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FAA AD on Turbomeca SA Arriel 2B turboshaft engines (2005-13-25R1)
Washington, Usa - To prevent loss of control of engine fuel flow in manual control mode or mixed control mode, which can lead to engine overspeed, and in-flight engine shutdown resulting in a forced autorotation landing
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Airworthiness Directive Federal Register Information [Page 19110-19112] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2005-21624; Directorate Identifier 2005-NE-17-AD; Amendment 39-15028; AD 2005-13-25R1] RIN 2120-AA64 Airworthiness Directives; Turbomeca S.A. Arriel 2B Turboshaft Engines PDF Copy (If Available): Preamble...
fra/pec - 1073438
AVIONEWS - World Aeronautical Press Agency
AVIONEWS - World Aeronautical Press Agency