In the first section of the EX2 Fuselage Manual (Page 11) there is a requirement to remove powder coat at the left top bolt housing on the fuselage to later enable an earth connection to the Firewall forward part of the aircraft.
I am at the point of final boot cowl fixing, however there is no further information or parts call to complete the earth connection to the forward section. I am aware of a braided earth connection further forward from the engine mount to engine itself and expected something similar.
What is the proposed method and what components are used?