DAR Solo UL – Light, strong, reliable.
The DAR Solo is a single seat, single engine ultralight airplane. The aircraft is based on mixed construction: Aluminum wings and composite airframe.
New advanced technologies have been introduced and the result is a remarkable aircraft of extra low weight and good flight performance. For the first time a Sheet Management software has been
used in aluminum sheet parts manufacturing, to eliminate the subjective factor.
All composite parts of the DAR Solo are made from carbon, aramid and fiberglass in molds under vacuum and controlled temperature. The composite technology allows integrating different parts in one. Due to this, the central beam and vertical stabilizer have been combined in one piece. The Main Landing Gear is made from fiberglass under a new 2-stage vacuuming.
Type certificate: LTF-UL
Design method: Aluminium/Composite
Engine: Polini Thor 250
Wingspan
|
9.45 m |
Overall length | 4.76 m |
Overall hight | 2.47 m |
Wing area | 9.765 m² |
Cabin width | 0.6 m |
Empty weight | 130 kg |
MTOW | 245 kg |
Max. loading | +4/-2 g |
Fuel tank capacity | 15 l |
Take-off Groundroll | 140 m |
Rate of climb | 3.6 m/s |
Cruising speed | 110 km/h |
Maximum speed | 130 km/h |
Stall speed | 50 km/h |
Fuel consumption | 6.4 l/h |
Range | 130 km |
Für alle Fragen bezüglich möglicher Optionen und Konfigurationen, Wartung, Lieferzeiten sowie Preisen, nehmen sie bitte mit uns Kontakt auf.
DAR-Flugzeuge Deutschland - Wezel Flugzeuge GmbH | Segelfliegerweg 39 | D-49324 Melle
E-Mail: Dar-Flugzeuge@gmx.de