# AD 69-02-02: Compressor

- Type: Airworthiness directive
- Status: Current
- Products: General Electric CJ805-23, CJ805-23B, CJ805-23C, CJ805-3, CJ805-3A and CJ805-3B
- Effective: February 14, 1969
- Superseded by: Nothing supersedes this AD
- Product type: Engine
- Amendment: 39-710
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/F5BF6045538F52758625685B00596FF7.0001
- DRS record last changed: May 30, 2024
- Page: https://openairdocs.org/ad/69-02-02

## The airworthiness directive

69-02-02 GENERAL ELECTRIC: Amendment 39-710. Applies to Type CJ805-3, -3A, -3B, -23, -23B, and -23C Turbojet Engines.

Compliance required as indicated.

Within the next 6,000 hours' time in service after the effective date of this AD or at the next compressor disassembly, whichever occurs first, unless already accomplished, replace the 12th, 13th, and 14th stage compressor discs with new ones as indicated below:

Disc Stage G.E. P/N'S to be replaced New P/N 12 106R686P1 or 108R627P1 111R232P2 13 106R687P1 or 108R628P1 111R233P2 14 106R688P1 or 108R629P1 111R234P2

The information in this AD is similar to that contained in General Electric Service Bulletins (880) 72-253 and (990) 72-260 and Revisions Nos. 1 and 2.

This amendment is effective February 14, 1969.

## Affected data sheets (2) (OpenAirDocs)

The type certificate data sheets whose models the AD names.

- [TCDS 1E5](https://openairdocs.org/tcds/1E5): General Electric Company; names 3 of 3 models: CJ805-23B, CJ805-23, CJ805-23C
- [TCDS E-306](https://openairdocs.org/tcds/E-306): General Electric Company; names 3 of 3 models: CJ805-3, CJ805-3B, CJ805-3A

## Registered aircraft it may apply to (OpenAirDocs)

No registered aircraft matched the models it names.

Its text cites no advisory circulars or STCs.

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