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 = '580' 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 = '580' 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 VGCA20231009001Clamp · brokenRH ENGINE ZONE 1 FIRE INDICATION AND LH ENGINE ZONE 2 FIRE INDICATION. FOUND RH TAILPIPE DISCONNECTED CAUSING RH ZONE 1 FIRE INDICATION. LH ZONE 2 FIRE INDICATION WAS FALSE WARNING CAUSE BY BAD DIODE.SDR VGCA20220218001Spring · brokenNOSE LANDING GEAR NOT INDICATING DOWN AND LOCKEDSDR CVGA20211227001Fuel Control · failedRIGHT ENGINE SHUTDOWN IN FLIGHT DURING DESCENT IN THE MID FL300. NO N1 ROTATION FOR ATTEMPTED RESTART.SDR VGCA20211119001None · noneDURING TAKE OFF, THE RH ENGINE RPM DROPPED TO 13,400. ENGINE RPM RECOVED WHEN PROP SYNC IS SELECTED OFFSDR VGCA201809143001Fire Warning · activatedNR 2 ENGINE ZONE 1 FIRE WARNING IN FLIGHT.SDR VGCA201806210001Spar · corrodedCORROSION FOUND ON THE REAR SPAR RAIL LEFT WING, BETWEEN LWS 14 AND 15.SDR VGCA20170919001Engine · overtempLEFT ENGINE INDICATED HIGH TEMPERATURES WHICH COULD NOT BE IMMEDIATELY CONTROLLED BY POWER LEVER, EVENTUALLY TIT INDICATION WERE RETURNED TO NORMAL PARAMETERS. CAUSE STILL UNDER INVESTIGATION.SDR VGCA20160920001Relay · shortedBELLY DOOR LIGHT ON IN FLIGHT, WITH ELECTRICAL ODOR.SDR VGCA20160725002Plug · corrodedCORROSION ON WINDOW PLUG FRAME BS 375 - 465. REPAIRED THE WINDOW PLUG IAW DWG R508-053-004-001.SDR VGCA20160725001Skin · corrodedSKIN CORRODED AT BS 193-210 STRINGER 7L. REPAIRED THE AREA IAW DWG R508-053-003-001.SDR VGCA20151015001Channel · crackedRIGHT LOWER C CHANNEL NLG ATTACH STATION 76 CRACKED.SDR VGCA20150608003Stringer · crackedDISCOVERED CRACKED STRINGER 22L AT STATION 210.SDR VGCA20150608002Beltframe · dentedDISCOVERED DAMAGED, DENTED, BELT FRAME AT STATION 395R FLOOR LEVEL..SDR VGCA20150608001Beltframe · crackedDISCOVERED CRACKED BELT FRAME AT STATION 261L, FLOOR LEVEL.SDR VGCA20150428013Doubler · corrodedFOUND CORROSION ON AFT CARGO DOOR ACTUATOR DOUBLER.SDR VGCA20150428012Angle · crackedREPLACED CRACKED CARGO DOOR ACTUATOR MOUNT ANGLES.SDR VGCA20150428011Hinge · corrodedFOUND CORROSION ON CARGO DOOR HINGE. REPLACED DOOR HINGE.SDR VGCA20150428010Stringer · crackedSTRINGER 30 CRACKED AT STATION 661.SDR VGCA20150428009Structure · corrodedFOUND STRINGER TO SKIN CORROSION AT RT FS 210 - 227.SDR VGCA20150428008Stringer · crackedRIGHT WING STRINGER IN DRY BAY BETWEEN RIB 0 - 1 CRACKED.SDR VGCA20150428004Stringer · crackedRIGHT WING STRINGER IN DRY BAY BETWEEN RIB 0 - 1 CRACKED.SDR VGCA20150428007Structure · crackedFOUND CRACKS IN NOSE WW AT STATION 26 RT.SDR VGCA20150428006Structure · corrodedCORROSION FOUND AROUND RT PRESS VESSEL ELEC PASS THROUGH.SDR VGCA20150428005Longeron · crackedLEFT SLIDING WINDOW LONGERON CRACKED.SDR VGCA201504280004Skin · corrodedREMOVED PREVIOUS REPAIR BETWEEN STRINGERS 15 - 16 DUE TO CORROSION. CLEANED CORROSION, PRIMED, RESEALED & REINSTALLED.SDR VGCA20150428003Structure · corrodedREMOVED PREVIOUS REPAIR BETWEEN STRINGERS 18 - 19 DUE TO CORROSION. CLEANED CORROSION, PRIMED, RESEALED & REINSTALLED.SDR VGCA20150428002Rib · crackedLEFT WING DRY BAY RIB 2 CRACKED.SDR VGCA20150428001Longeron · crackedLEFT SLIDING WINDOW LOWER LONGERON FRAME STATION 64 IS CRACKED.SDR VGCA20150315002Splice · corrodedCORROSION FOUND ON THE FWD KEEL BEAM SPLICE.SDR VGCA20150315001Extension · crackedNOSE LANDING GEAR WW BEAM EXTENSION CRACKED.SDR VGCA20150303002Fire Warning · activatedAT THE TOP OF CLIMB, A ZONE 3 FIRE INDICATION APPEARED. FOLLOWED PRECAUTIONARY ENG SHUTDOWN & FIRE BOTTLES WERE DISCHARGED. WHILE PERFORMING MX, TECHNICIAN VISUALLY VERIFIED RT FWD FIRE BOTTLE FAILED TO DISCHARGE.SDR VGCA20150127001Anti-Skid Valve · bypassingLOSS OF HYD QTY IN FLIGHT. UTILIZED APPROPRIATE CHECKLIST. UPON LANDING EMER BRAKE FAILED. WHILE TROUBLESHOOTING DETERMINED PROBLEM WAS WITH THE ANTI-SKID SYS.SDR CA141023006Pin · sheared(CAN) DURING A 375 HR ANNUAL INSPECTION, IT WAS FOUND THAT THE RIGHT MECHANICAL FUEL SHUTOFF VALVE AT THE FIREWALL HAD A SHEARED ACTUATOR PIN. THIS CAUSED THE FUEL PORTION OF AN EMERGENCY SHUTDOWN TO REMAIN IN AN OPEN CONFIGURATION. THE COMPONENT HAS BEEN RSDR VGCA20131108001Skin · crackedLEFT WING LOWER SKIN REPAIR AT DRAIN FITTING BETWEEN WS 4 & 5.SDR CA130807006Coupling · cracked(CAN) DURING OVERHAUL OF RUDDER TORQUE TUBE ASSY, THE LOWER COUPLING WAS FOUND CRACKED.SDR VGCA20130523001Longeron · crackedNACELLE, RT LOWER INBD LONGERON CRACKED.SDR VGCA20130403001Spar · corrodedLEFT HORIZONTAL STABILIZER LWR REAR SPAR CORRODED.SDR CA130705008Static Inverter · failed(CAN) DURING PRE-DEPARTURE GROUND CHECKS THE FLIGHT CREW WAS UNABLE TO APPLY INVERTER POWER. TROUBLESHOOTING DETERMINED THAT THE INVERTER SYSTEM, 2 INVERTERS IN PARALLEL, WAS INOPERATIVE. BOTH INVERTERS WERE REPLACED AND WHEN POWER WAS APPLIED IT WAS FOUND TSDR VGCA201205010001Spar · corrodedCORROSION LT AND RT WING, OUTER, UPPER REAR SPAR WS23-WS29.SDR VGCA20120313Exhaust Duct · crackedNR 1 ENGINE ZONE 1 FIRE WARNING. FOUND EXHAUST DUCT CRACKED.SDR VGCA20110517Longeron · corrodedRIGHT NACELLE STA 8 AND 6 LONGERON HAD SEVERE CORROSION.SDR VGCA20100805Longeron · corrodedLEFT INBD UPPER NACELLE LONGERON HAD EXCESSIVE CORROSION.SDR 2010FA0000778Unknown · odorFLIGHT CREW NOTICED ELECTRICAL SMELL, RETURNED TO BASE. MX INSPECTED CTR CONSOLE AREA. COULD NOT DUPLICATE MALFUNCTION. PERFORMED OPS CHECK OF AFCS, FMS, WX RADAR, RTU, EFIS AND NAV SYSTEMS. NO DEFECTS NOTED. NO SMOKE OR BURNING SMELL NOTED. OPS CK GOOD IAW CSDR VGCA20090928Fuel Control · malfunctionedFLAMEOUT OF NR 2 ENGINE DUE TO MECHANICAL MALFUNCTION OF FUEL SHUTOFF IN FUEL CONTROL.SDR I5HA0858015Skin · damagedDURING CLIMB OUT, EN-ROUTE, THE CREW FELT A "THUMP" POSSIBLY FROM THE LT WING. THE CREW COULD NOT SEE ANY DAMAGE AND DID NOT EXPERIENCE ANY CONTROL PROBLEMS. THE CREW CONTINUED THEIR FLIGHT AND LANDED UNEVENTFULLY. EXAMINATION BY THE CREW OF THE LT WING REVSDR 15HA0858014O-Ring · leakingDURING THE TAKEOFF ROLL DEPARTING, ENROUTE, THE NR ONE ENG AUTO-FEATHERED. THE CREW ABORTED THE TAKEOFF AND RETURNED TO BASE. MX PERSONNEL OBSERVED A LARGE AMOUNT OF OIL AROUND THE FRONT OF THE PROPELLER. FURTHER INSP REVEALED A FAILED O’RING BENEATH THE FESDR CA081203012Valve · failed(CAN) IN FLIGHT, CREW EXPERIENCED A FAILURE OF THE NR 2 ENG PITCH LOCK VALVE. ENGINE WAS E-HANDLED AND AC LANDED WITHOUT INCIDENT. MAINT REPLACED THE NR 2 PITCH LOCK VALVE AND ACFT RETURNED TO SERVICE.SDR I5HA08580004Hub · leakingON APPROACH, THE CREW FELT A VIBRATION ON THE NR1 ENGINE AND SHUT IT DOWN AS A PRECAUTIONARY MEASURE. MAINT INSPECTED THE AC AND FOUND THE NR 1 PROP LEAKING BETWEEN THE HUB AND REGULATOR. THE PROP WAS REMOVED AND REPLACED WITH A SERVICEABLE PROP, RIG CHECKS COSDR I5HA041108001Volt Regulator · out of adjustAFTER CLIMB OUT, THE CREW LOST THE NR1 DC GENERATOR. AS A PRECAUTIONARY MEASURE THEY RETURNED TO DEPARTURE FOR MAINT TO CORRECT THE PROBLEM. MAINT RERACKED THE NR1 DC GEN CONTROL PANEL AND PARALLEL THE DC GENERATORS IAW THE MM. THE AC WAS RETURNED TO SERVICE ASDR I5HA0858005EChannel · damagedDURING A STORM (MIA) A CARGO CAN (ULB) WAS THROWN INTO THE RT SIDE OF N581P. THE RT PROPELLER WAS ALSO STRUCK A GLANCING BLOW. THERE WAS SIGNIFICANT DAMAGE TO THE SKIN AND SUPPORT STRUCTURE BENEATH THE SKIN. THERE WAS DAMAGE TO WIRING IN THE AREA. THE NOSE
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