Garrett TFE731-5BR
Service difficulty reports · 328
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 = 'TFE7315BR' 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 = 'TFE7315BR' 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 2003FA0000026Line · crackedDURING CRUISE FLIGHT, NR 2 OIL LIGHT ON MASTER WARNING PANEL CAME ON. POWER LEVER WAS REDUCED TO IDLE, OIL PRESSURE INDICATION CONTINUED TO FALL TO LESS THAN 25 PSI, THIS TOOK APPROXIMATELY 15-20 SECONDS. CHECKLIST WAS CALLED, NR 2 ENGINE WAS SHUT DOWN. CREW SDR AUS20020872Roller · worn(AUS) LEADING EDGE SLAT ROLLERS WORN.SDR AUS20020659Display · faulty(AUS) ADVISORY DISPLAY FROZE. AIRCRAFT IS RAAF FALCON 900 A26-077.SDR AUS20020660Transmitter · faulty(AUS) RT ANGLE OF ATTACK TRANSMITTER FAULTY. INVESTIGATION FOUND THAT THE INTERNAL POTENTIOMETER WAS OPEN CIRCUITED. AIRCRAFT IS A RAAF FALCON 900 A26-076.SDR AUS20020862Acm · leaking(AUS) TURBOCOOLER LEAKING OIL. SUSPECT CAUSED BY INTERNAL SEAL FAILURE.SDR AUS20020662Controller · faulty(AUS) ATC CONTROLLER FAULTY. INVESTIGATION FOUND THE CONTROLLER HAD ANUNSERVICEABLE PHOTOELECTRIC CELL. AIRCRAFT IS AN RAAF FALCON 900A26-070.SDR AUS20020661Transmitter · faulty(AUS) RT ANGLE OF ATTACK TRANSMITTER FAULTY. INVESTIGATION FOUND THAT THE INTERNAL POTENTIOMETER WAS SHORT CIRCUITED. AIRCRAFT IS A RAAF FALCON 900 A26-073.SDR 2002FA0000587Retainer · brokenUPON AIRCRAFT ARRIVAL AND SUBSEQUENT SHUTDOWN, MECHANICS HEARD A SCRAPING AND A THUNKING SOUND FROM THE NR 1 ENGINE AS THE ENGINE WAS SPOOLING DOWN. WHEN THE FAN ASSY WAS TURNED BY HAND, THE SAME NOISES CAN BE HEARD AND FELT. INSPECTION OF THE OIL FILTER REVSDR EYK2002F00000Transfer Tube · crackedON APPROACH, THE RIGHT ENGINE OIL PRESSURE STARTED TO DROP. OIL TEMP WAS NORMAL. ENGINE WAS SHUT DOWN BY CREW WHEN OIL PRESSURE DROPPED TO 20PSI. TOUCHDOWN AND ROLL-OUT, UNEVENTFUL. INSPECTED, FOUND OIL TRANSFER TUBE CRACKED AT FLARE. REMOVED AND REPLACEDSDR 2002FA0000397Tube · crackedON APPROACH PBI, THE RIGHT ENGINE OIL PRESSURE STARTED TO DROP, OIL TEMP WAS NORMAL. ENGINE WAS SHUTDOWN BY CREW WHEN OIL PRESSURE DROPPED TO 20 PSI. TOUCH DOWN AND DROPPED TO 20 PSI. TOUCH DOWN AND ROLLOUT WAS UNEVENTFUL. FOUND OIL TRANSFER TUBE CRACKED ASDR EYK2002F00001Transfer Tube · crackedON APPROACH PBI, THE RIGHT ENGINE OIL PRESSURE STARTED TO DROP, OIL TEMPERATURE WAS NORMAL. ENGINE WAS SHUTDOWN BY CREW WHEN OIL PRESSURE DROPPED TO 20 PSI. TOUCH DOWN AND ROLLOUT WAS UNEVENTFUL. MADE INVESTIGATION. FOUND OIL TRANSFER TUBE CRACKED AT FLARE.SDR EYK2002F00002Transfer Tube · crackedON APPROACH PBI, THE RIGHT ENGINE OIL PRESSURE STARTED TO DROP. OIL TEMPERATURE WAS NORMAL. ENGINE WAS SHUTDOWN BY CREW WHEN OIL PRESSURE DROPPED TO 20 PSI. TOUCHDOWN AND ROLL OUT UNEVENTFUL. MADE INSPECTION, FOUND OIL TRANSFER TUBE CRACKED AT FLARE. REMOSDR CA020220010Starter Gen · failed(CAN) DURING START SEQUENCE, NR 2 ENGINE FAILED TO ROTATE, START SEQUENCE WAS CANCELLED, AND TRIED A SECOND TIME WITH NO ROTATION OF ENGINE. FAULT WAS TRACED TO THE STARTER GENERATOR, UNIT WAS REPLACED WITH A NEW AND START SEQUENCE WAS OK. NR 2 ENGINE STARTED SDR AUS20020072Stator · damaged(AUS) FOURTH STAGE LOW PRESSURE COMPRESSOR STATOR INNER RING FAULTY. RTV COMPOUND SEPARATED FROM THE STATOR AND WAS INGESTED INTO THE ENGINE. CONTAMINATION OF THIRD STAGE LPT BLADES.SDR 2002FA0000124Odor · detectedDURING CLIMB AT FL240, PILOTS NOTICED "BURNING" SMELL FOLLOWED BY A HUMMING SOUND FROM THE LEFT-HAND SIDE OF AIRCRAFT. PILOT ELECTED TO SHUTDOWN ENGINE.SDR CA011101019Bearing · vibration(CAN) DURING FLIGHT ON CLIMB A VIBRATION WAS NOTED. THEN DISAPPEARED AFTER WHILE ON CRUISE VIBRATION CAME BACK. ALSO GIVING OIL PRESSURE FLUCTUATION. AT DESTINATION, TROUBLESHOOTING WAS DONE, OIL PRESSURE WAS CHECKED "S". STARTER/GENERATOR REPLACED. VIBRATION SDR DXT2001F00002Tire · separatedGOODYEAR FLIGHT EAGLE PN 237K23-2, SN 10961491 FAILED ON TAKE-OFF. SEPARATED TREAD PENETRATED WING UPPER SURFACE, ALSO DAMAGED FUSELAGE SIDE FAIRING AND RIGHT ENGINE NACELLE. A BRAKE HYDRAULIC LINE WAS ALSO RUPTURED. CAUSE OF FAILURE UNKNOWN AT THIS TIME. SDR 2001FA0000351Cover · brokenWHEN REMOVING THE APU OIL FILTER COVER, THE RETAINING EARS THAT HOLD THE END OF THE COVER, THE RETAINING EARS THAT HOLD THE COVER IN PLACE BREAKS OFF. RECOMMEND MANUFACTURING A FILTER COVER WITH A HEX FITTING ON THE END OF THE COVER, IT WOULD MAKE IT EASIER TSDR RO462097Stator · separatedENGINE RETURNED FOR MAINTENANCE WHEN AIRCRAFT WAS EXPERIENCING ENGINE TEMPERATURE LIMIT AT TAKE OFF AND SUBSEQUENT HUNG STARTS. THE INNER HUB OF THE 4TH LOW COMPRESSOR STATOR WAS FOUND SEPARATED DURING ENGINE MAINTENANCE DISASSEMBLY. MAJOR ENGINE COMPONENT DSDR AUS20010653Clevis · cracked(AUS) MAIN ENTRY DOOR COMPENSATING SPRING CLEVIS CRACKED ACROSS ALL THREE CABLE ATTACHMENT LUGS. AIRCRAFT SERIAL NUMBER A26-074.FLEET INSPECTION FOUNDTHE CLEVIS CRACKED ON ALL OTHER AIRCRAFTIN THE RAAF FLEET. THIS DEFECT WAS RECEIVED FROM THE RAAF AND ISENTERESDR 20010510AP002Valve · contaminatedNR 1 TIRE FLAT SPOTTED, NR 2 TIRE FLAT SPOTTED AND DEFLATED, NR 3 TIRE FLAT SPOTTED. VISUAL INSPECTION FOUND NR 1 MODULATOR VALVE CONTAMINATED WITH PAINT CHIPS AND SHAVINGS OF PLASTIC. FOUND NR 2 MODULATOR VALVE PISTON O-RING DECOMPOSED/CONTAMINATED. REPLACEDSDR 20010510AP005Maxaret · inoperativeNR 1 AND 2 TIRES FOUND FLAT SPOTTED DURING POST-FLIGHT INSPECTION. NR 1 MAXARET UNIT DID NOT PASS ANTI-SKID FUNCTIONAL TEST. REPLACED NR 1 MAXARET UNIT WITH OVERHAULD UNIT.SDR 20000403SH007Retainer · brokenDISASSEMBLED ENGINE BECAUSE OF BAD S.O.A.P. SAMPLE. FOUND NR 3 SEAL RUNNER RETAINER BROKEN. (X)SDR AU000203009Power Supply · failed(AU) A NOISE WAS HEARD EMANATING FROM THE LT VALANCE LIGHTING. UPON INVESTIGATION, AN ELECTRICAL ARC WAS FOUND OCCURING BETWEEN 2 WIRES COMING OUT OF THE LIGHTING POWER SUPPLY.SDR CA000203009Power Supply · shorted(CAN) A NOISE WAS HEARD EMANATING FROM THE LT VALANCE LIGHTING. UPON INVESTIGATION, AN ELECTRICAL ARC WAS FOUND OCCURING BETWEEN 2 WIRES COMING OUT OF THE LIGHTING POWER SUPPLY.SDR 99ZZZX3323Disk · failedWHILE IN CRUISE AT FL 390, ENGINE BEGAN VIOLENT VIBRATION WITH INCREASE ITT. IF&D AND SAFE LANDING EXECUTED.SDR CA981207006Line · cracked(CAN) CRACK RUNNING THROUGH 50 PERCENT OF THE TUBE CIRCUMFERENCE AT THE INSIDE RADIUS RESULTED IN A LOSS OF PRESSURE TO THE WATER SYSTEM. REPLACED. PART TC: 2,109.SDR 96ZZZX3394Igniter · failedDURING ROUTINE MAINTENANCE, THE IGNITER FIRING TIP OF THE CENTER ELECTRODE WAS FOUND LOOSE. THE IGNITER IS AN EXTENDED LIFE IRIDIUM IGNITER. THIS WAS A NON-SERIALIZED IGNITER, BUT THE 'TST' INDICATES PREVIOUS SPECIAL TESTING FOR LOOSE CENTER ELECTRODE WAS CO
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