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To declutter the display, the following annunciators are removed when
an excessive attitude condition exists:
D
Vertical, lateral, and non–synched flight director mode annunciators
D
Flight director arrow
D
Low bank limit
D
Flight director command bars
D
Vertical deviation scale, pointer, and label
D
Vertical track alert annunciator
D
Marker beacons and box
D
Radio altitude digital readout
D
Selected airspeed bug
D
V
bug and readout
SPEED
D
Selected altitude bug and digital readout
D
All failure flags for items listed above
D
The following comparison monitor annunciators:
— Heading
— Radio altitude
— Localizer
— Glideslope
— ILS
D
Lateral transition box (that surrounds captured lateral or vertical
flight director modes).
Minimum altitude annunciator and box symbols are restored when the
following two conditions exist:
D
Roll attitude is less than 63_ left or right
D
Pitch attitude less than 28_ nose up or 18_ nose down.
A28–1146–134
REV 1 Jan/03
R
PRIMUS
1000 Integrated Avionics System
Electronic Flight Instrument System (EFIS)
3-75
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