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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.) |
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