Disassembly and final prep of the forward fuselage continued. First the side skins were removed and set aside. Then the forward bulkheads were removed, deburred, dimpled, platenuts attached and rudder cable bole enlarged to proper size.
Forward skin stiffener and angle clip removed, deburred, and countersunk.
Auxillary longeron removed, deburred, and dimpled.
Baggage area floor skins removed, deburred and dimpled.
A coat of primer was applied to the angle components.