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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
- No engine starter
- Crank-case-pressure operated fuel pump
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 DUCATI |
| Ignition plugs |
BOSCH W 5 AC or Champion L82 C, Gap 0,5 mm. Thread M 14X1,25 mm. In combination with sparkplug-cap (23 00 701, R=5kOhm) |
| Carburetor |
Solo, metering-device WALBRO |
| Fuel pump |
BING |
| 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 |
Approx. 23,5 kg, complete with muffler, without propeller |
| Belt drive |
Ratio 1 : 1,56 |
| Operational data and limitations |
| Take-off-speed, power and Max. cont. speed, power |
22 kW at 6,500 1/min. |
| Max. rpm |
6,600 1/min. |
| Idle rpm |
Not available - no throttle control |
| Cylinder head temp. |
Max. 275°C (measured at spark plug) |
| Fuel consumption at cruise |
Approx 3.7 US gal./hr (14 l/hr.) |
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