Honeywell SPZ-8000 Maintenance Manual page 324

Digital automatic flight control system for gulfstream iv
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CHASSIS GND ~
ON-SIDE
DADC
{n"
II
ARINC 429
II
'?'"
CROSSIDE
DADC
{n"
II
ARINC 429
'
I
c
lPARITY+
PROGRAM
PIN
COMMON
SHIELD GND—
~
16
9
?4
53
49
4s
55
44
w
11
47
17
26
25
34
32
33
19
18
Honeywell !!!!!gb.c'
KEl=
3
G
H
L
3
c
-1
FAN DUCT
PRESSURE
J
I
I
.
1- —————————..
J1
]
31
39
WI
37
52
45
7
1
3
12
2
EPR
OUTPUT
ARINC 42S
(12.8 KHZ)
MONITOR
) INPUT
RS 232
1
TEST
ONLY
NON-VOLATILE
~
MEMORY
RESET
~
BITE FAULT
AD-213E6
Engine Pressure Ratio Transmitter
Block Diagram
Figure 10-2
22-14-00
Page 198.159
Aug 15/91
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