FIELD: aviation.
SUBSTANCE: aircraft includes the windshield (50), located on the front side of the aircraft, the edge (55) of which defines a visualization area (49), visible to the operator, and displaying device (58), designed to display visual information (20, 25, ) relating to the flight parameters, within the visualization area (49). The visual information comprises the first image (25,), connected with the aircraft aiming relative to the ground and containing a line parallel to the horizon line(26). The mentioned line is visible to the pilot on the panel (7), when the aircraft is tilted relatively the horizontal plane so, that the nose is higher than the anti-torque rotor.
EFFECT: ability to use the machine under low visibility conditions.
15 cl, 11 dwg
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