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 = 'TBM700' 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 = 'TBM700' 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 2023FA0000290Starter Gen · failedSTARTER/GEN FAILURE IN FLIGHT FORCING PILOT TO DECLARE EMERGENCY LANDING. UPON INSPECTION, STARTER BEARING FOUND THROUGHOUT STARTER HOUSING, ALONG WITH STATOR WINDINGS AND OTHER FOD MATERIAL. SPLINED SHAFT WAS ALSO SHEARED.SDR DGCA 23 3100Elevator · delaminatedELEVATOR LEADING EDGE DELAMINATIONSDR 2020FA0000379Pump · bypassingLANDING GEAR PUMP FAILURE. GEAR WOULD NOT GO DOWN. USED EMERGENCY HAND PUMP TO EXTEND THE GEAR.SDR 2019FA0000129Control Rod · detachedTHE RUDDER TRIM TAB IS OPERATED BY AN ELECTRIC ACTUATOR AND CONNECTED BY A LOWER AND AN UPPER RUDDER TRIM TAB CONTROL ROD. AFTER RUDDER REMOVAL FOR ROUTINE INSPECTION, THE UPPER RUDDER TRIM CONTROL ROD DETACHED FROM THE ACTUATOR WHILE THE BEARING WAS STILL IN SDR V94R2019022831002Roll Pin · backed outROLL PIN THAT HOLDS PINION GEAR ON SERVO DRIVESHAFT WORKED ITS WAY OUT SO THAT THE GEAR SLIPPED ON THE SHAFT AND THE SERVO WAS MECHANICALLY DISCONNECTED FROM THE FLIGHT CONTROLS. THE SYSTEM DID NOT PROVIDE ANY WARNING OF THIS FAILURE. IT IS ALSO LIKELY THAT SDR 2018FA0000133Generator · power lossPILOT DIVERTED TO PMP DUE TO LOST POWER FROM MAIN GENERATOR.SDR URZR20170117001Wire · not reportedTHE PILOT CHANGED SWITCH POSITION FROM AUTO TO MAX DIFF AND EXPERIENCED LOSS OF BLEED AIR. PILOT WAS ALERTED BY A BLEED OFF MESSAGE, CABIN PRESSURE BEGAN TO DECREASE. INITIATED A DESCENT, RESET BLEED, STABILIZED PRESSURIZATION AND MADE UNEVENTFUL LANDING. WISDR 2016FA0000664Valve · defectiveDURING ANNUAL INSPECTION, A TEST OF THE PASSENGER OXYGEN MASK DROP IS REQUIRED. PASSENGER MASK DEPLOYED @10,500 FT INSTEAD OF THE 12,500 REQUIREMENT. REMOVED AND REPLACED ALTMETRIC VALVE WITH OVERHAULED UNIT.SDR 2016FA0000665Valve · no testDURING ANNUAL INSPECTION, A FUNCTIONAL CHECK OF THE OXYGEN MASKS WAS PERFORMED. THE OXYGEN MASKS DROPPED AT 105000 FT INSTEAD OF 125. ALTIMETRIC VALVE REPLACEDSDR 2016FA0000657Fuel Control · malfunctionedENGINE SLOW TO START, HANGING AT 33 PERCENT 50+ SECONDS TO START. CHANGED ACFT BATTERY SAME RESULTS. CALIBRATED FCU STARTS AT 38 SECONDS.SDR 2016FA0000618Fuel Control · malfunctionedSLOW STARTS. RE-CALIBRATE FCU.SDR 2016FA0000611Fuel Control · malfunctionedENGINE SURGES IN MAX REVERSE. FCU TO RECALIBRATE.SDR 2016FA0000610Fuel Control · malfunctionedMAX REVERSE FAILED CHECK. RE-CALIBRATE FCU.SDR 2016FA0000609Fuel Control · malfunctionedAFTER RECEIPT OF FCU AFTER RE-CALIBRATION ENGINE WILL START NORMALLY BUT WILL NOT MAKE MAX REVERSE CHECK. SEND OUT FOR RE-CAL.SDR 2016FA0000608Fuel Control · malfunctionedENGINE HANGS DURING START BELOW 40%. SEND FOR RE-CALIBRATION.SDR 2016FA0000625Fuel Control · malfunctionedITT LIGHT WHEN GOING INTO MAX REVERSE. RECALIBRATE FCU.SDR 2016FA0000623Fuel Control · abnormalMAX ITT LIGHT WHEN GOING INTO MAX REVERSE. RE-CALIBRATE FCU.SDR 2016FA0000622Fuel Control · malfunctionedENGINE STARTING WARM. RE-CALIBRATE FCU.SDR 2016FA0000621Fuel Control · malfunctionedENGINE STATING WARM. RE-CALIBRATE FCU.SDR 2016FA0000620Fuel Control · malfunctionedENGINE STARTS WARM. RE-CALIBRATE FCU.SDR 2016FA0000624Fuel Control · malfunctionedENGINE STARTING WARM AND SLOW STARTS. RE-CALIBRATE FCU.SDR 2016FA0000619Fuel Control · malfunctionedENGINE SLOW TO START. RE-CALIBRATE FCU.SDR 2016FA0000617Fcu · malfunctionedHIGH TEMPS DURING START. RE-CLAIBRATE FCU.SDR 2016FA0000615Fuel Control · malfunctionedMAX ITT LIGHT COMES ON WHEN PULLING INTO MAX REVERSE. RE-CALIBRATE FCU.SDR 2016FA0000616Fcu · malfunctionedENGINE START TEMPS EXCESSIVE. RECALIBRATE FCU.SDR 2016FA0000614Fuel Control · malfunctionedFAILED MAX REVERSE CHECK. RE-CALIBRATED FCU.SDR 2016FA0000613Fuel Control · malfunctionedENGINE IS SLOW TO START AND DOES NOT MAKE MAX REVERSE CHECK. RECALIBRATED THE FCU.SDR 2016FA0000612Fuel Control · malfunctionedENGINE IS SLOW TO START. RECALIBRATED THE FCU.SDR 2016FA0000595Fuel Control · out of limitsMANUAL OVER RIDE LOWER THAN 40 PERCENT AND FUEL FLOW LOWER THAN 60 PERCENT. FUEL CONTROL UNIT CONTACTING STOPS.SDR 2016FA0000599Fuel Control · out of adjustDEAD BAND ADJUSTMENT SCREW IS AFT OF THE FLIGHT IDLE ROLLER. RE-CALIBRATED FUEL CONTROL UNIT.SDR 2016FA0000598Fuel Control · out of adjustAIRCRAFT WILL NOT MAKE MAX REVERSE. RE-CALIBRATED FUEL CONTROL UNIT.SDR 2016FA0000597Fuel Control · abnormalENGINE IS SLOW TO START AND NOT MAKING MAX REVERSE. CALIBRATED FUEL CONTROL UNIT.SDR CA141024008Oil System · low pressure(CAN) WHILE ENROUTE, HAD AN INDICATION OF LOW OIL PRESSURE. THE PILOT WAS UNABLE TO LAND. WHILE MANEUVERING FOR A FORCED LANDING ON A FOOTBALL FIELD THE AIRPLANE COLLIDED WITH TREES THAT SEPARATED THE RT WING. THE AIRPLANE CAME TO REST UPRIGHT ON THE FOSDR 2014FA0000536Cabin Pressure · malfunctionedDURING CRUISE, WHILE AT FL310, CABIN PRESSURE BEGAN TO RISE AS CONFIRMED BY THE G1000 ELECTRONIC GAUGES FOR CABIN ALT, ROC AND DIFF PRESSURE. AT 10,300' CABIN ALTITUDE THE CABIN ALTITUDE CAS MESSAGE APPEARED. WHEN THE CABIN ALTITUDE REACHED APPROXIMATELY 10,5SDR 2016FA0000596Fuel Control · abnormalENGINE IS SLOW TO START. FUEL CONTROL UNIT HAD TO BE RE-CALIBRATED.SDR CA140721003Engine · vibration(CAN) AFTER TAKEOFF, THE PILOT NOTICED A VIBRATION HAD COME BACK AFTER THE ENGINE WAS REINSTALLED. THE PILOT MENTIONED THAT THIS VIBRATION HAD NOT BEEN FELT WHEN THE RENTAL ENGINE WAS INSTALLED.SDR 2014FA0000294Structure · contaminatedHORIZONTAL STABILIZER STRUCTURE COMPROMISED BY APPARENT WATER DAMAGE CREATING CRACKS AND CORROSION. DEFECTS WITHIN THE PRIMARY STRUCTURE OF THE HORIZONTAL STABILIZER. HONEYCOMB CORE CONTAMINATED WITH WATER INTRUSION.SDR CA131007007Fuel Control · malfunctioned(CAN) DURING FLIGHT, THE ENGINE TQ STAYED AT 72.7 PERCENT AND THE ENGINE ITT WAS 752. IT REMAINED BELOW 72.7 PERCENT EVEN WHEN THE MANUAL OVERRIDE USED TO 100 PERCENT TORQUE. THE FCU WAS REMOVED FOR INVESTIGATION.SDR RL8R2013FA0000544Roll Pin · looseDURING A ROUTINE ANNUAL INSPECTION, THE LT INBD AILERON MOUNTING PIVOT POINT ROLL PIN WAS FOUND TO BE LOOSE AND WORKING.SDR RL8R2013FA0000543Roll Pin · looseDURING A ROUTINE ANNUAL INSPECTION, THE LT & RT INBD AILERON MOUNTING PIVOT POINT ROLL PINS WERE FOUND TO BE LOOSE AND WORKING.SDR RL8R2013FA0000542Roll Pin · looseDURING A ROUTINE ANNUAL INSPECTION, THE LT & RT INBD AILERON MOUNTING PIVOT POINTS ROLL PINS WERE FOUND TO BE LOOSE AND WORKING.SDR RL8R2013FA0000541Roll Pin · looseDURING A ROUTINE ANNUAL INSPECTION, THE LT AND RT AILERON MOUNTING PIVOT POINT ROLL PINS WERE FOUND TO BE LOOSE AND WORKING.SDR RL8R2013FA0000540Roll Pin · looseDURING A ROUTINE ANNUAL INSPECTION, THE LT AILERON MOUNTING PIVOT POINT ROLL PINS WERE FOUND TO BE LOOSE AND WORKING.SDR CA130603004Engine · making metal(CAN) THE PILOT REPORTED THAT 5 MINUTES AFTER TAKEOFF DURING CLIMB HE FELT A SLIGHT VIBRATION AND THE OIL PRESSURE WENT MOMENTARILY IN TO THE YELLOW RANGE. THE PILOT MADE RIGHT TURN TO RETURN TO HOME BASE WITH THE LOP WARNING LLUMINATED AND A GROWL NOISE BEINGSDR CA130502001Engine · power loss(CAN) SHORTLY AFTER T/O, A LOSS OF ENGINE POWER OCCURRED AND THE A/C MADE A FORCED WHEELS UP LANDING IN AN OPEN FIELD. NO ONE ON BOARD WAS SERIOUSLY INJURED. THE A/C SUFFERED DAMAGE TO THE PROPELLER AND LOWER FUSELAGE. OFFER OF ASSISTANCE WILL BE MADE TO THE DSDR RL8R2014030700151Carriage · damagedINBD FLAP CARRIAGE INSERTS HAVE LOOSENED UP UNDER NORMAL USE. COULD POSSIBLY LEAD TO FLAP CARRIAGE ATTACHMENT FAILURE DURING FLAP DEPLOYMENT WITH SUBSEQUENT LOSS OF FLAP OR WORSE. REQUIRES REPAIR TO FLAP END AND INSTALLATION OF NEW FLAP CARRIAGE INSERTS. THSDR RL8R2014030700150Carriage · damagedINBD FLAP CARRIAGE INSERTS HAVE LOOSENED UP UNDER NORMAL USE. COULD POSSIBLY LEAD TO FLAP CARRIAGE ATTACHMENT FAILURE DURING FLAP DEPLOYMENT WITH SUBSEQUENT LOSS OF FLAP OR WORSE. REQUIRES REPAIR TO FLAP END AND INSTALLATION OF NEW FLAP CARRIAGE INSERTS. THSDR 2014FA0000149Insert · looseINBD FLAP CARRIAGE INSERTS HAVE LOOSENED UP UNDER NORMAL USE. COULD POSSIBLY LEAD TO FLAP CARRIAGE ATTACHMENT FAILURE DURING FLAP DEPLOYMENT WITH SUBSEQUENT LOSS OF FLAP OR WORSE. REQUIRES REPAIR TO FLAP END AND INSTALLATION OF NEW FLAP CARRIAGE INSERTS. THSDR 2013FA0000283Insert · looseINBOARD FLAP CARRIAGE INSERTS HAVE LOOSENED UP UNDER NORMAL USE. COULD POSSIBLY LEAD TO FAP CARRIAGE ATTACHMENT FAILURE DURING FLAP DEPLOYMENT WITH SUBSEQUENT LOSS OF FLAP OR WORSE. REQUIRES REPAIR TO FLAP END AND INSTALLATION OF NEW FLAP CARRIAGE INSERTS. SDR 2013FA0000282Insert · looseINBD FLAP CARRIAGE INSERTS HAVE LOOSENED UP UNDER NORMAL USE. COULD POSSIBLY LEAD TO FAP CARRIAGE ATTACHMENT FAILURE DURING FLAP DEPLOYMENT WITH SUBSEQUENT LOSS OF FLAP OR WORSE. REQUIRES REPAIR TO FLAP END AND INSTALLATION OF NEW FLAP CARRIAGE INSERTS. THI
Back to Daher TBM 700