Air frame structural components are everything comprising the fuselage including: doors, wing spars, flight control surfaces, ailerons, bulkheads, stringers, and wing panels. Not only is the air frame subjected to the forces in flight, but also the impact loads associated with take-off and landing.
Corrosion resistant materials are used in areas where strength and resistance to the elements are mandatory. Aluminium and titanium are used in areas where strength and lightness is a priority. Many titanium components are heat treated in vacuum furnaces. Aluminium can be treated in vacuum or air atmosphere.
Process solutions for this component include: