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FAA AD on Boeing model 747-100, -200B, -200F, - 200C, -100B, -300, -100B SUD, -400, -400D, and -400F; and 747SR series airplanes

Washington, Usa - To prevent cracking and other damage of the actuator attach fittings of the trailing edge flaps, which could result in abnormal operation or retraction of a trailing edge flap, and possible loss of controllability of the airplane

Airworthiness Directive Federal Register Information [Federal Register: October 4, 2005 (Volume 70, Number 191)] [Page 57740-57746] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2005-20917; Directorate Identifier 2004-NM-85-AD; Amendment 39-14312; AD 2005-20-18] RIN 2120-AA64 Airworthiness Directives;...

fra/pec - 128305

AVIONEWS - World Aeronautical Press Agency
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