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A window replacement for filling a window frame in an aircraft is provided, in particular a passenger aircraft, the window replacement being fixable by a retainer in the window frame in place of the window assembly when the window assembly is removed. The window replacement includes a panel-shaped e

A window replacement for filling a window frame in an aircraft is provided, in particular a passenger aircraft, the window replacement being fixable by a retainer in the window frame in place of the window assembly when the window assembly is removed. The window replacement includes a panel-shaped element with at least a single curvature, the panel-shaped element being made of a synthetic material. The window replacement is formed by a monolithic panel-shaped element. The panel-shaped element of the window replacement may also be formed by a sandwich panel. This allows a weight reduction in comparison with a window replacement of a metallic material.

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1. A window replacement assembly for filling a window frame in an aircraft, the window replacement assembly being fixable by a retainer in the window frame in place of a window assembly when the window assembly is removed, wherein the window replacement assembly is pressed by the retainer onto a sli

1. A window replacement assembly for filling a window frame in an aircraft, the window replacement assembly being fixable by a retainer in the window frame in place of a window assembly when the window assembly is removed, wherein the window replacement assembly is pressed by the retainer onto a slightly conical bearing surface, the retainer being fastened by a fastening element, the fastening element comprising an eye-bolt and a nut screwed onto the eye-bolt, and wherein the window replacement assembly comprises a panel-shaped element with at least a single curvature, with the panel-shaped element being made of a synthetic material and the panel-shaped element being of a monolithic form, the panel-shaped element being enclosed by a peripheral seal, the peripheral seal having a peripheral inner groove for accommodating the panel-shaped element. 2. The window replacement assembly according to claim 1, wherein the window replacement assembly is an aircraft window replacement assembly.