Garmin G1000 Pilot’s Guide for the Diamond DA40/40F 190-00592-06 Rev. A78ENGINE INDICATION SYSTEMSYSTEMOVERVIEWFLIGHTINSTRUMENTSEISAUDIO PANEL& CNSFLIGHTMANAGEMENTHAZARDAVOIDANCEAFCSADDITIONALFEATURESAPPENDICESINDEX3.1 EIS DISPLAY1 Engine Manifold PressureGauge (MAN IN HG)Displays manifold pressure in inches of Mercury (in Hg) to indicateengine power (DA40 only)2 Tachometer (RPM) Displays propeller speed in revolutions per minute (rpm); the red bandindicates propeller overspeed3 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 forEASA certified DA40 aircraft only)5 Cylinder Head TemperatureIndicator (CHT)Displays the head temperature of the hottest cylinder (number is shownin pointer)6 Oil Temperature Indicator(OIL TEMP)Displays engine oil temperature7 Oil Pressure Indicator(OIL PRES)Displays pressure of oil supplied to the engine8 Ammeter (AMPS) Displays the alternator load in amperes9 Voltmeter (VOLTS) Displays the primary bus voltage10 Fuel Quantity Indicator(FUEL QTY GAL)Displays the quantity, in gallons (gal), of fuel in the tanks; pointers labeledL and R indicate the fuel quantity in each tankStandard Tanks: Indicator ranges from 0 to 20 gal with tick marks every 5gal; only displays to 17 gal per side when fullLong Range Tanks (optional): Indicator ranges from 0 to 25 gal with tickmarks every 5 gal; only displays to 24 gal per side when full
