The leading edge of the shoulder-mounted wing was swept back at an angle of 43° and the wing itself was given a dihedral of 6°. Seven fuel tanks were housed in the two-spar wing and dive brakes were positioned on its upper surface.
The leading edge of the shoulder-mounted wing had an angled backward tilt of 43°, and the wing itself exhibited a slight upward inclination of 6°. The wing's upper surface accommodated seven fuel tanks, and the dive brakes were positioned there as well.