A system and method for installing a window panel onto an aircraft including providing a retaining device having an outside edge that is sealed against an inboard surface of the aircraft. A biasing member mounted to an inside edge of the retaining device includes spring clips that press against the window panel. The spring clips push the window panel outward against the outside edge of the retaining device to maintain a seal around the edge of the window panel.
Window assembly installation
17.05.2016
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |