Honeywell SPZ-8000 - NAV Source Reversions

SPZ--8000 Digital Integrated Flight Control System
A28--1146--055
REV 2
4-27
Electronic Flight Instrument System (EFIS)
AD--58069@
Flight Director Reversionary Mode, Couple Arrow
Figure 4--20
NAV Source Reversions
NAV source reversions are performed using the V/L and FMS buttons
on the display controller . Repeatedly pushing the V/L or FMS buttons
scrolls through the available NAV sources. The NAV source reversions
are indicated by annunciating the NAV source (VOR 1, VOR 2, LOC 1,
LOC 2, FMS 1, FMS 2) and by changing the following annunciators and
displays from green to yellow on the side where transfer is performed.
(These functions are on the EHSI unless otherwise specified.)
D NAV source annunciator
D BC annunciator
D Rising runway pointer (EADI)
D Vertical deviation pointer (EADI and EHSI)
D CRS/DTK arrow and digital display
D TO/FROM display
D Distance to WPT/DME, distance annunciator, and identifier
D Tim e-- t o-- go
D FMS route and WPT/VOR/DME symbols (MAP format)
D Cross track distance readout (MAP format).
There is no annunciation or color change on the other side.