Garrett TFE731-2-1C
Service difficulty reports · 29
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 = 'TFE73121C' 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 = 'TFE73121C' 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 O2JA2020022100173Engine · failedWHILE FLYING AT FL 390 RIGHT FIRE LIGHT ILLUMINATED, FOLLOWED EMERGENCY CHECK LIST. WHEN ENGINE WAS PULLED TO IDLE, ENGINE STARTED MAKING LOUD BANGING NOSE UNTIL IT WAS SHUT DOWNSDR CA190913004Anti-Skid Valve · cracked(CAN) TROUBLESHOOTING A LEAKING LH MLG ANTI-SKID VALVE THE BODY WAS FOUND CRACKED.. UNIT WAS REPLACED WITH A SERVICEABLE UNIT. (TC# 20190913004)SDR 2CJA2018020700003Display · malfunctionedFLIGHT CREW REPORTED ONE HOUR FROM DESTINATION, DURING CRUISE, PILOT SIDE AIR SPEED DECREASING AND EVENTUALLY WENT TO ZERO. THE AUTO PILOT ALTITUDE HOLD STARTED TO HUNT UP AND DOWN AND OR - 200 FEET AND THE YOKE STARTED SHAKING RIGHT TO LEFT. CREW SHUT OFF TSDR CA151022002Fan · failed(CAN) DURING CRUISE, THE CREW NOTICED AND SMELLED SMOKE FROM THE GASPERS. SHUTOFF THE FANS AND THE SMOKE DISAPPEARED. THE ACFT LANDED WITH NO ISSUES. AFTER INSPECTION THE RT EVAPORATOR FAN WAS FOUND SEIZED AND SMELT BURNED. THE FAN WAS REPLACED WITH ANOTHER SDR CA140122008Hose · collapsed(CAN) DURING DESCENT, THE CREW NOTICED THAT THE LT INBD SLAT WAS NOT SHEDDING ICE. THE ANTI-ICE FLEX HOSE FOR THE LT INBD SLAT WAS REMOVED AND THE INNER LINING WAS FOUND TO BE DE-LAMINATED, RESTRICTING FLOW TO THE SLAT. UPON FURTHER INSPECTION, THE LEFT OTBD SSDR CA130515008Tire · damaged(CAN) DURING DAILY INSPECTION, A PIECE OF THREAD MISSING FROM NR 3 MAIN WHEEL TIRE WAS NOTICED.SDR CA130109009Hose · collapsed(CAN) DURING CRUISE FLIGHT, THE CREW NOTICED THAT THE LT INBD SLAT WAS NOT SHEDDING ICE. THE ANTI-ICE FLEX HOSE FOR THE LT INBD SLAT WAS REMOVED AND FOUND TO BE DELAMINATED IN SEVERAL AREAS OF THE INNER LINING.SDR SFOA20111201001Indicator · defectiveDURING CRUISE FLIGHT THE NR 1 ITT INDICATOR WENT TO ZERO. THE AIRCRAFT RETURNED TO HOME BASE WHERE AN UNEVENTFUL LANDING WAS MADE, DURING RETURN FLIGHT THE INDICATOR BEGAN TO WORK BUT WAS LOWER THAN NORMAL AND ERRATIC. THE GAUGE WAS PARTIALLY REMOVED FROM THSDR CA110607012Fcu · unserviceableACT WAS AT 35,000 FT WHEN THE CREW NOTICED THE NR 2 ENGINE WAS SHUTTING DOWN. THE WAS NO ANNUNCIATORS TO GIVE THE CREW NOTICE OF POSSIBLE FUEL LOSS. THE CREW DESCENDED TO 30,000 TO RE-LIGHT THE ENGINE. THEY STARTED THE ENGINE WITH NO ISSUES. AFTER INSP, NO FAUSDR SFOA20110317001Fuel Control · malfunctionedJUST PRIOR TO DESCENT TO SCHEDULED AIRPORT, THE LT ENGINE COMPUTER ANNUNCIATOR ILLUMINATED. FOLLOWING AFM PROCEDURES THE COMPUTER WAS RESET AND THE LIGHT WOULD NOT REMAIN EXTINGUISHED. ALL OTHER ENGINE INDICATIONS WERE NORMAL. A SAFE LANDING WAS MADE. THE SDR SFOA77N2MONOMonopole · faultyAFTER DEPARTURE FROM AIRPORT THE RT ENGINE COMPUTER ANNUNCIATOR ILLUMINATED. FOLLOWING AFM PROCEDURES THE COMPUTER WAS RESET AND THE LIGHT EXTINGUISHED. A SHORT TIME LATER THE ANNUNCIATOR ILLUMINATED AGAIN AND WAS AGAIN RESET. ALL OTHER ENGINE INDICATIONS WSDR 2010FA0000710Wheel · bentNOSE WHEEL AND TIRE SEPARATED FROM ACFT AFTER ROTATION AT APPROX 20 FEET IN AIR. PILOT HEARD A "THUD" AT ROTATION AND SUSPECT ENCOUNTER WITH FOD. WHEEL BENT ON ONE SIDE AND TIRE SIDEWALL HAD CORD SEPARATION DUE TO TIRE COMPRESSION.SDR CA091123001Hose · leaking(CAN) UPON DESCENT, PILOTS NOTICED THE HYD PRESSURE WAS AT 0. THEY DECLARED AN EMERGENCY, EXTENDED GEAR USING EMERGENCY AIR BOTTLE AND MADE A SUCCESSFUL LANDING. THERE WAS ENOUGH BRAKING PRESSURE USING STANDBY HYD PUMP, EMERGENCY BRAKES WERE NOT USED. DURING SDR MJN1Seal · wornCREW REPORTED SMOKE IN CABIN, FOLLOWED PROCEDURES TO CLEAR SMOKE AND ISOLATED POWER TO MEDICAL EUIPMENT BELIEVING THAT WAS THE SOURCE. NO ADDITIONAL SMOKE OR SMELL WAS OBSERVED. WHILE EN ROUTE TO MAINTENANCE FACILITY THE CREW REPORTED HEARING AND FEELING A LSDR CA070509003Signal Cond Unit · malfunctioned(CAN) IN FLIGHT, ON THE WAY BACK TO BASE THE CREW NOTICED THE RT FUEL GAUGE WAS INTERMITTENT AND NOT WORKING MOST OF THE TIME. THE DEFECTIVE PART WAS JUST REPLACED 7 HOURS PRIOR WITH THE SAME ISSUE. ANOTHER SIGNAL CONDITIONER HAS BEEN INSTALLED AND CALIBRATESDR CA060515006Fcu · inoperative(CAN) UPON RIGGING OF FCU, LOW IDLE STOPS ON THE THROTTLE QUADRANT WERE ADJUSTED TO ACHIEVE DESIRED 20 DEGREES ON THE FCU. THIS ADJUSTMENT WOULD NOT PHYSICALLY ALLOW THE QUADRANT TO DEPLOY THE THRUST REVERSERS. ENGINES WERE GROUND RUN AND FOUND TO BE SERVICESDR CA050603004Servo Valve · leaking(CAN) HYDRAULIC LEAK AT NOSE GEAR. HYDRAULIC SERVO VALVE FOUND LEAKING. VALVE REPLACED.SDR CA050608010Separator · making metal(CAN) DURING OIL CHANGE, METAL FOUND IN OIL AND FILTER. SOURCE OF METAL FOUND TO BE AIR/OIL SEPARATOR ALUMINUM LIGAMENTS. PART CHANGED AS PER SB TFE731-72-3696 TO NEWPART NUMBER 3075781-1.SDR CA050322009Flow Divider · leaking(CAN) DURING GROUND RUN, FUEL WAS OBSERVED TO BE LEAKING FROM THE RT AFT ENGINE AREA. THE PROBLEM WAS FOUND TO BE A LEAKING FUEL FLOW DIVIDER. THE PART WAS REPLACED, A SATISFACTORY GROUND RUN AND LEAK CHECK WAS CARRIED OUT AND THE AIRCRAFT WAS RETURNED TO SERVSDR 2004FA0000908Hose · collapsedDURING ENGINE RUN-UP, PHYSICALLY CHECKED LEADING EDGE FOR HEAT AND FOUND COLD. RT IB ANTI-ICE FLEXHOSE WAS REMOVED AND VISUALLY INSPECTED. FOUND THE INNER LINING HAD COLLAPSED, BLOCKING AIRFLOW THROUGH HOSE. HOSE WAS REPLACED WITH NEW. FAULTY HOSE WAS MARKSDR 2002FA0000690Turbine · damagedAFTER TAKEOFF AND DURING CLIMBOUT, THE PILOT EXPERIENCED A COMPUTER GENERATED AUTOMATIC ROLL BACK OF POWER ON THE NR 1 ENGINE. THE NR 2 ENGINE WAS BROUGHT BACK TO A MATCHING POWER SETTING. IT WAS THEN NOTICED THAT THE NR 1 ENGINE ITT WAS MORE THAN 100 DEGREESDR GLA2002F00000Bolt · backed outTAKEOFF, AC WAS CLIMBING THROUGH WHEN NR1 ENG CHIP DETECTOR/LOW PRES WARNING LIGHT ILLUMINATED. ENG WAS SHUT DOWN AND SAFE SINGLE ENG LANDING WAS MADE. INVESTIGATION REVEALED NR1 ENGINE OIL PUMP HAD RUPTURED AND FAN ASSY WOULD NOT ROTATE. ENG WAS REMOVED ANSDR CA020207001Squat Switch · contaminated(CAN) LOSS OF PRESSURIZATION AFTER TAKEOFF. RECTIFICATION: MOISTURE WAS FOUND ON THE LT LANDING GEAR SQUAT SWITCH 9G1. SUSPECT SQUAT SWITCH 9G1 WAS COLD SOAKED, CLEANED AND LUBED. PASSENGER OXYGEN MASK HAD NO OXYGEN FLOW. SYSTEM IS OPERATING IAW F10 MSDR SW15200110653Carbon Seal · failedTHE NR 5 CARBON SEAL COKED AND FAILED CAUSING OIL STARVATION ON THE NR 5 BEARING WHICH SUBSEQUENTLY FAILED. THE CARBON SEAL WAS INSTALLED.SDR CA000222005Engine · leaking(CAN) OIL PRESSURE FLUCTUATIONS EXPERIENCED, POWER WAS REDUCED BUT OIL WARNING CAME ON. CORRECTIVE ACTION WAS TAKEN TO SHUT ENGINE DOWN. OIL QUANTITY DOWN 4 QUARTS. REPORT TO FOLLOW. OIL LOSS WAS DUE TO BREATHER VALVE LEAK AND VIBRATIONS WERE EXPERIENCED DSDR 20000328SH014Seal · leakingENGINE EXPERIENCED HIGH GEARBOX PRESSURE AT TEST CELL AFTER ENGINE CORE REPAIR WITH NEW NR 4 AND NR NR 5 SEALS AND RUNNERS. (X)SDR 20000328SH015Seal · leakingENGINE EXPERIENCED HIGH GEARBOX PRESSURE AT TEST CELL AFTER ENGINE CORE REPAIR WITH NEW NR 4 AND AND NEW NR 5 SEALS AND RUNNERS. (X)SDR 20000328SH016Seal · leakingENGINE EXPERIENCED HIGH GEARBOX PRESSURE AT TEST CELL AFTER ENGINE CORE REPAIR WITH NEW NR 4 AND NR 5 SEALS AND RUNNERS. (X)SDR 20000328SH017Seal · leakingENGINE EXPERIENCED HIGH GEARBOX PRESSURE AT TEST CELL AFTER ENGINE CORE REPAIR WITH NEW NR 4 AND NEW NR 5 SEALS AND RUNNERS. (X)
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