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FAA AD on General Electric Company CF34-8C1 series and CF34-8C5 series turbofan engines
Washington, Usa- To prevent dual-channel electrical signal faults in the VG master actuator, which will cause an uncommanded reduction of thrust to idle with a subsequent loss of the ability to advance thrust above idle, and which will result in a multie
Airworthiness Directive Federal Register Information [Federal Register: March 31, 2005 (Volume 70, Number 61)] [Page 16401-16403] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2003-NE-58-AD; Amendment 39-14030; AD 2005-07-06] RIN 2120-AA64 Airworthiness Directives; General Electric Company CF34-8C1 Series...
fra/pec - 117687
AVIONEWS - World Aeronautical Press Agency
AVIONEWS - World Aeronautical Press Agency