| AD Number | 74-14-08 | Status | Active |
| Effective Date | July 12, 1974 | Issue Date | Not specified |
| Docket Number | Unknown | Amendment | 39-1894 |
| Product Type | ["Engine"] | Product Subtype | Not specified |
| CFR Part | --- - Part 39 | CFR Section | N/A |
| Citation | This information is not available. | ||
| Manufacturer(s) | General Electric Company |
| Model(s) | CF6-6D CF6-6D1 |
74-14-08 GENERAL ELECTRIC: Amendment 39-1894. Applies to Models CF6-6D, 6D1, and 6H Turbofan Engines.
Compliance required by September 30, 1974.
To prevent expulsion from the engine of fifth stage low pressure turbine blades, unless already accomplished, install improved blade retainer P/N 9083M19P07 per the instructions of General Electric Service Bulletin (CF6-6) 72-399 Revision 1 dated March 20, 1974, or subsequent FAA approved revision.
This amendment becomes effective July 12, 1974.