|
Typical Installation weights for Rotax 4
stroke aircraft engines
|
|
912UL
|
912 ULS
|
914UL |
|
KW/HP |
60.4 |
81.0 |
73.5 |
100. |
85.7 |
115.0 |
|
Items |
Kg. |
Lbs. |
Kg. |
Lbs. |
Kg. |
Lbs. |
|
Engine with carbs |
55.0 |
121.2 |
56.6 |
124.7 |
64.0 |
141.1 |
|
Exhaust system |
4.0 |
8.8 |
4.0 |
8.8 |
4.0 |
8.8 |
| Airbox |
- |
- |
1.3 |
2.9 |
- |
- |
|
Air filter(s) |
0.3 |
0.7 |
0.3 |
0.7 |
0.2 |
0.4 |
|
Radiator |
1.0 |
2.2 |
1.0 |
2.2 |
1.0 |
2.2 |
|
Oil Radiator |
0.5 |
1.1 |
0.5 |
1.1 |
0.5 |
1.1 |
| Engine truss assembly |
- |
- |
- |
- |
2.0 |
4.4 |
| Rectifier / regulator |
0.1 |
0.2 |
0.1 |
0.2 |
0.1 |
0.2 |
| Electric fuel pumps |
- |
- |
- |
- |
0.7 |
1.5 |
|
External alternator |
- |
- |
- |
- |
3.0 |
6.6 |
| |
|
|
|
|
|
|
| Installed weight |
60.9 |
134.2 |
63.8 |
140.6 |
75.5 |
166.4 |
|
Weight to power |
1.008 |
1.657 |
0.868 |
1.406 |
0.881 |
1.447 |
| |
Kg/KW |
Lbs/HP |
Kg/KW |
Lbs/HP |
Kg/KW |
Lbs/HP |
|
Specifications and performance data shown is
typical for the engines described and is general in nature. All
information is subject to change without notice. Information shown
is not to be used for flight or flight planning purposes. Consult
the appropriate engine and/or aircraft manual(s) for specific technical
information. |
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| 
