Climate-neutral aviation requires resource-efficient composite manufacturing technologies and viable solutions for the reuse of carbon fibers (CF). In this context, thermoplastic composites (TPC) can make a strong contribution. Thermoforming of TPC is an efficient and established process for aerospace components. But it’s efficiency could be further increased by integration of joining processes, which would otherwise be separate steps. In this work, a two-step thermoforming process for hollow box structures, particularly uplift structures, is presented. The starting point are two organosheets. First, one of the organosheets, intended for the bottom skin of the uplift structure, is thermoformed. After cooling, the press opens, the organosheet remains in the press and an infrared heater is pivoted in, to locally heat up just the joining area. Meanwhile, a second organosheet, intended for the top skin, is heated and thermoformed and simultaneously joined to the lower skin, thereby forming