G1000 TM engine indication system pilot’s guide for Mooney M20M & M20R
Record of Revisions Revision Date of Revision Revision Page Range A 05/23/05 7-1 – 7-8 Description Initial release. Garmin G1000 EIS Pilot’s Guide for Mooney M20M & M20R 190-00447-01 Rev.
ENGINE INDICATION SYSTEM The G1000 Engine Indication System (EIS) is designed to provide gauges, bar graphs and numeric readouts of engine parameters to the pilot. The EIS is displayed on the left side of the MFD during normal operations. NOTE: Refer to the System Overview for information regarding reversionary mode. The EIS contains three distinct pages, which are accessed by the ENGINE softkey: Engine Page This is the default page, which displays all critical engine, fuel and electrical indicators.
ENGINE INDICATION SYSTEM Long Range Tanks (optional) The Long Range tank option allows for 55 gallons per side (110 total). The indicator range is the same as the standard tank. The pointers will remain at Full until the quantity decreases below 44.5 gallons. NOTE: Refer to the Aircraft Flight Manual (AFM) for limitations regarding fuel quantity. Fuel Flow GPH Indicator (Normally Aspirated) The Fuel Flow indicator displays current fuel flow in gallons per hour (GPH). The indicator ranges from 0 to 30.
ENGINE INDICATION SYSTEM Manifold Pressure Gauge Tachometer Fuel Quantity Indicator Fuel Flow Indicator Fuel Pressure Indicator Oil Pressure Indicator Oil Temperature Indicator Turbine Inlet Temperature Indicator Exhaust Gas Temperature Cylinder Head Temperature Indicator Voltmeter Ammeter Figure 7.1.1 ENGINE Page (Normally Aspirated) 190-00447-01 Rev. A Figure 7.1.
ENGINE INDICATION SYSTEM 7.2 LEAN The Lean Page is accessible by pressing the LEAN softkey. A color-coded horizontal bar indicator for fuel quantity and a numeric readout for fuel flow reside below the tachometer. Beneath the fuel flow indication is the turbo inlet temperature indicator (turbocharged) followed by bar graphs and numeric readouts for exhaust gas temperature (normally aspirated) and cylinder head temperature in degrees Fahrenheit.
ENGINE INDICATION SYSTEM Manifold Pressure Gauge Tachometer Fuel Quantity Indicator Fuel Flow Indicator Hollow Bar Representing Peak Turbine Inlet Temperature Indicator Exhaust Gas Temperature Bar Graph Temperature Deviation From Peak Exhaust Gas Temperature Indicator Cylinder Head Temperature Bar Graph Cylinder Head Temperature Indicator Figure 7.2.1 LEAN Page (Normally Aspirated) 190-00447-01 Rev. A Figure 7.2.
ENGINE INDICATION SYSTEM 7.3 SYSTEM The System Page is accessible by pressing the SYSTEM softkey. Beneath the Tachometer is a color-coded horizontal bar indicator for fuel quantity (normally aspirated) or fuel pressure (turbocharged), followed by numeric readouts for oil pressure, oil temperature and engine hours (tach). The fuel calculations reside below the engine indicators. A numeric readout is provided for fuel flow, and gallons remaining.
ENGINE INDICATION SYSTEM Manifold Pressure Gauge Tachometer Fuel Quantity Indicator Fuel Pressure Indicator Oil Pressure Indicator Oil Temperature Indicator Engine Hours (Tach) Gallons Remaining Indicator Exhaust Gas Temperature Indicator Fuel Flow Indicator Voltmeter Ammeter Figure 7.3.1 SYSTEM Page (Normally Aspirated) 190-00447-01 Rev. A Figure 7.3.
ENGINE INDICATION SYSTEM 7.4 FLAP & TRIM INDICATIONS Rudder Trim Position Indicator The Rudder Trim Position indicator is located beneath the EIS strip. Rudder trim position is displayed by a cyan (light blue) triangle on a horizontal bar indicator. L (left) and R (right) tick marks are shown. The white bar indicates the takeoff setting range. The rudder trim is not displayed on the LEAN page. Figure 7.4.
190-00447-01 Rev.
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