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FAA AD on Boeing model 737-100, -200, -200C, - 300, -400, and -500 series airplanes (2005-20-03)
Washington, Usa - To detect and correct fatigue cracking of the intercostals on the forward and aft sides of the forward entry door, which could result in loss of the forward entry door and rapid decompression of the airplane
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Airworthiness Directive Federal Register Information [Federal Register: September 27, 2005 (Volume 70, Number 186)] [Page 56361-56365] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2005-18788; Directorate Identifier 2003-NM-203-AD; Amendment 39-14296; AD 2005-20-03] RIN 2120-AA64 Airworthiness Directives;...
fra/pec - 127901
AVIONEWS - World Aeronautical Press Agency
AVIONEWS - World Aeronautical Press Agency