A fully loaded Boeing $737-800$ weighs $70,000kg$ and can have a very large lift coefficient when its flaps are fully deployed. If the plane is capable of cruising at $160$ mph with its flaps fully deployed, has a wing area of $125m^2,$ and an average cord length of $3\mathrm{.}37$ m determine the lift coefficient and Reynolds number for this plane in this configuration. $C_l=[1\mathrm{.}5-1\mathrm{.}9]$ and $Re=[1\mathrm{.}0{10}^7-1\mathrm{.}0{10}^8]$