| AD Number | 72-16-03 | Status | Active |
| Effective Date | August 08, 1972 | Issue Date | Not specified |
| Docket Number | Unknown | Amendment | 39-1495 |
| 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 |
72-16-03 GENERAL ELECTRIC: Amendment 39-1495. Applies to Models CF6-6D and CF6-6D1 turbofan engines.
Compliance required as indicated.
To prevent cracking and possible failure of stage 2 high pressure turbine discs, unless already accomplished, remove from service stage 2 high pressure turbine discs Part No. 9687M40P03, P04, P05, or P06 prior to reaching a life limit of 2100 cycles.
For the purposes of this AD, the definition of cycles is that appearing in the CF6 Shop Manual GEK 9266 Section 72-00-00 Inspection page 301.
(General Electric Alert Service Bulletin CF6 72-320 pertains to this subject.)
This amendment is effective August 8, 1972.