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Questa traduzione è in preparazione. Nel frattempo mostriamo temporaneamente la versione originale in inglese.

Imprese · 19/09/19941 min di lettura

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

Traduzione automatica locale · Lingua originale della fonte

Riepilogo

This document proposes to supersede 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. The proposed action would require installing these fuel inlet float valves of improved design. The actions specified by the proposed AD are intended to prevent possible loss of engine power caused by failure of a fuel inlet float valve.

Lingua originale della fonte: Federal Register — Transportation DepartmentApri il comunicato originale →

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