User manual GARMIN G1000 MOONEY EIS PILOTS GUIDE M20M M20R
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Manual abstract: user guide GARMIN G1000 MOONEY EIS PILOTS GUIDE M20M M20R
Detailed instructions for use are in the User's Guide.
[. . . ] Two (2) triangular pointers labeled L (Left) and R (Right) indicate the number of gallons in each fuel tank. · Green Normal · Yellow Caution · Red Warning Standard Tanks The indicator ranges from 0 (Empty) to F (Full) with tick marks at 5 gallon intervals.
NOTE: The Fuel Quantity indicator only displays to 44. 5 gallons when full.
7. 1 ENGINE
Atop all three pages are two (2) round dial gauges with a white pointer and digital readouts for manifold pressure and revolutions per minute (RPM). Below those gauges are color-coded horizontal bar indicators with triangular 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. [. . . ] 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. It is also disabled when the ASSIST softkey is pressed. The CYL SLCT softkey is 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.
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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 calculations reside below the engine indicators. A numeric readout is provided for fuel flow, and gallons remaining. 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. · GAL REM Quantity of fuel remaining in gallons. Below the fuel calculations is a color-coded horizontal bar indicator with a numeric readout for EGT (normally aspirated). Located at the bottom of the page are the electrical indicators. A numeric readout is provided for bus voltage and battery amperage. If desired, the pilot can utilize the DEC FUEL, INC FUEL and RST FUEL softkeys to adjust the amount of fuel remaining for totalizer calculations. · DEC FUEL Decreases totalizer based fuel quantity remaining in one gallon increments. [. . . ] 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
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Garmin G1000 EIS Pilot's Guide for Mooney M20M & M20R
190-00447-01 Rev. A
Garmin G1000 EIS Pilot's Guide for Mooney M20M & M20R
Garmin International, Inc. [. . . ]
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