# Garrett TFE731-5AR

- Type: Engine model (FAA registry)
- Registry code: 29106
- Manufacturer (registry): GARRETT
- Model: TFE731-5AR
- Engine type: Turbo-fan
- Power: 4,500 lb thrust
- Data sheet: [TCDS E6WE](https://openairdocs.org/tcds/E6WE) (OpenAirDocs)
- Holder: Honeywell Aerospace US LLC
- Installed in: 3 registered aircraft
- Page: https://openairdocs.org/engine/garrett-tfe731-5ar

Model codes come from the FAA registry's reference file.

## ADs that may apply (OpenAirDocs)

Matched to this engine model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment.

- [AD 2016-07-02](https://openairdocs.org/ad/2016-07-02): Failure of the interstage turbine transition duct · Honeywell International TFE731-4, TFE731-4R, TFE731-5AR and 2 more. Effective May 5, 2016
- [AD 2014-12-52](https://openairdocs.org/ad/2014-12-52): Engines · Honeywell International TFE731-20AR, TFE731-20BR, TFE731-20R and 11 more. Effective Jul 28, 2014
- [AD 2012-17-05](https://openairdocs.org/ad/2012-17-05): First stage low-pressure turbine (LPT1) rotor assembly · Honeywell International TFE731-4, TFE731-4R, TFE731-5 and 3 more. Effective Oct 2, 2012
- [AD 2010-06-11](https://openairdocs.org/ad/2010-06-11): Second stage low-pressure compressor rotor (LPCR) discs · Honeywell International TFE731-2, TFE731-2A, TFE731-2C and 16 more. Effective Apr 21, 2010
- [AD 2008-19-12](https://openairdocs.org/ad/2008-19-12): ITT duct · Honeywell International TFE731-4, TFE731-4R, TFE731-5 and 3 more. Effective Oct 27, 2008
- [AD 2008-02-19](https://openairdocs.org/ad/2008-02-19): High pressure (HP) turbine rotor assemblies · Honeywell International TFE731-20AR, TFE731-20BR, TFE731-20R and 15 more. Effective Mar 6, 2008
- [AD 2000-15-09](https://openairdocs.org/ad/2000-15-09): HPC Impeller · Honeywell International TFE731-2, TFE731-2A, TFE731-2B and 20 more. Effective Oct 10, 2000
- [AD 90-24-06](https://openairdocs.org/ad/90-24-06): Thermocouple Lead Assemblies · Honeywell International TFE731-2, TFE731-2A, TFE731-3 and 8 more. Effective Nov 13, 1990
- [AD 89-22-16](https://openairdocs.org/ad/89-22-16): Engine Acceleration or Deceleration · Honeywell International TFE731-2, TFE731-5, TFE731-5AR and 1 more

## Registered aircraft (3)

- [N450FV](https://openairdocs.org/aircraft/N450FV): [Yellowdome LLC](https://openairdocs.org/faa-owner/YELLOWDOME%20LLC), [Emigrant, MT](https://openairdocs.org/faa-place/MT/Emigrant), built 1992, S/N 112
- [N7BD](https://openairdocs.org/aircraft/N7BD): [757bd LLC](https://openairdocs.org/faa-owner/757BD%20LLC), [Albuquerque, NM](https://openairdocs.org/faa-place/NM/Albuquerque), built 1987, S/N 31
- [N9CU](https://openairdocs.org/aircraft/N9CU): [Jani King International Inc](https://openairdocs.org/faa-owner/JANI%20KING%20INTERNATIONAL%20INC), [Addison, TX](https://openairdocs.org/faa-place/TX/Addison), built 1987, S/N 19

## NTSB investigations

None matched to aircraft with this engine model.

## FAA accident and incident reports

None matched to aircraft with this engine model.

## Service difficulty reports (1)

As reported by operators and repair stations, by the model named in the report.

- [SDR Y9PA20150911001](https://openairdocs.org/sdr/Y9PA20150911001), Aug 19, 2015: BEARING. DISINTEGRATED. AFTER LANDING, & TURNING OFF THE RUNWAY, THE CREW HEARD A POP, AFTER STOPPING AT THE FBO, THE CREW NOTICED THE NR 2 MAIN TIRE HAD LOST THE NITROGEN CHARGE. R & 

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