| 摘要 |
The aircraft has a control unit which controls the aileron function of the aircraft. The control unit is provided with several drive units to adjust the landing flaps (30,40) arranged at the bearing area of the aircraft such that the aileron function of the aircraft is controlled by the operation of drive units during flight mode by the displacement of the flaps. Independent claims are included for the following: (1) method for operating aircraft; and (2) method for reducing weight of aircraft. |
