Page 2- 5
Section 2 - Limitations
POWERPLANT LIMITATIONS
1
st
Edition - Rev. 0
4.
P
OWERPLANT LIMITATIONS
Following table reports the operating limitations for aircraft engine installed:
E
NGINE MANUFACTURER
:
Bombardier Rotax GmbH.
E
NGINE MODEL
:
912 ULS2
M
AXIMUM POWER
:
Max Power
kW (hp)
Max RPM.
Prop. RPM (engine)
Time max.
(minutes)
Max. T.O.
73.5
(98.5)
2388
(5800)
5
Max. Cont.
69
(92.5)
2265
(5500)
-
With full throttle, at fixed point in no wind conditions, the maximum
propeller’s RPM should be 2100
100.
Temperatures:
Max CHT*
135°C
Max CT:
120°C
Min/Max Oil:
50 °C / 130 °C
Oil normal operating range (approx.):
90 °C / 110 °C
*
applicable for En
repaired engine
one (part no. 413
gines up to serial no. 4924543(included) and
hich doesn’t change the cylinder head n°3 with new
195)
Oil Pressure:
Minimum:
0.8 Bar / 12 psi
Normal:
2-5 Bar / 29-73 psi
Maximum:
7 Bar / 102 psi
Engine starting: allowable temperature range
OAT Min
-25° C
OAT Max
+50° C
WARNING
In event of cold starting operation, it is permitted a maximum
oil pressure of 7 bar for a short period.
Fuel pressure:
Minimum:
2.2 psi (0.15 Bar)
Normal:
5.8 psi (0.40 Bar) or 7.26 psi* (0.5 Bar)
* only applicable for fuel pump part no. 893110, 893114 and 893115
NOTE
Summary of Contents for P92 Echo MKII
Page 8: ...Page 0 8 Aircraft Flight Manual SECTION LISTS 1st Edition Rev 0 Intentionally left blank ...
Page 22: ...Page 1 14 Section 1 General 1st Edition Rev 0 INTENTIONALLY LEFT BLANK ...
Page 68: ...Page 4 12 Section 4 Normal Procedures CHECKLISTS 1st Edition Rev 0 INTENTIONALLY LEFT BLANK ...
Page 128: ...Page 9 4 Section 9 AFM Supplements 1st Edition Rev 0 INTENTIONALLY LEFT BLANK ...
