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FAA AD on The Boeing Company model 737/200, /200C, /300, /400, and /500 series airplanes (2011-24-12)

Washington, Usa - To detect and correct fatigue cracking of the fuselage skin panels, which could result in sudden fracture and failure of the fuselage skin panels, and consequent rapid decompression of the airplane

[Federal Register Volume 76, Number 231 (Thursday, December 1, 2011)] [Rules and Regulations] [Pages 74667-74670] From the Federal Register Online via the Government Printing Office [www.gpo.gov] [FR Doc No: 2011-30608] –––––––––––––––––––––––––––––––––– DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2011-0914; Directorate Identifier 2010-NM-166-A...

fra/pec - 1136217

AVIONEWS - World Aeronautical Press Agency
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