Honeywell PRIMUS 1000 - Brake Temperature; Brake Temperature Limits; Electric Hydraulic Pump Status; Electrical (Elec) System

PRIMUSr 1000 Integrated Avionics System
A28--1146--112--00
4-93
Electronic Flight Instrument System (EFIS)
D Electric Hydraulic Pump Status -- The electric hydraulic pumps
can be switched ON and OFF. The ON/OFF status is shown onthe
display.
D Brake Temperature -- Brake temperature is displayed on vertical
analogscalesthatactasamonitorreference.Thepointerandscale
are green and remains green until the pointer enters the yellow
region. The color changes according to limits in table 4--28.
Color Range
Green Less than 200 °C
Amber More than 200 °C
Brake Temperature Limits
Table 4--28
ELECTRICAL (ELEC) SYSTEM
The electrical system display shown in figure 4--54, shows the dc
electrical block diagram. Bus voltage and amperage loads and battery
temperatures are shown.
AD--50951@
Electrical (ELEC) System Display
Figure 4--54