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FAA AD on Boeing model 747 airplanes (2005-14-08)

Washington, Usa - To prevent loss of the underwing fitting load path due to missing or damaged alloy-steel or A286 taperlock fasteners, which could result in separation of the engine and strut from the airplane

Airworthiness Directive Federal Register Information [Federal Register: July 11, 2005 (Volume 70, Number 131)] [Page 39644-39647] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2005-20243; Directorate Identifier 2004-NM-153-AD; Amendment 39-14185; AD 2005-14-08] RIN 2120-AA64 Airworthiness Directives;...

fra/pec - 123645
Rome, Italy, 07/12/2005 14:51
AVIONEWS - World Aeronautical Press Agency

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