(For this question use annex 032-009 or Performance Manual MEP 1 Figure 3.1).
OAT: 24°C
Pressure Altitude: 3000 ft RWY: 12L
Wind: 080°/12 kt
Take-Off Mass: 3800 lb
Other conditions are as associated in the header of the graph.
Given the following information, what is the Take-Off Distance?
Refer to figure.
Head wind component = Wind Speed x cosine (Relative Bearing)
Head wind component = 12 x cosine (120 - 080) = 9 kt
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