Thrust Setting At Takeoff | Airbus A320

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On all jet engines, but particularly on high bypass ratio engines, the engine acceleration profile is not linear. It follows the engine control law that is defined to optimize the acceleration in a way that the risk of engine stall is reduced because of this the aircraft engines accelerate asymmetrically at takeoff when moved directly to takeoff thrust from idle. To overcome this Airbus recommends 2-step thrust application procedure for takeoff, in which the flight crews must wait for all engines to reach the stabilization step before advancing the thrust levers to takeoff thrust.

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