Garmin Flight Deck 100 Manuel D’Utilisation
Embraer Prodigy
®
Flight Deck 100 Pilot’s Guide
190-00728-04 Rev. A
452
AUTOMATIC FLIGHT CONTROL SYSTEM
FLIGHT DIRECTOR MODES
Flight director modes are normally selected independently for the pitch and roll axes. Unless otherwise
specified, all mode keys are alternate action (i.e., press on, press off). In the absence of specific mode selection,
the flight director reverts to the default pitch and/or roll modes(s).
the flight director reverts to the default pitch and/or roll modes(s).
Armed modes are annunciated in white and active in green or magenta (if the mode reference is provided by
the GPS navigation function) in the AFCS Status Box. Under normal operation, when the control for the active
flight director mode is pressed, the flight director reverts to the default mode(s) for the axis(es). Automatic
transition from armed to active mode is indicated by the white armed mode annunciation moving to the active
mode field and flashing for 5 seconds.
flight director mode is pressed, the flight director reverts to the default mode(s) for the axis(es). Automatic
transition from armed to active mode is indicated by the white armed mode annunciation moving to the active
mode field and flashing for 5 seconds.
If the information required to compute a flight director mode becomes invalid or unavailable, the flight
director automatically reverts to the default mode for that axis. A flashing yellow mode annunciation indicates
loss of sensor (ADC) or navigation data (VOR, LOC, GPS, VNV, SBAS) required to compute commands. When
such a loss occurs, the system automatically begins to roll the wings level (enters Roll Hold Mode) or maintain
the pitch angle (enters Pitch Hold Mode), depending on the affected axis. The flashing annunciation stops
when the affected mode key is pressed or another mode for the axis is selected. After 5 seconds, if no action is
taken, the flashing annunciation stops and the flight director enters the default mode for the affected axis.
loss of sensor (ADC) or navigation data (VOR, LOC, GPS, VNV, SBAS) required to compute commands. When
such a loss occurs, the system automatically begins to roll the wings level (enters Roll Hold Mode) or maintain
the pitch angle (enters Pitch Hold Mode), depending on the affected axis. The flashing annunciation stops
when the affected mode key is pressed or another mode for the axis is selected. After 5 seconds, if no action is
taken, the flashing annunciation stops and the flight director enters the default mode for the affected axis.
Figure 7-3 Loss of VOR Signal
The flight director is automatically disabled if the attitude information required to compute the default flight
director modes becomes invalid or unavailable.
FLIGHT DIRECTOR SELECTION
The GFC 700 flight director can be coupled to either the pilot-side or copilot-side PFD data using the CPL
Key. When the pilot-side or copilot-side data source is changed, the vertical and lateral modes revert to default.
The autopilot follows the selected flight director only, indicated by an arrow pointing toward either the pilot or
copilot side, in the center of the AFCS Status Box.
The autopilot follows the selected flight director only, indicated by an arrow pointing toward either the pilot or
copilot side, in the center of the AFCS Status Box.
The currently active flight director may be turned off and the Command Bars removed from the displays
by pressing the active FD Key again. Pressing the FD Key for the inactive flight director only removes the
Command Bars from the corresponding display. The FD key for the selected flight director is disabled when
the autopilot is engaged.
Command Bars from the corresponding display. The FD key for the selected flight director is disabled when
the autopilot is engaged.
Figure 7-4 Flight Director Selection Indications
Pilot-side Flight Director Selected
Copilot-side Flight Director Selected