Variable pitch propellor, retractable undercarriage
Lycoming IO-540-C4 D5D, 6 cylinder, fuel injected, 250 HP
Full IFR (certified BRNAV) including: Flight Director, coupled HSI, Garmin GNS 430, KNS 80, RMI
Two axis Autopilot, with height hold and coupled to HSI
Shadin Fuel Flow computer coupled to GPS
Empty weight 1872 lbs
Max takeoff weight 2943 lbs
Total payload 1071 lbs
Payload with full fuel 535 lbs
Cruise speed: 155 Kts
Fuel capacity 330 litres
Fuel consumption: 60 litres per hour
Endurance: 5 hours 30 minutes without reserves
Still air range: 850 miles without reserves