SAMPLE
2-3
Document No.:
Z601XLFMEN
Date of Issue:
12/2002
Revision:
2.4 Powerplant
Z
Z
E
E
N
N
A
A
I
I
R
R
C
C
H
H
6
6
0
0
1
1
Z
Z
O
O
D
D
I
I
A
A
C
C
, S/N:
is fitted with ROTAX 912
, S/N
and prop, Type / S/N
Engine Model:
ROTAX 912A
(or UL)
ROTAX 912S
(or ULS)
Engine Manufacturer:
Bombardier-Rotax GMBH
Max Take-off:
59.6 kW / 80 hp
at 5800 rpm, max.5 min.
73.5 kW / 100 hp
at 5800 rpm, max.5 min.
Max. Continuous:
58 kW / 78 hp
at 5500 rpm
69 kW / 93.8 hp
at 5500 rpm
Power
Cruising:
53 kW / 71 hp
at 4800 rpm
53 kW / 71 hp
at 4800 rpm
Max. Take-off:
Max. Continuous:
Cruising:
Engine
speed
Idling:
5800 rpm, max. 5 min.
5500
rpm
4800
rpm
~1400
rpm
Minimum:
60
°C
140 °F
60
°C
140 °F
Cylinder
head
temperature:
Maximum:
150
°C
302 °F
135
°C
275 °F
Minimum:
50
°C
122 °F
50
°C
122 °F
Maximum:
140
°C
284 °F
130
°C
266 °F
Oil
temperature
Optimum:
90 °C - 110 °C
194 - 230°F
90 °C - 110 °C
194 - 230°F
Minimum: 7,0
bar
Maximum: 1,5
bar
Oil
pressure:
Optimum: 1,5-4,0
bar
Fuel: see
2.13
Oil:
Automotive engine oil of registered brand with gear additives,
but not aircraft oil (refer to engine Operator’s Manual).
API classification „SF“ or „SG“.
Propeller type
and Manufacturer
i
WOODCOMP KLASSIC 170 R
i
WOODCOMP VARIA 170
i
WARP
DRIVE
i
SR
2000
For technical data refer to documentation supplied by the
propeller manufacturer.
WARNING
The Rotax 912 UL has not been certified as an aircraft engine and its failure may occur
at any time. The pilot is fully responsible for consequences of such a failure.
