- Effective
- March 18, 1975
- Model
- G-1159
- Data sheet
- TCDSA12EA
- Registered aircraft
- 14 matched by model
- Product
- Aircraft · Large airplane
- Amendment
- 39-2124
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 | 7aecd44d…6a3a6fd | FAA DRS (API key needed) |
On this page
The airworthiness directive
75-06-08 GRUMMAN AMERICAN AVIATION CORPORATION: Amendment 39- 2124. Applies to G-1159 airplanes certificated in all categories.
Compliance required within the next 150 hours' time in service after the effective date of this AD, unless already accomplished.
To prevent possible loss of all DC and AC power, connect the battery switch ground leads to separate studs at the center overhead panel in accordance with Grumman ASC 188 or in an equivalent manner approved by Chief, Engineering and Manufacturing Branch, Southern Region, Atlanta, Georgia.
This amendment becomes effective March 18, 1975.
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 | 1 |
|---|---|
| 1968 | 2 |
| 1971 | 1 |
| 1974 | 1 |
| 1976 | 1 |
| 1977 | 1 |
7 with no year recorded