1) Performance Graphs For Stand. Conditions (Isa)10 - Rotax 912 series Operator's Manual

10.1.1.1) Performance graphs for stand. conditions (ISA)
kW
00450
60
50
40
30
20
10
0
3000
00451
in.Hg
30
20
10
0
3000
Effectivity: 912 UL / A / F
OM initial issue
A: max. engine output
B: power requirement of propeller
A
B
4000
C: manifold pressure
D: fuel consumption
C
4000
Values along propeller curve
AIRCRAFT ENGINES
5000
D
5000
hp
80
70
60
50
40
30
20
10
fig. 9
5800 rpm
(Gal/h)
L/h
30 (7,93)
(5,28)
20
(2,64)
10
0
5800 rpm
fig. 10
page 10 - 3
July 01/98