| AD Number | 77-13-07 | Status | Active |
| Effective Date | July 01, 1977 | Issue Date | Not specified |
| Docket Number | Unknown | Amendment | 39-2932 |
| Product Type | ["Aircraft"] | Product Subtype | ["Small/Large Airplane"] |
| CFR Part | --- - Part 39 | CFR Section | N/A |
| Citation | This information is not available. | ||
| Manufacturer(s) | Textron Aviation Inc. |
| Model(s) | 200 |
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.