- Effective
- July 5, 1978
- Model
- G102 ASTIR CS
- Data sheet
- TCDSG33EU
- Registered aircraft
- 38 matched by model
- Product
- Aircraft · Glider
- Amendment
- 39-3244
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 | 5a88d2cf…ae8c7e8 | FAA DRS (API key needed) |
On this page
The airworthiness directive
78-13-03 BURKHART GROB: Amendment 39-3244. Applies to Model G102 Astir CS gliders, Serial numbers, 1001 to 1234 and 1300 to 1315, certificated in all categories.
Compliance is required within the next 25 hours time in service after the effective date of this AD, unless already accomplished.
To reduce the possibility of elevator control failure due to possible loss of an elevator control pivot bolt, modify the elevator control assembly by installing a mechanical stop to the elevator control pivot (bearing) bolt, part no. 4205.06, in accordance with Burkhart Grob Technical Information TM102-4 dated August 16, 1976, or an equivalent, approved by the Chief, Aircraft Certification Staff, FAA, Europe, Africa and Middle East Region.
This amendment becomes effective July 5, 1978.
Affected TCDS · 1
The type certificate data sheets for the models this AD names, matched by model and maker.
Registered aircraft · 38
Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.
| 1975 | 1 |
|---|---|
| 1976 | 18 |
| 1977 | 4 |
| 1978 | 1 |
| 1981 | 4 |
10 with no year recorded