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2-person ULM aircraft B2XD-DS-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
32'10"
(10.03 m)- Wing surface
180 ft²
- Empty weight
650 lb
(295 kg)- Max. take-off weight
1,320 lb
(599 kg)- Cruise speed
66 mph, 78 mph, 92 mph
(106 km/h, 126 km/h, 148 km/h)- Never exceed speed
103 mph
(166 km/h)- Take-off distance required
165'00"
(50 m)- Landing distance required
300'00"
(91 m)
Description
rotax 912 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 ana iury struts with adjustable fittings,
High lift airfoil with 14"rib spacing,
center hard-shell gap cover,
Bungee trim system
GENERAL SPECIFICATIONS
Model Rotax912UL
No. Cylinders4
Displacement82.6 CI
Horsepower80 H.P.
Recommended T.B.O.2000 Hrs
PropellerWD-ADJ
Wing Loading7.33 lb/sq
Seats2
Useful Load670 lbs
Payload w/Full Fuel574 lbs
PERFORMANCE
Takeoff Distance, 50 Ft
Obstacle 425 ft
Rate of Climb 825 fpm
Max Level Speed, Sea Level 92 mph
Landing Distance, Ground Roll 85 ft
Minimum Sink Rate 625 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.