Garrett TPE331-10T

Service difficulty reports · 27

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 = 'TPE33110T'
  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 V8ZA202009100001Fitting · detachedPILOT TAXIED FOR TAKEOFF AND USED THE RUDDER SYSTEM TO MAINTAIN DIRECTIONAL CONTROL BOTH ON THE GROUND AND DURING THE TAKEOFF ROLL. WHEN IN THE AIR HE NOTICED A LACK OF YAW CONTROL DURING A CLIMBING TURN, THE FLIGHT WAS ABORTED AND A NORMAL LANDING ACCOMPLISHSep 8, 2020 · N112EE · Gulstm 690A · Rudder Control SystemSDR XV6A2016052200002Unknown · odorELECTRICAL "HOT" ODOR NOTED WHILE IN PATTERN. PERFORMED POWER/ON OPS CHECKS OF EXTERNAL POWER, AVIONICS POWER, STATIC INVERTERS, INSTRUMENT PANEL AND COCKPIT LIGHTS, AND PASSENGER INFORMATION LIGHTS. APPLIED HYD POWER, CHECKED COCKPIT HEATERS, EXTENDED AND REMay 22, 2016 · N501VA · Dorner DO228202 · Air Distribution SystemSDR XV6A2016050300001Hose · chafedAFTER GEAR EXTENSION NWS, NOSE WHEEL STEERING, BYPASS ANNUNCIATOR ILLUMINATED AND HYDRAULIC PRESSURE INDICATED 0 BAR. AFTER INSPECTION FOUND NWS HYD LINE CHAFED, CAUSING LOSS OF HYDRAULIC PRESSURE. R & R SAID LINE IAW DO-228, AMM 32-20-01. TIMES AND CYCLES OMay 3, 2016 · N409VA · Dorner DO228202 · Hydraulic System, MainSDR CA160222010Fuel Line · worn(CAN) WHILE REMOVING LT STARTER/GEN FOR INSPECTION PURPOSES IT WAS FOUND THE FUEL LINE (P/N 3102762-1) WAS RUBBED ALMOST ALL OF THE WAY THROUGH BY THE PROPELLER GOVERNOR. AFTER REMOVAL OF THE FUEL LINE IT WAS THEN FOUND THAT THE FUEL LINE WAS RUBBING ON THE OIFeb 22, 2016 · Gulstm 690D · Engine Fuel DistributionSDR CA150831007Filter · missing(CAN) WHILE CARRYING OUT AD 2015-12-04 FCU SPLINE SHAFT INSPECTION, THE FCU WAS FOUND TO BE MISSING IT`S FILTER SCREEN. A REPLACEMENT FILTER WAS INSTALLED.Aug 28, 2015 · Gulstm 690A · Fuel Control/Turbine EnginesSDR XV6A2014071500002Engine · warning lightDURING CRUISE FLIGHT AT 9500 FT, MASTER WARNING HORN & LIGHT SOUNDED. LT OIL PRESSURE ANNUNCIATOR ILLUMINATED & TORQUE DROPPED. RAN QRH ENG FAILURE CHECKLIST, DECLARED AN EMERGENCY & DIVERTED. REMOVED LT PROPELLER & ENGINE AS AN ASSEMBLY. INSTALLED SERVICEJul 15, 2014 · N405VA · Dorner DO228202 · Engine (Turbine/Turboprop)SDR XV6A2013112500009Shutoff Valve · stuckLEFT ENGINE FIRE BOTTLE FIRED DUE TO FIRE INDICATION DURING VENT. 1C EMERGENCY EXIT REMOVED FOR POSSIBLE GROUND EVAC. ENGINE VENT WAS DUE TO ABORTED START, LEFT ENGINE HUNG AT 32-33 PERCENT, NO TEMP LIMIT REACHED - 60 SECONDS. DURING TROUBLESHOOTING OF NR 3Nov 25, 2013 · N402VA · Dorner DO228202 · Fuel Controlling SystemSDR CA130904010Angle · cracked(CAN) LEFT MLG TRUSS ANGLE NOTED TO HAVE CRACK APPROXIMATELY 0.7" LONG IN RADIUS. CRACK DISCOVERED BY VISUAL INSPECTION AND CONFIRMED USING FLPI. THIS ANGLE PROVIDES SECONDARY ATTACHMENT OF THE MLG TRUSS FORGING TO THE LOWER WING SKIN. CRACK WAS REPAIRED USIAug 1, 2013 · Gulstm 690A · Main Landing Gear Attach SectionSDR CA140107004Fairing · unknown(CAN) THIS AIRCRAFT HAS BEEN MODIFIED BY STC SA1584SW. DURING HEAVY MAINTENANCE IT WAS NOTED THAT THE ACFT HAD AN UNAPPROVED FAIRING INSTALLED FORWARD OF THE CAMERA DOOR. THE 7.5 LB FIBERGLASS FAIRING WAS REMOVED AS A SUSPECTED UNAPPROVED PART. THE FAIRING WAMar 26, 2013 · Gulstm 690A · Aerodynamic FairingsSDR CA120127011Adapter · cracked(CAN) THE RT STARTER-GENERATOR OF THE RT ENGINE WAS REMOVED DURING SCHEDULED MAINTENANCE. ALSO, REMOVED WAS THE STARTER-GENERATOR MOUNTING ADAPTER TO ALLOW BETTER ACCESS FOR ENGINE MAINTENANCE AND INSPECTION. AFTER REMOVAL, IT WAS FOUND THAT THE MOUNTING ADAJan 25, 2012 · Gulstm 690A · Starter-GeneratorSDR O9IA2011112100011Motor · burned outDURING CRUISE FLIGHT AIR CONDITIONER BLOWER FAN FAILED CAUSING SMOKE TO ENTER CABIN.Nov 21, 2011 · N83WA · Gulstm 695B · Air Distribution FanSDR XV6A2011102500015Thermocouple · faultyDURING FLIGHT, NR 1 ENGINE INDICATED HIGH OIL TEMP, IN YELLOW. CREW ACCOMPLISHED QRH AND MADE AN UNSCHEDULED LANDING INTO 1G4. REPLACED LT OIL TEMP INDICATOR WITH REPAIRED INDICATOR, PROBLEM STILL EXISTS. REPLACED LT OIL TEMP BULB WITH NEW BULB. OPS CHECK Oct 25, 2011 · N405VA · Dorner DO228202 · Engine Oil TemperatureSDR CA110914011Seat Back · cracked(CAN) DURING DESCENT, THE SEAT BACK ON THE PILOT`S SEAT BROKE AND FELL BACKWARDS. THE ACFT WAS ON AUTOPILOT SO THERE WAS NO TEMPORARY LOSS OF CONTROL. THE PILOT CONTINUED THE DESCENT AND LANDED NORMALLY. IT APPEARS TO BE A CLEAN BREAK ON THE EDGE OF THE WESep 12, 2011 · Gulstm 690C · Flight Compartment EquipmentSDR 2011FA0000321Scavenge Pump · failedPILOT REPORTED THAT THE RT ENGINE RPM ACCELERATED UNCOMMANDED FROM 98 PERCENT TO APPROXIMATELY 103.5 PERCENT MOMENTARILY, A FEW SECONDS LATER IT DID IT AGAIN AND THE PILOT ELECTED TO SHUTDOWN THE ENGINE AND LAND THE ACFT SINGLE ENGINE, HE DID SO WITHOUT INCIDEMay 17, 2011 · N840GH · Gulstm 690C · Turbine Engine Oil SystemSDR CA100816007Panel · crackedACFT WAS BEING MODIFIED IAW CK-159-3 KIT "UPPER DECK NOSE GEAR RETRACTION SUPPORT STRUCTURE MODIFICATION". MULTIPLE CRACK INDICATIONS WERE NOTED EXTENDING FROM EXISTING FASTENER HOLES AND PANEL CUTOUT RADIUS LOCATIONS IN THE 310181-97 AVIONICS DECK PANEL UNDEAug 16, 2010 · Gulstm 690A · Fuselage Miscellaneous StructureSDR CA090623006Gauge · leaking(CAN) GAUGE OVERHAULED, DATE MAR 24/2009. GAUGE HAS INTERNAL LEAK.Jun 23, 2009 · Gulstm 690A · Landing Gear SystemSDR CA081031002Housing · cracked(CAN) DURING THE REQUIRED 5 YEAR OVERHAUL ON THE LANDING GEAR, A CRACK WAS DISCOVERED ON THE MLG HSG VISUALLY. IR WAS CONFIRMED USING NDT METHODS LPI AS WELL AS EDDY CURRENT FOR CONFIRMATION. EDDY CURRENT READING INDICATED A DEPTH OF .040". THIS WAS THE FOct 29, 2008 · Gulstm 690A · Main Landing GearSDR XV6A200700002Fabric · tornDURING CRUISE FLIGHT, PILOT FELT A BUMP IN THE CONTROL COLUMN. CONTROL COLUMN MOVED UNCOMMANDED FORWARD AND AFT. POWER REDUCTION RESULTED IN NORMAL FLIGHT CHARACTERISTICS. AFTER NORMAL LANDING FOUND LEFT ELEVATOR UPPER SURFACE FABRIC TORN OFF. DURING INVESSep 24, 2007 · N403VA · Dorner DO228202 · Elevator, Plate/SkinSDR 2007F00052Tach Generator · false indicationLEFT RPM INDICATION ABNORMAL PERFORMED PRECAUTIONARY SHUTDOWN. INSPECTION FOUND TACH GENERATOR SHAFT BROKEN. REMOVED AND REPLACED TACH GENERATOR IAW AMM 77-11-03. ENGINE GROUND PERFORMANCE RUN C/W AND PASSED. ALL PARAMETERS NORMAL. AIRCRAFT APPROVED FOR RSep 4, 2007 · N403VA · Dorner DO228202 · Engine RPM Indicating SystemSDR 2007FA0000092Turbine Wheel · damagedINSPECTION OF ENGINE REVEALED DAMAGE TO 3RD STAGE TURBINE ROTOR VISIBLE THROUGH ENGINE TAILPIPE. ENGINE WAS REMOVED FROM AIRCRAFT AND THE TURBINE SECTION MODULE REMOVED TO INVESTIGATE FOR CAUSE OF DAMAGE. UPON INSPECTION 4 EA PINS WERE FOUND MISSING FROM 2NDJan 15, 2007 · N690LL · Gulstm 690B · Turbine SectionSDR 2006FA0000476Gear · crackedPILOT REPORTED DURING CRUISE LEVEL FLIGHT FEELING A SUDDEN VIBRATION AND HEARING A SCREAMING NOISE FROM THE LT ENGINE. PILOT THEN NOTICED TORQUE INDICATION ON LT ENGINE INDICATING 120 PERCENT WITH NO YAW INDICATED OR NOTICED BY PILOT. WHILE RETARDING LT POWERApr 26, 2006 · N777LP · Mtsbsi MU2B36A · Turbine Engine Reduction GearSDR XV62005F00002Adapter · crackedOIL FILTER ADAPTER CRACKED AT MOUNTING PLATE. (WP19200505213) (K)Feb 14, 2005 · N405VA · Dorner DO228202 · Turbine Engine Oil SystemSDR CA041209006Strap · corroded(CAN) DURING REPLACEMENT OF LOWER SPAR CAP, WE WERE ADVISED THAT AN NEW AD IS PENDING AND WILL BE ISSUED IN JANUARY 2005 TO ADDRESS A CORROSION PROBLEM WITH THE PART NUMBERS. THE STRAPS WERE REMOVED AND EXTENSIVE CORROSION WAS FOUND UNDER THE STEEL STRAPS ON TNov 24, 2004 · Gulstm 690A · Wing Miscellaneous StructureSDR MV52004F00001Pulley · fodWHILE IN FLIGHT, PILOT EXPERIENCED SEVERE AILERON BINDING. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. AFTER INSPECTION OF THE COMPLETE AILERON SYSTEM, IT IS SUSPECTED THAT FOD HAD COME IN CONTACT BETWEEN THE AFT AILERON PULLEY AND CASep 21, 2004 · N690HM · Gulstm 690A · Aileron Control SystemSDR XV62005F00001Adapter · crackedOIL FILTER ADAPTER CRACKED AT MOUNTING PLATE. (WP19200501116)Sep 5, 2004 · N405VA · Dorner DO228202 · Turbine Engine Oil SystemSDR CA020829007Windshield · cracked(CAN) PILOTS WINDSHIELD CRACKED AFTER TAKEOFF, CLIMBING THROUGH 2,000 FEET. AIRCRAFT FLOWN TO HOME BASE UNPRESSURIZED.Aug 13, 2002 · Gulstm 690A · Window/Windshield SystemSDR IZ22001F00004Solenoid Valve · leakingPILOT REPORTED FUEL LEAKING FROM COWLING. INVESTIGATION FOUND FUEL LEAK FROM MATING SURFACES OF PRIMARIES ONLY SOLENOID VALVE. REPLACED VALVE WITH SN 3894.Nov 7, 2001 · N895MA · Mtsbsi MU2B36A · Engine Fuel Distribution
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