RE: Finding cg on plane
The spar is about 20 to 25% back from the leading edge of the wing. On some wings the front part from the leading edge is sheeted to the spar. The spar will go the entire length of the wing. Swept wing is one where the leading edge is not straight from one side of the wing to the other. The tip of the wing will be farther back towards the tail than the wing at the fuselage.