Navigation Sensors Interface; Pz-800 Performance Computer Interface; Vor; Ils/Mls - Honeywell SPZ-8000 Maintenance Manual

Digital automatic flight control system for gulfstream iv
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6.
B.
(8) Navigation Sensors Interface
MAINTENANCE
MANUAL
GULFSTREAM
IV
The following independent navigation
sensors
are interfaced
with
the
symbol generators via ARINC 429:
VOR
G
ILS/MLS
DME
ADF
LASEI?TRAK'" (optional)
.
TCAS (optional)
(a) VOR
The
VOR navigation
sensors
provide
the
symbol
generators
with
bearing
and frequency
information
for display.
The
symbol
generators generate lateral deviation for both display and
transmission
on the ASCB.
(b)
ILS/MLS
The
ILS navigation sensors provide
the
symbol
generators
with
lateral
deviation,
vertical
deviation,
and frequency
information
for display.
The symbol generator transmits
lateral and vertical deviation to the FZ-820 Flight Guidance
Computer
over
the ASCB.
(c)
DME
The DME sensors
provide
distance
and frequency
information
for
display. Distance information is transmitted over the ASCB for
utilization by the FZ-820 Flight Guidance Computers.
(d) ADF
The ADF
sensors
provide
the symbol
generators
with
bearing
and
frequency
information
for display
purposes
only.
(e) LASERTRAKW
The LASERTRAKN Navigation Display Unit may be configured to
provide additional outputs for display purposes only.
(f) TCAS
The optional TCAS Computer provides the symbol generators with
traffic advisories, resolution advisories, performance
resolution advisories, and map data for display.
(9)
PZ-800 Performance Computer Interface
The PZ-800 Performance Computer provides autothrottle mode status
and priority select information. This information is provided on
both"PFDs.
22-14-00
Page 160
Apr 15/93
Use or disclosure
of informationon
this page is subject
to the restrictions
onthe
title page of this document.

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