| AD Number | 75-15-07 | Status | Active |
| Effective Date | July 25, 1975 | Issue Date | Not specified |
| Docket Number | Unknown | Amendment | 39-2268 |
| 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) | 99 99A A99A B99 |
75-15-07 BEECH: Amendment 39-2268. Applies to Models 99, 99A, A99A and B99 (Serial Numbers U-1 through U-163) airplanes which are equipped with the 99-8010-1P hydraulic landing gear system.
Compliance: Required as indicated, unless already accomplished.
To prevent main landing gear malfunction:
Within the next 100 hours' time in service after the effective date of this AD, modify the main landing gear system in accordance with Beechcraft Service Instructions 0743-231, or subsequent revisions, or any alternative modification approved by the Chief, Engineering and Manufacturing Branch, FAA, Central Region.
This amendment becomes effective July 25, 1975.