Honeywell SPZ-8000 - Component Description; General; LASEREF@ II Inertial Reference System (IRS)

SECTION 2
COMPONENT DESCRIPTION
1. General
This section provides an illustration, leading particulars, a brief
descri~tion, and a block diaqram or schematic of each component used in the
System-. The information is ~nly for the specific standard components
in Section 1, Table 1.
The components are separated into the following subsystems:
Subsvstem Paraqrat)h
LASEREF@ II Inertial Reference System (IRS)
ADZ-81O Air Data System
AA-300 Radio Altimeter System
Reserved Subsystem Not Applicable to G-IV Aircraft
EDZ-884 Electronic Display System
DFZ-820 Dual Flight Guidance System
PRIMUS@ 800 Weather Radar System
PRIMUS@ 870 Weather Radar System
FMZ-800 Flight Management System (FMS)
Engine Pressure Ratio (EPR) System
Optional VLF/Omega System
Optional LSZ-850 Lightning Sensor System
Optional TCZ-91O Traffic Alert and Collision
Avoidance System (TCAS)
Optional MLZ-850 Microwave Landing System (MLS)
Optional Global Positioning System (GPS)
2
3
4
5
6
7
8
8.1
9
10
11
12
13
14
15
NOTE-
Refer to the contents section in the front of this manual for a
‘“ listing of each component contained in each subsystem.
1isteal
Page 101
Apr 15/93
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