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. The green band is indicative of normal areas of operation. [. . . ] 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. It is also disabled when the ASSIST softkey is pressed. 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. A Garmin G1000 EIS Pilot's Guide for Mooney M20M & M20R 7-5 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). Below the engine indicators are the fuel calculations. A numeric readout is provided for fuel flow, and gallons used. The fuel calculation portion of the System Page is based on the fuel flow totalizer and displays the following: · FF GPH ­ Fuel flow in gallons per hour. · GAL USED ­ Quantity of fuel used in gallons. [. . . ] 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 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. 2 Elevator Trim Figure 7. 4. 6 Flaps ­ In Transit 7-8 Garmin G1000 EIS Pilot's Guide for Mooney M20M & M20R 190-00447-00 Rev. A Garmin G1000 EIS Pilot's Guide for Mooney M20M & M20R Garmin International, Inc. 1200 East 151st Street Olathe, KS 66062, U. S. A. [. . . ]