# GE GE90-77B

- Type: Engine model (FAA registry)
- Registry code: 30043
- Manufacturer (registry): GE
- Model: GE90-77B
- Engine type: Turbo-fan
- Power: 81,700 lb thrust
- Data sheet: [TCDS E00049EN](https://openairdocs.org/tcds/E00049EN) (OpenAirDocs)
- Holder: General Electric Company GE Aviation
- Installed in: 0 registered aircraft
- Page: https://openairdocs.org/engine/ge-ge90-77b

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 2018-17-12](https://openairdocs.org/ad/2018-17-12): Turbine Engine Compressor Section · General Electric GE90-76B, GE90-77B, GE90-85B and 2 more. Effective Sep 24, 2018
- [AD 2017-08-05](https://openairdocs.org/ad/2017-08-05): Engine Compressor Section · General Electric GE90-76B, GE90-77B, GE90-85B and 2 more. Effective May 19, 2017
- [AD 2016-19-09](https://openairdocs.org/ad/2016-19-09): High-pressure compressor (HPC) · General Electric GE90-76B, GE90-77B, GE90-85B and 2 more. Effective Nov 4, 2016
- [AD 2015-27-01](https://openairdocs.org/ad/2015-27-01): High-pressure compressor (HPC) stage 8-10 spool · General Electric GE90-76B, GE90-77B, GE90-85B and 2 more. Effective Jan 27, 2016
- [AD 2013-15-20](https://openairdocs.org/ad/2013-15-20): Transfer gearbox assembly (TGB) radial gearshafts · General Electric GE90-110B1, GE90-113B, GE90-115B and 5 more. Effective Aug 21, 2013
- [AD 2011-15-06](https://openairdocs.org/ad/2011-15-06): High-pressure compressor rotor (HPCR) · General Electric GE90-76B, GE90-77B, GE90-85B and 2 more. Effective Aug 18, 2011
- [AD 2002-04-11](https://openairdocs.org/ad/2002-04-11): Life Limits Section of Instructions for Continued Airworthiness (ICA) · General Electric GE90-76B, GE90-77B, GE90-85B and 2 more. Effective Apr 8, 2002
- [AD 2002-01-12](https://openairdocs.org/ad/2002-01-12): High Pressure Turbine (HPT) Interstage Seal · General Electric GE90-76B, GE90-77B, GE90-85B and 2 more. Effective Feb 26, 2002
- [AD 2002-01-27](https://openairdocs.org/ad/2002-01-27): High Pressure Compressor Stage 2-6 Spool · General Electric GE90-76B, GE90-77B, GE90-85B and 1 more. Effective Feb 14, 2002
- [AD 2001-21-03](https://openairdocs.org/ad/2001-21-03): P3B and Ps3 Sense Lines · General Electric GE90-76B, GE90-77B, GE90-85B and 1 more. Effective Nov 26, 2001
- [AD 97-12-05](https://openairdocs.org/ad/97-12-05): (VSCF) Gearshaft Flange ball Bearing · General Electric GE90-76B, GE90-77B, GE90-85B and 1 more. Effective Jun 27, 1997
- [AD 97-12-04](https://openairdocs.org/ad/97-12-04): Liberated CDP Manifold Material · General Electric Aircraft Engines GE90-92B, GE90-76B, GE90-77B and 2 more. Effective Jun 27, 1997

Historical (superseded or no longer in force):

- [AD 2016-13-05](https://openairdocs.org/ad/2016-13-05) (historical): High-pressure compressor (HPC) stage 8-10 spool · General Electric GE90-76B, GE90-77B, GE90-85B and 2 more. Effective Jul 29, 2016
- [AD 2000-08-10](https://openairdocs.org/ad/2000-08-10) (historical): Life-limited Rotating Engine Parts · General Electric Aircraft Engines GE90-76B, GE90-77B, GE90-85B and 1 more. Effective Oct 23, 2000
- [AD 99-27-15](https://openairdocs.org/ad/99-27-15) (historical): Full Authority Digital Engine Control · General Electric Aircraft Engines GE90-76B, GE90-77B, GE90-85B and 17 more. Effective Jan 11, 2000
- [AD 99-08-17](https://openairdocs.org/ad/99-08-17) (historical): General Electric Aircraft Engines GE90-76B, GE90-77B, GE90-85B and 2 more. Effective May 13, 1999
- [AD 98-15-03](https://openairdocs.org/ad/98-15-03) (historical): High Pressure Compressor · General Electric Aircraft Engines GE90-76B, GE90-77B, GE90-85B and 17 more. Effective Jul 29, 1998

## Registered aircraft

None registered with this engine model now.

## NTSB investigations

None matched to aircraft with this engine model.

## FAA accident and incident reports

None matched to aircraft with this engine model.

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