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 = '172N' 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 = '172N' 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 CA190201017Alternator · inoperative(CAN) AT CRUISE RETURNING TO BASE CREW NOTICED ALTERNATOR DROPPED OFF. CREW CHECKED SWITCH AND CIRCUIT BREAKER. CHECKED OK. ON FINAL INTO CYBW INTERMITTENT FLAPS, RADIO AND LIGHT FAILURES. UPON INVESTIGATION AND INSPECTION THE POWER TERMINAL TO THE ALTERNATOR SDR 2020FA0000034Magneto · malfunctionedRIGHT SIDE OF MAG FAILED CHECK. UPON INSPECTION IT WAS FOUND THAT THE LEFT SIDE WAS TIMED TO 22 AND THE RIGHT SIDE WAS TIMED TO 10 BTDC, ALSO THE RIGHT POINTS WERE ONLY OPENING EVERY OTHER CYLINDER CAUSING IT TO ONLY FIRE 2 OF THE 4 CYLINDERS. WHEN I OPENED SDR CA180207025Limit Switch · failed(CAN) PILOT NOTED THAT THE FLAPS WOULD NOT RETRACT FROM 10 DEGREES AFTER LANDING. AIRCRAFT WAS BROUGHT INTO HANGAR AND FLAP SYSTEM WAS CHECKED. IT WAS DISCOVERED THAT THE FLAP UP LIMIT SWITCH P/N S1906-1 ON THE FLAP POSITION SELECTOR HAD FAILED. AME DECIDEDSDR 2017FA0000607Collar · looseFLAPS FAILED IN FLIGHT: FOUND FLAP SWITCH'S ACTUATING COLLAR UNSCREWED FROM FLAP ACTUATING TUBE ON JACK SCREW.SDR 2017FA0000295Pump · lowTHIS AIRCRAFT WAS MODIFIED BY INSTALLATION OF A 180 HP ENGINE IN ACCORDANCE WITH STC SA00461SE AT AIRCRAFT TOTAL TIME 7898.6 AND HAS FLOWN 26.9 HOURS SINCE. IN THOSE 26.9 HOURS, AIRCRAFT HAS EXPERIENCED TWO INFLIGHT COMPLETE ENGINE SHUTDOWNS. THE CAUSE WAS DETSDR 2016FA0000504Line · chafedDURING INVESTIGATION FOLLOWING AN INSTRUMENT PANEL FIRE ON LANDING ROLLOUT, THE INCOMING PRIMER LINE UNDER THE INSTRUMENT PANEL HAD BEEN CHAFFED THROUGH BY A LANDING LIGHT WIRE. THE CHAFFING HAD CREATED A PIN HOLE IN THE PRIMER LINE AND THE RESULTING FIRE APPSDR 2016FA0000402Cylinder Head · crackedENGINE FOUND TO MAKE WHISTLING SOUND WHEN PROP PULLED THROUGH ON PRE-FLIGHT. INSPECTION FOUND THE NR 1 CYLINDER HEAD CRACKED AFT OF THE INTAKE VALVE. CRACK LENGTH APPROXIMATELY 2 INCHES IN LENGTH. THIS CYLINDER PRESSURE CHECKED GOOD 5.98 HOURS EARLIER WHEN ITSDR 2016FA0000401Cylinder Head · crackedENGINE FOUND TO MAKE A WHISTLING SOUND WHEN PROP PULLED THROUGH ON PRE-FLIGHT. INSPECTION FOUND THE NR 3 CYLINDER HEAD CRACKED AFT OF THE INTAKE VALVE. CRACK LENGTH APPROXIMATELY 2 INCHES IN LENGTH. THE CRACK ALSO HAD A SMALL HOLE AT IT'S CENTER APPROXIMATELY SDR RTE2016F00000Magneto · failedMAGNETO FAILED IN FLIGHT, 30.1 HRS TSN 11 DAYS AFTER FIRST INSTALLATION. DID NOT OPEN MAGNETO TO DETERMINE CAUSE OF FAILURE DUE TO MFG WARRANTY LIMITATIONS CONCERNING DISTURBING THE SEAL. MAGNETO BEING RETURNED TO MFG UNDER WARRANTY.SDR CA160221004Control Cable · frayed(CAN) BOTH RUDDER CABLES FOUND FRAYED AT PULLEYS.SDR CA160221003Control Cable · frayed(CAN) BOTH AILERON DIRECT CABLES FRAYED AT PULLEYS. NORMAL WEAR.SDR CA160211008Tube · failed(CAN) STUDENT AND INSTRUCTOR WERE TAXING TO RUNWAY WHEN STUDENT NOTICED STEERING FELT STIFF. INSTRUCTOR TOOK OVER AND MOVED ACFT OFF TO SIDE OF TAXIWAY. INSTRUCTOR SHUTDOWN ACFT, GOT OUT AND FOUND NOSE WHEEL TIRE FLAT.SDR CA160205007Heater · smoke(CAN) DURING TAXI FOR TAKOFF, PILOT REPORTED SMOKE IN THE COCKPIT AND REQUESTED RETURN TO BLOCKS. SUBSEQUENT INSPECTION COULD FIND NO DEFECT WITH WIRING OR WITH TUBING IN THE ACFT AND THE ELECTRICAL AND HEATING SYS WAS GROUND CHECKED SERVICEABLE. THE ACFT WASDR CA160114007Lifter · loose(CAN) UPON TAKEOFF, THE PILOT FELT SIGNIFICANT ENGINE VIBRATION AND REDUCTION OF POWER. AN UNSCHEDULED AND UNEVENTFUL LANDING WAS EXECUTED. ON INSPECTION, MAINTENANCE FOUND THE NR 2 CYLINDER INTAKE HYDRAULIC LIFTER, PN 15B28040/17113IM, HAD LOST THE RETAINING SDR CA151217005Magneto · not reported(CAN) MAGNETO TIMING ADVANCED 3 DEGREES IN 50HRS SINCE 500HR INSP.SDR CA151217004Magneto · out of limits(CAN) MAGNETO TIMING ADVANCED 5 DEGREES IN 50 HRS SINCE 500 HR INSPECTION.SDR 2015FA0000558Bolt · brokenPISTON CONNECTING ROD BOLT BROKE CAUSING PISTON ROD TO PENATRATE ENGINE CRANKCASE CAUSING OIL DEPLETION AND ENGINE FAILURE.SDR CA151008006Exhaust Valve · failed(CAN) A FLIGHT INSTRUCTOR AND STUDENT WERE PRACTISING PRECAUTIONARY LANDINGS. AFTER INSPECTING A SUITABLE FIELD, STUDENT PROCEEDED TO OVERSHOOT. AFTER FULL POWER WAS APPLIED, THE ENGINE BEGAN TO RUN ROUGH WITH LOSS OF RPM OBSERVED. THE FLIGHT INSTRUCTOR TOSDR 2015FA0000390Wheel · crackedWHILE VISUALLY INSPECTING A WHEEL HALF ASSEMBLY, PN 16204700, OF 40113 WHEEL ASSEMBLY. A CRACK WAS DISCOVERED IN ONE OF THE WHEEL BOLT FEED THROUGHS ON THE INSIDE OF THE WHEEL HALF. THIS WAS MOST LIKELY CAUSED BY IMPROPER TORQUE OF THE WHEEL HALF BOLTS. THESDR CA150611007Magneto · malfunctioned(CAN) MAGNETO WOULD NOT TIME PROPERLY AT 490 HRS TTSN. SUSPECT CARBON TRACKING OR OTHER INTERNAL FAILURE.SDR FTUR20150526002Rotor · looseREMOVED AND DISASSEMBLE MAGNETOS FOR 500 HOUR INSPECTION AND FOUND ELECTRODE ON ROTOR LOOSE AND CAM EXCESSIVELY WORN.SDR FTUR20150526001Electrode · looseREMOVED AND DISASSEMBLED MAGNETOS FOR 500 HR INSPECTION AND FOUND ELECTRODE ON ROTOR LOOSE AND CAMS EXCESSIVELY WORN.SDR BQVR201505260001Door Frame · crackedWHILE COMPLYING WITH SEB 03-5, DISCOVERED CRACK IN LT DOOR POST ASSEMBLY WHERE 3 LOWER DOOR HINGE ATTACH FASTENERS ARE LOCATED. SEB 03-5 HAS YOU INSPECT FOR CRACKS IN THIS AREA AND DIRECTS YOU TO SK172-154 TO MODIFY THE FORWARD LOWER CABIN DOOR POST IF CRACKSSDR CA150526001Transponder · smoke(CAN) DURING TAXI OF ACFT, SMOKE WAS NOTICED COMING OUT FROM FACE OF TRANSPONDER. ACFT WAS SHUTDOWN & MAIN BASE NOTIFIED. AN INSPECTION WAS CARRIED OUT FROM A LOCAL AMO & DETERMINED TO BE AN INTERNAL PROBLEM WITH THE TRANSPONDER. THE UNIT WAS REMOVED & ACFTSDR CA150511012Tube · broken(CAN) THE ACCELERATOR TUBE BROKE & BECAME JAMMED IN BETWEEN THE BUTTERFLY VLV & HOUSING OF THE CARB. THE PILOT WAS UNABLE TO ADJUST THE THROTTLE CONTROL. THE TUBE EVENTUALLY DISLODGED & WAS SUCKED INTO THE INTAKE OF THE ENG CAUSING PARTIAL POWER LOSS.SDR CA150505003Magneto · out of adjust(CAN) MAGNETO TIMING OUT BY 5 DEGREES ONLY 101.5 HRS AFTER 500 HR INSPECTION.SDR CA150417007Starter · failed(CAN) BETWEEN 2014-06-20 TO 2014-12-16 STARTER WAS CHANGED 5 TIMES, 2 OF THE TIMES IT WAS A LOADER STARTER AFTER THE O/H STARTER DID NOT WORK PROPERLY. THE STARTER USED WAS PN MZ 4222.SDR CA150316009Points · failed(CAN) MAGNETO POINTS FAILED TO OPEN DURING ROUTINE TIMING CHECK AT 253 HRS SINCE 500HR INSPECTION.SDR CA150202013Attach Fitting · cracked(CAN) ON ROUTINE SCHEDULED MAINTENANCE INSPECTION IT WAS FOUND ON RUN-UP THAT THE VACUUM INDICATOR WAS FLUXUATING BACK AND FORTH. ON FURTHER INSPECTION IT WAS FOUND THAT THE PLASTIC FITTING ATTACHED TO THE BACK OF THE GAUGE HAD CRACKED. GAUGE WAS REPLACED WITHSDR CA141029011Chain · disconnected(CAN) AN ACCEPTANCE INSPECTION OF OUTSIDE CONTRACT WORK, WAS PERFORMED ON THIS AIRCRAFT, AFTER WORK WAS PERFORMED ON THE HORIZONTAL STAB. IT WAS FOUND THAT THE ELEVATOR TRIM CHAIN WAS NOT CONNECTED TO THE SPROCKET AT THE PILOTS TRIM HAND WHEEL. THE TRIM MOVED SDR CA140910010Cylinder Head · damaged(CAN) SEPTEMBER 8, 2014, PILOT REPORTS THAT ENGINE RAN ROUGH IN DOWNWIND OF FIRST CIRCUIT. MAGS FUNCTIONED NORMALLY. NO DIFFERENCE WITH CARB HEAT. ENGINE WAS POPPING ON TAXI BACK IN. ABNORMAL ENGINE NOISE OBSERVED BY MAINTENANCE PERSONEL WHILE AIRCRAFT TAXIEDSDR CA140829005Magneto · malfunctioned(CAN) MAGNETO MISFIRING AND CAUSING HARD STARTING.SDR CA140904004Carburetor · out of adjust(CAN) IDLE MIXTURE ADJUSTMENTS MADE NO CHANGE TO IDLE MIXTURE SETTING ON CARBURETOR.SDR CA140827008Lifter · damaged(CAN) A/C WAS FLYING FOR 10 MINUTES WHERE THE ENGINE STARTED TO RUN ROUGH. PILOT CHECKED MAGS AND CARB HEAT (NO CHANGE). PILOT DECIDED TO MAKE PRECAUTIONARY LANDING OUTSIDE OF CITY LIMITS ON PRIVATE ROAD INSTEAD OF FLYING OVER CITY. MAINTENANCE WAS SENT TO HAVSDR 2014FA0000418Cable · failedFLAP FAILURE OCCURRED WHILE PRACTICING POWER OFF STALLS. LT FLAP FAILED TO RETRACT DUE TO THE FLAP CABLE SWAGED BALL PULLED THROUGH THE FLAP DRIVE PULLEY GROOVE. THE LOAD BEARING WASHER WAS NOT POSITIONED BETWEEN THE SWAGGED BALL ON THE END OF THE CABLE AND SDR 2014FA0000262Tube · puncturedPIN HOLE IN SIDE OF INNER TUBE, NOSE GEAR.SDR CA140325005Tube · failed(CAN) ACFT EXPERIENCED A FLAT TIRE ON TAXING FOR RUN-UP. INSPECTION FOUND SMALL HOLE IN TUBE, BUT TIRE SHOWED NO DEFECT OR DEBRIS THAT COULD HAVE CAUSED HOLE.SDR CA140312008Selector Valve · malfunctionedORIGINAL EQUIPMENT SHOWS LARGE DEVIATIONS IN ACCURACY OF THE FUEL VALVE SELECTOR. WHEN INCORRECTLY POSITIONED, EG BETWEEN BOTH AND LT ENGINE WILL OPERATE AT LOWER RPM. FULL POWER APPLICATION SEES A DEGRADATION OF AVAILABLE POWER 20-30 SECS AFTER ADVANCE OF THSDR CA140225020Magneto · out of adjust(CAN) RIGHT MAGNETO TIMING FOUND TO BE OUT 4 DEGREES AFTER ONLY 26 HRS SINCE NEW.SDR CA140225019Magneto · out of adjust(CAN) LEFT MAGNETO TIMING FOUND TO BE OUT 4 DEGREES AFTER ONLY 26 HRS SINCE NEW.SDR CA140127007Magneto · out of adjust(CAN) MAG TIMING FOUND TO BE OUT 6 DEGREES AFTER ONLY 77 HRS OPERATION SINCE NEW.SDR CA140127006Magneto · out of adjust(CAN) MAGNETO TIMING FOUND TO BE OUT 5 DEGREES AFTER ONLY 77 HRS OPERATION SINCE NEW.SDR CA140124010Magneto · out of adjust(CAN) MAG TIMING FOUND TO BE OUT 4 DEGREES ONLY 50HRS AFTER 500 HR INSPECTION.SDR CA140124009Magneto · out of adjust(CAN) MAG TIMING FOUND TO BE OUT 3 DEGREES ONLY 50HRS AFTER 500HR INSPECTION.SDR CA140124012Magneto · out of adjust(CAN) MAGNETO TIMING FOUND TO BE OUT 5 DEGREES, ONLY 100 HRS AFTER 500 HR INSPECTION.SDR CA140124011Magneto · malfunctioned(CAN) MAGNETO TIMING FOUND TO BE OUT 5 DEGREES ONLY 100 HRS AFTER 500 HR INSPECTION.SDR YAAA20140109001Crankcase · crackedFOUND ENG LT CRANKCASE ASSEMBLY CRACKED DURING MAINTENANCE PRE-FLIGHT. REMOVED ENG & SENT CRANKCASE ASSEMBLY REPLACEMENT.SDR OW6A201312130001Cylinder · damagedNR 4 CYLINDER HEAD SEPARATED FROM BARREL DURING NORMAL OPERATION. AD2009-26-12 WAS COMPLIED WITH 24.5 HRS PRIOR WITH NO INDICATIONS STATED IN AD THAT WOULD INDICATE CYLINDER WOULD FAIL.SDR CA131023008Collar · cracked(CAN) NOSEGEAR STEERING COLLAR DISCOVERED CRACKED DURING SCHEDULED INSPECTION. CRACK THROUGH MAIN COLLAR AT FORWARD GREASE FITTING. SUSPECT OVER STEERING BY GROUND TUG.SDR 2013FA0000718Brake Assy · draggingBRAKE CALIPER DRAGGING.
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