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When the glideslope deviation is not valid, the vertical deviation limits are removed and the lateral
deviation limits are vertically centered on the FPV.
FLIGHT INSTRUMENTS
REV 51, Aug 14, 2006 Flight Crew Operating Manual
CSP 700−6
Volume 2
11−10−89
HUD SYMBOLOGY (CONT'D)
CAT 2 ILS Deviation Margin (Cont’d)
CAT 2 ILS
Deviation Margin
Lateral
Deviation
Scale
VNAV
Vertical
Deviation
Scale
CA 2 Annunciation
35
10
T
GF1110_088a
Lateral Deviation Scale
The lateral deviation scale is a conventional CDI scale that rotates with the course pointer
according to the course selected/desired track.
LOC Lateral Deviation
The LOC lateral deviation scale is a conventional CDI scale. The LOC lateral deviation is
displayed when the primary navigation source is LOC and a valid LOC frequency is tuned. The
LOC CDI is not displayed in TO or GA modes.
FMS Lateral Deviation
The FMS lateral deviation is a conventional CDI scale. The lateral deviation scale varies with the
FMS approach sensitivity as follows:
• ±5 NM when the lateral scale factor is not valid
• ±2 NM when the FMS approach sensitivity is set.
The FMS lateral deviation is displayed when the primary navigation source is FMS. The FMS
lateral deviation is not displayed in TO or GA modes.
FLIGHT INSTRUMENTS
Flight Crew Operating Manual REV 51, Aug 14, 2006
CSP 700−6
Volume 2
11−10−90
HUD SYMBOLOGY (CONT'D)
VOR Lateral Deviation
The VOR lateral deviation scale is a conventional CDI scale. The VOR CDI is displayed when the
primary navigation source is VOR. The VOR CDI is not displayed in TO or GA mode.
VOR/LOC/FMS
Deviation Scale
VOR
Deviation
Scale
GF1110_089a
Marker Beacon
The marker beacon annunciation is displayed below the airplane reference and blinks when
passing the outer, middle and inner marker beacons.
DME/FMS Distance Readout
The DME/FMS distance is located below the navigation source indication. The range is limited
from 0 through 4096 NM with a resolution of 1 NM above 100 NM and of 0.1 NM below 100 NM.
The distance information is associated with the primary navigation source indication as follows:
• VOR 1 or LOC 1 = DME 1 readout
• FMS 1 = FMS readout
• VOR 2 or LOC 2 = DME 2
• FMS 2 = FMS readout
DME HOLD Annunciation
The DME HOLD annunciation is indicated by an “H” displayed at the left of the DME/FMS distance
readout. It is displayed when the navigation source is VOR/LOC and DME HOLD has been
selected
FLIGHT INSTRUMENTS
REV 51, Aug 14, 2006 Flight Crew Operating Manual
CSP 700−6
Volume 2
11−10−91
HUD SYMBOLOGY (CONT'D)
Waypoint ID
The waypoint identification consists of a maximum of 6 letters located below the DME/FMS
distance readout. Depending on the navigation source selection, it displays the identifier of the
DME radio frequency selected by the pilot or the next FMS waypoint. The waypoint identification is
flashing when the it is overflown.
Marker Beacon Annunciation
DME/FMS
Distance Readout
DME HOLD
Annunciation
W
Identification
aypoint
GF1110_090a
Wind Data
The wind direction is displayed in vector format using a rotary arrow at the lower right side of the
airspeed tape.
The wind speed is displayed as a digital readout. The wind speed readout is enabled with wind
greater than 6 kt and is disabled when below 4 kt or when weight-on-wheels is applied.
GPWS Annunciations
The GPWS warning annunciations are located above the airplane reference. The windshear
caution annunciation WNDSHR CAUTION is annunciated without a box below the airplane
reference symbol.
The annunciations are displayed in the following priority:
Windshear Warning − WINDSHEAR
Command − PULL UP
Ground Proximity − GND PROX
Windshear Caution − WNDSHR CAUTION
FLIGHT INSTRUMENTS
Flight Crew Operating Manual REV 51, Aug 14, 2006
CSP 700−6
Volume 2
11−10−92
HUD SYMBOLOGY (CONT'D)
CAT 2
The CAT 2 status is located below the AP annunciation. It flashes for 5 seconds, then remains
steady during the approach as long as conditions remain. In the case of the loss of CAT 2
capability, the CAT 2 annunciation is boxed and striked through.
GPWS Annunciation
CAT2 Annunciation
Wind Data
GF1110_091
Overspeed Protection Annunciation
The overspeed protect annunciation is displayed when the Flight Director has entered the
　
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