If the aircraft weight is 162,617 with a wing surface area of 48, and it is under an equilibrium fly condition. The True airspeed is 69, the altitude is 995, please compute the coefficient of lift. Calculate the answer to 2 decimal points. **reminder: air density is 1.2 kg/m^3**

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 If the aircraft weight is 162,617 with a wing surface area of 48, and it is under an equilibrium fly condition. The True airspeed is 69, the altitude is 995, please compute the coefficient of lift. Calculate the answer to 2 decimal points. **reminder: air density is 1.2 kg/m^3**

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