Abstract: An aircraft galley configuration (10) extending along a longitudinal axis of a fuselage of an aircraft and on one side of the aircraft includes a forward end (12) of the galley (10) closest to the front of the aircraft and a rear end (14) of the galley (10) on an opposite longitudinal end of the galley (10) and closest to a passenger section of the aircraft, and a plurality of galley modules (20, 22, 24, 26) disposed in the galley (10) between the forward (12) and rear ends (14) of the galley. The galley modules comprise a storage module (20), a heating module (22), a preparation module (24), and a service module (26). The storage module (20) is disposed at the forward end (12) of the galley (10) and the service module (26) is disposed at the rear end (14) of the galley (10), An efficient work flow in the direction of the passenger section is created by the galley configuration (10).

Abstract: Door assemblies for aircraft interiors are described. Such door assemblies may comprise a door for opening and closing an aperture between zones of the aircraft interior and an interface configured to couple the door to the aircraft interior. A pressure-relief element may form at least a portion of the door wherein the pressure-relief element is retained by a magnetic force calibrated to permit release of the pressure-relief element upon presence of a predetermined pressure differential across the pressure-relief element. Components and mechanisms useful in reducing light bleed across doors for aircraft interiors are also disclosed.