After I had completed a lot of cleaning, abrading and alodining of the forward fuselage parts yesterday I carried out their priming today. My brother Bernie came over so we also dimpled the F-706 bulkhead and all the associated skins on the fuselage production joint, as well as preparing the skin for riveting at the F-704 bulkhead, we riveted in the brake bracket and fuel pump firewall doubler onto the firewall, located and drilled the holes for the static ports in the aft fuselage assembly, deburred and dimpled the aft fuselage assembly skins where they mate with the F-718 longerons and riveted in the bracket for the autopilot elevator servo.
Primed longerons, ribs, etc..
Brake bracket and fuel pump firewall doubler riveted on
