Single-seat ULM aircraft BR-DS-503
2-stroke engineinstructionalsingle-engine

Single-seat ULM aircraft - BR-DS-503 - M-Squared Aircraft, Inc. - 2-stroke engine / instructional / single-engine

Single-seat ULM aircraft - BR-DS-503 - M-Squared Aircraft, Inc. - 2-stroke engine / instructional / single-engine - image - 2

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Characteristics

Number of seats: single-seat
Motorization: 2-stroke engine
Applications: instructional
Other characteristics: single-engine
Length: 19'00"
(5.79 m)
Height: 7'00"
(2.13 m)
Wingspan: 30'00"
(9.14 m)
Wing surface: 168 ft²
Empty weight: 405 lb
(184 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)
Take-off distance required: 425'00"
(130 m)
Landing distance required: 200'00"
(61 m)

Description

ROTAX 503 Power plant Engine with "C" Gearbox 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, Side 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 Model Rotax503 No. Cylinders Displacement 5032 CC Horsepower 54 H.P. Recommended T.B.O.300Hrs Propeller WDADJ Wing Loading 5.95 lb/ft Useful Load 595lbs Payload W/Full Fuel 499 lbs PERFORMANCE Takeoff Distance, 50 Ft