Dar Solo

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Dar Solo
Motor glider
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STOL
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Personal helicopter
FAR 103
Canard
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Experimental
Low wing
Mid wing
High wing
Canard
Parasol wing
Gull wing
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Composite
Electric
Nose wheel
Tail wheel
Open cockpit
Retractable gear
Pusher
V-tail
Twin engine
Single place
Small plane
Aerobatic
Amphibious
Autogyro
Classic
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FAR 103
Helicopter
Homebuilt
Jet
Kit
Light sport
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Paraglider
Paramotor
Paratrike
Powered parachute
Prototype
Replica
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STOL
Trike
TMG
Ultralight helicopter
Warbird
Pilotmix Aircraft database DAR Solo
Motor glider
Biplane
STOL
Gyrocopter
Seaplane
Personal helicopter
FAR 103
Canard
Amphibian
Experimental
Low wing
Mid wing
High wing
Canard
Parasol wing
Gull wing
Biplane
Triplane
Composite
Electric
Nose wheel
Tail wheel
Open cockpit
Retractable gear
Pusher
V-tail
Twin engine
Single place
Small plane
Aerobatic
Amphibious
Autogyro
Classic
Concept
Flying car
General aviation
Glider
Experimental
FAR 103
Helicopter
Homebuilt
Jet
Kit
Light sport
Motor glider
Paraglider
Paramotor
Paratrike
Powered parachute
Prototype
Replica
Rotorcraft
STOL
Trike
TMG
Ultralight helicopter
Warbird
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The Solo by Aeroplanes DAR is a single seat, single engine ultralight aircraft. The Solo was designed to meet the FAR 103 and the European 120kg class rules.
DAR Solo is based on a mixed construction, composite fuselage with metal wings.
Customers can choose between 3 types of wings, 3 types of engines, and 4 types of wheels.
There are two technologies used in the DAR Solo construction:
Metal construction Wings are built by conventional sheet metal working practice. Wing construction uses two spars,12 ribs and metal skin. All parts are cut and bent on CNC equipment. Wing assembly is designed to be simple and straightforward.
Composites The rest of the airframe is a composite construction. Parts are made from carbon and glass fiber in temperature controlled vacuum molds. The molding process minimizes the weight of Epoxy resin required in construction, and results in lightweight but very strong parts. Sandwich construction techniques are also used to minimize weight and maximize strength. All airframe composite parts in the kit are completely finished, ready for final assembly.
Engine options: Hirth F-33 28HP, Hirth F-23 50HP twin cylinder boxer, Hirth F200
Instruments: The instruments are minimal, Airspeed, Vertical Speed, Altitude and Compass. The engine monitoring is a specially developed Aeroplanes DAR Solo unit. Options:
Enclosed cabin Wheel fairings Engine Floats Trailer Color Hydraulic brakes Wheels
For more information contact Aeroplanes DAR Ltd.
Official site of Aeroplanes DAR ltd
Home About DAR Solo
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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.
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.
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DAR Solo 120 is a light weight version of DAR Solo UL. Visually there are no differences between both models and the structure of the airframe is similar
DAR Solo 120 covers the German LTF - UL rules as well as the LTF-L rules. With an empty weight of 120 kg the aircraft can be either registered as a normal
german Ultralight or in the 120 kg category, where the pilot doesn`t need a medical.
Here are the biggest differences from the DAR Solo ( normal Ultralight version ) to the DAR Solo 120 ( 120 kg category ) :
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
Wingspan
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