AIRCRAFT ITEM INFORMATION
Engine Lycoming IO-360-M1A
Horsepower 180 hp
Propeller Hartzell 2-blade scimitar structural composite propeller
Airworthiness category Normal and utility
Length 26 ft 5 in
Height 6 ft 6 in
Wing Span 39 ft 6 in
Maximum takeoff weight 2,645 lbs
Useful load 860 lbs (standard equipped airplane)
Fuel capacity, usable 50 gal
Fuel AVGAS 100 LL
Takeoff distance, ground roll 1,175 ft
Takeoff distance, 50-foot obstacle 1,700 ft
Landing distance, ground roll 1,155 ft
Landing distance, 50-foot obstacle 2,093 ft
Rate of climb, sea level 1,120 ft/min
Maximum operating altitude 16,400 ft
Maximum speed 157 ktas
Cruise speed at 75% 150 ktas/10 gal/hr
Stall speed, full flaps 49 kias
Maximum demonstrated crosswind 20 kts
Range, at 75% 45 minute reserve 720 nm
Range, at 55% 45 minute reserve 785 nm