# Service difficulty reports: Garrett TPE331-10T

A list on [Garrett TPE331-10T](https://openairdocs.org/engine/garrett-tpe331-10t.md).

Newest first. General aviation reporting is voluntary.

- [SDR V8ZA202009100001](https://openairdocs.org/sdr/V8ZA202009100001.md): Fitting · detached · Sep 8, 2020 · N112EE · Gulstm 690A · Rudder Control System
  > PILOT 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 ACCOMPLISH
- [SDR XV6A2016052200002](https://openairdocs.org/sdr/XV6A2016052200002.md): Unknown · odor · May 22, 2016 · N501VA · Dorner DO228202 · Air Distribution System
  > ELECTRICAL "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 RE
- [SDR XV6A2016050300001](https://openairdocs.org/sdr/XV6A2016050300001.md): Hose · chafed · May 3, 2016 · N409VA · Dorner DO228202 · Hydraulic System, Main
  > AFTER 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 O
- [SDR CA160222010](https://openairdocs.org/sdr/CA160222010.md): Fuel Line · worn · Feb 22, 2016 · Gulstm 690D · Engine Fuel Distribution
  > (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 OI
- [SDR CA150831007](https://openairdocs.org/sdr/CA150831007.md): Filter · missing · Aug 28, 2015 · Gulstm 690A · Fuel Control/Turbine Engines
  > (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.
- [SDR XV6A2014071500002](https://openairdocs.org/sdr/XV6A2014071500002.md): Engine · warning light · Jul 15, 2014 · N405VA · Dorner DO228202 · Engine (Turbine/Turboprop)
  > DURING 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 SERVICE
- [SDR XV6A2013112500009](https://openairdocs.org/sdr/XV6A2013112500009.md): Shutoff Valve · stuck · Nov 25, 2013 · N402VA · Dorner DO228202 · Fuel Controlling System
  > LEFT 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 3
- [SDR CA130904010](https://openairdocs.org/sdr/CA130904010.md): Angle · cracked · Aug 1, 2013 · Gulstm 690A · Main Landing Gear Attach Section
  > (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 USI
- [SDR CA140107004](https://openairdocs.org/sdr/CA140107004.md): Fairing · unknown · Mar 26, 2013 · Gulstm 690A · Aerodynamic Fairings
  > (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 WA
- [SDR CA120127011](https://openairdocs.org/sdr/CA120127011.md): Adapter · cracked · Jan 25, 2012 · Gulstm 690A · Starter-Generator
  > (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 ADA
- [SDR O9IA2011112100011](https://openairdocs.org/sdr/O9IA2011112100011.md): Motor · burned out · Nov 21, 2011 · N83WA · Gulstm 695B · Air Distribution Fan
  > DURING CRUISE FLIGHT AIR CONDITIONER BLOWER FAN FAILED CAUSING SMOKE TO ENTER CABIN.
- [SDR XV6A2011102500015](https://openairdocs.org/sdr/XV6A2011102500015.md): Thermocouple · faulty · Oct 25, 2011 · N405VA · Dorner DO228202 · Engine Oil Temperature
  > DURING 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
- [SDR CA110914011](https://openairdocs.org/sdr/CA110914011.md): Seat Back · cracked · Sep 12, 2011 · Gulstm 690C · Flight Compartment Equipment
  > (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 WE
- [SDR 2011FA0000321](https://openairdocs.org/sdr/2011FA0000321.md): Scavenge Pump · failed · May 17, 2011 · N840GH · Gulstm 690C · Turbine Engine Oil System
  > PILOT 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 INCIDE
- [SDR CA100816007](https://openairdocs.org/sdr/CA100816007.md): Panel · cracked · Aug 16, 2010 · Gulstm 690A · Fuselage Miscellaneous Structure
  > ACFT 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 UNDE
- [SDR CA090623006](https://openairdocs.org/sdr/CA090623006.md): Gauge · leaking · Jun 23, 2009 · Gulstm 690A · Landing Gear System
  > (CAN) GAUGE OVERHAULED, DATE MAR 24/2009. GAUGE HAS INTERNAL LEAK.
- [SDR CA081031002](https://openairdocs.org/sdr/CA081031002.md): Housing · cracked · Oct 29, 2008 · Gulstm 690A · Main Landing Gear
  > (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 F
- [SDR XV6A200700002](https://openairdocs.org/sdr/XV6A200700002.md): Fabric · torn · Sep 24, 2007 · N403VA · Dorner DO228202 · Elevator, Plate/Skin
  > DURING 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 INVES
- [SDR 2007F00052](https://openairdocs.org/sdr/2007F00052.md): Tach Generator · false indication · Sep 4, 2007 · N403VA · Dorner DO228202 · Engine RPM Indicating System
  > LEFT 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 R
- [SDR 2007FA0000092](https://openairdocs.org/sdr/2007FA0000092.md): Turbine Wheel · damaged · Jan 15, 2007 · N690LL · Gulstm 690B · Turbine Section
  > INSPECTION 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 2ND
- [SDR 2006FA0000476](https://openairdocs.org/sdr/2006FA0000476.md): Gear · cracked · Apr 26, 2006 · N777LP · Mtsbsi MU2B36A · Turbine Engine Reduction Gear
  > PILOT 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 POWER
- [SDR XV62005F00002](https://openairdocs.org/sdr/XV62005F00002.md): Adapter · cracked · Feb 14, 2005 · N405VA · Dorner DO228202 · Turbine Engine Oil System
  > OIL FILTER ADAPTER CRACKED AT MOUNTING PLATE. (WP19200505213) (K)
- [SDR CA041209006](https://openairdocs.org/sdr/CA041209006.md): Strap · corroded · Nov 24, 2004 · Gulstm 690A · Wing Miscellaneous Structure
  > (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 T
- [SDR MV52004F00001](https://openairdocs.org/sdr/MV52004F00001.md): Pulley · fod · Sep 21, 2004 · N690HM · Gulstm 690A · Aileron Control System
  > WHILE 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 CA
- [SDR XV62005F00001](https://openairdocs.org/sdr/XV62005F00001.md): Adapter · cracked · Sep 5, 2004 · N405VA · Dorner DO228202 · Turbine Engine Oil System
  > OIL FILTER ADAPTER CRACKED AT MOUNTING PLATE. (WP19200501116)
- [SDR CA020829007](https://openairdocs.org/sdr/CA020829007.md): Windshield · cracked · Aug 13, 2002 · Gulstm 690A · Window/Windshield System
  > (CAN) PILOTS WINDSHIELD CRACKED AFTER TAKEOFF, CLIMBING THROUGH 2,000 FEET. AIRCRAFT FLOWN TO HOME BASE UNPRESSURIZED.
- [SDR IZ22001F00004](https://openairdocs.org/sdr/IZ22001F00004.md): Solenoid Valve · leaking · Nov 7, 2001 · N895MA · Mtsbsi MU2B36A · Engine Fuel Distribution
  > PILOT REPORTED FUEL LEAKING FROM COWLING. INVESTIGATION FOUND FUEL LEAK FROM MATING SURFACES OF PRIMARIES ONLY SOLENOID VALVE. REPLACED VALVE WITH SN 3894.

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/engine/garrett-tpe331-10t/reports

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