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 = 'U206F' 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 = 'U206F' 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 96ZZZX4316Hose · leakingHOSE ASSY FAILED AFTER 2 YEARS AND LESS THAN 200 HOURS OF OPERATION. HOSE TSO: C531, MFG DATE A1094, LOT NR 06827.SDR 96ZZZX4318Nut · fracturedLIFT STRUT HAS 5 BOLTS, AN5, THROUGH TOP AND BOTTOM. TOTAL OF '5' NUTS HAD FAILED (FIFTY PERCENT). RIGHT LIFT STRUT ALL NORMAL. CAUSE UNKNOWN, NUT P/N NAS679AW.SDR AU960974Battery · leaking(AUS) ELT BATTERY PACK LEAKING - CORROSIVE MATERIAL FROM THE BATTERY HAD LEAKED ONTO THE AIRFRAME STRUCTURE CAUSING CORROSION - EXPIRRATION DATE OF BATTERY IS 22 MAY 1996SDR AU960996Bulkhead · cracked(AUS) FORWARD DOORPOST BULKHEAD CRACKEDSDR AU960993Hub · cracked(AUS) PROPELLER HUB CRACKED AND LEAKING IN TWO PLACESSDR 96ZZZX3441Ring · brokenTEMPORARY POWER LOSS DURING CRUISE. SUSPECT CAUSE: BROKEN PISTON RING WHICH BECAME WEDGED BETWEEN PISTON AND CYLINDER WALL. REPLACED COMPLETE CYLINDER ASSY.SDR CA970527012Blade · cracked(CAN) PROPELLER RECEIVED FOR OVERHAUL. PROPELLER BLADE WAS FOUND WITH CRACKED THREADS. PROPELLER WAS NEW IN 1986, CORROSION INSPECTION CARRIED OUT IN 1992. THIS WAS THE FIRST OVERHAUL, NOT REQUIRED BY CARS, BUT DONE AT CUSTOMERS REQUEST. THE PROPELLER WAS SCRASDR AU961004Crankcase · cracked(AUS) CRANKCASE CRACKED FROM NO2 CYLINDER MOUNT PADSDR AU960862Mount · deteriorated(AUS) FORWARD LH RUBBER ENGINE MOUNT PERISHED AND HOLED - SUSPECT CAUSED BY EXHAUST AFTER PROTECTIVE HEAT SHROUD FELL OFFSDR CA960424021Rod End · broken(CAN) BOW WHEEL FAILED TO RETRACT, FOUND ROD END HAD BEEN BROKEN NEXT TO THE CENTRE BALL ALLOWING THE ROD END TO PULL AWAY FROM THE BALL END. SUSPECT INCORRECT RIGGING DUE TO THE 1/4 INCH DISTANCE OF THE ROD END FROM THE GEAR WITH THE GEAR MANUALLY RETRACTED USDR 96ZZZX2454Servo · leads shortingSERVO MOTOR LEADS SHORTING TO FRAME OF PITCH SERVO ONLY WHEN TORQUE APPLIED ON MOTOR WHICH CAUSES PITCH OSCILLATION, PLUS OR MINUS 1,500 FEET/MINUTE. SUBMITTER RECOMMENDS ROUTING TO PREVENT TOUCHING FRAME.SDR 96ZZZX1480Torque Plate · bushing partedDURING AN ANNUAL INSPECTION, GUIDE BUSHING ON BRAKE TORQUE PLATE FOUND SEPARATED.SDR CA960223005Reinforcement · cracked(CAN)LEFT HAND HORIZONTAL STABILIZER REINFORCEMENT PART #12326231 FOUND CRACKED.SDR 96ZZZX1995Hub · crackedINSPECTION FOUND CRACK IN BLADE RETENTION THREAD OF HUB SOCKET.SDR CA960430201Crankshaft · failed(CAN) FOUND CRACK IN CRANKCASE AT #2 CYLINDER. #4 CONNECTING ROD DEPARTED CRANKSHAFT CAUSING INTERNAL ENGINE DAMAGE. DISASSEMBLY OF ENGINE FOUND ALL MAIN BEARING BABBITT OVERLAYS WERE SMEARED FROM OIL STARVATION. ALL CONNECTING ROD BEARINGS SMEARED FROM LUB DISDR 96ZZZX2787Bulkhead · crackedDURING ROUTINE ANNUAL INSP, DISCOVERED FWD CABIN DOORPOST BULKHEAD CRACKED ON LT AND RT SIDES AT WING LIFT STRUT ATTACH FITTINGS. INSP WAS DONE IAW CESSNA SEB 93-5 R1. PREVIOUS INSP OF THIS AREA DURING ANNUAL AND WHEN C/W CESSNA SEB 93-5, FAILED TO FIND THISSDR EY2R9600243Hub · corrodedPROP ASSY HUB IS CORRODEDSDR EY2R9600242Nut · corrodedPROP ASSY NUT IS CORRODEDSDR EY2R9600241Ferrule · corrodedPROP ASSY FERRULE IS CORRODEDSDR EY2R9600240Ferrule · corrodedPROP ASSY FERRULE IS CORRODEDSDR EY2R9600239Retain Bearing · corrodedPROP ASSY RETAIN BEARING IS CORRODEDSDR EY2R9600238Blade · corrodedBLADE SN KK041YSI CORRODEDSDR CA951221013Mount · cracked(CAN)WHILE CARRYING OUT ROUTINE INSPECTION, BOTH REAR ENGINE MOUNTS WERE FOUND CRACKED. CRACKS WERE APPROXIMATELY ONE INCH LONG. NEW MOUNTS INSTALLED AND AIRCRAFT RETURNED TO SERVICE.SDR CA951114009Hub · cracked(CAN)PROPELLER HAD PERSISTENT "RED DYE" OIL LEAKS SINCE SEPTEMBER 1989, PROPELLER REMOVED SIX TIMES FOR LEAKS. LAST REMOVAL/INSPECTION HUB THREADS FOUND CRACKED AND PROPELLER REMOVED FROM SERVICE.SDR 95ZZZX2378Cylinder · misinstalledTOTAL TIME 1067.8 SMOH. TIME SINCE TOP OVERHAUL 125.0. DURING MAINTENANCE TO REPAIR BURNED VALVES UPON CYLINDER REMOVAL, FOUND CYLINDERS GLUED ON AT BASE. (IT TOOK OVER AN HOUR USING AIR PRESSURE AND PULLING AND PRYING TO REMOVE ONE CYLINDER). IT SEEMS THASDR 95ZZZX1426Impulse Coupling · stop brokeTHE IMPULSE COUPLING STOP ON LEFT MAG BROKE OFF AND FELL DOWN INTO OIL SUMP. IT MADE THE IMPULSE COUPLING INOPERATIVE FOR STARTING, BUT DID NOT HARM NORMAL OPERATION OF MAG. THE STOP PIECES COULD HAVE DAMAGED ACCESSORY DRIVE GEARS, BUT DID NOT. SUBMITTER RECSDR 95ZZZX1097Line · corrosionDURING AN ANNUAL INSPECTION OF ACFT, LT WING TIP FUEL TANK (FLINT AERO) FUEL LINE TO TRANSFER PUMP FOUND TO HAVE FUEL STAINS IN SEVERAL PLACES & WAS WET TO THE TOUCH. UPON REMOVAL OF FUEL LINE FOR INSP, FOUND SEVERAL PIN HOLES IN AREAS OF THE FUEL STAINS & CO
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