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 = '200' 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 = '200' 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 2005FA0001206Valve · bypassingWHEN THE THRUST REVERSERS WERE DEPLOYED ON THE AIRCRAFT, A VERY LOUD SQUEALING NOISE CAME FROM THE NOSE LANDING GEAR STEERING CONTROL VALVE.SDR 2005FA0001207Valve · leakingTHE NOSE WHEEL STEERING VALVE WAS LEAKING BEYOND LIMITS.SDR DXTA200500902Structure · bird strikeBIRD STRIKE DURING T/O ROLL OUT OF KSAV. ABORTED AT ABOUT 100 KTS. ACCOMPLISHED BIRD STRIKE INSPECTION IN ACCORDANCE WITH G200 MAINTENANCE MANUAL CHAPTER 05-55-00, NO DISCREPANCIES NOTED.SDR DXTA200500873Wire · damagedSTRONG SMOKE SMELL IN THE COCKPIT, THAT SMELLED LIKE BURNING WIRES ON APPROACH. TURNED OFF ALL LIGHTS AND AUDIO IN THE CABIN THE SMELL WENT AWAY SHORTLY AFTER. THE SMELL WAS MUCH STRONGER IN THE COCKPIT THAN THE CABIN. FOUND SCREW IN WIRE BUNDLE, REPAIRED WSDR DXTA200500846Flap System · malfunctionedSLATS AND FLAPS INTERMITTANT AFTER TAKEOFF, SELECTED FLAPS, SLATS & KRUEGERS UP. FLAPS STAYED AT 20 DEGREES, SLATS STAYED DOWN AND KRUEGER'S RETRACTED. ALSO HAD THE FOLLOWING ICAS MSG SLAT/FLAP MAINTEN. ITEM IS UNDER INVESTIGATION.SDR DXTA200500746Connector · shortedVIP SEAT VIDEO MONITOR PORT SHORTED OUT. SMOKE AND ACID SMELL WAS OBSERVED COMING FROM THE MONITOR PORT. - VERIFIED DISCREPANCY, FOUND VIP VIDEO MONITOR CONNECTOR TO BE BAD. DISABLED AND STOWED VIP VIDEO MONITOR CONNECTOR CANNON PLUG. ALL OTHER VIDEO MONITOR OSDR DXTA200500644Position Switch · shortedT/O UNSAFE EICAS ILLUMINATED DURING TAKEOFF ROLL. ABORTED AT 120 KNOTS. ATTEMPTED TO DUPLICATE INDICATION IN HANGER WITH EXTERNAL POWER SUPPLIED, COULD NOT DUPLICATE. INSPECTED ALL 8 AIRBRAKE SWITCHES VISUALLY FOR OBVIOUS DEFECTS, NONE NOTED. RANG OUT AIRBSDR DXTA200500619Door · icedRT MAIN GEAR WILL NOT LOCK UP. WHILE ACCOMPLISHING INCOMING INSP TO ACFT FOUND ICE TO BE FORMED ON I/B GEAR DOOR OF RT MLG. SUSPECT ICE BUILT UP TO CAUSE DOOR INTERFERANCE TO STRUCTURE AND NOT ALLOW DOOR TO FULLY UP AND LOCK. VERIFIED INTEGRITY OF SWITCHES.SDR 2005FA0000248Heater · inoperativeLT PITOT HEAT INOPERATIVE. FOUND PITOT PROBE HEATING ELEMENT ARCED. REMOVED AND REPLACED LT PITOT PROBE. (K)SDR DXTA200500602Panel · leakingFUEL LEAKING OUT OF RT WING IN FRONT OF AILERON ON TOP. AIRCRAFT WAS INFLIGHT FOR 1.4 HRS AND LOST APPROX 1000 LBS OF FUEL OVER THE NORMAL BURN. INSPECTED RT WING FOUND SEEPAGE FROM RT BOTTOM WING VENT (NACA SCOOP). OPEN WING PANEL 640UT, REMOVED OLD SEALANSDR CA050221009Engine · failed(CAN) DURING CLIMB THE ENGINE EMITTED A LOUD NOISE ACCOMPANIED BY A DECAY IN ALL ENGINE PARAMETERS. THE CREW SHUT THE ENGINE DOWN IN FLIGHT, DECLARED AN EMERGENCY AND DIVERTED TO POINT OF DEPARTURE. SUBSEQUENT INSPECTION REVEALED DAMAGE TO THE HIGH PRESSURE SDR DXTA200500595Engine · failedRIGHT ENGINE FAILED ON CLIMBOUT ABOUT 3 MINS AFTER TAKEOFF. FOUND ENGINE HAD INTERNAL FAILURE. REMOVED AND REPLACED RT ENGINE, LEAK CHECKED AND OPS CHECKED GOOD PER G200 MM 71-00-00.SDR DXTA200500507Door · bentLEFT MAIN GEAR WOULD NOT INDICATE UP, UPON GEAR RETRACTION (RED, UNKNOWN WAS SHOWING). JACKED AIRCRAFT AND ACCOMPLISHED RIGGING CHECK FOUND LT MLG I/B DOOR TO BE BENT. REMOVED AND REPLACED DOOR & RIGGED IAW G-200 MM 32-10-10.SDR 2005FA0000371B-Nut · splitLT HYDRAULIC PRESSURE LINE IN AFT EQUIPMENT BAY SPLIT AT AFT B-NUT FITTING. INSTALLATION WAS POST SB. PROBABLE CAUSE WAS STRESSED INSTALLATION AND VIBRATION. (K)SDR DXTA200400346Switch · malfunctionedLOST RT HYDRAULIC SYSTEM IN FLIGHT, RT HYD LEVEL LOW MESSAGE DISPLAYED. SYSTEM PRESSURE 400-600 PSI, LANDED AIRCRAFT USING EMERGENCY BRAKE SYSTEM. REMOVED AND REPLACED BRAKE CONTROL VALVE, PERFORM EMERGENCY BRAKE CHECK IAW MM CHAPTER 32-30-710-802. REPLACED RSDR VJ12004F00000Stiffener · crackedTHE THRUST REVERSER ASSY HAS STIFFNER ANGLES THAT GO AROUND THE BARREL. THE POINT WHERE THE ANGLE ATTACHES IS CRACKED AT ONE LOCATION. SEVERAL OTHER THRUST REVERSER ASSY WERE EVALUATED ON AIRCRAFT IN HOUSE AND NO CRACKS WERE NOTED. IT APPEARS THAT THE ANGLESDR DXTA200400313Controller · malfunctionedDURING FLIGHT THE COCKPIT AUTO TEMP MESSAGE ILLUMINATED, AFTER SWITCHING COCKPIT TEMP CONTROLLER TO MANUAL, SYSTEM WAS NORMAL AS LONG AS THE TEMP CONTROL KNOB WAS FULL COLD. PLACED TEMP CONTROL KNOB TO WARM AND NOTICED FUMES OF HOT MELTING PLASTIC, FOLLOWED BSDR K5S2004F00000Connector · failedJ2 CONNECTOR FAILED TO LOCK.SDR DXTA200400298Controller · malfunctionedCOULD NOT CONTROL PRESSURIZATION IN AUTO OR MANUAL MODE WITH SEVERAL ATTEMPTS, DECLARED EMERGENCY AND DIVERTED TO ILM. COMPLIED WITH ENGINE RUN UP TO MAX CLIMB DETENT SEVERAL TIMES, UNABLE TO DUPLICATE DISCREPANCY AT THIS TIME. ALL WORK DONE PER GULFSTREAM-2SDR 2004F00155Brushes · wornCREW REPORTED APU INOPERATIVE TROUBLESHOT SYSTEM AND FOUND VOLTAGE AVAILABLE AT STARTER GEN. REMOVED STARTER GEN AND BRUSH COVER. FOUND 2 OUT OF 4 BUSHES WELDED IN BRUSH HOLDERS AND BUSH WIRES BROKEN OFF. INSULATION STRIP ON INSIDE OF BRUSH COVER WORN BURNESDR DXTA200300167Arm · malfunctionedAFTER SELECTING GEAR UP, THE RIGHT GEAR WOULD NOT INDICATE UP, HAD RED GEAR DISAGREEMENT LIGHT. REMOVED LT & RT MAIN GEAR DOOR ASSEMBLY ARMS AND INSTALLED NEW ARMS OF SUPERCEDED P/N'S. PERFORMED MAIN GEAR DOORS OUTBOARD AND INBOARD RIGS AND OPS CHECKS. GEAR
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