General characteristics

• Crew: one

• Length: 17 ft 0 in (5.18 m)

• Wingspan: 23 ft 0 in (7.01 m)

• Wing area: 141.0 sq ft (13.10 m²)

• Airfoil: Clark YH

• Empty weight: 851 lb (386 kg)

• Gross weight: 1,150 lb (522 kg)

• Fuel capacity: Wing tank – 12 U.S. gallons (45 Ltrs) Fuselage tank –  10 U.S. gallons (38 Ltrs)

• Powerplant: 1 × Lycoming O-290D four cylinder, air-cooled, four stroke aircraft engine, 125 hp (93 kW) @ 2600 rpm

• Propeller: 3-blade wooden, fixed pitch by Catto

Performance

• Maximum speed: 105 kts  (194 kph; 120 mph) @ 2600 rpm

• Cruise speed: 92 kts (170 kph; 105 mph) @ 2300 rpm

• Stall speed: 48 kts (88 kph; 55 mph)

• Rate of climb: 1,400 fpm (7.1 m/s)

• Range: 400 miles (347 nm; 643 km) @2300 rpm (estimated)

• Design g limits: +/-6g operational, +/-9g ultimate (at 1000 lbs / 453 kgs AUW)

• Wing loading: 8.2 lbs/sq ft  (39.8 kg/m²)

Included Additional Equipment

• Icom A24 Transceiver

• Garmin Aera 500

• Flying cap with David Clark headset