| AD Number | 78-13-03 | Status | Active |
| Effective Date | July 05, 1978 | Issue Date | Not specified |
| Docket Number | Unknown | Amendment | 39-3244 |
| Product Type | ["Aircraft"] | Product Subtype | ["Glider"] |
| CFR Part | --- - Part 39 | CFR Section | N/A |
| Citation | This information is not available. | ||
| Manufacturer(s) | GROB-WERKE GMBH & CO KG |
| Model(s) | G102 ASTIR CS |
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.