Autopilot Status Annunciations; Vertical Track Alert (Vta) Annunciation; Altitude Trend Vector - Honeywell PRIMUS 1000 Pilot's Manual

Integrated avionics system for embraer 145
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PRIMUSr1000 Integrated Avionics System
NOTES:
1. When the AHRS is in DG mode, the on--side
2. When the MAG heading is invalid, the source
Autopilot Status Annunciations -- Displays the engage status of
D
the autopilot. The annunciation is displayed above and left of center
of the attitude sphere. See table 4--7.
Autopilot Status
Engaged
Autopilot Test
Normal YD
Disconnect
Abnormal YD
Disconnect
Normal AP
disconnect
Abnormal AP
disconnect
Normal AP
disconnect in
CAT 2
Touch Control
Steering
Turn Knob Out of
Detent
Vertical Track Alert (VTA) Annunciation -- An amber VTA is
D
displayed above the vertical deviation scale when the FMS VNAV
is selected. The input is sent from the selected FMS.
Altitude Trend Vector -- The altitude trend vector is displayed when
D
the aircraft is in either a climb or a descent. The top of the vector
points to the altitude that the aircraft is at, if the current vertical speed
is maintained.
Electronic Flight Instrument System (EFIS)
4-32
heading source annunciations are DG1, DG2,
respectively.
annunciation is an amber HDG1 or HDG2.
Annunciation
AP
AP TEST
YD
YD
AP
AP/YD
AP
TCS
TKNB

Autopilot Status Annunciations

Table 4--7
Display Type
Steady
Steady
5 second flash
5 second steady
5 second flash
5 second flash,
then steady
5 second flash
Steady, while
TCS button is
held
Steady
A28--1146--112--00
Color
Green
Amber
Amber
Amber
Amber
Red
Red
White
Amber

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