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

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

Add to favorites

Compare this product

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