Technify TAE125-02-99
Service difficulty reports · 69
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 = 'TAE1250299' 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 = 'TAE1250299' 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 CA110727008Fuel Line · chafed(CAN) THIS FUEL RETURN LINE IS PART OF THE HIGH PRESSURE FUEL INJECTION COMMON RAIL P/N 05-7313-K006801 AND THE ELBOW AT THE END OF THE HOSE CHAFFED ON A HOSE CLAMP FOR THE COOLANT SYSTEM. AN ELBOW FOR THE COOLANT SYSTEM WAS REORIENTED TO PROVIDE MORE CLEARANCSDR 2011FA0000146Clutch · failedCLUTCH DISC LINING FAILURE, CAUSE UNKNOWN. DAMAGE TO THE CLUTCH PRESSURE PLATE AND ENGINE FLYWHEEL OCCURED. ENGINE AUTOMATICALLY SHUTDOWN DUE TO OVERSPEED SIGNAL AS COMMANDED BY THE FADEC CONTROL. UNSCHEDULED ON AIRPORT LANDING SUCCESSFUL.SDR NX4R00006Fuel Cell · crackedDURING AN ANNUAL INSP, THE TECH NOTICED A WET FUEL STAIN UNDER THE RT AUX FUEL TANK. WHEN THE TANK WAS REMOVED, THE TANK WAS FOUND TO BE CRACKED AROUND SEVERAL OF THE AFT SPOT WELD LOCATION ON THE LOWER AFT SURFACE OF THE TANK.SDR 2010FA0000838Chain · brokenLT ENGINE STOPPED ON TAXI, WOULD NOT RESTART. FOUND TIMING CHAIN BROKEN.SDR 2010FA0000530Clutch · blownDURING CRUISE FLIGHT THE PILOT SAID THE LT ENGINE LOST POWER THEN IT OVERSPEED. ENGINE SHUTDOWN.SDR CA091127002Control Valve · leaking(CAN) IT WAS REPORTED ON NOVEMBER 25, 2009 THAT DURING A TRAINING FLIGHT THE RT ENGINE EXPERIENCED A SEVERE POWER LOSS. JUST PRIOR TO THIS INCIDENT ENGINE WAS NOTICED SURGING BETWEEN 50 AND 70 PERCENT POWER. JUST AFTER THE INITIAL POWER LOSS THE ENGINE INADVSDR CA091117007Engine · failed(CAN) LT ENG LOST PWR AND STOPPED DURING FLIGHT. ACFT WAS LANDED. ENG FIELD REP REMOVED A CAMSHAFT POSITION SENSOR AND CONFIRMED THAT THE CAMSHAFT DOES NOT MOVE WHEN THE CRANKSHAFT IS ROTATED. ENG REMOVED FROM AIRFRAME AND SHIPPED TO MFG IN GERMANY FOR INVESTSDR 2009FA0000874Control Valve · defectiveTHE LEFT ENGINE PROPELLER CONTROL VALVE FAILED CAUSING THE PROPELLER TO FEATHER AND COMMANDED THE FADEC TO SHUT DOWN ENGINE. THIS ISSUE CAN BE RESOLVED BY COMPLYING WITH SB TAE 125-1007 P1, REV 2. (K)SDR 2009FA0000819Control Valve · defectiveTHE LT ENGINE PROPELLER CONTROL VALVE FAILED, CAUSING THE PROPELLER TO FEATHER AND COMMANDED THE FADEC TO SHUTDOWN ENGINE. THIS ISSUE CAN BE RESOLVED BY COMPLYING WITH SB TAE 125-1007P1, REV 2. (K)SDR 2009FA0000461Sense Line · splitTHE MAP SENSE HOSE, MATING TO (PN 52-7150-H000102) HAD BURST ON 2 OF OUR ENGINES. THIS CAUSES MAP A AND MAP B PRESSURE SPLIT, FAILING EDU A AND B. IN BOTH CASES, THE BURST OCCURRED APPROX 2 INCHES FROM THE ENGINE MANIFOLD FITTING. THIS HOSE IS A TYPE 306 HOSDR 2009FA0000363Valve · malfunctionedTHE LT ENGINE BEGAN TO SURGE ON NIGHT CROSS-COUNTRY TRAINING FLIGHT. AFTER CHECKING THE ENGINE, MFG WAS CONTACTED AND SAID THEY HAVE HAD SEVERAL REPORTS OF THIS SAME THING HAPPENING. THERE IS ARCING BETWEEN THE MALE PINS ON THE VALVE AND THE FEMALE CONNECTIOSDR 2009FA0000211Wire Harness · burnedDURING IMC FLIGHT, THE RT ENGINE EXPERIENCED A RAPID 50 PERCENT POWER EXCURSION DOWNWARD TO 25 PERCENT AND RAPID SURGING THEREAFTER. AN EMERGENCY WAS DECLARED TO ATC, THE FLIGHT COMPLETED SAFELY. INVESTIGATION: ON THE FADEC ENGINE WIRING LOOM, THE PROPELLER SDR 2008FA0000839Sensor · dirtyFADEC CONTROLLED POWERPLANT/ HAD UNCOMMANDED POWER REDUCTION TO 75 PERCENT (3 SEPARATE WRITE-UPS) ACCOMPANIED BY MINOR ENGINE SURGING AT VARIOUS TIMES DURING NORMAL CRUISE FLIGHT. MFG FIX WAS RE-DESIGNED FADEC SOFTWARE, THAT DID NOT ALLEVIATE THE PROBLEM. WHILSDR 2008FA0000290Fastener · missingDURING PREFLIGHT, THE CREW NOTICED THAT THE SMALL CIRCLIP (PN DIN471-08-VERZ) THAT SECURES THE MLG DOWNLOCK HOOK PIN IN POSITION WAS MISSING. MAINT JACKED THE AC AND INSTALLED A NEW CLIP. WHEN THIS CLIP IS NOT IN PLACE, THE PIN MIGRATES AFT AND IN SOME CASES DSDR 2008FA0000241Engine · power lossAFTER TAKEOFF AND PULLING LANDING GEAR UP, LT ENGINE POWER REDUCTION TO 75 PERCENT FOR ABOUT ONE MINUTE AND POWER WAS RESTORED. THIS SAME ISSUE HAS BEEN INDUCTED TWICE IN LESS THAN 24 HRS. THERE IS NO FEDAC WARNINGS SHOWN ON SYS. A REPORT HAS BEEN SENT TO MFG.SDR 2008FA0000149Connector · arcedCONNECTOR IS NOT MAKING GOOD CONTACT AND CAUSING ARCING. PROBABLE CAUSE IS AUTOMOTIVE QUALITY AND NOT OF THE THREADED TYPE. TO PREVENT OCCURRENCE RECOMMEND USING AVIATION THREADED TYPE PLUG. (K)SDR 2008FA0000169Line · crackedPILOT WAS FLYING AT 5,500 FEET WHEN THE ENGINE STARTED RUNNING ROUGH. WITHIN MOMENTS THE FADEC (A) LIGHT CAME ON THEN FADEC (B) ILLUMINATED. THE PILOT TRIED TO ACTIVATE THE MANUAL OVERRIDE BUT WAS UNABLE TO PUT OUT THE WARNING LIGHTS. THE RPMS DROPPED UNTIL ENSDR CA080213014Selector · damaged(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 2007FA0001040Fadec · malfunctionedDURING FLIGHT TRAINING MANEUVERS, SIMULATED SINGLE ENGINE OPERATIONS AT 5000 FT ASL, THE LT ENGINE WAS THROTTLED BACK TO FLIGHT IDLE (5 PERCENT POWER, THROTTLE RETARDED). UPON RETURN TO NORMAL POWER OPERATIONS THE LT ENGINE BEGAN TO SURGE FROM 20-100 PERCENT P
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