AGUSTA Model A109S helicopters [Docket No. FAA-2012-0448; Directorate Identifier 2010-SW-016-AD] – proposes to require modifying the electrical power distribution system to carry a higher electrical load. This proposed AD is prompted by an electrical failure on an Agusta Model A109E helicopter that resulted from “inadequate functioning of the 35 amperes (amps) BATT BUS circuit breaker.” The proposed actions are intended to require modifying the electrical power distribution system to ...
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