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FAA AD on Boeing model 737-100, -200, -200C, - 300, -400, and -500 series airplanes (2005-07-12)
Washington, Usa - To detect and correct fatigue cracking of the aft frame and frame support structure of the forward galley door, which could result in a severed fuselage frame web, rapid decompression of the airplane, and possible loss of the forward ga
Airworthiness Directive Federal Register Information [Federal Register: April 7, 2005 (Volume 70, Number 66)] [Page 17596-17598] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2004-18997; Directorate Identifier 2004-NM-19-AD; Amendment 39-14036; AD 2005-07-12] RIN 2120-AA64 Airworthiness Directives;...
fra/pec - 118142
AVIONEWS - World Aeronautical Press Agency
AVIONEWS - World Aeronautical Press Agency