FIELD: transport.
SUBSTANCE: invention refers to aircraft industry, and namely to the door of aircraft cabin. Door (1) includes one-piece door construction (2) from fibrous composite material, which contains outer skin (4) and door frame located on inner side of outer skin (4). The main load-carrying elements of the frame are edge bearing members (6a, 6b) and longitudinal bearing members (8; 8a-8f) attaching edge bearing members (6a, 6b). Gaps (2a) of door frame, which are restricted with inner side of outer skin (4), edge bearing members (6a, 6b) and longitudinal bearing members (8; 8a-8f), are made so that they are open on inner side of the door.
EFFECT: weight is decreased and strength of door is increased.
28 cl, 11 dwg
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