# Airworthiness directives that may apply: GE CF6-80A

A list on [GE CF6-80A](https://openairdocs.org/engine/ge-cf6-80a.md).

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

- [AD 2021-26-22](https://openairdocs.org/ad/2021-26-22.md): Turbine Section · Effective Mar 14, 2022 · Supersedes AD 2020-20-13
- [AD 2021-14-11](https://openairdocs.org/ad/2021-14-11.md): Turbine Section · Effective Aug 27, 2021
- [AD 2018-07-05](https://openairdocs.org/ad/2018-07-05.md): Turbine Section · Effective May 11, 2018
- [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 2009-08-06](https://openairdocs.org/ad/2009-08-06.md): Stage 1 high-pressure turbine (HPT) rotor disks · Effective May 18, 2009
- [AD 2009-07-10](https://openairdocs.org/ad/2009-07-10.md): High-pressure turbine rotor (HPTR) · Effective May 6, 2009
- [AD 2009-04-10](https://openairdocs.org/ad/2009-04-10.md): Critical life-limited parts · Effective Mar 30, 2009 · Supersedes AD 2002-07-12
- [AD 2006-16-06](https://openairdocs.org/ad/2006-16-06.md): Certain stage 1 high- pressure turbine (HPT) rotor disks · Effective Sep 5, 2006 · Supersedes AD 2004-04-07
- [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 98-22-06](https://openairdocs.org/ad/98-22-06.md): Fan Disks · Effective Nov 23, 1998
- [AD 95-17-16](https://openairdocs.org/ad/95-17-16.md): Compressor Rear Frame · Effective Nov 7, 1995
- [AD 94-07-04](https://openairdocs.org/ad/94-07-04.md): High Pressure Turbine Disk · Effective May 23, 1994
- [AD 93-14-18](https://openairdocs.org/ad/93-14-18.md): High pressure turbine (HPT) thermal shields · Effective Oct 4, 1993
- [AD 92-04-08](https://openairdocs.org/ad/92-04-08.md): Stage 1 Disk/Shafts · Effective Mar 27, 1992
- [AD 91-23-13](https://openairdocs.org/ad/91-23-13.md): Fan Disks · Effective Nov 22, 1991
- [AD 91-15-25](https://openairdocs.org/ad/91-15-25.md): High Pressure Compressor Rotor · Effective Sep 6, 1991
- [AD 91-11-05](https://openairdocs.org/ad/91-11-05.md): High Pressure Compressor Rotor · Effective Jul 5, 1991
- [AD 91-01-04](https://openairdocs.org/ad/91-01-04.md): Fan Disk · Effective Jan 22, 1991
- [AD 89-16-08](https://openairdocs.org/ad/89-16-08.md): Manifold · Effective Aug 31, 1989
- [AD 86-15-04](https://openairdocs.org/ad/86-15-04.md): Stage 1 High Pressure Turbine (HPT) Disks · Effective Jul 23, 1986
- [AD 85-15-51](https://openairdocs.org/ad/85-15-51.md): Fuel Manifold Supply Tube · Effective Dec 23, 1985
- [AD 2020-20-13](https://openairdocs.org/ad/2020-20-13.md): Turbine Section · Historical · Effective Nov 12, 2020 · Replaced by AD 2021-26-22
- [AD 2018-15-04](https://openairdocs.org/ad/2018-15-04.md): Turbine/Turboprop Engine--Turbine Section · Historical · Effective Oct 2, 2018 · Replaced by AD 2020-20-13
- [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 2004-04-07](https://openairdocs.org/ad/2004-04-07.md): Stage 1 HPT rotor disks · Historical · Effective Mar 12, 2004 · Replaced by AD 2006-16-06
- [AD 2003-01-05](https://openairdocs.org/ad/2003-01-05.md): Dovetail slots · Historical · Effective Jan 28, 2003 · Replaced by AD 2004-04-07
- [AD 2002-07-12](https://openairdocs.org/ad/2002-07-12.md): Life Limits Section of Continued Airworthiness (ICA) - Selected Critical Life-limited Parts · Historical · Effective May 15, 2002 · Replaced by AD 2009-04-10
- [AD 2000-08-12](https://openairdocs.org/ad/2000-08-12.md): Life-limited Parts · Historical · Effective Oct 23, 2000 · Replaced by AD 2002-07-12
- [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 99-18-19](https://openairdocs.org/ad/99-18-19.md): Inadvertent Thrust Reverser · Historical · Effective Sep 24, 1999 · Replaced by AD 2005-06-07
- [AD 99-08-13](https://openairdocs.org/ad/99-08-13.md): Airworthiness Directives; General Electric Company CF6-80A, CF6-80C2, and CF6-80E1 Series Turbofan Engines · Historical · Effective May 13, 1999 · Replaced by AD 2000-08-12

## 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 ('30093'))
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-cf6-80a/ads

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