|Displacement||2592 cc [158.17 cu in]|
|Bore||105.6 mm [4.157 in]|
|Stroke||74 mm [2.913 in]|
|Compression Ratio||8.16 : 1|
|Firing Order||1 - 3 - 2 - 4|
|Direction of Rotation||Clockwise - seen from cockpit|
|218 Nm [160.8 ft.lbf] @ 2700 rpm|
|97 hp @ 3300 rpm / 85 hp @ 2800 rpm|
|Installed weight||72.3 kg [159.3 lbs] (including all accessories, oil and exhaust)|
|DC output||30 Amp (+/- 15 Amp available above engine/fuel pump needs)|
|Oil capacity||2.5 L [0.66 US gal]|
|Fuel|| Regular unleaded automotive gasoline with min. 95 Octane RON (87 MON = 91 AKI)
AVGAS 100LL may also be used if regular fuel is not available.
The power and torque curve of the engine has been established by repeated dyno tests, which were performed at sea level and in weather conditions close to the ISA standard. The following graph shows the real, available power and torque coming from the crankshaft of the UL260i engine corrected to the International Standard Atmosphere conditions at sea level.
The following graph shows the power the UL260i engine produces at a given manifold pressure (MAP) running at a particular rpm. When taking your MAP reading and corresponding RPM at cruising speed, the graph gives you a good idea of how much (little) power your aircraft actually needs in flight.
The following graph shows the calculated available power of the UL260i engine at different RPM settings, WOT (wide open throttle) and varying density altitude.
For more information on ISA, density altitude, interpretation of this graph, the conversion of the figures to actual atmospheric conditions, refer to the "Engine Resources" section on our website and more specifically: "ISA conditions & conversion".
|Maximum dimension in X direction (length)*||553 mm [21.77 inch]|
|Maximum dimension in Y direction (width)*||655 mm [25.75 inch]|
|Maximum dimension in Z direction (height)*||472 mm [18.6 inch]|
For more details please check the installation manual.
These are values at full throttle. When cruising estimated average is UL260 ±13l.
(depending on type of plane, personal style of flying, cruise speed , climate circumstances)
The following is a list of the ULPower engine standard design features, all included at no additional cost.
Please contact us for more info / prices
Note: Pictures may not always represent the exact colour or shape.
All prices indicated are excluding taxes and transportation costs.
Deliveries to private individuals within the European Union are subject to 21% Belgian VAT. Prices subject to change without notice.