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 737-100, -200C, -300, - 400, and -500 series airplanes (2005-07-19)
Washington, Usa - To find and fix fatigue cracking in the fuselage skin, doubler, bearstrap, and frames, which could result in reduced structural integrity of the frames, possible loss of a cargo door, and consequent rapid decompression of the fuselage
Airworthiness Directive Federal Register Information [Federal Register: April 7, 2005 (Volume 70, Number 66)] [Page 17600-17603] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2004-19003; Directorate Identifier 2003-NM-245-AD; Amendment 39-14044; AD 2005-07-19] RIN 2120-AA64 Airworthiness Directives;...
fra/pec - 118147
AVIONEWS - World Aeronautical Press Agency
AVIONEWS - World Aeronautical Press Agency