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Remos GX - Engine

Remos GX
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Rev. 02 – July 16
th
, 2009
2 Airplane and Systems Descriptions
Airplane and Systems Descriptions 2 - 2
2.1 Engine
Manufacturer:
Bombardier-Rotax
Engine type: 912 UL-S *
Max. power: at take-off: 73,6 kW / 100 hp
permanent: 69,9 kW / 95 hp
Max. rpm: at take-off: 5.800 rpm.
permanent: 5.500 rpm.
Max. cylinder head temp: 275°F (135°C)
Max. fuel pressure: 5,7 psi (0,4 Bar)
Max. oil temperature: 266°F (130° C)
Min. oil temperature: 120°F (50°C)
2.2 Propeller, Gearbox
Propeller Manufacturer:
Propeller type / nr. of blades:
Sensenich
2A0-R5R70-EN
2-blade, carbon **
Neuform
CR3-65-47-101.6
3-blade, composite **
Gearbox Manufacturer:
Rotax
Gearbox ratio, Engine / Prop: 2,43 : 1
Clutch: yes
*
Manufacturer specification until overhaul / TBO = 1.500 hrs.
**
Refer to manufacturer specification for servicing information.
!
Values are subject to change without notice; please refer to the latest issues
of the appropriate manufacturer manuals.

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