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FAA AD on Airbus model A-300B4-601, A-300B4-603, A-300B4-605R, A-300C4-605R Variant F, A-310/204, and A-310/304 airplanes equipped with General Electric CF6-80C2 engines (2007-07-15)

Washington, Usa - To prevent electrical arcing in the engine pylon, which could result in loss of the relevant alternating current (AC) bus bar, reduced structural integrity of the engine pylon, possible loss of control of plane

Airworthiness Directive Federal Register Information [Page 17376-17379] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2007-27012; Directorate Identifier 2006-NM-188-AD; Amendment 39-15017; AD 2007-07-15] RIN 2120-AA64 Airworthiness Directives; Airbus Model A300 B4-601, A300 B4-603, A300 B4-605R, A300 C4-605R...

fra/pec - 1073087

AVIONEWS - World Aeronautical Press Agency
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