- Effective
- July 11, 1978
- Model
- G102 ASTIR CS
- Data sheet
- TCDSG33EU
- Registered aircraft
- 38 matched by model
- Product
- Aircraft · Glider
- Amendment
- 39-3254
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 | 49ba74c7…f348afd | FAA DRS (API key needed) |
On this page
The airworthiness directive
78-14-04 BURKHART GROB: Amendment 39-3254. Applies to Model "G102" Astir CS gliders, serial numbers 1180 through 1536, certificated in all categories, that have rudder control levers with lightening cutouts.
Compliance is required with in the next 25 hours time in service after the effective date of this AD, unless already accomplished.
To reduce the possibility of failure of the intermediate rudder control lever and subsequent loss of rudder control, replace the rudder control lever in accordance with Burkhart Grob, Technical Information TM 102-8, dated November 28, 1977, or equivalent approved by the Chief, Aircraft Certification Staff, FAA, Europe, Africa, and Middle East Region.
This amendment becomes effective July 11, 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