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Description of construction
- In-line-two-cylinder-two-stroke engine
- Air-cooling
- mixture control via
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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. |
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