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FAA AD on Boeing model 747-100B SUD, -300, -400, and -400D series airplanes (2005-05-08)

Washington, Usa - To prevent fatigue cracking of the fuselage frame to tension tie joints, which could result in severing of the tension ties and consequent rapid decompression of the airplane fuselage

Airworthiness Directive Federal Register Information [Federal Register: March 11, 2005 (Volume 70, Number 47)] [Page 12113-12115] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2004-19470; Directorate Identifier 2003-NM-268-AD; Amendment 39-13997; AD 2005-05-08] RIN 2120-AA64 Airworthiness Directives;...

fra/pec - 116196
Rome, Italy, 03/14/2005 13:38
AVIONEWS - World Aeronautical Press Agency

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