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SOLO Aircraft Engine 2350 C


Description of construction
- In-line-two-cylinder-two-stroke engine
- Air-cooling
- mixture control
- two diaphragm carburetors with additional fuel pump
- CDI ignition
- Propeller mounted on belt drive
- Electric engine starter 12 V, 400 W

Download of technical drawing as pdf-file here.

Technical data
Engine Displacement 430 ccm, cyl. bore 70 mm, stroke 56 mm
Compression rartio 12 : 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 MIKUNI BN 38
Direction of rotation Counterclockwise, seen in direction of flight
Starter Fa. SJCE Tyep: 101
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. 25 kg
Belt drive Ratio 1:2,3


Operational data and limitations
Take-off-speed, power 22 kW (30 HP) at 6,500 1/min.
Max. cont. speed, power 20 kW (27 HP) at 6,100 1/min.
Recommended rpm 6,500 1/min.
Idle rpm 3,000 1/min.
Cylinder head temp. Max. 275°C
Fuel consumption 100% cont. speed approx 3.96 US gal./hr. (15.0 l/hr.)
75% cont. speed approx. 3.7 US gal./hr. (14.0 l/hr.)