Tecnam P92 Echo MKII - Powerplant limitations

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Section 2 - Limitations
POWERPLANT LIMITATIONS
1
st
Edition - Rev. 0
4. POWERPLANT LIMITATIONS
Following table reports the operating limitations for aircraft engine installed:
ENGINE MANUFACTURER: Bombardier Rotax GmbH.
ENGINE MODEL: 912 ULS2
MAXIMUM 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