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FAA AD on Turbomeca Turmo IV A and IV C Series Turboshaft Engines (2009-02-08)
Washington, Usa - To prevent helicopter engine in-flight shutdown of one or both engines resulting in an emergency auto-rotation landing or accident
Airworthiness Directive Federal Register Information Federal Register: February 17, 2009 [Page 7310-7313] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2006-25730; Directorate Identifier 2006-NE-31-AD; Amendment 39-15798; AD 2009-02-08] RIN 2120-AA64 Airworthiness Directives; Turbomeca Turmo IV A and IV C...
fra/pec - 1099957
AVIONEWS - World Aeronautical Press Agency
AVIONEWS - World Aeronautical Press Agency