Airmaster 3-blade variable pitch propellers and their control unit
ROTAX ® 914 UL DCDI Turbo Charged engine
DESCRIPTION
DESCRIPTION• 4-cylinder
• 4-stroke liquid/air-cooled engine with opposed cylinders
• with turbo charger
• with automatic waste gate control
• dry sump forced lubrication with separate oil tank
• automatic adjustment by hydraulic valve tappet
• 2 carburetors
• dual electronic ignition
• electric starter
• propeller speed reduction unit
• engine mount assembly
• air intake system
• exhaust system
FACTS
The turbo charged Rotax 914 series offers more performance at high altitudes while keeping weight at a low level. This series offers a time between overhauls of 2.000 hrs and is available as certified (Rotax 914 F) according to FAR 33 and JAR-E and non-certified version (Rotax 914 UL).
|
VERSION |
PERFORMANCE |
TORQUE |
MAX RPM |
||||
|
914 ULS1)/S2) |
kW |
ft. lb. |
1/min |
Nm |
ft. lb. |
1/min |
1/min |
Limited for max. 5 min.
|
BORE |
STROKE |
DISPLACEMENT |
FUEL |
|||
|
79.5 mm |
3.31 in |
61 mm |
2.4 in |
1211.2 cm3 |
73.91 cu. in. |
min. MON 85 RON 95* |
* leaded, unleaded, AVGAS 100LL or Ethanol 10
1) ULS = non certified | 2) S = certified acc. to FAR 33
| WEIGHT |
kg |
lb |
| engine with propeller speed reduction unit i = 2.43 |
64.0 |
140.8 |
| exhaust system |
4.0 |
8.8 |
| engine suspension frame |
2.0 |
3.7 |
| overload clutch |
1.7 |
3.7 |
| external alternator |
3.0 |
6.6 |
| air guide hood |
0.8 |
1.8 |
