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FAA AD on Boeing model 747-100, 747-100B, 747-100B SUD, 747-200B, 747-200C, 747-200F, 747-300, 747-400, 747-400D, 747-400F, and 747SR series airplanes (2008-25-07)
Washington, Usa - To detect and correct cracks or fractures of the primary structural and fail-safe load paths of the inboard and outboard trailing edge flaps, which could result in the loss of a flap during takeoff or landing
Airworthiness Directive Federal Register Information Federal Register: [Page 75305-75307] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2008-0590; Directorate Identifier 2008-NM-057-AD; Amendment 39-15765; AD 2008-25-07] RIN 2120-AA64 Airworthiness Directives; Boeing Model 747-100, 747-100B, 747- 100B SUD,...
fra/pec - 1097894
AVIONEWS - World Aeronautical Press Agency
AVIONEWS - World Aeronautical Press Agency