| AD Number | 75-16-09 | Status | Active |
| Effective Date | August 27, 1975 | Issue Date | Not specified |
| Docket Number | Unknown | Amendment | 39-2281 |
| Product Type | ["Engine"] | Product Subtype | Not specified |
| CFR Part | --- - Part 39 | CFR Section | N/A |
| Citation | This information is not available. | ||
| Manufacturer(s) | Rolls-Royce plc |
| Model(s) | RB211-22B-02 RB211-22B/MOD 72-8700 RB211-524B-02 RB211-524B-B-02 RB211-524B2-19 RB211-524B2-B-19 RB211-524B3-02 RB211-524B4-02 RB211-524B4-D-02 RB211-524C2-19 RB211-524C2-B-19 RB211-524D4-19 RB211-524D4-39 RB211-524D4-B-19 RB211-524D4-B-39 RB211-524D4X-19 RB211-524D4X-B-19 RB211-524G2-19 RB211-524G2-T-19 RB211-524G3-19 RB211-524G3-T-19 RB211-524H-36 RB211-524H-T-36 RB211-524H2-19 RB211-524H2-T-19 |
75-16-09 ROLLS ROYCE (1971) LIMITED: Amendment 39-2281. Applies to Rolls Royce RB 211 series engines, serial numbers 10479 and prior.
Compliance required before September 1, 1975, unless already accomplished.
To prevent engine loss of oil and possible inflight engine shutdown, modify the HS external gearbox oil tank filler cap and housing in accordance with Rolls Royce (1971) Limited Service Bulletin RB211-72-3533, dated August 12, 1974, or an FAA-approved equivalent.
This amendment becomes effective August 27, 1975.