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OBSTACLE, OBSTACLE
PULL UP, PULL UP
NOTE
If in PLAN mode and auto pop.up occurs, MFD format will automatically change to MAP mode, with the terrain map displayed.
WARNING LOOK AHEAD
Volume 2 Flight Crew Operating Manual Rev 2A, Apr 11, 2005
Annunciations
All terrain annunciations are displayed on the MFD. The annunciations are as follows:
BLANK:TERR not selected.
TERR: TERR has been selected.
TERR TEST: Indicates a self-test.
TERR FAIL: Indicates internal failure, or loss of communication with EFIS.
CNTRL FAIL: Indicates loss of range control for terrain map. TERR N/A: Position Uncertain.
: Terrain sytem selected OFF, using the switch selection on the overhead panel.
NOTE
In a case where landing at an airport that is not in the database, all TERRAIN functions can be inhibited, by selecting the TERRAIN switch, located on the overhead panel.
GF1710_087
Terrain Clearance Floor (TCF)
The TCF function supplements the GPWS function by providing an additional terrain clearance alert envelope around airports. The TCF criteria is used to determine alert and warning envelopes.
TCF creates an increasing terrain clearance envelope around the intended airport runway directly related to the distance from the runway. TCF alerts are based on current airplane location, nearest runway center point position and radio altitude, along with an internal database that includes all worldwide, hard-surfaced runways greater than 3500 feet in length.
Penetration of the alert envelope will generate an aural “TOO LOW TERRAIN”and a GND PROX message is displayed on the PFD. The aural alert is repeated twice and again thereafter if the radio altitude value decreases by more than 20% from the altitude at which the initial warning was issued. The GND PROX message remains displayed until the airplane exits the alert envelope.
TOO LOW
TERRAIN
DISTANCE TO SELECTED RUNWAY (NM)
Rev 2A, Apr 11, 2005 Flight Crew Operating Manual Volume 2
Volume 2 Flight Crew Operating Manual Rev 2A, Apr 11, 2005
The FMS performs the functions of navigation, flight planning and guidance of the airplane. The FMS is a full flight regime in both Lateral Navigation (LNAV) and Vertical Navigation (VNAV).
There are two Control Display Units (CDU), located on the pedestal. A third FMS (optional) can also be installed on the pedestal. The displayed data is shown in the following colours:
CYAN
GREEN
YELLOW
MAGENTA
ORANGE
WHITE
(Vertical & Atmospheric Data).
(Lateral and Index Sections).
(FROM Waypoint).
(TO Waypoint).
(Flight Plan Names).
(Prompts and Titles).
GF1710_091
FMS Display Unit
The CDU is a full color Liquid Crystal Display (LCD) capable of displaying video from various external sources and can offer other graphical capabilities.
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