AIRCRAFT WITH MULTI SPAR BOX CONNECTION TO FUSELAGE

The invention provides an aircraft with a multi spar box connection to a fuselage. The aircraft has a vertical stabilizer with a multi-spar box and a base rib assembly secured to the multi-spar box. The base rib assembly has front longitudinal lugs, rear longitudinal lugs, and opposing middle longitudinal lugs. Front clevises corresponding to the front longitudinal lugs are secured to frame members of the fuselage of the aircraft and each has a first, second, and third mounting arms. Rear clevises corresponding to the rear longitudinal lugs are secured to frame members and each has a first, second, and third mounting arms. Middle clevises corresponding to the middle longitudinal lugs are secured to frame members and each has only first and second mounting arms. Retaining members inserted through mounting holes in each longitudinal lug and mounting holes in each corresponding clevis secures the vertical stabilizer to the fuselage. 一种具有连接至机身的多翼梁盒的飞机，该飞机具有垂直尾翼，该垂直尾翼具有多翼梁盒和固定至多翼梁盒的基肋组件。基肋组件具有前纵向凸耳、后纵向凸耳和相对的中间纵向凸耳