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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
Wind Data
Overspeed Protection Annunciation
The overspeed protect annunciation is displayed when the Flight Director has entered the 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.
Rev 7, Dec 01, 2005 Flight Crew Operating Manual Volume 2
TCAS Annunciation (Cont’d)
FMS Message Annunciation TCAS Target Zone
GF1110_092b
Volume 2 Flight Crew Operating Manual Rev 7, Dec 01, 2005
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)
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ALT for discrepancy of more than 200 feet
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HDG for discrepancy of more than 10 degrees
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GS or LOC for excessive deviation
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RAD for radio altitude miscompare.
Indicated Altitude Attitude
Airspeed
SPD
405 00F250
280
415 00
260
253
410 00240 405 00220
Glide Slope
Heading Localiser Radio Altitude
GF1110_093a
Rev 7, Dec 01, 2005 Flight Crew Operating Manual Volume 2
FLIGHT INSTRUMENTS
Power-up
Take-off
HDG T/O
ASEL
GF1110_095GF1110_094
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.
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