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FAA AD on Airbus model A-300B2 and B4 series airplanes

Washington, Usa - To ensure that the flightcrew is aware of the procedures for resetting the trim and pitch trim levers after each landing and to prevent failure of the servomotors of the pitch trim systems during flight

Airworthiness Directive Federal Register Information [Federal Register: January 17, 2007 (Volume 72, Number 10)] [Page 1928-1931] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2006-25670; Directorate Identifier 2006-NM-027-AD; Amendment 39-14868; AD 2006-26-10] RIN 2120-AA64 Airworthiness Directives;...

fra/pec - 72703
Rome, Italy, 01/18/2007 12:06
AVIONEWS - World Aeronautical Press Agency

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