Overview
The wing is a fully cantilevered, one piece, sweepback airfoil that is the primary structure to hold the load of the aircraft. The wing is found at the bottom of the fuselage middle section. The wing is attached to the fuselage keel longerons and the fuselage frames. It is attached to the fuselage keel longerons at the center of the front and rear spars. It is attached to the fuselage frames at two locations on the front and rear spars of the wing center section. The aspect ratio of the wing is 7.28 (net wing), the dihedral is 2.15 degrees, and the sweepback is 27°. The front spar is set at 8 percent chord. The rear spar is set at 67 percent chord.
