Honeywell SPZ-8000 Maintenance Manual page 538

Digital automatic flight control system for gulfstream iv
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10
0,
0
%
B
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A
x
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a
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10
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1
FZ-S20 FLIGHT GUIDANCE COMPUTER (PILOT'S)
1
2
3
4
5
6
M
rT
71
66
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rs
9
10
15
16
w
46
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L
l-+
(H)
(c)
SERIAL
DATA IN
{H)
(cl
CLOCK
(Llm&r4
I
SERIAL lN-
PARALLEL OUT
OEVICE (SIPO)
\
ANN
~
LATCHEW
DRIvERS
A/P ON
PFO-CMO
m
<
(H)
(c)
}
P
*
LAMP
TEST I
}
*
LAMP
!
7
9
LAMP TEST
TEST 1
ANN VLO
ORIVE I
ENO AROUNO
( I
*
CLOCK
-
STR08E
PARALLEL
*
INPUTS
(
:
-
-,
,
WRALLEL
lN-
SERIAL OUT
*
PFD-CMO
~
cL~R
DEVICE (PISO)
LEFt/RIGliT
JLD
-:
1
-
LOGIC 1
SERIAL
+tl
-
WRALLEL
OATA OUT
5V
INPUTS
}
STROBE
PARALLEL
STROBE
OUTPUTS
T
PILOT'S
I
r-
LAMP
COPILOT
S
TEST
AP
AP
8
2LOCK
c-
*
I
NOTES
1.
THE GP-620
PILOT'S SIDE (CH ! ) IS
I
SHOWN,
THE COPILOT'S
SIDE (CH2) IS
SHOWN
ON SHEET 2.
,
2.
13
:?
LEVEL
SHIFTERS
(NOTE 2)
T
SERIAL lN-
PARALLEL OUT
A
OEVICE
(SIPO)
THE INPUT IS LEVEL SHIFTED
TO
PROVIDE
A 5 VDC PARALLEL INPUT
TO THE PISO
ALL CIRCLED
LETTERS
DENOTE
TIE
POINTS
ON StiEET
2,
..w
PROCESSOR
wow
-9
28 VOC ANNUNCIATOR
VALID
9
11
r
6
K3
Is
{
(H)
(c)
L
%"%-'
J
5V —
PBARMMO
1
I
I
8
AP
I '-
I
-
E!!K
- DISENGAGE
HORN
1'
- &ENGAGE
ANN
o-
a p
I
I
(
I
I
I
@
@
a
PFD-CMD
+
@
-@
1
I
1
20 Voc
YD OISENG
-
MACH TRIM
DISENG
-
L
1
I
(
3
ASCBOUTPUT
TO SYMBOL
w
GENERATORS
O-5vDC *
6
PUSHBUTTONSERIALOATA
=/
EDGE
LIGHTING
I-(H
-——
———
— ———
———
———
———
———
—.—
_
——
———
———
—.
AP, YD, MACH TRIM, and PFD-CMD
Select Diagram
Figure 254 (Sheet 1)
22-14-00
Page 298.51/298.52
Aug 15/91
Use or disclosure of mtormatlon on this page is subject to the reslricllons on the title page of this document.

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