Garrett TPE331-11U
Service difficulty reports · 625
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 = 'TPE33111U' 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 = 'TPE33111U' 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 CA980504028Bearing · seized(CAN) DURING TAXI, THE AIRCRAFT VEERED TO THE RIGHT. THE NR 2 NOSE WHEEL BEARINGS HAD SEIZED ONTO THE AXLE. AXLE, NOSE WHEEL, AND BEARINGS REPLACED.SDR CA980415019Harness · worn(CAN) EGT ON AIRCRAFT WAS FLUCTUATING AND GOING TO ZERO. EGT HARNESS WIRE WAS FOUND FATIGUED CAUSING FLUCTUATING EGT. HARNESS REPLACED.SDR AU980313Tube · chafed(AUS) REAR TURBINE OIL SUPPLY TUBE CHAFING ON UTS SYSTEM OIL SUPPLY TUBE.SDR CA980325039Bearing · failed(CAN) PILOT COMPLAINED OF A LOUD NOISE COMING FROM THE RIGHT ENGINE ON START. STARTER REMOVED AND DRIVE END SHAFT FOUND VERY SLOPPY. DRIVE END BEARING HAD BLOWN APART.SDR CA980325036Downlock Switch · intermittent(CAN) INTERMITTENT RIGHT MAIN GEAR GREEN LIGHT ON APPROACH TO LAND. DOWN SWITCH REPLACED.SDR CA980325037Connector · cold solder jt(CAN) AIRCRAFT EXPERIENCED FALSE EGT READING WHICH CAUSED THE SRL TO BYPASS FUEL AND CAUSE THE RIGHT ENGINE TO SURGE. WIRE FOUND WITH A COLD SOLDER JOINT ON TOP OF THE ENGINE IN THE EGT WIRING SYSTEM. WIRE REPAIRED AND AIRCRAFT SENT ON A TEST FLIGHT. AIRCRAFT SDR CA980318006Beta Switch · leaking(CAN) CREW REPORTED NO BETA INDICATION WHEN ON LANDING ROLL AND TAXI. BETA SWITCH AND PLUMBING CHECKED. OIL LEAK WAS EVIDENT ON ENGINE COWL FLAP. SOURCE OF OIL LEAK DETERMINED TO BE FROM BETA SWITCH VENT HOLES. 0.5 LITERS OF OIL WAS LOST IN THIS MISHAP.SDR CA980318005Pump · worn(CAN) SPLINES FOUND WORN ON INSPECTION. UNIT S/N 491719C REPLACED.SDR CA980318018Switch · intermittent(CAN) NO GREEN INDICATION FOR THE NOSE ALTHOUGH THE IN-TRANSIT LIGHT WAS OK.GEAR DOWN SWITCH WAS INTERMITTENT.SDR CA980318007Line · cracked(CAN) HYDRAULIC LINE IN LEFT ENGINE NACELLE CRACKED IN FLIGHT.ALL FLUID LEFT THE AIRCRAFT.AIRCRAFT RETURNED TO BASE WITH GEAR DOWN AND LOCKED. A 1/4 INCH CRACK FOUND IN THE 90 DEGREE BEND.SDR CA980318008Duct · cracked(CAN) EXHAUST DUCT FOUND CRACKED AROUND 3/4 QUARTERS OF THE CIRCUMFERENCE OF THE FLANGE.SDR CA980318009Screw · sheared(CAN) ON ENGINE CHANGE ON THE RIGHT HAND SIDE AND DURING THE RUN UP A LARGE HYD. LEAK WAS NOTED.LEAK COMING FROM HYD. PUMP VALVE PLATE AS 2 OF THE 4 SCREW HEADS HAD BEEN SHEARED OFF.SDR CA980318010Actuator · ratcheting(CAN) PITCH TRIM ACTUATOR FOUND OUT OF LIMITS WHILE DOING FAA AD 97-23-01.SDR ARWA980204Engine · leakingNR 2 ENGINE NO OIL PRESSURE/OIL QUANTITY WENT DOWN TO 1.5 QUARTS. REMOVED AND REPLACED NR 2 ENGINE. PERFORMED ENGINE NR 2 CHANGE AS PER ARROW AIR PAPER WORK 8275 ENGINE S/N OFF 671003, ENGINE S/N ON 645654.SDR AU980053Torque Link · cracked(AUS) LH AND RH MAIN LANDING GEAR UPPER TORQUE LINKS CRACKED IN AREA OF THE CENTRE PIVOT LUGS.SDR 98ZZZX935Hydraulic Line · crackedBTV/ALB - AFTER TAKEOFF, NOSE WHEEL LANDING GEAR WOULD NOT STAY UP AND LOCKED. BOTH THE LEFT AND RIGHT HYDRAULIC PRESSURE FAIL LIGHTS ILLUMINATED AND THE AIRCRAFT LOST ALMOST ALL HYDRAULIC PRESSURE. THE AIRCRAFT RETURNED TO BTV AND LANDED WITH AN EMERGENCY GSDR 98ZZZX936Hydraulic Line · failedALB/ROC - EN ROUTE, LEFT AND RIGHT HYDRAULIC PRESSURE LIGHTS ILLUMINATED AND HYDRAULIC PRESSURE DROPPED ALMOST TO ZERO. CREW LANDED AT ROC WITH AN EMERGENCY GEAR EXTENSION, NO FLAP, AND NO NOSE WHEEL STEERING. LANDING UNEVENTFUL, NO EMERGENCY DECLARED, ANSDR AU980020Bolt · loose(AUS) LH LOWER ENGINE MOUNT BRACKET BOLTS LOOSE. SUSPECT BOLTS INCORRECTLY TORQUED AT MANUFACTURE.SDR AU980060Blade · failed(AUS) FIRST STAGE TURBINE BLADES (3OFF) FAILED AT APPROXIMATELY MID SPAN. SEVERE DOWNSTREAM FOD TO SECOND AND THIRD STAGE TURBINE ASSEMBLIES.SDR 98ZZZX286Fcu · required adjustBWD/DFW - FLT 1230 - ON TAKEOFF ROLL JUST BEFORE V1, EXPERIENCED A POWER DROP IN LT ENGINE AND ACFT YAWED TO THE LEFT. ABORTED TAKEOFF AND RETURNED TO GATE WITH NO FURTHER ABNORMALITIES NOTED. MAINTENANCE CONTROL DISPATCHED FROM DFW AND ADJUSTED SCREW 'X' ON SDR QXEA9800006Engine · bird strikeRETURN TO FIELD, BIRD STRIKE AFTER TAKEOFF. NR 1 ENGINE INLET SHOWS EVIDENCE OF INGESTION. INSPECTED AIRCRAFT AND NR 1 ENGINE IAW GARRETT MAINTENANCE MANUAL. NO PARTS REPLACED, OPERATIONAL CHECK GOOD.SDR PNSA980104Exciter Box · inoperativeLT ENGINE WOULD NOT START, REPLACED IGNITION EXCITER BOX. OPS CHECK OK.SDR AU971537Static Port · contaminated(AUS) LH STATIC PORT BLOCKED BY WATER FOLLOWING HEAVY RAIN.SDR AU971535Indicator · faulty(AUS) RH MAIN LANDING GEAR POSITION LIGHT FAULTY.SDR 97ZZZM1227Fuel Control · out of adjustTHE PILOT ABORTED THE TAKEOFF AT SAT FOR LOW TORQUE ON RIGHT ENGINE. MAINTENANCE PERFORMED GROUND CHECK, ADJUSTED SCREW 'X', VERIFIED EGT COMP, AND TSC. ALL CHECKED OK. AN ENGINE GROUND RUN WAS ACCOMPLISHED TO VERIFY ADJUSTMENTS THAT WERE MADE. NO DEFECTS SDR 98ZZZM107'X' Screw · out of adjustDFW - FLT 1231 - LEFT ENGINE READS 80 PERCENT TORQUE AND RIGHT ENGINE READS 95 PERCENT TORQUE AT 100 PERCENT RPM IN FLIGHT. EGT 620 DEGREES. AIRCRAFT RETURNED TO DFW. MAINTENANCE PERFORMED GROUND RUNS IAW SA227 MM AND GARRETT MM 71-00-00. COULD NOT DUPLICATSDR CA971210001Stop Screw · out of adjust(CAN) ON TAKEOFF, LEFT ENGINE RPM FLUCTUATED AND CONTINUED TO DO SO, CAUSING CREW TO FEATHER PROP AND SHUT DOWN ENGINE. LEFT FUEL CONTROL TO PROP GOVERNOR HIGH RPM CORRELATION OUT OF ADJUST.SDR AU971381Pipe · cracked(AUS) HYDRAULIC PIPE SPLIT IN RADIUS LOCATED ON THE FIRST BEND FORWARD OF THE RH ENGINE FIREWALL.SDR AU971352Pin · broken(AUS) RH MAIN LANDING GEAR TORQUE LINK LOWER PIN MISSING.SDR AU971485Bracket · cracked(AUS) LH AILERON CENTRE ATTACHMENT BRACKET CRACKED ON UPPER AND LOWER WEBS AT AILERON INPUT BELLCRANK PIVOT BOLT ATTACHMENT AREA.SDR QXEA9700656Compensator · malfunctionedPDX- ON TAKEOFF, NR 2 ENGINE DID NOT MAKE TARGET TAKEOFF TORQUE. POWER LEVERS WERE TO THE STOPS. ABORTED TAKEOFF AND RETURNED TO THE GATE. REPLACED EGT COMPENSATOR, OPERATIONAL CHECKS GOOD.SDR QXEA9700653Tq Indication · malfunctionedPDX- ON TAKEOFF ROLL, NR 2 ENGINE TORQUE INDICATION STARTED TO FLUCTUATE. ABORTED TAKEOFF AND RETURNED TO THE GATE. AIRCRAFT UNDER REPAIRS.SDR 97ZZZM1211P2t2 Sensor · frozenWHILE EN ROUTE FROM ANC TO BET, THERE WAS A DROP IN TORQUE AND EGT ON THE RIGHT ENGINE. THE CREW DID AN AIR TURNBACK ANC. MAINTENANCE DETERMINED THAT THE P2T2 SENSOR FROZE DURING FLIGHT. MAINTENANCE THE COMPLIED WITH PARA B OF AD 97-15-10 BY COMPLYING WITH SDR CA980615008Filter · failed(CAN) DURING TAKEOFF, THE FUEL BYPASS LIGHT CAME ON WITH A LOSS OF TORQUE ON NR 2 ENGINE. TROUBLESHOOTING WAS CARRIED OUT ON THE BYPASS AND FUEL SYSTEM. THE FLOW DIVIDER FILTER WAS CHECKED AND THE FUEL FILTER WAS REPLACED. GROUND RUNS COMPLETED WITH NO FAULSDR PNSA970809Fuel Control · malfunctionedENGINE WOULD NOT REACH TARGET TORQUE. FUEL LIMITED, REPLACED FCU.SDR 97ZZZM902Engine · failedEN ROUTE FROM ANC TO DLG, THE LEFT ENGINE OIL PRESSUR LIGHT CAME ON. THE CAPTAIN DID A PREPLANNED ENGINE SHUTDOWN AND REQUESTED PRIORITY HANDLING INTO DLB. MAINTENANCE REMOVED AND REPLACED THE ENGINE. (M)SDR QXEA9700355Bypass Valve · malfunctionPDX - ABORTED TAKEOFF, NR 1 ENGINE TORQUE SURGES OF 10 TO 15 PERCENT DURING TAKEOFF ROLL. REPLACED NR 1 ENGINE FUEL BYPASS VALVE. OPERATIONAL CHECK GOOD.SDR 97ZZZM900Washers · failedDEPARTING BIS FOR FAR, ACCELERATING DOWN THE RUNWAY DURING T/O, THE RT CHIP DETECT LIGHT WAS OBSERVED TO BE ILLUM DURING THE 80 KTS CROSS CHECK. THE T/O WAS ABORTED. MX REMOVED AND INSPECTED THE CHIP DETECT. NO SIGNIFICANT METAL PARTICLES WERE FOUND. DETECSDR 97ZZZM909Engine · failedDURING TAKEOFF ROLL FROM MIQ TO POS, THE LEFT ENGINE DID NOT MAKE THE CHARTED TORQUE. THE CAPTAIN ABORTED THE TAKEOFF. THE ENGINE WAS REMOVED AND REPLACED WITH AN OVERHAULED UNIT. (M)SDR QXEA9700314Carbon Seal · wornOIL SMELL IN BLEED AIR SYSTEM. GROUND RAN DETERMINED SMELL COMING FROM NR 2 BLEED. PLACED ON MEL. MEL CLEARED BY REPLACING THE NR 2 ENGINE GEARBOX CARBON SEAL. PERFORMED GROUND RUN ON AIRCRAFT, CHECKED GOOD.SDR QXEA9700306Wiring Harness · chafedAT TAKEOFF UPON APPLICATION OF POWER LEVER NR 1 WF DROPPED OFF TO 150 PPH. ABORTED TAKEOFF. INSPECTED AND REPAIRED CHAFED FUEL FLOW TRANSMITTER WIRING HARNESS, OPERATIONAL CHECK GOOD.SDR 97ZZZM739Fuel Control · failedDURING TAKEOFF ROLL OUT OF ANC, THE RIGHT ENG TORQUE INDICATIONS BEGAN FLUCTUATING. THE PILOT ABORTED THE TAKEOFF AND RETURNED TO MAINTENANCE WITH THE AIRCRAFT. MAINTENANCE PERFORMED A GROUND RUNUP CHECK AND ISOLATED THE PROBLEM TO THE RIGHT FUEL CONTROL UNISDR 97ZZZX2953Fuel Manifold · leakedDURING TAKEOFF ROLL, CAPTAIN NOTICED A LOW TORQUE ON RT ENGINE. CAPTAIN ELECTED TO ABORT TAKEOFF ROLL AND TAXIED TO A RUN-UP AREA TO CHECK THE RT ENGINE'S POWER. DURING RUN-UP, RT ENG DID NOT MAKE CHARTED TORQUE. AS CAPTAIN STARTED TAXIING BACK TO MX, THE RSDR CA970421071Bearings · stiff(CAN) PILOT REPORTED THE CONTROL COLUMN WAS STIFF IN FLIGHT. UPPER BEARING WAS FOUND STIFF AND HARD TO TURN.SDR AU970289Pipe · leaking(AUS) LH MAIN LANDING GEAR `UP' RIGID PIPE HOLED AND LEAKING - PIPE IS MANUFACTURED FROM ALUMINIUM ALLOYSDR MALA975355Heat Duct · malfunctionedFLT 2997 - DURING FLIGHT, LEFT OIL COOLER DUCT HEAT WOULD NOT OPERATE. PULLED AND RESET CIRCUIT BREAKER WITH NO CHANGE. FLIGHT RETURNED TO DTW. MAINTENANCE INSPECTED OIL COOLER DUCT HEAT AND CANNON PLUG. NO DEFECTS NOTED. MAINTENANCE PERFORMED FUNCTIONAL SDR PNSA970309Igniter Box · failedLEFT ENGINE NO START, REPLACED IGNITER BOX.SDR AU970339Truss · cracked(AUS) ENGINE MOUNT ASSEMBLY CRACKED BETWEEN TWO WELDED SEAMS IN AREA OF UPPER REAR CLUSTERSDR PNSA970303Engine · will not startLEFT ENGINE NO START AT GATE, NO FAULT FOUND BY MAINTENANCE.SDR AU970225Pin · incorrect fit(AUS) LANDING GEAR EMERGENCY GEAR EXTENSION SHUTOFF VALVE HANDLE LOCK PIN INCORRECTLY FITTED - EMERGENCY GEAR EXTENSION HANDLE WAS PUSHED FORWARD TOWARDS THE EMERGENCY POSITION PREVENTING CORRECT OPERATION OF THE LANDING GEAR RETRACTION SYSTEM - PERSONNEL ERRO
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