System On--Off Page - Honeywell PRIMUS 1000 Pilot's Manual

PRIMUSr1000 Integrated Avionics System
ALL SWITCHES POSITIONED ON THIS PAGE REMAIN IN
THE SAME STATUS AFTER POWER DOWN. THE RADIO PRE-
FLIGHT SHOULD INCLUDE THE RADIO ON--OFF PAGE TO EN-
SURE THAT ALL MODULES ARE ON. A SWITCH LEFT OFF IS INDI-
CATED BY DASHES IN THE CORRESPONDING FREQUENCY
WINDOW ON THE MAIN PAGE, AND BY AN ERROR MESSAGE FOR
THE TURNED--OFF MODULE DURING POWER--ON SELF--TEST.
NOTES: 1. This feature is dependent upon installation, but
2. Single DME and ADF installations have their
â
PRIMUS II Radio System
C--12
CAUTION

System On--Off Page

Figure C--5
typically only one side' s COM and NAV is wired for
ON--OFF controls. The COM and NAV (VOR) that are
the emergency radios (and, therefore, cannot be
turned ON or OFF) have an N/A annunciation in place
of ON or OFF. In some installations, the RMU can be
inhibited from calling up the RADIO ON--OFF page.
respective ON--OFF functions removed from the No.
2 RMUs radio ON--OFF page.
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