Do you want to access to this and other private contents?
Log in if you are a subscriber or click here to request service
FAA AD on Boeing model 747 airplanes (2006-24-05)
Washington, Usa - To detect and correct fatigue cracks at the fastener rows of the fuselage skin in section 41, which could join together and cause a loss of structural integrity and rapid decompression of the airplane
Airworthiness Directive Federal Register Information [Federal Register: November 27, 2006 (Volume 71, Number 227)] [Page 68434-68437] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2006-26388; Directorate Identifier 2006-NM-234-AD; Amendment 39-14834; AD 2006-24-05] RIN 2120-AA64 Airworthiness Directives;...
fra/pec - 70316
AVIONEWS - World Aeronautical Press Agency
AVIONEWS - World Aeronautical Press Agency