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maximum airspeed mode.
FMS Message Annunciation
This annunciation is displayed when there is a message on the FMS CDU.
TCAS Annunciation
A TCAS target zone is displayed on the HUD in relation to the FPV. When the airplane is below
1100 ft radio altitude or when the TCAS is manually selected to TA, a TA ONLY annunciation is
posted on the HUD.
During Resolution Advisories (RA), the TCAS avoidance zone is displayed. A flight path correction
is needed when the avoidance zone is flashing. The TCAS Resolution Advisory is not displayed in
case of excessive airplane attitude. The HSI is removed to avoid clutter in TCAS RA scenarios.
The FD cue is removed to avoid misleading or incoherent guidance.
A boxed TCAS RA annunciation is posted above the airplane reference when the TCAS test is
activated.
FLIGHT INSTRUMENTS
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CSP 700−6
Volume 2
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HUD SYMBOLOGY (CONT'D)
TCAS Annunciation (Cont’d)
Overspeed Protection Annunciation
FMS Message Annunciation TCAS Target Zone
−600VS
GF1110_092b
FLIGHT INSTRUMENTS
Flight Crew Operating Manual REV 51, Aug 14, 2006
CSP 700−6
Volume 2
11−10−94
HUD SYMBOLOGY (CONT'D)
Miscompare/Failure Annunciation
The miscompare/failure annunciations are boxed and remains steady as long as the miscompare
condition exists or the applicable data is invalid.
A miscompare annunciation is indicated by a sensor flag and the corresponding parameter
remains displayed (e.g. IAS boxed: speed readout and tape in view).
A failure annunciation is indicated by a flag and the removal of the associated data (e.g. ADC
boxed: speed readout and tapes removed).
The following annunciations can be displayed:
• ATT for discrepancy in pitch > 5 degrees or in roll > 6 degrees
• IAS for discrepancy of more than 20 knots (for IAS > 60 knots)
• ALT for discrepancy of more than 200 feet
• HDG for discrepancy of more than 10 degrees
• GS or LOC for excessive deviation
• RAD for radio altitude miscompare.
Attitude
Heading Localiser
Glide Slope
Indicated
Airspeed
Altitude
Radio Altitude
415 00
405 00
410 00
SPD
F250
280
260
253
240
220
405 00
GF1110_093a
FLIGHT INSTRUMENTS
REV 51, Aug 14, 2006 Flight Crew Operating Manual
CSP 700−6
Volume 2
11−10−95
FLIGHT PROFILE
Power-up
GF1110_094
Take-off
T/O
ASEL
HDG
GF1110_095
When the Flight Director is in the take-off mode and the nose wheel is off the ground, the pitch
scale changes to a pitch target. The take-off mode pitch target is normally set at 17.5 degrees;
however, if an engine failure is detected, it is reset automatically to 13 degrees.
The aircraft symbol is superimposed on the roll and pitch scale to provide airplane attitude
reference.
FLIGHT INSTRUMENTS
Flight Crew Operating Manual REV 51, Aug 14, 2006
CSP 700−6
Volume 2
11−10−96
FLIGHT PROFILE (CONT'D)
Cruise
GF1110_096a
Approach CAT I
GF1110_097a
FLIGHT INSTRUMENTS
REV 51, Aug 14, 2006 Flight Crew Operating Manual
CSP 700−6
Volume 2
11−10−97
FLIGHT PROFILE (CONT'D)
Approach CAT II
GF1110_098a
FLIGHT INSTRUMENTS
Flight Crew Operating Manual REV 51, Aug 14, 2006
CSP 700−6
Volume 2
11−10−98
FLIGHT PROFILE (CONT'D)
Excessive Attitude
The excessive attitude format is used in the following conditions:
• Roll is greater than 65° or less than −65°
• Pitch is greater than 29° or less than −20°
The excessive attitude format is kept until the Roll is between ±63° and the Pitch is between 28°
and −18°.
To enable the pilot to focus on the essential parameters for the excessive attitude recovery, some
parameters (for example, navigation information) are removed to provide a decluttered display.
When an excessive attitude occurs, a sphere is included in the center of the FPV. The sphere has
3 positions according to Pitch angle:
• One third illuminated when Pitch is greater than 5°
• One half illuminated when Pitch is between ±5°
• Two thirds illuminated when Pitch is lower than −5°.
When excessive attitude occurs, chevrons are displayed each 10° from 30° to 80° and from −20°
to −80° on the pitch tape, and a roll command is displayed around the FPV. The roll command
　
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