Airworthiness Directive

AD 95-09-13 60 FR 22496

Federal Aviation Administration · 14 CFR part 39

FR document
95-10833
Amendment
39-9217
Published
1995-05-08
Models covered
5
Last live check
2026-08-17
AD

95-09-13

FR doc 95-10833 · 60 FR 22496

AD 95-09-13Published 1995-05-08Effective 1995-06-14

Requires repetitively inspecting each fuel inlet float valve in accordance with certain test procedures on Cessna Aircraft Company (Cessna) Models T303, 402C, 404, 414A, and 421C airplanes, and replacing any valve that does not…

Full official abstract

This amendment supersedes AD 93-05-03, which currently requires repetitively inspecting each fuel inlet float valve in accordance with certain test procedures on Cessna Aircraft Company (Cessna) Models T303, 402C, 404, 414A, and 421C airplanes, and replacing any valve that does not pass this test. The manufacturer has developed fuel inlet float valves of improved design, and the Federal Aviation Administration (FAA) has determined that the improved valves should be installed to reduce the number of repetitive tests currently required by AD 93-05-03. This action requires installing these fuel inlet float valves of improved design. The actions specified by this AD are intended to prevent possible loss of engine power caused by failure of a fuel inlet float valve.

Applies to 5 models in our index