Dimensions
Wing Span 32 feet
Length, 19.3 feet
Height 9.5 feet
Fuselage Width 48 inches
Fixed Landing Gear Wheelbase 6 feet
Power Plant
Type four-stroke-cycle
Designation ROTAX-912ULS
Maximum power, kW(hp)/rpm 73.5 (99) / 5800
Cruise (hp/rpm) 51 / 5000
Fuel specification 93 octane Premium Auto Fuel or 100LL
Fuel tanks capacity 17 Gallons
Equipment Fixed Pitch Propeller
Aircraft instrumentation
• Speed indicator US-250
• Altitude indicator VD-10
• Altitude-rate indicator VR-10
• Sideslip indicator (ball)
• Fuel indicator
Radio equipment
• Optional
Electrical equipment
• Storage battery 27Ah 12 V
• Rectifier regulator
• Switches, automatic circuit-breaker
Aircraft performance characteristics
Maximum takeoff weight 1320 lbs
Empty weight 750 lbs
Fuel 105 lbs
Payload 570 lbs
Center-of-gravity of airplane with equipment, percent of MAC 32…30
Extreme forward center-of-gravity, percent of MAC 22
Extreme aft center-of-gravity, percent of MAC 34
Stalling speed, MPH
- landing configuration 47 MPH
- takeoff configuration 49 MPH
- cruise configuration 52 MPH
Speed, MPH
- takeoff speed 49 MPH
- climbing speed 75 MPH
- cruising speed 105 MPH
- maximum horizontal flight speed 130 MPH
- maximum limit speed 149 MPHlanding approach speed 65 MPH
- maximum speed in takeoff configuration 93 MPH
- maximum speed in landing configuration 81 MPH
Takeoff run 328 feet
Takeoff distance (over 50 foot obstacle) 754 feet
Landing distance 328 feet
Landing distance (over 59 foot obstacle)1312 feet
Maximum range ability 435 Miles
Maximum flight duration, h 5.5
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