPECTION, NR 5 L/E SLAT WAS FOUND WITH L/E SUPPORT RIB NR 5 CRACKED. REPAIRED PER SRM 57-54-0 PG 814.SDR DL72K952653Angle · crackedFOUND DURING A-2 LETTER CHECK, NR 4 L/E SLAT LOWER COVE SKIN ATTACH ANGLE CRACKED AT O/B END. REPAIRED PER MM 57-54-0 PAR 5A.SDR DL72K952652Skin · crackedFOUND DURING A-2 LETTER CHECK, NR 2 L/E SLAT LOWER COVE SKIN ATTACH ANGLE CRACKED AT O/B END. REPAIRED PER MM 57-54-0 PAR 5A.SDR DL72K952651Skin · crackedFOUND DURING A-2 LETTER CHECK, NR 1 L/E SLAT LOWER COVE SKIN ATTACH ANGLE CRACKED AT I/B STOP PAD. REPAIRED PER MM 57-54-0 PG 12.SDR DL72S952646Skin · crackedCOVE SKIN ATTACH ANGLE CRACKED UNDER ANTI-ICE DUCT NR 2 SLAT, FOUND DURING E-1 LETTER CHECK. REPAIRED PER M/M 57-54-0 PG 80.SDR DL72S952645Angle · crackedFOUND DURING E-1 LETTER CHECK, COVE SKIN ATTACH ANGLE CRACKED UNDER ANTI-ICE DUCT AT NR 3 SLAT. REPAIRED PER M/M 57-54-0 PG 807A.SDR DL72W952631Fairing · crackedFOUND DURING E-2 LETTER CHECK, SEVERAL CRACKS AT NR 8 SLAT I/B TRACK FAIRING. REPAIRED PER MM 57-54-0.SDR UPS203512Guide Hooks · crackedWHILE IN C-CHECK, MAINTENANCE FOUND CRACKED AND WORN NR 1 SLAT I/B GUIDE HOOK. INSTALLED FABRICATED PARTS IAW SRM 57-50-3, 51-30-2, M/M 27-81-0.SDR UPS203511Guide Hooks · crackedWHILE IN C-CHECK, MAINTENANCE FOUND WORN AND CRACKED NR 5 SLAT GUIDE HOOKS. INSTALLED FABRICATED PARTS IAW SRM 57-30-3, M/M 27-81-11.SDR DL72W952571Angle · crackedFOUND DURING A-1 LETTER CHECK, 1.75 INCH CRACK IN ANGLE ON THE LOWER AFT SIDE I/B CORNER OF NR 6 SLAT. REPAIRED PER M/M 57-54-0 PG 807A.SDR DL72S952619Skin · crackedON WALK-AROUND FOUND CRACKS IN NR 5 KRUGER FLAP. CRACKS WERE REPAIRED PER SRM 57-50-3.SDR AWXA9500376Skin · crackedPHX - DURING SCHEDULED C8 INSPECTION, FOUND NR 1 SLAT LOWER L/E CRACKED AT RIVETS. FABRICATED AND INSTALLED REPAIRS IAW ER 2 57 55 33. TOTAL CYCLES 34804. (W)
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