User manual GARMIN G1000 MOONEY EIS PILOTS GUIDE M20M M20R

[. . . ] Located beneath the horizontal bar indicators are the electrical indicators. A numeric readout is provided for the bus voltage and battery amperage. Manifold Pressure Gauge The Manifold Pressure gauge displays the engine power in inches of mercury (in Hg). · White ­ Normal operating range · Red ­ Maximum manifold pressure (turbocharged) 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. Lean Page The Lean Page provides engine leaning information and a user interface to perform engine leaning. [. . . ] · Green ­ Normal · Yellow ­ Caution (low and high indications are on turbocharged aircraft only) · Red ­ Warning (minimum and maximum) 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: Refer to the Aircraft Flight Manual (AFM) for limitations. Oil Temperature Indicator The Oil Temperature indicator displays the engine oil temperature in degrees Fahrenheit. · Green ­ Normal · Red ­ Warning 7-2 Garmin G1000 EIS Pilot's Guide for Mooney M20M & M20R 190-00447-01 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) 190-00447-01 Rev. A Garmin G1000 EIS Pilot's Guide for Mooney M20M & M20R 7-3 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. 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 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. The ASSIST softkey is available by pressing the LEAN softkey. From the Lean Page, press the ASSIST softkey to identify the peak. NOTE: The Lean Assist function is not available for the turbocharged Mooney models. NOTE: If any parameters are exceeded the system automatically switches back to the default Engine 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. From the Lean Page, press the CYL SLCT softkey to cycle through each cylinder and view the EGT and CHT. 7-4 Garmin G1000 EIS Pilot's Guide for Mooney M20M & M20R 190-00447-01 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) 190-00447-01 Rev. A Garmin G1000 EIS Pilot's Guide for Mooney M20M & M20R 7-5 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 calculation portion of the System Page is based on the fuel flow totalizer and displays the following: · FFLOW GPH ­ Fuel flow in gallons per hour. Below the fuel calculations is a color-coded horizontal bar indicator with a numeric readout for EGT (normally aspirated). [. . . ] The flap indications are displayed inside the box on top the elevator trim. The flap positions are as follows: · UP · T/O (takeoff) · DN (down) Figure 7. 4. 1 Rudder Trim Figure 7. 4. 3 Flaps ­ Up Elevator Trim Position Indicator The Elevator Trim Position indicator is located to the lower right of the EIS strip. Elevator trim position is displayed by a cyan (light blue) triangle pointer on a vertical bar indicator. The white bar indicates the takeoff setting range. Figure 7. 4. 4 Flaps ­ Takeoff Figure 7. 4. 5 Flaps ­ Down When the flaps are in transit and not within these ranges, `///' is displayed inside the box. Figure 7. 4. 6 Flaps ­ In Transit Figure 7. 4. 2 Elevator Trim 7-8 Garmin G1000 EIS Pilot's Guide for Mooney M20M & M20R 190-00447-01 Rev. [. . . ]