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FAA AD on Turbomeca Arriel 1B, 1D, 1D1, and 1S1 turboshaft engines (2008-07-01)

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

Airworthiness Directive Federal Register Information Federal Register: [Page 15866-15868] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2005-21242; Directorate Identifier 2005-NE-09-AD; Amendment 39-15442; AD 2008-07-01] RIN 2120-AA64 Airworthiness Directives; Turbomeca Arriel 1B, 1D, 1D1, and 1S1 Turboshaft...

fra/pec - 1087947
Rome, Italy, 04/03/2008 15:28
AVIONEWS - World Aeronautical Press Agency

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