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2-person ULM aircraft B2XD-SS-912-WF2-stroke engineinstructionalsingle-engine
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Characteristics
- Number of seats
- 2-person
- Motorization
- 2-stroke engine
- Applications
- instructional
- Other characteristics
- single-engine, amphibious
- Length
19'00"
(5.79 m)- Height
7'00"
(2.13 m)- Wingspan
32'10"
(10.03 m)- Wing surface
180 ft²
- Empty weight
755 lb
(342 kg)- Max. take-off weight
1,430 lb
(649 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 912ULS 100 H.P. Power plant Engine,
warp drive propeller,
EIS Engine information System,
Center mounted controls,
Large lord mounted anti-vibration engine mount,
Stainless 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,
Full Lotus 1450 Floats std. (Other manuf. call for quote)
GENERAL SPECIFICATIONS
Model Rotax912 ULS
No. Cylinders2
Displacement82.6 CI
Horsepower100 H.P.
Recommended T.B.O.2000 Hrs
PropellerWD-ADJ
Wing Loading7.94 lb/sq
Seats2
Useful Load675 lbs
Payload W/Full Fuel579 lbs
PERFORMANCE
Takeoff Distance, 50 Ft
Obstacle 425 ft Rate of Climb 625 fpm
Max Level Speed, Sea Level 74 mph
Landing Distance, Ground Roll 85 ft
Minimum Sink Rate 745 fpm
Glide Ratio 5.95 to 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.