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 = 'U206E' 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 = 'U206E' 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 HXXC2016F00015Tube · failedUPON LANDING, LEFT MAIN TUBE WENT FLAT.SDR CA150716007Fastener · detached(CAN) FOUND LT WING FUEL BLADDER INBD MIDDLE AND INBD REAR CLIPS HAD FALLEN OFF, CAUSING THE FUEL BLADDER TO DROOP AND PUT PRESSURE ON THE FUEL LEVEL TRANSMITTER FLOAT AND CAUSE A LOWER FUEL LEVEL INDICATION. CLIPS WERE REINSTALLED AND A FUEL LEVEL INDICATIONSDR CA150706013Engine · power loss(CAN) IN CRUISE FLIGHT THE ENGINE BEGAN RUNNING VERY ROUGHLY. PILOT RETURNED TO BASE FOR MAINTENANCE. SPARK PLUGS REMOVED, INSPECTED, AND TESTED, NO FAULTS FOUND. SPARK PLUGS CLEANED AND REINSTALLED. MAG TIMING CHECKED AND FOUND TO BE OUT +4 DEG, MAGNETO TIMINSDR CA150704002Alternator · failed(CAN) ON RUN UP PILOT DISCOVERED THE ALTERNATOR WAS NOT CHARGING. REMOVED ALTERNATOR PN DOFF10300JR, 123.9 TSOH. INSTALLED SERVICEABLE ALTERNATOR PN DOFF10300JR. RUN UP CARRIED OUT ALTERNATOR FUNCTION CHECKED OK.SDR CA150424002Bushing · failed(CAN) UPON REMOVING THE NR 5 CYLINDER DUE TO LOW COMPRESSION, THE CONNECTING ROD WRIST PIN BUSHING WAS FOUND CRACKED ALONG THE CURVED AREA OF THE "KEYED" SEAM. AFTER CONSULTATION WITH THE ENGINE O/H FACILITY, THEY RECOMMENDED THAT THE REMAINING 5 CYLINDERS BE SDR CA150407004Shaft · broken(CAN) FUEL SELECTOR SHAFT TOP U-JOINT WAS TWISTED AND 1 TAB BROKEN AS PILOT WAS SELECTING DIFFERENT TANK GOING THROUGH THE OFF POSITION, DUE TO STIFF FUEL SELECTOR VALVE CAUSED BY ICE BUILDUP ON VALVE,SDR R01A2014F00146Magneto · failedRIGHT MAGNETO OF A NEWLY INSTALLED FACTORY REBUILT ENGINE, FAILED ON PRE-TAKEOFF MAG CHECK, FLIGHT ABORTED. 5.8 TT ON NEW ENGINE. MAGNETO WAS FACTORY REMANUFACTURED AND CAME PREINSTALLED ON THE NEW ENGINE.SDR MKT2013F00000Tube · splitTHIS IS 1 OF ABOUT 10 INNER TUBES WE HAVE HAD SPLIT IN A SEAM AND CAUSED A FLAT TIRE, THERE HAVE BEEN NO SIGN OF A HOLE IN THESE TIRES AND NO HARD LANDING, NOT OVER INFLATED, JUST A SPLIT SEAM IN THE TUBE.SDR CA111103015Trunnion · cracked(CAN) SMALL CRACK ON THE UPPER TRUNNION ASSY ON THE NOSE GEAR AT THE ARM ON LT SIDE.SDR CA100826003Selector · failedTHIS FUEL SELECTOR HAS 3 POSITIONS THAT HAVE DETENTS, LT, RT, AND OFF. IT WAS DETERMINED THAT DURING FUEL MX ON THIS FUEL SELECTOR THAT IF THE SELECTOR IS MOVED JUST OFF OF THE DETENT IN THE LT OR RT POSITION, IT WILL ALSO FEED THE ENGINE FROM THE OPPOSITE TASDR CA100730006Contact · brokenMAG RECEIVED FOR WARRANTY CONSIDERATION WITH A SMALL BAG CONTAINING 1 OF THE CONTACT SECTIONS OF THE POINTS. THE MAG WAS UNSERVICEABLE AND HAD BEEN REMOVED BY THE CUSTOMER. THE CONTACT HAD BROKEN AWAY AT THE AREA WHERE IT IS WELDED OR BRAZED TO THE RIVET THAT SDR CA090707009Cable · frayed(CAN) FRAYED AT STA 138, PULLEY NOT SEIZED.SDR CA090707008Hinge · cracked(CAN) CRACKS LOCATED AT DOUBLER ANGLE BENDS, TOP AND BOTTOM, ONLY LWR CRACKS ARE VISIBLE. CRACKS AT TOP ONLY VISIBLE WITH BORESCOPE OR REMOVING THE SKIN.SDR CA090707007Hinge · cracked(CAN) HINGE DOUBLERS CRACKED AT LWR ANGLE BEND, UPON REMOVAL OF HINGE, FOUND MORE CRACKS NEAR TOP OF HINGE, NOT VISIBLE UNLESS THE SKIN IS PEELED BACK OR THE USE OF A BORESCOPE.SDR CA090620002Case · failed(CAN) CASE HALVES FOUND LOOSE.SDR CA090601005Cylinder Head · cracked(CAN) FOUND 4 CYLINDERS CRACKED HEAD AT INJECTOR NOZZLE AREA.SDR CA090302001Alternator · failed(CAN) CHARGING SYS QUIT - BATTERY WENT DEAD - FOUND ALTERNATOR HSG LOOSE AND ALTERNATOR WOULD NOT SPIN WHEN FIELD POWER APPLIED.SDR CA090204014Exhaust Valve · stuck100 HOUR INSPECTION CARRIED OUT AND ENGINE LEAKDOWN CARRIED OUT NORMAL. AFTER ENGINE WAS COOL THE PROPELLER WAS ROTATED TO CHECK MAGNETO TO ENGINE TIMING. A BANG WAS HEARD IN THE FRONT AREA OF THE ENGINE. NR 5 AND NR 6 CYLINDER EXHAUST VALVES WERE STICKING OSDR CA090109011Valve · sheared(CAN) VALVE STEM SHEARED OFF AND TIRE WENT FLAT - REPLACED WHEEL ASSY.SDR CA080325006Bulkhead · cracked(CAN) BULKHEAD CRACK 1.25 IN LONG AT RT SIDE FROM LIGHTNING HOLE. NEAR STAB ATTACH POINT. (TC NR 20080325006)SDR CA070905012Cylinder Head · cracked(CAN) CRACKED FROM SPARK PLUG HOLE TO EXHAUST VALVE (TC NR 20070905012)SDR CA050704004Housing · loose(CAN) PILOT REPORTED HEARING A NOISE AND THEN NOTICED HIS ALTERNATOR WAS OFF LINE. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THAT THE HOUSING HALVES ON THE ALTERNATOR WERE QUITE LOOSE. REPLACE ALTERNATOR STILL NO CHARGE. FURTHER REPLACED SDR CA050609012Reservoir · cracked(CAN) PILOT REPORTED DURING WALKAROUND, FUEL DRAIN ON LT BELLY WOULD NOT STOP DRIPPING. CLOSER INSPECTION REVEALED THAT FAULT WAS IN DRAIN VALVE BUT THE RESEVOIR ITSELF AND FOUND THAT WELD WAS CRACKED ADJACENT TO MOUNTING TAB TO AIRCRAFT STRUCTURE. RESEVOIR SDR 2005FA0000439Adc · malfunctionedALTITUDE WAS 100 FEET OFF. UNIT INSTALLED AS PRAT OF THE FLIGHT SYSTEM, INC EFIS-SV IAW STC NR SA02203AK. (AL05200500175) (K)SDR CA041014007Reservoir · damaged(CAN) UPON 1000 HR FUEL SYSTEM INSPECTION AS REQUIRED BY CESSNA, THE FUEL WAS COMPLETELY DRAINED FROM THE AIRCRAFT.UPON REMOVING THE LOWER R/H RESEVOIR QUICK DRAIN,IT WAS REVEALED IT WAS QUITE LOOSE BUT NOT LEAKING. UPON REINSTALLATION OF QUI CK DRAIN VALVE ISDR CA041014006Reservoir · cracked(CAN) COULD SMELL STRONG FUEL ODOR IN COCKPIT AND ALSO NOTED FUEL STAIN ON BELLY OF AIRCRAFT DURING INSPECTION. SUSPECTED RESEVOIR QUICK DRAIN LEAKY BUT FURTHER INVESTIGATION REVEALED A 1 INCH CRACK ON FORWARD LOWER WELD SEAM ON RESEVOIR. RESEVOIR REMOVED, RSDR CA030225005Crankshaft · disconnected(CAN) NR 6 CONNECTING ROD CRANKSHAFT END BECAME DISCONNECTED AND SMASHED THROUGH ENGINE CASE. BOLTS EITHER WRE NOT TORQUED CORRECTLY OR CLAMPSHELL BOLT FAILURE.SDR CA020830020Spar · cracked(CAN) - INSPECTION REVEALED CRACK AT BOTTOM ANGLE OF AILERON HINGE. FURTHER INSPECTION REVEALED CRACKED REAR SPAR AT HINGE ATTACH POINT AND CRACKED RIB STA 109. INSPECTION OF RIB AND REAR SPAR IS DIFFICULT BECAUSE OF LACK OF INSPECTION PANELS. THE INSPECTIONSDR CA020510024Exhaust Valve · burned(CAN) WHILE INSPECTING THE CYLINDER ASSEMBLIES IN ORDER TO PUT THE ENGINE "ON CONDITION", WE DISCOVERED THE EXHAUST VALVE ON CYLINDER NR 4 AND 5 SEVERELY BURNED. THE STEM AND NECK OF EXHAUST VALVE NR 4 APPEARS TO BE APPROXIMATELY 40 PERCENT DETERIORATED AND ESDR AUS20011116Bracket · cracked(AUS) LT AILERON HINGE BRACKET CRACKED AND BROKEN AT LOWER ATTACHMENT POINTS. LT INBOARD AND RT OUTBOARD BRACKETS ALSO CRACKED. SPAR AND RIB ALSO CRACKED.SDR AU010347Rocker Boss · cracked(AUS) ENGINE CYLINDER ROCKER HATS (2OFF) CRACKED AT PUSHROD END. EVIDENCE OF ROCKER HAT CONTACT ON THREE OTHER CYLINDERS.SDR 20000602SH004Crankshaft · unserviceablePER TELEDYNE CONTINENTAL MOTORS MSB 00-5, CRANKSHAFT WAS REJECTED BY TELEDYNE CONTINENTAL MOTORS. (X)SDR CA991229054Valve Guide · damaged(CAN) HIGH OIL CONSUMPTION - EXCESS OIL BEING SUCKED PASSED INTAKE VALVE GUIDE.SDR CA991112006Cylinder · worn(CAN) CYLINDER BORE EXIBITED EXCESSIVE WEAR RIDGE, OPERATOR SUSPECTS OVERHEAT IN THE PAST.SDR CA991027074Fitting · cracked(CAN) DURING SCHEDULED MAINTENANCE, THE LEFT OUTBOARD MAIN LANDING GEAR FITTING WAS FOUND CRACKED AT THE AFT LOWER RADIUS.SDR 97ZZZX4335Yoke · failedCESSNA HEAVY DUTY NOSE FORK SHEARED NEXT TO 4 BOLTS THAT SECURE IT TO THE NOSE STRUT. PN 1243620-1 NOSE GEAR HUB WAS NOT BROKEN AND DID NOT FAIL NOR DID THE 4 BOLTS. THE YOKE SHOWED NO SIGNS OF CORROSION OR CRACKS PREVIOUS TO ACCIDENT.SDR AU960257Bracket · broken(AUS) HORIZONTAL STABILISER TRIM ACTUATOR MOUNT BRACKET BROKEN - AIRCRAFT IS USED FOR SKYDIVING WITH DOORS REMOVED AND DEFLECTORFITTED - SUSPECT TURBULANCE CAUSED BY DEFLECTORS CAUSES EXCESSIVETURBULANT AIRFLOW OVER EMPENNAGE - SEE MDR 96/0178 FOR FURTHER INFOSDR AU960178Bracket · broken(AUS) ELEVATOR TRIM TAB CONTROL ACTUATOR MOUNTING BRACKET BROKEN AWAY FROM TAILPLANE CONNNECTION - AIRCRAFT IS USED FOR PARACHUTEOPERATIONS WITH THE DOORS OFF AND A WIND DEFLECTOR FITTED - SUSPECT CAUSED BY EMPENNAGE BUFFETING DUE TO FITMENT OF WIND DEFLECTOSDR 95ZZZX2684Bracket · brokenOUTBOARD TAB OF BRACKET BROKE OFF AFTER ONLY 434 HOURS. THIS IS THE SECOND BROKEN BRACKET IN 2 YEARS. BROKEN AT RADIUS NEAR NUTPLATE AND RIVETS WHERE IT ATTACHES TO THE HORIZONTAL STAB REAR SPAR.
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