AMC 25.147(f) Lateral control: All engines operating

• ED Decision 2003/2/RM found in: CS-25 Amdt 27 - Large Aeroplanes (Jan 2023)

AMC 25.147(f) Lateral control: All engines operating ED Decision 2003/2/RM An acceptable method of demonstrating that roll response and peak roll rates are adequate for compliance with [CS 25.147(f)](#_DxCrossRefBm1709820699) is as follows: It should be possible in the conditions specified below to roll the aeroplane from a steady 30° banked turn through an angle of 60° so as to reverse the direction of the turn in not more than 7 seconds. In these demonstrations the rudder may be used to the extent necessary to minimise sideslip. The demonstrations should be made rolling the aeroplane in either direction, and the manoeuvres may be unchecked. Conditions: (a) En-route: Airspeed. All speeds between the minimum value of the scheduled all-engines-operating climb speed and VMO/MMO. Wing-flaps. En-route position(s). Air Brakes. All permitted settings from Retracted to Extended. Landing Gear. Retracted. Power. All engines operating at all powers from flight idle up to maximum continuous power. Trim. The aeroplane should be in trim from straight flight in these conditions, and the trimming controls should not be moved during the manoeuvre. (b) Approach: Airspeed. Either the speed maintained down to the 15 m (50 ft) height in compliance with [CS 25.125(a)(2)](#_DxCrossRefBm1709820685), or the target threshold speed determined in accordance with [CS 25.125(c)(2)(i)](#_DxCrossRefBm1709820685) as appropriate to the method of landing distance determination used. Wing-flaps. In each landing position. Air Brakes. In the maximum permitted extended setting. Landing Gear. Extended. Power. All engines operating at the power required to give a gradient of descent of 5·0%. Trim. The aeroplane should be in trim for straight flight in these conditions, and the trimming controls should not be moved during the manoeuvre.