I ended up redoing some of it. I calculated R = 284,272N, then used a(centripetal) = v^2/K, => a = 0.35 m/s^2.
I then used F(centripetal) = ma(centripetal), = 10,408N.
Then I done R - F(centripetal) to calculate lift. I got the answer on the sheet, but is that the correct process?
I also...