Dropped back to install the nuts and washers on the bolts that I have installed so far on the flight controls.
The control sticks get castle nuts and cotter pins where they connect to the control column fork. I guess they could have used regular nylon locknuts here because the bolt and bushing do not rotate. I don't know why they went this route but I don't ask questions.The aileron rod end at the control stick gets a nylon locknut and washer because the bolt does not rotate when torqued down.
The elevator control cable attach points get castle nuts and cotter pins because these are only finger tight so the spade end of the cable can freely pivot on the bolt in between the steel forks.
The inboard aileron control pushrod ends get nylon locknuts on the studs because the studs do not rotate after torquing.
The carnage to get all of these fasteners installed. The DNA left on this airplane will definitely prove that I built it.