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& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES
INDEX
101202421232391214191316151718564711228
1NAV Frequency Box2Airspeed Indicator3Mach Number4Current Heading5Current Track Indicator6Course Deviation Indicator (CDI)7Horizontal Situation Indicator (HSI)8Ram Air Temperature (RAT)9ISA Temperature Deviation10Softkeys11System Time12Transponder Status Box13Selected Heading Bug14Turn Rate Indicator15Barometric Altimeter Setting16Vertical Speed Indicator (VSI)17Selected Altitude Bug18Altimeter19Selected Altitude20COM Frequency Box21Navigation Status Box22AFCS Status Box23Slip/Skid Indicator24Attitude Indicator
Figure 2-1 Primary Flight Display (Default)
190-00494-02 Rev. B Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 47
Flight Instruments
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS EICAS AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE AFCS ADDITIONAL
FEATURES APPENDICES INDEX
27314569148101215111316
1Traffic Annunciation2Flap Speed Reference3Selected Heading4Wind Data5Inset Map6DME Information Window7Bearing Information Windows8Timer/References Window9Minimum Descent Altitude/Decision Height10Selected Course11Required Vertical Speed12Current Vertical Speed13Vertical Deviation Indicator (VDI)14Comparator Window15VNV Target Altitude16AFCS Status Annunciation
Figure 2-2 Primary Flight Display (Additional Information)
48 Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 190-00494-02 Rev. B
Flight Instruments
SYSTEM
OVERVIEW
FLIGHT
AUDIO PANEL EICAS INSTRUMENTS
& CNS
FLIGHT
MANAGEMENT
HAZARD
ADDITIONAL AFCS AVOIDANCE
INDEX APPENDICES FEATURES
2.1 Flight Instruments
Airspeed Indicatorndicatorndicator Noteote: Refer to the Airplane Flight Manual (AFM) for speed criteria and Vspeed values. NOTE: VREF cannot be set above the indicated value for VAPR.
The Airspeed Indicator displays airspeed on a rolling number gauge using a moving tape. The numeric labels and major tick marks on the moving tape are marked at intervals of 10 knots, while minor tick marks on the moving tape are indicated at intervals of 5 knots. Speed indication starts at 20 knots, with 60 knots of airspeed viewable at any time. The actual airspeed is displayed inside the black pointer. The pointer remains black until reaching the high airspeed limit, at which point it turns red along with the Mach number readout.
The Mach number is displayed below the Airspeed Indicator (see Figure 2-1) for airspeeds at or above Mach 0.4 or at altitudes exceeding 27,120 feet. The color of the readout corresponds to the color of the actual airspeed pointer.
Figure 2-4 Red Pointer Showing OverspeedFigure 2-3 Airspeed IndicatorActual AirspeedAirspeed Trend VectorReference Approach SpeedVspeed References
Speeds above the maximum operating speed, VMO or MMO depending on aircraft altitude, appear in the high speed awareness range, represented on the airspeed tape by red/white barber pole coloration. An aural overspeed warning tone is generated if the airspeed exceeds the high airspeed limit.
A red low speed awareness band extends up to the low speed awareness velocity, VLSA. An aural stall warning is generated and the airspeed pointer turns red if the airspeed falls below VLSA. An open green circle on the airspeed tape represents 1.3VS1.
The Airspeed Trend Vector is a vertical, magenta line, extending up or down on the airspeed scale, located to the right of the color-coded speed range strip. The end of the trend vector displays approximately what airspeed will be reached in 6 seconds if the current rate of acceleration is maintained. If the trend vector crosses VLSA, or VMO/MMO, the text of the actual airspeed readout and the Mach readout changes to yellow. The trend vector is absent if the speed remains constant or if any data needed to calculate airspeed is not available due to a system failure.
190-00494-02 Rev. B Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 49
Flight Instruments
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS EICAS AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE AFCS ADDITIONAL
FEATURES APPENDICES INDEX
Flap extension maximum speed references (for takeoff/approach, TA, and landing, LD, conditions) are displayed as flags to the right of the Airspeed Indicator for altitudes below 18,000 feet. These flags cannot be turned off or modified. The airspeed pointer will turn red upon exceeding these speeds if the flaps are in the corresponding configuration.
Vspeeds can be changed and their flags along the right of the airspeed scale turned on/off. By default, all Vspeed values are reset and all flags turned off when power is cycled.
Figure 2-5 Flap Speed ReferencesVspeedFlagTakeoffV11VRRV22VENRELandingVAPRAPVREFRFTable 2-1 Vspeed Flag Labels
　
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