Garmin Flight Deck 100 Manual De Usuario
190-00728-04 Rev. A
Embraer Prodigy
®
Flight Deck 100 Pilot’s Guide
465
AUTOMATIC FLIGHT CONTROL SYSTEM
VNV TARGET ALTITUDE CAPTURE MODE (ALTV)
VNV Target Altitude Capture is analogous to Selected Altitude Capture Mode and is armed automatically
after the VNV Key is pressed and the next VNV Target Altitude is to be intercepted before the Selected Altitude.
The annunciation ‘ALTV’ indicates that the VNV Target Altitude is to be captured. VNV Target Altitudes are
shown in the active flight plan or direct-to (with vertical constraint), and can be entered manually or loaded
from a database (see the Flight Management Section for details). At the same time as “TOD within 1 minute”
is annunciated in the Navigation Status Box, the active VNV Target Altitude is displayed above the Vertical
Speed Indicator (see Figure 7-14).
The annunciation ‘ALTV’ indicates that the VNV Target Altitude is to be captured. VNV Target Altitudes are
shown in the active flight plan or direct-to (with vertical constraint), and can be entered manually or loaded
from a database (see the Flight Management Section for details). At the same time as “TOD within 1 minute”
is annunciated in the Navigation Status Box, the active VNV Target Altitude is displayed above the Vertical
Speed Indicator (see Figure 7-14).
As the aircraft nears the VNV Target Altitude, the flight director automatically transitions to VNV Target
Altitude Capture Mode with Altitude Hold Mode armed. This automatic transition is indicated by the magenta
‘ALTV’ annunciation flashing for up to 5 seconds and the appearance of the white ‘ALT’ annunciation. The
active VNV Target Altitude is shown in magenta above the Vertical Speed Indicator.
‘ALTV’ annunciation flashing for up to 5 seconds and the appearance of the white ‘ALT’ annunciation. The
active VNV Target Altitude is shown in magenta above the Vertical Speed Indicator.
At 50 feet from the VNV Target Altitude, the flight director automatically transitions from VNV Target
Altitude Capture to Altitude Hold Mode and tracks the level leg. As Altitude Hold Mode becomes active, the
white ‘ALT’ annunciation moves to the active vertical mode field and flashes magenta for 5 seconds to indicate
the automatic transition. The flight director automatically arms Vertical Path Tracking, allowing upcoming
descent legs to be captured and subsequently tracked.
white ‘ALT’ annunciation moves to the active vertical mode field and flashes magenta for 5 seconds to indicate
the automatic transition. The flight director automatically arms Vertical Path Tracking, allowing upcoming
descent legs to be captured and subsequently tracked.
Figure 7-17 VNV Altitude Capture
Flash Up to 5 sec, Indicating Automatic Transition
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arget
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ltitUDe
NOTE:
Pressing the CWS Button while in VNV Target Altitude Capture Mode does not cancel the mode.
Changing the current VNV Target Altitude while VNV Target Altitude Capture Mode is active causes the
flight director to revert to Pitch Hold Mode. Vertical Path Tracking and the appropriate altitude capture
mode are armed in preparation to capture the new VNV Target Altitude or the Selected Altitude, depending
on which altitude is to be intercepted first.
mode are armed in preparation to capture the new VNV Target Altitude or the Selected Altitude, depending
on which altitude is to be intercepted first.
VNV target altitudes can be changed while editing the active flight plan (see the Flight Management
Section for details).
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ontrol
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Current Speed Control (if available) can be engaged if the the autopilot is engaged and Altitude Hold Mode
(ALT) or VNV Target Altitude Capture (ALTV) Mode is active. When the CSC Key is pressed, the Full Authority
Digital Engine Control (FADEC) varies engine thrust to maintain the desired Airspeed Reference (green Airspeed
Reference Bug), within a certain control range.
Digital Engine Control (FADEC) varies engine thrust to maintain the desired Airspeed Reference (green Airspeed
Reference Bug), within a certain control range.
NOTE:
For CSC engagement and disengagement detailed conditions, see the approved Pilot’s Operating
Handbook (POH).