Tecnam P92-JS - POWERPLANT LIMITATIONS

FLIGHT MANUAL
Date: Issue 3: 25
th
May 2010
2-4
P92-JS
S E C T I O N 2
LIMITATIONS
POWERPLANT LIMITATIONS
The following table lists operating limitations for aircraft installed engine:
ENGINE MANUFACTURER: Bombardier Rotax GmbH.
ENGINE MODEL: 912 S2
MAXIMUM POWER: (see table below)
Max Power
kW (hp)
Max RPM.
RPM prop (eng.)
Time max.
(min.)
Maximum
73.5 (98.6)
2388 (5800)
5
Max cont.
69 (92.5)
2265 (5500)
-
The static rpm range at full throttle (carburetors heat: Off) is 2100  100 prop.
rpm.
TEMPERATURES:
Max cylinder heads
135° C
Cooling liquid, monitored at cylinder heads
135° C
Max Oil:
130° C
Min Oil
50° C
OIL PRESSURE:
Min
0.8 bar
Max
5 bar
ENGINE START, OPER. TEMP:
OAT Min
-25° C
OAT Max
+50° C
Admissible pressure for cold start is 7 bar maximum for short periods.
WARNING
NOTE