FIELD: transport.
SUBSTANCE: invention relates to aircraft building, particularly to window unit fitted in aircraft outer skin opening. Window unit (1) to be fitted into opening (3) in aircraft outer skin (4) comprises frame (2, 34, 40) to receive package (6). Proposed unit comprises also frame (25, 36). Window frame (2, 34, 40) can be riveted to inner surface (50) of outer skin (4). Also one fastener (14) to secure pressure frame (25, 36) is riveted to window frame (2, 34, 40) and outer skin (4). Window frame (2, 34, 40) has L-like or rectangular cross section.
EFFECT: simplified design, increased glasing area.
13 cl, 5 dwg
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