Rotax 912 ULS 3 Operator's Manual page 55

Performance data
Engine 912 A/F/UL
Effectivity: 912 A/F/UL
OM Edition 2 / Rev. 0
Performance data for variable pitch propeller
Engine speed over 5500 rpm is restricted to 5 minutes.
Run the engine in accordance with the following table.
Engine
Power setting speed
Take-off power
max. continous
power
75 %
65 %
55 %
NOTE: Further essential information regarding engine
behavior see Service Letter SL-912-016, latest
edition.
BRP-Powertrain
Perfor-
mance
(rpm) (kW)/(HP)
5800 59.6 80
5500 58.0 78
5000 43.5 58
4800 37.7 50
4300 31.9 43
Manifold
Torque (Nm)
pressure
(ft.lb)
(in.HG)
72.35
98.1 full throttle
ft.lb
74.27
100.7 full throttle
ft.lb
61.29
83.1 27.2
ft.lb
55.32
75.0 26.5
ft.lb
52.22
70.8 26.3
ft.lb
page 5-3
April 01/2010