# Service difficulty reports: Garrett TPE331-8

A list on [Garrett TPE331-8](https://openairdocs.org/engine/garrett-tpe331-8.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 2 · 89 reports

- [SDR DSCR20151005001](https://openairdocs.org/sdr/DSCR20151005001.md): Relief Valve · fractured · Sep 24, 2015 · N14FJ · Cessna 441 · Engine Fuel Pump
  > DURING CRUISE PHASE OF FLIGHT, THE RT ENG EXPERIENCED LOSS OF FUEL PRESS. PILOT SHUT THE RT ENG DOWN, CONTACTED ATC & WAS DIVERTED. TECHNICIANS INSPECTED THE ENG & FOUND THE CAP HAD SEPARATED FROM THE HIGH PRESS RELIEF VLV, WHICH RESULTED IN THE LOSS OF FUEL
- [SDR 5XWR201307110363](https://openairdocs.org/sdr/5XWR201307110363.md): Structure · misoverhauled · Jul 11, 2013 · N440DA · Cessna 441 · Fuselage Main, Structure
  > PERFORMED A PHASE 2, 3, & D, TASK A361004, BLEED AIR LINE EXHIBITED CORROSION WHERE ITS FLANGE FASTENS TO THE FUSELAGE SKIN BS 187.87 RBL 27, AND WL 62.79. ON DISASSEMBLY, FLANGE TO FUSELAGE JOINT FOUND WITH HEAVY DISSIMILAR METAL CORROSION. INVESTIGATION
- [SDR CA080304011](https://openairdocs.org/sdr/CA080304011.md): Actuator · failed · Jan 18, 2008 · Cessna 441 · Landing Gear Actuator
  > (CAN) AIRCRAFT INDICATED (3 GREEN) ON APPROACH, UPON LANDING, NOSE GEAR RETRACTED RESULTING IN AC DAMAGE. UPON ARRIVAL, MAINT NOTED GEAR INDICATION REMAINED (3 GREEN) AND AC WAS SITTING ON ITS NOSE. THE AC WAS RAISED AND THE NOSE GEAR WAS PULLED INTO THE DOWN
- [SDR AU510001538](https://openairdocs.org/sdr/AU510001538.md): Tensioner · sheared · Dec 12, 2005 · Cessna 441 · HF Communications System
  > HF ANTENNA SUPPORT AND TENSION UNIT SNAPPED AT ANTENNA CONNECTION TO VERTICAL STABILIZER.
- [SDR AU510001559](https://openairdocs.org/sdr/AU510001559.md): Actuator · faulty · Dec 12, 2005 · Cessna 441 · Landing Gear Actuator
  > RT MAIN LANDING GEAR NIL DOWN INDICATION.
- [SDR AU510001724](https://openairdocs.org/sdr/AU510001724.md): Rivet · cracked · Dec 12, 2005 · Cessna 441 · Elevator Structure
  > ELEVATOR LT OUTBOARD HINGE BRACKET ATTACHMENT RIVET HEAD CRACKED. FOUND DURING INSPECTION IAW AD/C400/102 AMDT3.
- [SDR AU510001767](https://openairdocs.org/sdr/AU510001767.md): Cap · cracked · Dec 12, 2005 · Cessna 441 · Wing, Rib/Bulkhead
  > (AUS) RT WING CANTED RIB CAP CRACKED. CRACK LENGTH APPROXIMATELY 40MM (1.574IN). CRACK WAS LOCATED IN THE RADIUS OF THE UPPER CAP AND TRAVELLED REARWARDS FROM THE AUXILIARY SPAR. FOUND DURING NDI IAW SB CQB03-01 PART B REV 1. (AD/SB DESC: SB CQB03-01 PART B RE
- [SDR AU510001768](https://openairdocs.org/sdr/AU510001768.md): Bracket · cracked · Dec 12, 2005 · Cessna 441 · Elevator Structure
  > (AUS) LT ELEVATOR OB HINGE ASSY IB ATTACHMENT BRACKET CRACKED IN LOWER FORWARD RADIUS. FOUND DURING INSPECTION IAW AD/C400/102 AMDT 3 PART 3. BOTH LT AND RT ELEVATOR OB BRGS STIFF IN OPERATION. (AD/SB DESC: AD/C400/102 AMDT 3 PART 3) (CASA NR 510001768)
- [SDR AU510001769](https://openairdocs.org/sdr/AU510001769.md): Bulb · burned out · Dec 12, 2005 · Cessna 441 · Landing Gear Position and Warning
  > (AUS) RT MAIN LANDING GEAR POSITION INDICATOR LIGHT BULB BLOWN. (CASA NR 510001769)
- [SDR AU510001776](https://openairdocs.org/sdr/AU510001776.md): Rib · cracked · Dec 12, 2005 · Cessna 441 · Wing, Rib/Bulkhead
  > LT WING ROOT CANTED RIB UPPER CAP LOCATED AT CWS 26.85 CRACKED.
- [SDR AU510001885](https://openairdocs.org/sdr/AU510001885.md): Rib · cracked · Dec 12, 2005 · Cessna 441 · Wing, Rib/Bulkhead
  > RT CANTED RIB CAP CRACKED BENEATH REPAIR.
- [SDR AU510001886](https://openairdocs.org/sdr/AU510001886.md): Rib · cracked · Dec 12, 2005 · Cessna 441 · Wing, Rib/Bulkhead
  > RT CANTED RIB CAP FORWARD PN 5720001-4S AND AFT PN 5720001-6S ANGLES CRACKED, FOUND DURING EDDY CURRENT INSPECTION.
- [SDR AU510001944](https://openairdocs.org/sdr/AU510001944.md): Governor · faulty · Dec 12, 2005 · Cessna 441 · Propeller Governor
  > (AUS) RT ENGINE PROPELLER GOVERNOR FAULTY. INVESTIGATION CONTINUING. (CASA NR 510001944)
- [SDR AU510001993](https://openairdocs.org/sdr/AU510001993.md): Altimeter · failed · Dec 12, 2005 · Cessna 441 · Altimeter, Barometric/Encoder
  > ENCODING ALTIMETER FAILED.
- [SDR AU510002026](https://openairdocs.org/sdr/AU510002026.md): Engine · seized · Dec 12, 2005 · Cessna 441 · Engine (Turbine/Turboprop)
  > RT ENGINE SEIZED. INVESTIGATION CONTINUING.
- [SDR AU510002156](https://openairdocs.org/sdr/AU510002156.md): Door · separated · Dec 12, 2005 · Cessna 441 · Cargo/Baggage Doors
  > LT FORWARD NOSE LOCKER SEPARATED FROM AIRCRAFT SEVERING BOTH HINGES. ONE BAG LOST OVERBOARD. DOOR STRUCK PROPELLER CAUSING A TORQUE SHIFT IN THE ENGINE. LT ENGINE, PROPELLER AND LT WING INBOARD LEADING EDGE DAMAGED. INVESTIGATION CONTINUING.
- [SDR AU510002181](https://openairdocs.org/sdr/AU510002181.md): Acm · failed · Dec 12, 2005 · Cessna 441 · Cabin Cooling System
  > AIR CYCLE MACHINE (ACM) FAILED AND EMERGENCY PRESSURISATION VALVE AUTOMATICALLY OPENED.
- [SDR AU510002089](https://openairdocs.org/sdr/AU510002089.md): Skin · cracked · Oct 11, 2005 · Cessna 441 · Nacelle/Pylon, Plate/Skin
  > UPPER AFT RT NACELLE SKIN CRACKED AND CORRODED.
- [SDR AU510001809](https://openairdocs.org/sdr/AU510001809.md): Rib · cracked · Feb 9, 2005 · Cessna 441 · Wing, Rib/Bulkhead
  > LT WING UPPER FORWARD PN 572001-3S AND AFT PN 572001-5S DRAG ANGLES CRACKED. FOUND DURING EDDY CURRENT INSPECTION IAW CQB03-1 REV 1. EDDY CURRENT INSPECTION REVEALED A TOTAL OF NINE CRACKS ALL AROUND 5MM (0.196IN) IN LENGTH.
- [SDR AUS20040448](https://openairdocs.org/sdr/AUS20040448.md): Selector Valve · faulty · May 21, 2004 · Cessna 441 · Landing Gear Selector
  > (AUS) LANDING GEAR SELECTOR VALVE SOLENOID FAILED.
- [SDR AUS20040447](https://openairdocs.org/sdr/AUS20040447.md): O-Ring · damaged · May 17, 2004 · Cessna 441 · Landing Gear Actuator
  > (AUS) NOSE LANDING GEAR UPLOCK ACTUATOR O-RING DAMAGED. HYDRAULIC FLUID LEAKING FROM ACTUATOR BODY.
- [SDR AUS20040368](https://openairdocs.org/sdr/AUS20040368.md): Boot · failed · Apr 29, 2004 · Cessna 441 · Airfoil Anti/De-ice System
  > (AUS) RT WING OUTER DE-ICE BOOT BURST AT THE UPPER SEAM AND SPLIT FOR THE ENTIRE LENGTH FROM THE OB RT NACELLE TO THE WINGTIP.
- [SDR AUS20040324](https://openairdocs.org/sdr/AUS20040324.md): Wire · worn · Apr 27, 2004 · Cessna 441 · Fuel System Wiring
  > (AUS) RT FUEL TANK QUANTITY WIRE CHAFED ON STRINGERS LOCATED AT STATION PWS 61.80.
- [SDR AUS20040327](https://openairdocs.org/sdr/AUS20040327.md): Pump · cracked · Apr 24, 2004 · Cessna 441 · Turbine Engine Oil System
  > (AUS) ENGINE OIL PUMP HOUSING CRACKED.
- [SDR AUS20040333](https://openairdocs.org/sdr/AUS20040333.md): Valve · leaking · Apr 21, 2004 · Cessna 441 · Fuel Controlling System
  > (AUS) START FUEL VALVE LEAKING BETWEEN VALVE BODY AND SOLENOID.
- [SDR AUS20040183](https://openairdocs.org/sdr/AUS20040183.md): Pipe · cracked · Mar 8, 2004 · Cessna 441 · Hydraulic System, Main
  > (AUS) HYDRAULIC PIPE CRACKED AND LEAKING. LOSS OF HYDRAULIC FLUID. PIPE IS LOCATED IN RT WING LEADING EDGE. INVESTIGATION FOUND TOOLING MARKS ON THE PIPE IN THE AREA OF THE PIPE BEND.
- [SDR AUS20040128](https://openairdocs.org/sdr/AUS20040128.md): Switch · out of adjust · Feb 24, 2004 · Cessna 441 · Landing Gear Position and Warning
  > (AUS) LT MAIN LANDING GEAR UPLOCK SWITCH OUT OF ADJUSTMENT. MICROSWITCH WAS SWITCHING OFF LOADING VALVE BUT NOT THE IN TRANSIT LIGHT. INVESTIGATION FOUND SOME WEAR IN THE SWITCH WHICH AFFECTED ADJUSTMENT.
- [SDR CA040220007](https://openairdocs.org/sdr/CA040220007.md): Valve · failed · Feb 18, 2004 · Cessna 441 · Pressure Regulator/Outflow Valve
  > (CAN) DURING THE CLIMB THE AIRCRAFT EMERGENCY PRESSURIZATION VALVE OPENED WITH OUT BEING SELECTED. THE CREW DEPRESSURIZED THE AIRCRAFT AND RETURNED TO BASE. THE EMERGENCY PRESSURIZATION VALVE WAS REPLACED AND THE AIRCRAFT SYSTEMS FUNCTION CHECKED SERVICABLE
- [SDR AUS20040076](https://openairdocs.org/sdr/AUS20040076.md): Spar · debonded · Feb 11, 2004 · Cessna 441 · Wing Spar
  > (AUS) LT WING SPAR WEB DISBONDED IN AREA LOCATED AT CWS 57.
- [SDR AUS20040037](https://openairdocs.org/sdr/AUS20040037.md): Bracket · cracked · Jan 21, 2004 · Cessna 441 · Wing, Control Surface Attach Fittings
  > (AUS) LT WING OB AILERON ATTACHMENT BRACKET CRACKED. INVESTIGATION FOUND INDICATIONS OF SURFACE INTERGRANNULAR CORROSION AND CONFIRMATION OF A CRACK LOCATED APPROXIMATELY 3.175MM (0.125IN) BEHIND THE BEARING HOUSING. CRACK LENGTH APPROXIMATELY 12.7MM (0.5IN).
- [SDR AUS20031313](https://openairdocs.org/sdr/AUS20031313.md): Seal · leaking · Dec 16, 2003 · Cessna 441 · Turbine Engine Compressor Section
  > (AUS) RT ENGINE COMPRESSOR SEAL SUSPECT FAULTY. LEAKING OIL CAUSED SMOKE IN COCKPIT.
- [SDR AUS20031179](https://openairdocs.org/sdr/AUS20031179.md): Tire · deflated · Nov 14, 2003 · Cessna 441 · Tire
  > (AUS) RT MAIN LANDING GEAR TIRE, DEFLATED DURING LANDING ROLL.
- [SDR AUS20030552](https://openairdocs.org/sdr/AUS20030552.md): Web · cracked · Jun 4, 2003 · Cessna 441 · Fuselage Main, Structure
  > (AUS) BEAM WEB CRACKED. CRACK LENGTH APPROXIMATELY 25.4MM (1IN).
- [SDR AUS20030595](https://openairdocs.org/sdr/AUS20030595.md): Beam · cracked · Jun 4, 2003 · Cessna 441 · Fuselage Main, Structure
  > (AUS) BEAM WEB CRACKED. CRACK LENGTH APPROXIMATELY 25.4MM (1IN).
- [SDR AUS20030485](https://openairdocs.org/sdr/AUS20030485.md): Bolt · missing · Apr 26, 2003 · Cessna 441 · Wheel/Ski/Float
  > (AUS) MAIN WHEEL BRAKE DISC RETAINING BOLTS (3OFF) MISSING AND FIVE BOLTS LOOSE.
- [SDR CA030421010](https://openairdocs.org/sdr/CA030421010.md): Bearing · failed · Dec 21, 2002 · Cessna 441 · Starter-Generator
  > (CAN) STARTER GEN WAS HAVING NEW BRUSHES SEATED AT MID-TBO USING GEN DRIVESTAND METHOD.APPRX 3 HRS INTO THE PROCESS, THE ANTI-DRIVE END BEARING FAILED COMPLETELY. 5 OF 8 BALLS DISINTEGRATED,AS DID THE CAGE.DAMAGE WAS SUSTAINED TO THE ARMATURE, STATOR, FAN AND
- [SDR AUS20021376](https://openairdocs.org/sdr/AUS20021376.md): Valve · failed · Nov 6, 2002 · Cessna 441 · Pressure Regulator/Outflow Valve
  > (AUS) EMERGENCY PRESSURISATION VALVE FAILED.
- [SDR AUS20021305](https://openairdocs.org/sdr/AUS20021305.md): Solenoid · leaking · Aug 28, 2002 · Cessna 441 · Engine Fuel Distribution
  > (AUS) LT ENGINE PRIMARY-ONLY SOLENOID LEAKING FROM VALVE BODY.
- [SDR AUS20020943](https://openairdocs.org/sdr/AUS20020943.md): Boot · split · Aug 19, 2002 · Cessna 441 · Airfoil Anti/De-ice System
  > (AUS) LEADING EDGE DE-ICE BOOT SPLIT LONGITUDINALLY.
- [SDR AUS20020792](https://openairdocs.org/sdr/AUS20020792.md): Valve · failed · Jul 16, 2002 · Cessna 441 · Engine Start Valves/Controls
  > (AUS) RT ENGINE PRIMARY FUEL SOLENOID VALVE FAULTY. INVESTIGATION FOUND THE OPERATING COIL SHORT CIRCUITED TO EARTH.
- [SDR CA020611001](https://openairdocs.org/sdr/CA020611001.md): Wire Harness · chafed · Jun 10, 2002 · Cessna 441 · Fuel System Wiring
  > (CAN) DURING INSPECTION AND COMPLYING WITH AD 2002-09-13 AND CESSNA SERVICE BULLITEN CQB02-1 REV. 1, FOUND THAT THE BLACK WIRE IN THE HARNESS WAS CHAFED THROUGH AND ARCING TO GROUND ON THE FUEL PUMP SHROUD. THE OTHER WIRES IN THE HARNESS WERE ALSO CHAFED, BU
- [SDR AUS20020577](https://openairdocs.org/sdr/AUS20020577.md): Pump · failed · Jun 4, 2002 · Cessna 441 · Turbine Engine Oil System
  > (AUS) LT ENGINE TORQUE FLUCTUATIONS. METAL CONTAMINATION OF OIL FILTER AND CHIP DETECTOR. SUSPECT CAUSED BY FAILURE OF OIL SCAVENGE PUMP.
- [SDR AUS20020530](https://openairdocs.org/sdr/AUS20020530.md): Wire Harness · chafed · May 31, 2002 · Cessna 441 · Fuel System Wiring
  > (AUS) FUEL BOOST PUMP WIRING HARNESSES CHAFED. FOUND DURING INSPECTION IAW AD/CESSNA400/111 (SB CQB02-1R1).
- [SDR AUS20020464](https://openairdocs.org/sdr/AUS20020464.md): Harness · worn · May 13, 2002 · Cessna 441 · Fuel System Wiring
  > (AUS) LT FUEL BOOST PUMP WIRING HARNESS CHAFED. FOUND DURING INSPECTION IAW SB CQB02-1.
- [SDR AUS20020453](https://openairdocs.org/sdr/AUS20020453.md): Fastener · misinstalled · May 9, 2002 · Cessna 441 · Fasteners
  > (AUS) CHERRY RIVETS IN FUSELAGE EMERGENCY EXIT DOOR CUTOUT FRAMEPREVENTING OPERATION OF EMERGENCY EXIT.
- [SDR AUS20020408](https://openairdocs.org/sdr/AUS20020408.md): Harness · chafed · May 4, 2002 · Cessna 441 · Fuel System Wiring
  > (AUS) LT FUEL TANK HARNESS WIRE CHAFFED BUT WITHIN ACCEPTABLE LIMITS OF SB CQB02-1. HARNESS MODIFIED IAW SB AND REINSTALLED.
- [SDR AUS20020409](https://openairdocs.org/sdr/AUS20020409.md): Harness · chafed · May 3, 2002 · Cessna 441 · Fuel System Wiring
  > (AUS) RT FUEL TANK HARNESS WIRE CHAFED BUT WITHIN ACCEPTABLE LIMITS OF SB CQB02-1. HARNESS MODIFIED IAW SB AND REINSTALLED.
- [SDR AUS20020323](https://openairdocs.org/sdr/AUS20020323.md): Pump · cracked · Mar 27, 2002 · Cessna 441 · Turbine Engine Oil System
  > (AUS) LT ENGINE OIL PRESSURE PUMP CRACKED.
- [SDR AUS20020263](https://openairdocs.org/sdr/AUS20020263.md): Pushrod · cracked · Mar 12, 2002 · Cessna 441 · Aileron Tab Control System
  > (AUS) LT AILERON TRIM TAB PUSH ROD AFT ROD END CRACKED ACROSS BEARING RETAINER. RODEND BEARING CORRODED. CRACK FOUND WHEN PUSHROD WAS REMOVED FOR REPLACEMENT DUE TO WEAR.
- [SDR AUS20020043](https://openairdocs.org/sdr/AUS20020043.md): Bearing · failed · Jan 22, 2002 · Cessna 441 · Trailing Edge Flap Control System
  > (AUS) LT OUTBOARD FLAP INBOARD BELLCRANK BEARING HAD EXCESSIVE PLAY. SUSPECT CAUSED BY WATER INGRESS.

Next page: https://openairdocs.org/engine/garrett-tpe331-8/reports.md?page=2

## 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 = 'TPE3318'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/engine/garrett-tpe331-8/reports

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