| AD Number | 77-18-04 | Status | Active |
| Effective Date | September 12, 1977 | Issue Date | Not specified |
| Docket Number | Unknown | Amendment | 39-3028 |
| 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 200T A100 B100 C90 E90 |
77-18-04 BEECH: Amendment 39-3028. Applies to Models C90 (serial numbers LJ-689 through LJ-713), E90 (serial numbers LW-167 through LW-216), A100 (serial numbers B-213 through B-232), B100 (serial numbers BE-10 through BE-22), Model 200 (serial numbers BB- 175 through BB-185, BB-187 through BB-193, BB-195 through BB-198, BB-200 through BB- 202, and BB-204 through BB-223), and Model 200T (serial numbers BT-1 and BT-2) airplane certificated in all categories.
Compliance: Required as indicated unless already accomplished.
To assure proper locking of the cabin door and to prevent possible incidents involving loss of cabin pressurization, within the next 25 hours time-in-service after the effective date of this AD, accomplish the following in accordance with Beechcraft Service Instructions No. 0914 or later approved revisions and instructions contained in the applicable airplane maintenance manual:
A. Visually inspect the cabin door latch hooks and pins for proper engagement and adjustment, check the door latch mechanism for over center position when locked, and adjust latch hooks, pins and/or door latch mechanism if necessary.
B. Any equivalent means of compliance with this AD must be approved by the Chief, Engineering and Manufacturing Branch, FAA, Central Region.
This amendment becomes effective on September 12, 1977.