Single-seat ULM aircraft BR-SS-HKS

2-stroke engineinstructionalsingle-engine

STANDARD EQUIPMENT (included) HKS 700 Powerplant Engine, warp drive propeller, EIS - Engine information system, 15" Main gear tires with aluminum wheels and Hydraulic brakes, 13" Nose gear with aluminum wheel, Steel main wheel axle stubs, Center mounted controls with brake handle, Large lord mounted anti-vibration engine mount, Steel pilot roll cage and nose struts, Aerodynamic lift ana jury struts with adjustable fittings, High lift airfoil with 14" rib spacing, Center hard-shell gap cover, 16 Gal wing Mounted Fuel Cells, Bungee trim system GENERAL SPECIFICATIONS MModelHKS 700 No. Cylinders2 Displacement580 CC Horsepower58.5 H.P. Recommended T.B.O.1000 Hrs PropellerPF ADJ Length19 ft Height7 ft 10 in Wi ngspan30 ft 9 in Wing Area168 sq. ft Wing Loading5.95 lb/ft Seats1 Empty weight425 lbs Useful Load575 lbs Payload W/Full Fuel479 lbs Max Take-off Weight1000 lbs Fuel Capacity (Standard)16 gal PERFORMANCE Takeoff Distance, Ground Roll 125 ft Takeoff Distance, 50 Ft Obstacle 425 ft Rate of Climb 825 fpm Max Level Speed, Sea Level 67 mph Landing Distance, 50 Ft Obstacle 200 ft Landing Distance, Ground Roll 55 ft Minimum sink Rate 475 fpm Glide Ratio 5.95 : 1