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If there is a failure of one Audio Panel, the remaining one will not have access to the others side’s COM and NAV. For example, if the pilot side Audio Panel fails, the copilot side Audio Panel has access to all the radios except for COM1 and NAV1.
Reversionaryeversionary Mode
The red DISPLAY BACKUP Button selects the Reversionary Mode. See the System Overview Section for more information on Reversionary Mode.
Figure 4-56 Reversionary Mode Button
190-00494-02 Rev. B
Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang
137
Flight Managementanagement
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EICAS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES
INDEX
Section 5 Flight Managementanagement
5.1 Introduction
The G1000 is an integrated flight, engine, communication, navigation and surveillance system. This section of the Pilot’s Guide explains flight management using the G1000.
The most prominent part of the G1000 are the three full color displays: two Primary Flight Displays (PFD) and a Multi Function Display (MFD). The information to successfully navigate the aircraft using the GPS sensors is displayed on the PFD and the MFD. See examples in the Figure 5-1 and Figure 5-2. Detailed descriptions of flight management functions are discussed later in this section.
A brief description of the GPS navigation data on the PFD and MFD follows.
Navigation mode indicates which sensor is providing the course data (e.g., GPS, VOR) and the flight plan phase (e.g., Departure (DPRT), Terminal (TERM), Enroute (ENR), Oceanic (OCN), Approach (LNAV, LNAV+V, L/VNAV, or LPV), or Missed Approach (MAPR)).
The Inset Map is a small version of the MFD Navigation Map and can be displayed in the lower left corner of the PFD. When the system is in reversionary mode, the Inset Map can be displayed in the lower right corner. The Inset Map is displayed by pressing the INSET Softkey. Pressing the INSET Softkey again, then pressing the OFF Softkey removes the Inset Map.
The Navigation Map displays aviation data (e.g., airports, VORs, airways, airspaces), geographic data (e.g., cities, lakes, highways, borders), topographic data (map shading indicating elevation), and hazard data (e.g., traffic, terrain, weather). The amount of displayed data can be reduced by selecting the DCLTR Softkey. The Navigation Map can be oriented four different ways: North Up (NORTH UP), Track Up (TRK UP), Desired Track Up (DTK UP), or Heading Up (HDG UP).
An aircraft icon is placed on the Navigation Map at the location corresponding to the calculated present position. The aircraft position and the flight plan legs are accurately based on GPS calculations. The basemap upon which these are placed are from a source with less resolution, therefore the relative position of the aircraft to map features is not exact. The leg of the active flight plan currently being flown is shown as a magenta line on the navigation map. The other legs are shown in white.
There are 28 different map ranges available, from 500 feet to 2000 nm. The current range is indicated in the lower right corner of the map and represents the top-to-bottom distance covered by the map. To change the map range on any map, turn the Joystick counter-clockwise to zoom in ( -, decreasing), or clockwise to zoom out (+, increasing).
The Direct-to Window, the Flight Plan Window, the Procedures Window, and the Nearest Airports Window can be displayed in the lower right corner of the PFD. Details of these windows are discussed in detail later in the section.
Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang
190-00494-02 Rev. B
138
Flight Managementanagement
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EICAS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES
INDEX
Figure 5-1 GPS Navigation Information on the PFDLocation of:- Direct To Window- Flight Plan Window- Procedures Window- Nearest Airports WindowInset MapNavigation Status Box Navigation Mode
Figure 5-2 GPS Navigation Information on the MFD Navigation PageActive Flight Plan LegNavigation Map- Aviation Data- Geographic Data- Topographic Data- Hazard DataNavigation Status BoxAircraft Iconat Present PositionMap RangeMap OrientationFlight Plan Leg
190-00494-02 Rev. B Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 139
Flight Management anagement
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS EICAS AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE AFCS ADDITIONAL
FEATURES APPENDICES INDEX
Navigationavigationavigation Statustatustatus BoxBox
The Navigation Status Box located at the top of the PFD contains two fields displaying the following information:
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Cessna Citation Mustang Pilot’Guide 1(55)
