Garrett TPE-331-10UG
Service difficulty reports · 100
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 = 'TPE33110UG' 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 = 'TPE33110UG' 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 CA100826012Engine · making metal(CAN) ON APPROACH THE NR 2 ENGINE LOST POWER, FLAMED OUT AND STARTED TO NEGATIVE TORQUE SIGNAL (NTS). THE PILOTS WENT THROUGH THE PROCEDURE TO SHUT DOWN AND FEATHER THE NR 2 ENGINE AND LANDED THE PLANE SAFELY. UPON INVESTIGATION, IT WAS DISCOVERED THAT THERESDR CA100827002Seal · failed(CAN) DURING SERVICE CHECK TECH FOUND ENGINE OIL TO BE OVER SERVICED. ENGINE OIL ALSO HAD A REDDISH COLOR. UPON FURTHER INSPECTION HYDRAULIC OIL FOUND TO BE UNDER SERVICED. AIRCRAFT WAS GROUNDED UNTIL SOAP SAMPLE WAS RETURNED CONFIRMING HYDRAULIC OIL HAD BESDR CA080724003Bearing · spalled(CAN) SN OF THE PART IS MS030633106124 WAS UNABLE TO PUT THIS INTO SN FIELD. A/C WAS DOWN FOR A ROUTINE OIL SAMPLE. AT THIS TIME THE OIL SAMPLE WAS NOTED TO HAVE A UNUSUAL AMOUNT OF METAL IN THE OIL SAMPLE. THE ENGINE SHOP WAS INFORMED TO HAVE A LOOK AT THE MSDR CA080709005Retaining Ring · missing(CAN) RUDDER PEDAL BECAME DISENGAGED FROM PEDAL SPIGOT, RS87 RETAINING RING CAME OUT OF RETAINING SLOT. RETAINING RING SEEMED TO HAVE INSUFFICIENT TENSION TO STAY IN SLOT. NEW RING INSTALLED AND NO FURTHER PROBLEMS. FLEETWIDE INSPECTION CARRIED OUT AND NO SIMISDR CA080609009Attach Fitting · cracked(CAN) WHILE CARRYING OUT A 7 DAY SERVICE CHECK, TECH FOUND 3 FLAP TO SLAT ATTACHEMENT CLEATS, P/N`S 137201B88, 137202B62 AND 137203B57 WERE FOUND TO BE CRACKED. THE FLAP SECTION WAS REMOVED AND A SERVICEABLE UNIT INSTALLED. FUNCTION CHECKS CARRIED OUT WITH NOSDR CA080606005Bearing · lack of lube(CAN) ON TAXI FOR DEPARTURE THE PILOT NOTICED A VIBRATION FROM THE NOSE GEAR. HE RETURNED AND MAINT FOUND LT NOSE WHEEL INNER BEARING SEAL WAS STICKING OUT FROM ITS SEAT. WHEEL BEARING WAS ALSO FOUND TO BE ROUGH TO THE (FEEL) AND WERE DRY. NOSE WHEEL ASSY REPSDR 2008FA0000250Engine · overheatedIN CRUISE TO 8000 FT, INDICATION OF RED LIGHT OF OIL PRESSURE WITH 870 DEGREE TEMPERATURE. LIGHT TURNS OFF. AFTER 15 SECONDS, THE LIGHT TURNS ON AGAIN WITH 870 DEGREE TEMPERATURE, BUT THE PRESSURE DOWN NEAR ZERO. THE CREW MADE THE SHUTDOWN ENGINE PROCEDURESDR CA080306002Valve · failed(CAN) THE RT NON RETURN VALVE ASSEMBLY DOWNSTREAM OF THE RT HYDRAULIC PUMP FAILED. NON RETURN VALVE ASSEMBLY IS A UNIT THAT IS SWAGED TOGETHER. THE SWAGE LET GO, ALLOWING HYDRAULIC FLUID TO VENT OVERBOARD. THIS VALVE IS INSTALLED TO PREVENT PRESSURE FROM EITHESDR CA071217006Bolt · backed out(CAN) ON CLIMB OUT, THE PILOT REPORTS NR 1 ENG RPM DROPPED TO 97 PERCENT AND HE WAS NOT ABLE TO RESTORE THE ENG TO 100 PERCENT RPM. PROCEEDED TO MAKE AN UNSCHEDULED LANDING AT DEPARTURE AIRFIELD. UPON INVESTIGATION IT WAS FOUND THAT THE BOLT ATTACHING THE SPESDR CA071219010Tube · chafed(CAN) DURING A SCHEDULED FLIGHT BETWEEN, A WARNING INDICATION OF OIL PRESSURE LOSS ON THE NR 1 ENGINE APPEARED ON THE ANNUNCIATOR PANEL. THE CREW VERIFIED THE WARNING BY OBSERVING THE OIL PRESSURE GAUGE. THE ENGINE WAS SHUTDOWN AND AN EMERGENCY WAS DECLARED. TSDR CA071026008Line · leaking(CAN) DURING A ROUTINE 200 HOUR AIRFRAME INSP, HYD FLUID WAS FOUND TO BE LEAKING FROM ABOVE THE BAGGAGE POD ON THE BELLY OF THE AC. THE AIRCRAFT`S IMPENDING DEPARTURE WAS CANCELLED, AND THE POD REMOVED TO INVESTIGATE. IT WAS FOUND THAT THERE WAS A CLAMP MISSSDR CA070927003Bolt · sheared(CAN) DURING INSPECTION IAW AD 024-05-87 BAE SB 53-A-JA870510R1 PART B, IT WAS NOTED THAT THE TWO UPPER BOLTS WERE SHEARED. THE AIRCRAFT WAS REMOVED FROM SERVICE AT THIS TIME. THE LOWER 2 BOLTS HAVE NOT YET BEEN REMOVED FOR INSPECTION. DUE TO THIS FINDING ANSDR CA070615003Switch · failed(CAN) DURING APPROACH, THE CREW EXPERIENCED A LANDING GEAR FAILURE AND OBSERVED THE CIRCUIT BREAKER HAD POPPED. THEY PROCEEDED WITH AN EMERGENCY LANDING GEAR EXTENSION AND LANDED WITHOUT INCIDENT. THE FAULT WAS TRACED TO THE LT UPLOCK MICROSWITCH. WHEN THE MICSDR CA070615004Bolt · failed(CAN) SCHEDULE INSPECTION AD UK 024-05-87 / SB53A-JA870510R1, WE NOTICE THE 2 UPPER BOLT OF THE NLG JACK MOUNTING BRACKET WERE SHEARED AND THE 2 LOWER ONES WERE LOOSE. ACCOMPLISHED PART A OF THE SB C/OUT(ALL 4 BOLTS AND NUTS REPLACED), PARTS INSPECTED AND AIRSDR BMAC07002Bulb · wrong partDURING APPROACH PHASE AT BED UNABLE TO GET GREEN LIGHT ON RT MAIN AND NOSE. SWAPPED BULBS AND FINALLY GOT GREEN LIGHT ON RT MAIN. STILL NO RED OR GREEN LIGHT ON NOSE. PROCEEDED WITH CHECK LIST AND LANDED UNEVENTFULLY. INSTALLED GEAR LOCK PINS. MAINT FOUND INCOSDR BMAC07003Line · leakingUPON LANDING, BRAKES AND STEERING FOUND TO BE VERY SLUGGISH AND BOTH HYD PUMPS INDICATED NEAR ZERO, APPROX. 100 PSI. TAXI TO GATE WITH NO FURTHER INCIDENT. MAINT FOUND HYD SUPPLY PIPE IN RT IB WING CHAFED. REPLACED PIPE AND ARE REPLACING BOTH HYD PUMPS DUE TOSDR CA070409007Gear · unknown(CAN) GEARS DRIVING THE FUEL PUMP FAILED CAUSING THE ENGINE TO SHUTDOWN IN FLIGHT. (TC NR 20070409007)SDR CA070215002Housing · broken(CAN) ACCESSORY DRIVE HOUSING BOTTOM CASE DRAIN THREADED MOUNTING BOSS DISCOVERED BROKEN. ENGINE REMOVED AND LOANER ENGINE INSTALLED. (TC NR 20070215002)SDR CA070212005Engine · unserviceable(CAN) DURING PRE FLIGHT INSPECTION FLIGHT CREW HEARD ABNORMAL NOISE COMING FROM ENGINE WHILE THEY TURNED THE PROPELLER. MAINTENANCE WAS NOTIFIED AND ENGINE WAS INSPECTED, SUSPECT REAR BEARING FAILURE, OIL SYSTEM INSPECTED AND FOUND TO HAVE NO METAL CONTAMINATISDR CA070131007Windshield · delaminated(CAN) DURING MAINTENANCE INSPECTION, WINDOW WAS FOUND TO BE DELAMINATING AT THE CENTER OF THE BOTTOM EDGE. WINDOW WAS REPLACED. (TC NR 20070131007)SDR BMAC06012Battery Pack · dischargedPILOT REPORTED FORWARD EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED AFT BATTERY PACK, SYSTEM OPERATION CHECKED GOOD IAW AMM 33-50-00.SDR CA070115011Planetary Gear · damaged(CAN) UPON DOING A OIL SAMPLE, METAL WAS NOTED IN THE OIL FILTER. THE ENGINE P-63235C WAS REMOVED. ENGINE WAS FORWARDED TO THE ENGINE SHOP FOR INSPECTION OF THE METAL AND FOUND THAT 1 PLANETARY GEAR WITH THE INNER RACE PEELING METAL AND 3 PLANETARY GEARS WITH SDR CA061024003Unknown · odor(CAN) DURING CRUISE FLIGHT CREW COULD DETECT FUMES OF AN ELECTRICAL NATURE. AIRCRAFT RETURNED TO DEPARTURE POINT WITHOUT INCIDENT. A MAINTENANCE INVESTIGATION IS UNDER WAY TO DETERMINE THE CAUSE OF THE FUMES/ODOUR. A REPORT WILL FOLLOW WHEN CAUSE IS IDENTIFIEDSDR CA061020004Line · cracked(CAN) P3 LINE FLANGE FOUND WITH SMALL CRACK DURING ROUTINE ENGINE CHANGE. LINE REPLACED WITH NEW UNIT. (TC# 20061020004)SDR CA061108005Bracket · cracked(CAN) FLAP SLAT BRACKETS CRACKED AT RADIUS. (TC NR 20061108005)SDR CA061109005Bracket · cracked(CAN) IB FLAP P/N 13760B463, SLAT BRACKETS P/N 137204B51 AND 137205B67 FOUND CRACKED AT BEND RADIUS. REMOVED AND REPLACED WITH NEW. (TC NR 20061109005)SDR CA060719005Wheel · damaged(CAN) DURING TOWING OF AIRCRAFT THE PIC AND GROUND HANDLERS NOTICED A WOBBLE ON THE RH MLG. MAINTENANCE WAS CONTACTED AND IT WAS DISCOVERED THAT A 10" PIECE OF THE EDGE OF THE INNER WHEEL RIM WAS MISSING. THE TIRE STILL REMAINED INFLATED. THE WHEEL AND TIRE WASDR CA060616006Connector · damaged(CAN) AFTER DEPARTURE CLIMBING THROUGH 7500FT THE RIGHT ENGINE TORQUE STARTED TO FLUCTUATE.CREW PULLED THE QRH AND FOLLOWED THE DRILLS AND WERE GETTING 10-20% FLUCTUATION CAUSING THE A/C TO YAW RADICALLY LEFT AND RIGHT AT ALL POWER SETTINGS WITH TTL ON OR OFF SDR CA060525003Engine · malfunctionedIN CRUISE, RT ENGINE TORQUE INCREASED TO 104.5%, WHEN TTL TURNED OFF WENT TO 120%. FUEL FLOW ON RT ENG DROPPED TO 200LBS.SDR CA060529004Flange · splitFOUND OIL DRIPPING UNDER RIGHT ENGINE AFTER SHUT DOWN, ENGINE CLEANED AND CASE NEGATIVE PRESSURE CHECKED, FOUND SERVICEABLE. ENGINE GROUND RUN/MAX POWER CARRIED OUT. OIL FOUND TO BE LEAKING FROM THE PROP GOVERNOR. PROP GOVERNOR REPLACED WITH SERVICEABLE UNISDR CA060209005Starter Gen · failed(CAN) RT GENERATOR FAILER INDICATION ON APPROACH. CREW LANDED A/C WITH NO MORE PROBLEMS. STARTER/GENERATOR REPLACED. STARTER/GEN 67.9 HOURS REMAINING BEFORE OVERHAUL DUE. BRUSH INSPECTED TO BE 20 PERCENT REMAINING. (TC NR 20060209005)SDR CA060116001Valve · crackedON APPROACH, UPON FLAP SELECTION, NO SYSTEM HYD PRESSURE. EMERG GEAR SELECTION USED TO EXTEND L/G, AND TO OBTAIN 10 DEGREES FLAP. A/C LANDED W/O INCIDENT, DUE TO LOSS OF SYS HYD PRESSURE, N/W STEERING INOP AND MAIN BRAKING WAS LIMITED. TOWED TO HANGAR. MX SDR CA060104004Windscreen · crackedAT CRUISE ALT 20,000 FT, NOTICED CRACK AND SUBSEQUENT FLAME WITHIN LAYERS OF LT WINDSHIELD. FLAME SELF EXTINGUISHED WITH DE-SELECTION OF WINDSHIELD HEAT. DURING DESCENT ADDITIONAL CRACKING. DIVERTED TO CYMM. MX DISPATCHED, REPLACED WINDSHIELD. UPON MX REVSDR CA051214001Generator · failed(CAN) IAW AMM 24-30-00 501 DC GENERATION-ADJUSTMENT/TEST. GENERATOR VOLTAGE MUST BE WITHIN 0.3 VOLTS OF EACH OTHER. WHEN REPLACING COMPONENTS IN THE GENERATOR SYSTEM, A CHECK OF THE GCU'S VOLTAGE IS RECOMMENDED AS NUMEROUS HOURS OF TROUBLESHOOTING AND PARTS SDR CA051011005Generator · separated(CAN) GENERATOR WENT OFF LINE IN CLIMB OUT. AIRCRAFT RETURNED TO BASE. GENERATOR REPLACED WITH OVERHAULED UNIT. SYSTEM TESTED SATISFACTORY.SDR CA050919008Engine · unknown(CAN) ENGINE REMOVED AND SENT REPAIR STATION. RESULTS TO FOLLOW.SDR CA051003009Brushes · frayed(CAN) FOUND WIRES NOT FASTENED TO STARTER GENERATOR BRUSHES, DUE TO RIVET BEING LOOSE,WHICH THEN CAUSED ARCING OF WIRE AND RIVET TO CAUSE THE TEMPOR OUT OF THE RIVET .SDR CA050818003Bulkhead · cracked(CAN) CRACK ON FRONT PRESSURE BULKHEAD LT VERTICAL WEB, AT LT NOSE GEAR TRUNNION ATTACHMENT BRACKET TOP CENTER BOLT HOLE.SDR BMAC050010Connector · dirtyERATIC TORQUE +/- 4 PERCENT RT ENGINE INDICATION. MAINTENANCE CLEANED PLUG AT DELTA P/P TRANSDUCER IAW J31 MM 76-10-21, PERFORMED ENGINE RUN, OPS CHECKED GOOD AT THIS TIME.SDR CA050506011Case · cracked(CAN) RT ENGINE FAILED TO MEET TAKEOFF TORQUE SETTING. EX ONLY GOT 90 PERCENT TORQUE ON A +7C, 1900 ASL (TRUE) DAY. SHOULD BE 104.5. ON INSPECTION, IT WAS FOUND THAT THE GAS GENERATOR CASE WAS CRACKED AT THE AIRFRAME SERVICE FLANGE. ENGINE REMOVED AND LOANER SDR CA050414008Line · leaking(CAN) IT WAS NOTICED AFTER A FUEL NOZZLE CHANGE THAT THERE WAS FUEL LEAKING. FUEL LEAK WAS CAUSED BY CHAFING BY THE ADEL CLAMP THAT WAS ATTACHED TO THE TUBE ASSY. TUBE ASSY REPLACED. NO FURTHER PROBLEMS.SDR CA050308012Bracket · cracked(CAN) FLAP SLAT BRACKET FOUND CRACKED DURING MAINTENANCE, CHECK THE CRACKS IN THOSE 3 BRACKETS ARE 1 INCH LONG LOCATED IN THE FORWARD RADIUS OF THE BENDS.SDR CA050131006Engine · failed(CAN) ENGINE FAILED IN FLIGHT, AIRCRAFT HAD JUST EXITED ICING CONDITIONS, CONTINUOUS IGNITION WAS TURNED OFF A FEW MINUTES PRIOR TO ENGINE FAILURE. AIRCRAFT RETURNED TO BASE AND ENGINE WAS INSPECTED FOR ANY CAUSE OF THE FAILURE, NOTHING WAS FOUND. GROUND/POWESDR CA050217003Stud · failed(CAN) GEARBOX COMPRESSOR BEARING RETAINING STUDS FAILED CAUSING THE NR 1 IDLER TO MISALIGN WITH THE FCU DRIVE TRAIN AND THE ROTATING GROUP TO MOVE FORWARD.SDR CA050131004Starter Gen · failed(CAN) GENERATOR WENT OFF LINE, SMOKE AND OIL VISUAL ON COWLING.SDR CA050131007Engine · failed(CAN) SOAP SAMPLE INDICATED MAJOR ALUMINIUM IN THE OIL SYSTEM, 2ND SOAP SAMPLE TAKEN AND FOUND MAGNESIUM AND CARBON STEEL PARTICLES IN THE SAMPLE. ENGINE REMOVED AND SENT FOR EVALUATION, AMO 50-04.SDR BMAC05001Windscreen · crackedPILOT REPORTED: DURING CLIMB OUT, (W/S) CAPTION APPEARED FOR THE RT WINDSCREEN. UPON FURTHER INSPECTION NOTICED CRACKS IN THE UPPER PORTION OF THE WINDSCREEN. CREW DECIDED TO RETURN TO DEPARTURE. REPLACED RT WINDSCREEN DUE TO CRACKING OF OUTER PANE. (K)SDR BMAC040019Handle · out of adjustPILOT REPORTED: DOOR CAP LIGHT CAME ON DURING FLIGHT. PERFORMED DOOR HANDLE ADJUSTMENTS IAW AMM. OPS CHECKED GOOD AT THIS TIME.SDR BMAC040018Selector Switch · inoperativePILOT REPORTED: ON TAKE-OFF, GEAR HANDLE WOULD NOT MOVE TO THE UP POSITION. RETURNED TO DEPARTURE. REMOVED AND REPLACED LANDING GEAR SELECTOR SWITCH IAW AMM. OPERATIONALLY CHECKED OK AT THIS TIME. (K)SDR BMAC040017Selector Valve · inoperativeUNCOMMANDED FLAP DEPLOYMENT IN FLIGHT VERIFIED VISUALLY TO APPROXIMATELY 20 DEGREES. FLAPS CONTINUED TO DEPLOY TOWARD 35. UPON LANDING FLAPS RETURNED TO ZERO VERIFIED VISUALLY UNCOMMANDED. NO HORN WAS HEARD WITH FLAPS DEPLOYED AND POWER LEVER BELOW 20 PERCE
Back to Garrett TPE-331-10UG