A330 L/D & SFC

[HazelNuts39]

The Breguet Range paramater: K=(Vcruise/SFC)*(L/D)/g

may be written as: K = (V/F)*(W/g), where -
V/F = specific air range in NM/kg of fuel
W/g = mass of the airplane in kg

so for the example I gave:

K = 80*200 = 16.000 NM