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2-person ULM aircraft B2XD-SS-912-NF2-stroke engineinstructionalsingle-engine
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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
VIDEO
*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.