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11876439113121025151614Figure 2-19 Horizontal Situation Indicator (HSI)1Turn Rate Indicator2Selected Heading3Current Track Indicator4Lateral Deviation Scale5Navigation Source6Aircraft Symbol7Course Deviation Indicator (CDI)8Rotating Compass Rose9To/From Indicator10Course Pointer11Selected Heading Bug12Flight Phase13Selected Course14Turn Rate/HeadingTrend Vector15Current Heading16Lubber Line
190-00494-02 Rev. B Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 59
Flight Instruments
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS EICAS AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE AFCS ADDITIONAL
FEATURES APPENDICES INDEX
A digital reading of the current heading appears on top of the HSI. The current track is represented on the HSI by a magenta diamond bug. To the upper left of the HSI, the Selected Heading is shown in light blue; the light blue bug on the compass rose corresponds to the Selected Heading. The Selected Course is shown to the upper right of the HSI. The color of the Selected Course corresponds to the selected navigation source: magenta for GPS or green for NAV (VOR, LOC).
SelectedHeadingBugSelectedCourseSelectedHeadingCurrent TrackIndicatorFigure 2-20 Heading and Course IndicationsCurrent Heading
Adjusting the Selected Heading:
Turn the HDG Knob to set the Selected Heading on both PFDs.
Press the HDG Knob to synchronize the bug to the current heading.
Adjusting the Selected Course:
Turn the CRS Knob to set the Selected Course (for each PFD).
Press the CRS Knob to re-center the CDI and return the course pointer to the bearing of the active waypoint or navigation station (see OBS Mode for adjusting a GPS course).
The heading displayed on the HSI and all other navigation angles (track, heading, course, bearing) are magnetic when the NAV ANGLE is set to Magnetic on the AUX - System Setup Page. When True is selected, all navigation angles and the HSI display a T next to the angle value. When an approach referenced to true north has been loaded into the flight plan, the system generates a message alerting the pilot to switch the NAV ANGLE setting to True at the appropriate time.
Figure 2-21 Heading and Course Indications (True)
60 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
Changing the navigation angle setting:
1) Use the FMS Knob to select the AUX - System Setup Page on the MFD.
2) Press the FMS Knob to activate the cursor.
3) Turn the large FMS Knob to highlight Nav Angle in the Display Units box.
4) Turn the small FMS Knob to highlight the desired setting and press the ENT Key.
Figure 2-22 Navigation Angle Settings(AUX - System Setup Page)
190-00494-02 Rev. B Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 61
Flight Instruments
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS EICAS AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE AFCS ADDITIONAL
FEATURES APPENDICES INDEX
Turn Rateate Indicatorndicatorndicator
The Turn Rate Indicator is located directly above the rotating compass card. Tick marks to the left and right of the lubber line denote half-standard and standard turn rates. A magenta Turn Rate Trend Vector shows the current turn rate. The end of the trend vector gives the heading predicted in 6 seconds, based on the present turn rate. A standard-rate turn is shown on the indicator by the trend vector stopping at the standard turn rate tick mark, corresponding to a predicted heading of 18˚ from the current heading. At rates greater than 4 deg/sec, an arrowhead appears at the end of the magenta trend vector and the prediction is no longer valid.
Figure 2-23 Turn Rate Indicator and Trend VectorHalf-std Turn RateStd Turn RateArrow Shown for Turn Rate > 4 deg/sec
Bearing Pointers and Informationnformation Windowsindows
Two bearing pointers and associated information can be displayed on the HSI for NAV, GPS, and ADF sources. The pointers are light blue and are single- (BRG1) or double-lined (BRG2); an icon is shown in the respective information window to indicate the pointer type. The bearing pointers never override the CDI and are visually separated from the CDI by a white ring (shown when bearing pointers are selected but not necessarily visible due to data unavailability).
Figure 2-24 HSI with Bearing and DME InformationBearing 2 Information WindowNo Waypoint SelectedPointer IconBearing SourceBearing 1 Information WindowPointer IconDistance to Bearing SourceBearing SourceBearing 2 PointerBearing 1 PointerFrequencyTuning ModeDistanceStation IdentifierDME Information Window
When a bearing pointer is displayed, its associated information window is also displayed. The Bearing Information windows (Figure 2-24) are displayed to the lower sides of the HSI and show:
　
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