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.

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 CLEARANCJul 27, 2011 · Diamon DA42 · Engine Fuel DistributionSDR 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.Mar 3, 2011 · N490TS · Diamon DA42 · Engine (Turbine/Turboprop)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.Nov 24, 2010 · N906ER · Diamon DA42 · Fuel StorageSDR 2010FA0000838Chain · brokenLT ENGINE STOPPED ON TAXI, WOULD NOT RESTART. FOUND TIMING CHAIN BROKEN.Aug 19, 2010 · N729PA · Diamon DA42 · Engine (Reciprocating)SDR 2010FA0000530Clutch · blownDURING CRUISE FLIGHT THE PILOT SAID THE LT ENGINE LOST POWER THEN IT OVERSPEED. ENGINE SHUTDOWN.Jun 11, 2010 · N208PA · Diamon DA42 · Reciprocating Engine Front SectionSDR 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 INADVNov 20, 2009 · Diamon DA42 · Propeller Controlling SystemSDR 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 INVESTNov 10, 2009 · Diamon DA42 · Engine (Reciprocating)SDR 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)Oct 22, 2009 · N3RZ · Diamon DA42 · Propeller Controlling SystemSDR 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)Oct 9, 2009 · N3RZ · Diamon DA42 · Propeller Controlling SystemSDR 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 HOMay 7, 2009 · N48LU · Diamon DA42 · Engine Indicating SystemSDR 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 CONNECTIOApr 28, 2009 · N131TS · Diamon DA42 · Propeller Feathering/ReversingSDR 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 Feb 26, 2009 · N49LU · Diamon DA42 · Engine Fuel System WiringSDR 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. WHILNov 22, 2008 · N490TS · Diamon DA42 · Engine Indicating SystemSDR 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 DApr 23, 2008 · N966WW · Diamon DA42 · Main Landing GearSDR 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.Apr 9, 2008 · N49OTS · Diamon DA42 · Engine (Reciprocating)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)Feb 27, 2008 · N4129M · Diamon DA42 · Electrical Power System WiringSDR 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 ENFeb 20, 2008 · N1735L · Cessna 172S · Aircraft Fuel Distribution SystemSDR 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 Jan 4, 2008 · Cessna 172M · Fuel Selector/Shut-Off ValveSDR 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 PNov 8, 2007 · N490TS · Diamon DA42 · Fuel Controlling System
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