Thielert TAE-125-01
Service difficulty reports · 25
Newest first. General aviation reporting is voluntary.
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 engine_model_key = 'TAE12501' 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 engine_model_key = 'TAE12501' 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 2024FA0000337Turbocharger · crackedTURBO EXHAUST MANIFOLD CRACKED ABOUT 2 INCHES LONG.SDR CA190510016Turbocharger · failed(CAN) LOW OIL PRESSURE IN RH ENGINE OBSERVED, FOLLOWED BY OIL ODOR IN CABIN, FOLLOWED BY LOSS OF ENGINE POWER. ENGINE WAS SHUTDOWN AND EMERGENCY LANDING REQUESTED. LANDING WAS SUCCESSFUL WITH NO FURTHER ISSUES. MAINTENANCE INSPECTION REVEALED THE TURBOCHARGER SDR 8HBR20180906018Gearbox · failedENGINE GEARBOX INPUT SPLINE SHEARED DURING STARTUP. AD 2015-21-01 "START MONITORING SYSTEM" PCW, BY START MONITORING SYSTEM IAW MSB-42-109-KIT AT 3.11.2016 591.3 ETT 1584.3 ACTTSDR CA150506001Cartridge · damaged(CAN) PILOTS REPORTED THAT THE RT ENGINE OIL TEMPERATURE WAS HIGH, 136 DEGREES C. MAINTAINER CHANGED OIL TEMPERATURE PROBE, OIL COOLERS, OIL, AND FILTER. OIL TEMPERATURE REPORTED AS STILL RUNNING HIGH. IT WAS DISCOVERED THAT THE SILICATE CARTRIDGE, USED TO PSDR 7UVR2014031400158Governor · malfunctionedPILOT STATED THAT THE LT PROP DID NOT FEATHER AFTER ENGINE SHUTDOWN IN FLIGHT, 2 ATTEMPTS, ENGINE CONTINUED TO WINDMILL. VERIFIED FAULT ON GROUND, ENGINE SHUTS DOWN BUT PROP DOES NOT FEATHER, INSPECTED PROP CONTROL PANEL FROM REAR NACELLE FOR BROKE WIRES AND SDR XGKR201311200001Clutch · disintegratedGEARBOX CLUTCH DISINTEGRATED CAUSING COMPLETE POWER FAILURE, CAUSING ENGINE OVER-SPEED AND LOSS OF ENGINE OIL AND OIL PRESSURE. PILOT SHUTDOWN THE FAILED ENGINE AND LANDED AIRCRAFT.SDR CA131029003Tire · failed(CAN) LT MLG WOULD NOT EXTEND DURING APPROACH. AFTER NUMEROUS ATTEMPTS PILOT ELECTED TO LAND WITH GEAR RETRACTED AND ENGINES SHUTDOWN. ACFT WAS HOISTED INTO AIR, GEAR LOWERED AND LOCKED, ACFT TAXIED TO RAMP AND SECURED. TYPICAL DAMAGE TO ACFT FOR A WHEELS RSDR 2013FA07240001Belt · failedV-BELT FAILURE ON RT ENGINE CAUSED RT ALTERNATOR TO FAIL AND ENGINE COOLANT TEMP TO RISE. SHUTDOWN RT ENGINE AND FEATHERED THE PROPELLER. ACFT DIVERTED. V-BELT HAD RECENTLY BEEN REPLACED ON BOTH RT AND LT ENGINES. INVESTIGATION REVEALED POSSIBLE INCORRECT INSSDR 2013FA0000272Warning System · malfunctionedWHILE TROUBLESHOOTING THE ALTERNATOR OUT WARNING SYSTEM, DISCOVERED THAT T1 ALTERNATOR OUT WOULD NOT GIVE ANY WARNING.SDR 2012FA0000482Propeller · leakingPROPELLER LEAKING OIL FROM VENT IN DOME.SDR 2011FA0000667Fadec · malfunctionedRECEIVING INTERMITTENT ECU B FAILURE ON LT ENGINE. EVENT LOG SHOWS CAM SENSOR FAILURE. PROBLEM OCCURS RANDOMLY AND NOT BEEN ABLE TO ISOLATE TO PHASE OF FLIGHT OR OPERATING CONDITIONS. PILOT ABLE TO RESET AND CONTINUE WITH NO FURTHER ISSUES, BUT SPORADICALLYSDR 2010FA0000887Control Valve · failedLT ENGINE SHUTDOWN IN CRUISE FLIGHT. FOUND DEFECTIVE PROP CONTROL VALVE AFTER PERFORMIND MX DOWNLOAD. REPLACED VALVE AND OPS CHECKED NORMAL.SDR 2010FA0000424Ecu · malfunctionedAFTER A SERIES OF 3 POWER OFF STALLS (BOTH GEAR/FLAPS UP & DOWN), APPLICATION OF FULL THROTTLE (IN ORDER TO RECOVER) RESULTED IN 65 TO 75 PERCENT POWER (MAX,100 PERCENT POWER NOT AVAILABLE) 2 OUT OF 3 ATTEMPTS, RT ENGINE, OPERATED NORMALLY. THIS WAS THE SECONSDR CA091013010Fuel Tank · contaminated(CAN) ACFT WAS UNDERGOING MX (200 HR INSP AND ENG REPAIR). ACFT HAD BEEN IN HANGAR FOR APPROX 6 MONTHS. AT COMPLETION OF MX, WHILE TRYING TO TROUBLESHOOT A FUEL QUANTITY INDICATION PROBLEM, A FUEL SAMPLE WAS TAKEN TO CHECK FOR WATER. REMOVED A LARGE QUANTITY OSDR 2009FA0000234Tube · bentDURING A PREFLIGHT INSPECTION, THE NLG DRAG BRACE PIVOT WAS FOUND TO BE LOOSE, BENT AND DAMAGED. THE FOLLOWING PARTS NEEDED TO BE CHANGED BECAUSE OF DAMAGE. 1 CAMP BOLT TUBE, 1 BRACE BEARING, 1 NIG BRACKET, 2 GUDGEON AND 2 BEARINGS. INVESTIGATION REVEALED THROSDR 2009FA0000358Downlock Switch · failedDURING NORMAL OPERATION, PILOT REPORTED THAT THE RT MLG DOWN AND LOCKED INDICATION FAILED. UPON UNEVENTFUL LANDING AND SUBSEQUENT INSP, THE RT MLG DOWN LOCK SWITCH NEEDED TO BE ADJUSTED. GEAR FUNCTIONAL CHECKS WERE PERFORMED IAW MM AND ACFT WAS RETURNED TO SSDR 2008FA0000517Fitting · looseCIRCLIP THAT SECURES DOWNLOCK PIN IN MLG LEGS HAS BEEN TWISTING OFF RENDERING THIS DOWNLOCK PIN LOOSE ENOUGH TO FALL OUT WHEN GEAR IS RETRACTED, THIS PARTICULAR AC HAD THE AFT SECTION OF THE WHEELWELL DAMAGED DUE TO THE PIN HANGING HALF WAY OUT AND CONTACT THRSDR B4V2008F00000Connector · arcedCONNECTOR IS NOT MAKING GOOD CONTACT AND CAUSING ARCING AND ENGINE TO QUIT. PROBABLE CAUSE IS AUTOMOTIVE QUALITY AND NOT OF THE THREADED TYPE. TO PREVENT RECURRENCE RECOMEND USING AVIATION THREADED TYPE PLUG. (K)SDR CA080115006Pushrod · bent(CAN) AFTER RECEIVING A REPORT OF AN ANOMALY WITH THE CONTROL ROD FROM ANOTHER OPERATOR, WE INSPECTED THE ROD ENDS ON OUR AC. WE ALSO FOUND THE ROD ENDS ON BOTH LT AND RT AILERONS BENT. THE ROD ENDS APPEAR TO HAVE BEEN BENT TO ACCOMODATE THE MOVEMENT OF THE AISDR CA080115008Control Rod · bent(CAN) AFTER RECEIVING A REPORT OF AN ANOMALY WITH THE CONTROL ROD FROM ANOTHER OPERATOR, WE INSPECTED THE ROD ENDS ON OUR AC. ALSO FOUND THE ROD ENDS ON BOTH LT AND RT AILERONS BENT. THE ROD ENDS APPEAR TO HAVE BEEN BENT TO ACCOMODATE THE MOVEMENT OF THE AILESDR CA080115003Rod End · bent(CAN) WHILE RIGGING THE AILERON SYS FOLLOWING MAINT, NOTICED BOTH THE LT AND RT AILERON CONTROL ROD END FITTINGS WERE BENT WHERE THE CONTROL ROD IS ATTACHED TO THE BELLCRANK AT THE MOST OB POINT. NEW STRAIGHT FITTINGS WERE INSTALLED BUT THIS CAUSED THE AILERONSDR CA080211019Selector · malfunctioned(CAN) AC WAS BEING RETRO-FITTED WITH A 2.0 TURBO DIESEL ENGINE IAW STC. THE FUEL SYS WAS COMPLETED, FUEL INSTALLED AND INSPECTED FOR LEAKS. A LEAK WAS DISCOVERED COMING FROM THE FUEL SELECTOR AT THE NIPPLE FOR THE FUEL LINE GOING TO THE HEADER TANK. THE B-NUT SDR 2007FA0000864Cylinder Head · failedENGINE BEGAN LOSING COOLANT BY PRESSURIZING THE COOLING SYSTEM WITH COMBUSTION PRESSURE AND BLOWING COOLANT OVERBOARD. WHEN CYLINDER HEAD WAS REMOVED, EACH CYLINDER HAD A CRACK BETWEEN THE GLOW PLUG AND EXHAUST VALVE RECESS. THE ENGINE HAD PASSED A COMPRESSISDR 2007FA0000865Cylinder Head · failedENGINE BEGAN LOSING COOLANT BY PRESSURIZING THE COOLING SYSTEM WITH COMBUSTION PRESSURE AND BLOWING COOLANT OVERBOARD. WHEN CYLINDER HEAD WAS REMOVED, EACH CYLINDER HAD A CRACK BETWEEN THE GLOW PLUG AND EXHAUST VALVE RECESS. THE ENGINE HAD PASSED A COMPRESSISDR 2007FA0000871Cylinder Head · damagedENGINE BEGAN LOSING COOLANT BY PRESSURIZING THE COOLING SYSTEM WITH COMBUSTION PRESSURE AND BLOWING COOLANT OVERBOARD. WHEN THE ENGINE WAS REMOVED AND THE OIL DRAINED, COOLANT WAS FOUND IN THE OIL AND FILLING UP CYLINDER NR 3. IT IS SUSPECTED THAT IF THE CYL
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