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2-person ULM aircraft B2-DS-582-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

585 lb
(265 kg)

Max. take-off weight

1,320 lb
(599 kg)

Fuel capacity

16 gal

Cruise speed

63 mph, 69 mph, 90 mph
(101 km/h, 111 km/h, 145 km/h)

Never exceed speed

105 mph
(169 km/h)

Take-off distance required

165'00"
(50 m)

Landing distance required

300'00"
(91 m)

Description

ROTAX 582 Power plant Engine with "C" Gearbox, 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 No. Cylinders2 Displacement580.5 CC Horsepower65 H.P. Recommended T.B.O.300 Hrs PropellerWD-ADJ wing Loading7.63 lb/sq Seats2 CRUISE PERFORMANCE At 65% Power (rpm/mph) 5300/63 At 75% Power (rpm/mph) 5600/69 At 100% Power (rpm/mph) 6500/90 FUEL FLOW At 65% Power (gph/mi) 4.8/210 At 75% Power (gph/mi) 5.6/197 At 100% Power (gph/mi) 7.4/195

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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.