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SOLO Aircraft Engine 2350 B



Description of construction
- In-line-two-cylinder-two-stroke engine
- Air-cooling
- mixture control via
- two diaphragm carburetors
- CDI ignition
- Propeller mounted on belt drive
- Electric starter
- AC generator

Download of technical drawing as pdf-file here.

Technical Data
Engine Displacement 430 ccm, cyl. bore 70 mm, stroke 56 mm
Compression rartio 10 : 1
Ignition unit Magneto SOLO, ignition coil BOSCH or PVL
Ignition plugs BOSCH W 5 AC heat range 225 or Champion L82 C, Gap 0,5 mm
Carburetor WALBRO
Direction of rotation Counterclockwise, seen in direction of flight
Starter Fa. SJCE Tyep: 102 or UNITED TECHNOLOGIES Tyep: 1077-28-Mo 30 sM
Fuel 2-Stroke mix, AVGAS 100LL, premium gas (min. 95 ROZ)
Mixture Mixture ratio 1 : 40 , 2-stroke Castrol mineral oil or synthetic oil, or other oils with specification according to JASO FC oder FD
Dry Weight Appropx. 26 kg
Belt drive Ratio 1:2,1


Operational data and limitations
Take-off-speed, power and Max. cont. speed, power 17 kW (23 HP) at 6,300 1/min.
Max. rpm 6,500 1/min.
Recommended rpm 5,500 1/min.
Idle rpm 2,000 1/min.
Cylinder head temp. Max. 275°C
Fuel consumption Max. speed approx. 2.25 US gal./hr. (8.5 l/hr.)
Cruising speed approx. 2.03 US gal./hr. (7.7 l/hr.) at 5,500 1/min.