Single-seat ULM aircraft BR-DS-HKS
2-stroke engineinstructionalsingle-engine

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Go to the M-Squared Aircraft, Inc. website for more information

Characteristics

Number of seats: single-seat
Motorization: 2-stroke engine
Applications: instructional
Other characteristics: single-engine
Length: 17'00"
(5.18 m)
Height: 7'00"
(2.13 m)
Wingspan: 30'00"
(9.14 m)
Wing surface: 168 ft²
Empty weight: 425 lb
(193 kg)
Max. take-off weight: 1,000 lb
(454 kg)
Fuel capacity: 16 gal
Cruise speed: 57 mph, 63 mph, 77 mph
(92 km/h, 101 km/h, 124 km/h)
Never exceed speed: 93 mph
(150 km/h)
Take-off distance required: 425'00"
(130 m)
Landing distance required: 200'00"
(61 m)

Description

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 and jury struts with adjustable fittings, High lift airfoil with 14" rib spacing, Center hard-shell gap cover, 16 Gal Wing Mounted Fuel Cells, GENERAL SPECIFICATIONS ModelHKS700 No. Cylinders2 Displacement580 CC Horsepower58.5 H.P. Recommended T.B.O.1000Hrs PropellerPFADJ wing Loading5.95 lb/ft Seats1 useful Load575lbs Payload W/Full Fuel479lbs PERFORMANCE Rate of Climb 825 fpm Max Level Speed, sea Level 77 mph Landing Distance, 50 Ft Ground Roll 55 ft Glide Ratio 5.95 : 1 Minimum sink Rate 475 fpm

Go to the M-Squared Aircraft, Inc. website for more information