Garrett TPE331-10UA

Service difficulty reports · 375

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 = 'TPE33110UA'
  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 CA960610008Motor · failed(CAN) THE COPILOTS PITCH TRIM ACTUATOR DROVE SLOWER THAN NORMAL AND POPPED THE CIRCUIT BREAKER. THE PITCH TRIM ACTUATOR REPLACED. ACTUATOR DID NOT HAVE THE NUTS AND SHAFT REPLACED WITH NEW PARTS AT THE LAST OVERHAUL AS REQUIRED BY AD 93-15-02R1. THEREFORE THISMay 31, 1996 · Swrngn SA226TC · Stabilizer Control SystemSDR CA960521201Bolt · broken(CAN)ENGINE MOUNT TO FIREWALL BOLT, INBOARD UPPER POSITION, FOUND BROKEN IN TWO PIECES. NO FRETTING OF FIREWALL AT ANY MOUNT LOCATION. 91 HOURS SINCE LAST INSPECTION. PARTS NEW IN JUNE 95. PARTS SENT FOR LAB ANALYSIS.May 14, 1996 · Swrngn SA226TC · Engine Mount SectionSDR CA960521001Inner Ring · cracked(CAN) ONE MINUTE AFTER TAKEOFF, THE LEFT ENGINE WAS SHUT DOWN AND AUTO FEATHERED. THE DISASSEMBLY AND EXAMINATION OF THE ENGINE REVEALED THE REAR TURBINE CARRIER CRACKED, ALL FIRST STAGE TURBINE BLADES BROKEN. COMBUSTION CHAMBER INNER RING CRACKED 350 DEGREES.May 9, 1996 · Swrngn SA226TC · Turbine Engine Combustion SectionSDR AU960560Housing · cracked(AUS) ENGINE ACCESSORY HOUSING CRACKED IN GUSSET CASTING ADJACENT TO THE RH ENGINE MOUNTING PAD - CRACK LENGTH 25.4MM (1IN)Apr 26, 1996 · Swrngn SA226TC · Turbine Engine Accessory DriveSDR CA960502053Actuator · noisy(CAN)NOSE GEAR FAILED TO EXTEND. EMERGENCY EXTENSION CARRIED OUT. FROZEN SLUSH ON NOSE GEAR. NLG FAILED TO EXTEND NORMALLY AFTER WARMING UP IN HANGAR AND GEAR SWINGS CARRIED OUT. SOME SAND CONTAMINATION IN GEAR MECHANISM. LH NLG ACTUATOR IS ONLY ACTUATOR THAT Apr 22, 1996 · Swrngn SA226TC · Landing Gear ActuatorSDR CA960416003Diaphragm · worn(CAN)AFTER TAKEOFF, ENGINE POWER AND TORQUE FELL OFF 50 PERCENT WITH THE POWER LEVER MOVED AFT. SUBSEQUENT INVESTIGATION FOUND THAT THE RIGHT HAND FUEL CONTROL "ROLLING DIAPHRAGM" HAD AN EXCESSIVE LEAK RATE AND WAS REPLACED. ON CAREFUL EXAMINATION, THE "ROLLINMar 30, 1996 · Swrngn SA226TC · Fuel Control/Reciprocating EnginesSDR CA960404006Line · chafed(CAN)HYDRAULIC FLUID BEING LOST NOTED BY CREW. INVESTIGATION FOUND THE RIGHT HAND WING ROOT FLAP DOWN LINE HAD CHAFED THROUGH. THIS IS A 1/4 INCH ALUMINUM LINE. A STAINLESS STEEL REPLACEMENT WAS MADE. THI S LINE IS IN AREA BEHIND AIR CYCLE MACHINE AND HEAT EXMar 22, 1996 · Swrngn SA226TC · Trailing Edge Flap Control SystemSDR CA960412007Start Lock Pin · pulled through(CAN)ON ROUTINE PHASE INSPECTION, THE SPLIT PINS WERE FOUND TO BE PULLING THROUGH THE ENDS OF THE START LOCKS. NEW START LOCKS P/N 57B08030-37 NOW SUPPLIED BY HARTZELL HAS A THICKER END WALL ALTHOUGH THE P/N HAS NOT BEEN CHANGED.Mar 22, 1996 · Swrngn SA226TC · Propeller AssemblySDR CA960412009Cable · broken(CAN)LEFT HAND POWER LEVER FOUND LOOSE AT START BUT DID NOT AFFECT ENGINE POWER. LEFT POWER LEVER CABLE, INNER RIBBON FOUND BROKEN JUST FORWARD OF THE PEDESTAL. THIS CABLE HAS AN UPPER AND LOWER ASSEMBLY. UPPER ASSEMBLY REPLACED. IN ADDITION, CABLE RE-ROUTED Mar 20, 1996 · Swrngn SA226TC · Power LeverSDR BDHA960007Connector · broken wirePIR - FLT NR 421 - ON FIRST START ATTEMPT, ENGINE WOULD NOT LIGHT OFF. AFTER A LONG PREHEAT, THE ENGINE STARTED. MAINTENANCE INVESTIGATED AND FOUND THE WIRE TO THE PRIMARIES ONLY SOLENOID CANNON PLUG BROKEN. AFTER REPLACING THE CANNON PLUG, THE ENGINE STARTMar 19, 1996 · N229AM · Swrngn SA226TC · Ignition SystemSDR CA960214011Fire Warn · illuminated(CAN)ON TAKEOFF ROLL, AND SHORTLY AFTER SELECTING 'SPEED LEVERS HIGH', RIGHT ENGINE FIRE WARNING CAME ON. POWER REDUCED AND RH 'STOP AND FEATHER' PULLED. NO SMOKE OR FIRE NOTED FROM ENGINE. INVESTIGATION FOUND RH FIRE WARNING STILL ON AND ENGINE COLD. LIGHT OUFeb 4, 1996 · Swrngn SA226TC · Fire DetectionSDR BDHA960004Fuel Control · out of adjustMSP - FLT NR 475 - CREW REPORTED A POWER LEVER SPLIT ON TAKEOFF AND RETURNED. THE ENGINE RIGGING WAS INSPECTED AND MAX POWER WAS ADJUSTED. ENGINE POWER RUNS WERE PERFORMED AND ALL INDICATIONS WERE NORMAL. A TEST FLIGHT WAS PERFORMED AND THE AIRCRAFT WAS RETJan 22, 1996 · N229AM · Swrngn SA226TC · Fuel Control/Turbine EnginesSDR CA960131004Fuel Contrl Unit · faulty(CAN)ON START #1 ENGINE FUEL FLOW INDICATED 250 LBS WITH START TEMPERATURE RISING TO MAXIMUM LIMITS. THE START WAS ABORTED. AFTER ALLOWING FOR A COOLING DOWN PERIOD A FURTHER TWO STARTS WERE UNSUCESSFUL. T HE FUEL CONTROL UNIT AND THE HP FUEL PUMP WERE REPLACEJan 18, 1996 · Swrngn SA226TC · Fuel Control/Reciprocating EnginesSDR 96ZZZM930Fuel Contl Unit · failedLEFT ENGINE POWER BEGAN CLIMBING UNCOMMANDED DURING CLIMB-OUT AT APPROX 500 FEET AGL. POWER LEVER (FCU) MOVEMENT UNRESPONSIVE. ENGINE SHUTDOWN AND AIRCRAFT RETURNED TO LWT AND LANDED UNEVENTFULLY. INTERNAL FCU FAILURE. IT WAS DETERMINED THAT INTERNAL FCU FDec 27, 1995 · N115BS · Swrngn SA226TC · Fuel Control/Turbine EnginesSDR CA960102004Fcu · over adjusted(CAN)INSTALLED NEWLY OVERHAULED FCU. HAD TO ADJUST MAX FUEL TWICE AT 1/2 CW TURN EACH TIME. 5 MONTHS LATER, ADJUSTED ANOTHER 30 POUNDS PER HOUR. ENGINE WAS NOW UNABLE TO GO BELOW 95 PERCENT, REPLACED FCU. SUBMITTER SUGGESTS THAT THE FCUS ARE BEING RECEIVED FRDec 19, 1995 · Swrngn SA226TC · Fuel Control/Reciprocating EnginesSDR CA951122018Idler Gear · excessive wear(CAN) IMMEDIATELY AFTER AN OIL SAMPLE, THE CHIP DETECTOR LIGHT ILLUMINATED. MAINT INVEST REVEALED A SMALL AMOUNT OF UNIDENTIFIED METAL ACROSS THE CHIP DET CONTACTS. THE ACFT WAS CLEARED TO CONTINUE IN SERVICE. SEVERAL WEEKS LATER THE CHIP DET LIGHT AGAIN ILLUMNov 11, 1995 · Swrngn SA226TC · Turbine Engine Accessory DriveSDR MEJA951005Contl Mech · wornFLIGHT 9935, BIS TO FAR, WHILE ON DESCENT TO FAR THE LEFT ENGINE POWER WOULD NOT REDUCE BELOW 47 PERCENT TORQUE. THE FLIGHT CREW SHUT DOWN THE ENGINE FOR POSITIVE CONTROL AND LANDED AT FAR WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE POWER LEVER BALL JOINOct 27, 1995 · N163MA · Swrngn SA226TC · Power LeverSDR BDHA9500025Lock Out Vl Wire · brokenBIS - FLT 421 - THE LEFT ENGINE WOULD NOT LIGHT-OFF AFTER 10 PERCENT RPM. INSPECTION REVEALED A BROKEN WIRE AT THE FUEL ANTI-ICE LOCK OUT VALVE. REPAIRS WERE MADE AND THE ENGINE OPERATED NORMALLY. THE AIRCRAFT WAS RETURNED TO SERVICE. (X)Oct 25, 1995 · N328BA · Swrngn SA226TC · Fuel Controlling SystemSDR 96ZZZM17Fuel Control · leakingRIGHT ENGINE TORQUE BEGAN FLUCTUATING 900 LBS. NR 2 ENGINE FUEL CONTROL HAS A LEAK IN THE P3 BELLOWPHRAM. REMOVED AND REPLACED P3 BELLOWPHRAM. GROUND POWER RUN OPS CHECKED NORMAL.Oct 24, 1995 · N139PA · Swrngn SA226TC · Fuel Control/Turbine EnginesSDR MEJA951003Egt Harness · brokenFLIGHT 9936, FAR TO BIS, THE LEFT ENGINE EGT FLUCTUATED AND THEN WENT TO ZERO DURING THE TAKEOFF ROLL. THE FLIGHT CREW ABORTED THE TAKEOFF AND RETURNED TO THE RAMP. MAINTENANCE FOUND BROKEN EGT HARNESS. REMOVED AND REPLACED HARNESS IN ACCORDANCE WITH GARRETOct 21, 1995 · N163MA · Swrngn SA226TC · Engine EGT/TIT Indicating SystemSDR BDHA9500021Fuel Line · looseBIS - FLT NR 421 - CREW REPORTED, THE LEFT ENGINE WAS DRIPPING FUEL OUT OF COWLING. MAINTENANCE PERSONNEL INSPECTED THE ENGINE AND FOUND THE LINE TO THE FUEL FLOW TRANSMITTER WET WITH FUEL. THE LINE WAS TIGHTENED AND ENGINE RUN AND LEAK CHECK PERFORMED. THESep 21, 1995 · N329BA · Swrngn SA226TC · Fuel Flow IndicatingSDR 95ZZZX3967Oil Cooler Inlet · leakingOIL PRESSURE DROPPED ON FINAL APROACH ON LEFT ENGINE. ENGINE WAS SHUT DOWN AFTER LANDING. OIL LEAK IN OIL COOLER INLET RING. PILOT NOTICED OIL PRESSURE STARTING TO DROP ON FINAL APPROACH. PRESSURE DROPPED TO 5 PSI AFTER LANDING ENGINE WAS SHUT DOWN. LEFT May 5, 1995 · N115BS · Swrngn SA226TC · Engine Oil CoolerSDR BDHA9500007Chip Detector · dirtyMSP - FLT 421 - LT ENGINE CHIP LIGHT ILLUMINATED WHILE TAXIING. AIRCRAFT RETURNED TO HANGER. THE CHIP DETECTOR WAS CLEANED AND PENALTY RUN PERFORMED. THE CHIP DETECTOR WAS REINSPECTED AND ALL INDICATIONS WERE NORMAL. THE AIRCRAFT WAS RELEASED. (W)Mar 17, 1995 · N328BA · Swrngn SA226TC · Turbine Engine Reduction GearSDR MEJA9502004Packing · cutFLIGHT 6692, MTY TO SAT, RIGHT ENGINE EGT BEGAN TO RISE. REDUCED POWER AND EGT STARTED TO DECREASE. ADVANCED POWER AND EGT/TORQUE BEGAN TO SURGE. SHUTDOWN ENGINE AND PROCEEDED TO SAT. AIRCRAFT LANDED WITHOUT FURTHER INCIDENCE. MAINTENANCE TROUBLESHOT SYSTMar 14, 1995 · N4206M · Swrngn SA226TC · Fuel Controlling SystemSDR 95ZZZX1380Fuel Control · failedDURING REPOSITION FLIGHT FROM CIT TO BWI 20 MINUTES INTO FLIGHT, RT ENGINE STARTED BYPASSING FUEL, REDUCED POWER AND CONTINUED CLIMB. AT 19,000 FEET, NOTICED EGT AT 655. REDUCTION OF POWER DID NOT CHANGE EGT. POWER LEVER REDUCED TO FLIGHT IDLE, EGT WENT TO Mar 12, 1995 · N608JX · Bag JETSTM3101 · Fuel Control/Turbine Engines
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