Engine T/O Mode Logic; Engine T/O Status Arrow; Environmental Control System/Anti--Ice (Ecs A/I) - Honeywell PRIMUS 1000 Pilot's Manual

PRIMUSr1000 Integrated Avionics System
Takeoff Mode 1
0
0
1
1
Engine T/O Status Arrow -- This arrow moves up and down the
D
three categories (T/O MODE, REF TO TEMP, and REF A--ICE) to
indicate a valid status condition. In the case of REF A--ICE, ON is
the valid condition.

ENVIRONMENTAL CONTROL SYSTEM/ANTI--ICE (ECS A/I)

The ECS display, shown in figure 4--51, displays the following information.
Environmental Control System (ECS)
Electronic Flight Instrument System (EFIS)
4-88
Takeoff Mode 2
0
1
0
1

Engine T/O Mode Logic

Table 4--23
C
System Display
Figure 4--51
Annunciation
T/O--1
ALT T/O--1
ALT T/O--2
ALT T/O--3
AD--50948@
A28--1146--112--00