Snap-in window assembly and method

Details Snap-in window assembly and method Snap-in window assembly and method

B - Operations, Transporting

64

C

B64C 1/14 (2006.01) B60J 1/08 (2006.01)

Patent

CA 2405923

An aircraft window assembly with a readily attachable window assembly for efficient and easy installation and maintenance of aircraft windows is provided. The aircraft has a sidewall having an inner perimeter that defines an opening. An inner window frame is readily attachable to the sidewall adjacent to the inner perimeter. The inner window frame defines a first opening. An outer window frame is readily attachable to the inner window frame adjacent the first opening and the outer window frame defines a second opening. The outer window frame and the inner window frame are releasably coupled within the first opening of the inner window frame. The snap-in window assembly is readily detachable from the sidewall adjacent to the inner perimeter.

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