# Airworthiness directives that may apply: GE CF6-50C2

A list on [GE CF6-50C2](https://openairdocs.org/engine/ge-cf6-50c2.md).

Matched by model name and maker. Each AD’s applicability may narrow it by serial number, part number or configuration.

- [AD 2023-04-11](https://openairdocs.org/ad/2023-04-11.md): Turbine Section · Effective Apr 28, 2023 · Supersedes AD 2012-02-07
- [AD 2011-23-04](https://openairdocs.org/ad/2011-23-04.md): Forward engine mount assembly side links · Effective Dec 12, 2011 · Supersedes AD 2006-12-24
- [AD 2011-07-01](https://openairdocs.org/ad/2011-07-01.md): Forward and aft centerbodies · Effective Apr 22, 2011 · Supersedes AD 2009-04-17
- [AD 2007-11-18 R1](https://openairdocs.org/ad/2007-11-18-R1.md): Forward fan stator cases · Effective Jan 4, 2010 · Supersedes AD 2007-11-18
- [AD 2008-02-17](https://openairdocs.org/ad/2008-02-17.md): Thrust reverser actuation systems · Effective Feb 28, 2008 · Supersedes AD 99-18-20
- [AD 2007-19-06](https://openairdocs.org/ad/2007-19-06.md): Compressor discharge pressure (CDP) · Effective Oct 23, 2007
- [AD 2005-26-06](https://openairdocs.org/ad/2005-26-06.md): Low pressure turbine (LPT) stage 2 interstage seal assemblies · Effective Jan 26, 2006
- [AD 2005-07-05](https://openairdocs.org/ad/2005-07-05.md): Low pressure turbine (LPT) · Effective May 4, 2005
- [AD 2005-08-04](https://openairdocs.org/ad/2005-08-04.md): Low-cycle-fatigue (LCF) · Effective Apr 28, 2005
- [AD 2003-09-06](https://openairdocs.org/ad/2003-09-06.md): Low pressure turbine (LPT) · Effective Jun 3, 2003
- [AD 2003-02-07](https://openairdocs.org/ad/2003-02-07.md): Low pressure turbine (LPT) shrouds · Effective Mar 3, 2003
- [AD 2002-25-08](https://openairdocs.org/ad/2002-25-08.md): High pressure compressor rotor · Effective Jan 23, 2003 · Supersedes AD 2000-16-12, AD 95-18-14
- [AD 2002-05-03](https://openairdocs.org/ad/2002-05-03.md): Life-Limited Rotating Parts · Effective Apr 12, 2002 · Supersedes AD 2000-08-11
- [AD 2002-02-09](https://openairdocs.org/ad/2002-02-09.md): Low Pressure Turbine Rotor (LPTR) Stage 2 Disks · Effective Mar 15, 2002
- [AD 2001-12-20](https://openairdocs.org/ad/2001-12-20.md): Air Ducts and Reworked Mating Hardware · Effective Jul 26, 2001
- [AD 2001-04-16](https://openairdocs.org/ad/2001-04-16.md): Low Pressure Turbine (LPT) Nozzle Lock Assembly Studs · Effective Mar 21, 2001 · Supersedes AD 2000-20-02
- [AD 2000-11-12](https://openairdocs.org/ad/2000-11-12.md): High Pressure Compressor Disk Lock Slots · Effective Aug 14, 2000
- [AD 98-22-06](https://openairdocs.org/ad/98-22-06.md): Fan Disks · Effective Nov 23, 1998
- [AD 97-22-14](https://openairdocs.org/ad/97-22-14.md): (HPCR) 3-9 Spool · Effective Nov 17, 1997
- [AD 95-08-03](https://openairdocs.org/ad/95-08-03.md): High Pressure Turbine Rotor Stage 2 Disks · Effective Jun 12, 1995
- [AD 91-10-03 R1](https://openairdocs.org/ad/91-10-03-R1.md): High Pressure Compressor · Effective Apr 28, 1995
- [AD 94-08-05](https://openairdocs.org/ad/94-08-05.md): Fan Stator Case · Effective Jul 5, 1994
- [AD 94-09-18](https://openairdocs.org/ad/94-09-18.md): High Pressure Turbine Disk · Effective Jun 6, 1994
- [AD 93-14-18](https://openairdocs.org/ad/93-14-18.md): High pressure turbine (HPT) thermal shields · Effective Oct 4, 1993
- [AD 93-13-10](https://openairdocs.org/ad/93-13-10.md): Compressor Spools · Effective Sep 21, 1993
- [AD 91-23-13](https://openairdocs.org/ad/91-23-13.md): Fan Disks · Effective Nov 22, 1991
- [AD 91-15-16](https://openairdocs.org/ad/91-15-16.md): High Pressure Turbine Thermal Shields · Effective Sep 4, 1991
- [AD 91-01-04](https://openairdocs.org/ad/91-01-04.md): Fan Disk · Effective Jan 22, 1991
- [AD 90-23-15](https://openairdocs.org/ad/90-23-15.md): Turbine Mid-frame · Effective Dec 6, 1990
- [AD 90-19-09](https://openairdocs.org/ad/90-19-09.md): High Pressure Turbine Stage One Disks · Effective Oct 1, 1990
- [AD 90-12-06](https://openairdocs.org/ad/90-12-06.md): Low Pressure Turbine · Effective Jun 25, 1990
- [AD 89-01-02](https://openairdocs.org/ad/89-01-02.md): High Pressure Turbine Stage 2 Disks · Effective Dec 29, 1988
- [AD 87-23-06](https://openairdocs.org/ad/87-23-06.md): High Pressure Turbine Impeller Spacer · Effective Nov 5, 1987
- [AD 86-12-03](https://openairdocs.org/ad/86-12-03.md): High Pressure Turbine Rotor (HPTR) Stage 1 Disk · Effective Jun 29, 1986
- [AD 84-01-01](https://openairdocs.org/ad/84-01-01.md): Compressor Assemblies · Effective Feb 10, 1984
- [AD 82-25-08](https://openairdocs.org/ad/82-25-08.md): HPT Spacer/Impeller · Effective Dec 30, 1982
- [AD 82-20-03](https://openairdocs.org/ad/82-20-03.md): Inspect First Stage HPT Disks · Effective Oct 31, 1982
- [AD 85-25-56 R1](https://openairdocs.org/ad/85-25-56-R1.md): Seventh Stage Low Pressure Turbine (LPT) Cooling Air Manifold Tube
- [AD 79-13-09](https://openairdocs.org/ad/79-13-09.md): Compressor Rotor Spools
- [AD 2012-02-07](https://openairdocs.org/ad/2012-02-07.md): LPT rotor stage 3 disks · Historical · Effective Mar 6, 2012 · Replaced by AD 2023-04-11
- [AD 2011-18-01](https://openairdocs.org/ad/2011-18-01.md): LPT rotor stage 3 disks · Historical · Effective Sep 26, 2011 · Replaced by AD 2012-02-07
- [AD 2011-02-07](https://openairdocs.org/ad/2011-02-07.md): Rotor · Historical · Effective Feb 22, 2011 · Replaced by AD 2012-02-07
- [AD 2010-12-10](https://openairdocs.org/ad/2010-12-10.md): High-pressure turbine (HPT) · Historical · Effective Jun 24, 2010 · Replaced by AD 2011-02-07
- [AD 2010-06-15](https://openairdocs.org/ad/2010-06-15.md): Low-pressure turbine (LPT) stage 3 disks · Historical · Effective Apr 1, 2010 · Replaced by AD 2010-12-10
- [AD 2009-04-17](https://openairdocs.org/ad/2009-04-17.md): Long fixed core exhaust nozzle (LFCEN) assembly · Historical · Effective Apr 2, 2009 · Replaced by AD 2011-07-01
- [AD 2007-11-18](https://openairdocs.org/ad/2007-11-18.md): Forward fan stator cases · Historical · Effective Jul 5, 2007 · Replaced by AD 2007-11-18 R1
- [AD 2006-12-24](https://openairdocs.org/ad/2006-12-24.md): Five-link forward mount assembly · Historical · Effective Jul 21, 2006 · Replaced by AD 2011-23-04
- [AD 2000-20-02](https://openairdocs.org/ad/2000-20-02.md): Turbine Nozzle Lock Assemblies · Historical · Effective Oct 17, 2000 · Replaced by AD 2001-04-16
- [AD 2000-16-12](https://openairdocs.org/ad/2000-16-12.md): High Pressure Compressor Rotor Stage 3-9 Spools · Historical · Effective Sep 5, 2000 · Replaced by AD 2002-25-08
- [AD 99-24-15](https://openairdocs.org/ad/99-24-15.md): High Pressure Compressor Rotor (HPCR) Stage 3-9 Spools · Historical · Effective Jan 28, 2000 · Replaced by AD 2002-25-08
- [AD 99-08-18](https://openairdocs.org/ad/99-08-18.md): Airworthiness Directives; General Electric Company CF6-6, CF6-45, and CF6-50 Series Turbofan Engines · Historical · Effective May 13, 1999 · Replaced by AD 2000-08-11

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT d.ad_number, d.status, d.subject, d.effective_date
FROM 'https://openairdocs.org/data/latest/faa_directive.parquet' d
WHERE d.ad_id IN (SELECT ad_id FROM 'https://openairdocs.org/data/latest/faa_engine_model_directive.parquet' WHERE engine_model_code IN ('30085'))
ORDER BY coalesce(d.effective_date, d.publication_date, d.issue_date) DESC, d.ad_number DESC
```

This list as a web page: https://openairdocs.org/engine/ge-cf6-50c2/ads

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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.
