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 = 'U206G' 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 = 'U206G' 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 CA040322007Cylinder Head · separated(CAN) IN FLIGHT SEPARATION OF CYL NR 3 HEAD.SDR AUS20040078Landing Gear · collapsed(AUS) LT MAIN LANDING GEAR LEG COLLAPSED. THE LEG WAS A NEWLY FITTED ITEM AND FAILED 530MM (20.8IN) FROM THE IB TIP OF THE LEG. AIRCRAFT TAILPLANE, ELEVATOR, WINGTIP AND POD DAMAGED.SDR AUS20040090Spring · broken(AUS) ENGINE STARTER ADAPTER CLUTCH SPRING TANG BROKEN OFF CAUSING SPRING TO SLIP ON GEAR. BROKEN PIECE OF SPRING FOUND IN BASE OF STARTER ADAPTER.SDR AUS20031305Brushes · worn(AUS) ALTERNATOR GROUND BRUSH ALMOST WORN AWAY. POSITIVE BRUSH WAS HARDLY WORN.SDR CA031103004Exhaust Valve · broken(CAN) THE FLIGHT CREW REPORTED A MINOR ENGINE VIBRATION AND HIGH NR 2 CYLINDER EGT AS WELL AS ERRATIC CHT INDICATIONS. EXAMINATION FOUND THAT DUE TO FAULTY INFORMATION FROM THE MULTI PROBE SYSTEM THE OBSERVED INFORMATION ACTUALLY REFLECTED NR 6 CYLINDER OPERASDR CA031013001Balance Weight · cracked(CAN) UPON INSPECTION IT WAS DISCOVERED THAT THERE WERE SMALL HAIRLINE CRACKS (HORIZONTAL) AT THE THREE MOST OUTBOARD MASS BALLANCE WEIGHT ATTACH SCREW LOCATIONS. ONE INCH IN LENGTH.SDR AUS20030997Hose · loose(AUS) STRONG SMELL OF FUEL IN COCKPIT. INVESTIGATION FOUND A LOOSE HOSE NUT CONNECTION ON THE FCU AND A LOOSE HOSE ON THE FUEL STRAINER ASSEMBLY. PERSONNEL/MAINTENANCE ERROR.SDR AUS20031008Hose · loose(AUS) FUEL PUMP TO FCU HOSE LOOSE AND LEAKING.SDR CA030912001Mount · cracked(CAN) CRACKS IN RADIUS OF ENGINE MOUNT SUPPORTSDR AUS20030927Attach Fitting · cracked(AUS) LT MAIN LANDING GEAR OUTBOARD ATTACHMENT FITTING CRACKED IN AREAOF UPPER REAR RADIUS.SDR AK02003F00003Battery · inoperativeDURING AN ANNUAL INSPECTION OF THE ELT UNIT, THE ELT BATTERY PACK WAS INSPECTED FOR CORROSION IAW FAR 91.207 PARA (D). VOLTAGE WAS PRESENT AT THE POWER SUPPLY PLUG PRIOR TO DISCONNECTING. THE BATTERY POWER SUPPLY ELECTRICAL PLUG WAS DISCONNECTED AND INSPECTESDR AUS20031071Capsule · misinstalled(AUS) AUTOPILOT ALTITUDE HOLD CAPSULE FITTED IN A DIFFERENT POSITION TO THAT STATED BY STC. PERSONNEL/MAINTENANCE ERROR. INCORRECT FIT.SDR AUS20031070Gps · misinstalled(AUS) AGPS AND RADIO TRANSCEIVER REMOVED AND GPS/COM FITTED. AUDIO PANEL REMOVED AND A DIFFERENT ITEM FITTED. SEVERAL DEFECTS FOUND ASSOCIATED WITH INSTALLATION. NO ENTRY IN LOG BOOK, NO WEIGHT AND BALANCE CHANGE, NO ELECTRICAL LOAD ANALYSIS NO E/O'S IN LOSDR AUS20030646Drive Gear · damaged(AUS) ENGINE STARTER DRIVE GEAR TEETH (7OFF) MISSING. INVESTIGATION ALSO FOUND CORRESPONDING CRANKSHAFT DRIVE GEAR TEETH DAMAGED.SDR AUS20030606Elevator · fod(AUS) ELEVATOR JAMMED. INVESTIGATION FOUND A PIECE OF METAL PROTRUDING FROM THE LT ELEVATOR BALANCE HORN DIRECTLY BEHIND THE BALANCE WEIGHT ATTACHMENT RIB. METAL MEASURED 12.7MM BY 57.15MM (0.5IN BY 2.25IN) WITH A THICKNESS OF 0.8128MM (0.032IN) AND APPEARSDR AUS20030631Bolt · failed(AUS) NOSE LANDING GEAR DRAG LINK ATTACHMENT BOLT HEAD SEPARATED FROM SHANK.SDR 2003FA0000584Bearing · wornWHILE INSPECTING THE AIRCRAFT, THE PILOTS YOKE TUBE WAS OBSERVED TO HAVE BEEN WORN DUE TO CHAFFING ON THE UNDERSIDE. THE COATING ON THE YOKE GUIDE ROLLER BEARINGS HAD WORN OFF AND THE TUBE HAD WORN ABOUT .3333 OF THICKNESS OF THE TUBE. IN ADDITION TO THE GUISDR CA030505006Skin · corroded(CAN) THE AIRCRAFT HAS A BLACK MATERIAL BONDED TO THE AIRCRAFT BELLY SKIN INTERIOR TO PREVENT OIL CANNING.SEVERE CORROSION WAS FOUND BETWEEN THE BONDED MATERIAL AND THE SKIN. IN SOME AREAS THE CORROSION EXTENDED TO A DEPTH EQUAL TO HALF OF THE SKINS .032 THICKSDR IKDC2003001Crankshaft · brokenWHILE CRUISING AT 6500 FT, THE ENGINE MOMENTARILY RAN ROUGH AND QUIT, NO WARNING INDICATIONS. THE AIRCRAFT SUCCESSFULLY LANDED ON A ROAD WITH NO INJURIES OR DAMAGE. AFTER LANDING, IT WAS NOTED THAT THE PROPELLER COULD NOT BE ROTATED. THE SUBSEQUENT ENGINE SDR AUS20030599Bolt · broken(AUS) NOSE LANDING GEAR DRAG LINK ATTACHMENT BOLT HEAD SEPARATED FROM SHANK.SDR EA332003B0364Propeller · overservicedGREASING PROP FOUND GREASE DID NOT COME OUT AFT ZERK FITTING HOLE ON SAME BLADE. AFT/TRAILING EDGE ZERKS WERE REMOVED. RATHER IT CAME OUT ANOTHER AFT GREASE ZERK FITTING HOLE. PROP WAS REMOVED AND SENT TO PROP SHOP WHO UPON DISASSEMBLY FOUND PROP HUB WAS COSDR RAIA00302051Connector5521-MLI - LANDING GEAR WOULD NOT RETRACT. MAINTENANCE DEFERRED IAW MEL 32-31-03. SUBSEQUENTLY REPLACING CONNECTOR 5004VC AND WIRES, OPS CK OK.SDR AUS20030020Exhaust Valve · worn(AUS) NO4 CYLINDER EXHAUST VALVE SEAT LEAKING. FOLLOWING VALVE REMOVALSEVERE EROSION WAS THEN FOUND ON THE NECK OF THE VALVE. NO5 CYLINDER EXHAUST VALVE WAS ALSO FOUND TO HAVE A SIMILAR EROSION PROBLEM. ALL OTHER VALVES WERE CHECKED AND FOUND TO BE IN NORMALCOSDR CA030115002Pump · cracked(CAN) DURING THE SCHEDULED OPERATION NR 2 ENGINE OF THE AIRCRAFT. A CRACK WAS NOTED ON THE ENGINE ATTACH BRACKET OF THE INSTALLED VACUUM PUMP. UPON REMOVAL OF THE PUMP IT WAS DISCOVERED THAT THE ENTIRE ATTACH BRACKET WAS COMPLETELY SEPARATED FROM THE PUMP. FLSDR CA021204005Fuel Line · ruptured(CAN) WATER CONTAMINATION IN ALUMINIUM FUEL LINE CAUSE DETERIOTION OF THE LINE BY CORROSION AND RUPTURE BY FREEZING. THIS LINE IS LOCATED BETWEEN WING TIP TANK AND ELECTRIC TRANSFER PUMP LOCATED IN WING.SDR 2003FA0000003Alternator · seizedPILOT REPORTED THAT THE AMMETER WAS SHOWING A DISCHARGE UPON ENGINE STARTUP. IT WAS DISCOVERED THAT THE ALTERNATOR HAD SEIZED AND THE BELT HAD BROKEN.SDR 2003FA0000001Thru Bolt · undertorquedTHE ALTERNATOR THROUGH BOLTS SECURING THE FRONT CASE HALF TO THE REAR CASE HALF WERE FOUND TO HAVE BACKED OUT, ALLOWING THE CASE HALVES TO SEPARATE APPROXIMATELY .1250 INCH. THE THROUGH BOLT RETAINERS AND SAFETY WIRE WERE STILL IN PLACE. THE ALTERNATOR HAD SDR AUS20021378Seat Track · cracked(AUS) SEAT TRACK CRACKED ACROSS LOCK PIN HOLES.SDR FMAA2002004Cylinder · crackedPROBLEMS ENCOUNTERED WITH SUPERIOR CYLINDERS, B OR B SERIES. NR 4 CYLINDER HAD STUCK EXHAUST VALVE AND BENT PUSH ROD. NR 1 AND NR 2 CYLINDERS HAD CRACKS EXTENDING FROM THE SPARK PLUG HOLE TO THE FIN AREA LEFT OF THE SPARK PLUG HOLE TO THE FIN AREA LEFT OF THSDR AUS20021380Dipstick · distorted(AUS) ENGINE OIL DIPSTICK BENT, GIVING AN INCORRECT READING OF OILQUANTITY. SUSPECT CAUSED BY BENDING THE DIPSTICK WHILE WIPING OFF THE OIL. BENT DIPSTICK CAN ALSO WEAR ON THE BOTTOM OF THE SUMP.SDR AUS20021188Motor · shorted(AUS) STARTER MOTOR WINDINGS SHORT CIRCUITED TO GROUND.SDR AUS20021009Magneto · worn(AUS) IMPULSE COUPLINGS WORN ON BOTH MAGNETOS.SDR AUS20020859Wheel · cracked(AUS) WHEEL CRACKED ALONG INBOARD EDGE OF BEAD SEAT. CRACK LENGTH APPROXIMATELY 120MM (4.72IN).SDR CA020726020Screw · broken(CAN) DURING CRUISE FLIGHT THE TRIM TAB ON THE HORIZONTAL STABILIZER STARTED TO FLUTTER CAUSING VIBRATION IN THE CONTROL COLUMN. TRIM MECHANISM JAMMED IN THE FULL NOSE UP SETTING. PILOT WAS FORCED TO OVERRIDE TRIM SETTING WITH CONTROL INPUTS AND LAND ON A NEARSDR 2002FA0000973Crankcase · crackedCRACK 1.3750 INCH OUT OF THE UPPER REAR CYLINDER BASE STUD, AT THE ONE OCLOCK POSITION.SDR AUS20020507Keel · cracked(AUS) FORWARD FUSELAGE RH KEEL MEMBER CRACKED IN UPPER FLANGE.SDR AUS20020482Control Cable · faulty(AUS) CSU CONTROL SYSTEM OUTER CABLE STRETCHED.SDR AUS20020481Fitting · loose(AUS) LT AFT INDUCTION DRAIN FITTING LOOSE ALLOWING FUEL TO RUN DOWN THE OUTSIDE OF THE DRAIN LINE AND DRIP ONTO THE EXHAUST.SDR 2002FA0000875Hub · corrodedPROPELLER CAME IN REPAIR STATION BECAUSE IT WOULD NOT CHANGE PITCH. THE PROPELLER WAS DISASSEMBLED. PROPELLER WAS FULL OF RUST, ALL STEEL PARTS WERE CONDEMNED. PROPELLER BLADES AND HUB WERE CONDEMNED FOR EXTENSIVE CORROSION. THE PROPELLER WAS FOUND TO BE USDR CA020515003Spark Plug · broken(CAN) ENGINE DEVELOPED A KNOCK ON RETURN FLIGHT IN CRUISE. REELED LOWER SPARK PLUG ON NR 6 CYLINDER BROKEN FLUSH WITH THE OUTSIDE OF THE CYLINDER. REMAINDER OF SPARK PLUG WAS FOUND HANGING ON THE LEAD. SPARK PLUG WAS REPLACED.SDR AUS20020578Csu · faulty(AUS) CONSTANT SPEED UNIT (CSU) FAULTY.SDR AUS20020421Exhaust Valve · failed(AUS) NR 4 CYLINDER EXHAUST VALVE LEAKING. INVESTIGATION FOUND EROSION AROUND THE HEAD OF THE EXHAUST VALVE AS WELL AS LEAKING AT THE VALVE SEAT SEALING FACE.SDR AUS20020876Bulkhead · cracked(AUS) RH FORWARD DOORPOST BULKHEADCRACKED.SDR AUS20020462Valve Guide · faulty(AUS) NR 5 CYLINDER EXHAUST VALVE STICKING IN VALVE GUIDE.SDR AUS20020423Exhaust Valve · leaking(AUS) ENGINE EXHAUST VALVES (2OFF) LEAKING. ENGINE HAD ONLY 441 HOURS SINCE FACTORY REMANUFACTURE.SDR AUS20020330Line · loose(AUS) CRANKCASE OIL PRESSURE LINE LOOSE.SDR AUS20020329Bracket · misinstalled(AUS) THROTTLE AND MIXTURE CABLE CLAMP BRACKET INSTALLED UPSIDE DOWN.SDR AUS20020328Control Cable · worn(AUS) ALL AILERON SYSTEM CABLES AND FLAP CABLES (4OFF) HAD BROKEN STRANDS OR WERE WORN EXCESSIVELY.SDR AUS20020025Condenser · faulty(AUS) MAGNETO CONDENSER FAULTY. A TOTAL OF FIVE CONDENSERS FAILED INAPPROXIMATELY 500 HOURS OF OPERATION. INVESTIGATION FOUND THATTHE FAILURE OCCURRED IN THE SMALL ATTACHMENT BRACKET HOLDING THECONDENSER IN THE POINTS CAVITY.SDR AUS20011385Ignition Switch · worn(AUS) IGNITION SWITCH TERMINALS WORN BEYOND LIMITS.
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