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FAA AD on Boeing model 747-100, 747-100B, 747- 200B, 747-200C, 747-200F, 747-300, 747SR, and 747SP series airplanes (2007-15-07)

Washington, Usa - To detect and correct fatigue cracking of the fuselage skin near stringer 5. Cracks in this area could join together and result in in-flight depressurization of the airplane

Airworthiness Directive Federal Register Information [Federal Register: July 30, 2007 (Volume 72, Number 145)] [Page 41433-41436] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2007-27359; Directorate Identifier 2006-NM-042-AD; Amendment 39-15136; AD 2007-15-07] RIN 2120-AA64 Airworthiness Directives; Boeing...

fra/pec - 1077645

AVIONEWS - World Aeronautical Press Agency
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