G1000 TM engine indication system pilot’s guide for Mooney M20M & M20R
Record of Revisions Revision Date of Revision Revision Page Range A 10/18/04 7-1 – 7-8 Description Initial release. Garmin G1000 EIS Pilot’s Guide for Mooney M20M & M20R 190-00447-00 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 flight crew. The EIS also displays the rudder trim, elevator trim and flap position indicators. The EIS is displayed on the left side of the MFD during normal operations. In reversionary mode, the CDUs are re-configured to present the PFD symbology together with the EIS (the EIS is displayed on the left side).
ENGINE INDICATION SYSTEM Fuel Flow GPH Indicator (Normally Aspirated) EGT Indicator (Normally Aspirated) The Fuel Flow indicator displays current fuel flow in gallons per hour (GPH). The indicator ranges from 0 to 30. This indicator does not have a color band. The EGT (Exhaust Gas Temperature) indicator displays the exhaust gas temperature of the hottest cylinder in degrees Fahrenheit.
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) 190-00447-00 Rev. A Figure 7.1.
ENGINE INDICATION SYSTEM 7.2 LEAN The Lean Page provides information and a user interface to perform engine leaning. Located beneath the tachometer is a color-coded horizontal bar indicator for fuel quantity and a numeric readout for fuel flow. Below these indicators are bar graphs and numeric readouts for exhaust gas temperature (EGT) – for normally aspirated aircraft and cylinder head temperature (CHT) 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) 190-00447-00 Rev. A Figure 7.2.
ENGINE INDICATION SYSTEM 7.3 SYSTEM The System Page displays a numeric readout for the fuel pressure (turbocharged), engine and electrical indicators. Located beneath the Tachometer is a color-coded horizontal bar indicator for fuel quantity (an additional color-coded horizontal bar indicator is displayed for fuel pressure in the turbocharged aircraft). Beneath these indicators are the numeric readouts for oil pressure, oil temperature and engine hours (tach).
ENGINE INDICATION SYSTEM Manifold Pressure Gauge Tachometer Fuel Quantity Indicator Fuel Pressure Indicator Oil Pressure Indicator Oil Temperature Indicator Engine Hours (Tach) Exhaust Gas Temperature Indicator Gallons Used Indicator Fuel Flow Indicator Voltmeter Ammeter Figure 7.3.1 SYSTEM Page (Normally Aspirated) 190-00447-00 Rev. A Figure 7.3.
ENGINE INDICATION SYSTEM 7.4 FLAP & TRIM INDICATIONS Rudder Trim Position Indicator The 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. Flap Position Indicator The flap position indicator is collocated with the elevator trim position indicator. The flap indications are displayed inside the box on top the elevator trim.
190-00447-00 Rev.
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