Honeywell PRIMUS 1000 - Engine T;O Mode Logic; Engine T;O Status Arrow; Environmental Control System;Anti-Ice (Ecs A;I)

PRIMUSr 1000 Integrated Avionics System
A28--1146--112--00
Electronic Flight Instrument System (EFIS)
4-88
Takeoff Mode 1 Takeoff Mode 2 Annunciation
0 0 T/O--1
0 1 ALT T/O--1
1 0 ALT T/O--2
1 1 ALT T/O--3
Engine T/O Mode Logic
Table 4--23
D Engine T/O Status Arrow -- This arrow moves up and down the
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.
AD--50948@
C
Environmental Control System (ECS)
System Display
Figure 4--51