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Airworthiness Directives; Cessna Aircraft Company Models T303, 402C, 404, 414A, and 421C Airplanes

airworthiness · Rule · Final rule. · Published 1995-05-08 · Effective 1995-06-14 · 60 FR 22496

Document

Document number
95-10833
Federal Register citation
60 FR 22496
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Cessna
Publication date
1995-05-08
Effective date
1995-06-14
FAA docket
Docket No. 94-CE-06-AD

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.

Source

Authoritative
Federal Register document
Machine
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