CS 25.775 Windshields and windows

• ED Decision 2016/010/R found in: CS-25 Amdt 27 - Large Aeroplanes (Jan 2023)

CS 25.775 Windshields and windows ED Decision 2016/010/R (See AMC 25.775) (a) Internal panes must be made of non-splintering material. (b) Windshield panes directly in front of the pilots in the normal conduct of their duties, and the supporting structures for these panes, must withstand, without penetration, the bird impact conditions specified in [CS 25.631](#_DxCrossRefBm1709821047). (c) Unless it can be shown by analysis or tests that the probability of occurrence of a critical windshield fragmentation condition is of a low order, the aeroplane must have a means to minimise the danger to the pilots from flying windshield fragments due to bird impact. This must be shown for each transparent pane in the cockpit that – (1) Appears in the front view of the aeroplane; (2) Is inclined 15° or more to the longitudinal axis of the aeroplane; and (3) Has any part of the pane located where its fragmentation will constitute a hazard to the pilots. (d) The design of windshields and windows in pressurised aeroplanes must be based on factors peculiar to high altitude operation, including the effects of continuous and cyclic pressurisation loadings, the inherent characteristics of the material used, and the effects of temperatures and temperature differentials. The windshield and window panels must be capable of withstanding the maximum cabin pressure differential loads combined with critical aerodynamic pressure and temperature effects after any single failure in the installation or associated systems. It may be assumed that, after a single failure that is obvious to the flight crew (established under [CS 25.1523](#_DxCrossRefBm1709821183)), the cabin pressure differential is reduced from the maximum, in accordance with appropriate operating limitations, to allow continued safe flight of the aeroplane with a cabin pressure altitude of not more than 4572m (15 000 ft) (see [AMC 25.775(d)](#_DxCrossRefBm1709821195)). (e) The windshield panels in front of the pilots must be arranged so that, assuming the loss of vision through any one panel, one or more panels remain available for use by a pilot seated at a pilot station to permit continued safe flight and landing. [Amdt 25/18]