<p>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.</p>
