- Effective
- February 14, 1969
- Models
- CJ805-23, CJ805-23B, CJ805-23C, CJ805-3, CJ805-3A, CJ805-3B
- Product
- Engine
- Amendment
- 39-710
Unofficial copy of the text in the FAA’s Dynamic Regulatory System. The FAA’s own copy is the authoritative one. DRS record last changed May 30, 2024.
Copies of the files this page was built from, with their SHA-256. Retrieved October 18, 2026.
| File | Size | SHA-256 | Original |
|---|---|---|---|
| FAA DRS HTML | 20 KB | f51353f3…db8f82d | FAA DRS (API key needed) |
On this page
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 TCDS · 2
The type certificate data sheets for the models this AD names, matched by model and maker.