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Figure 2-14 Baro Sync Setting (AUX - System Setup Page)
56 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
A Baro Transition Alert is provided to alert the pilot to change the barometric pressure setting when crossing the transition altitude (in either direction). This is displayed by the barometric pressure setting flashing light blue when crossing the transition altitude.
Setting the Baro Transition Alert:
1) Use the FMS Knob to select the AUX - System Setup Page.
2) Press the FMS Knob to activate the cursor.
3) Turn the large FMS Knob to highlight ON or OFF in the Baro Transition Alert box.
4) Turn the small FMS Knob to turn the alert OFF or ON and press the ENT Key.
5) With the altitude field highlighted, turn the small FMS Knob to set desired altitude and press the ENT Key.
6) To cancel the selection, press the FMS Knob.
Figure 2-15 Baro Transition Alert(AUX - System Setup Page)
190-00494-02 Rev. B Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 57
Flight Instruments
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS EICAS AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE AFCS ADDITIONAL
FEATURES APPENDICES INDEX
Vertical Speed Indicatorndicatorndicator (VSI)
The Vertical Speed Indicator (VSI) displays the aircraft vertical speed with numeric labels and tick marks at 2000 and 4000 fpm in each direction on the non-moving tape. Minor tick marks are at intervals of 1000 fpm. The current vertical speed is displayed in the pointer, which also points to that speed on the non-moving tape. Digits appear in the pointer when the climb or descent rate is greater than 100 fpm. If the rate of ascent/descent exceeds 4000 fpm, the pointer appears at the corresponding edge of the tape and the rate appears inside the pointer.
A magenta chevron is displayed as the Required Vertical Speed Indication (RVSI) for reaching a VNV Target Altitude once the “TOD [Top of Descent] within 1 minute” alert has been generated. See the Flight Management and AFCS sections for details on VNV features, and refer to Section 2.2, Supplemental Flight Data, for more information about VNV indications on the PFD.
Vertical Deviationeviation
The Vertical Deviation Indicator (VDI) uses a magenta chevron to indicate the baro-VNV vertical deviation when Vertical Navigation (VNV) is being used; the VDI appears in conjunction with the “TOD within 1 minute” alert. Full-scale deflection (two dots) is 1000 feet. The VDI is removed from the display if vertical deviation becomes invalid. See the Flight Management and AFCS sections for details on VNV features, and refer to Section 2.2, Supplemental Flight Data, for more information about VNV indications on the PFDs.
The Glideslope Indicator appears to the left of the Altimeter whenever an ILS frequency is tuned in the active NAV field. A green diamond acts as the Glideslope Indicator, like a glideslope needle on a conventional indicator. If a localizer frequency is tuned and there is no glideslope, “NO GS” is annunciated.
The glidepath is analogous to the glideslope for GPS approaches supporting WAAS vertical guidance (LNAV+V, LNAV/VNAV, LPV) and is generated by the system to reduce pilot workload during approach. When an approach of this type is loaded into the flight plan and GPS is the selected navigation source, the Glidepath Indicator appears as a magenta diamond. If the approach type downgrades past the final approach fix (FAF), “NO GP” is annunciated.
Figure 2-16 Vertical Speed and Deviation Indicators (VSI and VDI)Vertical Deviation IndicatorVNV Target AltitudeVertical Speed IndicatorVertical Speed PointerRequiredVertical Speed Indicator Figure 2-17 Glideslope IndicatorMarker Beacon AnnunciationGlideslope IndicatorFigure 2-18 Glidepath IndicatorGlidepath Indicator
58 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
Horizontalorizontal Situationituationituation Indicatorndicatorndicator (HSI)
The Horizontal Situation Indicator (HSI) displays a rotating compass card in a heading-up orientation. Letters indicate the cardinal points and numeric labels occur every 30˚. Major tick marks are at 10˚ intervals and minor tick marks at 5˚ intervals. The HSI presents heading, turn rate, course deviation, bearing, and navigation source information in a 360˚ compass-rose format.
The HSI contains a Course Deviation Indicator (CDI) with a course pointer arrow, a To/From arrow, a sliding deviation bar, and scale. The course pointer is a single line arrow (GPS, VOR1, and LOC1) or a double line arrow (VOR2 and LOC2) which points in the direction of the set course. The To/From arrow rotates with the course pointer and is displayed when the active NAVAID is received.
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Cessna Citation Mustang G1000 Integrated Flight Dec(28)
