- Effective
- July 1, 1977
- Model
- 200
- Data sheet
- TCDSA24CE
- Registered aircraft
- 234 matched by model
- Product
- Aircraft · Small/large airplane
- Amendment
- 39-2932
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 January 21, 2026.
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 | 9849ece0…0d42521 | FAA DRS (API key needed) |
On this page
The airworthiness directive
77-13-07 BEECH: Amendment 39-2932. Applies to Model 200 (Serial Numbers BB-2 thru BB-250) airplanes certificated in all categories.
Compliance: Required as indicated, unless already accomplished.
To assure that wings will carry the 50 feet/second gust design loads, within 50 hours' time in service after the effective date of this AD, accomplish the following:
A) With aileron control system pinned in the neutral position rerig the droop of right and left aileron to zero degrees, with a tolerance of plus one-half degree up, minus zero degrees down in accordance with Beechcraft Service Instructions Number 0906 or later approved revisions.
B) Any equivalent method of compliance with this AD must be approved by the Chief, Engineering and Manufacturing Branch, FAA, Central Region.
This amendment becomes effective July 1, 1977.
Affected TCDS · 1
The type certificate data sheets for the models this AD names, matched by model and maker.
Registered aircraft · 234
Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.
| 1975 | 14 |
|---|---|
| 1976 | 16 |
| 1977 | 20 |
| 1978 | 28 |
| 1979 | 49 |
| 1980 | 47 |
| 1981 | 30 |
| 1982 | 3 |
| 1983 | 1 |
| 1984 | 3 |
23 with no year recorded