| AD Number | 76-25-05 | Status | Active |
| Effective Date | January 24, 1977 | Issue Date | Not specified |
| Docket Number | Unknown | Amendment | 39-2789 |
| Product Type | ["Aircraft"] | Product Subtype | ["Small Airplane"] |
| CFR Part | --- - Part 39 | CFR Section | N/A |
| Citation | This information is not available. | ||
| Manufacturer(s) | Textron Aviation Inc. |
| Model(s) | 19A 23 A23 A23-19 A23-24 A23A A24 A24R B19 B23 C23 M19A |
76-25-05 BEECH: Amendment 39-2789. Applies to Models A23-19, 19A, M19A and B19 (Serial Numbers MB-1 thru MB-545 and MB-547), Models 23, A23, A23A, B23 and C23 (Serial Numbers M-2 thru M-1415), Models A-23-24 and A24 (Serial Numbers MA-1 thru MA- 368), and Models A24R (Serial Numbers MC-2 thru MC-127) airplanes.
Compliance: Required as indicated, unless already accomplished.
To prevent interchanging left and right ailerons during reinstallation and resulting reversed aileron control response, accomplish the following:
A) Within the next 100 hours' time in service after the effective date of this AD or at the next removal of the ailerons or within one year after the effective date of this AD, whichever occurs first, install one each Beech P/N 169-110000-481 strap in the left and right wing trailing edge in accordance with Beechcraft Service Instruction 0510-032 or later approved revisions.
B) Any alternate method of compliance with this AD must be approved by theChief, Engineering and Manufacturing Branch, FAA, Central Region.
This amendment becomes effective January 24, 1977.