Garmin G2000 Pilot’s Guide for the cessna T240
190-01263-01 Rev. A
118
engine indication SyStem
Sy
Stem
o
Ver
VieW
fligHt
inStrUmentS
eiS
aUdio p
anel
& cnS
fligHt
mana
gement
HaZard
aV
oid
ance
afcS
additional fea
tUreS
appendiceS
indeX
Figure 3-21 Engine and Systems Display
3
1
2
4
6
5
7
1
Exhaust Gas Temperature
(EGT °F)
For each cylinder, the exhaust gas temperatures are shown in degrees
Fahrenheit (°F). Each bar segment on the graph represents 25 degrees.
2
Alternator Amps
(ALT AMPS)
Currents for the right and left alternators are displayed using vertical bar
indicators and readouts.
3
Oxygen Outlet Pressure
Gauge (OXY OUTLET
PSI)
Oxygen outlet pressure in psi. Gauge ranges are dependent on type of
oxygen outlet pressure system installed (high or low).
4
Fuel Calculations Group
(GAL REM, GAL USED,
ENDUR, RANGE NM)
The fuel totalizer fuel remaining and used and the totalizer-based
endurance and range calculations are displayed
5
Anti-Ice Time Remaining
(A-ICE TIME REM)
(Optional)
The Anti-Ice Time Remaining based on the Anti-Ice fl uid quantity and
the Anti-Ice fl uid fl ow rate. FIKI (Flight Into Known Icing) Anti-Ice
option only.
6
Cylinder Head
Temperature (CHT °F)
For each cylinder, the head temperatures are shown in degrees Fahrenheit
(°F). Each bar segment on the graph represents 100 degrees.
7
Oxygen Quantity Gauge
(OXY QTY PSI)
Oxygen amount in psi; note that gauge increment is 100 psi
This manual downloaded from http://www.manualowl.com
