Use Performance Manual SEP 1 Figure 2.3 Using the climb performance chart, for the single engine aeroplane, determine the ground distance to reach a height of 2000 ft above the reference zero in the following conditions: Given: O.A.T. at take-off: 25°C Airport pressure altitude: 1000 ft Aeroplane mass: 3600 lbs Speed: 100 KIAS Wind component: 15 kts Headwind