§25.899 Electrical bonding and protection against static electricity.

[(a) Electrical bonding and protection against static electricity must be designed to minimize accumulation of electrostatic charge that would cause-- (1) Human injury from electrical shock, (2) Ignition of flammable vapors, or (3) Interference with installed electrical/electronic equipment. (b) Compliance with paragraph (a) of this section may be shown by-- (1) Bonding the components properly to the airframe; or (2) Incorporating other acceptable means to dissipate the static charge so as not to endanger the airplane, personnel, or operation of the installed electrical/electronic systems.]