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 = 'PC12' 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 = 'PC12' 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 CA060129007Governor · faulty(CAN) DURING CRUISE THE PROPELLER SPEED DECREASED. AN UNSCHEDULED LANDING WAS CARRIED OUT WHICH RESULTED IN A PROPELLER STRIKE. SUBSEQUENT INSPECTION REVEALED A FAULTY PROPELLER OVERSPEED GOVERNOR. IAW WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCESDR CA060227007Fuel Control · failedDURING AIRCRAFT FLIGHT TESTING, THE ENGINE DID NOT RE-LIGHT FOLLOWING A COMMANDED INFLIGHT SHUT DOWN FOR RE-LIGHT TEST PURPOSES. A DEAD STICK LANDING WAS ACCOMPLISHED. THE FUEL CONTROL UNIT AND FLOW DIVIDER VALVE WERE SUBSEQUENTLY REPLACED. P&WC WILL MONITOSDR CA060129010Engine · malfunctioned(CAN) DURING FLIGHT TEST OPERATIONS (PERFORMING ENGINE RELIGHT) ENGINE DID NOT RELIGHT. A DEADSTICK LANDING WAS ACCOMPLISHED. MFG WILL INVESTIGATE THE EVENT AND WILL ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TC NR 20060129010)SDR CA060129020Fuel Control · faultedDURING TAXI, THE ENGINE EXPERIENCED AN UNCOMMANDED POWER REDUCTION. THE ENGINE WAS SHUT DOWN. SUBSEQUENT INSPECTION REVEALED A FAULTY FUEL CONTROL UNIT. P&WC WILL INVESTIGATE THE INCIDENT AND ADVISE OF ROOT CAUSE ONCE DETERMINED.SDR AU510001581Accumulator · leaking(AUS) HYDRAULIC ACCUMULATOR LEAKING.(OTHER CAUSE: HIGH CYCLES ) (CASA NR 510001581)SDR AU510001494Actuator · faultyAUTOPILOT PITCH ACTUATOR INCORRECT OPERATION. ACTUATOR HAD BEEN MODIFIED IAW HONEYWELL SB KSA372-M1 TO COMPLY WITH PILATUS SB 22-004 AND AD/PC12/39A1.SDR QML2005F00001Actuator · inoperativeWHEN THE AIRCRAFT IS FLOWN AT VERY LOW TEMPERATURES (BELOW -15 C) FOR MORE THAN 30 MINUTES, AND THE FLAPS ARE SELECTED THE FLAPS FAIL TO MOVE, FLAP WARNING IS GIVEN ON THE CAWS PANEL AND THE FLAPS ARE RENDERED INOPERATIVE. ONCE THE AIRCRAFT IS ON THE GROUND, SDR QML2005F00000Actuator · inoperativeWHEN THE AIRCRAFT IS FLOWN AT VERY LOW TEMPERATURES (BELOW -15 C) FOR MORE THAN 30 MINUTES, AND THE FLAPS ARE SELECTED THE FLAPS FAIL TO MOVE, FLAP WARNING IS GIVEN ON THE CAWS PANEL AND THE FLAPS ARE RENDERED (INOPERATIVE). ONCE THE AIRCRAFT IS ON THE GROUNDSDR CA051006015Fcu · failed(CAN) IN FLIGHT, THE CREW REPORTED A LOUD NOISE ACCOMPANIED BY AN ENGINE SURGE. ENGINE POWER ROLLED BACK AND RECOVERED WITHOUT PILOT INPUT. THE AIRCRAFT DIVERTED FOR AN UNSCHEDULED LANDING. THE FUEL CONTROL UNIT WAS SUBSEQUENTLY REMOVED FOR INVESTIGATION. MSDR TVD2005F00000Line · deterioratedWHILE FLYING AT 170 KIAS, THE PILOT NOTED HE HAD TO REDUCE POWER TO MAINTAIN 170 KIAS. SHORTLY AFTER THAT THE AIRCRAFT`S (STICK SHAKER) ACTIVATED. INSPECTION REVEALED SEVERELY DETERIORATED PLASTIC TUBING FROM FWD PRESSURE BULKHEAD TO AIR DATA COMPUTER. LINESDR CA041215007Engine · failed(CAN) DURING CLIMB (6000 FT) THE ENGINE EXPERIENCED AN UNCOMMANDED POWER ROLL-BACK ACCOMPANIED BY ITT INCREASE, A LOUD BANG AND FLAMES EVIDENT FROM THE EXHAUST. THE PILOT SHUT THE ENGINE DOWN IN FLT, DECLARED AN EMERGENCY AND SUBSEQUENTLY LANDED ON A ROAD. PWSDR CA040831001Relay · burned(CAN) UPON APPROACH GEAR DOWN POSITION WAS SELECTED AND THE POWERPACK FAILED TO OPERATE THE MAIN GEAR EXTENDED FULLY AS DESIGNED AND THE NOSE GEAR FAILED TO GIVE A GREEN DOWN AND LOCKED POSITION INDICATION. THE APPROACH WAS ABORTED AND A GO AROUND WAS CARRIEDSDR AUS20040302Pad · separated(AUS) BRAKE ASSEMBLY WEAR PAD SEPARATED FROM BRAKE DISC ROTOR AND DAMAGED FOUR MORE PADS CAUSING THE BRAKE UNIT TO LOCK UP.SDR AUS20040271Servo · faulty(AUS) AUTOPILOT ROLL SERVO FAULTY. INVESTIGATION FOUND THAT THE SCREWS HOLDING THE CLUTCH HAD LOOSENED ALLOWING THE CLUTCH TO REMAIN ENGAGED WHEN THE AUTOPILOT WAS DISENGAGED.SDR AUS20040270Drive Shaft · sheared(AUS) NR 2 GENERATOR DRIVESHAFT SHEARED.SDR CA040406004Actuator · failed(CAN) PILOT REPORTED A CLACKING NOISE IN FLIGHT COMING FROM THE INSTRUMENT PANEL. DURING TROUBLESHOOTING THE INTERNAL BY PASS DOOR WAS FOUND INOP. IN THE CLOSED POSITION. FURTHER INVESTIGATION REVEALED AN INTERNAL FAILURE AS THE STOP BUTTON THAT ACTUATES THE ISDR AUS20040251Balance Weight · separated(AUS) RT MAIN LANDING GEAR TIRE BALANCE WEIGHT SEPARATED.SDR AUS20040256Seat · cracked(AUS) PILOTS SEAT BACKREST ASSEMBLY CRACKED IN TWO PLACES.SDR AUS20040203Ring · worn(AUS) NOSE LANDING GEAR OVEREXTENDED. INVESTIGATION FOUND THE OLEO GUIDE RING WORN AND DAMAGED ALLOWING THE RETAINING PINS TO MIGRATE OUT DISCONNECTING THE GUIDE TUBE FROM THE NOSE FORK.SDR AUS20040106Drive Shaft · worn(AUS) NR 2 GENERATOR DRIVESHAFT WORN AT INNER (FORWARD) BEARING AREA.SDR AUS20040088Rotor · broken(AUS) RT BRAKE ROTOR BROKEN INTO TWO PIECES WITH ONE PIECE LODGING BETWEEN THE BRAKE ASSEMBLY AND WHEEL. ON DISASSEMBLY IT WAS NOTED THAT THE ROTOR HAD BEEN BROKEN FOR SOME TIME.SDR AUS20040001Rod · sheared(AUS) LT NOSE LANDING GEAR DOOR OPERATING ROD BROKEN IN AREA LOCATEDADJACENT TO LOWER WITNESS HOLES.SDR AUS20031224Pressure Switch · intermittent(AUS) HYDRAULIC PRESSURE SWITCH INTERMITTENT IN OPERATION.SDR AUS20031201Actuator · corroded(AUS) PITCH TRIM ACTUATOR TOP ATTACHMENT FITTING CORRODED. SUSPECTED INTERGRANNULAR TYPE CORROSION IS CAUSING THE SURFACE PROTECTIVE COATING TO LIFT.SDR AUS20031162Windshield · cracked(AUS) COPILOT'S WINDSHIELD CRACKED IN OUTER LAYER.SDR AUS20031113Governor · failed(AUS) ENGINE OVERSPEED GOVERNOR FAULTY.SDR AUS20031043Drive Shaft · sheared(AUS) NR 2 GENERATOR DRIVESHAFT SHEARED.SDR AUS20031105Switch · failed(AUS) HYDRAULIC PRESSURE SWITCH FAILED.SDR AUS20031104Pump · failed(AUS) RT FUEL BOOST PUMP FAILED.SDR AUS20030963Structure · damaged(AUS) LT ELEVATOR DAMAGED. LT HINGE POINT ON HORIZONTAL STABILISER ANDTRIM ACTUATOR ALSO DAMAGED.SDR AUS20030856Pdu · faulty(AUS) FLAP POWER DRIVE UNIT (PDU) FAULTY.SDR AUS20030814Actuator · faulty(AUS) FLAP LINEAR ACTUATOR FAILED BACKLASH TEST IAW AD/PC-12/13. FLAP BACKLASH 0.8128MM (0.032IN). MAXIMUM BACKLASH LIMIT 0.508MM (0.020IN).SDR AUS20030820Wire · chafed(AUS) FUEL BOOST PUMP WIRING CHAFING NEAR PLUG. FOUND DURING INSPECTION IAW SB PC12/37.SDR AUS20030819Wire · worn(AUS) FUEL BOOST PUMP WIRING CHAFING. FOUND DURING INSPECTION IAW SBPC12/37.SDR AUS20030818Wire · chafed(AUS) LT AND RT FUEL BOOST PUMP WIRING CHAFING. FOUND DURING INSPECTION IAW SB PC12/37.SDR AUS20030726Actuator · failed(AUS) LT TRAILING EDGE FLAP INNER LINEAR ACTUATOR FAILED.SDR AUS20030725Actuator · failed(AUS) RT TRAILING EDGE FLAP OUTER LINEAR ACTUATOR FAILED.SDR AUS20030579Transmitter · failed(AUS) ANGLE OF ATTACK (AOA) TRANSMITTER STUCK.SDR AUS20030605Wire · worn(AUS) ALTIMETER POWER WIRING CHAFING IN AREA APPROXIMATELY 175MM(6.8IN) FROM ALTITUDE SELECT CONTROL PANEL. WORN WIRING GROUNDED ON INSTRUMENT PANEL FRAMEWORK.SDR AUS20030554Blade · fod(AUS) FIRST STAGE COMPRESSOR BLADES SEVERELY DAMAGED BY FOD. FOUND DURING INSPECTION IAW AD/ENG/5 A7.SDR AUS20030362Potentiometer · out of adjust(AUS) AIRCRAFT HEATING SYSTEM POTENTIOMETER INCORRECTLY SET.SDR AUS20030356Separator · contaminated(AUS) WATER SEPARATOR BAG CLOGGED.SDR AUS20030337Transmitter · failed(AUS) ANGLE OF ATTACK (AOA) TRANSMITTER FAULTY. INSPECTION FOUND THEVANE BEARING ROUGH TO ROTATE AND VANE STICKING.SDR AUS20021423Transmitter · seized(AUS) RT ANGLE OF ATTACK TRANSMITTER SEIZED.SDR AUS20021422Pressure Switch · failed(AUS) HYDRAULIC POWERPACK LOW PRESSURE SWITCH FAILED.SDR AUS20021317Drive Shaft · sheared(AUS) NR 2 GENERATOR DRIVE SHAFT FRACTURED AT SHEAR POINT.SDR AUS20021283Relay · faulty(AUS) HYDRAULIC POWER RELAY FAULTY.SDR AUS20021117Transmitter · failed(AUS) LT ANGLE OF ATTACK (AOA) TRANSMITTER VANE SPRING DEFECTIVE.SDR AUS20021147Proximity Switch · failed(AUS) FLAP PROXIMITY SWITCH FAULTY.SDR AUS20021284Windshield · cracked(AUS) RT WINDSHIELD OUTER LAYER CRACKED.
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