Honeywell SPZ-8000 Pilot's Manual page 86

If TTG, GS, or ET is not available or invalid, the annunciator remains
displayed, but the digital readout is removed.
Reciprocal Course Pointer -- The reciprocal course pointer
D
indicates 180 from the course select pointer.
Reciprocal Course Preselect Pointer -- The reciprocal course
D
preselect pointer indicates 180 from the course preselect pointer.
Course Deviation Bar and Lateral Deviation Scale -- The course
D
deviation bar represents the centerline of the selected VOR or
localizer course and moves to the left or right of the course pointer
on the lateral deviation scale. The aircraft symbol shows aircraft
position relative to the selected course. In VOR operation, each dot
on either side of the aircraft symbol represents 5 deviation from
centerline. In ILS operation, each dot represents 1 deviation from
centerline. For FMS operation, each dot represents 2--1/2 miles
from desired track outside the terminal area. In the approach mode,
each dot represents 0.75 miles from desired track. The course
deviation is automatically reversed to properly sense deviation with
respect to the course centerline when one of the following occurs:
— When the back course (BC) mode is selected
— When tuned to a localizer frequency and the selected course is
more than 90 from aircraft heading.
The course deviation bar always indicates the location of the course
centerline relative to the nose of the aircraft.
Bearing Pointers -- The bearing pointers indicate relative bearing
D
to the selected NAVAID. Two bearing pointers are available and can
be selected to NAVAID or selected off from the display controller.
When the bearing pointer navigation source is invalid or a localizer
frequency is chosen, the respective bearing pointer is removed.
Bearing Pointer Source Annunciators -- The bearing source
D
annunciators
annunciator, indicate the current source of input to the bearing
pointers. The annunciator (A for ADF, V for VOR, and F for FMS) is
located inside the
Z Z Z Z for bearing pointer No. 2.
If the heading display is in TRU and FMS magnetic variation is
invalid, the VOR bearing V annunciator flashes continuously.
Course Preselect Annunciator (FMS) -- This annunciator
D
indicates the source of the course preselect information. The
annunciator is LOC 1 for the pilot's side and LOC 2 for the copilot's
side.
A28--1146--055
REV 2
SPZ--8000 Digital Integrated Flight Control System
(f f f f and Z Z Z Z (white)), located under the NAV source
for bearing pointer No. 1 and inside the white
f f f f
Electronic Flight Instrument System (EFIS)
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