The Boeing Company
Light-limiting header assembly for a transition area within an interior cabin of an aircraft

Abstract:

A header assembly is configured to be secured between an inboard structure and an outboard structure within an internal cabin of an aircraft. The header assembly includes a main body including a first panel connected to an opposed second panel by a base panel. The main body is configured to limit light from passing therethrough. At least three separate and distinct anchoring members are configured to securely connect the main body to at least three separate and distinct reciprocal structures of the inboard and outboard structures.