Garrett TPE331-10

Service difficulty reports · 185

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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 = 'TPE33110'
  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.

SDR 99ZZZX354Engine · failedDURING NORMAL CRUISE AT FL 220, THE RIGHT ENGINE WENT TO FEATHER. UPON A NON-EVENTFUL LANDING, DETERMINED THE TURBINE HAD UNCOUPLED FROM THE GEARBOX. ENGINE TIME SINCE OVERHAUL 731.5 HOURS.Dec 16, 1998 · N44MM · Mtsbsi MU2B60 · Engine (Turbine/Turboprop)SDR CA981207013Wheel · failed(CAN) DURING AN OVERSHOOT, THE PILOT HEARD A LOUD BANG AND NOTED EXCESSIVE EGT, FOLLOWED BY NR 1 ENGINE FAILURE. THE ENGINE WAS SHUTDOWN. ENGINE DISASSEMBLY FOUND 1ST TURBINE BLADE HAD SEPARATED AT THE BLADE ROOT. THE BLADE FAILURE DOES NOT APPEAR TO BE A RESNov 29, 1998 · Mtsbsi MU2B60 · Turbine SectionSDR 98ZZZX4616Turbine Wheel · damagedENGINE COULD NOT BE TURNED BY HAND ON PRE-FLIGHT. THIRD ROTOR WAS FOUND TO HAVE PIECES MISSING FROM T-BLADES. ENGINE TEAR DOWN REVEALED THAT SEVERAL PLUGGING RIVETS INSTALLED IN HOLES AT THE BLADE ROOTS ON SECOND ROTOR HAD BROKEN. THE FLARED END ON ALL RIVEOct 9, 1998 · N11MM · Cessna 441 · Turbine SectionSDR 98ZZZX3695Housing · crackedHOUSING ASSY ACCESSORY DRIVE P/N 3101836 HAS A CRACK IN THE MOUNTING PAD BOSS. FOUR BOLTS ATTACH THE RT ENGINE MOUNT TO THE BOSS. THE LOWER OUTBOARD BOLT INSERT CRACKED OUT.Sep 15, 1998 · N423CA · Casa C212CC · Turbine Engine Accessory DriveSDR AU981192Spring · broken(AUS) AIRCRAFT TAILSPRING CRACKED AND BROKEN. AIRCRAFT HAD BEEN PARKED OVERNIGHT WITH A FULL HOPPER. PART TC: 1,775.Sep 9, 1998 · Ayres S2RG10 · Nose/Tail Landing GearSDR 99ZZZX880Pump · failedDROP IN OIL PRESSURE. OIL LUBRICATION SYSTEM/REAR SCAVENGE PMP BEGINNING TO FAIL. SCAVENGE PUMP FAILURE.Jul 25, 1998 · N46AK · Mtsbsi MU2B60 · Turbine Engine Oil SystemSDR CA970605003Wheel · cracked(CAN) OUTBOARD WHEEL HAS A .500 INCH CRACK RUNNING FROM BASE OF BOLT HOLE COUNTER BORE TO INSIDE OF WHEEL .500 INCH ABOVE O-RING AIR SEAL. CRACK ALLOWED TUBELESS TIRE TO SLOWLY DEFLATE. REPLACED.Mar 19, 1998 · Cessna 441 · Wheel/Ski/FloatSDR 98ZZZX98Torque Sensor · failedAIRCRAFT TOTAL TIME: 8,643.5 HOURS. ENGINE TOTAL TIME: 5,609.6 HOURS. ENGINE TSO: 2,518.7 HOURS. AIRCRAFT HAD CHIP LIGHT ON NR 1 ENGINE ON GROUND. SUBSEQUENT INSPECTION FOUND THAT PROPELLER FAILED TO TURN. SUSPECT GEARBOX FAILURE.Dec 10, 1997 · N423CA · Casa C212CC · Turbine Engine Reduction GearSDR 98ZZZX155Oil Jet · brokeOIL JET BROKE AND LODGED ITSELF IN PLANETARIES AND RING GEAR. RING GEAR BROKE AND COUPLER SHAFT SHEARED RESULTING IN ENGINE SHUT DOWN.Dec 2, 1997 · N46AK · Mtsbsi MU2B60 · Turbine Engine Oil SystemSDR CA971219007Fcu · malfunction(CAN) DURING START, ENGINE INTERMITTENTLY SLOW TO ACCELERATE 40 PERCENT TO 60 PERCENT. OK ABOVE 60 PERCENT. CONDITION GOT WORSE. FCU REPLACED. PART TC: 661.Oct 21, 1997 · Cessna 441 · Fuel Control/Reciprocating EnginesSDR CA971222003Transducer · failed(CAN) TRANSDUCER GAVE INCORRECT SIGNAL TO ENGINE COMPUTER-CAUSING SRL TO BE INCORRECT. THE ERROR WAS GREATER AS THE AIRCRAFT CLIMBED. THUS; TORQUE, FUEL FLOW, AND EGT DID NOT MATCH THE OTHER ENGINE AS THE AIRCRAFT CLIMBED. THIS IS THE P/P TRANSDUCER.Oct 7, 1997 · Cessna 441 · Engine Indicating SystemSDR CA971222002Fuel Pump · failed(CAN) ENGINE WOULD NOT LIGHT UP DURING START UNTIL 18 PERCENT-20 PERCENT. A NORMAL START LIGHT OFF IS 12 PERCENT-14 PERCENT. FOUND FUEL PUMP OUTPUT PRESSURE AT LOW RPM BELOW SPECS.Sep 7, 1997 · Cessna 441 · Engine Fuel PumpSDR 97ZZZX4457Support · crackedFUEL CONTROL SUPPORT SPLIT BETWEEN TWO BOLT HOLES. PART NEEDS TO BE LONGER.Sep 2, 1997 · N3330S · Cessna 441 · Fuel Control/Reciprocating EnginesSDR CA971223002Ignition Box · failed(CAN) IGNITION BOX FAILED.Jul 11, 1997 · Cessna 441 · Ignition Power SupplySDR CA970620003Governor · low output(CAN) DURING APPROACH, THE CREW COULD NOT REDUCE THE POWER AT FLIGHT IDLE ON THE L/H ENGINE BELOW ABOUT 40 PERCENT TORQUE. DUE TO THE SHORT RUNWAY, ENGINE WAS SHUT DOWN AND LANDING MADE. THE FUEL CONTROL WAS REMOVED AND REPLACED. ENGINES WERE GROUND RUN AND FOJun 17, 1997 · Swrngn SA226TC · Propeller GovernorSDR 97ZZZX2710Hose · wrong partFOUND CLEVELAND BRAKE KIT 199-101 STC 648GL BRAKE HOSES WERE SAE DOT 3000 PSI AIR BRAKE HOSES. FITTINGS WERE 45 DEGREES.May 22, 1997 · N223JS · Mtsbsi MU2B60 · Landing Gear Brake SystemSDR 97ZZZX1739Engine · failedLEFT ENGINE SHUT DOWN IN-FLIGHT DUE TORQUE PRESSURE DROP (40 PSI). SPEED INCREASE TO 103+ . ON INSPECTION, NO OUTWARD SIGN OF DAMAGE, BUT COULD NOT ROTATE PROPELLER. ENGINE OIL FILTER REMOVED, METAL IN FILTER. METAL ON CHIP DETECTOR (NO LIGHT). OIL BLACK Mar 28, 1997 · N3U · Gulstm 695 · Turbine Engine Reduction GearSDR 97ZZZX1172Engine · failedTHE FOLLOWING DETAILS WERE REPORTED BY THE PILOT. THEY OCCURRED WHILE EN ROUTE. A/C YAWED TO LEFT. NR 1 TQ INDICATOR SPOOLED DOWN RAPIDLY. CHIP DET LT LIGHT ILLUMINATED ON WARNING ANNUNCIATOR PANEL. NR 1 RPM INDICATOR SPOOLED DOWN. NR 1 OIL PRESSURE, FUEFeb 27, 1997 · N422CA · Casa C212CC · Engine (Turbine/Turboprop)SDR REXA97034Screw X · out of adjustNR 2 ENGINE DID NOT REACH TARGET TORQUE OF 100.5 PERCENT, ONLY REACHED 84 PERCENT. ADJUSTED SCREW 'X' IAW GARRETT MM AND GROUND RAN. (X)Feb 20, 1997 · N300PX · Bag JETSTM3101 · Fuel Controlling SystemSDR 97ZZZX3561Engine · failedNR 2 ENGINE SHUT DOWN IN-FLIGHT DUE TO ZERO TORQUE AND DECREASING ENGINE RPM FUEL FLOW. ENGINE OIL OVER-SERVICE SUSPECTED DUE TO OIL TANK VENT VALVE OPEN.Jan 10, 1997 · N348CA · Casa C212CC · Engine (Turbine/Turboprop)SDR BSAA082396Nut · brokenGDV - ENGINE HARD TO PULL THROUGHT AND NOISEY. FOUND AFT TURBINE NUT (P/N 865082-1) BROKEN ALLOWING TURBINE RUB. PERFORMED COMPLETE ENGINE TEARDOWN AND INSPECTION FOR DAMAGE. PARTS WILL BE REPLACED AS REQUIRED AND MAINTENANCE CHECKS COMPLETED. (M)Aug 23, 1996 · N115BS · Swrngn SA226TC · Turbine SectionSDR CA960812006Valve · stuck(CAN) DURING CRUISE, THE CREW NOTICED HIGH OIL TEMP ON RT ENGINE AND DIVERTED FOR LANDING. MAINTENANCE FOUND HIGH OIL TEMP IN THE OIL TANK AND COOL OIL IN THE COOLER. THE VERNATHERM VALVE P/N 8A575-000 WAS REPLACED AND GROUND CHECKED SERVICEABLE.Aug 8, 1996 · Swrngn SA226TC · Engine Oil Temperature RegulatorSDR CA960826005Vernatherm Valve · failed(CAN) DURING CRUISE, THE CREW NOTICED HIGH OIL TEMP ON THE RIGHT ENGINE. INVESTIGATION REVEALED HIGH OIL TEMP IN THE TANK AND COLD OIL IN THE COOLER. THE VERNATHERM VALVE P/N 8A575-000 S/N 000123 WAS REPLACED WITH A SERVICEABLE ONE AND ENGINE GROUND RUN. THE OAug 8, 1996 · Swrngn SA226TC · Engine Oil Temperature RegulatorSDR CA971128007Bearing · corroded(CAN) AFT PROPELLER SHAFT BEARING FOUND CORRODED.Jul 9, 1996 · Mtsbsi MU2B60 · Turbine Engine Reduction GearSDR 96ZZZX3045Gearshaft · shearedAIRCRAFT EXPERIENCED AN UNCOMMANDED ENGINE SHUT DOWN. ENGINE DISASSEMBLY REVEALED GEARSHAFT HAD SHEARED CAUSING FUEL PUMP TO STOP TURNING. REFERENCE: 1PC 72-01-16, SECTION 72-10-17, PAGE 2, ITEM 40.May 9, 1996 · N175CA · Mtsbsi MU2B60 · Turbine Engine Accessory DriveSDR 95ZZZX2613Gasket · leaksENGINE OIL LEAK DETERMINED TO BE PROP PITCH CONTROL GASKET. INSTALLED THREE MORE NEW GASKETS WITH SAME OIL LEAK. GASKETS HAVE THE WORD 'CANADA' MARKED ON THE EDGE OF THE TACH GENERATOR MOUNT FACE. GASKETS WERE INSTALLED PER GARRETT MM.May 11, 1995 · N441JD · Cessna 441 · Turbine Engine Oil SystemSDR 95ZZZX7025Engine · damagedAIRCRAFT LEVEL FLIGHT 17,000 FEET NORMAL TORQUE FOR BOTH ENGINES. TEMPS NORMAL, FUEL FLOW NORMAL. LEFT ENGINE WENT TO ZERO TORQUE, FLUCTUATED SOME. EGT REMAINED BELOW RED LINE, FUEL FLOW WAS STILL NORMAL. OIL PRESSURE NORMAL. PILOT USED EMERGENCY CUT-OFF,Mar 10, 1995 · N479MA · Mtsbsi MU2B60 · Engine (Turbine/Turboprop)SDR 95ZZZX6938Nozzle Assy · not torquedENGINE WILL NOT START. HIGH EGT AND HUNG AT 24 PERCENT RPM. UNABLE TO TEST HIGH CROSS FLOW. HEAD NOT TORQUED PER SPECS.Mar 8, 1995 · N479MA · Mtsbsi MU2B60 · Fuel Injector NozzleSDR 95ZZZX6939Nozzle Assy · defectiveENGINE WILL NOT START. HIGH EGT AND HUNG AT 24 PERCENT RPM. NOZZLE FOUND TO BE SPLITTING PER SPECS.Mar 8, 1995 · N479MA · Mtsbsi MU2B60 · Fuel Injector NozzleSDR 95ZZZX6940Nozzle Assy · defectiveENGINE WILL NOT START. HIGH EGT AND HUNG AT 24 PERCENT RPM. FOUND PRIMARY SIDE OF NOZZLE PLUGGED, EXCEPT FOR SOLID THIN STREAM AT 40 DEGREE PATTERN POSITION, PER SPECS.Mar 8, 1995 · N479MA · Mtsbsi MU2B60 · Fuel Injector NozzleSDR 95ZZZX6941Nozzle Assy · defectiveENGINE WILL NOT START. HIGH EGT AND HUNG AT 24 PERCENT RPM. FOUND PRIMARY SIDE OF NOZZLE PLUGGED, EXCEPT FOR SOLID THIN STREAM AT 40 DEGREE PATTERN POSITION, PER SPECS.Mar 8, 1995 · N479MA · Mtsbsi MU2B60 · Fuel Injector NozzleSDR 95ZZZX6942Nozzle Assy · defectiveENGINE WILL NOT START. HIGH EGT AND HUNG AT 24 PERCENT RPM. NOZZLE INSPECTED AND FOUND TO BE EJECTING A SOLID STREAM PER SPECS.Mar 8, 1995 · N479MA · Mtsbsi MU2B60 · Fuel Injector NozzleSDR 95ZZZX6943Nozzle Assy · defectiveENGINE WILL NOT START. HIGH EGT AND HUNG AT 24 PERCENT RPM. NOZZLE FOUND LEAKING PER SPECS.Mar 8, 1995 · N479MA · Mtsbsi MU2B60 · Fuel Injector NozzleSDR 95ZZZX5291Solenoid Valve · failedSOLENOID VALVE NO RESPONSE WHEN POWERED. REPLACED WITH NEW UNIT(S) CORRECTED PROBLEM.Mar 3, 1995 · N454MA · Mtsbsi MU2B60 · Engine Fuel DistributionSDR 95ZZZX1139Blade · failedDURING TAKEOFF POWER APPLICATION, LT ENGINE DEVELOPED HIGHER THAN NORMAL ITT. THE ENGINE WAS VISUALLY INSPECTED AND WAS FOUND TO HAVE EJECTED INTERNAL PARTS FROM THE TAILPIPE. TEAR DOWN INSPECTION REVEALED CAUSE TO HAVE BEEN GENERATED FROM ONE FIRST STAGE TUFeb 22, 1995 · N132BK · Mtsbsi MU2B60 · Turbine Section
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