ED Decision 2003/18/RM
(a) Electrical continuity must be provided to prevent the existence of difference of potential between components of the powerplant including fuel and other tanks, and other significant parts of the aeroplane which are electrically conductive.
(b) The cross-sectional areas of bonding connectors if made from copper must not be less than 1.3 mm*.
(c) There must be provisions for electrically bonding the aeroplane to the ground fuelling equipment.
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