The engines feature FADEC (full authority digital engine control) with multi-point electronic fuel injection, and dual electronic ignition (with variable timing), excellent power-to-weight ratio, and high fuel efficiency in a conventional configuration: Air-cooled, direct drive, horizontally opposed four-cylinder.
UL Power Engines have been developed specifically for use in light aircraft and are manufactured with fully electronic ignition and multi-point fuel injection (FADEC) system as standard equipment.
- Four-stroke, air cooled, four-cylinder opposed engine
- Dual (redundant) electronic spark ignition (variable timing)
- Multi-point electronic fuel injection with automatic altitude and temperature compensation
- Electronic RPM limiter
- Direct propeller drive
- Wet sump forced lubrication with integrated pressure regulator
- 5 bearing crankshaft with thrust ball bearing
- Ram air cooled cylinders and cylinder heads
- Electric fuel pump and pressure regulator to eliminate vapor lock and facilitate starting even under adverse conditions.
UL Power engines are manufactured in Europe.
The UL260iF is specially dedicated to the French market. The engine is based on the UL260iS and specially adapted to be compliant with the French ULM (ultralight) regulations.
On 7 October 2013 the first Europa (G-BWUP) to be fitted with a UL Power UL260iS 107 Hp engine flew for the first time from a Private strip in Wiltshire, UK. With the test pilot going up for a 30 min first flight and no real probs reported apart from the Constant speed prop needed adjusting. The second flight was a little shorter but the Prop was working well now and the take off roll with one up and half fuel and nil wind was only 220 meters.
UL260i
Configuration: Flat-4, direct propeller drive, air-cooled
Max Power: 72 kW / 97 hp @ 3300 rpm / 82 hp @ 2800 rpm
Capacity: 2592 / 158 cc / cu.in
Bore: 105.6 mm / 4.157 in
Stroke: 74 mm / 2.913 in
Max Torque: 207Nm
Weight: 72.3 kg/ 159.3 lb
Compression Ratio: 8.16:1
Fuel: min 95 OCT / 87 MON
Cylinders: 4
Firing Order: 1 – 3 – 2 – 4
Oil capacity: 2.5 lt / 0.66 US gal
Direction of Rotation: Clockwise – seen from cockpit
DC output: 30 Amp (+/- 15 Amp available above engine/fuel pump needs)
TBO: 1500h / 10y
UL260iS
Configuration: Flat-4, direct propeller drive, air-cooled
Capacity: 2592 cc / 158 cu.in
Bore: 105.6 mm / 4.157 in
Stroke: 74 mm / 2.913 in
Max Power: 80 kW / 107 hp @ 3300 rpm
Max Torque: 240 Nm / 177 ft.lb @ 2800 rpm
Installed Weight: 72.3 kg/159.3 lb
Compression Ratio: 9.1:1
Firing Order: 1 – 3 – 2 – 4
Direction of Rotation: Clockwise – seen from cockpit
Fuel: min 98 OCT / 89 MON
Cylinders: 4
Oil capacity: 2.5 lt / 0.66 US gal
DC output: 30 Amp (+/- 15 Amp available above engine/fuel pump needs)
TBO: 1500h / 10y
UL260iF
Configuration: Flat-4, direct propeller drive, air-cooled
Max Power 74 kW / 100 hp @ 3000 rpm
Max Torque 240 Nm @ 2800 rpm
Capacity: 2592 cc
Bore: 105.6 mm
Stroke: 74 mm
Compression ratio: 9.10 : 1
Firing order: 1 – 3 – 2 – 4
Weight: 72.3 kg/159.3 lb
Fuel: min 98 OCT / 89 MON
Cylinders: 4
Oil capacity: 2.5 lt / 0.66 US gal
DC output: 30 Amp (+/- 15 Amp available above engine/fuel pump needs)
TBO: 1500h / 10y
UL260iSA
Configuration: Flat-4, direct propeller drive, air-cooled
Displacement: 2592 cc / 158.17 cu in
Bore: 105.6 mm / 4.157 in
Stroke: 74 mm / 2.913 in
Compression Ratio: 9.10 : 1
Max Power: 80 kW / 107 hp @ 3300 rpm
Max Torque: 240Nm / 177 ft.lb @ 2800 rpm
Firing Order: 1 – 3 – 2 – 4
Direction of Rotation: Clockwise – seen from cockpit
Installed Weight: 74.8 kg/164.9 lb
Fuel: min 98 OCT / 89 MON
Cylinders: 4
Oil capacity: 3.0 lt / 0.79 US gal
DC output: 30 Amp (+/- 15 Amp available above engine/fuel pump needs)
TBO: 250h
Equipped with an inverted oil kit
All Aero 