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Single-seat ULM aircraft Solo UL2-stroke enginesportsingle-engine
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Characteristics
- Number of seats
- single-seat
- Motorization
- 2-stroke engine
- Applications
- sport
- Other characteristics
- single-engine, kit
- Length
4.8 m
(15'08" )- Height
2.5 m
(8'02" )- Wing surface
9.8 m²
(105.5 ft²)- Max. take-off weight
245 kg
(540 lb)- Fuel consumption
6.5 l/h
(1.7 us gal/h)- Range
130 km
(81 mi)- Maximum speed
105 km/h
(65 mph)- Cruise speed
90 km/h
(56 mph)- Stall speed
50 km/h
(31 mph)- Rate of climb
2 m/s
(7 ft/s)- Take-off distance required
140 m
(459'03" )
Description
DAR Solo UL is a typical ultralight airplane with MTOW 260 kg. Powered by Polini THOR 250 DS (36.5HP). Two blade wooden prop, rescue system GRS 260.
Catalogs
DAR Solo UL
2 Pages
*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.