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

single-seat ULM aircraft
single-seat ULM aircraft
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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

51 mph, 60 mph, 67 mph
(82 km/h, 97 km/h, 108 km/h)

Never exceed speed

81 mph
(130 km/h)

Take-off distance required

425'00"
(130 m)

Landing distance required

300'00"
(91 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 Ceils, GENERAL SPECIFICATIONS Model Rotax 503 No. Cylinders 2 Displacement 503 CC Horsepower 54 H.P. Recommended T.B.O.300 Hrs Propeller WD ADJ Wing Loading5.95 lb/ft Seats1 Useful Load 595 lbs Payload W/Full Fuel 499 lbs PERFORMANCE Takeoff Distance, 50 Ft Obstacle 425 ft Rate of Climb 625 fpm Max Level Speed, Sea Level 67 mph Landing Distance, Ground Roll 75 ft Minimum sink Rate 575 fpm Glide Ratio 5.75 : 1
*Prices are pre-tax. They exclude delivery charges and customs duties and do not include additional charges for installation or activation options. Prices are indicative only and may vary by country, with changes to the cost of raw materials and exchange rates.