Garrett TPE331-11U
Service difficulty reports · 625
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 = 'TPE33111U' 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 = 'TPE33111U' 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 KY7A20260808001Transfer Tube · occludedDURING LANDING ROLLOUT, THE ENGINE LOST OIL PRESSURE, RESULTING IN A LOSS OF POWER AND ENGINE SHUTDOWN. TROUBLESHOOTING IDENTIFIED AN OCCLUDED MAIN SHAFT OIL TRANSFER TUBE. CLEANED THE MAIN SHAFT OIL TRANSFER TUBE IN ACCORDANCE WITH TPE331-11 MM 72-00-25, CHAPSDR 2025FA0000687Bearing · spalledIDLER GEAR [PN: 896804-2] TEETH GALLED DUE TO BEARINGS (2EA) [PN: 3103035-1, SN: 10-151725-07307 & 10-151725-07323, TSN: 5,558.3] WORN AND SPALLING. RESULTED IN UNCOMMANDED SHUTDOWN OF ENGINE DUE TO FUEL PRESSURE LOSS.SDR 2024FA0000798Shaft · shearedENGINE REMOVED FOR DISCOLORED OIL AND EXCESSIVE OIL CONSUMPTION, ONE QUART EVERY TWO HOURS. INSPECTION REVEALED OIL SCAVENGE PUMP ASSEMBLY SCORED (PN: 3108282-2). SCAVENGE PUMP GEAR SHAFT DRIVE KEY SLOT ELONGATED (PN: 3108286-1) DRIVE KEY SHEARED (PN: 3108289-SDR 2024FA0000372Bearing · failedTORQUE SENSOR BEARING FAILED (PN: 3103585AL-1, SN: TA43-0510123, TSN: 2,125.4). SPECTROMETRIC OIL ANALYSIS PROGRAM RESULT REPORT DISCOVERED M50 PLATELETS, SHINY, >100, UP TO 1.1MMX0.9MM. M50 IS A BEARING RACE MATERIAL AND THE QUANTITY OF PLATELETS FOUND IN THESDR 2024F00080Egt Indication · activatedLH SRL COMPUTER INDICATES SPIKES, OPEN FUEL BY PASS.SDR 2023FA0000807Bearing · crackedFAILED BEARING [PN: 3103035-1, SN: 17-151725-05437, TSN: 2,824.4] RESULTED IN LOSS OF ENGINE DRIVEN FUEL CAUSING IN FLIGHT SHUTDOWN OF ENGINE [TPE331-11U-612G, SN: P-44713C, TSN: 19,659.1, CSN: 19,659.1, TSO: 5,649.1, CSO: 4,730, TSHSI: 2,824.4, CSHSI: 2,475].SDR 2023FA0000761Bearing · crackedFAILED BEARING [PN3103035-1, SN: 09-151725-07615, TSN: 1,440.5] RESULTED IN LOSS OF ENGINE DRIVEN FUEL CAUSING IN FLIGHT SHUTDOWN OF ENGINE [TPE331-11U-611G, SN: P-44197C, TSN: 17,783.9, CSN: 19,400, TSCAM: 1,440.5, CSCAM: 1,370].SDR KY7A2023110920038Engine · failedRH ENGINE INOP (FAIL IN FLIGHT) - E2 INSTALLED QEC ASSY FROM N787C E1 5EA TASK CARD 72 & 902 WORK PREFORMED BY SIAWASH ALOKOZAI 01250.SDR 2023FA0000600Bearing · failedFAILED BEARING [PN: 3103035-1, SN: 13-151725-02623, TSN: 2,892.6].SDR 2023FA0000599Bearing · crackedFAILED BEARING [PN: 3103035-1WD, SN: J042A, TSN: UNKNOWN].SDR 2023FA0000154Bearing · crackedFAILED BEARING [PN: 3103035-1, SN: 09-151725-06157, PART TT: 646.0] RESULTED IN LOSS OF ENGINE DRIVEN FUEL CAUSING IN FLIGHT SHUTDOWN OF ENGINE [TPE331-11U-611G, SN: P-44299C, TSN: 23,620.0, CSN: 20,148, TSCAM: 5,111.2, CSCAM: 4,306, TSHSI: 1,413.3, CSHSI: 1,1SDR JIKA2019072501Sending Unit · defectiveDURING DESCENT APPROXIMATELY 20 MILES INTO KSAT, THE PILOT NOTICED THE LEFT ENGINE OIL TEMPERATURE REGISTERED AT 90 DEGREE CREW THEN CONSULTED THE QRH. POWER LEVER WAS REDUCED TO FLIGHT IDLE AS INSTRUCTED BY QRH AND CONTINUED MONITORING THE OIL TEMPERATURE GASDR CA190729009Pin · sheared(CAN) NOSE GEAR UPPER SCISSOR LINK SPRING PIN FOUND SHEARED. FLEET CAMPAIGN WAS CONDUCTED. ROLL PIN REPLACED AND AIRCRAFT RETURNED TO SERVICE. (TC# 20190729009)SDR CA190529022Control Cable · broken(CAN) C-XXXX HAD A REJECTED TAKE OFF DUE TO THE R/H ENGINE HAVING NO RESPONSE WITH POWER LEVER MOVEMENT. REPLACED BROKEN R/H POWER CABLE PEDESTAL SEGMENT AND BALL JOINT ASSEMBLY GROUND RUN FUNCTION TESTED SERVICEABLE. THE PHASE INSPECTION MANUALS HAVE BEEN RESDR CA190402015Nozzle · failed(CAN) THE MAIN OIL JET CRACKED IN THE GEAR BOX CAUSING A BEARING TO FAIL DUE TO LACK OF OIL ON THE BEARING IN THE MAIN GEAR CASE. THE ENGINE WAS PULLED DUE TO THE OIL LAB BECAUSE OF MAJOR M50 MATERIAL THAT WAS NOTED FROM THE BEARING.THE ENGINE PART HAS 4612.9 SDR KY7A20181204001Turbine Wheel · failedPILOT REPORTED LOUD BANG IN FLIGHT FOLLOWED BY ACTIVATION OF NTS SYSTEM; PILOT SECURED ENGINE AND LANDED. ENGINE REMOVED/REPLACED IN THE FIELD AND TRANSPORTED TO MAIN MX BASE FOR TEARDOWN. MX PERSONNEL FOUND DURING TEARDOWN THAT SEVERAL BLADES ON THE 1ST HPT WSDR DUFA20180529001Gear · strippedWHILE IN CRUISE DURING A PART 91 REPOSITION FLIGHT, THE NR 2 ENGINE FLAMED OUT AND SHUT DOWN. MAINTENANCE CREW WAS DISPATCHED TO THE LOCATION AND THE ENGINE GEARBOX OPENED UP FOR INVESTIGATION. FOUND ACCESSORY GEAR ASSEMBLY HAD FAILED LOSING CONTINUITY TO FUELSDR K51A2017111600001Bearing · failedRIGHT ENGINE LOST POWER DURING DESCENT. ENGINE SHUTDOWN AND PROPELLER FEATHERED. FOUND THE GEARBOX BEARING FAILED.SDR DUFA2017002Indication Sys · false indicationWHILE IN CRUISE FLIGHT, THE PILOT NOTICED THE RIGHT ENGINE OIL TEMP CLIMBING TO NEAR RED LINE TEMPERATURE. THE OIL PRESSURE AND ALL OTHER ENGINE PARAMETERS APPEARED NORMAL BUT AS A PRECAUTION, THE PILOT SHUT DOWN THE RIGHT ENGINE. DIVERTED TO THE NEAREST SUITSDR HKGA20170303003Engine · fireAFTER ENGINE SHUTDOWN, THE CREW NOTICED A BURNING ODOR WHEN EXISTING THE AIRCRAFT AND SAW SMOKING COMING FROM THE NR 1 NACELLE. WHEN THE NACELLE WAS OPENED, IT WAS DETERMINED THAT AN EXTERNAL ENGINE FIRE HAD OCCURRED. DURING THE SHUTDOWN, NO FIRE INDICATION WASDR JIKA2016111601Engine · malfunctionedDEPARTED WAS NORMAL. PASSING THROUGH 1000AGL, RT ENGINE QUIT. NO INDICATION, TORQUE READ 0%, AND LATER TORQUE INCREASED BACK TO 60% & BACK TO 0%. QRH FOLLOWED AND SECURED RT ENGINE. DECLARED AN EMERGENCY, RETURNED TO DEPARTURE, & LANDED WITHOUT INCIDENT. SDR JIKA201609060001Governor · leakingTHE PILOT WAS EN-ROUTE AND WAS ACQUIRING TEND MONITORING DATA AND NOTICED THAT THE RT ENGINE HAD EXCESSIVELY HIGH OIL TEMPERATURE. THE PILOT FOLLOWED THE ABNORMAL PROCEDURES CHECKLIST AND PERFORMED AN IN-FLIGHT SHUTDOWN OF THE RT ENGINE. HE RETURNED TO DEPARSDR JIKA2016090301Sensor · frozenENROUTE, DISCOVERED THE LEFT ENGINE WAS UN-RESPONSIVE TO POWER LEVER MOVEMENT. FOLLOWED EMERGENCY PROCEDURES, AND SHUTDOWN THE LEFT ENGINE, DECLARING AN EMERGENCY, DIVERTED. AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT THE LEFT ENGINE POWER LEVER COSDR CA160224010Shaft · fractured(CAN) DURING A ROUTINE LANDING GEAR INSPECTION THE RT UPPER TORQUE LINK SHAFT WAS FOUND TO BE PROTRUDING FROM THE RT TORQUE LINK. THE SHAFT HAD FRACTURED INSIDE THE STRUT. PROTRUDING PORTION WAS APPROX 1 1/2` LONG. THE REMAINING PORTION OF THE SHAFT WAS REMOVESDR CA160203029Tube · split(CAN) WHILE PERFORMING AN GENERAL UNSCHEDULED ENGINE INSPECTION MAINTENANCE FOUND THE NR 1 ENGINE FUEL PRESSURE TRANSMITTER TUBE ASSEMBLY LEAKING FUEL ONTO THE ENGINE. CLOSER INSPECTION OF THE TUBE FOUND A SPLIT IN THE TUBE WALL APPROXIMATELY 0.180". LOCATION SDR KY7A20160122001Warning System · activatedPILOT REPORTED THAT AFTER LANDING, THE RT ENG OIL PRESS WARNING & RT GEN CAUTION LIGHTS ILLUMINATED. THE PILOT PULLED THE STOP & FEATHER CONTROL TO SHUT DOWN THE ENG. GND PERSONNEL REPORTED SOME SMOKE & TORCHING FROM THE ENG EXHAUST AFTER SHUTDOWN. THIS IS SDR CA160113003Scavenge Pump · failed(CAN) DURING FLIGHT THE PILOT NOTED THAT THE LT OIL PRESSURE INDICATION WAS FLUCTUATING. WHEN THE AIRCRAFT LANDED WITH NO ISSUES THERE WAS OIL NOTED ON THE GROUND BEHIND THE EXHAUST ON THE GROUND. THE MAINTENANCE DEPARTMENT WAS NOTIFIED OF THE ISSUE AND WHEN TSDR CA151222002Line · chafed(CAN) RIGHT HYDRAULIC FAILURE ALERT FOLLOWING FLAP RETRACTION. UPON SELECTING GEAR DOWN COMPLETE HYDRAULIC SYSTEM FAILURE. TOTAL SYSTEM PRESSURE WAS LOST. THE GEAR TOOK A LONGER THAN NORMAL TO EXTEND AND ALTERNATE GEAR DOWN WAS USED FOR HYDRAULIC LOCKS. NR 2 SDR CA151021008Impeller · damaged(CAN) ENGINE CAME INTO THE TURBINE SHOP FOR A ROUTINE 7000 HR CAM INSPECTION AND WHEN THE ENGINE WAS BEING DISMANTLED TO START THE INSPECTION OF THE ENGINE THE NR 2 IMPELLER WAS NOTICED TO HAVE A BROKEN BLADE ON IT.SDR JIKA2015081001Wire Harness · damagedEN-ROUTE THE PILOT NOTICED THE RT ENG EGT SPIKED 100 DEGREES CELSIUS, THE RT ENG FUEL BYPASS LIGHT ALSO ILLUMINATED. THE PILOT FOLLOWED THE EMER CHECKLIST & PERFORMED A PRECAUTIONARY RT ENG SHUTDOWN. DECLARED AN EMER & DIVERTED. THE PILOT LANDED WITHOUT FURSDR KY7A20150416001Disk · failedE2 SUFFERED UNCONTAINED ENG FAILURE ON CLIMB OUT. 2ND STAGE TURBINE DISK FAILED & WAS THROWN FROM THE ENG THROUGH THE LT & RT SIDES OF THE ENG. APPROX 1/4 OF THE 2ND STAGE TURBINE DISK PENETRATED THE CABIN & WAS FOUND ON THE CARGO FLOOR.SDR JIKA2015031001Wire · faultyDURING CRUISE FLIGHT, THE PILOT NOTICED THAT THE RT ENG OIL TEMP GAUGE WAS FLUCTUATING & READING ABOVE THE RED LINE. THE PILOT FOLLOWED THE PROCEDURES IN THE QRH & REDUCED POWER, OIL TEMP REMAINED ABOVE THE RED LINE. THE PILOT PERFORMED AN INFLIGHT SHUTDOWN SDR JIKA2015021801Bulb · faultyDURING CRUISE FLIGHT, THE PILOT NOTICED THE LT ENG OIL TEMP INDICATED ABOVE REDLINE, APPROX 110 DEGREES. THE PILOT ELECTED TO DIVERT BACK, DURING DESCENT THE OIL PRESS INDICATED IN THE YELLOW ARC, APPROX 65 PSI, AT THAT POINT PILOT DECIDED TO PERFORM A PRECAUSDR 2015FA0000031Oil System · lowAPPROXIMATLY 100 MILES FROM THE DESTINATION OF THE FLIGHT, THE PILOT NOTICED A OIL PRESSURE LOW CAUTION LIGHT FOR THE LT ENGINE. THE PILOT SECURED THE ENGINE AND FEATHERED THE PROPELLER, ACFT LANDED AT DESTINATION WITHOUT INCIDENT. MAINTENANCE FOUND THE ENGISDR CA150126003Bracket · cracked(CAN) DURING AN ENGINE REPLACEMENT INSTALL PROCESS, IT WAS FOUND THAT THE LH POWER LEVER WAS HITTING THE UPPER QUADRANT AND FOUND THAT THE ENGINE CONTROL CABLE SUPPORT BRACKET TO BE BROKEN OFF AND FREELY MOVING. THE BRACKET HAS REMOVED AND REPLACED. (TC# 20150SDR CA141126002Housing · damaged(CAN) ENGINE P-44016 WAS BROUGHT INTO THE TURBINE SHOP FOR ROUTINE OVERHAUL AND WHEN THE ENGINE WAS TAKEN APART THE COMPRESSOR HOUSING WAS DAMAGED IN THE AREA WERE THE NR 2 IMPELLER SITS AND RIDES IN. THIS AREA HAS A SPRAY METAL REPAIR THAT IS DONE TO BUILD UPSDR JIKA2014050201Engine · contaminatedDURING CRUISE, PILOT TURNED ON ENGINE DE-ICING SYS, RT ENGINE EGT EXCEEDED LIMITS & RT ENGINE FUEL BYPASS LIGHT ILLUMINATED. ENGINE REDUCED TO FLIGHT IDLE BUT RT ENGINE EGT NOT RESPONSIVE & RT ENGINE BYPASS LIGHT REMAINED. ENGINE SHUTDOWN, DECLARED AN EMERGSDR CA140331003Pulley · noisy(CAN) THE FLIGHT CREW REPORTED ROUGHNESS IN CONTROL COLUMN IN FULL NOSE UP CONFIGURATION. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NOISE IN TAIL IN THE FULL NOISE UP CONFIGURATION. MAINTENANCE FOUND A CABLE OFF THE PULLEY, FWD ELEVATOR DOWN SPRINSDR CA140226005Smoke Detector · failed(CAN) LAV FIRE LIGHT ILLUMINATED ON TAXI PRIOR TO TAKEOFF. UPON ENGINE SHUTDOWN LIGHT EXTINGUISHED AND ILLUMINATED UPON RESTART OF ENGINES. REMOVED LAV DETECTOR CAUSING FALSE FIRE INDICATION AS IT WAS NOT REQUIRED FOR CURRENT ACFT CONFIGURATION.SDR MCCA2014011300017Engine · flamed outDURING APPROACH, TURNED ON THE ENGINE INTAKE HEAT. RT ENGINE THEN INGESTED ICE AND FLAMED OUT. PILOT WENT AROUND, RESTARTED ENGINE AND LANDED WITHOUT FURTHER INCIDENT.SDR FAA20140131003468Bearing · mismanufacturedSCHEDULED SOAP SAMPLE REVEALED MINOR SILVER PLATELETS. REMOVED COMPRESSOR BEARING AND NOTED SILVER COATING ON BEARING CAGE TO BE PEELING AND BUBBLING. BEARING WAS INSTALLED ON 10/26/2012 AND WAS REMOVED ON 1/3/2014. MANUFACTURER`S DEFECT ON SILVER PLATING. SDR CA131211002Fcu · unresponsive(CAN) ENGINE WAS STARTED, YET WHEN POWER LEVERS WERE MOVED FORWARD TO TAXI THE LT ENGINE WAS UNRESPONSIVE. ACFT WAS RETURNED TO MAINTENANCE AND AFTER TROUBLESHOOTING WAS CARRIED OUT THE DRIVE BETWEEN THE FUEL PUMP AND FCU WAS FOUND TWISTED AND THE VESPAL SPLISDR CA130812006Line · cracked(CAN) FLIGHT CREW SNAGGED HYD SIGHT GLASS EMPTY AND NO FLAP MOVEMENT WHILE SPOOLING ENGINE, LOCATED AND REPLACED CRACKED HYD LINE UNDER RT CABIN FLOORBOARD JUST FORWARD OF MAIN SPAR. LEAK CHECKED AND ACFT RETURNED TO SERVICE.SDR 4CIA2013F00156Indicator · reads highENGINE OIL PRESSURE INDICATED HIGH ON THE DESCEND PHASE OF FLIGHT, PASS THE UPPER RED LINE OF THE OIL PRESSURE GAUGE.SDR CA130703006Line · leaking(CAN) AIRCRAFT WAS IN CRUISE WHEN THE CREW NOTICED 2 ENGINE LOW HYDRAULIC PRESSURE LIGHTS ILLUMINATED ALONG WITH A DROP ON THE HYDR SYS PRESSURE INDICATOR, THEY ALSO REPORTED A WHINING SOUND COMING FROM THE CENTER SECTION OF THE ACFT. THE ACFT HAD EXPERIENCED SDR CA130624003Mixing Valve · damaged(CAN) DURING INVESTIGATION INTO PILOT REPORTED DEFECT, FULL COLD SELECTED, LT SIDE HOT, MAINTENANCE PERFORMED A FUNCTIONAL CHECK OF THE MIXING VALVE AND FOUND THE BUTTERFLY VALVE TO BE STAYING IN THE OPEN POSITION WHEN SELECTED CLOSED. VALVE ASSY REMOVED. THSDR CA130527009Bulkhead · cracked(CAN) CREW REPORTED MAX DIFF AT 5.0. UPON INSPECTION IT WAS FOUND THAT THE FORWARD PRESSURE BULKHEAD HAD LARGE CRACKS ON LT & RT SIDES JUST BELOW W.L 100.00.SDR CA130527010Bulkhead · cracked(CAN) CREW REPORTED MAX DIFF AT 5.0. UPON INSPECTION IT WAS FOUND THAT THE FORWARD PRESSURE BULKHEAD HAD LARGE CRACKS ON LH & RH SIDES JUST BELOW W.L 100.00.SDR CA130515014Terminal · burned(CAN) FLIGHT RETURNED AFTER TAKEOFF DUE TO BURNING ODOR IN COCKPIT. FOUND TRANSISTOR AND WIRING AT RELAY K61 TERMINALS, IN THE EP9 LT CONSOLE, BURNED AND BLACKENED. RELAY REPLACED.SDR JIKA2013042701Engine · failedDURING CRUISE AT 16000 FT, THE PILOT GOT A R CHIP DETECT LIGHT. WHILE MONITORING THE ENGINE THE TORQUE INDICATION FLUCTUATED, AND THE ENGINE FAILED. DECLARED AN EMERGENCY AND DIVERTED. REVIEW OF THE ENGINE TEAR DOWN REPORT REVEALED THAT THE PROBABLE CAUSE
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