User manual GARMIN G1000 MOONEY EIS PILOTS GUIDE M20

[. . . ] Below those gauges are color-coded horizontal bar indicators with triangle pointers and numeric readouts indicating fuel quantity (no numeric readout), fuel flow (normally aspirated), fuel pressure (turbocharged), oil pressure, oil temperature, exhaust gas temperature (EGT) of the hottest cylinder ­ for normally aspirated aircraft, turbine inlet temperature (TIT) ­ for turbocharged aircraft, and cylinder head temperature (CHT) of the hottest cylinder. The pointer on the horizontal bar indicators appears in white, which represents acceptable areas of operation. The pointer color changes to yellow or red upon exceeding areas of normal operation. Located beneath the horizontal bar indicators are the electrical indicators. [. . . ] · Green ­ Normal · Red ­ Warning Voltmeter The Voltmeter displays the bus voltage for the selected battery (i. e. , VOLTS1 or VOLTS2). Ammeter The Ammeter displays the battery amperage for the selected battery (i. e. , BAT1 or BAT2). NOTE: The pilot should refer to the Aircraft Flight Manual (AFM) for limitations. 7-2 Garmin G1000 EIS Pilot's Guide for Mooney M20M & M20R 190-00447-00 Rev. A ENGINE INDICATION SYSTEM Manifold Pressure Gauge Tachometer Fuel Quantity Indicator Fuel Flow Indicator Oil Pressure Indicator Oil Temperature Indicator Exhaust Gas Temperature Cylinder Head Temperature Indicator Voltmeter Ammeter Figure 7. 1. 1 ENGINE Page (Normally Aspirated) Fuel Pressure Indicator Turbine Inlet Temperature Indicator Figure 7. 1. 2 ENGINE Page (Turbocharged) 190-00447-00 Rev. A Garmin G1000 EIS Pilot's Guide for Mooney M20M & M20R 7-3 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. By default, the numeric readouts of EGT and CHT are associated with the hottest cylinder and are graphically indicated in cyan (light blue). Color coding for the EGT and CHT bar graphs is listed below: · · · · Cyan ­ Selected cylinder (EGT and CHT) White ­ Normal (EGT and CHT) Yellow ­ Caution (CHT only) Red ­ Warning (CHT only) Lean Assist The ASSIST softkey can be utilized to assist in the leaning process. Normally Aspirated When a cylinder peaks, its peak is represented by a hollow bar on the EGT bar graph. The EGT readout for the peaked cylinder, indicated in cyan (light blue), appears directly beneath the bar graph. The system automatically switches to the first peak obtained and displays the temperature deviation from peak in degrees Fahrenheit below the EGT readout. NOTE: The Lean Assist function is not available for the turbocharged Mooney models. NOTE: The pilot should follow the engine manufacturer's recommended leaning procedures in the Aircraft Flight Manual (AFM). The temperature deviation from peak in degrees Fahrenheit for normally aspirated aircraft is displayed beneath the EGT readout. Located to the lower right of the EIS strip are the flap and elevator trim position indicators. The rudder trim is not shown on this page. Cylinder Select The CYL SLCT softkey can be utilized to obtain information about a particular cylinder. The CYL SLCT softkey becomes disabled when a particular cylinder turns yellow (Caution) or red (Warning), until the temperature decreases and returns to normal, which is indicated by white on the bar graph. The CYL SLCT and ASSIST softkeys are available by pressing the LEAN softkey. From the Lean Page, press the CYL SLCT softkey to cycle through each cylinder and view the EGT and CHT. The ASSIST softkey is available by pressing the LEAN softkey. From the Lean Page, press the ASSIST softkey to acquire EGT peak. NOTE: Pilots should refer to the Aircraft Flight Manual (AFM) for limitations. 7-4 Garmin G1000 EIS Pilot's Guide for Mooney M20M & M20R 190-00447-00 Rev. A ENGINE INDICATION SYSTEM Manifold Pressure Gauge Tachometer Fuel Quantity Indicator Fuel Flow Indicator Hollow Bar Representing Peak Exhaust Gas Temperature Bar Graph Exhaust Gas Temperature Indicator Turbine Inlet Temperature Indicator Temperature Deviation From Peak Cylinder Head Temperature Bar Graph Cylinder Head Temperature Indicator Figure 7. 2. 1 LEAN Page (Normally Aspirated) Figure 7. 2. 2 LEAN Page (Turbocharged) 190-00447-00 Rev. [. . . ] NOTE: Pilots should refer to the Aircraft Flight Manual (AFM) for limitations. 7-6 Garmin G1000 EIS Pilot's Guide for Mooney M20M & M20R 190-00447-00 Rev. A ENGINE INDICATION SYSTEM Manifold Pressure Gauge Tachometer Fuel Quantity Indicator Fuel Pressure Indicator Oil Pressure Indicator Engine Hours (Tach) Fuel Flow Indicator Oil Temperature Indicator Exhaust Gas Temperature Indicator Gallons Used Indicator Voltmeter Ammeter Figure 7. 3. 1 SYSTEM Page (Normally Aspirated) Figure 7. 3. 2 SYSTEM Page (Turbocharged) 190-00447-00 Rev. A Garmin G1000 EIS Pilot's Guide for Mooney M20M & M20R 7-7 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. The white bar indicates the takeoff setting range. Flap Position Indicator The flap position indicator is collocated with the elevator trim position indicator. [. . . ]