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FAA AD on Pratt & Whitney Canada (PWC) PW535A turboshaft engines

Washington, Usa - To prevent lack of engine response to power lever input, which could cause a single or dual engine in-flight shutdown event

Airworthiness Directive Federal Register Information [Federal Register: April 21, 2006 (Volume 71, Number 77)] [Page 20531-20533] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2006-24117; Directorate Identifier 2006-NE-07-AD; Amendment 39-14570; AD 2006-08-13] RIN 2120-AA64 Airworthiness Directives;...

fra/pec - 139657
Rome, Italy, 04/24/2006 14:15
AVIONEWS - World Aeronautical Press Agency

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