The Learjet $31$A aircraft is powered by two Honeywell TFE $731-2$ engines.

These engines have an inlet diameter of $39\mathrm{.}4$ inches and can produce a maximum of $3500$ lbf per engine.

a maximum of $3500$ lbf per engine. Assuming that the aircraft is required to achieve

a takeoff speed of $180$ knots at sea level, is it possible to take off with these specifications?

How much thrust must each engine produce? Take into account that $1$kt $($knot$)$

Note that $1$kt $($knot$)$ is equal to $1\mathrm{.}852$ km$/$h