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FAA AD on Lockheed model 382, 382B, 382E, 382F, 382G, and 382J series airplanes (2008-14-10)

Washington, Usa - To prevent failure of the upper engine mount bolts, which could result in reduced structural capability of an engine mount, and possible separation of a strut and engine from the airplane during flight

Airworthiness Directive Federal Register Information Federal Register: July 7, 2008 [Page 38311-38313] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2008-0740; Directorate Identifier 2008-NM-077-AD; Amendment 39-15605; AD 2008-14-10] RIN 2120-AA64 Airworthiness Directives; Lockheed Model 382, 382B, 382E, 382F,...

fra/pec - 1092030

AVIONEWS - World Aeronautical Press Agency
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