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Honeywell PRIMUS 1000 - Page 224

Honeywell PRIMUS 1000
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PRIMUSr 1000 Integrated Avionics System
A28--1146--112--00
Modes of Operation
8-36
Step Procedure
2 The mode is armed, as shown in the display below.
3030
3030
3 The altitude flare point (ASEL capture) is dependent on
vertical speed, as shown in the display below.
15500
3030
3030
3
2
1
0
1
2
3
153
20
M
40
00
Altitude Preselect Mode Procedure
Table 8--10 (cont)

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