User manual GARMIN G1000 MOONEY PILOTS GUIDEFRONTMATTERANDINDEX M20

[. . . ] The green band is indicative of normal operations. Bar Graphs (Lean Page Only) Each bar graph is numbered and represents a cylinder. The graphs appear white (when a cylinder is selected that graph changes to cyan), representing areas of normal operation. The color changes to yellow or red upon exceeding areas of normal operation. Digital Readouts These readouts appear as white text on a black background, representing areas of normal operation. The color changes to black text on a yellow background (caution) or white text on a red background (warning) upon exceeding areas of normal operation. 190-00550-00 Rev. [. . . ] Parameter Fuel Flow GPH Cylinder Head Temperature Oil Temperature Oil Pressure Alternator 1 Load Alternator 2 Load Exceedance Greater than 27. 4 GPH Greater than 238 ºC Greater than 116 ºC Less than 30 PSI or greater than 100 PSI Greater than 100% (100 Amps) Greater than 100% (20 Amps) for 240s or longer Less than 24V or greater the 30V Less than 24V or greater the 30V Less than 13 GAL Less than 13 GAL Bus 1 Volts Bus 2 Volts Left Fuel Quantity Right Fuel Quantity Table 7. 1. 1 Auto Switch Default ENGINE Page 7-2 Garmin G1000 EIS Pilot's Guide for the A36/G36 190-00550-00 Rev. A ENGINE INDICATION SYSTEM 7. 2 ENGINE PAGE Atop all three pages are two round dial gauges for manifold pressure and revolutions per minute (RPM). Beneath those gauges are horizontal bar indicators for fuel flow, cylinder head temperature (CHT), oil temperature, oil pressure, alternator amperage, bus voltage and fuel quantity. Fuel Flow Leaning Pointer The Fuel Flow Leaning Pointer provides a leaning reference for the pilot during a Max Power Climb (MPC) or Cruise Climb. The pointer is displayed on the bottom of the Fuel Flow indicator if the RPM exceeds 2530, or fuel flow exceeds a specified value based on altitude during a MPC or Cruise Climb (see table below). Fuel Flow Leaning Leaning Leaning Max Power Cruise Climb Climb GPH GPH 25. 7 23. 7 25. 7 23. 7 25. 1 23. 1 24. 0 22. 0 22. 4 20. 4 20. 9 18. 9 19. 6 17. 6 18. 8 16. 8 17. 9 15. 9 Table 7. 2. 1 Fuel Flow Leaning Manifold Pressure Gauge The Manifold Pressure gauge displays the engine power in inches of mercury (in Hg). Altitude x1000ft 0 2 4 6 8 10 12 14 16 Tachometer The Tachometer displays propeller speed in revolutions per minute (RPM). · Red ­ Propeller overspeed. Fuel Flow GPH Indicator The Fuel Flow indicator displays current fuel flow in gallons per hour (GPH). A Garmin G1000 EIS Pilot's Guide for the A36/G36 7-3 ENGINE INDICATION SYSTEM CHT Indicator The CHT (Cylinder Head Temperature) indicator displays the temperature of the hottest cylinder in degrees Fahrenheit. · Green ­ Normal · Red ­ Warning Voltmeter The Voltmeter displays the primary bus voltage. The Voltmeter displays two (2) pointers which indicate the voltage for Buses 1 and 2. From the Lean Page, press the CYL SLCT softkey to cycle through each cylinder and view the EGT and CHT. 7-6 Garmin G1000 EIS Pilot's Guide for the A36/G36 190-00550-00 Rev. A ENGINE INDICATION SYSTEM Manifold Pressure Gauge Tachometer Fuel Flow Indicator Cyan Line Representing Peak EGT Readout For Selected Cylinder Temperature Deviation From Peak Exhaust Gas Temperature Bar Graph CHT Readout For Selected Cylinder Cylinder Head Temperature Bar Graph Figure 7. 3. 1 LEAN Engine Page 190-00550-00 Rev. A Garmin G1000 EIS Pilot's Guide for the A36/G36 7-7 ENGINE INDICATION SYSTEM 7. 4 SYSTEM PAGE The System Page is accessible by pressing the SYSTEM softkey. The readouts on this page are separated into three categories: System, Fuel Calculation and Electrical. To decrease the fuel totalizer quantity: 1. From the System Page, press the DEC FUEL softkey to obtain the desired number of gallons remaining. From the System Page, press the INC FUEL softkey to obtain the desired number of gallons remaining. This also resets the GAL USED to zero. System · OIL ºC ­ Oil temperature in degrees Celsius · OIL PSI ­ Oil pressure in pounds per square inch To reset the fuel totalizer: 1. Fuel Calculation 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 ­ Current fuel remaining in gallons as set by the pilot and adjusted for fuel burn since last set. · ENDUR ­ Flight time remaining with fuel onboard (HH:MM when more than an hour remains). Fuel calculations do not use the aircraft fuel quantity indicators and are calculated from the last time the fuel was reset. [. . . ] Fuel calculations do not use the aircraft fuel quantity indicators and are calculated from the last time the fuel was reset. 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. · INC FUEL ­ Increases totalizer based fuel quantity remaining in one gallon increments. [. . . ]