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Fuel quantity for each tank is normally shown along a slider scale with readouts below for each tank and the total. The fuel flow readout for each engine is shown below the fuel quantity and the fuel temperature is displayed under this. Only readouts are given in reversionary mode and total fuel quantity is not shown.
Tank FuelQuantitiesTotal FuelQuantityFuelTemperatureFigure 3-9 Fuel Display (Normal Mode)Fuel Flow
86 Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 190-00494-02 Rev. B
Engine Indication ndication & Crew Alerting System ystem
SYSTEM
OVERVIEW
FLIGHT
AUDIO PANEL EICAS INSTRUMENTS
& CNS
FLIGHT
MANAGEMENT
HAZARD
ADDITIONAL AFCS AVOIDANCE
INDEX APPENDICES FEATURES
Interstagenterstagenterstage Turbine Temperatureemperature
Interstage Turbine Temperatures (ITT) are displayed along a slider scale in °C. ITT values and limits are obtained from the FADEC. ITT is shown in the same format in display reversionary mode. During normal operations, the sliders appear in white and no readout is shown. Readouts are provided for each engine below the scale during engine start, for values below 200°C, or for caution and warning values. When the respective engine ignitors are on, ‘IGN’ appears in green text at the top of the ITT scales.
Ignitor OnIndicationWarningLineFigure 3-10 Interstage Turbine Temperature Display
Electrical Displayisplay
Voltage and current for the direct current (DC) generators and battery are obtained directly from the electrical system buses. Generator voltages and currents are normally shown along color-coded scales, with readouts below. Battery voltage and current are displayed as readouts. In reversionary mode, battery current is not shown.
GeneratorVoltageGeneratorCurrentBattery CurrentBattery VoltageFigure 3-11 Electrical Display (Normal Mode)
190-00494-02 Rev. B Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 87
Engine Indication ndication & Crew Alerting System ystem
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS EICAS AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE AFCS ADDITIONAL
FEATURES APPENDICES INDEX
Pressurizationressurization Displayisplay
Cabin pressurization information (cabin altitude and rate of change, destination elevation, differential cabin pressure) is shown beneath the electrical display. Only cabin altitude and the pressure differential readouts are displayed in reversionary mode.
Cabin altitude is shown on a color-coded scale labeled in 5,000-ft increments with a readout (in feet) below (unless on the ground). The cabin altitude scale and corresponding “CABIN ALT” CAS messages shift up to higher altitude when in high altitude pressurization mode. High altitude mode is active whenever all the following are true:
• The takeoff or destination elevation is above 8,000 feet
• The aircraft altitude is less than 24,500 feet
• The pressurization system has verified the conditions
Cabin altitude change rate is displayed on a scale in terms of 1,000-fpm increments with a readout (in fpm) below. Cabin pressure differential (DIFF PSI), in pounds per square inch (psi), is indicated on a color-coded scale with a readout.
PressureAltitudeDestinationElevationPressureDifferentialPressureChange RateFigure 3-12 Cabin Pressure Display (Normal Mode)
88 Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 190-00494-02 Rev. B
Engine Indication ndication & Crew Alerting System ystem
SYSTEM
OVERVIEW
FLIGHT
AUDIO PANEL EICAS INSTRUMENTS
& CNS
FLIGHT
MANAGEMENT
HAZARD
ADDITIONAL AFCS AVOIDANCE
INDEX APPENDICES FEATURES
The destination elevation (from -1,000 to 14,000 feet) entered in the PFD Timer/References Window is displayed below the cabin altitude readings. This value is retained by the G1000 on power-down.
Setting the destination elevation:
1) Press the TMR/REF Softkey.
2) Turn the large FMS Knob to highlight the ‘DEST ELV’ field.
3) Use the small FMS Knob to enter the destination elevation (in 10-ft increments from -1,000 to 14,000 feet).
4) To remove the window, press the CLR Key or the TMR/REF Softkey.
DestinationElevationFigure 3-13 Timer/References Window
Trim and Flap Indicatorsndicatorsndicators
Lateral trim indications are shown along a slide bar scale beneath the pressurization display in normal display mode. Aileron trim is displayed at the top of the scale and rudder trim is displayed at the bottom. The trim display is not present in reversionary mode.
Flap deflection is normally displayed beneath the trim indications using a rotating pointer. Flap positions for takeoff/approach, landing, and up positions are labeled. In reversionary mode, a digital readout of the flap position (UP, TO/APR, LAND) is provided.
　
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