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FAA AD on Boeing model 747-200B, -200C, -200F, and -400F series airplanes (2005-08-09)

Washington, Usa - To find and fix fatigue cracking of the fuselage frame, which could result in reduced structural integrity of the frame and consequent rapid decompression of the airplane

Airworthiness Directive Federal Register Information [Federal Register: April 19, 2005 (Volume 70, Number 74)] [Page 20273-20275] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2005-20136; Directorate Identifier 2004-NM-185-AD; Amendment 39-14061; AD 2005-08-09] RIN 2120-AA64 Airworthiness Directives;...

fra/pec - 118965
Rome, Italy, 04/20/2005 11:58
AVIONEWS - World Aeronautical Press Agency

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