# Airworthiness directives that may apply: GE CF6-6D

A list on [GE CF6-6D](https://openairdocs.org/engine/ge-cf6-6d.md).

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

- [AD 2003-10-01](https://openairdocs.org/ad/2003-10-01.md): High pressure turbine rotor (HPTR) rear shafts · Effective Jun 17, 2003
- [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 98-22-06](https://openairdocs.org/ad/98-22-06.md): Fan Disks · Effective Nov 23, 1998
- [AD 98-18-10](https://openairdocs.org/ad/98-18-10.md): Low Pressure Turbine Disks · Effective Sep 30, 1998
- [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 91-24-01](https://openairdocs.org/ad/91-24-01.md): Compressor Rear Frame Casing · Effective May 26, 1992
- [AD 91-15-03](https://openairdocs.org/ad/91-15-03.md): Fan Disks · Effective Aug 5, 1991
- [AD 91-12-09](https://openairdocs.org/ad/91-12-09.md): Fan Disks · Effective Jun 27, 1991
- [AD 91-01-04](https://openairdocs.org/ad/91-01-04.md): Fan Disk · Effective Jan 22, 1991
- [AD 90-19-08](https://openairdocs.org/ad/90-19-08.md): Low Pressure Turbine Rotor Stage One Disk · Effective Oct 15, 1990
- [AD 89-20-01 R1](https://openairdocs.org/ad/89-20-01-R1.md): Fan Disks · Effective Dec 12, 1989
- [AD 88-12-01](https://openairdocs.org/ad/88-12-01.md): High Pressure Compressor Rear Shafts · Effective Jun 6, 1988
- [AD 81-19-08](https://openairdocs.org/ad/81-19-08.md): Low Pressure Turbine Rotor Stage 2 Disks · Effective Sep 21, 1981
- [AD 80-03-06](https://openairdocs.org/ad/80-03-06.md): Stage 2 HPT Disks · Effective Feb 8, 1980
- [AD 78-07-03](https://openairdocs.org/ad/78-07-03.md): Compressor Spool · Effective May 22, 1978
- [AD 76-21-04](https://openairdocs.org/ad/76-21-04.md): High Pressure Compressor · Effective Nov 30, 1977
- [AD 76-05-10](https://openairdocs.org/ad/76-05-10.md): Turbofan Engines · Effective Mar 24, 1976
- [AD 75-22-11](https://openairdocs.org/ad/75-22-11.md): High Pressure Turbine Thermal Shield · Effective Oct 28, 1975
- [AD 74-14-08](https://openairdocs.org/ad/74-14-08.md): Turbine Blades · Effective Jul 12, 1974
- [AD 72-16-03](https://openairdocs.org/ad/72-16-03.md): Turbine Discs · Effective Aug 8, 1972
- [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
- [AD 95-18-14](https://openairdocs.org/ad/95-18-14.md): High Pressure Compressor Rotor · Historical · Effective Sep 21, 1995 · Replaced by AD 2002-25-08

## 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 ('30076'))
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-cf6-6d/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.
