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2-person ULM aircraft B2XD-SS-912-NF
2-stroke engineinstructionalsingle-engine

2-person ULM aircraft
2-person ULM aircraft
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Characteristics

Number of seats
2-person
Motorization
2-stroke engine
Applications
instructional
Other characteristics
single-engine
Length

19'00"
(5.79 m)

Height

7'00"
(2.13 m)

Wingspan

31'00"
(9.45 m)

Wing surface

173 ft²

Empty weight

645 lb
(293 kg)

Max. take-off weight

1,320 lb
(599 kg)

Fuel capacity

16 gal

Cruise speed

58 mph, 65 mph, 74 mph
(93 km/h, 105 km/h, 119 km/h)

Never exceed speed

89 mph
(143 km/h)

Take-off distance required

165'00"
(50 m)

Landing distance required

300'00"
(91 m)

Description

STANDARD EQUIPMENT (included) rotax 912ul 80 H.P. Power plant Engine, warp drive propeller, EIS Engine Information System, 8:00x6 Main gear tires with aluminum wheels and Hydraulic brakes, 13" Nose gear with aluminum wheel, Center mounted controls with brake handle, Large lord mounted anti-vibration engine mount, Steel pilot roll cage. Aerodynamic lift and iury struts with adjustable fittings, High lift airfoil with 14"rib spacing, Center hard-shell gap cover, Bungee trim system GENERAL SPECIFICATIONS Model Rotax912 UL No. Cylinders4 Displacement82.6 CI Horsepower80 H.P. Recommended T.B.O.2000 Hrs PropellerWD-ADJ Wing Loading7.33 lb/ft Payload W/Full Fuel 579 lbs performance Takeoff Distance, 50 Ft Obstacle 425 ft Rate of Climb 825 fpm Max Level Speed, Sea Level 74 mph Landing Distance, Ground Roll 85 ft Minimum Sink Rate 725 fpm Glide Ratio 5.95 to 1

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*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.