DAR Solo

DAR Solo is a single seat, 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.

Originally, DAR Solo has been designed to be sold as an airplane kit. That`s why airfoil and assembly have been specially chosen and modified to be easily handled with by customers, specially trained in sphere of engineering and can be assembled in a regular workshop (table). In fact, the customer receives all-important parts ready for final assembly. These important features are required for a product that will be sold as kit set, intended for private manual assembly.

DAR Solo UL

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.

Type certificate: LTF UL
Design method: Aluminium/Composite
Engine: Polini Thor 250

Span	31. ft	9.45 m
Overall length	15.6 ft	4.76 m
Overall high	8 ft	2.47 m
Wing area	105 ft²	9.765 m²
Cabin width	2 ft	0.6 m
Empty weight (incl. BRS)	267 lb	120 kg
Empty weight	254 lb	114 kg
Max. take-off weight	540 lb	245 kg
Max. loading	+4/-2 g	+4/-2 g
Fuel tank capacity	3.3 gal.	15 l
Take-off Groundroll	459 ft	140 m
Rate of climb	394 fpm	2.0 m/s
Cruising speed	50 kts	90 km/h
Maximum speed	57 kts	105 km/h
Stall speed	27 kts	50 km/h
Stall speed flaps max	24 kts	45 km/h
Fuel consumption (cruise)	1.7 gal./h	6.5 l/h

DAR Solo 120

DAR Solo 120 is lighter version, which meet German 120 kg rules. This aircraft also meet other regulations as Russian 115, Korean, Brazilian and other. Powered by Polini THOR 200 EVO (28HP). Two blade wooden prop, rescue system GRS 240.

Musterzulassung / Type certificate: LTF-L
Bauweise / Design method: Aluminium/Composite
Motor / Engine - Polini Thor 200 / 250

Spannweite	9.45 m	Span	31. ft
Lange	4.76 m	Overall length	15.6 ft
Hohe	2.47 m	Overall high	8 ft
Flugelflache	9.765 m²	Wing area	105 ft²
Kabinenbreite width	0.6 m	Cabin	2 ft
Leermasse (inkl. Rettungssystem)	120 kg	Empty weight (incl. BRS)	267 lb
Maximale Ablugmasse	245 kg	Max. take-off weight	540 lb
Hochstzulassige Belastung	+4/-2 g	Max. loading	+4/-2 g
Tankinhalt	15 l	fuel tank capacity	3.3 gal.
Startrollstrecke	140 m	Take-off Groundroll	459 ft
Steigrate	3.6 m/s	Rate of climb	709 fpm
Reisegeschwindigkeit	110 km/h	Cruising speed	60 kts
Hochstzulassige Geschwindigkeit	130 km/h	Maximum speed	70 kts
Uberziehgeschwindigkeit	50 km/h	Stall speed	27 kts
Benzinverbrauch (im Reiseflug)	6.4 l/h	Fuel consumption (cruise)	1.69 gal./h
Reichweite	130 km	Range	70 nm