G1000 TM Engine Indication System Pilot’s Guide for the Beechcraft A36/G36
Record of Revisions Revision Date of Revision Revision Page Range A 07/22/05 7-1 – 7-9 Description Initial release. Garmin G1000 EIS Pilot’s Guide for the A36/G36 190-00550-00 Rev.
ENGINE INDICATION SYSTEM 7.1 INTRODUCTION The G1000 Engine Indication System (EIS) is designed to provide gauges, bar graphs and numeric readouts of engine parameters to the pilot. The EIS is displayed on the left side of the MFD during normal operations. NOTE: Refer to the System Overview for information regarding reversionary mode.
ENGINE INDICATION SYSTEM EIS PAGE REVERSION The EIS automatically switches to the default ENGINE Page upon exceedance of specific parameters which are listed in Table 7.1.1. Parameter Fuel Flow GPH Cylinder Head Temperature Oil Temperature Oil Pressure Alternator 1 Load Alternator 2 Load Bus 1 Volts Bus 2 Volts Left Fuel Quantity Right Fuel Quantity Exceedance Greater than 27.
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.
ENGINE INDICATION SYSTEM CHT Indicator Voltmeter 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. The Voltmeter displays the primary bus voltage. The Voltmeter displays two (2) pointers which indicate the voltage for Buses 1 and 2.
ENGINE INDICATION SYSTEM Manifold Pressure Gauge Tachometer Fuel Flow Leaning Pointer Fuel Flow Indicator Cylinder Head Temperature Indicator Oil Temperature Indicator Oil Pressure Indicator Ammeter Voltmeter Fuel Quantity Indicator Figure 7.2.1 ENGINE Page 190-00550-00 Rev.
ENGINE INDICATION SYSTEM 7.3 LEAN PAGE The Lean Page is accessible by pressing the LEAN softkey. A digital readout for fuel flow resides below the tachometer. Beneath the fuel flow indication are bar graphs and numeric readouts for exhaust gas temperature (EGT) and cylinder head temperature (CHT) in degrees Fahrenheit. The temperature deviation from peak resides above the EGT graph.
ENGINE INDICATION SYSTEM Manifold Pressure Gauge Tachometer Fuel Flow Indicator Cyan Line Representing Peak EGT Readout For Selected Cylinder CHT Readout For Selected Cylinder Temperature Deviation From Peak Exhaust Gas Temperature Bar Graph Cylinder Head Temperature Bar Graph Figure 7.3.1 LEAN Engine Page 190-00550-00 Rev.
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. System 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.
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.
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