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Garmin G1000 Pilot’s Guide for the Diamond DA40/40F
190-00592-06 Rev. A78
ENGINE INDICATION SYSTEM
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICESINDEX
3.1 EIS DISPLAY
1
Engine Manifold Pressure
Gauge (MAN IN HG)
Displays manifold pressure in inches of Mercury (in Hg) to indicate
engine power (DA40 only)
2
Tachometer (RPM)
Displays propeller speed in revolutions per minute (rpm); the red band
indicates propeller overspeed
3
Fuel Flow Indicator
(FUEL FLOW GPH)
Displays current fuel flow in gallons per hour (gph)
4
Fuel Pressure Indicator
(FUEL PRESS PSI)
Displays the fuel pressure in pounds per square inch (psi) (Option for
EASA certified DA40 aircraft only)
5
Cylinder Head Temperature
Indicator (CHT)
Displays the head temperature of the hottest cylinder (number is shown
in pointer)
6
Oil Temperature Indicator
(OIL TEMP)
Displays engine oil temperature
7
Oil Pressure Indicator
(OIL PRES)
Displays pressure of oil supplied to the engine
8
Ammeter (AMPS)
Displays the alternator load in amperes
9
Voltmeter (VOLTS)
Displays the primary bus voltage
10
Fuel Quantity Indicator
(FUEL QTY GAL)
Displays the quantity, in gallons (gal), of fuel in the tanks; pointers labeled
L and R indicate the fuel quantity in each tank
Standard Tanks: Indicator ranges from 0 to 20 gal with tick marks every 5
gal; only displays to 17 gal per side when full
Long Range Tanks (optional): Indicator ranges from 0 to 25 gal with tick
marks every 5 gal; only displays to 24 gal per side when full