Garrett TFE731-3
Service difficulty reports · 68
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 = 'TFE7313' 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 = 'TFE7313' 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 CA970624009Bearing · separated(CAN) ON ROUTINE ENGINE INSPECTION, METAL CONTAMINATION WAS FOUND IN OIL FILTER. ACCESSORY GEARBOX WAS OPENED AND METAL CONTAMINATE SOURCE WAS FOUND TO BE BEARING CAGES. ALL BEARINGS AND SEALS WERE REPLACED. THE AIR/OIL SEPARATOR IMPELLER AND DRIVE GEAR WERE RSDR 97ZZZX3730Splined Adapter · strippedWHEN ATTEMPTING TO START NR 2 ENGINE, STARTER SPUN, BUT ENGINE DID NOT ROTATE. FOUND THE SPLINED ADAPTER STRIPPED INSIDE OF GEARBOX. REPLACED SPLINE ADAPTER.SDR 97ZZZX1208Pump · failedFUEL PUMP WAS OVERHAULED BY CRS NR ZK3R027M ON 10-5-93. OVERHAUL REQUIREMENT IS 2000 HOURS. TIME SINCE OVERHAUL ON PART WAS 466 HOURS. PUMP WOULD NOT MAINTAIN PRESSURE WITH COLD FUEL. SUBMITTER STATED SEVERAL OPERATORS HAVE COMPLAINED ABOUT SIMILAR PROBLEMSSDR CA970225002Controller · failed(CAN) DURING CRUISE FLIGHT, THE LEFT HAND STABILIZER ANTI-ICE FAIL LIGHT ILLUMINATED. FLIGHT LANDED AND CONTROLLER WAS CHANGED.SDR VJ1R96003Plug · detachedENGINE COWLING WAS OPENED TO INVESTIGATE LOSS OF OIL. 'FOUND THE TRANSFER GEARBOX OIL JET CLEAN OUT PLUG (CHAPTER 72-60-03, FIG 1, ITEM 25) UNSEATED AND HANGING ON ITS MOUNTING STUD'. LUBE OIL WAS VENTED OVERBOARD ONCE THE PLUG WAS UNSEATED. (X)SDR 96ZZZM1077Eec · failedEN ROUTE FROM HOU TO APA WHILE CRUISING AT 35,000 FEET, THE LEFT ENGINE ROLLED BACK TO FLIGHT IDLE WITH NO PILOT INPUT. THE ENGINE WAS SWITCHED TO MANUAL MODE AND OPERATION WAS RESTORED TO NORMAL. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE ELECTRONIC ENGINE SDR CA960227014Oil System · depleted(CAN) L/H OIL PRESSURE DROPPED AND L/H LOW OIL PRESSURE LIGHT CAME ON. ENGINE SHUT DOWN, AND AIRCRAFT LANDED. FOUND LOWER COWL AND ENGINE SOAKED WITH OIL AND OIL TANK EMPTY. NO EVIDENCE OF OIL IN JET PIPE OR BYPASS DUCT. ENGINE AND COWL WASHED DOWN, AND OIL TSDR 95ZZZX6834Blade · failedFL 24,000 FEET CRUISE - LOUD BOOM NOISE OCCURRED WITH VIBRATION FOLLOWING. RIGHT ENGINE WAS PULLED BACK TO IDLE BY CREW WHICH CUT DOWN ON VIBRATION LEVEL. ENGINE WAS SHUT DOWN AS PRECAUTIONARY MEASURE.SDR 95ZZZX3942Seal · failedIN-FLIGHT SMOKE IN COCKPIT CAUSED BY FAILED NR 1 CARBON SEAL AND GEARBOX RELIEF VALVE, PN 3075323-2, OVER PRESSURE OF GEARBOX WITH FAILED NR 1 CARBON SEAL CAUSED OIL TO ENTER COMPRESSOR SECTION AND SMOKE IN BLEED AIR SYSTEM.SDR 95ZZZX3592Line · damagedLINE ASSEMBLY FOUND KINKED AT LOWER END. THIS PART IS AN ENGINE MAIN FUEL SUPPLY LINE (FLEXIBLE). THIS LINE MUST BE DISCONNECTED IN ORDER TO ALLOW CERTAIN DEFUELING OPERATIONS. CARE MUST BE EXERCISED WHEN DISCONNECTING THE LOWER FITTING; OTHERWISE, KINKING SDR 95ZZZX2940Blade · separatedSECOND STAGE L.P. BLADE SEPARATED IN STRESS RUPTURE, 4712 CYCLES. OCCURRED ON 1-31-95 IN-FLIGHT. REF: SB TFE 731-72-3556.SDR 95ZZZX2941Blade · failedOCCURRENCE 4-26-95. SECOND STAGE L.P. BLADE FAILURE IN-FLIGHT TO EWR. REF: SB TFE731-72-3556 STRESS RUPTURE.SDR 95ZZZX4452Line · crackedTHE CREW INDICATED THE LEFT ENGINE WOULD NOT MAKE POWER AT CRUISE ALTITUDE. UPON INVESTIGATION, FOUND THE P2T2 SENSE LINE WAS CRACKED AT THE PROBE. SUBMITTER RECOMMENDS THE LINE BE REPLACED WITH A SUITABLE FLEXIBLE LINE. THIS WILL ELIMINATE THE POSSIBILITY SDR 95ZZZX2831Filter Assy · o-ring crimpedABOUT 30 MINUTES BEFORE LANDING IN GRI, RT HYDRAULIC ANNUNCIATOR STARTED FLICKERING, ALL OTHER INDICATIONS NORMAL. AFTER PARKING AND WHEN SETTING THE PARKING BRAKES, BOTH HYDRAULIC ANNUNCIATORS CAME ON AND HYDRAULIC PRESSURE WAS LOST. A CRIMPED TEFLON O-RINGSDR 95ZZZX2309Engine · failedDAY/EWR - IN-FLIGHT SHUT DOWN 4-23-95, ENGINE EXPERIENCED INTERMITTENT VIBRATION AND ODOR EMISSION INTO CABIN. ABNORMAL N1 AND ITT READINGS INCREASED VIBRATION, PROMPTED SHUT DOWN WHILE DESCENDING INTO EWR AT 6,000 FEET. THE NR 1 ENGINE ON THIS AIRCRAFT HAD SDR 95ZZZX3091Bracket · brokenWHILE COWL OPENED FOR NON-RELATED MAINTENANCE, NOTED INBOARD ACCESSORY GEARBOX TO FAN SUPPORT STRUT HANGING LOOSE DUE TO BROKEN MOUNTING EARS ON GEARBOX STRUT ROD ATTACH BRACKET. WHILE REPLACING BRACKET AND ADJUSTING PER TFE 731-3 L.M.M. 72-60-01, NOTED SLIGHSDR 95ZZZX1000Blade · failureAN IN-FLIGHT SHUT DOWN OF NR 1 ENGINE OCCURRED ON 1-31-95 DURING FLIGHT FROM DAY TO ATW. AT 35,000 FEET, CREW HEARD AND FELT NOISE (THUMP) AND VIBRATION. THEY DETERMINED CAUSE TO BE NR 1 ENGINE AND IT WAS SHUT DOWN, VIBRATION CONTINUED UNTIL ACFT DESCENDED TSDR 95ZZZX897Fuel Control · defectiveENGINE WAS INSTALLED AFTER 4200 HOUR CORE INSPECTION. AFTER 2.6 HOURS OF OPERATION, THE PILOT EXPERIENCED SLUGGISH RESPONSE TO THROTTLE CHANGES. THIS WAS A PROBLEM IN TRAFFIC PATTERNS BECAUSE OF AIRCRAFT YAW WHEN POWER CHANGES RESULTED IN SLOW ENGINE RESPONS
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