この記事の翻訳を準備しています。それまでの間、英語の原文を表示します。
ビジネス · 2005/6/211 分で読めます
Airworthiness Directives; General Electric Company CT64-820-4 Turboprop Engines
ローカル自動翻訳 · 情報源の原言語
概要
The FAA is adopting a new airworthiness directive (AD) for General Electric Company (GE) CT64-820-4 turboprop engines with stage 1 turbine disk and shaft, part number (P/N) 6004T47P03 or 4921T10P02 installed. This AD requires removing from service these stage 1 turbine disk and shafts at reduced compliance times. This AD results from the discovery by the manufacturer of low-cycle-fatigue (LCF) cracks found in stage 1 turbine disk and shafts, P/Ns 6004T47P03 and 4921T10P02. We are issuing this AD to prevent uncontained failure of the stage 1 turbine disk and shaft, resulting in damage to the airplane.
情報源の原言語: Federal Register — Federal Aviation Administration原文の発表を開く →