105 - ATPL - The determination of the maximum mass on brake release, of a certified turbojet aeroplane with 5°, 15° and 25° flap angles on take-off, leads to the following values: Flap angle: 5° 15° 25°; Runway limitation (kg): 66000 69500 71500; 2nd segment climb limitation: 72200 69000 61800; Wind correction: Headwind: +120 kg / KT Tailwind: -360 kg / KT; Given that the tailwind component is equal to 5 KT, the maximum mass on brake release and corresponding flap angle will be:

Question 105 - Performance - ATPL - Airline Transport Pilot license