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FAA AD on Boeing model 747-100, -100B, -100B SUD, -200B, -200C, -300, -400, and -400D series airplanes; and model 747SR series airplanes (2005-10-18)
Washington, Usa - To detect and correct stress corrosion cracking of the stop support fittings of the MEDs, which could result in damage to the adjacent forward edge frame of the door and consequent loss of a MED and rapid decompression of the airplane
Airworthiness Directive Federal Register Information [Federal Register: May 19, 2005 (Volume 70, Number 96)] [Page 28800-28803] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2004-19796; Directorate Identifier 2004-NM-61-AD; Amendment 39-14095; AD 2005-10-18] RIN 2120-AA64 Airworthiness Directives;...
fra/pec - 120872
AVIONEWS - World Aeronautical Press Agency
AVIONEWS - World Aeronautical Press Agency