|Displacement||3503 cc [213.77 cu in]|
|Bore||105.6 mm [4.157 in]|
|Stroke||100 mm [3.937 in]|
|Compression Ratio||8.7 : 1|
|Firing Order||1 - 3 - 2 - 4|
|Direction of Rotation||Clockwise - seen from cockpit|
|320 Nm [236 ft.lb] @ 2400 rpm|
|130 hp @ 3300 rpm / 123 hp @ 2800 rpm|
|Installed weight||78.4 kg [172.8 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||Unleaded automotive gasoline with min. 97 oct. RON (89 MON = 93 AKI).
AVGAS 100LL or AVGAS UL91 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 UL350iS engine corrected to the International Standard Atmosphere conditions at sea level.
The following graph shows the calculated available power of the UL350iS engine at different RPM settings, WOT (wide open throttle) and varying density altitude.
|Maximum dimension in X direction (length)*||553.0 mm [21.7 inch]|
|Maximum dimension in Y direction (width)*||735.6 mm [28.96 inch]|
|Maximum dimension in Z direction (height)*||472 mm [18.6 inch]|
For more details please check the technical data document.
These are values at full throttle. When cruising estimated average is UL350 ±18l.
(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.