# Garrett TFE731-3D

- Type: Engine model (FAA registry)
- Registry code: 29100
- Manufacturer (registry): GARRETT
- Model: TFE731-3D
- Engine type: Turbo-fan
- Power: 3,700 lb thrust
- Data sheet: [TCDS E6WE](https://openairdocs.org/tcds/E6WE) (OpenAirDocs)
- Holder: Honeywell Aerospace US LLC
- Installed in: 1 registered aircraft
- Page: https://openairdocs.org/engine/garrett-tfe731-3d

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 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 2008-02-19](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 2005-13-07](https://openairdocs.org/ad/2005-13-07): Turbine rotor discs. · Honeywell International TFE731-2, TFE731-2A, TFE731-2B and 12 more. Effective Jul 27, 2005
- [AD 2001-23-09](https://openairdocs.org/ad/2001-23-09): Fan Rotor Discs · Honeywell International TFE731-2, TFE731-2A, TFE731-2B and 14 more. Effective Dec 21, 2001
- [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 98-17-01 R1](https://openairdocs.org/ad/98-17-01-R1): Flex Fuel Tube · Honeywell International TFE731-2, TFE731-2A, TFE731-2B and 14 more. Effective Nov 29, 1999
- [AD 96-05-03](https://openairdocs.org/ad/96-05-03): Fan rotor disks · Honeywell International TFE731-2, TFE731-2A, TFE731-2B and 13 more. Effective Apr 2, 1996
- [AD 96-04-01](https://openairdocs.org/ad/96-04-01): Fan Rotor Assembly · Honeywell International TFE731-2, TFE731-2A, TFE731-2B and 12 more. Effective Mar 15, 1996
- [AD 82-23-03 R1](https://openairdocs.org/ad/82-23-03-R1): High Pressure Compressor Impellers · Honeywell International TFE731-2, TFE731-2A, TFE731-2B and 12 more. Effective Dec 9, 1983
- [AD 75-07-10](https://openairdocs.org/ad/75-07-10): Transfer Gearbox Vertical Bevel Gear Bearing · Honeywell International TFE731-2, TFE731-2A, TFE731-2B and 12 more. Effective May 1, 1975

Historical (superseded or no longer in force):

- [AD 98-17-01](https://openairdocs.org/ad/98-17-01) (historical): Honeywell International TFE731-2, TFE731-2A, TFE731-2B and 14 more. Effective Oct 13, 1998
- [AD 96-18-13](https://openairdocs.org/ad/96-18-13) (historical): Fan rotor disk · Honeywell International TFE731-2, TFE731-2A, TFE731-3 and 10 more. Effective Nov 12, 1996

## Registered aircraft (1)

- [N49GG](https://openairdocs.org/aircraft/N49GG): [Gainesville Aircraft Sales Inc](https://openairdocs.org/faa-owner/GAINESVILLE%20AIRCRAFT%20SALES%20INC), [Gainesville, FL](https://openairdocs.org/faa-place/FL/Gainesville), built 1981, S/N 132120

## 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 (4)

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

- [SDR 2010FA0000511](https://openairdocs.org/sdr/2010FA0000511), Jan 21, 2009: CABIN PRESSURE. FAILED. AFTER INITIAL TO FL260 THE CREW HEARD A LOUD SOUND FOLLOWED BY AN IMMEDIATE RAPID LOSS OF PRESSURIZATION.
- [SDR PRI2007F00000](https://openairdocs.org/sdr/PRI2007F00000), Aug 1, 2007: WIRE HARNESS. DAMAGED. DURING A ROUTINE BLOCK INSPECTION, A VISUAL INSPECTION OF THE WINGS REVEALED MULTIPLE WIRES SHOWING DAMAGE IN THE FLAP WELL AREA, FWD OF THE IB FLAPS. THE CAUSE
- [SDR 20010321CW001](https://openairdocs.org/sdr/20010321CW001), Feb 9, 2001: TIRE. FLAT. UPON LANDING, CREW NOTICED ON POST FLIGHT NR 2 TIRE, FLAT SPOTED. DISPATCHED MAINTENANCE TECH. WITH THE APPROPRIATE PARTS, REMOVED AND REPLACED NR2 MAIN WHEEL A
- [SDR 20000830SH001](https://openairdocs.org/sdr/20000830SH001), Aug 21, 2000: DISK. CRACKED. C/W NDT INSPECTION AND FOUND FORWARD RIM CRACKED IN 7 EACH PLACES AND 1 EACH DOVE TAIL CRACKED. (X)

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