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 = '727281' 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 = '727281' 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 VGCA20230814001Skin Panel · crackedCRACKED SKIN RESULTING FROM TOOLING DAMAGE AT L1 DOOR UPPER HINGE CUTOUT NEAR S-10LSDR VGCA20200923001Engine · fodAFTER TAKEOFF DURING CLIMB, NR 3 STARTED VIBRATING EXCESSIVELY. SHUT DOWN ENGINE AND RETURNED TO AIRPORT. UPON INSPECTION OF ENGINE, FOUND EVIDENCE OF FOD DAMAGE TO THE FAN BLADES. REMOVED ENGINE FROM SERVICE.SDR VGCA2019112619002Floorbeam · corrodedFLOOR BEAM UPPER CAP CORRODED AT STATION 870 BETWEEN LOWER BODY BUTTOCK LINE 44-55SDR VGCA2019112619008Fitting · corrodedAT STATION 950, THE LEFT BULKHEAD FITTING WAS CORRODED ON THE HORIZONTAL WEB ATTACH FLANGE AT WATER LINE 201.4SDR VGCA201911269007Skin · dentedDENT IN FUSELAGE SKIN AT STATION 348 BETWEEN STRINGER 4R AND 5RSDR VGCA2019112619006Spar · corrodedLEFT HORIZONTAL STABILIZER REAR SPAR CHORD CORRODED AT STABILIZER STATION 46SDR VGCA2019112619005Skin · corrodedCORROSION ON CENTER WING BOX UPPER SKIN PANEL AT BODY STATION 870, LEFT BODY LINE 67SDR VGCA2019112619004Floorbeam · corrodedFLOOR BEAM CORRODED AT STATION 920 AT LEFT BODY LINE 55SDR VGCA2019112619001Pressure Deck · corrodedLEFT MAIN LANDING GEAR WELL PRESSURE DECK UPPER WEB CORRODED BETWEEN BODY STATION 940-950 AND LOWER BODY BUTTOCK LINES 30-70.SDR VGCA2018043009007Skin · corrodedCORRODED UPPER T/E SKIN PANEL ON THE LT HORIZONTAL STAB UPPER REAR SPAR.SDR VGCA20170309006Frame · corrodedCORROSION FOUND ON THE FRAME AT BS 1142.SDR VGCA2017043009005Frame · crackedCRACK FOUND ON THE FRAME AT BS 480, STRINGERS 16L & 17L.SDR VGCA20170309003Butt Joint · corrodedCORROSION ON BUTTSTRAP, STR 29R, BS 1010, RT SIDE, AFT CARGO BAY.SDR VGCA20170309002Floorbeam · corrodedCORROSION ON THE WEB OF FLOORBEAM, BS 880, LBL 70 AND LBL 30.SDR VGCA2018043000001Beam · corrodedBS 1203, RBL 6 TRANSVERSE BEAM CORRODED.SDR CA140923009Circuit Breaker · failed(CAN) DURING TAXI, THE FLT CREW REPORTED THEY HAD NO HYDRAULIC PRESSURE FROM THE NR 1 HYDRAULIC B PUMP AND RETURNED TO THE RAMP. DURING MAINTENANCE TROUBLESHOOTING, THEY FOUND A SYS 40 AMP CIRCUIT BREAKER TRIPPED WITH SIGNS OF BEING BURNED. THE FAULTY BREAKESDR CA131007024Engine · flamed out(CAN) AT TOP OF DECENT, THE NR 2 ENGINE FLAMED OUT. ENGINE FLAMEOUT CHECKLIST WAS COMPLIED WITH AND THE ENGINE WAS RESTARTED. THE NR 2 ENGINE FUEL FILTER WAS INSPECTED, AND REPLACED. THE FUEL S/O VALVE WAS FUNCTION CHECKED WITH NO FAULTS FOUND. ENGINE RUNS SDR CA130803010Pressure Switch · malfunctioned(CAN) IN CRUISE, CREW NOTICED THE NR 3 ENGINE, LOW OIL PRESSURE/FILTER BYPASS, LIGHT ILLUMINATE. THE LOW OIL PRESSURE WARNING SYS WAS DEFERRED AND THE ACFT CONTINUED TO FINAL DESTINATION. MAINTENANCE REPLACED THE LOW OIL PRESSURE SWITCH AND THE ACFT RETURNEDSDR CA100712011Ball Joint · leakingNR 3 ENGINE FIRE INDICATION ON CLIMB. INFLIGHT SHUTDOWN CARRIED OUT AND AIRCRAFT RETURNED TO STATION. AIRCRAFT INSPECTED, 8TH AND 13TH STAGE DUCT BALL JOINTS (BETWEEN ENGINE AND PYLON) FOUND LEAKING, REPAIRED AND AIRCRAFT RETURNED TO SERVICE.SDR CA060309003Turbine Blades · failed(CAN) ON START UP THE CREW WAS UNABLE TO SUCCESSFULLY START THE NR 2 ENGINE. LARGE PIECES OF TURBINE BLADES WERE DISCOVERED LAYING IN THE TAILPIPE AREA. THE ENGINE WAS REPLACED AND A/C RETURNED TO SERVICE. (TC NR 20060309003)SDR C7WA200500118Switch · out of adjustAIR RETURN, RIGHT MAIN LANDING GEAR DOOR ANNUNCIATOR LIGHT CAME ON WHEN GEAR HANDLE IS PUT IN OFF POSITION. ADJUSTED RIGHT MAIN LANDING GEAR DOOR SWITCH. OPERATIONAL CHECKS GOOD PER B727 MM 32-62-11. (M)SDR AUS20030568Skin · separated(AUS) LT INBOARD FOREFLAP UPPER SKIN DISBONDED AND SEPARATED. SIZE OF DISBONDED PIECE APPROXIMATELY 355.6MM BY 177.8MM (14IN BY 7IN). SUSPECT CAUSED BY FOREIGN OBJECT LODGED BETWEEN FOREFLAP AND WING UPPER SURFACE. FOD.SDR AUS20021240Piston · broken(AUS) NO1 LEADING EDGE FLAP ACTUATOR PISTON SHEARED IN HALF. RETAINER PITTED, KEY CHROME CHIPPED AND RODEND REQUIRED REPLACEMENT.SDR AUS20021048Fitting · loose(AUS) NO2 ENGINE OIL QUANTITY INDICATION DROPPED FROM 7.6 LITRES (2GAL) TO 3.8 LITRES (1GAL) DURING APPROACH TO LAND. INVESTIGATION FOUND THAT THE AUXILIARY GEARBOX LP5 FITTING THREAD WAS DAMAGED AND LOOSE. PERSONNEL/MAINTENANCE ERROR.SDR AUS20020985Clamp · broken(AUS) LH PRIMARY HEAT EXCHANGER SUPPLY LINE CLAMP BROKEN.SDR AUS20020395Shim · corroded(AUS) LT ELEVATOR COUNTER WEIGHT SHIM PLATE FITTING HEAVILY CORRODEDZONE 93 STA ELE 210 TO STA ELE 222. CPCP - LEVEL 2 CORROSION.SDR AUS20020405Fitting · corroded(AUS) VERTICAL STABILISER BEARING ATTACHMENT FITTINGS CORRODED. CPCP -LEVEL 2 CORROSION.SDR AUS20020391Fitting · corroded(AUS) HORIZONTAL STABLISER BEARING ATTACHMENT FITTINGS CORRODED. CPCP - LEVEL 2 CORROSION.SDR AUS20020392Spar · corroded(AUS) HORIZONTAL STABILISER CENTRAL UPPER REAR SPAR AREA CORRODED ZONE97 STN BS1586.81. CPCP - LEVEL 2 CORROSION.SDR AUS20020390Bracket · corroded(AUS) LT WING BRACKET ATTACHED TO LOWER CHORD DELAMINATED FROM CORROSION ZONE 72, STN WS204.0. CPCP - LEVEL 2 CORROSION.SDR AUS20020397Sill · corroded(AUS) RT AFT SERVICE DOOR SILL CHORD CORRODED AT INNER EDGE ATTACHMENT POINT. LEVEL 2 CORROSION.SDR AUS20020396Sill · corroded(AUS) LT REAR ENTRY AND SERVICE DOOR AFT LOWER DOOR SILL CORRODED AT INNER PART OF SCUFF PLATE ZONE 24 STA 1035 TO STN 1065. CPCP -LEVEL 2 CORROSION.SDR AUS20020399Door Frame · corroded(AUS) CORROSION FOUND IN EMERGENCY DOOR EXIT (AFT OVERWING) AREA AT LOWER RH CORNER OF WEB ON HATCH ASSEMBLY FRAME ZONE 49 STN 825.95 TO STN 848.95. CPCP - LEVEL 2 CORROSION.SDR AUS20020394Shim · corroded(AUS) RT STABILISER ELEVATOR SHIM PLATE FITTINGS CORRODED AT COUNTERWEIGHT ATTACHMENT POINT. CPCP - LEVEL 2 CORROSION.SDR AUS20020393Skin · corroded(AUS) RT STABILISER SKIN CORRODED AT ATTACHMENT POINT TO REAR UPPER AUXILIARY SPAR CHORD ZONE 92, ELE 118.0 TO ELE 120.0. CPCP -LEVEL 2 CORROSION.SDR AUS20020398Seat Track · corroded(AUS) SEAT TRACK CORRODED AT ZONE 24 STA 1130 TO STA 1110 LBL 2475 LT.CPCP - LEVEL 2 CORROSION.SDR 20000425SH030Skin · corrodedFOUND DURING SCHEDULED B-SERVICE CHECK, CORROSION ON INTERNAL SKIN AROUND LEFT SCAN LIGHT. CORROSION POSSIBLY CAUSED BY MOISTURE AROUND THE EDGES OF LIGHT ASSY LEAKING INTO FUSELAGE AREA. (X)SDR 20000425SH029Stringer · crackedFOUND DURING SCHEDULED B-CHECK, CRACK AT END OF STR 15L BS 720C AFT OF SCAN LIGHT. STRINGER CRACK WAS POSSIBLY CAUSED BY CORROSION FOUND IN THIS AREA. (X)SDR 20000425SH028Stringer · crackedFOUND DURING SCHEDULED B-CHECK, STRINGER 15R CRACKED AT END. BS 720B FORWARD OF SCAN LIGHT. STRINGER CRACK WAS POSSIBLY CAUSED BY CORROSION FOUND IN THIS AREA. (X)SDR 20000425SH027Stringer · crackedFOUND DURING SCHEDULED B-SERVICE CHECK. CRACK AT END OF STR 15L, BS 720B FORWARD OF SCAN LIGHT. STRINGER CRACK POSSIBLY CAUSED BY CORROSION FOUND IN THIS AREA. (X)SDR 20000425SH026Floorbeam · misdrilledFOUND DURING SCHEDULED B-CHECK SERVICE CHECK AND ''G9'' BULKHEAD INSTALLATION, CABIN FLOORBEAM BS 344 UPER CAP HAS ELONGATED HOLES. SUBMITTER STATED HOLES MISDRILLED DURING PREVIOUS MODIFICATION. (X)SDR 20000425SH024Skin · corrodedFOUND DURING SCHEDULED B-SERVICE CHECK AND ACCOMPLISHMENT OF AD 85-24-02, SB 727-51-17. APPROXIMATELY 1.50 INCH DIAMETER AREA OF EXFOLIATING CORROSION AT WING CENTER SECTION SKIN ABOVE LT AFT HEAT EXCHANGER VIEWED THROUGH AFT OUTBOARD CUT IN FIBERGLASS PLENUMSDR 20000425SH023Skin · corrodedFOUND DURING SCHEDULED B-MAINTENANCE CHECK, INNER SKIN HAS INTERGRANULAR CORROSION. BS 720B BL 12 INCHES, STR 15R BELOW SCAN LIGHT. CORROSION POSSIBLE CAUSED BY MOISTURE AROUND THE EDGES OF THE LIGHT ASSY LEAKING INTO FUSELAGE AREA. (X)SDR 99ZZZM621Fuel Control · leakingUNSCHEDULED LANDING IN STL DUE TO HIGH FUEL FLOW ON NR 1 ENGINE. FUEL CONTROL WAS FOUND TO BE LEAKING AT MATING SURFACE AFT OF THE MOISTURE TRAP. THE FUEL CONTROL WAS REPLACED, ENGINE TRIMMED AND AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR 99ZZZX1774Skin · corrodedDURING A C-CHECK, CORROSION WAS NOTED ON TRAILING EDGE OF INBOARD LOWER SKIN LEFT ELEVATOR.SDR 99ZZZX1773Vent Door · corrodedDURING A C-CHECK, CORROSION WAS NOTED ON FORWARD AND AFT VENT DOORS IN C-2 DOOR.SDR 99ZZZX1772Beam · corrodedDURING A C-CHECK, CORROSION WAS NOTED ON LEFT HORIZONTAL STABLIZER UPPER TRAILING EDGE BEAM.SDR 99ZZZX1771Skin · corrodedDURING A C-CHECK, CORROSION WAS NOTED ON SKIN AT FS 460 AT STR 19R.SDR 99ZZZX1769Fitting · corrodedDURING A C-CHECK, CORROSION WAS NOTED ON RIGHT NR 5 LEADING EDGE FLAP NOSE FAIRING AND OUTER DRIVE FITTING.SDR 99ZZZX1768Bullnose · corrodedDURING A C-CHECK, CORROSION WAS NOTED ON RIGHT NR 5 LEADING EDGE FLAP NOSE FAIRING AND OUTER DRIVE FITTING.
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