Ultralight airplanes for aviation fanciers

DAR Solo 120 – The Lightweight

 

Type certificate / Musterzulassung: LTF-L

Design method / Construction / Bauweise: Aluminium/Composite

Engine / Moteur / Motor: Polini Thor 250

 

Span Envergure Spannweite 9.45 m
Overall length Longueur Lange

4.76 m
Overall high Hauteur Hohe

2.47 m
Wing area Surface alaire

Flugelflache 9.765 m²
Cabin width Largeur cabine

Kabinenbreite 0.6 m
Empty weight Masse à vide Leermasse
(inkl.Rettungssystem)
120 kg
MTOW Masse maxi Maximale Ablugmasse 245 kg
Max. loading Facteurs de charge Hochstzulassige
Belastung
+4/-2 g
Fuel
tank capacity
Volume réservoir

Tankinhalt 15 l
Take-off Groundroll Distance décollage Startrollstrecke 140 m
Rate of climb Taux de montée

Steigrate 3.6 m/s
Cruising speed Vitesse de croisière Reisegeschwindigkeit 110 km/h
Maximum speed Vitesse maxi Hochstzulassige
Geschwindigkeit
130 km/h
Stall speed Vitesse décrochage Uberziehgeschwindigkeit 50 km/h
Fuel consumption Consommation Benzinverbrauch (im
Reiseflug)
6.4 l/h
Range Rayon
d’action

Reichweite 130 km

 
 
 

DAR Solo 120 ultralight airplane

 
 

DAR Solo 120 is a light weight version of DAR Solo UL. Visually no difference between both models.
DAR Solo cover the German LTF-L rules. The empty weight is 120 kg.
The biggest differences are:

1. All cockpit composites parts, are made from 100% carbon fiber, racing manner (no gelcoats) under vacuum in thermal chamber. The lightweight parts are: front nose fairing, instrument panel and backseat.

2. Fuel tank is 14 liter alum welded.

3. Wing is shorter (with 250 mm half wing span is shorter), additionally composite winglet is replaced by alum sheet winglet (lightweight)

4. No flaps (Flaps mechanism is removed)

5. Wheels are 4 inch lightweight tubeless.

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