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FAA AD on Boeing model 747-100, -100B, 100B SUD, -200B, -200C, -200F, and -300 series airplanes; and model 747SP and 747SR series airplanes (2005-08-01)

Washington, Usa - To detect and correct fatigue cracks in the body frames, skin and other internal structure in fuselage section 41, which could lead to rapid decompression and loss of the structural integrity of the airplane

Airworthiness Directive Federal Register Information [Federal Register: April 11, 2005 (Volume 70, Number 68)] [Page 18290-18294] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2005-20915; Directorate Identifier 2005-NM-042-AD; Amendment 39-14053; AD 2005-08-01] RIN 2120-AA64 Airworthiness Directives;...

fra/pec - 118370
Rome, Italy, 04/12/2005 15:56
AVIONEWS - World Aeronautical Press Agency

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