Method assistance takeoff of aircraft.

- According to the invention, is arbitrarily chosen VRref a reference value in the range of possible rotational speeds, is deflected at least the adjustable horizontal stabilizer according to the centering for this value VRref is determined the gap between this reference value and the VC value of the speed of the aircraft in the acceleration phase and is, prior to rotation, on the elevators and / or the adjustable horizontal tailplane of the aircraft (1) for holding account said deviation.