AD 75-26-04

Airworthiness directive · Fuel Transfer System · Textron 200

Effective
December 19, 1975
Model
200
Data sheet
TCDSA24CE
Registered aircraft
234 matched by model
Product
Aircraft · Small/large airplane
Amendment
39-2458

Unofficial copy of the text in the FAA’s Dynamic Regulatory System. The FAA’s own copy is the authoritative one. DRS record last changed January 21, 2026.

On this page

The airworthiness directive

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.

Affected TCDS · 1

The type certificate data sheets for the models this AD names, matched by model and maker.

Registered aircraft · 234

Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.

By aircraft maker
  • Beech234 aircraft
By year built
19751984
Registered aircraft by year built: 211 aircraft
197514
197616
197720
197828
197949
198047
198130
19823
19831
19843

23 with no year recorded

By model

Aircraft

See all 234 aircraft