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FAA AD on General Electric Company CF34-8E series turbofan engines

Washington, Usa - To prevent dual-channel electrical signal faults in the master VG actuator which will cause an uncommanded reduction of thrust to idle with a subsequent loss of the ability to advance thrust above idle, and will result in a multiengine

Airworthiness Directive Federal Register Information [Federal Register: April 5, 2005 (Volume 70, Number 64)] [Page 17199-17201] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2004-NE-06-AD; Amendment 39-14033; AD 2005-07-09] RIN 2120-AA64 Airworthiness Directives; General Electric Company CF34-8E Series...

fra/pec - 117882
Rome, Italy, 04/06/2005 11:45
AVIONEWS - World Aeronautical Press Agency

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