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FAA AD on Boeing model 737-100, -200, -200C, - 300, -400, and -500 series airplanes (2008-13-12)

Washington, Usa - To detect and correct fatigue cracking of the upper frame to side frame splice of the fuselage, which could result in reduced structural integrity of the frame and adjacent lap joint

Airworthiness Directive Federal Register Information Federal Register: [Page 38905-38908] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2007-0184; Directorate Identifier 2007-NM-140-AD; Amendment 39-15575; AD 2008-13-12] RIN 2120-AA64 Airworthiness Directives; Boeing Model 737-100, -200, -200C, - 300, -400,...

fra/pec - 1092218
Rome, Italy, 07/11/2008 12:14
AVIONEWS - World Aeronautical Press Agency

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