Display System Formats; Efis/Eicas System Components - Honeywell SPZ-8000 Maintenance Manual

Digital automatic flight control system for gulfstream iv
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2.
EDZ-884 Electronic Dis~lav Svstem
The cockpit's display system configuration is shown in Figure 201.
Each
pilot has a display controller and corresponding EFIS displays (PFD and ND).
The center panel houses the EICAS displays (ENGINE and CAS).
The remote
display unit dimming panel is located in the pedestal area.
A.
Display System Formats
Each display format
will be discussed in detail in the following
sections. Generally, the following four formats are available for
display in the GIV
system:
.
Primary
Flight
Display
(PFD)
Navigation
Display
(ND) - MAP,
COMPASS,
or PLAN
Engine
Instrument
Display
(EI)
Crew
Alerting
System
(CAS) With
System
Page Display
B.
EFIS/EICAS
System
Components
(1)
(2)
(3)
Display Units (DU)
The GIV system contains six color display units as shown in Figure
201. The DU is the media by which flight data is conveyed to both
the pilot and copilot.
Display Controllers (DC)
The GIV display system contains two display controllers. The DCS
are used to control the various display unit formats. Basically,
each pilot can control the formats for the on-side PFD and ND
displays in addition to the ENGINE and CAS displays.
Symbol Generators (SG)
The GIV display system has three symbol generators, each one
containing the four formats described in paragraph 2.A. The purpose
of the SG is to supply all the displayed data to the individual
display units in the system.
Each symbol generator has the
capability to drive all six display units in the event the other two
fail. With two or three SGS operational, all six display units have
unique formats displayed. With one SG operational, the
Copilot's
displays (PFD and ND) are repeaters of the pilot's displays.
Normally (3 SGS operational), SG 1 drives the pilot's displays, SG 2
drives the copilot's displays, and SG 3 drives the EICAS displays.
22-14-00
Page
202
Aug 15/91
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