The left long aileron push rod was inserted into the wing and temporarily connected to the bellcrank. The left aileron joiner was clamped in its neutral position. The inboard fitting for the push rod was temporarily bolted to the right aileron joiner and held in position against the push rod, and the push rod was marked for cutting to length. The pushrod and its inboard end fitting were removed, the tube cut to the mark, both were fit together, then drilled and riveted together. The push rod assembly was reinserted into the wing and connected on both ends.
The deflection of both ailerons was checked with the entire wing control system in place, and found to be in good shape.
Both fuselage joiners were mounted in their respective positions, and the joiner pushrods were attached to the control stick tab with temporary fasteners.
