- Effective
- December 29, 1975
- Models
- Bergfalke-III, Bergfalke-II/55
- Data sheet
- TCDS7G9
- Registered aircraft
- 6 matched by model
- Product
- Aircraft · Glider
- Amendment
- 39-2463
Unofficial copy of the text in the FAA’s Dynamic Regulatory System. The FAA’s own copy is the authoritative one. DRS record last changed May 30, 2024.
Copies of the files this page was built from, with their SHA-256. Retrieved October 18, 2026.
| File | Size | SHA-256 | Original |
|---|---|---|---|
| FAA DRS HTML | 19 KB | 446e7d3e…2c02fc0 | FAA DRS (API key needed) |
On this page
The airworthiness directive
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.
Affected TCDS · 1
The type certificate data sheets for the models this AD names, matched by model and maker.
Registered aircraft · 6
Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.
| 1955 | 1 |
|---|---|
| 1957 | 1 |
| 1959 | 1 |
3 with no year recorded