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Pilot Operating Handbook - Ecoflight.ch

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Rev. 02 – July 16 th , 2009<br />

2 Airplane and Systems Descriptions<br />

2.1 Engine<br />

Manufacturer:<br />

Bombardier-Rotax<br />

Engine type: 912 UL-S *<br />

Max. power: at take-off: 73,6 kW / 100 hp<br />

permanent: 69,9 kW / 95 hp<br />

Max. rpm: at take-off: 5.800 rpm.<br />

permanent: 5.500 rpm.<br />

Max. cylinder head temp: 275°F (135°C)<br />

Max. fuel pressure:<br />

5,7 psi (0,4 Bar)<br />

Max. oil temperature: 266°F (130° C)<br />

Min. oil temperature:<br />

120°F (50°C)<br />

2.2 Propeller, Gearbox<br />

Propeller Manufacturer:<br />

Senseni<strong>ch</strong><br />

Neuform<br />

Propeller type / nr. of blades:<br />

2A0-R5R70-EN<br />

2-blade, carbon **<br />

CR3-65-47-101.6<br />

3-blade, composite **<br />

Gearbox Manufacturer: Rotax<br />

Gearbox ratio, Engine / Prop: 2,43 : 1<br />

Clut<strong>ch</strong>:<br />

yes<br />

* Manufacturer specification until overhaul / TBO = 1.500 hrs.<br />

** Refer to manufacturer specification for servicing information.<br />

!<br />

Values are subject to <strong>ch</strong>ange without notice; please refer to the latest issues<br />

of the appropriate manufacturer manuals.<br />

Airplane and Systems Descriptions 2 - 2

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