The wing electrical wires exit the wing aft of the main spar. I did not want the loom entering the fuselage aft of the main spar near the aileron and flap torque tubes. I remembered a Sling 4 builder years ago re-directed the loom forward of the spar, therefore entering the fuselage clear of the torque tubes. ( thanks Jim ). I made a bracket to support the loom with a P-Clamp and the loom will now enter the fuselage forward of the main spar. This will also allow the fuel sender wire to be added to the wing loom.