AD 69-02-02

Active

Compressor

Key Information
69-02-02
Active
February 14, 1969
Not specified
Unknown
39-710
Applicability
["Engine"]
Not specified
General Electric Company
CJ805-23 CJ805-23B CJ805-23C CJ805-3 CJ805-3A CJ805-3B
Regulatory Text

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.

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References
This information is not available.
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FAA Documents