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FAA AD on Turbomeca Arriel 1B, 1D, 1D1, and 1S1 turboshaft engines (2010-10-09)

Washington, Usa - To prevent the failure of 2nd stage turbine blades, which could result in an uncommanded in- flight engine shutdown, and a subsequent forced autorotation landing or accident

Airworthiness Directive Federal Register Information Federal Register: [Page 27411-27414] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2005-21242; Directorate Identifier 2005-NE-09-AD; Amendment 39-16288; AD 2010-10-09] RIN 2120-AA64 Airworthiness Directives; Turbomeca Arriel 1B, 1D, 1D1, and 1S1 Turboshaft...

fra/pec - 1118299
Rome, Italy, 06/16/2010 18:22
AVIONEWS - World Aeronautical Press Agency

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