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DAR Solo
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

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

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