Honeywell SPZ-8000 - General; System Components; System Description

SECTION 1
SYSTEM DESCRIPTION
1.
General
The SPZ-8000 Digital Automatic Flight Control System (Figure 1) provides
flight director, autopilot, pitch trim, Mach trim,
system operates in conjunction with the electronic
consists of the primary flight displays (PFD), the
and the engine instrument and crew alerting system
Table 1 lists the components and part numbers that
Figure 2 shows the approximate component locations
installation.
and autothrottle.
The
display system (EDS) that
navigation displays (ND),
(EICAS) displays.
compose a System, and
for a Gulfstream IV
A/C
Honeywell
Ref
System Component
Qty Part No.
Des
AZ-81O Digital Air Data Computer
2 7000700-964,
9[C9
-864 (CAA or
ASC 61)
FZ-820 Flight Guidance Computer
2
7003974-905(PHASE 2) lo/clo
-906 ****
_907 ****
~:
The -907 FZ-820 Flight Guidance Computers were factory installed
on aircraft 1198 and subsequent.
GP-820 Flight Guidance Controller
1 7007546-901/-902* 11
SM-600 Dual Servo (Aileron)
1 4015373-705
12
SB-600 Servo Bracket (Aileron)
1
4015374-905
N/A
SM-600 Dual Servo (Elevator)
1 4015373-704
13
SB-600 Servo Bracket (Elevator)
1 4015”374-904
N/A
RT-300 Radio Altimeter Receiver
2 7001840-922
20/c20
Transmitter
AT-222 Antenna (Receive)
2 4007637-002
21/c21
System Components
Table 1
22-14-00
Page 1
Apr 15/93
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