| AD Number | 75-26-04 | Status | Active |
| Effective Date | December 19, 1975 | Issue Date | Not specified |
| Docket Number | Unknown | Amendment | 39-2458 |
| 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 |
75-26-04 BEECH: Amendment 39-2458. Applies to Model 200 (BB-2 through BB-71) airplanes.
Compliance: Required as indicated, unless already accomplished.
To prevent malfunction of the fuel transfer system, within the next 50 hours' time in service after the effective date of this AD, accomplish the following:
A) Inspect the P/N 100-920067-1 fuel vent float valve for opening and operation in accordance with the criteria set forth in Beechcraft Service Instruction No. 0772-295 or later FAA-approved revision. (P/N 101-320035-1 baffle, if installed, must be removed to perform this inspection.)
B) Replace any fuel vent float valve assembly that does not meet the criteria set forth in Beechcraft Service Instruction No. 0772-295 or later FAA-approved revision with new P/N 100-920067-1 fuel vent float valve assembly.
C) Any equivalent method of compliance with this AD must be approved by the Chief, Engineering and Manufacturing Branch, FAA, Central Region.
Thisamendment becomes effective December 19, 1975.