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 = '2105' 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 = '2105' 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 2017FA0000170Wire Rope · brokenFAILURE OF SECONDARY SEAT STOP INSTALLED PER SEB07-5. PILOT WAS UNABLE TO SLIDE THE SEAT AFT TO EXIT THE AIRCRAFT. INSPECTION DETERMINED THAT THE WIRE ROPE USED IN THE ACTUATOR MECHANISM FAILED AT THE CRIMPED END FITTING THAT ATTACHES TO THE SEAT.SDR 2013FA0000446Bracket · crackedBALANCE TUBE MOUNTING BRACKET CRACKED. TUBE CRACKED AT ONE END.SDR 2009FA0000330Bulkhead · crackedINSP PURSUANT TO AD-72-07-09 REVEALED A CRACK IN THE UPPER LT FLANGE AREA OF THE BULKHEAD. BULKHEAD WAS REPLACED. (K)SDR CA071227003Bolt · broken(CAN) WHILE TAXING ON BUSH STRIP, NOSE GEAR AFT DRAG STRUT BOLT BROKE AND WORKED OUT CAUSING NOSE GEAR TO FOLD FWD. (TC NR 20071227003)SDR 2006FA0000515Elt · failedELT FAILED UPON INSPECTION AFTER 12 MONTHS OF SERVICE, DID NOT TRANSMIT THROUGH ANTENNA, LIGHT WENT ON INDICATING FUNCTION. THIS IS THE 3RD FAILURE ON UNITS NEWER THAN ONE YEAR OLD, IN 1.5 YEARS IN OUR SHOP. (K)SDR CA060228011Magneto · failedNR 1 CYLINDER NOT FIRING. TRACED BACK TO INTERNAL PROBLEM WITH MAGNETO, RETURNED FOR WARRANTY.SDR CA060228012Oil Cooler · crackedOIL LEAK FROM OIL COOLER.SDR CA060228010Magneto · failedROUGHNESS ON STARTUP OF LT MAGNETO.SDR AU510001732Bulkhead · cracked(AUS) FUSELAGE DOORPOST BULKHEAD CRACKED. FOUND DURING INSPECTION IAW AD/C205/21. (AD/SB DESC: AD/C205/21 ) (CASA NR 510001732)SDR W322004F00000Yoke · crackedPILOT REPORTED THAT DURING LANDING FLARE, THE YOKE SNAPPED RESULTING IN A GO AROUND. AFTER INITIAL INSPECTION, YOKE WAS FOUND CRACKED COMPLETELY THROUGH ON UPPER LEFT HAND CORNER. YOKE MATERIAL APPEARS TO MANUFACTURED FROM PLASTIC, SUGGEST REMOVAL OF ALL PLASDR CA030305008Propeller · failed(CAN) FACTORY NEW PROPELLER STC SA00920CH. ONLY OBTAIN 2300 RPM STATIC, SHOULD BE 2600 RPM. FOUND BLADE LOW END STOPS INCORRECTLY SET.- PROP RETURNED TO OBTAIN NEEDED 2600 RPM. ERROR IN ENGINEERING APPROVAL AT MCCAULEY INCORRECT BLADE ANGLES.SDR AUS20021364Valve Guide · unserviceable(AUS) NO2 CYLINDER EXHAUST VALVE GUIDE CARBON BUILDUP. EXHAUST VALVESEIZED IN GUIDE CAUSING PUSHROD TO BEND AND SHROUD TUBE TO BE BROKEN.SDR 2002FA0000796Pump · failedENGINE LOST POWER, AIRCRAFT LANDED OFF AIRPORT. FOUND FUEL CONTAMINATION AND FUEL PUMP PRESSURE RELIEF VALVE STUCK. AD841001, WAS SIGNED OFF BUT FUEL HEADER TNKS WERE CONTAMINATED AND NO DRAIN VALVES HAD BEEN INSTALLED. CUSTOMER WAS NOTIFIED THAT PUMP HAD TSDR 20010501CW005Wheel · crackedMAGNESIUM 5.00-5 TYPE III WHEEL HALVES. FOUND CRACKS ADJAVENT TO THRU BOLT BOSSES AT PERIMETER ON BOTH WHEEL HALVES. POSSIBLE CAUSES, HARD LANDINGS OR OVER TORQUING.SDR 20010410AP002Floorbeam · corrodedDURING ANNUAL INSPECTION DISCOVERED SEVERE INTERGRANULAR CORROSION ON LEFT 4 INCHES OF ANGLE. CORROSION OCCURED PRIMARILY WHERE .25 IN. HI-SHEAR RIVITS ATTACH ANGLE TO BULKHEAD AND WING LIFT STRUT ATTACH FITTING. ANGLE WAS LESS THAN HALF ORIGINAL THICKNESS SDR CA000925033Crankcase · cracked(CAN) OIL LEAK TRACED TO CYLINDER HOLD DOWN AREA OF NR 2 CYLINDER. LARGE CRACK FROM 3 O''CLOCK POSITION. NR 2 CYLINDER UP TO 11 O''CLOCK. (X)SDR 20000831SH012Pump · leakingDURING POST-FLIGHT SECURING OF ACFT, PILOT NOTICED FUEL DRIPPING FROM LT COWL FLAP OPENING. INVEST REVEALED FUEL COMING FROM ENGINE DRAIN LINE TRACED TO THE FUEL INJECTION PUMP. SELECTING THE OFF POSITION OF THE FUEL SELECTOR VALVE RELIEVED THE FUEL TANK HEASDR AU980999Piston Ring · broken(AUS) NR 2 AND NR 4 CYLINDER OIL CONTROL RINGS BROKEN. PART TC: 89.SDR CA961018002Cylinder · head separated(CAN) HEAD BLOWN OFF CYLINDER.SDR AU961186Angle · corroded(AUS) DURING INSPECTION OF LH AND RH WINGS MISSING RIVET HEADS WERE FOUND ON THE WING UPPER SKIN THROUGH THE MAIN SPAR INBOARD TOP CAP - FOLLOWING REMOVAL AND DISASSEMBLY OF THE WINGS THE SEVERE EXFOLIATION CORROSION WAS FOUND ON THE FOLLOWING ANGLES ANDPLATSDR CA960515004Static Sensor · leaking(CAN) PIEZO STATIC SENSOR HOUSING LEAKING IN EXCESS OF LIMITSSDR 96ZZZX2295Static Port · leakingTHE SEALANT BETWEEN STATIC PORT AND SKIN OF AIRCRAFT HAD TURNED TO POWDER MAKING A LEAK IN THE STATIC SYTSEM. DRILLED RIVETS OUT OF STATIC PORT, SEALED WITH PR-1422 SEALANT. STARTED STATIC CHECK AGAIN, GOT UP TO 11,000 FEET AND A SEVERE LEAK STARTED AGAIN.
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