I'm curious about some of the carbon fiber items that some have added into the aircraft -- things like floorboards, wing root blank, panel, centre console sides, accessory jack panels behind the shoulder on seat - maybe even the fairings on the trailing edge of the tail and leading edge of the rudder?

I'm considering making some gap seals for the horizontal/elevator and I have kinda gone down a rabbit hole here, and I'm looking for some advice - More specifically on Carbon Fiber and using it in EAB.

I got to reading about galvanic corrosion and how it relates to carbon fibre and dissimilar conductive metals. Is this an issue for the afore mentioned items? And if so -- what are people doing about it?

Any advice would be great. Thanks.