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 aircraft_model_key = '73736N' 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 aircraft_model_key = '73736N' 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 2026F00172Windshield · crackedFLIGHT 650 CBB-VVI CRACKED WINDOW #R1 DURING DESCENT. CORRECTIVE ACTION: REMOVED AND REPLACED WINDOW #1 AND CHANGED CONTROL CABIN WINDOW HEAT. IN TEST NORMALSDR 2025F00017Battery · dischargedBOTH DC FAIL. LIGHTS ILLUMINATED. LOW BATTERY VOLTAGE. CANCELLED AIRCRAFT IN SLVR. CORRECTIVE ACTION: REMOVED AN REPLACED MAIN BATTERYSDR 2024F00268Control System · failedCANCELED FLIGHT 646 CBB/VVI DUE TO ENGINE #2 SLOW ACCELERATION IN DIFFERENTE PHASES OF FLIGHT AND HOT STARTS. CORRECTIVE ACTION: REMOVED AN INSTALLED MAIN ENGINE CONTROL MEC.SDR 2024F00183Tire · failedTIRE#2 TREAD LOSS. CANCELLED AIRCRAFT LEG CBB/TDD FLIGHT 466. CONDITIONAL INSPECTION PERFOMED. FOUND DAMAGE IN FLAP I NLEFT INBOARD FORE FLAP WITHIN LIMITS. LEFT INBOARD AFT FLAP REMOVED AND REPLACEDSDR 2024F00029A/C Pack · trippedQRF TO VVI DUE TO PACK TRIP OFF#2 LIGHT ILLUMINATE AFTER TAKE OFF. CORRECTIVE ACTION: PERFORMED ADJUSTMENT/TEST IAW AMM 21-51-00/501 SYST WORK PROPERLY ON GROUND WITH POWER PLANT TEST.SDR 2023F00010Fitting · corrodedMLG LH AND RH LUG FITTINGS WITH CORROSION DAMAGE LEFT SIDE: 0.070" AND 11HRS; 0.044" AT 10HRS; 0.049" AT 12HRS. RIGHT SIDE: 0.069" AT 12HRS,0.057" AT 11HRS.SDR 2022F00227Motor · failedTRAILING EDGE FLAP ASSYMETRY DURING TKEOFF, FLAPS ON THE RIGHT WING STUCK ON 1 AND FLAPS ON THE LEFT WING WENT UP. CORRECTIVE ACTION: HAS BEEN CHANGED FLAP HYDRAULIC MOTOR IAW AMM 27-51-57/401 AND TE FLAP BYPASS VALVE IAW AMM 27-52-82/401 AND PERFORMED OPERATISDR 2022F00232None · noneSTRONG NOISE AND VIBRATION DOOR 1L. CORRECTIVE ACTION:HAS BEEN CHANGED DOOR 1L IAW AMM 52-11-00/401 AND ADJUSTED TEST NORMAL IAW AMM 52-11-00/501SDR 2022F00127None · noneCRACKING ON STA 291.5 FRAME WEB - INTERCOSTAL STRAT CUTOUT AT STRINGER 14R. CRACKING ON STA 277 INTERCOSTAL - STRINGER 16R RADIUS TRIMOUT. THESE CRACKINGS WERE FOUND AS PER AD 2014-22-06SDR 2022F00009Relay · blockedLANDING GEAR LEVE WILL NOT MOVE UP AFTER TAKEOFF. LANDING GEAR DOWN, THERE IS NO ANY GREEN LIGHT INDICATORSSDR UIEA2021072201607Flap · damagedMULTIPLE AREAS OF DAMAGE ON LH IB FLAP ASSY, FOUND OUT OF LIMITS IAW B767 SRM 51-10-02. CUSTOMER REQUEST FLAP REPLACEMENT. REMOVED AND REPLACED LH IB FLAP ASSY AND OPS CHECK GOOD IAW B767 AMM 27-51-06-422-059.SDR CA1912050006Adapter · failed(CAN) FINAL APPROACH CONDUCTING LPV APPROACH AIRCRAFT WAS FULLY CONFIGURED AND STABLE ON APPROACH WITH LOCALIZER AND GLIDE SLOPE CAPTURED. EXACTLY WHILE CROSSING FAF GLIDE SLOPE HAD A LARGE UPWARD DEVIATION AND AUTOPILOT RAPIDLY PITCHED AIRCRAFT NOSE UP. I IMMSDR CA140627001Mechanism · stiff(CAN) PILOT REPORTED: F/O YOKE FEELS STIFF DURING CONTROL CHECK. ONLY STIFF WITH LT AILERON, F/O SIDE. FOUND STIFFNESS AND NOISE EMANATING FROM AILERON TRANSFER CONTROL MECHANISM ASSY. MECHANISM ASSEMBLY REPLACED.SDR 7AHR201404152372Floor Support · corrodedAFT CARGO FLOOR STRUCTURE AT LBL 14.00 AT STA 727A, 727D, 747, 787 AND 847 CARGO TIE DOWN FITTINGS CORRODED. REMOVED CORROSION ON FITTINGS AND FABRICATED NEW SECTION OF CARGO TRACK THAT WAS OUT OF LIMITS IAW SRM 51-40-02, PGS 2, 3 & 4.SDR 7AHR201404152449Floorbeam · corrodedMAIN CABIN FLOORBEAM AT BS 994, LBL 33-44 CORRODED. REMOVED CORROSION IN AREA AND REPAIRED IAW SRM 51-40-02.SDR 7AHR201404152522Floor Support · corrodedMAIN CABIN FLOOR SUPPORT CHANNEL HAS CORROSION AT BS 956, RBL 50. REMOVED CORROSION, FABRICATED FLOOR SUPPORTS AND INSTALLED IAW SRM 51-10-07 AND 53-40-02.SDR 7AHR201404152462Floorbeam · corrodedAFT CARGO FLOORBEAM HAS CORROSION AT BS 867, BL 0. REMOVED CORROSION AND INSTALLED REPAIR IAW SRM 53-00-07, FIG 202, PGS 208-214.SDR 7AHR201404152451Frame · corrodedRIGHT FUSELAGE FRAME AT BS 994, RBL 48 HAS CORROSION ON FWD & INBD SIDE OF FRAME. REMOVED CORROSION AND INSTALLED REPAIR TO FRAME IAW SRM 56-60-15 & 51-40-05.SDR 7AHR201404152335Frame · corrodedAFT CARGO BAY, FRAME BS 747 BETWEEN S28L & 27R CORRODED. REMOVED CORROSION FROM AREAS, REPAIRED IAW SRM 53-00-07, FIG 201.SDR 7AHR201404152532Seat Track · corrodedSEAT TRACK CORRODED AT BS 390, RBL 45. R & R SECTION OF SEAT TRACK IAW SRM 53-00-52.SDR 7AHR201404152106Intercostal · crackedLEFT INBD MIDFLAP INTERCOSTAL INBD END OF OTBD TORQUE TUBE IS CRACKED. REMOVED INTERCOSTAL IAW SRM 51-40-02. INTERCOSTAL FABRICATED IAW DWG 57-14105-01, REV NEW. INSTALLED INTERCOSTAL IAW SRM 51-40-02.SDR 7AHR201404082448Floorbeam · corrodedMAIN CABIN FLOORBEAM AT BS 986.5 HAS CORROSION AROUND NUTPLATE HOLES FROM RBL 4-44 UPPER CAP. INSTALLED REPAIR IAW SRM 53-60-51.SDR 7AHR201404082445Floor Support · corrodedMAIN CABIN FLOOR SUPPORT AT BS 967 LBL 16 HAS CORROSION ON UPPER SURFACE. REMOVED CORROSION AND INSTALLED REPAIR IAW SRM 53-60-51.SDR 7AHR548B2444Floor Support · corrodedMAIN CABIN FLOOR SUPPORT AT BS 952, LBL 16 HAS CORROSION ON UPPER SURFACE. REMOVED CORROSION, FABRICATED AND INSTALLED FLOOR SUPPORT IAW SRM 51-40-2.SDR 7AHR201404082442Floorbeam · corrodedMAIN CABIN FLOORBEAM HAS CORROSION BS 948, RBL 4. REMOVED CORROSION AND INSTALLED REPAIR TO IAW SRM 53-30-51, REPAIR 2.SDR 7AHR201404082374Striker · corrodedFWD CARGO DOOR SURROUND STRUCTURE AFT EDGE BS 490 LOWER AFT DOOR STOP HAS BROKEN STRIKER PLATE AND FITTING IS CORRODER. R & R STRIKER PLATE AND FITTING IAW SRM 51-40-02.SDR 7AHR201404082339Frame · corrodedAFT CARGO BAY FRAME AT BS 807 HAS CORROSION FROM STRINGER 27L - 28RT. REMOVED CORROSION IAW SRM 53-00-07, FIG 207, REPAIR 17.SDR 7AHR201404082334Shear Tie · corrodedAFT CARGO BAY, BS 727E SHEAR TIE HAS CORROSION BETWEEN STRINGERS 27-28RT. REMOVED CORROSION AND FABRICATED NEW SHEAR TIE IAW SRM 53-00-07, FIG 202, REPAIR 17.SDR 7AHR201404082288Intercostal · corrodedFWD CARGO BAY INTERCOSTAL BS 420-440 RT HAS DOUBLE DRILLED HOLES AND CORROSION. R & R IAW SRM 53-30-04, FIG 1 AND 51-40-02.SDR F3LA200500011Roller · wornMAINTENANCE REPORTED R1 DOOR HARD TO CLOSE. REPLACED GUIDE ARM ROLLER PER MM 52-61-20. ADJUSTED R1 DOOR PER MM 52-41-00. REMOVED AND REINSTALLED R1 DOOR SLIDE PER MM 25-61-35. REMOVED AND REINSTALLED R1 DOOR LINER PER MM 52-41-31. REMOVED AND REINSTALLED RSDR F3LA200300191Actuator · inoperativeDURING C-7 CHECK, INSPECTION REPORTED NR 3 SLAT ACTUATOR FAILED LOCK PIN TEST. REPLACED NR 3 SLAT ACTUATOR IAW MM 27-81-41 AND ACCOMPLISHED LE SLAT ACTUATOR LOCK PIN TEST AND LE SLAT ALTERNATE SYSTEM TESTS IAW TASK CARD 5-2710 AND MM 27-81-00.SDR F3LA200300190Skin · dentedDURING C-7 CHECK, INSPECTION REPORTED CREASED DENT IN EXTERNAL FUSELAGE SKIN AT STA 368, 4 IN BELOW STR 18R. REPAIRED PER SRM 53-00-01 FIG 202.SDR F3LA200300188Flap Track · corrodedDURING C-7 CHECK, INSPECTION REPORTED CORROSION ON NR 7 OTBD FLAP TRACK ASSY. REMOVED EXISTING BUSHINGS TO EXPOSE ALL SURFACES TO INSPECTION. INSPECTED FLAP TRACK PER OHM 57-53-15. MACHINED THE HOLE FORWARD OF BUSHING NR 60 PER SOPM 20-10-01 AND SOPM 20-10-SDR F3LA200300187Battery Pack · failedDURING C-7 CHECK, INSPECTION REPORTED FWD GALLEY DOOR ESCAPE SLIDE BATTERY PACK FAILED VOLTAGE TEST. REPLACED FWD GALLEY DOOR ESCAPE SLIDE.SDR F3LA200300186Intercostal · crackedDURING C-7 CHECK, INSPECTION REPORTED MAIN DECK FLOOR INTERCOSTAL CRACKED BETWEEN STA 294 AND STA 312 AT RBL 32. REPLACED DAMAGED UPPER CHORD OF FLOOR INTERCOSTAL PER SRM 51-40-2.SDR F3LA200300185Oxygen Bottle · dischargedDURING C-7 CHECK, INSPECTION REPORTED SEAT 7 ABC OXYGEN CANISTER DISCHARGED. REPLACED OXYGEN GENERATOR CANISTER PER MM 35-22-11, PAGE 201, STEPS 1-3 AND MM 35-22-11, PAGE 401, STEPS 1-3.SDR F3LA200300184Module · faultyDURING C-7 CHECK, INSPECTION REPORTED FIRE WARN LIGHT ON P-7, ENG 1/2 OVERHEAT LIGHTS ON P-8 AND CONTROL CABIN ALARM BELL DID NOT OPERATE IN STEPS 1 G-3 AND 1 G-7 OF FIRE WARNING SYSTEM TEST. TEST 1 G-10 PASSED. REPLACED FIRE DETECTION MODULE PER MM 26-10-01SDR F3LA200300183Frame · crackedDURING C-7 CHECK, INSPECTION REPORTED FRAME CRACKED AT BIN RAIL ATTACH BRACKET HOLE, STA 907, BETWEEN STR 8L AND 9L. REPAIRED PER SRM 53-00-07 FIG 202, STEPS 1-10.SDR F3LA200300182Shear Tie · corrodedDURING C-7 CHECK, INSPECTION REPORTED SHEAR TIE IN FWD CARGO COMPARTMENT CORRODED AT STA 500B, BETWEEN STR 28L AND 28R. REPAIRED PER SRM 53-00-07.SDR F3LA200300181Shear Tie · corrodedDURING C-7 CHECK, INSPECTION REPORTED SHEARTIE IN FWD CARGO COMPARTMENT CORRODED AT STA 500B, BETWEEN STR 27R AND 28R. REPAIRED IAW SRM 53-00-07.SDR F3LA200200394Strap · corrodedDURING C-6 CHECK, INSPECTION REPORTED FILLER/STRAP CORRODED BETWEEN STA 787 AND 807, RBL 20 ABOVE STR 25-R. REPLACED FILLER/STRAP PER SRM 51-40-02 AND 51-10-02.SDR F3LA200200393Strap · corrodedDURING C-6 CHECK, INSPECTION REPORTED CORROSION ON AFT CARGO DOOR LOWER SILL STRAP, STA. 774 TO 858, RBL 20. REPLACED SILL STRAP PER SRM 51-40-07 AND 51-10-02.SDR F3LA200200392Web · corrodedDURING C-6 CHECK, INSPECTION REPORTED WEB BETWEEN STA 794.3 AND 847, STR 25-R, CORRODED AROUND SEVERAL NUT PLATE HOLES. REPLACED AND INSTALLED WEB PER SRM 51-40-02 AND 51-10-02.SDR F3LA200200391Angle · corrodedDURING C-6 CHECK, INSPECTION REPORTED CORROSION ON L-ANGLE IN FWD CARGO COMPARTMENT, STA 500D, LBL 29 TO RBL 21. REPAIRED ANGLE PER SRM 51-40-02, 51-40-05 AND 51-10-02.SDR F3LA200200396Support Angle · gougedDURING C-6 CHECK, INSPECTION REPORTED SUPPORT ANGLE ON AFT SIDE OF AFT DOOR LATCH CUTOUT GOUGED ON APU DOOR. FABRICATED NEW SUPPORT ANGLE PER SRM 52-40-02 AND 51-70-11. ALODINED AND PRIMED PER MM 51-21-41 AND SOPM 20-41-02. INSTALLED NEW ANGLE PER SRM 52-40SDR F3LA200200395Cowl Door · chafedDURING C-6 CHECK, INSPECTION REPORTED PREVIOUS REPAIR ON LT. SECTION OF APU COWL DOOR CHAFFED/GROOVED. REMOVED ADDITIONAL DAMAGE FOUND AT EDGE OF PREVIOUS REPAIR. FABRICATED NEW DOUBLER TO ENCOMPASS NEW CUTOUT IN SKIN PER SRM 52-40-02, 52-40-01, MM 51-21-41 SDR F3LA200200250Shutoff Valve · failedAIR TURNBACK. FLIGHT CREW REPORTED WING/BODY OVERHEAT ILLUMINATED IN FLIGHT. COMPLIED WITH CHECKLIST AND LIGHT REMAINED ILLUMINATED. PRESSURE IN RT DUCT 10 PSI, WHICH DECREASED TO 5 PSI WHEN THRUST LEVER REDUCED IN POWER. SHUT DOWN NR 2 ENGINE AND MONITORESDR F3LA200100123Wire · brokenPRIOR TO DEPARTURE, FLIGHT CREW REPORTED EMERGENCY EXIT FLOOR PATH WIRING EXPOSED AT ROW 15. SPLICED BROKEN WIRE PER STANDARD PRACTICES 20-30-12, PERFORMED OPERATIONAL TEST OF EMERGENCY LIGHT SYSTEM AND CHECKED OKAY.SDR F3LA200000277Fitting · corrodedDURING C-4 CHECK, INSPECTION REPORTED CORROSION AROUND RT. AFT LAVATORY OTBD AFT FLOOR MOUNT. MAINTENANCE FABRICATED AND REPLACED NEW FITTING PER EA 25-737-108.SDR F3LA99050Battery · dischargedDEN - DURING C-CHECK INSPECTION REPORTED R-2 EMERGENCY ESCAPE SLIDE BATTERY FAILED VOLTAGE TEST. REPLACED R-2 EMERGENCY ESCAPE SLIDE. CYCLES: 2,635. (X)
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