FIELD: aircraft engineering.
SUBSTANCE: claimed aircraft extra indicator comprises the panel with point electric instrument and glass arranged there ahead. Said panel is located on one side or ahead and sideways of the pilot. Contrast or illuminated horizontal line is applied on said glass. Said point is shaped to aircraft side contour. The instrument is connected to available gyro with electric display of its parameters.
EFFECT: lower risks of the spatial orientation loss.
9 cl, 1 dwg
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