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 = '172B' 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 = '172B' 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 2015FA0000106Rib · crushedSKIN CRACKED UNDER RT HORIZONTAL STABILIZER. FURTHER INVESTIGATION REVEALED THAT THE INNER NOSE RIB WAS CRUSHED, BROKEN AND CRACKED. THE INNER NOSE RIB ON THE LT SIDE WAS DEFORMED BUT NOT ACTUALLY BROKEN. THE APPEARANCE OF BOTH RT & LT NOSE RIBS WAS CONSISTENTSDR 2005FA0001365Yoke · brokenUPON THE FLAIR ON LANDING AT NORMAL WEIGHTS THE CONTROL YOLK BROKE AT THE OUTSIDE LT RADIUS. THIS CAUSED THE NOSE WHEEL OF THE AC TO DROP AT A GREATER SPEED THAN NORMAL AND SHIMMY WAS EXPERIENCED THE MAIN GEAR HAD JUST TOUCHED DOWN WHEN THE FAILURE OCCURRED. SDR CA050624002Wheel · failedAS AIRCRAFT TAXIED FROM TIE-DOWN, NOSE WHEEL FAILED ABRUPTLY, APPROXIMATELY 15 FEET FROM TIE-DOWN, TUBE, TIRE AND NOSE WHEEL REMAINED IN YOKE, WITH NO DAMAGE TO TIRE OR YOKE.SDR 2003FA0000371Bolt · misinstalledDURING ANNUAL INSPECTION, THE RT DIRECT AILERON CABLE (PN 0510105-72) WAS FOUND TO BE CHAFFING ON THE RT WING AFT ATTACH BOLT THREADS AND NUT. FURTHER INVESTIGATION REVEALED THAT BOTH THE LEFT AND RT AFT WING ATTACH BOLTS WERE INSTALLED BACKWARDS WITH THE THRSDR CA020530009Piston · broken(CAN) ENGINE RAN WELL NO VISIBLE PROBLEM. PIECE OF PISTON SKIRT BROKEN LOOSE HELD IN BY OIL RING AND CYLINDER CURVE ONLY.SDR CA020102003Spar · cracked(CAN) AT ANNUAL INSPECTION THE CENTRE SECTION OF THE STABILIZER SPAR WAS FOUND TO BE BUCKLED AND CRACKED AT THE CENTRE LIGHTENING HOLE, WHERE THE TRIM CABLES RUN THROUGH. THERE WERE TWO CRACKS ABOUT 2 IN. LONG, RUNNING FROM THE BOTTOM RIGHT AND TOP LEFT SIDES SDR AU010180Crankcase · cracked(AUS) ENGINE IN AN EXTREMELY POOR CONDITION. DEFECTS INCLUDE CRACKED CRANKCASE, WORN CRANKSHAFT, WORN GEARS, WORN CYLINDERS AND VALVES.SDR 20001207SH012Hose · brokenDURING ANNUAL INSPECTION, OIL PRESSURE HOSE WAS FOUND WET WITH OIL. AFTER REMOVING HOSE, HOSE CRACKED AND BROKE WHEN TWISTED. FUEL HOSE WAS CHECKED AND WAS IN THE NEAR SAME CONDITION. NO LOG ENTRY FOUND AS TO WHEN AND IF THESE HOSES HAD BEEN REPLACED. (X)SDR 20001207SH011Elt · failedDURING ANNUAL INSPECTION, ELT WAS FOUND NOT TO MEET FAR 91.207(D). IT FAILED G-TEST AND WAS MOUNTED IMPROPERLY IN AIRCRAFT. IT WAS MOUNTED WITH VELCRO AND A DETERIORATED STRAP. (X)SDR 20001207SH010Selector Valve · inoperativeDURING ANNUAL INSPECTION, NOTED THE FUEL SELECTOR VALVE WOULD NOT SHUT OFF FUEL. THIS COULD BE A HAZARD IF AN IN-FLIGHT FIRE OCCURRED. (X)SDR AU990344Washer · missing(AUS) SEAT BELT FLOOR ATTACHMENT FITTINGS HAD THE WASHERS UNDER THE FORWARD NUTS MISSING.SDR 98ZZZX4063Rivets · corrodedDURING INSPECTION, AILERON BALANCE WEIGHTS WERE OBSERVED TO HAVE SEVERAL RIVET HEADS POPPED. FURTHER RIVETS COULD BE POPPED BY HAND (HEADS POPPING OFF). THE RIVET CORROSION WAS NOT VISIBLE FROM UNDER/AROUND HEADS.SDR AU980585Venturi · loose(AUS) CARBURETOR VENTURI LOOSE.SDR 97ZZZX2660Cylinder · crackedDURING AN INSPECTION, CYLINDER WAS FOUND WITH LOW COMPRESSION/EXHAUST VALVE LEAKAGE. CYLINDER WAS REMOVED FOR REPAIR AND SENT TO ENGINE SHOP. AFTER CLEANING, NOTED THE HEAD WAS CRACKED FROM THE ROCKER COVER FLANGE THROUGH THE EXHAUST PORT AND ACROSS TO THE USDR 97ZZZX2665Angle Cap · corrodedDURING HIDDEN DAMAGE INSPECTION OF WINGS AFTER HAIL AND WIND DAMAGE, THE FORWARD LT WING SPAR CAP WAS FOUND TO HAVE EXTENSIVE INTERGRANULAR CORROSION. SUBMITTER STATED THIS IS A COMMON PROBLEM ON CESSNAS THAT DID NOT HAVE WING PARTS PRIMED AT THE FACTORY.SDR 97ZZZX2664Spar · corrodedDURING HIDDEN DAMAGE INSPECTION OF WINGS AFTER HAIL AND WIND DAMAGE, FORWARD LEFT WING SPAR, EXTRUDED STIFFENER WAS FOUND TO HAVE SEVERAL SPOTS OF INTERGRANULAR CORROSION. SUBMITTER STATED THIS IS A COMMON PROBLEM ON CESSNAS THAT DID NOT HAVE ANY WING PARTS PSDR AU961158Seat Belt · wrong part(AUS) SEAT BELT WEBBING AND HARDWARE WAS OF AUTOMOTIVE ORIGIN - UNAPPROVED PART - PERSONNEL/MAINTENANCE ERRORSDR 95ZZZX4397Rib · corrodedFLAP TRACK PART DID NOT FAIL, HOWEVER, SEVERE CORROSION WAS FOUND DURING AN ANNUAL INSPECTION AT A POTENTIALLY WEAK AREA ON THE PART. CORROSION FOUND WAS INTERGRANULAR AND WAS ON BOTH SIDES OF THE PART IN AFFECTED AREA. SUBMITTER SUGGESTS A CLOSE INSPECTION
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