Correct choice is (d) Cruise weight and air density
For explanation: Range factor consists of cruise weight and air density. Range factor in cruise method 1 is given by \(\left[\frac{V_{mdi}}{C} E_{max}\right]\). The range equation in cruise method 1 is given by R1=\(\left[\frac{V_{mdi}}{C} E_{max}\right]\Big\{\frac{2u^3}{u^4+1}\Big\}\) ln ω where V is true airspeed, C is specific fuel consumption, L is lift, D is drag, Emax is endurance, u is relative airspeed and ω is fuel ratio.