Garrett TFE731-3A
Service difficulty reports · 33
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 = 'TFE7313A' 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 = 'TFE7313A' 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 2017F00178Flow Valve · faultyON DEPARTING KCXY "CABIN ALT" LIGHT ILLUMINATED PASSING THROUGH 10,000 FEET. CAPTAIN ELECTED TO LAND AT KMDT INSTEAD OF THE FILED DESTINATION (FXE).SDR 2016F00229Line · wornLOST HYDRAULIC FLUID. FOUND HYD LINE WORN.SDR G41A20160628002Wire · pulledON THE AFTERNOON OF 6-24-2016, ACFT DEPARTED, AT FL290, THE CAPTAIN NOTICED THE NR 2 ENGINE HAD STARTED A SLIGHT ROLLBACK ON THE N1 AND N2 INDICATORS. THEY ATTEMPTED TO CONTINUE TO THEIR CRUISING ALTITUDE, THE ROLLBACK CONTINUED AND GRADUALLY GOT WORSE. THE SDR G41A20160203001Filter · collapsedAFTER DEPART, CLIMBING THROUGH 34000', THE CAPTAIN NOTICED THE MASTER WARNING FLASHING, LT FUEL PRESS LIGHT FLASHED MOMENTARILY, WENT OUT & THEN CAME BACK ON. THE LT STANDBY PUMP WAS SWITCHED ON, ALL ENG INSTRUMENTS AT FIRST WERE INDICATING NORMAL. A FEW SECSDR 2015FA0000388Valve · leakingON DESCENT, THE CAPTAIN NOTICED THE OIL PRESSURE ON THE RT ENGINE, FLUCTUATING FROM NORMAL OPERATING PRESSURE OF 42PSI DOWN TO 25PSI. IT GRADUALLY DROPPED DOWN TO 20PSI AND HE THEN ELECTED TO SHUT THE ENGINE DOWN AND DECLARE AND EMERGENCY. THE ACFT WAS LANDESDR A8JA201506040021Indicator · faultyAT APPROX 0800 CST AT, TAXIED ACFT TO RUNWAY 12R FOR DEPARTURE. CREW SET THRUST ON ENGS & NOTICED NO N1 INDICATION ON NR 1 ENG. ALL OTHER INDICATIONS WERE NORMAL. ABORTED TAKEOFF & NOTIFIED TOWER IT WAS DUE TO GAUGE MALFUNCTION. TAXIED ACFT BACK TO CHOCKS SDR G41A20141126002Unknown · malfunctionedEN ROUTE, THE CAPTAIN EXPERIENCED THE RT & LT ADIS FAILING WITH FLAGS & NO USE FULL INFORMATION. AN EMER WAS DECLARED & THE CAPTAIN STARTED DESCENDING. DESCENDING THROUGH 4000FT, ALL NORMAL ADI INDICATIONS & FUNCTIONS RETURNED. THE ACFT SAFELY LANDED. AVIOSDR G41A2013F00113Turbine Blades · damagedSTARTING ENGINES PREPARING FOR DEPARTURE, NR 2 ENGINE RUNNING AFTER BEING STARTED WITH A POWER CART. CAPTAIN DECIDED TO TAXI OUT AND START NR 2 ENGINE. NR 2 STARTER ENGAGED, CAPTAIN NOTICED BATTERY VOLTS HAD DROPPED TO 19 VOLTS AND A HOT START WAS EMINENT. SDR G41A20130613002Connector · damagedDURING CLIMB, BETWEEN 150 AND 170, CABIN AREA BECAME UNCOMFORTABLY WARM. CREW NOTICED CABIN TEMPERATURE INDICATOR WAS INDICATING FULL HOT AND WOULD NOT MOVE IN AUTO MODE. TEMPERATURE CONTROL WAS MOVED TO MANUAL AND TEMP INDICATOR MOVED TOWARDS COOL. AFTERSDR BKEA2012F00041Landing Gear · inoperativeAFTER T/O, THE LANDING GEAR HANDLE WAS SELECTED TO THE UP POSITION AND LANDING GEAR FAILED TO RETRACT. PILOTS THEN PROCEDED TO RETURN TO DEPARTURE.SDR CA110816009Turbine · failed(CAN) AFTER ENGINE START THE PILOTS HEARD A STRANGE SOUND FROM THE NR 2 ENGINE AND IMMEDIATELY SHUTDOWN. MX CONTACTED MFG WHO INSTRUCTED THE PILOTS TO RUN THE ENGINE AND PERFORM A SERIES OF CHECKS. DURING THE RUN THE ACFT TEMPERATURE STARTED TO CLIMB TOWARDSSDR 2011F00143Warning Light · false activationDEPARTING, THE CAPTAIN REPORTED THAT AT ABOUT 60 KTS THE AMBER CABIN PRESSURE WARNING LIGHT ILLUMINATED, THE CAPTAIN DECIDED TO ABORT THE TAKEOFF. AFTER ROLLING CLEAR OF THE RUNWAY ONTO A TAXIWAY, HE SWITCHED THE CABIN AIR FROM ON TO OFF THEN BACK ON. THE CABSDR 2010FA0001007O-Ring · damaged(QFYR) O-RING PACKING FAILED ON THE LT MLG ACTUATOR SWIVEL FITTING ALLOWING HYDRAULIC FLUID TO LEAK OVERBOARD. THIS O-RING IS AT THE BASE OF THE SWIVEL FITTING. WHERE IT ATTACHES TO THE ACTUATOR. THE ACFT SPOILERS WHEN OPERATED OPENED AND THEN SLAMMED BACKSDR V6N2010F00000Engine · failedENROUTE, ACFT EXPERIENCED A LOUD BANG AND SHUDDER WITH SUBSEQUENT IMMEDIATE LOSS OF THE RT ENGINE. AIRCREW EXECUTED EMERGENCY PROCEDURES AND LANDED UNEVENTFULLY. SUBSEQUENT POSTFLIGHT INSP BY AIRCREW REVEALED THAT FAILURE WAS CONTAINED. TS LAST MPI 1158/ TSSDR OZCA11082009Valve · defectiveDURING A REPOSITIONING FLIGHT FROM FLL TO ORL AFTER DEPARTURE THE CAPTAIN NOTICED SMOKE FORMING IN THE CABIN AND RETURNED TO FLL FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE EMERGENCY PRESSURIZATION VALVE TO BE DEFECTIVE. THE USDR DELA200800001Oil System · lowDURING CLIMB DETECTED LIGHT SMOKE ODOR IN A/C. OIL PRESSURE LIGHT CAME ON IN FLIGHT CLIMBING THROUGHFL300, REMAINED ON FOR APPROX 1 MIN. ANALOG GAUGE SHOWED 25 PSI. PULLED POWER TO IDLE TO START S/D PROCEDURE AND EVENTUALLY OIL PRESSURE BECAME NORMAL. MONITORESDR DELR200800001Oil System · lowDURING CLIMB, SMELLED LIGHT SMOKE ODOR IN A/C. OIL PRESSURE LIGHT CAME ON IN FLIGHT CLIMBING THROUGH FL300, REMAINED ON FOR APPROX 1 MIN. ANALOG GAUGE SHOWED 25 PSI. PULLED POWER TO IDLE TO START S/D PROCEDURE AND EVENTUALLY OIL PRESSURE BECAME NORMAL. WAS MONSDR CA071212003Ring · incorrect(CAN) MODIFICATION OF LOCKING PIN SLOT OF ITEM (PN 152734). RING SUPPORT FOUND ON THIS STBY ALTIMETER (TC NR 20071212003).SDR 200700001Motor · sticksAMBER DUCT OVHT ANNUNCIATOR ILLUMINATED ABOVE FL300 APPROXIMATELY 20 MINUTES INTO FLIGHT. CREW NOTICED THAT THE CREW TEMP INDICATOR READ 4 ON THE SCALE WITH SYSTEM IN MANUAL AND TEMP CONTROL SELECTED TO FULL COLD. CREW INITIATED THE APPROPRIATE ABNORMAL CHECKLSDR DELA200600003Gasket · leakingCLIMBING THROUGH FL 300, THE FLIGHT CREW WITNESSED THE RT ENG FIRE WARN LIGHT ILLUMINATE. FOLLOWING CHECKLIST PROCEDURES, THE LIGHT WENT OUT AFTER 15-20 SECONDS, AND REMAINED OUT. AN UNSCHEDULED LANDING WAS MADE AT THE DEPARTURE AIRPORT. INSPECTION BY MAINTENSDR MJF33006Fire Detector · shortedLEFT ENGINE FIRE WARNING LIGHT LIGHT CAME ON DURING DESCENT AT 17,000 FT TO HPN.SDR 2006FA0000249Gasket · leakingPILOT O2 MASK HAD ORIGINAL O/H DATE OF 6/05. MASK WAS PLACED IN SERVICE IN AC 55093. MASK DID NOT TEST PROPERLY AT DELIVERY DATE OF 6/23/05. MASK WAS SENT BACK, FOUND TO HAVE A LEAK. MASK WAS REPAIRED AND SENT BACK TO AC. MASK WAS FOUND TO BE LEAKING AGAISDR DEL2005F00000Tire · failedNOSE TIRE FAILED ON TAKEOFF RUN. REPLACED NOSE TIRE (WHEEL ASSY WITH NEW TIRE AND OVERHAULED WHEEL ASSY. (K)SDR 2005FA0001263Windshield · delaminatedWINDSHIELD HAS CONSIDERABLE DELAMINATIONS AT AREA BELOW DEFOG NOZZLE. DIMENSIONS OF AREA 3.5 INCH X 2 INCH. DEPTH OF DELAMINATIONS UP TO .125. THIS IS NOT THE FIRST WINDSHIELD FOUND IN THIS CONDITION. PROBABLE CAUSE IS ALCOHOL GETTING BETWEEN THE WINDSHIELSDR DELA20040002Motor · stuckDURING DESCENT, THE CABIN TEMPERATURE CLIMBED TO AN UNCOMFORTABLE LEVEL. USE OF MANUAL CABIN TEMPERATURE MODE DID NOT CORRECT THE PROBLEM. T/S REVEALED THAT THE CABIN TEMPERATURE CONTROL VALVE TORQUE MOTOR WAS STUCK. REMOVAL AND REPLACEMENT OF THE TORQUE MOTOSDR BAQ2004F00002Heat Exchanger · cloggedTHE COOLING FINS WERE COMPLETELY OBSTRUCTED WITH OIL, DUST, FILM. YOU CAN NOT GAIN ACCESS OF THE COMPONENT, SHORT OF REMOVING IT FROM THE SYSTEM.SDR CA030424004Duct · cracked(CAN) DURING A 1000 HR INSPECT, AFT BAGGAGE COMPARTMENT INTERIOR WAS REMOVED, ALLOWING INSPECTION ACCESS TO THE RAM AIR DUCT. THIS PLASTIC DUCT IS LOCATED ON THE RIGHT HAND SIDE TUCKED TIGHTLY AGAI NST THE FUSELAGE SKIN AT STA 350. DURING INSPECTION, A 10 INCHSDR CA020612007Stator · separated(CAN) AFTER TAKEOFF AT APPROXIMATELY 3,000 FT ASL EXPERIENCED A VIBRATION AND NOISE FROM THE RT ENGINE. THE POWER LEVER WAS RETARDED TO IDLE AND ALL VIBRATION AND NOISE DISAPPEARED, AND ENGINE INDICATIONS WHERE WITHIN LIMITS AT THIS TIME. REQUESTED VECTORS BACSDR DJFA20020208Engine · failedDURING DESCENT, THE AIRCRAFT SHOOK FOLLOWED BY A NR 2 ENGINE CHIP DETECTOR LIGHT ILLUMINATION. ENGINE WAS SHUT DOWN AND AN UNEVENTFUL LANDING WAS MADE. UPON VISUAL EXAMINATION, THERE WERE NO EXTERNAL OIL LEAKS, THE OIL RESERVOIR WAS FOUND FULL AND THE FAN WASDR DIN2001F00001Retainer · brokenENG WOULD NOT START. INVESTIGATION FOUND ACCESSORIES AND STARTER MOTOR WOULD TURN BUT ENGINE N1 AND N2 ROTORS DID NOT. FOUND HORIZ DR SHAFT (PN 3070201-11) HAD UNCOUPLED FROM ACCY GEARBOX DUE TO RETAINER RING (M27426-3116A) BECOMING UNLOCKED AND ALLOWING MOVSDR DIN2001F00002Retainer · brokenDURING FLIGHT, LEFT HAND ENGINE EXPERIENCED UNCOMMANDED SHUTDOWN. INVESTIGATION FOUND HORIZONTAL DRIVE SHAFT (PN 3070201-11) HAD UNCOUPLED FROM THE ACCESSORY GEARBOX DUE TO RETAINER RING (M27426-8116A) BREAKING ALLOWING MOVEMENT OF THE SHAFT TO OCCUR. PRIOR SDR 20010111SG010Blade · failedDURING LANDING ROLL-OUT, DURING REPOSITION, CREW NOTICED ENGINE VIBRATION. SHUT DOWN ENGINE DURING TAXI. TEAR DOWN DETERMINED 1ST STAGE LPT BLADE FAILURE. (M)SDR 97ZZZX2628Apr System · malfunctionAUXILIARY PERFORMANCE RESERVE (APR). WHEN SYSTEM IS 'ARMED' SYSTEM GOES STRAIGHT TO 'ON' WHEN N2'S ARE MATCHED.
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