Consider the example for a Boeing 767-200 discussed in class, with a lower weight (due to burning fuel). The aircraft is on approach to land. Assume standard sea-level conditions:
W = 300,000 lbs
S = 3,084 ft
Cd= 0.0642 (including landing gear, flaps down, in-ground effect)
Va = 260 ft/s
μb = 0.4 A
Ya= 6 deg
Calculate the total landing distance required, including the approach, flare, and ground roll segments. Assume Cᵢ.F /Cᵢ.ₐFCL 1.2 and on ground roll Cl=0.9.