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FAA AD on Airbus model A-300 B2 and B4; A-300 B4-600, B4-600R, and F4-600R, A-300 C4-605R Variant F; A-310/200 and -300 series airplanes (2005-17-14)
Washington, Usa-To prevent desynchronization of one of the three rudder servo actuators, which, if combined with an engine failure, could result in the loss of the related hydraulic system and could cause the loss of one of the two synchronized actuators
Airworthiness Directive Federal Register Information [Federal Register: August 26, 2005 (Volume 70, Number 165)] [Page 50157-50160] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2005-20794; Directorate Identifier 2004-NM-172-AD; Amendment 39-14235; AD 2005-17-14] RIN 2120-AA64 Airworthiness Directives;...
fra/pec - 125800
AVIONEWS - World Aeronautical Press Agency
AVIONEWS - World Aeronautical Press Agency