A flight display (100) is described. The flight display includes a display screen (102), a physical network interface (106), and multiple processors (110). The flight display interfaces with the flight deck by way of the physical network interface. The dis...

The method involves determining a pitch angle limiting value representative of a maximum admissible angle of incidence, depends on a set of flight parameters and aircraft configurations. A maximum angle of incidence pointer (33) indicating pitch angle limi...

There is described an aircraft (1, 1¹, 1¹¹, 1¹¹¹), comprising a windscreen (50, 50', 50", 50"') arranged in a front side of aircraft (1, 1¹, 1¹¹, 1¹¹¹), characterized in that an edge (55) of windscreen (50, 50', 50", 50¹¹¹) defines a visuali...

The method involves determining a current incidence of an aircraft, and defining a longitudinal scale (10) that depends on a current aerodynamic configuration of the aircraft. The longitudinal scale is presented on a visual display unit, where the scale is...