Hardware Id Page 1 - Honeywell PRIMUS 1000 Pilot's Manual

R
PRIMUS 1000 Integrated Avionics System
Table 7–2 describes the procedure to access hardware and software
ID pages.
Step
1 Set the RA knob on the display controller to 640.
2 Push and hold the TEST button for at least 5–7 seconds.
3 While holding the TEST button, push and release PB #4.
4 Release the TEST button. HW (hardware) ID 1 is
displayed, as shown in Figure 7–2.
Maintenance Test and Hardware/Software
Identification Page Access Procedure
Troubleshooting
7-4
Procedure

Hardware ID Page 1

Figure 7–2
Table 7–2 (cont)
AD–23175@
A28–1146–134
REV 1 Jan/03