# GE CF6-80E1A1 - Type: Engine model (FAA registry) - Registry code: 30071 - Manufacturer (registry): GE - Model: CF6-80E1A1 - Engine type: Turbo-fan - Power: 63,290 lb thrust - Data sheet: [TCDS E41NE](https://openairdocs.org/tcds/E41NE) (OpenAirDocs) - Holder: General Electric Company - Installed in: 0 registered aircraft - Page: https://openairdocs.org/engine/ge-cf6-80e1a1 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 2020-13-08](https://openairdocs.org/ad/2020-13-08): Turbine Engine Compressor Section · General Electric CF6-80E1A1, CF6-80E1A2, CF6-80E1A3 and 2 more. Effective Aug 11, 2020 - [AD 2016-08-10](https://openairdocs.org/ad/2016-08-10): Accessory heat shield · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 26 more. Effective Jun 1, 2016 - [AD 2016-06-14](https://openairdocs.org/ad/2016-06-14): Rotating compressor discharge pressure (CDP) seal · General Electric CF6-80E1A1, CF6-80E1A2, CF6-80E1A3 and 2 more. Effective May 9, 2016 - [AD 2014-21-01](https://openairdocs.org/ad/2014-21-01): Fuel manifold · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 26 more. Effective Nov 28, 2014 - [AD 2009-07-03](https://openairdocs.org/ad/2009-07-03): Eddy current inspection (ECI) · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 26 more. Effective Apr 30, 2009 - [AD 2009-04-10](https://openairdocs.org/ad/2009-04-10): Critical life-limited parts · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 30 more. Effective Mar 30, 2009 - [AD 2008-21-11](https://openairdocs.org/ad/2008-21-11): Low-pressure turbine (LPT) cases · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 25 more. Effective Nov 28, 2008 - [AD 2007-18-10](https://openairdocs.org/ad/2007-18-10): Compressor rear frames (CRFs) · General Electric CF6-80E1A1, CF6-80E1A2, CF6-80E1A3 and 2 more. Effective Sep 26, 2007 - [AD 2007-17-01](https://openairdocs.org/ad/2007-17-01): Removing electronic control unit (ECU) software · General Electric CF6-80E1A1, CF6-80E1A2, CF6-80E1A3 and 2 more. Effective Aug 29, 2007 - [AD 2007-11-20](https://openairdocs.org/ad/2007-11-20): Fuel shroud retaining rings · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 22 more. Effective Jul 10, 2007 - [AD 2005-22-12](https://openairdocs.org/ad/2005-22-12): Thrust reverser actuation system (TRAS) locks · General Electric CF6-80E1A1, CF6-80E1A2, CF6-80E1A3 and 2 more. Effective Dec 2, 2005 - [AD 2005-17-05](https://openairdocs.org/ad/2005-17-05): High pressure compressor rotor (HPCR) · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 25 more. Effective Sep 27, 2005 - [AD 2004-09-34](https://openairdocs.org/ad/2004-09-34): High Pressure Turbine (HPT) rotor Blades · General Electric CF6-80E1A1, CF6-80E1A2, CF6-80E1A3 and 1 more. Effective May 26, 2004 - [AD 2002-25-08](https://openairdocs.org/ad/2002-25-08): High pressure compressor rotor · General Electric CF6-45A, CF6-45A2, CF6-50A and 40 more. Effective Jan 23, 2003 - [AD 2002-10-08](https://openairdocs.org/ad/2002-10-08): Fan Thrust Reverser · General Electric CF6-80E1A1, CF6-80E1A2, CF6-80E1A3 and 1 more. Effective Jun 27, 2002 - [AD 2002-06-07](https://openairdocs.org/ad/2002-06-07): Directional Pilot Valve (DPV) Assembly · General Electric CF6-80E1A1, CF6-80E1A2, CF6-80E1A3 and 1 more. Effective May 1, 2002 Historical (superseded or no longer in force): - [AD 2009-05-02](https://openairdocs.org/ad/2009-05-02) (historical): Drainless fuel manifold assemblies · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 26 more. Effective Mar 31, 2009 - [AD 2005-23-09](https://openairdocs.org/ad/2005-23-09) (historical): High pressure compressor (HPC) cases · General Electric CF6-80E1A1, CF6-80E1A2, CF6-80E1A3 and 2 more. Effective Nov 25, 2005 - [AD 2005-10-16](https://openairdocs.org/ad/2005-10-16) (historical): ECU digital interface unit (DIU) · General Electric CF6-80E1A1, CF6-80E1A2, CF6-80E1A3 and 1 more. Effective Jun 3, 2005 - [AD 2002-07-12](https://openairdocs.org/ad/2002-07-12) (historical): Life Limits Section of Continued Airworthiness (ICA) - Selected Critical Life-limited Parts · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 27 more. Effective May 15, 2002 - [AD 2002-01-04](https://openairdocs.org/ad/2002-01-04) (historical): High Pressure Turbine (HPT) Stage 2 (S2) Nozzle Guide Vane (NGV) · General Electric CF6-80E1A1, CF6-80E1A2, CF6-80E1A3 and 1 more. Effective Feb 14, 2002 - [AD 2000-08-12](https://openairdocs.org/ad/2000-08-12) (historical): Life-limited Parts · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 10 more. Effective Oct 23, 2000 - [AD 2000-16-12](https://openairdocs.org/ad/2000-16-12) (historical): High Pressure Compressor Rotor Stage 3-9 Spools · General Electric CF6-45A, CF6-45A2, CF6-50A and 39 more. Effective Sep 5, 2000 - [AD 99-24-15](https://openairdocs.org/ad/99-24-15) (historical): High Pressure Compressor Rotor (HPCR) Stage 3-9 Spools · General Electric CF6-45A, CF6-45A2, CF6-50A and 39 more. Effective Jan 28, 2000 - [AD 99-08-13](https://openairdocs.org/ad/99-08-13) (historical): General Electric CF6-80A, CF6-80A1, CF6-80A2 and 26 more. Effective May 13, 1999 ## Information bulletins (advisory) (5) - [SAIB 2023-15](https://openairdocs.org/saib/2023-15): Falsified Forms from AOG Technics. Issued Dec 19, 2023 - [SAIB NE-16-15](https://openairdocs.org/saib/NE-16-15): Engine Starter. Issued Apr 4, 2016 - [SAIB NE-11-27](https://openairdocs.org/saib/NE-11-27): Fuel Injector Nozzle - CF6-80 Improperly Welded Fuel Nozzles. Issued Apr 5, 2011 - [SAIB NE-08-44](https://openairdocs.org/saib/NE-08-44): Engine Thrust Reverser Transcowl Clevis Pin. Issued Sep 3, 2008 - [SAIB NE-07-01](https://openairdocs.org/saib/NE-07-01): Dual engine flameouts on twin engine airplanes. Issued Oct 12, 2006 ## 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. --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.