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 747-100B SUD, -200B, - 200C, -200F, and -300 series airplanes
Usa - To detect and correct fatigue cracks in the frames and body skin at BS 420, 440, and 460 between stringers S-8 and S-12 inclusive, which could lead to severed frames, and consequent rapid decompression and loss of the structural integrity
Airworthiness Directive Federal Register Information [Federal Register: March 4, 2005 (Volume 70, Number 42)] [Page 10485-10488] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2005-20431; Directorate Identifier 2005-NM-040-AD; Amendment 39-13995; AD 2005-04-51] RIN 2120-AA64 Airworthiness Directives;...
fra/pec - 115674
AVIONEWS - World Aeronautical Press Agency
AVIONEWS - World Aeronautical Press Agency