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 = 'T207' 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 = 'T207' 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 2020F00280Lifter · spalledREMOVED ALL HYDRAULIC LIFTERS TO INSPECT FOR SPALLING, DISCOVERED BADLY SPALLED EXHAUST LIFTER ON CYLINDER #4. INSPECTED CAM IN ACCORDANCE WITH CONTINENTAL SERVICE DIRECTIVE SID05-1B, INSTALLED NEW LIFTER AND WILL INSPECT CAM AGAIN IN 100 HOURS. IT IS DOUBTFSDR OW6A202001220062Brake Caliper · leakingLEFT BRAKE FAILED, IT HAD WORKED FINE DURING RUN-UP. PILOT TOOK OFF AND THEN FOUND IT INOPERATIVE ON LANDING. LANDING WAS UNEVENTFUL.SDR YAAA20150428005Cylinder Head · crackedDURING 100 HR INSPECTION BORESCOPED ENG & FOUND NR 6 CYLINDER CRACKED FROM LOWER SPARK PLUG BOSS TOWARDS EXHAUST VLV SEAT.SDR YAAA20150428004Cylinder Head · crackedDURING 100 HR INSPECTION BORESCOPED ENG & FOUND NR 5 CYLINDER CRACKED FROM LOWER SPARK PLUG BOSS TOWARDS EXHAUST VLV SEAT.SDR YAAA20150428003Cylinder Head · crackedDURING 100 HR INSPECTION BORESCOPED ENG & FOUND NR 4 CYLINDER CRACKED FROM LOWER SPARK PLUG BOSS TOWARDS EXHAUST VLV SEAT.SDR YAAA20150428002Cylinder Head · crackedDURING 100 HR INSPECTION BORESCOPED ENG & FOUND NR 3 CYLINDER CRACKED FROM LOWER SPARK PLUG BOSS TOWARDS EXHAUST VLV SEAT.SDR YAAA20150428001Cylinder Head · crackedDURING 100 HR INSPECTION BORESCOPED ENG & FOUND NR 2 CYLINDER CRACKED FROM LOWER SPARK PLUG BOSS TOWARDS EXHAUST VLV SEAT.SDR CKE2013F00001Bushing · looseFUEL INJECTOR BUSHINGS DID NOT STAY IN PLACE WHEN FUEL INJECTORS WERE REMOVED. INJECTORS WERE REMOVED FOR CLEANING. THIS ENGINE HAS 11TSMOH AND 4 OUT OF THE 6 BUSHINGS LOOSENED WITH THE INJECTOR. PROBABLE CAUSE IS THAT THE LOCTITE 620 DOES NOT HOLD THE BUSHSDR YAA2010F00000Unknown · odorDEPARTED NORTH BOUND. EXPERIENCED A BURNING SCENT IN CABIN IN FLIGHT AND LATER CLAIMED TO SEE SMOKE EMITTING FROM ENGINE INSTRUMENT CLUSTER. PILOT THEN DIVERTED AND LANDED. FOLLOWING MORNING ACFT`S INSTRUMENT CLUSTER (WHERE THE PILOT CLAIMED TO SEE SMOKE),SDR 2005FA0001065Antenna · inoperativeFOUND UPPER UAT ANTENNA UNSERVICEABLE. (K)SDR 2005FA0001054Antenna · inoperativeFOUND UPPER UAT ANTENNA UNSERVICEABLE. (K)SDR FMA2004F00000Contactor · defectivePILOT REPORTED MISFIRE DURING MAG CHECK. TROUBLESHOOTING REVEALED RIVETING OF GROUND SIDE OF CONTACT TO MOUNTING BASE HAD FAILED ALLOWING ELECTRICAL CONTACT TO RATTLE IN BASE.SDR FMAA2002002Switch · inoperativeFLAP SWITCH IS HELD TO THE ARM ASSEMBLY WITH SMALL NR 40 MACHINE SCREWS. IF SCREWS ARE OVER TIGHTENED, THE PLASTIC SWITCH CRACKS, IF IT IS NOT TIGHTENED ENOUGH, IT LOOSENS WHICH CHANGES THE ADJUSTMENT OF THE FLAPS. THE SWITCH WIRES OBVIOUSLY LOOSENED ENOUGH SDR VDQ2001F00005Cylinder · crackedALL 6 CYLINDERS CRACKED AT 781.6 HOURS SINCE NEW. SERIAL NUMBERS: 52A0016149, 52A0016150, 52A0016201, 52A0016202, 52A0016215, 52A0016217.SDR VDQ2001F00004Cylinder · crackedALL 6 CYLINDERS CRACKED AT 781.6 HOURS SINCE NEW. SERIAL NUMBERS: 52A0016149, 52A0016150, 52A0016201, 52A0016202, 52A0016215, 52A0016217.SDR VDQ2001F00003Cylinder · crackedALL 6 CYLINDERS CRACKED AT 781.6 HOURS SINCE NEW. SERIAL NUMBERS: 52A0016149, 52A0016150, 52A0016201, 52A0016202, 52A0016215, 52A0016217.SDR VDQ2001F00002Cylinder · crackedALL 6 CYLINDER CRACKED AT 781.6 HOURS SINCE NEW. SERIAL NUMBERS: 52A0016149, 52A0016150, 52A0016201, 52A0016202, 52A0016215, 52A0016217.SDR VDQ2001F00001Cylinder · crackedALL 6 CYLINDERS CRACKED AT 781.6 HOURS SINCE NEW. SERIAL NUMBERS: 52A0016149, 52A0016150, 52A0016201, 52A0016202, 52A0016215, 52A0016217.SDR VDQ2001F00000Cylinder · crackedALL 6 CYLINDER CRACKED AT 781.6 HOURS SINCE NEW. SERIAL NUMBERS: 52A0016149, 52A0016150, 52A0016201, 52A0016202, 52A0016215, 52A0016217SDR HUK2001F00001Indicator · shortedOIL TEMPERATURE GAUGE SUPPLIED WITH SERVICE KIT-OIL GAUGE SHORTED OUT INTERNALLY BLOWING OUT POWER CONVERTER. THIS WAS THE 3RD GAUGE IN 4 YEARS. WHEN POWER CONVERTER BLEW POWER SURGE/SHORT CREATED MALFUNCTION IN ENGINE INSTRUMENT CLUSTER AND CREATING BURNINGSDR HUK2001F00000Gauge · damagedOIL TEMPERATURE GUAGE (ROCHESTER SERVICE KIT) FAILED CAUSEING OVER VOLTAGE PROBLEM THROUGH-OUT. SHORTING OUT ALTERNATOR, VOLTAGE REGULATOR, OVER VOLTAGE SENSOR, ENTIRE RADIO STACK, LIGHTING, ELECTRIC SERVICE KIT OIL TEMP WAS REMOVED AND REPLACED WITH ORIGINALSDR 20001101SH005Magneto · defectiveON INITIAL POWER-UP FOR THE FLIGHT''S TAKEOFF ROLL, THE ENGINE LOST SUBSTANTIAL POWER. THE PILOT ROLLED OFF TO A TAXIWAY AND SHUT DOWN. AFTER TROUBLESHOOTING THE IGNITION SYSTEM, THE RIGHT MAGNETO WAS FOUND DEFECTIVE AND REPLACED WITH NEW. RUN-UP SATISFACTOSDR 97ZZZX276Bulkhead · crackedDURING C/W OF AD 72 07-09, FOUND 4 CRACKS IN BULKHEAD P/N 1212859-1 AND 3 CRACKS IN BULKHEAD P/N 1212409-6. THE REST OF THE FIN STRUCTURE WAS DYE CHCKED AND INSPECTED AND NO FURTHER CRACKS WERE FOUND. ONE FORWARD VERTICAL FIN BOLT HAD SHOWN SIGNS OF LOOSENINSDR 97ZZZX275Bulkhead · crackedDURING C/W OF AD 72 07-09, FOUND 4 CRACKS IN BULKHEAD P/N 1212859-1 AND 3 CRACKS IN BULKHEAD P/N 1212409-6. THE REST OF THE FIN STRUCTURE WAS DYE CHCKED AND INSPECTED AND NO FURTHER CRACKS WERE FOUND. ONE FORWARD VERTICAL FIN BOLT HAD SHOWN SIGNS OF LOOSENINSDR 97ZZZX191Bulkhead · crackedINSPECTION FOUND 3 CRACKS IN BULKHEAD AND 4 IN BULKHEAD DOUBLER. INSPECTION AND REPLACEMENT OF PARTS DONE IAW AD 72-07-09 AND CESSNA SE 72-3 AND SE 72-29.SDR 95ZZZX7019Clamp · brokenPRE-FLIGHT REVEALED LOOSE TAILPIPE. FOUND CLAMP BROKEN. CLAMP APPEARED TO BE HIGH-TIME, BUT ENGINE WAS INSTALLED LESS THAN 50 HOURS EARLIER. SUBMITTER RECOMMENDS CLAMP BE CHANGED EVERY ENGINE CHANGE AND BE TORQUED PROPERLY.SDR 95ZZZX6450Cylinder · departedNR 6 CYLINDER DEPARTED THE CASE. ALL THE CYLINDER BASE STUDS WERE BROKEN.SDR 95ZZZX6175Cylinder · crackedROUGHLY 15 MINUTES INTO FLIGHT, THE ENGINE LOST MANIFOLD PRESSURE. MAXIMUM M/P WAS 25 INCHES. INSPECTION FOUND THE NR 4 CYLINDER CRACKED AND STARTING TO MELT THE NR 6 CYLINDER.SDR 95ZZZX6743Cylinder · crackedINSPECTION FOUND CYLINDER HEAD WAS SUBSTANTIALLY CRACKED FROM BOTTOM SPARK PLUG HOLE TO TOP SPARK PLUG HOLE THROUGH THE EXHAUST PORT. SUBMITTER STATED THIS IS THE FIFTH (OUT OF SIX) THAT HAVE HAD TO BE REPLACED SINCE ENGINE OVERHAUL (1,339 HOURS AGO) DUE TO HSDR 95ZZZX1306Mount Arm · failedFOUND TURBOCHARGER MOUNT EAR CRACKED IN TWO PIECES. SUBMITTER SUSPECTS THE MOUNTING ARMS WERE IMPROPERLY INSTALLED AND HARDWARE WAS OVERTORQUED. SUBMITTER SUGGESTS MECHANICS MUST TAKE EXTRA CARE TO INSURE PROPER ALIGNMENT OF MOUNTS TO PRECLUDE THIS TYPE OF F
Back to Cessna T207