14 CFR 27.610 - Lightning and static electricity protection.
(2) Incorporating acceptable means of diverting the resulting electrical current so as not to endanger the rotorcraft.
(2) Minimize the risk of electric shock to crew, passengers, and service and maintenance personnel using normal precautions;
(3) Provide an electrical return path, under both normal and fault conditions, on rotorcraft having grounded electrical systems; and
(4) Reduce to an acceptable level the effects of static electricity on the functioning of essential electrical and electronic equipment.
Title 14 published on 2014-01-01
no entries appear in the Federal Register after this date.