DAR 23

DAR 23 is a double seated, single engine, high wing ultra light 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 our Sheet Management software has been used in aluminum sheet parts manufacturing. This is a new approach to design and production of sheet parts and component developed in Aeroplanes DAR. Assembling elements, like wings and tail surfaces, is easy and the subjective factor at work has been eliminated.

All composite parts in DAR Solo are made by carbon, aramid and fiberglass in molds under vacuum and controlled temperature. The composite technology allows integrating the different parts in one. Due to this the central beam and vertical stabilizer has been combined in one. The main Landing Gear is made by fiberglass under a new 2-stage vacuuming.

Type certificate / Musterzulassung: LTF-UL
Design method / Construction / Bauweise: Aluminium/Composite
Engine / Moteur / Motor: Hirth F-23

 

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	10.76 m²
Cabin width	Largeur cabine	Kabinenbreite	1.2 m
Empty weight	Masse à vide	Leermasse (inkl.Rettungssystem)	150 kg
MTOW	Masse maxi	Maximale Ablugmasse	380 kg
Max. loading	Facteurs de charge	Hochstzulassige Belastung	+4/-2 g
Fuel tank capacity	Volume réservoir	Tankinhalt	32 l
Take-off Groundroll	Distance décollage	Startrollstrecke	140 m
Rate of climb	Taux de montée	Steigrate	2.2 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	60 km/h
Fuel consumption	Consommation	Benzinverbrauch (im Reiseflug)	15 l/h
Range	Rayon d’action	Reichweite	130 km