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FAA AD on Turbomeca Arriel 1B, 1D, and 1D1 turboshaft engines
Washington, Usa - To detect and prevent perforation of the NGV2 that could cause fracture of a turbine blade that could result in an uncommanded engine in-flight shutdown on a single-engine helicopter
Airworthiness Directive Federal Register Information [Federal Register: March 23, 2006 (Volume 71, Number 56)] [Page 14636-14638] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2005-22364; Directorate Identifier 2005-NE-26-AD; Amendment 39-14526; AD 2006-06-17] RIN 2120-AA64 Airworthiness Directives; Turbomeca...
fra/pec - 138151
AVIONEWS - World Aeronautical Press Agency
AVIONEWS - World Aeronautical Press Agency