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FAA AD on Turbomeca Astazou XIV B and XIV H turboshaft engines (2005-25-12)
Washington, Usa - To prevent failure of 2nd stage axial compressor wheel blades, leading to in-flight engine shutdown and autorotation landing
Airworthiness Directive Federal Register Information [Federal Register: December 13, 2005 (Volume 70, Number 238)] [Page 73581-73583] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2005-23004; Directorate Identifier 2005-NE-42-AD; Amendment 39-14405; AD 2005-25-12] RIN 2120-AA64 Airworthiness Directives;...
fra/pec - 132927
AVIONEWS - World Aeronautical Press Agency
AVIONEWS - World Aeronautical Press Agency