Honeywell SPZ-8000 Maintenance Manual page 271

Digital automatic flight control system for gulfstream iv
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OE1
(N)
h
TGT
\
,2
BUFFER
/
A2U1O
TBO – TB6
/
GAIN SW
FSB1
%
COMP
A2ul
0E2 (N)
/4
BUFFER
/
A2U1O
96
KHZ
t
PROGRAM
CTR
A3U19 AND A3U16
1
-El--@
A 2U5
BIN
CTR
WU21
TBO - TB6
GCR
GAIN WIPER
OE4
(N)
3
,5
1
,5
+'
/
i
CONTROL
LABEL
PROM
PROM
A3U13
A3U8
I
1
AD
*
CONV
GAIN
TBO - TB6
A3U3
D-
A3U1A
OP AMPL
*
A3U1 B
OP AMPL
I192KHZ
L
UART
A3U4
u
LINE
DRIVER
Scl
A3U2
TO RTA
INTERNAL
BUS
AID
CONV
TILT
A3U5
TILT WIPER
TBO - TB6
B
OE1
(N)
DECODER
OE2
(N)
MUX
OE3
(N)
10F8
0E4
(N)
A3U14
0E5
(N)
OE6
(N)
OE7
(N)
(N)-L-
Wx
SBY h
'AP-IW%17S
DELAY POR
A2U1
t-
POR
4-J
A2U7
TST
TURB
IrBo - TB6
1
I
0E3(N)+Ja
4E
POWER
+15VDC
28V
SUPPLY
INPUTPOWER
AIU1
-15VDC
AIQ1
+5VDC
1
I
JsJ
1
*
RNG 2°
-
RNG 2'
D
RNG 22
E
RNG 23
-
FPLN
*
A2U6
I
POWER SUPPLY
NOTE:
A
REFERENCE DESIGNATIONSARE AS FOLLOWS:
GCR
T
Al = POWER SUPPLY CCA (7007108)
A2 = LOGIC 1 CCA (701 3 373)
A' = LOGIC 2 CCA (701 3 378)
AD-15846-R3
Radar
Controller
Block
Dia~ram
WC-874 Weather
Use or dmclosure of Intormallon On this
Figure
8-11
22-14-00
Page 198.99/198.100
Aug
15/91
page
IS
subject
10
the restrictions
on the title page
of Ihls document

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