Abstract: To prevent deposition of ice on the frontal surface of for instance, the horizontal tail of aircraft anti-icing member is installed in front of the edge along its entire length. The member has an airfoil profile with a chord equal to 3-8% of that of the tail to be protected and is located in a zone not exceeding the tail is thickness, a duct being formed between the member and the surface to be protected for the passage of an accelerated air stream.

Abstract: The apparatus operates to prevent the rolling of an aircraft having an even number of propulsion units when one of the propulsion units stops operating due to a breakdown. Spoilers are mounted on the outboard wings. Each spoiler has an individual drive connected to a power circuit via a control valve which, in turn, is functionally associated with a failure detector of the propulsion unit disposed on the outboard wing opposite to that on which the respective spoiler is mounted. The apparatus is provided with an apparatus that is brought into action automatically, so as to counteract the rolling tendency of an aircraft when one of its propulsion units fails, or with a manual control for correcting the glidepath during landing, dissipating the lift and applying the aerodynamic braking during the landing roll.