- Effective
- April 5, 1969
- Model
- AS-K 13
- Data sheet
- TCDSG15EU
- Registered aircraft
- 14 matched by model
- Product
- Aircraft · Glider
- Amendment
- 39-730
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 | 0f6162db…f9298b4 | FAA DRS (API key needed) |
On this page
The airworthiness directive
69-05-04 SCHLEICHER: Amdt. 39-730. Applies to Schleicher Model ASK-13 gliders, Serial Numbers 13000 through 13104, 13108, 13109, except Serial Numbers 13071 and 13096.
Compliance required within the next 100 hours' time in service after the effective date of this AD, unless already accomplished.
To prevent the landing gear end buffer plate from slipping inside the rubber buffer, replace the 2.76-inch diameter buffer plate located on the left and right landing gear with a 3.55- inch diameter buffer plate, in accordance with Schleicher Modification No. 3, dated September 4, 1968, or later LBA-approved issue or an FAA-approved equivalent.
This amendment becomes effective April 5, 1969.
Affected TCDS · 1
The type certificate data sheets for the models this AD names, matched by model and maker.
Registered aircraft · 14
Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.
| 1967 | 6 |
|---|---|
| 1968 | 3 |
| 1972 | 2 |
3 with no year recorded