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FAA AD on Turbomeca Turmo IV A and IV C series turboshaft engines
Washington, Usa - To prevent centrifugal compressor intake wheel blade cracks, which can result in engine in-flight power loss, engine shutdown, or forced landing
Airworthiness Directive Federal Register Information [Federal Register: November 16, 2006 (Volume 71, Number 221)] [Page 66664-66665] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2006-25970; Directorate Identifier 99-NE-12-AD; Amendment 39-14829; AD 2006-23-17] RIN 2120-AA64 Airworthiness Directives;...
fra/pec - 69493
AVIONEWS - World Aeronautical Press Agency
AVIONEWS - World Aeronautical Press Agency