Stapled peel ply strip on leading edge of aileron. As usual had to strip down the stapler twice before the end...
Upper skin layup as per plans. Micro'd foam and floxed gaps between spar cap and shear web, ends of plies in the spar cap and trailing edge overlap are where foam was removed by the peel ply, 2 x UND crossways. 1 x UND along the wing forward of the aileron. 2 bits of UND reinforcement at the notch, and 1 x BID over the tip. All joins peel plied. 2.7kg of resin used, Made one batch of 350g when the lid fell off a resin bottle. Thankfully was able to calculate the required extra hardener before the scales reset.