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 = '95C55' 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 = '95C55' 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 2024FA0000298Rod · bentINSPECTED GEAR COLLAPSE ON BARON N7885C JACKED AIRCRAFT. POWER ON. GEAR GREEN LIGHT ILLUMINATED. GEAR DOORS DAMAGED. INSPECTED AIRCRAFT. NO VISIBLE DAMAGE TO WING SPARS. WINGS ARE STRAIGHT, NO BROKEN OR CRACKED RIBS. NO STRUCTURAL DAMAGE ON FIREWALL OSDR 2023FA0000122Control Cable · frayedUPON INSPECTION AT ANNUAL THE FORWARD ELEVATOR CONTROL CABLE WAS FOUND FRAYED, SIX STRANDS FOUND BROKEN. REF: AUSTRALIA AD/BEECH 36/54 DATED 4/2012.SDR 2020FA0000317Fuel Line · corrodedATTEMPTED TO START AIRCRAFT TO TAXI TO HANGAR. LT ENGINE STARTED NORMALLY. RT ENGINE WAS VERY DIFFICULT TO START AND WOULD QUIT AS SOON AS BOOST PUMP WAS TURNED OFF. OWNER VERIFIED THAT HE HAD BEEN HAVING SERIOUS DIFFICULTY STARTING AND MAINTAINING ENGINE OPSDR 2017FA0000048Gearbox · seizedAIRCRAFT CALLED ON RADIO WITH GEAR PROBLEMS. TOLD TO CRANK GEAR WITH EMERGENCY HANDLE. UNABLE TO DO SO AND LANDED GEAR UP. AFTER LIFING AIRCRAFT AND DISCONNECTING LINKAGES TO SAFETY GEAR DOWN FOR MOBILITY, FOUND GEAR BOX JAMMED IN THE UP POSITION. DISASSEMBLSDR XGN2015F00000Switch · inoperativeSWITCH FAILED.SDR 2012FA0000426Throttle Cable · brokenPILOT REPORTED RT THROTTLE CABLE BROKE ON LANDING ROLL OUT, SHUTDOWN LT TO BETTER CONTROL ACFT THEN SHUTDOWN RT AS ACFT WAS UNDER CONTROL AND ROLLED TO STOP. INSP FOUND RT CABLE BROKEN AT THROTTLE HANDLE END WHERE IT ENTERS INTO THE CABLE HSG. HOUSING APPEARSDR 2010FA0001173Drive Gear · failed(V7AR) DURING CRUISE FLIGHT THE RT ENGINE WENT TO 2700 RPM THEN DROPPED TO 1100 RPM. THE PILOT DID NOT NOTICE ANY OTHER GAGE READINGS. THE ENGINE STOPPED AND THE PILOT WAS UNABLE TO RESTART. THE ACFT LANDED OK. THE ENGINE HAS NOT BEEN INSPECTED. ON TEARDOSDR 2009FA0000587Line · corrodedON TAXI OUT, PILOT SMELLED FUEL IN THE COCKPIT AND NON RATED FRONT SEAT PASSENGER SAW STREAM OF FUEL ON RT SIDE RUDDER PEDALS. PILOT RETURNED TO THE HANGAR TO HAVE PROBLEM INVESTIGATED.
UPON FURTHER INVESTIGATION FOUND RT SIDE RIGID ALUMINUM FUEL LINE THAT DSDR CA090428005Hub · unserviceable(CAN) PROP RECEIVED FOR REPAIR OF RED OIL LEAK. UPON VISUAL INSP CORROSION DAMAGE UNDER THE PAINT WAS OBSERVED. THE AMOUNT OF DAMAGE RENDERS THE HUB UNSERVICEABLE IAW MM NR SPM100-1R4.SDR XGN2007F00014Cylinder · crackedCYLINDER HEAD CRACKED IN THE EXHAUST AREA. (K)SDR XGN2007F00013Cylinder · crackedCYLINDER HEAD CRACKED IN THE EXHAUST AREA. (K)SDR XGN2007F00008Cylinder Head · crackedCYLINDER HEAD CRACKED IN THE EXHAUST AREA. (K)SDR XGN2007F00006Cylinder Head · crackedCYLINDER HEAD CRACKED IN THE EXHAUST AREA. (K)SDR XGN2006F00055Cylinder · crackedCYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K)SDR XGN2006F00054Cylinder · crackedCYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K)SDR XGN2006F00053Cylinder · crackedCYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K)SDR XGN2006F00052Cylinder · crackedCYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K)SDR XGN2006F00051Cylinder · crackedCYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K)SDR XGN2006F00043Cylinder · crackedCYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K)SDR XGN2006F00042Cylinder · crackedCYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K)SDR XGN2006F00041Cylinder · crackedCYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K)SDR XGN2006F00040Cylinder · crackedCYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K)SDR XGN2006F00039Cylinder · crackedCYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K)SDR XGN2006F00038Cylinder · crackedCYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K)SDR XGN2006F00037Cylinder · crackedCYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K)SDR AUS20040173Wire · wrong part(AUS) RT ELEVATOR TRIM TAB HINGE WIRE MANUFACTURED FROM MILD STEEL. RT TRIM TAB FREEPLAY 7.366MM (0.290IN) AND LT TRIM TAB FREEPLAY 9.829MM (0.387IN). MAXIMUM FREEPLAY 2.133MM (0.084IN). PERSONNEL/MAINTENANCE ERROR. UNAPPROVED PART.SDR CM2RSeparator · obstructedOLD ENGINE SEPARATOR WAS CRACKED. ORDERED NEW PART. INSPECTED NEW PART AND COULD NOT BLOW THROUGH IT. THE AIR OUTLET TUBE WAS BLOCKED INTERNALLY. NEW OUT OF BOX FAILURE. IF THIS UNIT WAS INSTALLED ON THE ENGINE IT WOULD HAVE PRESSURIZED THE CASE AND LEAD SDR XGN2003F00003Hinge · brokenLT WING LEADING EDGE ASSY SAGGING AND FLEXING BETWEEN W/S 49.131 AND 91.131. WE WERE UNABLE TO DISASSEMBLE LEADING EDGE ASSEMBLY FROM THE FORWARD SPAR CAP DUE TO BROKEN (105774C-ZG18700) HINGE PIN. NOT ABLE TO DISASSEMBLE THE LEADING, COULD ONLY GUESS THAT TSDR XGN2003F00002Crankcase · crackedCRACK WAS DISCOVERED WHILE LOOKING FOR OIL LEAK DURING 100 HOUR INSPECTION. THIS HAS BEEN GOING ON FOR YEARS WITH MFG ENGINES. THEIR ATTEMPTS OF HEAVIER CRANKCASES AND 7TH STUD APPLICATIONS HAVE DOEN NOTHING TO GET RID OF THE PROBLEM.SDR 2003FA0000370Cylinder · wornCYLINDERS NR 2 AND 6 HAD LOW COMPRESSION WITH LEAKAGE PAST THE EXHAUST VALVES. REMOVEAL AND TEARDOWN OF THE CYLINDERS REVEALED THE FOLLOWING: CONDITION OF CYLINDER HEAD WAS NORMAL FOR TIME. EXHAUST VALVES EXHIBITED EXTREME WEAR FOR TIME IN SERVICE. CYLINDESDR 2002FA0001140Spar · crackedREMOVED LT ELEVATOR AND FOUND REAR SPAR CRACKED AT TRIM TAB ACTUATOR. TECH SUPPORT AND CONSENSUS IS TO REPLACE REAR SPAR.SDR AUS20021136Pivot · seized(AUS) RT MAIN LANDING GEAR OUTER DOOR PIVOTS SEIZED.SDR AUS20021135Link · seized(AUS) SQUAT SWITCH LINKS SEIZED.SDR AUS20021134Rib · corroded(AUS) LT AND RT WING OUTER RIBS LOCATED AT STA 191 CORRODED BEYOND LIMITS.SDR AUS20021133Rib · corroded(AUS) LH AND RH WING TRAILING EDGE RIBS CORRODED. RIBS AFFECTED ARE:- LH WING-PNO 95110014-121PNO 95110014-191PNO 95110014-153PNO 95110014-129PNO 95110014-135RH WING-PNO 95110014-122PNO 95110014-192PNO 95110014-154PNO 95110014-130PNO 95110014-120SDR AUS20021132Keel · corroded(AUS) LH AND RH KEEL SPLICE JOINTS LOCATED IN NOSE LANDING GEAR WHEEL WELL AT STN 49.000 CONTAINED SEVERE EXFOLIATION CORROSION BETWEEN THE JOINT FACES. ATTACHMENT RIVET HEADS MISSING. AFFECTED PARTS WERE:-1. LH FORWARD KEEL PNO 96-410032-6012. LH AFT KEEL PNOSDR AUS20021131Stringer · corroded(AUS) FUSELAGE STRINGER LOCATED AT STN 107.00 CONTAINED SEVEREEXFOLIATION CORROSION. EVIDENCE OF WATER ENTRY OVER AN EXTENDED PERIOD.SDR AUS20021130Cable · corroded(AUS) LH AND RH MAIN LANDING GEAR UPLOCK CABLES RUSTY. UPLOCK SPRINGS BROKEN AND RUSTY. CLOSING PANELS IN WHEEL WELL BAYS MISSING ALLOWING DIRT AND MUD ETC TO BUILD UP.SDR AUS20021129Bearing · seized(AUS) RUDDER BEARINGS UNSERVICEABLE. TOP BEARING SEIZED WITH A GROOVE WORN IN THE ATTACHMENT PIVOT BOLT. CENTRE BEARING WORN. LOWER BEARING PARTIALLY SEIZED.SDR AUS20021128Bracket · misrepaired(AUS) LT AILERON INCORRECTLY SECURED TO THE HINGE BRACKET ASSEMBLY. ATTACHMENT HOLE DRILLED OVERSIZE AND A RIVNUT FITTED. UNAPPROVED PART / REPAIR. PERSONNEL / MAINTENANCE ERROR.SDR AUS20021127Doubler · corroded(AUS) LH AND RH FUSELAGE DOUBLERS LOCATED AT STN 0.00 CONTAINED EXFOLIATION CORROSION. ADJACENT RIB PNO 95-410005-4 CORRODEDAWAY. AIRCRAFT HAS OPERATED IN A SALT AIR ENVIRONMENT FOR A CONSIDERABLE TIME.SDR AUS20021126Fitting · corroded(AUS) WING ATTACHMENT TOP BATHTUB FITTINGS CORRODED AND DRAIN HOLES BLOCKED. NO CORROSION PROTECTION ON FITTINGS.SDR AUS20021125Rod End · corroded(AUS) LH AILERON TRIM TAB RODEND FORK RUSTY AND CLEVIS PIN SEIZED.SDR AUS20021124Cylinder · corroded(AUS) RT ENGINE CYLINDERS CORRODED ON CYLINDER WALLS. CORROSION PITS WERE IN EXCESS OF 0.381MM (0.015IN) DEEP. THREE CYLINDERS WERE ALSO FOUND TO BE CRACKED FROM EXHAUST SEATS TO THE EXHAUST PORTS. AIRCRAFT OPERATES FOR APPROXIMATELY 100 HOURS PER YEAR.SDR AUS20021123Rib · corroded(AUS) LH WING RIB PNO 9511023-3 AND RH WING RIB PNO 9511023-4 CORRODEDTHROUGH. LH WING RIB CHANNEL PNO 9511023-5 AND RH WING RIBCHANNEL PNO 9511023-6 CORRODED THROUGH. RIBS AND CHANNELS ARE LOCATED AT STN 66.SDR AUS20021122Rod · faulty(AUS) LH MAIN LANDING GEAR RETRACTION ROD FAULTY. ROD HAD BEENILLEGALLY REPAIRED IN AN ATTEMPT TO STRAIGHTEN THE ROD. RIVETSHAD BEEN REPLACED WITH BOLTS AND PENNY WASHERS. UNAPPROVEDREPAIR. PERSONNEL/MAINTENANCE ERROR.SDR AUS20011347Cylinder · separated(AUS) RT ENGINE NR 4 CYLINDER AND PISTON SEPARATED IN FLIGHT. RT ENGINE COWL SEPARATED ALONG HINGE.SDR AUS20010990Exhaust Pipe · faulty(AUS) LH ENGINE EXHAUST PIPE HELD ON BY REAR CLAMP ONLY AND TOUCHINGFIREWALL. HEAT AFFECTED PLASTIC JOINER TUBE FOR PITOT SYSTEMLOCATED BEHIND FIREWALL.SDR 2001FA0000226Spar · crackedCRACK DEVELOPED ON TOP OF LEFT WING. INVESTIGATION REVEALED LOWER FORWARD WING SPAR HINGES AND PINS WORN OUT RESULTING IN EXCESS OF MOVEMENT IN THE LEADING EDGE OF WINGS. NEW WING SPARSSDR SIMA200119704Frame · damagedABI - DURING MBV INSPECTION MAINTENANCE, FOUND FRAME 658.5 TO HAVE WEB DAMAGE ON THE RIGHT SIDE ABOVE WL 73.5 DAMAGE WAS REPAIRED IAW SAAB 340 SRM AND AIRCRAFT WAS RETURNED TO SERVICE. (M)
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