Cessna 172R.htm
by Nicholas
http://www.enter.net/~kellys00/info.html http://en.wikipedia.org/wiki/Cessna_172#Specifications_.28172R.29 Maximum lift coefficient 1.60 (no flaps) Maximum lift coefficient 2.10 (with flaps) Frontal Area: 3.3m^2 Gross weight: 2,450 lb (1,111 kg) Engine: 160 hp (120 kW) @ 2,400 rpm Cruise speed: 122 kn (140 mph; 226 km/h) Stall speed: 47 kn (54 mph; 87 km/h) (power off, flaps down) Wing area: 174 sq ft (16.2 m2) Airfoil: modified NACA 2412 Takeoff Roll - 945 ft. Cabin Width - 39.5 in. Cabin Height - 48 in. Coefficient of Drag: 0.027 http://www.avweb.com/news/airman/182410-1.html speed (knots), drag(lbs) 30, 520 40, 510 50, 490 60, 475 70, 460 80, 435 90, 410 100, 380 110, 350 120, 315 speed (knots), drag (lbs) 30, 665 40, 400 50, 280 60, 240 70, 225 80, 235 90, 250 100, 275 110, 315 120, 360

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