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 ft2 CD = 0.0642 (including landing gear, flaps down, in-ground effect) VA = 260 ft/s b = 0.4 A = 6 deg