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 = 'U206G' 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 = 'U206G' 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 2013FA0000383Thru Bolt · looseWHILE IN THE PROCESS OF REMOVING AND REPLACING A ENGINE OIL TEMP PROBE, MECHANIC DISCOVERED ONE OF THE ENGINE CASE THROUGH BOLTS WAS MISSING NUTS AND WASHERS ON BOTH SIDES OF THE CASE. THE WASHER FOR THE RT SIDE OF THE BOLT WAS FOUND IN THE BOTTOM OF THE COWLSDR CA130722013Cylinder · cracked(CAN) ON A ROUTINE INSPECTION IT WAS FOUND THAT THE NR 5 CYLINDER HAD DEVELOPED A CRACK BETWEEN THE BARREL AND HEAD. THE SUPERIOR CYLINDER WAS R & R WITH A GENUINE CONTINENTAL CYLINDER. THE SYSTEM WAS GROUND FUNCTION CHECKED SERVICEABLE.SDR CA130722011Drive Assy · cracked(CAN) DURING A MAINTENANCE EVENT, CHANGING THE ENGINE DRIVEN FUEL PUMP, IT WAS DISCOVERED THAT THE ENGINE STARTER DRIVE WAS CRACKED, ONCE REMOVED IT WAS DISCOVERED THE STARTER DRIVE WAS MUCH WORN. THE STARTER DRIVE WAS REPLACED WITH NEW AND THE SYS FUNCTION CSDR CA130722010Pump · low pressure(CAN) ON AN INSPECTION PRE-RUN UP IT WAS FOUND BY MAINTENANCE THAT THE FUEL PRESSURE WAS ON THE LOW SIDE OF THE GREEN BUT NOT IN THE STANDARD RANGE. FURTHER INSPECTION REVEALED A WORN ENGINE DRIVEN FUEL PUMP, THE FUEL PUMP WAS R & R WITH AN O/H UNIT AND THE SDR 2013FA0000448Gasket · splitDURING EXTENDED FLIGHT, LOSS OF OIL PRESSURE OCCURED AND LEAD TO TOTAL ENGINE FAILURE. GASKET FOR OIL FILTER ADAPTER TO ENGINE FAILED. ON REMOVAL, NOTED THE GASKET HAD SPLIT AND WAS OFF TO ONE SIDE OF THE ADAPTER.SDR CA130513019Tire · fod(CAN) PILOT NOTED THE LT TIRE HAD GONE FLAT, SHUT THE ACFT DOWN ON THE RUNWAY. CHANGED THE TIRE. THE WHEEL ASSY WAS REPLACED. THE CAUSE OF THE FLAT TIRE WAS FOD DAMAGE, SINCE THE ACFT HAD SEVERAL TURN AROUND THAT DAY IT IS INCONCLUSIVE TO WHERE THE FOD WAS SDR 2013FA0000232Bulkhead · crackedDURING ANNUAL INSPECTION. AFTER REMOVING FLOAT BUMPERS OFF OF BOTH FLOATS, TWO LARGE CRACKS WERE FOUND ON EACH BULKHEAD NOSE ASSY . THE CRACKS STARTED FROM THE BOTTOM NUT PLATES AND WERE ABOUT THREE INCHES IN LENGTH.SDR ENEA2012F00235Crankcase · puncturedON SHORT FINAL, PILOT HEARD AN AUDIBLE BANG WITH ENGINE RUNNING SLIGHTLY ROUGH, MAKING A DIFFERENT NOISE AND NOT DEVELOPING FULL POWER. CONTINUED TO LANDING WITH OUT INCIDENT AND DURING TAXI TO TURN OUT STARTED ACCUMULATING OIL ON WINDSCREEN. REMOVED TOP COWSDR CA121024012Switch · faulted(CAN) ON SHUTDOWN, THE PILOT CONDUCTED A LIVE MAG CHECK AND FOUND THE MAGS WHERE BOTH LIVE. THE SWITCH WAS FOUND FAULTY AND WAS REPLACED.SDR CA121024011Tire · failed(CAN) THE ACFT CONDUCTED A BACK TRACK TAXI OUT TO THE RUNWAY, TURNED VERY SHARP USING BRAKES TO PIVOT THE WHEEL AND SHEARED THE VALVE STEM ON THE TUBE CAUSING THE TIRE TO DEFLATE AND RESULTING IN THE ACFT TO BE STUCK ON THE RUNWAY FOR APPROXIMATELY 30 MINUTESDR ERHA2012F00161G Switch · inoperativeELT G SWITCH WILL NOT ACTIVATE DURING TESTING.SDR CA120726012Alternator · damaged(CAN) DURING A ROUTINE FLIGHT, THE PILOT NOTED A LOW VOLTAGE LIGHT FOLLOWED BY A DISCHARGE RESULTING IN A TOTAL LOSS OF POWER. MAINTENANCE DISCOVERED THE ALTERNATOR CASE HALF BOLTS SHEARED AS A RESULT OF AN INTERNAL BEARING FAILURE. MAINTENANCE REPLACED THE ASDR 2012F00138Engine · power lossAIRCRAFT DEPARTED FOR A 2 HOUR FLIGHT. THE PILOT NOTICED FLUCTUATION IN OIL PRESSURE AND REMAINED AT 8000 FT AGL UNTIL OVER THE AIRPORT. WHILE CIRCLING TO LAND, THE ENGINE FAILED TO PRODUCE POWER. PILOT LANDED SAFELY WITHOUT POWER ON THE AIRFIELD.SDR CA120709012Indicator · stuck(CAN) ON ROTATION, THE AIRSPEED INDICATOR BECAME STUCK. THE PILOT ELECTED TO JOIN THE CIRCUIT AND LAND BACK AT EZ4. THE LANDING WAS UNEVENTFUL. MAINTENANCE DISCOVERED THAT AN INSECT WAS STUCK IN THE PITOT TUBE, THE SYS WAS SERVICED AND GROUND FUNCTION CHECSDR CA120620009Cylinder · leaking(CAN) ROCKER COVERS FOUND LEAKING. DISCOVERED THAT RELIEF CUT IN ROCKER COVER FACE ON ALL 6 NEW SUPERIOR CYLINDERS WAS CUT TOO DEEP & LEFT LITTLE AREA FOR GASKET TO SEAL. SOLUTION WAS TO INSTALL ORANGE SILICONE GASKETS, SO FAR SO GOOD.SDR CA120529005Indicator · reads high(CAN) FUEL PRESSURE SIDE OF GAUGE STICKS AT THE HIGHER SETTINGS TAPPING ON GAUGE BRINGS IT BACK TO NORMAL READINGS.SDR CA120604011Switch · inoperative(CAN) AFTER LANDING THE PILOT REPORTED THE FLAPS WOULD NOT RETRACT. MAINTENANCE FOUND A FAILED UP LIMIT SWITH ON THE FLAP ACCUATOR, THE SWITCH WAS REPLACED WITH NEW AND GROUND FUNCTION CHECKED SERVICABLE.SDR CA120604006Indicator · inoperative(CAN) ON A FLIGHT, THE PILOT DISCOVED THE TURN & BANK BECAME UNSERVICEABLE, THE ACFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE DISCOVERED THE CONNECTOR PLUG ON THE TURN & BANK INDICATOR HAD COME LOOSE, THE CONNECTOR PLUG WAS REINSTALLED AND FUNCTION SERVISDR CA120522013Bushing · swollen(CAN) ENGINE WAS BEING DISMANTLED FOR AN UNRELATED PROBLEM WHEN IT WAS DISCOVERED THAT THE MAGNETO RUBBER DRIVE BUSHINGS WERE SWOLLEN AND CAUSING THE MAGNETO DRIVE GEAR TO WEAR INTO THE ADAPTER ASSY. THERE WAS A LOT OF BRASS MISSING FROM THIS WEAR. SUPERIOR SDR CA120604005Switch · failed(CAN) ON A FLIGHT, UPON ENTERING THE CONTROL ZONE, THE PILOT HAD NO JOY CONTACTING FSS ON COMM NR 2. THE PILOT SELECTED COMM NR 1 AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE DISCOVERED THE PILOT, PUSH TO TALK, BUTTON WAS UNSERVICEABLE, THE SWITCH WAS REPSDR CA120514005Bearing · damaged(CAN) NR 3 CYLINDER WAS REMOVED DUE TO LOW COMPRESSION. WHILE THE CYLINDER WAS REMOVED IT WAS NOTED THAT THE MAIN CRANK BEARING, PN 653547. JUST AFT OF NR 3 CYLINDER WAS FOUND OUT OF POSITION SHUFFLED FORWARD APPROXIMATELY .1250" AND RUBBING ON THE CRANK CHESDR CA120510002Alternator · leaking(CAN) A CREWMAN REPORTED A SMALL OIL LEAK FROM THE FRONT OF THE ENGINE AFTER HIS POST FLIGHT INSPECTION. THE CAUSE WAS A BROKEN MOUNT LUG ON THE ALTERNATOR, 1 OF THE 4, USED TO BOLT THE ALTERNATOR TO THE ENGINE. THE REASON FOR THE BREAKAGE IS UNDETERMINED.SDR CA120503001Shaft · bent(CAN) DURING INTERNAL, 500 HR INSPECTION OF THE ALTERNATOR THE MAIN SHAFT WAS FOUND TO BE BENT AND THE CASE HALF HAD A SMALL CRACK. ALTERNATOR WAS R & R WITH AN O/H SPARE.SDR O592011F00003Cylinder · crackedDIR OMG 50 HR INSPECTION AND COMPRESSION CHECK, FOUND NR 3 CYLINDER LOW 56/80. AFTER REMOVAL, FOUND TO BE CRACKED BETWEEN SPARK PLUG HOLE AND INTAKE VALVE. THIS IS 1 OF SEVERAL FOUND TO BE CRACKED.SDR CA110919005Starter · failed(CAN) AFTER A WARM UP ENGINE SHUTDOWN. ON THE WARM START ATTEMPT,THE ENGINE "KICKED BACK", BREAKING THE SPRING INSIDE THE STARER DRIVE ASSY. STARTER DRIVE ASSY REPLACED WITH A SERVICEABLE UNIT AND ACFT RETURNED TO SERVICE.SDR CA110805005Bearing · separatedMAG WAS RECEIVED FOR REPAIR AFTER 123.1 HRS IN SERVICE. THE DISTRIBUTOR BLOCK BEARING HAD SEPARATED FROM THE PLASTIC DISTRIBUTOR BLOCK AND THE NYLON DISTRIBUTOR GEAR HAD COCKED WITH THE BEARING. THIS CAUSED WEAR ON THE TEETH AND THE ELECTRODE HAD STARTED TO MSDR CA110603005Engine · seizedIN CRUISE FLIGHT, PILOT HEARD A LOUD KNOCKING SOUND FROM ENGINE. ENGINE LOST ALL POWER. PILOT DECLARED AN EMERGENCY AND CARRIED OUT AN UNSCHEDULED LANDING. NO DAMAGE TO ACFT, PILOT WAS NOT INJURED. AT THIS TIME ALL WE KNOW IS THAT THE ENGINE IS SIEZED AND WISDR PNB2011F00004Cylinder · crackedDURING A 100 HR INSP, DISCOVERED BLOWBY BETWEEN FINS ON THE INTAKE SIDE OF THE CYLINDER. THE CYLINDER WAS REMOVED AND FOUND TO BE CRACKED BETWEEN THE INTAKE VALVE SEAT AND THE SPARK PLUG HOLE. THIS IS THE 5TH CYLINDER THIS YEAR WITH ALMOST IDENTICAL CRACKS.SDR PNB2011F00003Cylinder · crackedDURING A 100HR INSPECTION, DISCOVERED BLOWBY BETWEEN FINS ON THE INTAKE SIDE OF THE CYLINDER. THE CYLINDER WAS REMOVED AND FOUND TO BE CRACKED BETWEEN THE INTAKE VALVE SEAT AND THE SPARK PLUG HOLE. THIS IS THE 6TH CYLINDER THIS YEAR WITH ALMOST IDENTICAL CRASDR PNB2011F00005Cylinder · crackedLOW COMPRESSION NR2 CYLINDER ON 100HR INSPECTION. FOUND BLOWBY COMING AROUND FINS IN THE HEAD. CYLINDER WAS CRACKED BETWEEN SPARK PLUG HOLE AND INTAKE VALVE. ALL PREVIOUS COMPRESSION CHECKS WERE IN THE 70/60 RANGE.SDR PNB2011F00000Cylinder · crackedFOUND NR 1 CYLINDER CRACKED BETWEEN SPARK PLUG HOLE AND THE INTAKE VALVE. THIS IS THE 3RD CYLINDER FOUND WITH THIS SIMILAR CRACK. (END)SDR O592011F00002Cylinder Head · crackedNR 1 CYLINDER WAS FOUND CRACKED BETWEEN SPARK PLUG HOLE AND INTAKE VALVE. THIS IS THE 3RD CYLINDER WITH SIMILAR CRACK.SDR O592011F00000Cylinder · crackedLOW COMPRESSION NR2 CYLINDER ON 100 HR INSPECTION. FOUND BLOW-BY COMING AROUND FINS IN THE HEAD. CYLINDER WAS CRACKED BETWEEN SPARK PLUG HOLE AND INTAKE VALVE. ALL PREVIOUS COMPRESSION CHECKS WERE IN THE 70/60 RANGE.SDR 2011FA0000278Points · crackedACFT WAS DISCOVERED TO HAVE AN INOPERATIVE LT MAGNETO DURING A PILOT OPERATED ENG RUN. TROUBLESHOOTING FOUND THE FLAT SPRING PORTION OF THE CONTACT POINT ASSY HAD CRACKED THROUGH APPROX HALFWAY ALONG THE LENGTH OF THE SPRING AND ACROSS ITS ENTIRE WIDTH. THE SDR CA110330003Alternator · inoperative(CAN) NO OUTPUT FROM ALTERNATOR. ALTERNATOR REPLACED.SDR 2011FA0000174Plug · failedTHE ENGINE WAS REMOVED FROM THE ACFT AT ENG TT 2157.4 (AIRFRAME TT 4652.7) FOR REPAIR DUE TO LOW OIL PRESSURE. THE CRANKSHAFT PN 64134, SN 109903N WAS SENT TO MFG FOR ULTRASONIC INSP, BALANCE, POLISHED AND RECERTIFIED. THE CRANKSHAFT WAS RETURNED BY MFG AS SSDR CA110214023Elt · false activationA REOCCURANCE TO THE SAME REPORT ON SDR 20110204008. THE ELT AGAIN INADVERTENTLY ACTIVATED IN FLIGHT. THE REASON FOR THE ACTIVATION WAS POOR WIRING AT THE REMOTE SWITCH IN THE COCKPIT. THE POOR WIRING WAS A RESULT OF POOR STANDARDS USED DURING INSTALLATION. SSDR CA110204008Remote Switch · loose(CAN) ELT ACTIVATED ON ITS OWN IN FLIGHT. SUSPECTED LOOSE REMOTE SWITCH CONNECTION WAS LOOSE AT THE ELT CAUSING UNCOMMANDED ACTIVATION. TRENTON ADVISED OPERATIONS OF ELT SIGNAL FROM THIS AIRCRAFT.SDR CA101213007Mount · damaged(CAN) DURING UNSCHEDULED MAINTENANCE INSPECTION, IT WAS NOTED THAT THE ENGINE MOUNT BULKHEADS WERE WORKING. THE ENGINE MOUNTS WERE REMOVED AND IT WAS OBSERVED THAT BOTH THE LH AND RH KEEL BULKHEAD SKINS WERE SHATTERED FROM YEARS OF WORK HARDENING. THERE IS CSDR HYT2010F00001Clutch Spring · brokenHAVE HAD A CHRONIC PROBLEM WITH BREAKAGE OF STARTER CLUTCH SPRING PN 643109 WHICH IS A COMPONENT OF STARTER ADAPTER PN 643259A. THERE HAVE BEEN 9 FAILURES OF THIS SPRING IN 1592 HRS OF OPERATION. AVERAGE TIS HAS BEEN 173 HRS, WORST TIS 18 HRS, BEST TIS 422 HSDR 2010FA0001042Flap System · malfunctionedDURING A TRAINING FLIGHT, AT ABOUT 2000 FT FLAPS DID NOT RETRACT FROM FULL FLAP EXTENSION DURING RECOVERY FROM AN IMMINENT FULL-FLAP, POWER OFF STALL. SEVERAL UNSUCCESSFUL ATTEMPTS WERE MADE TO RETRACT THE FLAPS, THE FLAP CIRCUIT BREAKER HAD NOT TRIPPED AND THSDR ENE2010F00000Bearing · seizedACFT ENGINE STARTED RUNNING ROUGH IN CRUISE FLIGHT. PILOT MADE A PRECAUTIONARY BEACH LANDING. TROUBLESHOT, FOUND LT MAG TO BE INOPERATIVE. REMOVED MAG TO BE SEIZED. DISASSEMBLED MAG AND FOUND LOWER BEARING PN M3006 TO BE SEIZED. MAGNETOS WERE APPROX 58 HRSDR CA100902003Cylinder · crackedWHILE DOING COMPRESSION TEST ON INSP, FOUND 3 CYL WITH CRACKS FROM INTAKE VALVE TO SPARKPLUG HOLE.SDR CA100827003Control Cable · deteriorated(CAN) PILOT REPORTED NO WATER RUDDER STEERING. FOUND WATER RUDDER BALANCE CABLE BROKEN. ENTIRE CABLE FOUND SEVERELY RUSTED TO THE POINT OF FAILURE. ALSO FOUND CABLE GUARD/COTTER PINS SEVERELY RUSTED IN THE SAME AREA.SDR CA100825001Engine · failedIN FLIGHT, PILOT NOTICED OIL PRESSURE INDICATING ZERO, NOT POSITIVE EXACTLY HOW LONG IT HAD BEEN AT ZERO, APPROX 5 MINUTES SINCE HE SCANNED GAUGES LAST, OIL TEMP NORMAL, SHORTLY AFTER NOTICING, THE PROP STARTED SURGING, OIL TEMP STILL SEEMED NORMAL, MANIFOLD PSDR CA100616005Case Half · looseDURING A 50 HR INSP, THE ALTERNATOR CASE HALVES WERE FOUND LOOSE. THE THROUGH BOLT LOCKWIRE WAS STILL INTACT. ALTERNATOR TT SINCE O/H WAS 99.7 HRS. THE ALTERNATOR WAS REMOVED AND INSPECTED. NO FURTHER DEFECTS WERE FOUND. THROUGH BOLTS WERE RETIGHTENED ANDSDR CA100521006B-Nut · loose(CAN) AIRCRAFT ENGINE WAS REMOVED, OVERHAULED, AND REINSTALLED. ALL FIREWALL FORWARD HOSES WERE REPLACED IN ACCORDANCE WITH CUSTOMERS MSA. ENGINE GROUND RUNS, FUEL SYSTEM SETUP AND LEAK CHECKS WERE CARRIED OUT. NO EVIDENCE OF LEAKS WERE DETECTED. AFTER 48.SDR 2010FA0000595Bolt · wornDURING A 100 HR INSP, FOUND NOSE GEAR HAD FORE AND AFT MOVEMENT WHERE THERE SHOULD BE NONE. REMOVED AFT DRAG LINK BOLT TO INVESTIGATE AND FOUND IT TO BE WORN AND DEFORMED AS IF GETTING READY TO SHEAR. THIS IS THE THIRD OR FOURTH FOUND. THE OTHER ACFT THAT SDR 2010FA0000473Wire · overheatedAUTOPILOT DISABLED IAW FAR 91.213. FOUND WIRES FROM CIRCUIT BREAKER TO AUTOPILOT OVERHEATED. IT IS BELIEVED THAT THE PILOTS CUT THE PLASTIC TIE WRAP ON THE CIRCUIT BREAKER AND USED THE AUTOPILOT ANYWAY. THE AUTOPILOT FUNCTIONS ON MANUAL HEADING ONLY. RECOMMSDR 2010FA0000248Lifter · spalledLOW COMPRESSION NR 5 CYLINDER - BURNED VALVE. FOUND BOTH LIFTERS FOR INTAKE AND EXHAUST SPALLED. LOOKED AT OTHER LIFTERS IN ENGINE WITH A BORESCOPE AND FOUND SEVERAL OTHER LIFTERS IN ENGINE WITH SAME SPALLING DEFECT. PN ON LIFTERS IS 653888 AND 653877. THE
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