Joint assembly and method of assembling same

摘要

JOINT ASSEMBLY AND METHOD OF ASSEMBLING SAME Abstract Ajoint assembly (400) for an aircraft (300) is provided. The joint assembly (400) includes a single main fitting (402) including a first flange (410), a second flange (412), and a third flange (414), an external spar component (404) coupled to the first flange (410) using at least one fastener (420), an internal spar component (406) coupled to the second flange (412) using at least one fastener (420), and a body rib (408) coupled to the third flange (414) using at least one fastener (420). --------j 44----- ----------------