Eis Display; Section 3 Engine Indication System 3.1 Eis Display - Garmin Cirrus Perspective SR20 Pilot's Manual

ENGINE INDICATION SYSTEM

3.1 EIS DISPLAY

Refer to the Pilot's Operating Handbook (POH) for engine operating limitations.
NOTE:
Depictions of equipment may differ from the installed equipment. Examples shown may differ from
NOTE:
actual aircraft configurations.
1 Percent Power Indicator
(% Pwr)
2
Tachometer (RPM)
3
Engine Manifold Pressure
Indicator (Man "Hg)
4 Fuel Flow Indicator
(FFlow GPH)
5 Gallons Used Indicator
(Gal Used)
6
Oil Temperature Indicator
(Oil ºF)
7
Oil Pressure Indicator
(Oil PSI)
8 Ammeter (Batt1 A)
9 Voltmeter (ESS Bus V)
10
Cylinder Head Temperature
Indicator (CHT ºF)
11
Exhaust Gas Temperature
Indicator (EGT ºF)
Exhaust Gas Temperature/
Turbine Inlet Temperature
Indicator (EGT/TIT ºF)
12
Left and Right Turbine Inlet
Temperature
88 Cirrus Perspective
Displays engine power as a percentage
Displays propeller speed in revolutions per minute
Displays manifold pressure in inches of Mercury to indicate engine
power
Displays fuel flow in gallons per hour (Turbo models only – displays a light
blue target fuel flow indicator to the right of the fuel flow indicator strip,
shown in Figure 3-3)
Displays the fuel used in gallons
Displays engine oil temperature in degrees Fahrenheit
Displays pressure of oil supplied to the engine in pounds per square inch
(psi)
Displays the battery 1 load in amperes
Displays the essential bus voltage in volts
Displays the head temperature of the hottest cylinder (CHT; cylinder
number is shown below bar)
Displays the exhaust gas temperature (cylinder number is shown below
bar) (naturally aspirated models only)
Displays the exhaust gas temperature and turbine inlet temperature
(cylinder number or turbine inlet side is shown below bar) (Turbo
models only, shown in Figure 3-3)
Displays the temperature at the left (L) and right (R) turbine inlet (Turbo
models only, shown in Figure 3-3).
by Garmin – Pilot's Guide for the SR20/SR22/SR22T
™
190-00820-08 Rev. A