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The New Piper Aircraft, Inc.
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STANDARD EQUIPPED LIST PRICE $307,000 ENGINE Manufacturer Lycoming Model IO-360-C1C6 Horsepower 200 hp Number of Cylinders 4 WEIGHTS Maximum Take-off Weight 2,750 lbs/1,247 kg Maximum Ramp Weight 2,758 lbs/1,251 kg Standard Equipped Weight 1,795 lbs/814 kg Standard Useful Load (a and b) 963 lbs/437 kg a. Standard useful load is max ramp weight minus standard equipped weight. b. Useful load is indicated for a standard equipped aircraft. DIMENSIONS Wing Span 35.4 ft/10.8 m Length 24.7 ft/7.5 m Height 7.9 ft/2.4 m Wing Area 170 ft2/15.79 m2 FUEL AND OIL CAPACITY Usable Fuel 72 gal/273 liters MAXIMUM SPEED TAS Gross Weight, Best Power Mixture 145 kts/269 km/h CRUISING SPEEDS TAS 75% Power, 7,900 ft 137 kts/254 km/h Best Power Mixture CRUISING RANGE TAS 45 min. reserves at 55% power 880 nm/1,630 km @ 9,000 ft, peak EGT mixture STALL SPEED Flaps Full Down 40° 53 kias/98 km/h 55 kcas/102 kn/h SERVICE CEILING (100fpm 16,200 ft/4,983 m TAKE-OFF DISTANCE Total over 50 ft Obstacle 1,600 ft/487 m LANDING DISTANCE Total over 50 ft Obstacle 1,520 ft/463 m
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