Performance Graph For Non-Standard Conditions - Rotax 912 i series Operator's Manual

Hide thumbs Also See for 912 i series:
Table of Contents

Advertisement

POWER vs. ECO
mode
140
140
120
120
100
100
Propeller load curve at
80
80
zero mph ground speed
60
60
40
40
20
20
0
0
3000
3000
3300
Performance
graph
Engine 912 iSc/iS
Effectivity: 912 i Series
OM Edition 1/Rev. 2
The 912 iSc/iS engine has two different modes, the POWER and
ECO mode where the fuel consumption changes significantly.
See from Fig. 2 to Fig. 4.
Propeller Load curve
during flight
3500
3800
4000
4000
4300
Fig. 5

Performance graph for non-standard conditions

The following graph shows the performance drop with increasing
flight altitude. The curves show the performance at 5800, 5500,
5000, 4800 and 4300 rpm, at full throttle.
At deviation of temperature conditions from standard atmosphere
conditions the engine performance to be expected can be calcu-
lated from the performance indicated, multiplied by standard tem-
perature, divided by actual temperature in °K.
Fig. 6
BRP-Powertrain
Take off phase
cruising condition
4500
4500
4800
5000
5000
rpm
PWR
mode
ECO
Mode
5300
5500
5500
5800
page 5-5
April 01/2014
09857
08636

Advertisement

Table of Contents
loading

This manual is also suitable for:

912i series

Table of Contents