Garrett TFE731-5R
Service difficulty reports · 108
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 = 'TFE7315R' 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 = 'TFE7315R' 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 DGCA0606022Bearing · wornLT ENGINE VIBRATION NOTICED, UPON INVESTIGATION, FOUND THE STARTER/GENERATOR BEARINGS GOING BAD.SDR SQJ2006F00000Wire · chafedEVERY TIME THE NAV LIGHTS WERE SELECTED THE NAV LIGHT CIRCUIT BRAKER WOULD OPEN. LT AND TAIL NAVE LIGHTS WOULD MOMENTARILY ILLUMINATE THEN EXTINGUISH, RT WOULD NEVER ILLUMINATE. TROUBLESHOT PROBLEM TO A CHAFED WIRE IN A CONDUIT BEHIND THE RT WING LEADING EDGSDR SQJ2006F00001Tube · brokenBLEED AIR TUBE (PN C46P181211) WAS REMOVED TO GAIN ACCESS TO PYLON. WHEN TUBE WAS REMOVED 2 PIECES OF CURLED METAL FOUND LODGED IN NACELLE ANTI-ICE SHUTOFF VALVE (PN 27441482). PIECES OF METAL WERE REMOVED W/O EFFORT. INSP WAS PERFORMED ON TUBE, FOUND WHENSDR CA051130009Wire Harness · failedON APPROACH WHEN GEAR SELECTED DOWN, GEAR UNSAFE LIGHT CAME ON, GEAR IN TRANSIT. GOT ALL (3) GREENS LEFT, RIGHT AND NOSE, BUT NOSE UNSAFE LIGHT REMAINED ON. DID FLY BY, TOWER REPORTED NOSE GEAR APPEARS TO BE DOWN. PILOTS CONFIRMED (3) GREENS FOR GEAR, IT WASDR CA051130010Bracket · unserviceableON APPROACH WITH FLAPS SELECTED TO 15 DEG STALL IDENT LIGHT CAME ON THE ANNUNCIATOR PANEL. ON INVESTIGATION FOUND FLAP OUTBD MICROSWITCH OFF THE CAM FROM SWITCH ASSY. FURTHER INVESTIGATION WAS CARRIED OUT AND FOUND THE OUTBD BRACKET BROKEN FOR SWT SUPPORT. SDR DJFA2005155Autopilot Sys · malfunctionedWHEN CREW SELECTED VERTICAL SPEED ON MODE CONTROL PANEL TO BEGIN DESCENT, AC BEGAN STEEP CLIMB, AIRSPEED INDICATOR WAS NEAR BARBER POLE. CONTROL COLUMN YOKE WAS PUSHED FWD TO REDUCE CLIMB. AC FOUGHT CREW BY TRIMMING AC FURTHER NOSE UP. CLIMB WAS REPORTED TSDR CA050225004Ahrs · failed(CAN) AHRS NR 2 FAILED ON TAKEOFF, CAUSING THE AUTOPILOT AND YAW DAMPENER TO FAIL. AHRS WAS RECENTLY OVERHAULED. ATTITUDE AND HEADING REFERENCE SYSTEM (AHRS).SDR CA050215010Sleeve · disconnected(CAN) UPON REACHING CRUISING ALTITUDE, THE AIRCRAFT STARTED LOSING PRESSURIZATION. THE CREW DONNED THEIR OXYGEN MASKS, AT WHICH TIME THERE WAS A TOTAL LOSS OF PRESSURIZATION. UPON RETURNING TO MAINTENANCE, FOUND THAT THE SLEEVE CONNECTING THE DUCT TO THE WATESDR CA050215011Control Cable · mislocated(CAN) ELEVATOR CABLE UNDER CO-PILOT SEAT SLIPPED OFF THE CABLE GUIDESDR CA050131008Nut · missing(CAN) AFTER ARRIVAL TO BASE OF OPERATIONS DURING A POST FLIGHT INSPECTION NR 2 MAIN WHEEL ASSY. A WHEEL TIE BOLT NUT WAS FOUND MISSING AND ANOTHER 180 DEGREES APART WAS FOUND SPLIT. WHEEL WAS CHANGED. THESE NUTS WERE INSTALLED NEW AS THAT IS OUR POLICY. MFSDR DXTA200500541Filter Element · cloggedLEFT ENG FUEL LOOKUP LIGHT ILLUMINATED ON TAKEOFF ROLL FOLLOWING APPLICATION OF TAKEOFF POWER. REMOVED AND REPLACED LT & RT ENGINE FUEL FILTERS USING CUSTOMER SUPPLIED FILTERS. RAN A/C AND CHECKED FOR LEAKS, NO LEAKS NOTED. OPS CHECK GOOD. WORK DONE IAW TFSDR 2005FA0000010Clamp · crackedTHE DEFECT IS A FATIGUE CRACK, CAUSED BY BEING OVERSTRESSED DUE TO LOAD LIMITS, POSSIBLE OVERTORQUED. MAYBE THIS PART SHOULD BE MADE STRONGER, TO HANDLE THE STRESS. THIS DEFECT WAS FOUND BY A PENETRANT INSPECTION. THE LOCKING NUT NEEDS TO BE REMOVED, IN THSDR DJFA2004033Oil Tank · leakingHOU - MAF TRIP ID NR 731960. CREW REPORTED THAT DURING APPROACH TO MAF THE NR 2 ENGINE OIL PRESSURE DROPPED TO 10 PSI. ENGINE WAS SHUT DOWN AND SECURED. AIRCRAFT LANDED WITH OUT FURTHER INCIDENT. MAINTENANCE DISCOVERED A SMALL PIN HOLE IN THE RIGHT ENGINE OIL SDR CA041116005Shaft · worn(CAN) UPON PERIODIC INSPECTION IT WAS NOTED THAT THERE WAS APPARENT CONTACT BETWEEN THE IB FLAP VANES ON BOTH LT AND RT ASSEMBLIES ONTO THE TORQUE SHAFT AND BEVEL HOUSING ASSY. THIS UNUSUAL CONTACT WAS DEDUCED TO OCCUR DURING FLIGHT LOADS AS THE CLEARANCE BETWSDR 2005FA0000162Compressor Wheel · damagedRECENTLY EXPERIENCED A PROBLEM WITH A RELATIVELY LOW TIME COMPRESSOR WHEEL. THIS NEW STYLE COMPRESSOR WHEEL IS A REPLACEMENT WHEEL TO SUPPORT AD NR20021502. THE WHEEL IN QUESTION LOST A LARGE INDUCER TIP THAT PENETRATED, AND CAME VERY CLOSE TO EXITING THE AISDR DJFA2004017Filter · blockedDURING TAKEOFF THE NR 2 ENGINE FUEL BYPASS LIGHT ILLUMINATED. ABORTED TAKEOFF AND RETURNED TO THE FBO. FUEL FILTER WAS REPLACED, LEAK CHECKED AND FOUND TO BE OK.SDR DJFA2004016Filter · blockedDURING TAKEOFF, THE NR 2 ENGINE FUEL BYPASS LIGHT ILLUMINATED. ABORTED TAKEOFF AND RETURNED TO THE FBO. FUEL FILTER WAS REPLACED, LEAK CHECKED AND FOUND TO BE OK.SDR DJFA2004015Cap · unsecureAFTER DEPARTURE FIVE MINUTES INTO THE CLIMB THE NR 1 ENGINE OIL PRESSURE STARTED TO FLUCTUATE. THE CREW LEVELED AT 270 FT AND THE OIL PRESSURE WAS SLOWLY GOING DOWN, THE OIL PRESSURE LIGHT FLICKERED ON AND OFF AND AT THAT POINT THE CREW DECIDED TO SHUTDOWN THSDR DJFA2004014Oil Cap · unsecureAFTER DEPARTURE FIVE MINUTES INTO THE CLIMB THE NR 1 ENGINE OIL PRESSURE STARTED TO FLUCTUATE. THE CREW LEVELED AT 270 FT AND THE OIL PRESSURE WAS SLOWLY GOING DOWN, THE OIL PRESSURE LIGHT FLICKERED ON AND OFF AND AT THAT POINT THE CREW DECIDED TO SHUT DOWN TSDR DJFA2004013Blade · brokenAT FLIGHT LEVEL 390 FT THE CREW HEARD A LOUD THUMP AND VIBRATION ON THE NR 2 ENGINE. ENGINE WAS SHUT DOWN AND AIRCRAFT LANDED AT DAL WITH NO FURTHER PROBLEMS. AFTER FURTHER INSPECTION IT WAS FOUND THAT THERE WERE SOME TURBINE BLADES MISSING. ENGINE WAS REMOSDR 2004F00147Bearing · failedPILOTS NOTICED VIBRATION ASSOCIATED WITH THE NR 1 ENGINE. TECHNICIAN LOCATED SOURCE OF VIBRATION AS NR 1 STARTER/GENERATOR. THIS UNIT HAD BEEN REMOVED AND REINSTALLED TWO WEEKS PRIOR TO VIBRATION AFTER REBRUSHING BY AN OUTSIDE FACILITY. UNIT ACCUMULATED 70 SDR 258160002Carbon Seal · damagedON DESCENT TO KBCT, ENGINE POWER WAS REDUCED TO IDLE. OIL PRESSURE ON NR 2 ENGINE DROPPED TO RED LINE. POWER INCREASED ON NR 2 ENGINE AND OIL PRESSURE INCREASED. FOUND NR 1 CARBON SEAL RUNNER RETAINER DAMAGED. REPLACED RETAINER AND CARBON SEAL WITH NEW. ISDR 258160001Oil Cap · misinstalledDURING CRUISE FLIGHT, NOTICED FLUCTUATION IN OIL PRESSURE INDICATION ON LT ENGINE. INITIATED PRECAUTIONARY SHUTDOWN AND PROCEEDED WITHOUT INCIDENT. MAINTENANCE OPENED LOWER COWL AND FOUND IB OIL TANK SERVICE CAP DISLODGED AND LAYING IN LOWER COWLING. INSTALSDR CA040202016Control Cable · binding(CAN) UPON FUNCTIONAL TEST OF LANDING GEAR RETRACTION, THE SECONDARY MECHANICAL NOSE GEAR INDICATOR WAS NOT INDICATING PROPER EXTENSION (PROTRUSION OF CABLE END). PROBLEM TRACED TO BINDING CABLE. EXAMINATION OF DEFECTIVE PART (REMOVAL OF CABLE FROM METAL JACSDR CA031125004Engine · malfunctioned(CAN) A/C CLIMBING THROUGH 10K, RT ENGINE SPOOLED DOWN. STILL TROUBLESHOOTING.SDR 800LL112403Engine · vibrationVIBRATION FELT DURING FLT FROM REAR OF AC. ALL ENG INDICATIONS NORMAL. PASSING AC REPORTED WITNESSING SPARKS FROM REAR OF RT SIDE OF AC. UPON INITIAL INSP, METAL DEBRIS WAS NOTED IN LT ENGINE TAIL PIPE AREA. ENG MFG AND REPAIR FACILITY WERE CONTACTED FOR FSDR CA030807006Cooling Turbine · failed(CAN) POSSIBLE FAILURE OF BEARING (DEBRIS ON MAGNETIC PLUG) CAUSING SUBSEQUENT HIGH FREQUENCY VIBRATION RESULTING IN FAILURE OF THE FOLLOWING SUB-COMPONENTS: COOLING FAN (VANES BROKEN AND HOUSING PARTIALLY DETACHED. HEAT EXCHANGER 178092-1 (CRACKED AT WELDED SDR CA030110001Gearbox · leaking(CAN) LOW OIL PRESSURE INDICATION IN FLT ON LT, NR 1 ENGINE. PILOT SHUT DOWN NR 1 ENGINE AND CONDUCTED EMERGENCY LANDING. INITIAL VISUAL INSPECTION SHOWED OIL HAD SPEWED OVER COWLING. FURTHER INVESTIGATION LATER SHOWED EVIDENCE OF EXCESSIVE HIGH ENGINE GEARBOSDR CA020930006Duct · leaking(CAN) DUCT FROM WATER SEPERATOR SOCK IN AFT EQUIPMENT BAY DISCONNECTED FROM SEPERATOR. CABIN DEPRESSURIZEDAND AIRCRAFT DECENDED AND RETURNED TO BASE. DUCTS AND CLAMPS WERE INSPECTED AND AFTER RE-INSTALLATION AIRCRAFT WAS RUN TO MAX DIFF ON RAMP USING APU. NO SDR 2002FA0000991Seal · failedAFTER TAKEOFF, DURING CLIMBOUT, PILOT REPORTED AFT EQUIPMENT BYA OVERHEAT LIGHT ON MASTER CAUTION WARNING PANEL ILLUMINATED. RETURNED TO PLACE OF ORIGIN. AFTER TROUBLESHOOTING, FOUND DETERIORATED BLEED VALVE SEAL AT RIGHT ENGINE BLEED AIR SHUTOFF VALVE IN ASDR AUS20020449Adc · faulty(AUS) AIR DATA COMPUTER (ADC) FAULTY.SDR AUS20020448Gauge · faulty(AUS) ENGINE ITT GAUGE DIGITAL READOUT DIFFERENT TO ANALOGUE READOUT.SDR AUS20020521Engine · overtemp(AUS) NR 2 ENGINE ITT EXCEEDED LIMITS.SDR 2002F00985Control Cable · contaminatedPRECAUTIONARY SHUTDOWN OF LEFT ENGINE BECAUSE OF INABILITY TO REDUCE POWER FROM CRUISE. SUSPECT MOISTURE IN POWER CONTROL TELEFLEX CABLE ASSEMBLY FREEZING AT HIGH ALTITUDE. (M)SDR 2002FA0000270Blade · damaged3RD LPT BLADE SEPARATED AT MID-SPAN CAUSING DAMAGE BEYOND LIMITS TO 7EA 3RD LPT BLADES. ALSO DAMAGED THE EXHAUST NOZZLE AND 3RD LPT NOZZLE BEYOND LIMITS.SDR AUS20010900Indicator · failed(AUS) NR 1 ENGINE ITT INDICATOR INTERNAL FAILURE.SDR AUS20010899Transmitter · failed(AUS) NR 3 ENGINE OIL PRESSURE TRANSMITTER FAULTY.SDR UG82001F00000Pump · malfunctionedRIGHT ENGINE FUEL (PRESSURE) ANNUNICIATOR ILLUMINATED. ENGINE DRIVEN FUEL PUMP PERFORMANCE DEGRADING. REPLACED ENGINE DRIVEN FUEL PUMP WITH AN OVERHAULED UNIT.SDR AUS20011103Wheel · cracked(AUS) MAIN WHEEL INBOARD HALF CRACKED ADJACENT TO BRAKE TANG. FOUND DURING EDDY CURRENT INSPECTION.SDR ERYA258211Blade · brokenLEVEL CRUISE AT FL-390 VMC CONDITIONS. LOUD NOISE (BANG) FROM NR 1 ENGINE. N1 IMMEDIATELY DROPPED TO ABOUT 17 PERCENT. EMERGENCY WAS DECLARED, ENGINE SHUTDOWN CONDUCTED, AIRCRAFT WAS LANDED AT ELP. ENGINE IS BEING CHANGED. AT ENGINE DISASSEMBLY FOUND: 2NSDR 20010424CW008Seal · failedNR 4 RUNNER FAILED CAUSING DAMAGE TO NEARBY COMPONENTS.SDR 20010411CW002Bearing · failedFRONT END BEARING FAILED ON STARTER GENERATOR, IN FLIGHT.SDR 20010409CW010Blade · damaged3RD LPT BLADE SEPARATED AT MIDSPAN CAUSING DAMAGE BEYOND LIMITS TO ALL 3RD LPT BLADES. ALSO DAMAGED THE EXHAUST NOZZLE AND 3RD LPT NOZZLE BEYOND LIMITS.SDR CA010208013Battery · overheated(CAN) ENGINE ROTATION TOO SLOW AT START ATTEMPTS FOR SUCCESSFUL ENGINE LIGHT OFF. BATTERY VENTED EXCESSIVE AMOUNTS OF SMOKE AND VAPOR (STEAM AND ACID GAS) DUE TO SEVERAL SUCCESSIVE FAILED ENGINE START ATTEMPTS WITHOUT ALLOWING SUFFICIENT RECHARGING BY AIRCRSDR CA000328010Engine · failed(CAN) IN CRUISE, ENGINE FAILED. REPORT REQUIRED.SDR 20000328SH012Seal · leakingENGINE EXPERIENCED IN-FLIGHT SHUT DOWN BY HIGH GEARBOX PRESSURE WHICH EXPANDED OIL TANK AND CREATED HOLE IN OIL TANK AT A SPOT WELD DUE TO HIGH GEARBOX PRESSURE. ENGINE LOST OIL PRESSURE AND WAS SHUT DOWN BY PILOT. (X)SDR 99ZZZX4046Valve · failedAIRCRAFT RETURNED TO BASE AFTER NO REAR BAY OVERHEAT LIGHT ILLUMINATED. UPON INVESTIGATION, FOUND THE MIXING VALVE HAD SEPARATED AT THE FLANGE POINTED OUT IN THE ENCLOSED ILLUSTRATION. THE VALVE SEPARATION ALLOWED HP AIR TO LEAK, ILLUMINATING THE OVERHEAT WASDR 99ZZZX3382Deec · malfunctionedAIRCRAFT LEVEL FLIGHT - FL 350. ON ITS OWN, ENGINE WENT TO AN OVERSPEED CONDITION OF 105 PERCENT (103 PERCENT MAX ALLOWABLE). THROTTLE MOVEMENT HAD NO AFFECT. NORMAL THROTTLE CONTROL REGAINED ON DESCENT OUT OF FL 300. LANDING UNEVENTFUL. MANDATORY ENGINE OVSDR 99ZZZX1142Oil Tank · damagedAIRCRAFT TT: 4,375 HOURS. LANDINGS: 3,197. NORMAL PROCEDURES FOR REMOVING THE ALTERNATOR DID NOT WORK AS THE 0IL TANK HAD A BOW AT THE BOTTOM. THE TOP PART OF THE TANK HAD NORMAL CLEARANCES. AT THE TOP, THE NORMAL CLEARANCE IS THREE-FOURTHS OF AN INCH. SDR 99ZZZX876Housing · crackedHAIR LINE CRACK FOUND IN RADIUS OF OIL FILTER HOUSING.
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