User manual GARMIN G1000 MOONEY PILOTS GUIDEFRONTMATTERANDINDEX M20

[. . . ] 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). · White ­ Below normal flight operating range. · Green ­ Normal flight operating range. · Red ­ Propeller overspeed. Fuel Flow GPH Indicator The Fuel Flow indicator displays current fuel flow in gallons per hour (GPH). The Fuel Flow indicator ranges from 0 to 30. · Red ­ Abnormal fuel flow. 190-00550-00 Rev. 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. The number of the hottest cylinder appears in the triangular pointer. · 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. · Green ­ Normal · Yellow ­ Caution Fuel Qty GAL Indicator The Fuel Quantity indicator displays the quantity of fuel in the tanks, in gallons. 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. To increase the fuel totalizer quantity: 1. From the System Page, press the INC FUEL softkey to obtain the desired number of gallons remaining. From the System Page, press the RST FUEL softkey. 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. · GAL USED ­ Quantity of fuel used in gallons. · ENDUR ­ Flight time remaining with fuel onboard (HH:MM when more than an hour remains). · RANGE NM ­ Aircraft range in nautical miles. Fuel calculations do not use the aircraft fuel quantity indicators and are calculated from the last time the fuel was reset. [. . . ] · INC FUEL ­ Increases totalizer based fuel quantity remaining in one gallon increments. · RST FUEL ­ Reset totalizer based fuel quantity remaining relative to the aircraft fuel capacity. Performing the fuel reset also sets the GAL USED display to zero. 7-8 Electrical · ALT LOAD ­ Alternator load in amperes · BUS VOLTS ­ Primary bus voltage NOTE: Refer to the Pilot's Operating Handbook (POH) for limitations. Garmin G1000 EIS Pilot's Guide for the A36/G36 190-00550-00 Rev. A ENGINE INDICATION SYSTEM Manifold Pressure Gauge Tachometer Oil Temperature Fuel Flow Gallons Used Range in Nautical Miles Oil Pressure Gallons Remaining Endurance Amperes Voltage Figure 7. 4. 1 SYSTEM Engine Page 190-00550-00 Rev. [. . . ]