Honeywell SPZ-8000 Pilot's Manual page 55

Digital integrated flight control system
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Marker Beacon -- Marker beacon information is displayed in the
D
upper right corner of the EADI. The marker annunciators are
for outer marker,
marker.
Altitude Preselect Display -- The five--digit display indicates the
D
altitude from 0 to 60,000 feet that is selected using the ALT SEL
knob on the copilot's instrument remote controller. The resolution is
100 feet. The ASEL annunciator and box are cyan. The box turns
yellow
if altitude preselect is controlled by the cross--side DADC as
indicated by the flight director couple arrow. The power--up display
is the ASEL flag until the ASEL knob is turned, then the current value
of ASEL is displayed.
Vertical Track Alert (VTA) Annunciator -- With FMS selected, the
D
VTA
annunciator flashes approximately 60 seconds before the
aircraft reaches the vertical waypoint.
Vertical or Glideslope Deviation Pointer -- The vertical deviation
D
pointer and scale are displayed when VNAV mode is selected. The
vertical deviation pointer indicates the VNAV computed path center
that the aircraft is to fly. The glideslope pointer and scale are
displayed when an Instrument Landing System (ILS) frequency is
tuned. The scale and pointer display aircraft deviation from
glideslope beam center. The glideslope deviation pointer indicates
the glideslope beam center that the aircraft is to fly.
NOTE:
When back course is selected on the flight guidance
controller, the glideslope deviation scale and pointer are
removed.
Aircraft Symbol -- The symbol serves as a stationary
D
representation of the aircraft. Aircraft pitch and roll attitudes are
displayed by the relationship between the fixed miniature aircraft
and the movable sphere. The aircraft is flown to align the aircraft
symbol to the command cue to satisfy the commands of the selected
flight director mode.
A28--1146--055
REV 2
SPZ--8000 Digital Integrated Flight Control System
MM
for middle marker, and IM (white) for inner
Electronic Flight Instrument System (EFIS)
OM
4-11

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