An F$-16$ generating $30,000$ lbs of lift has a dynamic pressure of $134$ lb$/$ft$^2.$ The zero$-$lift drag coefficient for the F$-16$ is $0\mathrm{.}019$ and it has a k of $0\mathrm{.}117.$ With a wing area of $300$ft$^2,$ what is the drag on this aircraft?