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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
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. |
| Engine Displacement | 430 ccm, cyl. bore 70 mm, stroke 56 mm |
| Compression Ratio | 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 |
| 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 | 26 kg |
| Starter | Fa. SJCE Tyep: 102 or UNITED TECHNOLOGIES Tyep: 1077-28-Mo 30 sM |
| Belt Drive | Ratio 1:2,1 |
TM 4603-9
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a) Introduction of a nut with flange at the excentric axle. b) Intoduction of a lifetime limit of 15 years of operation for the ball bearings at the bearing block of the reduction gear.
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