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FAA AD on Turbomeca Makila 1A and 1A1 turboshaft engines (2008-08-16)

Washington, Usa - To prevent dual-engine continued operation at 65% N1 after reversion of the ECU to the 65% N1 back-up mode due to temporary loss of N2 speed signal, which could lead to inability to continue safe flight

Airworthiness Directive Federal Register Information Federal Register: [Page 20525-20526] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2007-0157; Directorate Identifier 2001-NE-23-AD; Amendment 39-15469; AD 2008-08-16] RIN 2120-AA64 Airworthiness Directives; Turbomeca Makila 1A and 1A1 Turboshaft Engines...

fra/pec - 1088790
Rome, Italy, 04/24/2008 14:10
AVIONEWS - World Aeronautical Press Agency

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