Garrett TPE331-12UHR
Service difficulty reports · 287
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 = 'TPE33112UHR' 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 = 'TPE33112UHR' 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 CA081020006Bearing · damaged(CAN) UPON TAKEOFF THE CREW REPORTED THAT THE RT GEAR WOULD NOT REMAIN LOCKED. ACFT RETURNED TO BASE AND UPON MX INSPECTION IT WAS FOUND THAT THE UP-LOCK HOOK BEARING AND ATTACHING HARDWARE WERE MISSING. IT WAS ALSO NOTED THAT THE UP-LOCK HOOK SHAFT ATTACH POISDR CA080905004Wire · burned(CAN) RT AVIONICS AUX MASTER SWITCH WAS SELECTED ON AND SMOKE WAS NOTICED WITHIN 5 SECONDS. SWITCH WAS SELECTED OFF AND SMOKE STOPPED. NO OTHER ABNORMALITIES WERE NOTICED EXCEPT VISUAL BLACK DISCOLORATION ON F/O PHONE JACK OF HEADSET. THIS OCCURRED ON THE GROUSDR CA080819010Starter Gen · failed(CAN) UPON DESCENT, THE RT GENERATOR FAILED AND COULD NOT BE RESET. MAINT WAS CALLED UPON LANDING AND FOUND THE AFT PART OF THE STARTER GENERATOR HAD FAILED. REAR COVER WAS DESTROYED, REAR FAN BLADES WERE ALL BROKEN AND REAR BEARING WAS DESTROYED. UNIT REPLACESDR 2008FA0000470Clevis · brokenWHEN FLYING IN TO LAND, LANDING GEAR WAS SELECTED DOWN, RT MLG CAME DOWN ABOUT A FOOT AND STOPPED ON (2) ATTEMPTS, UPON (3RD) ATTEMPT GEAR CAME DOWN AND INDICATED LOCKED. AC WAS BROUGHT INTO OUR SHOP AND WHEN THE RT MLG WAS INSPECTED, IT WAS FOUND THAT CLEVISSDR CA080611009Bearing Seal · displaced(CAN) DURING A PREFLIGHT WALK AROUND OF THE ACFT THE INNER BEARING SEAL OF THE RT NOSE WHEEL ASSY WAS NOTED TO BE DISPLACED SO THAT ONE SIDE OF THE SEAL WAS RIDING UP ON THE HUB AND THE OPPOSITE SIDE WAS IN TOWARD THE AXLE TO THE EXTENT THAT THE BEARING ROLLERSDR CA080613007Transducer · damaged(CAN) PILOT REPORTED DEICE PRESSURE GAUGE UNSERVICEABLE. DURING TROUBLESHOOTING MAINT FOUND THE DEICE PRESSURE TRANSDUCER CONTAMINATED WITH WATER.SDR CA080606004Switch · intermittent(CAN) LT SAS FAILED AND ALL STAB TRIM FUNCTIONS FAILED. MASTER DISCONNECT SWITCH REPLACED AND TEST FLIGHT CARRIED OUT SERVICIBLE.SDR U2RA290LP3020Oil System · damagedRIGHT ENGINE OIL LIGHT ALONG WITH RED ATTENTION LIGHT ILLUMINATED DURING FLIGHT NOTED WITH A RAPID DROP IN INDICATED OIL PRESSURE ON RIGHT ENGINE. PRECAUTIONARY ENGINE SHUT DOWN WAS SATISFACTORILY INITIATED WITHOUT FURTHER INCIDENT AS PER COMPANY QRH BY THE FSDR CA080124006Line · chafed(CAN) LINE FOUND LEAKING BETWEEN OIL COOLER TO FUEL HEATER. THE CHAF WAS FOUND BY THE STEEL IDENTIFIER ON THE LINE. LINE WAS REPLACED AND AREA WAS CORRECTED SO THAT THE NEW LINE WOULD CHAF IN THE FUTURE (TC NR 20080124006)SDR CA080124007Line · chafed(CAN) LINE FOUND LEAKING BETWEEN OIL COOLER TO FUEL HEATER. THE CHAFE WAS FOUND BY THE STEEL IDENTIFIER ON THE LINE. LINE WAS REPLACED AND AREA WAS CORRECTED SO THAT THE NEW LINE WOULD NOT CHAFE IN THE FUTURE. (TC NR 20080124007)SDR CA080102008Module · damaged(CAN) DURING CLIMB-OUT THE PILOTS NOTICED THE ENGINE FIRE DETECTION INDICATION LIGHT CAME ON. THE ENGINE WAS SHUTDOWN AND THE ENGINE FIRE EXTINGUISHING BOTTLE WAS ACTIVATED. THE PILOTS DECLARED AN EMERGENCY, LANDED SAFELY AT THE AIRPORT OF ORIGIN AND EVACUATEDSDR CA071010009Accumulator · cracked(CAN) AIRCRAFT WAS INBOUND WHEN CREW REPORTED THE AIRCRAFT HAD LOST ALL HYDRAULIC PRESSURE. EMERGENCY GEAR EXTENSION WAS USED AND AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE DISCOVERED A 6 CENTIMETER CRACK LOCATED ON THE TOP SHOULDER AREA OF THE HYDRAULIC ACSDR CA071005004Bolt · missing(CAN) PILOT CALLED AND REPORTED THAT THE BOLT WAS MISSING FROM THE RT MLG TORQUE KNEE. MAINTENANCE INSPECTED TORQUE KNEE ASSEMBLY AND NO SECONDARY DAMAGE WAS NOTED. NEW BOLT WAS INSTALLED AND SECURED AND AIRCRAFT RETURNED OUT OF SERVICE. (TC NR 20071005004)SDR CA071001008Gps · failed(CAN) ON APPROACH, THE GPS430W UNITS INDICATED A DISTANCE OF 30 MILES WHICH THEN, SUDDENLY CHANGED TO AN INDICATED DISTANCE OF (2) TO (3) MILES CAUSING A LOSS OF CREW SITUATION AWARENESS. THE APPROACH WAS ABORTED. MFG WAS CONTACTED AND INFORMED OF THE PROBLEM.SDR CA070910008Fcu · malfunctioned(CAN) AFTER AIRCRAFT LANDED AND SPEED LEVERS WERE PULLED BACK INTO LOW IDLE THE RT ENGINE LIGHT CAME ON AT WHICH POINT THE CREW REALIZED THAT THE ENGINE HAD SHUTDOWN. THE FCU AND FUEL PUMP WERE REPLACED. AIRCRAFT CHECKED OUT SERVICIBLE AND NO FURTHER REPORTED SDR CA070827008Wire · damaged(CAN) AFTER AIRCRAFT LANDED AND WAS TAXING THE SPEED LEVERS WERE PULLED BACK INTO LOW IDLE THE RT ENGINE OIL LIGHT CAME ON AT WHICH POINT THE CREW REALIZED THE RT ENGINE HAD SHUT ITSELF DOWN. CREW CONTACTED MAINTENANCE. MAINTENANCE INVESTIGATED AND REPAIRED WISDR CA070606003Turbine Blades · failed(CAN) THE AIRCRAFT WAS ON A SHORT REPOSITIONING FLIGHT. AFTER AN UNEVENTFUL TAKEOFF AND CLIMB, THE CREW LEVELED AT 9,000 FT AND REDUCED POWER TO 30 PERCENT. FIVE MINUTES LATER, THE RT ENGINE HAD A VIOLENT AND SUDDEN VIBRATION. THE CREW SHUTDOWN THE ENGINE ISDR CA070612001Switch · malfunctioned(CAN) CREW REPORTED THE LT MAIN LANDING GEAR DOWN AND LOCK INDICATION WAS SHOWING (IN TRANSIT) WHEN SELECTED DOWN. THE SYSTEM WAS TROUBLESHOT TO THE DOWNLOCK INDICATOR SWITCH IN THE GEAR ACTUATOR. ACTUATOR REPLACED AND AIRCRAFT RETURNED TO SERVICE. (TC NR 2SDR CA070518008Fuel Cap · leaking(CAN) SHORTLY AFTER TAKEOFF, THE CREW NOTICED THAT FUEL WAS LEAKING FROM THE LT WING FUEL CAP. THE CREW RETURNED TO BASE WITHOUT INCIDENT. THE AIRCRAFT WAS INSPECTED AND IT WAS DISCOVERED THAT THE FUEL CAP WAS DEFECTIVE. THE LARGE PLASTIC NUT AT THE BASE OF SDR CA070507008Truss · cracked(CAN) DURING A PHASE 6 INSPECTION, A GAPING CRACK WAS FOUND ON THE RT ENGINE TRUSS MOUNT AT THE UPPER IB WELD JOINT OF THE FIREWALL ATTACH FITTING. (TC NR 20070507008)SDR CA070502015Exhaust Pipe · broken(CAN) ON CLIMB PILOTS EXPERIENCED TORQUE FLUCTUATIONS ON RT ENGINE. THEY RETURNED TO THE AIRPORT WITH NO FURTHER PROBLEMS. ON TAXI THEY BLEW THE FIRE BOTTLES ON THE RT ENGINE. WHEN MAINTENANCE REMOVED THE COWLS THEY DISCOVERED HEAT DAMAGE TO SOME WIRING. ON FSDR FJT07014871Bearing · failedTHE ACFT WAS ON APPROACH, TOWER REPORTED SMOKE COMING FROM THE LT ENGINE. THE ACFT LANDED WITHOUT INCIDENT. UPON INSP OF LT ENGINE, FOUND OIL LEAKING FROM REAR TURBINE BEARING HOUSING. SUSPECT REAR TURBINE BEARING SCAVENGE PUMP FAILURE AND SUBSEQUENT SEAL FSDR CA070219010Wire · damaged(CAN) CREW REPORTED THAT THE AIRCRAFT NR 2 ENGINE STARTED TO SURGE AND THE TORQUE INDICATION FLUCTUATED BETWEEN 0-120 PERCENT. TTL AND SRL COMPUTERS TURNED OFF AND ENGINE SURGE STABILIZED AND CONTINUED TO RUN NORMALLY. INDICATION CONTINUED TO FLUCTUATE. TROUBLSDR CA070126012Feeder Cable · loose(CAN) TOTAL LOSS OF CAPT`S RADIO COMMUNICATIONS. TROUBLESHOOTING FOUND MAIN POWER FEED CONNECTION NOT TIGHTEN ON TERMINAL BLOCK T5GA CAUSING CONNECTOR TERMINAL RING TO FLOAT AND REMOVE POWER SUPPLY TO CAPT`S AUDIO STATION BOX (TC NR 20070126012)SDR CA070111017Structure · unbonded(CAN) CREW REPORTED THAT WHEN THE AIRCRAFT ENTERED INTO A CLOUD, THE RADIOS BECAME UNREADABLE. ALL RADIO NAVIGATION EQUIPMENT BECAME UNRELIABLE AS WELL AS THE GPS SYSTEM. AIRCRAFT ARRIVED AT MTC. BASE AND AVIONICS STATIC SPECIALIST CONTRACTED. P-STATIC TEST CASDR CA061220009Line · cracked(CAN) DURING CLIMB, THE ENGINE FIRE WARNING LIGHT ILLUMINATED. THE ENGINE WAS SHUTDOWN. THE FIRE LIGHT EXTINGUISHED, WHEN THE STOP FEATHER LEVERS WERE PULLED BACK. THE CREW BLEW A FIRE BOTTLE, DECLARED AN EMERGENCY AND LANDED. A DAMAGED FIRE DETECTOR (1000 DESDR CA061204003Engine · making metal(CAN) DURING ENGINE MAINTENANCE, IT WAS NOTICED THAT THE ENGINE OIL FILTER BYPASS PIN HAD POPPED. THE OIL FILTER WAS REMOVED AND INSPECTED. METAL CONTAMINATION WAS FOUND AND A SOAP SAMPLE WAS TAKEN. (TC NR 20061204003)SDR CA071212015Pump · failed(CAN) RT FUEL BOOST PUMP FAILED. (TC NR 20071212015)SDR CA060802010Engine · leaking(CAN) ON CLIMB, THE LT LOW OIL PRESSURE LIGHT ILLUMINATED, ALONG WITH A OIL PRESSURE GAUGE DECREASE. THE LT ENGINE WAS SHUTDOWN IN FLIGHT AND RETURNED TO BASE. ON INSPECTION IT APPEARS THAT THE OIL EXITED OUT THE EXHAUST. ENGINE REMOVED AND SENT FOR REPAIR ANDSDR CA060512003Bolt · failed(CAN) WHILE PERFORMING A 100 HOUR INSPECTION ON THE MLG WHEEL SKIS, MAINTENANCE FOUND THE RT WHEEL SKI ATTACH BOLT P/N:C3US156-3 TO BE BENT AND CRACKED. BOLT ATTACHES THE SKI BRACKET ASSEMBLY LINK P/N: C3US108-34 TO THE MLG STRUT AND AXLE. THE BOLT HAS CRACKESDR CA060104011Windshield · crackedLT WINDSHIELD CRACKED WHILE AT FL250. CREW CARRIED ON TO BASE AT LOWER ALTITUDE AND SLOWER AIRSPEED. MAINTENANCE IS CHANGING WINDSHIELD.SDR AU510001733Acm · seized(AUS) LT AIRCYCLE MACHINE COOLING TURBINE SEIZED. ( MATERIAL ) (CASA NR 510001733)SDR AU510001937Engine · fluctuates(AUS) RT ENGINE EXPERIENCED 20 PERCENT TO 30 PERCENT TORQUE DROP WITH ASSOCIATED EGT FLUCTUATIONS. MAINTENANCE INVESTIGATION COULD NOT FIND ANY FAULTS AND ENGINE PARAMETERS WERE NORMAL. AIRCRAFT RETURNED TO SERVICE. (CASA NR 510001937)SDR AU510002198Bolt · sheared(AUS) LT MAIN LANDING GEAR UPLOCK ROLLER BOLT SHEARED. (CASA NR 510002198)SDR CA051027001Line · cracked(CAN) ENROUTE, FLIGHT CREW OBSERVED A LOW OIL PRESSURE INDICATION ON NR 1 ENG. CONFIRMED LOW OIL PRESS ON GAUGE AND CONDUCTED AN IN-FLIGHT SHUTDOWN PROCEDURE. SINGLE ENG FLIGHT CONTINUED TO DESTINATION. CREW CARRIED OUT LANDING, WITH ERS STANDING BY, WITHOUT FSDR CA050630007Landing Gear · malfunctionedAFTER T/O FROM YXH FOR YQL, CREWS ATTEMPTED TO RETRACT L/G. GEAR WOULD NOT RETRACT SO THE CREW SELECTED OVERRIDE. THE GEAR RETRACTED BUT NLG DID NOT FULLY RETRACT INTO NOSE GEAR BAY. CREWS THEN SELECTED GEAR EXTENSION AND RETURNED BACK TO BASE WITH NO FURTHSDR AU510001476Line · worn(AUS) LH ENGINE DRIVEN HYDRAULIC PUMP PRESSURE LINE CHAFED AND HOLED BY OIL TANK UNION. LOSS OF HYDRAULIC PRESSURE RESULTED IN AN EMERGENCY LANDING. DUE TO NO HYDRAULIC PRESSURE, THE ANTISKID WAS NOT AVAILABLE AND THE BRAKES LOCKED UP. NO1, NO2 AND NO3 TYRES WSDR RAIA00501046Igniter · failedABE - NR 1 ENGINE WILL NOT START. MAINTENANCE REMOVED AND REPLACED IGNITERS ON LEFT ENGINE.SDR RAIA00410026Igniter · failedSTL - RIGHT ENGINE HUNG START AT 20 PERCENT. MAINTENANCE REMOVED AND REPLACED RIGHT ENGINE IGNITERS.SDR PNSA040707Strut · seizedHAD A NORMAL TAKEOFF CREW RAISED LANDING GEAR AND LANDING GEAR DID NOT RESPOND, GEAR REMAINED DOWN AND LOCKED. CREW MADE AN UNEVENTFUL LANDING AT DEPARTURE AIRPORT. MAINT DISCOVERED THAT THE LT MAIN GEAR STRUT WAS SEIZED IN UPPER HOUSING, THE LT MAIN GEAR ASSYSDR AUS20040471Blade · bird strike(AUS) RT ENGINE FIRST STAGE COMPRESSOR BLADE BENT DUE TO BIRDSTRIKE.SDR AUS20040482Engine · overtemp(AUS) LT ENGINE EGT ROSE TO APPROXIMATELY 720 DEGREES WITH A REDUCTION IN TORQUE AND FUEL FLOW. DUE TO THE EXCESSIVE EGT THE ENGINE WAS REMOVED FOR AN OVERTEMP INSPECTION. NO RESULTS TO DATE.SDR AUS20040403Drag Brace · fractured(AUS) RT MAIN LANDING GEAR UPPER DRAG BRACE UPLOCK LUGS FRACTURED. CAUSED BY DRAG BRACE OUT OF ADJUSTMENT.SDR CA040507004Tube · chafedAT FL 200 RT HYDRAULIC PRESSURE ANNUNCIATION WENT FROM INTERMITTENT TO CONTINUOUS. ON LANDING FLAPS AND GEAR SELECTION RESULTED IN FURTHER LOSS OF HYDRAULIC PRESSURE AND THE LT HYDRAULIC ANNUNCIATOR ILLUMINATED AND FLAPS WERE SLOW TO EXTEND. AUXILLIARY GEAR SDR AUS20040399Pipe · cracked(AUS) LT ENGINE NEGATIVE TORQUE SENSOR (NTS) OIL PIPE CRACKED IN FLARE.SDR AUS20040272Gear · failed(AUS) RT ENGINE SUFFERED AN UNCONTAINED GEARBOX FAILURE. DEBRIS FROM THE FAILED GEAR IMPACTED ON THE RT SIDE OF THE AIRCRAFT CABIN.SDR AUS20040294Bearing · failed(AUS) RT ENGINE STARTER-GENERATOR BEARING FAILED.SDR AUS20040225Wire · chafed(AUS) RT MAIN FUEL BOOST PUMP WIRING CHAFED.SDR AUS20040224Switch · misinstalled(AUS) PITCH TRIM SWITCH INSTALLED INCORRECTLY. SWITCH HAD BEEN REFITTED FOLLOWING REPAIRS TO THE PILOTS CONTROL YOKE. PERSONNEL/MAINTENANCE ERROR.SDR AUS20040208Switch · sticking(AUS) RT MAIN LANDING GEAR MICROSWITCH STICKING.
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