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 = 'V35' 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 = 'V35' 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 2026FA0000631Impulse Coupling · destroyedTHE PILOT/OWNER ATTEMPTED TO START THE PLANE. AFTER THE FIRST FAILED START, THE PROPELLER STOPPED SPINNING DURING THE SECOND ATTEMPTED START. THE PILOT ABORTED THE START AND ALERTED ME TO A GRINDING SOUND. UPON INSPECTING THE ENGINE, THE LEFT MAGNETO HOUSING HSDR 2022FA0000215Brake · corrodedRIGHT BRAKE FAILED ON ROLL OUT FROM LANDING, DEPARTED RUNWAY. NO DAMAGE TO AIRCRAFT. AIRCRAFT TOWED TO MAINTENANCE FACILITY. BRAKE LINE FROM RIGHT MASTER CYLINDER PASSING UNDER HEATING DUCT HOSE CLAMP (FORWARD CABIN, UNDER FLOOR BOARD) DEVELOPED LEAK FROM CORRSDR 2019FA0000033Control Cable · brokenDURING ANNUAL INSPECTION, FOUND RIGHT AILERON CABLE BROKEN AT SWAGED END BETWEEN SAFETY WIRE HOLE AND THREADED END. SAFETY WIRE WAS HOLDING IT TOGETHER.SDR 2018FA0000470Control Cable · corrodedDURING CRUSE ALTITUDE 7500FT, THERE WAS A LOSS OF AILERON CONTROL. THE AIRCRAFT DRIFTED TO THE RIGHT AND WAS CORRECTED BY ROLLING LEFT. THE PILOT THEN FELT SOMETHING BREAK AND THE RIGHT WING DROPPED. THE PILOT TURNED THE AILERON CONTROL YOKE TO THE LEFT, UNTISDR 2016FA0000316Warning System · failedGEAR WARNING HORN FAILED TO SOUND DURING LANDING WITH GEAR UP.SDR MAMR2015121600654Housing · damagedTURBOCHARGER RECEIVED IN FOR INSPECTION, FOUND THE TURNINE HOUSING HAD DEVELOPED A GROWTH OR DEFORMITY IN THE CASTING. THIS DECREASED THE CLEARANCE BETWEEN THE TURBINE HOUSING AND THE TURBINE WHEEL CAUSING THE TURBO TO RUB/STICK. REPLACED THE TURBINE HOUSINGSDR 2015FA0000606Housing · deformedTURBOCHARGER RECEIVED IN FOR INSPECTION. FOUND THE TURBINE HOUSING HAD DEVELOPED A GROWTH OR DEFORMITY IN THE CASTING. THIS DECREASED THE CLEARANCE BETWEEN THE TURBINE HOUSING AND TURBINE WHEEL CAUSING A SLIGHT RUB OR CLUNKING SOUND. REPLACED THE TURBINE HOSDR 2015FA0000281Throttle Arm · disconnectedPRACTICING AN INSTRUMENT APPROACH INTO AIRPORT. PILOT FLYING WAS SLIGHTLY LOW ON A NON-PRECISION INSTRUMENT APPROACH. POWER SETTING WAS 15" MAP. APPLICATION OF FULL THROTTLE, DID NOT INCREASE MANIFOLD PRESSURE. AFTER SAFE LANDING ON RUNWAY WITH NO DAMAGE TSDR 2013FA0000321Worm Gear · mismanufacturedWORM GEAR RECEIVED FROM MFG. VISUAL INSPECTION REVEALED A "ROUGH" SURFACE FINISH ON GEAR FACE. CONFIRMED "OUT OF LIMITS".SDR 2012FA0000295Fitting · crackedDURING INSPECTION AND REMOVAL OF TAIL CONE, FOUND RT ELEVATOR CONTROL FITTING CRACKED 75 PERCENT AROUND FITTING.SDR 2011FA0000413Lifter · spalledLIFTERS SPALLED, CAUSING A METAL CONTAMINATION IN THE ENGINE.SDR 2011FA0000412Lifter · spalledLIFTERS SPALLED, CAUSING A METAL CONTAMINATION IN THE ENGINE.SDR 2010FA0000961Gasket · looseGASKET CAME OFF THE AIR FILTER. THE ADHESIVE HAD FAILED LETTING THE GASKET GET LOOSE AND IT CAN BE SUCKED INTO THE ENGINE, SHUTTING IT DOWN. CALLED MFG AND TALKED TO REP ABOUT THIS.SDR 2008FA0000436Cylinder · crackedCRACK VISIBLE AT NR 4 CYLINDER. CRACK APPEARS TO START AT CASTING ANOMALY, CONTINUES TO EDGE OF FINS, AND IS VISIBLE AT THE FIRST FOUR COOLING FINS. ALSO VERIFIED, THROUGH USE OF EDDY CURRENT, THAT THE CRACK CONTINUES TO THE SPARK PLUG HOLE. ALL OTHER CYLINDERSDR 0000H2484Line · chafedFUEL LINE MOUNTED ON FIREWALL FABRICATED PER STC SA8676SW WAS CHAFING THE ENGINE TAILPIPE.SDR 07N911KD01Spar · crackedDURING DETAILED INSPECTION OF TAILBOOM VERTICAL SPAR AREA FOUND 2 EA CRACKS APPROX .7500 INCHES IN LENGTH AT THE 1:00 O'CLOCK AND 7:00 O'CLOCK POSITIONS ON THE SECOND LIGHTING HOLE DOWN FROM TAIL ROTOR GEARBOX MOUNT. SUSPECT CRACKS HAVE BEEN WORKING FOR SOME TSDR 2007FA0000090Control Cable · brokenFOUND BROKEN STRANDS ON ELEVATOR CABLE BEHIND INSTRUMENT PANEL ABOUT 10 INCHES ABOVE THE (PN 535521242-13) BOBWEIGHT. (K)SDR 2006FA0001229Line · brokenSTARFLEX 193, LOW PRESSURE HOSE, LP MIL-H-50555 WAS USED TO CONNECT OIL COOLER TO FIREWALL FITTING. OIL PRESSURE WILL RUN BETWEEN 50-100 PSI IN LINE. HOSE BROKE AT FITTING AT OIL COOLER OUTLET, ALL OIL WAS PUMPED OUT OF ENGINE CAUSING ROD TO BE RAMMED THROUSDR 2006FA0001207Case · damagedENGINE LT CASE, MALT DEVELOPED HOLE APPROX 6 INCHES X 4 INCHES AS ROD-PISTON APPEARS TO BE MISSING FOR NR 4 CYLINDER. ENGINE OPERATED: (104 HOURS - 2004), (14 HOURS - 2005), (12 HOURS - 2006). PROPELLER RECENTLY SHIMMED BLADE NR 3, RED DYE AROUND PROP SEAL.SDR H8A2004F00000Motor · inoperativePILOT REPORTED, COULD NOT LOWER GEAR ELECTRICALLY, PILOT PERFORMED EMERGENCY EXTENSION SUCESSIVELY. UPON INSPECTION OF LANDING GEAR FOUND MOTOR INOPERATIVE. BRUSHES WERE COMPLETELY WORN OUT, REPLACED MOTOR.SDR 2003FA0000305Pump · shearedENGINE QUIT DURING TAKEOFF. THE AIRCRAFT WAS SUBSTANTIALLY DAMAGED. INVESTIGATION REVEALED A SHEARED DRIVE SHAFT FOR THE ENGINE DRIVEN FUEL PUMP (INJECTOR PUMP). DISASSEMBLY REVEALED FOD (A SMALL PIECE OF WIRE) JAMMED IN THE ROTOR/VANE. FURTHER INVESTIGATIOSDR 2002FA0001005Bearing · failedBEARING FAILURE IN ALTERNATOR CAUSED FAILURE OF CLUTCH ASSEMBLY.SDR 2002FA0000328Pump · failedFUEL PUMP WOULD NOT PRODUCE FUEL FLOW OR PRESSURE. ENGINE WOULD NOT IDLE BELOW 1000 RPM AND WOULD NOT PRODUCE POWER.SDR 20000531SH018Nut · failedPENETRANT TESTING INDICATION IN O-RING AREA. (X)SDR 20000531SH017Hub · crackedEDDY CURRENT AND PENETRANT TESTING INDICATION IN THREAD AREA. (X)SDR AU000328Filter · contaminated(AUS) AIRFRAME FUEL FILTER CONTAMINATED BY AN UNKNOWN WHITE SUBSTANCE.SDR 99ZZZX1933Control Cable · misinstalledFOUND LEFT ELEVATOR TRIM TAB CONTROL CABLE IMPROPERLY INSTALLED. SUBMITTER STATED CABLE ENDS ARE NOT IDENTIFIED AND CAN BE EASILY INSTALLED IN WRONG POSITION CAUSING CABLE CHAFING AND INCORRECT TAB MOVEMENT.SDR AU980488Crankcase · cracked(AUS) AT ENGINE BULK STRIP, FOLLOWING THE SEPARATION OF NR 2 CYLINDER HEAD (REFER MDR 98/0488), A 127 MM (5 INCH) LONG CRACK WAS FOUND IN THE CRANKCASE RUNNING FROM THE MATING FACE BACKBONE FLANGE DOWN TO THE NR 2 CYLINDER PAD. THE CRACK WAS OBSCURED BY THE LSDR AU980487Cylinder Head · separated(AUS) NR 2 CYLINDER HEAD SEPARATED FROM THE CYLINDER BARREL.SDR 97ZZZX1930Uplock Cable · frayedDURING INSTALLATION OF OXYGEN SYSTEM, OBSERVED INBD END OF LEFT LANDING GEAR UPLOCK CABLE SEVERELY FRAYED AT THE TERMINAL END WHERE IT EXITS THE HOUSING: SUBMITTER SUSPECTS OLD AGE AND LACK OF LUBRICATION. SUBMITTER RECOMMENDS FREQUENT INSPECTION OF BOTH MLGSDR 96ZZZX5952Rib · crackedDURING RE-SKIN OF HAIL DAMAGED FLAP, FOUND NOSE RIB AT ACTUATOR ATTACH POINT CRACKED. CRACK IS IN WEB OF RIB AT THE RELIEF OF THE CAP FORMATION, LOWER FORWARD. SUBMITTER STATED THIS IS NOT AN UNCOMMON FIND. THIS CAN ONLY BE DETECTED IF THE SKIN IS REMOVED.SDR EY2R9600115Hub · crackedHUB CRACKED IN THREAD AREASDR 96ZZZX3767Fuel Selector · o-ring defectiveFUEL SELECTOR O-RING FOR THE RIGHT TANK FEED WAS RAISED BETWEEN THE SELECTOR BODY AND PLATE ALLOWING CONTINUOUS FEED OF FUEL FROM THE RIGHT TANK. THE FUEL SELECTOR WAS NOT DETERMINED TO BE A FACTOR IN THIS ACCIDENT.SDR EY2R9600089Hub · crackedHUB CRACKED IN THREAD AREASDR EY2R9600839Hub · corrodedHUB FOUND CORRODED.SDR EY2R9600045Hub · crackedINSP FOUND HUB CRACKEDSDR 96ZZZX2380Blade · crackedBLADE DYE CHECKED IAW AD 68-13-02. NO CRACKS INDICATED. CHECKED OK. FOUND ONE INCH LONG CRACK IN BLADE, USING EDDY CURRENT, APPROXIMATELY .040 INCH DEEP. SUBMITTER SUGGESTED MAKING EDDY CURRENT INSPECTION MANDATORY.SDR EY2R9600031Hub · crackedHUB CRACKED IN THREAD AREASDR AU960481Spar Cap · corroded(AUS) RH WING LOWER SPAR CAP CORRODEDSDR EY2R9601367Hub · mis drilledPROP ASSY HUB DRILLED PAST .152SDR EY2R9600209Hub · corrodedPROP HUB ASSY IS CORRODEDSDR 95ZZZX6158Hub · corrodedPROPELLER WAS LAST OVERHAULED 7-21-91. WAS SENT IN FOR OVERHAUL. AFTER TEAR DOWN AND CLEANING, FOUND TO HAVE EXCESSIVE CORROSION ON THE HUB PILOT TUBES AND AROUND THE HUB SPIDER ARMS INBOARD OF THE BEARINGS SEAT. CORROSION ON THE SPIDER ARMS COULD RESULT INSDR 95ZZZX6017Air Filter · defectiveAD95-03-02 SHOULD INCLUDE THIS BRACKETT, BA7210, AS WE FOUND THE GASKET MOVED FROM PROPER POSITION.SDR 95ZZZX2435Piston · failedPISTON SKIRT FAILED AT LOWER RING LAND ON THRUST SIDE. DEBRIS EXTENSIVELY DAMAGED CRANKCASE, CRANKSHAFT, CAMSHAFT, RODS, ADJACENT PISTONS AND CYLINDERS. ALSO, THE ENTIRE OIL SYSTEM WAS CONTAMINATED.
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