Honeywell PRIMUS 1000 Pilot's Manual page 224

Integrated avionics system for embraer 145
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PRIMUSr1000 Integrated Avionics System
Step
2
The mode is armed, as shown in the display below.
3
The altitude flare point (ASEL capture) is dependent on
vertical speed, as shown in the display below.
Altitude Preselect Mode Procedure
Modes of Operation
8-36
Procedure
30
30
30
30
30
30
M
30
30
Table 8--10 (cont)
15500
40
153
20
00
3
2
1
0
1
2
3
A28--1146--112--00

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