| AD Number | 75-26-14 | Status | Active |
| Effective Date | December 29, 1975 | Issue Date | Not specified |
| Docket Number | Unknown | Amendment | 39-2463 |
| Product Type | ["Aircraft"] | Product Subtype | ["Glider"] |
| CFR Part | --- - Part 39 | CFR Section | N/A |
| Citation | This information is not available. | ||
| Manufacturer(s) | Scheibe-Flugzeugbau GmbH |
| Model(s) | Bergfalke-III Bergfalke-II/55 |
75-26-14 SCHEIBE FLUGZEUGBAU GmbH: Amendment 39-2463. Applies to Model Bergfalke II/55 and III gliders, certificated in all categories, equipped with loose connecting bolt between the elevator push-pull rod and elevator control lever.
Compliance is required as indicated, unless already accomplished.
To ensure a reliable elevator control connection, within the next 10 hours' time in service after the effective date of this AD, replace the safety pin (Fokker needle) at the connecting bolt between the elevator push-pull rod and the elevator control lever with an aviation quality washer and cotter pin.
This supersedes Amendment 39-2334 (49 FR 33008), AD 75-17-29.
This amendment becomes effective December 29, 1975.