Which ATA chapter focuses on airplane statics and loads distribution?

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Understanding how static forces act on the airframe and how those forces are carried through the structure is the key idea. Airplane Statics focuses on equilibrium under static loading, determining how weight, payload, fuel, and aerodynamic forces translate into reactions, load paths, and stresses in the airframe, as well as how the center of gravity affects those loads. This makes it the chapter that covers the fundamentals of static loads and how they are distributed within the aircraft structure, which is essential for safe design, maintenance, and inspection. The other topics are about administrative tasks, handling during maintenance, or general support concepts, none of which address the analysis of static loads and load distribution the way Airplane Statics does.