Garrett TFE731 series
Service difficulty reports · 742
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 = 'TFE731' 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 = 'TFE731' 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 GMA2001F00001Wire · brokenIN SERVICE OF WIRE BUNDLE CAUSED THE SHIELDING TO BREAK, AND A WIRE TO BREAK AT THE AIRFRAME-TO-WIRE BUNDLE CLAMP. SERVICE LOOP DID NOT APPEAR TO BE OF SUFFICIENT SIZE TO ALLOW FOR THE NEEDED FLEXING OF THE WIRE BUNDLE. FORCE SENSOR DID NOT FUNCTION.SDR WIB2001F00001Seat · crackedBACKPLATE OF SEAT IS CRACKED AT THREE OF THE FOUR CORNERS OF THE HOLE WHERE THE SHOULDER STRAP INERTIA REEL MOUNTS. FOUND DURING INSPECTION.SDR BSY2001F00015Transmitter · faultyRIGHT ENGINE OIL PRESSURE RUNNING HIGH, OIL TEMPERATURE, RED LINE AT FLIGHT LEVEL 37,000. FOUND OIL PRESSURE TRANSMITTER 12 PSI HIGH, REMOVED AND REPLACED OIL PRESSURE TRANSMITTER OIL PRESSURE, CHECKS GOOD. COULD NOT DUPLICATE OIL TEMPERATURE PROBLEM.SDR E272001F00000Contactor · wrong partAIRCRAFT FOUND TO HAVE START CONTACTOR PN A703FSS INSTALLED IN PLACE OF BATTERY CONTACTOR PN A770RSS. PILOT REPORTED LOSS OF NR 1 AND NR 2 BATTERY CONTACTORS IN FLIGHT. (INSTALLED BY MANUFACTURER)SDR BAQ2001F00001Hydraulic Line · looseSCHEDULED LANDING GEAR HOSE CHANGE PERFORMED 15.5 HOURS EARLIER. AIRCRAFT WAS EN ROUTE, ABOUT 1.5 HOURS INTO FLIGHT, HYDRAULIC PRESSURE DROPPED TO 1000 PSI. AFTER 20 MINUTES, PRESSURE DROPPED TO ZERO. PILOT ELECTED TO DIVERT AND AN EVENTFUL LANDING WAS MADESDR 2001FA0000272Landing Light · damagedRECEIVED THIS PART FROM CESSNA WITH UNDAMAGED PACKING. THE GROUND LUG WAS BENT, LOOSE AND HAD DAMAGED THREADS. THIS PART WAS PROPERLY PACKED WITH SPRAYED IN FOAM. THIS PART WAS DAMAGED PRIOR TO BEING PLACED IN THE BOX.SDR BSY2001F00013Engine · leaking(ATL) IN ROUTE FROM (BNA) TO (ATL) LOST OIL PRESSURE, RIGHT ENGINE. SHUT ENGINE DOWN LANDED AT (ATL). HAD GARRETT FROM AUGUSTA LOOK AT ENGINE, HAS MAJOR OIL LEAK. REMOVED ENGINE FOR REPAIR AT AUGUSTA.SDR GLA2001F00000Sliding Window · crackedAFTER APPROXIMATELY 1 HOUR INTO THE FLIGHT, THE PILOT NOTICED NUMEROUS SMALL CRACKS IN THE LEFT SLIDING WINDOW. CRACKS WERE LOCATED IN THE UPPER LEFT HAND CORNER OF THE SLIDING WINDOW. THE AIRCRAFT RETURNED TO BASE AND AFTER LANDING, CLOSER EXAMINATION REVEASDR UG82001F00003Printed Ckt Board · defectiveNR 2 COMM INOPERATIVE. REPLACED STRAPPING PC CARD ON NR 2 COMM UNIT, OPERATION NORMAL CHECKED 1 & 2 TRANSPONDERS.SDR UG82001F00004Relay · stuckRIGHT ENGINE STARTER WOULD NOT DISENGAGE. STUCK START RELAY. REMOVED AND REPLACED START RELAY.SDR CA010813003Battery · overheated(CAN) DURING CRUISE NR 2 BATTERY OVERHEAT INDICATED IN COCKPIT, CREW DIVERTED TO CYXU, BATTERY WAS REPLACED WITH SERVICABLE UNIT AND AIRCRAFT PROCEEDED WITH NO ADDITIONAL FAULTS. FAULTY BATTERY WAS FORWARDED FOR REPAIR/DEEP CYCLE.SDR 2001FA0000348Bearing · failedAIRCRAFT EXPERIENCED RIGHT GENERATOR FAILURE. GENERATOR LINE CONTACTOR FAILED TO OPEN AUTOMATICLY AND CREW WAS UNABLE TO SELECT GENERATOR OFF. RIGHT AIRCRAFT MAIN POWER BUSS EXPERIENCED SPIKING WHICH RESULTED IN DAMAGING 3 OR THE MAIN POWER DISTRIBUTION PANESDR JGV2001F00010Window · chippedNR 2 RIGHT CABIN WINDOW WITH LOOSE CHIP ON EDGE. EDGE OF WINDOW WAS CHAFING ON A FUSELAGE RIVET. WINDOW IS CHIPPED BEYOND LIMITS.SDR JGV2001F00003Window · damagedLEFT NR 1,2,3,4, AND 5 WINDOWS AND RIGHT 1,2,3,4,5, AND 6 WINDOWS HAVE RAZOR BLADE SCRATCHES AT VARIOUS POINTS IN THE RADIUSED NON VIEWABLE AREA, THIS IS STRESS AREA OF WINDOW. ASSOCIATED WINDOW SEALS ARE CUT AS WELL. IT APPEARS THE WINDOWS WERE TRIMMED OF SSDR JGV2001F00004Window · damagedLEFT NR 1,2,3,4, AND 5 WINDOWS AND RIGHT NR1,2,3,4,5, AND 6 WINDOWS HAVE RAZOR BLADE SCRATCHES AT VARIOUS POINTS IN THE RADIUSED NON-VIEWABLE AREA, THIS IS A STRESS AREA OF THE WINDOW. THE ASSOCIATED WINDOW SEALS ARE CUT AS WELL. APPEARS THE WINDOWS WERE TRISDR JGV2001F00005Window · damagedLEFT NR 1,2,3,4, AND 5 WINDOWS AND RIGHT NR 1,2,3,4,5, AND 6 WINDOWS HAVE THE RAZOR BLADE SCRATCHES AT VARIOUS POINTS IN THE RADIUSED NON-VIEWABLE AREA, THIS IS A STRESS AREA OF THE WINDOW. THE ASSOCIATED WINDOW SEALS ARE CUT AS WELL. WINDOWS WERE TRIMMED OFSDR JGV2001F00006Window · damagedLEFT NR 1,2,3,4, AND 5 WINDOWS AND RIGHT NR 1,2,3,4,5, AND 6 WINDOWS HAVE RAZOR BLADE SCRATCHES AT VARIOUS POINTS IN THE RADIUSED NON-VIEWABLE AREA, THIS IS A STRESS AREA OF THE WINDOW. THE WINDOW SEALS ARE CUT AS WELL. THE WINDOWS WERE TRIMMED OF SEALANT (SSDR JGV2001F00007Window · damagedLEFT NR 1,2,3,4, AND 5 WINDOWS AND RIGHT NR 1,2,3,4,5, AND 6 WINDOWS HAVE RAZOR BLADE SCRATCHES AT VARIOUS POINTS IN THE RADIUSED NON-VIEWABLE AREA, THIS IS A STRESS ARE OF THE WINDOW. THE WINDOW SEALS ARE CUT AS WELL. IT APPEARS THE WINDOWS WERE TRIMMED OF SDR 2001FA0000687Bracket · brokenAFTER LANDING, THE CREW TRIED TO STOW THE THRUST REVERSER HAD A TRANSIT LIGHT ON IN THE COCKPIT. A VISUAL INSPECTION REVELED THE RIGHT THRUST REVERSER DOOR (PN C41B30212-39 SN 2287) HINGE ARM HAD BROKE BETWEEN THE LOWER HINGE BEARING AND THE DOOR. ALSO DAMASDR 20010504CW004Altimeter · out of toleranceWHEN CHECKING OUT STANDBY ALTIMETER, FOUND THAT IT WAS 50-60 FEET OUT OF LIMITS. RETURNED TO VENDOR.SDR MB5R055NAngle · crackedRIGHT MAIN LANDING GEAR OUTBOARD GEAR MOUNT SIDE BRACE TO WING ATTACHMENT ANGLE CRACKED. CRACK LOCATED AT THE AFT PORTION OF THE ANGLE EXTENDING ONE INCH FORWARD.SDR 20010430CW011Module · defectiveDURING A PREFLIGHT, NR 1 ALTIMETER C/B TRIPPED AND WOULD NOT RESET. AFTER TROUBLESHOOTING FOUND SDC MODULE DEFECTIVE WITH MOISTURE. THE TRIP WAS MOVET TO A LR55-119. REPLACED SDC MODULE, REPAIRED AVIONIC BOY SEDL. TESTED D/C FOUND OK.SDR 20010501CW010Block · inoperativeLANDING GEAR WOULD NOT RETRACT. COULD NOT DUPLICATE ON GROUND. CHANGED GEAR SELECTOR SWITCH AND JUNCTION BLOCK FOR PRECAUTIONARY MEASURES, OPS CHECKED GOOD.SDR 20010501CW011Selector Switch · inoperativeLANDING GEAR WOULD NOT RETRACT. COULD NOT DUPLICATE ON GROUND. CHANGED GEAR SELECTOR SWITCH AND JUNCTION BLOCK FOR PRECAUTIONARY MEASURES, OPS CHECKED GOOD.SDR 20010501CW012Engine · malfunctionedLEFT ENGINE CAUSING SMOKE IN CABIN. TROUBLE SHOT ENGINE TO NR 4 AND NR 5 CARBON SEALS. REMOVED AND REPLACED ENGINE.SDR 20010430CW010Controller · malfunctionedMODERATE LOSS OF PRESSURIZATION OCCURED AT FL330. THE CAUSE WAS OBVIOUSLY A MALFUNCTION OF THE CONTROLLERBECAUSE ONCE REPLACED THE AIRCRAFT OPERATED FINE.SDR AJC2002F00000Hinge · brokenLEFT MAIN LANDING GEAR DOOR SEPARATED DURING FLIGHT AT AFT GEAR DOOR HINGE PIN.SDR 2002FA0000264Solenoid · intermittentSPOILER OPERATION INTERMITTENT. MAINIFOLD ASSEMBLY HAS TWO SOLENOIDS, APPEARS THAT ONE MAY BE STICKING OR HAVE AN ELECTRICAL PROBLEM.SDR 27314101Pump · leakingOIL PUMP LEAKING THRU CASE DUE TO WORMING. REMOVED AND REPLACED PUMP.SDR 27314102Pump · leakingOIL PUMP LEAKING THRU CASE DUE TO WORMING. REMOVED AND REPLACED OIL PUMP.SDR 20010403CW004Starter Gen · destroyedAT FLIGHT LEVAL 390, CREW FELT A VIBRATION IN THE AIRCRAFT, AIRCRAFT DIVERTED. MAINTENANCE FOUND LEFT ENGINE STARTER GENERATOR DESTROYED. GENERATOR WAS REPLACED, GROUND CHECK NORMAL. THE GENERATOR CARRIES A TBO OF 1000 HOURS. THIS TIME IS RARELY ACHIEVED.SDR 20010413CW001Sensor · defectiveTEMPERATURE SENSOR CONNECTOR PINS FOUND TO BE RECESSED EXCESSIVELY. DEFECT FOUND DURING INSPECTION OF BATTERY. THIS CONDITION PROVIDES ONLY MINIMAL CONTACT BETWEEN MATING PINS.SDR DJFA200100012Oil Filter · misinstalledENGINE SHUTDOWN IN FLIGHT AFTER OIL PRESSURE INDICATION FLUCTUATION.SDR 20010403CW007Tire · failedA LANDING GEAR/WHEEL TYPE SPEED RELATED VIBRATION WAS REPORTED BY THE FLIGHT CREW. INVESTIGATION REVEALED A BUMPED OUT AREA OF TREAD ON THE RIGHT OUTBOARD MAIN TIRE. THE AREA WAS APPROX 9 INCHES LONG PLUS THE TIRE WIDTH OF THE TREAD AREA. THAT AREA WAS .18SDR 20010424CW012Turbine Blades · failedON LANDING ROLLOUT, CREW NOTICED, VIBRATION, TEMPERATURE, AND RPM FLUCTUATING. ENGINE SHUTDOWN DETERMINED, THIRD STAGE TURBINE BLADE FAILED.SDR 20010403CW015Skin · corrodedUPON REMOVAL OF GPS ANTENNA FROM AIRCRAFT, THE MATING SURFACE OF THE ANTENNA TO THE AIRCRAFT WAS RUSTING, CAUSING THE AIRCRAFT SKIN TO CORRODE. SUSPECT A VOID IN THE SEALANT AROUND BASE CAUSED MOISTURE TO GET UNDER ANTENNA AND CAUSE CORROSION. RECOMMEND CLOSDR 20010322CW010Bearing · failedUNIT REMOVED FOR SEVERE VIBRATION. DRIVE END BEARING HAD FAILED. BEARING RACE WAS RUSTED IN LINER OF END BELL AND COULD NOT FLOAT. RECOMMEND LUBRICATION ON BEARING RACE WHEN INSTALLED.SDR 20010403CW020Bearing · failedUNIT REMOVED BECAUSE OF EXCESS VIBRATION. ANIT DRIVE END BEARING HAD FAILED. THIS BEARING IS RETAINED AND DOES NOT MOVE. THE DRIVE END BEARING WHICH SHOULD FLOAT WAS RUSTED SOLID IN THE LINER BUT HAD NOT FAILED. BEARING SHOULD BE INSTALLED WITH LUBE ON RACSDR 20010320CW008Bulb · burned outON FINAL APPROACH, CREW NOTICED 1 LANDING LIGHT DOWNLOCK INOPERATIVE. PROCEEDED WITH CHECK LIST TO VERIFY GEAR DOWN AND LOCK. AFTER A FLY-BY THE TOWER, THEY CONDUCTED A VISUAL WITH NO CONSENSUS. REMOVED AND REPLACED LIGHT BULB. SYSTEM CHECKED OK.SDR 13001N71CKComputer · inoperativeLT ENGINE RPM ROLLED BACK 40 PERCENT DURING CLIMB, UNEVENTFULL LANDING ACCOMPLISHED. REPLACED LEFT ENGINE FUEL COMPUTER WITH SERVICEABLE UNIT. GROUND RUN AND FLIGHT TEST SATISFACTORYSDR 20010417CW008Retainer · wrong partUPON INSPECTION OF UNIT FOUND ALL THREE BATTERY CELL RETAINERS LOOSE. REMOVED RETAINERS AND FOUND BATTERY CELLS PHYSICALLY TOO SHORT TO MAKE PROPER CONTACT WITH BATTERY HOLDER TERMINALS. BATTERY CELL PART NUMBERS NOT FOUND. REPLACEMENT OF CELLS WITH PART NUSDR 20010417CW009Retainer · wrong partUPON INSPECTION UNIT FOUND ALL 2 CELL RETAINERS LOOSE. REMOVED RETAINERS AND FOUND BATTERY CELLS TOO SHORT TO MAKE PROPER CONTACE WITH BATTERY HOLDER TERMINALS. BATTERY CELL PART NUMBERS NOT FOUND. REPLACEMENT OF CELLS WITH PART NUMBER SPECIFIED IN MFG MANUSDR 20010417CW010Retainer · wrong partUPON INSPECTION FOUND ALL 3 CELLS UNAUTHORIZED. BATTERY CELL PART NUMBER NOT FOUND. REPLACEMENT OF CELLS WITH PART NUMBER SPECIFIED IN MFG MANUAL.SDR 20010305CW001Contactor · openWITH BATTERY SWITCH ON, NO START POWER. APPARENT CAUSE: NO DC POWER TO START POWER BUSS. CORRECTIVE ACTION: REPLACED GROUND POWER CONTRACTOR, OPERATIONAL CHECKED GOOD. AC RETURNED TO SERVICE.SDR G1FR100YHose · failedAFTER COMPLETING A MFG 1200 HR B INSPECTION, A MAINTENANCE GROUND RUN OPERATIONAL CK OF THE WING ANTI-ICE SYSTEM WAS REQUIRED AND ACCOMPLISHED. NO HEAT WAS NOTICED AT RT OUTBOARD SLAT WITH ANTI-ICE WINGS SELECTED AND GREEN OPERATIONAL LIGHT ILLUMINATED. FURTSDR AOQ2001F00000Clamp · looseAIRCRAFT WAS IN CRUISE AT FL 35000, WHEN CREW NOTICED THAT THE AIRCRAFT BEGAN TO GRADUALLY DEPRESSURIZE. THE CREW ELECTED TO DESCEND TO A LOWER ALTITUDE. DURING DESCENT CABIN PRESSURE DROP CAUSED THE AURAL WARNING HORN TO SOUND AND PAX OXYGEN MASKS TO DEPLOYSDR 20010212CW002Windshield · crackedAIRCRAFT DEPARTED CMI IN VFR CONDITIONS AND DURING CLIMB OUT THROUGH 15,000 FT, THE CO-PILOT''S FWD WINDSHIELD OUTER PANE CRACKED. PILOT ELECTED TO RETURN TO CMI. AIRCRAFT LANDED WITHOUT INCIDENT.SDR 20010419CW004Battery Pack · misinstalledBATTERY PACK ASSEMBLY HAS OTHER THAN ORIGINAL DATA PLATE INSTALLED, OTHER THAN ORIGINAL TOP AND BOTTOM COVERS INSTALLED APPEAR TO BE MAIN NICA CELL SHIMS; ROUND HEAD SCREWS IN CUNTER SUNK HOLES. OTHER THAN ORIGINAL TERMINAL POST, INSTALLED COUNTER SUNK SSDR 20010223CW004Actuator · failedNORMAL PITCH SYSTEM INOPERATIVE. AC WAS ON RAMP ALL NIGHT. DISCREPANCY FOUND BEFORE DEPARTURE. COLD AND DAMP WEATHER CONTRIBUTED TO ACTUATOR NOT WORKING. DURING REMOVAL AND INSTALLATION OF AN O/H ACTUATOR IN HANGER SYSTEM WORKED OK. NOTED: GREASE PLUGGINSDR 20010129CW012Wire · chafedPILOT REPORTED THAT IN FLIGHT, THE NOSE WHEEL STEERING SYSTEM DISARMS WHEN THE YAW DAMPER SYSTEM IS DISENGAGED USING THE AUTOPILOT/ NWS DISCONNECT SWITCH ON THE PILOT OR COPILOTS CONTROL WHEEL. THE TECH FOUND A CHAFFED STEERING SYSTEM WIRE SHORTING TO GROUND
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