Honeywell SPZ-8000 Maintenance Manual page 541

Digital automatic flight control system for gulfstream iv
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Honeywell
MAINTENANCE
MANUAL
GULFSTREAM IV
r
——— ——— ——— —
FZ-820 FLIGHTGUILIAHCE COMPUTER(COPILOT'S)
I
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L
.——
"A"
PROCESSOR
v
———
———
—.
1
SERIAL DATA
CLOCK
STROSE
c"
LAMP
TEST
2a VDC ANNUNCIATOR VALID
COPILOTS
TO(M
SW
*
COPILOTS
TCS SW
r'"
I
PS ARM NO. 2
/$
1
"PUSH BuTTON SERIAL DATA
28 VOC
ANN PWR —n
No.
2
r
*
.——.
————
————
————
——.
— ————
——
W-820 FLIGHT GUIDANCECONTROLLER(COPILOT%CHANNEL2)
1
P-+-
{
LEVEL
SHIFTERS
(NOTE
1}
SERIAL
DATA IN
SERIALlN-
PARALLEL CiJT
OEVICEF31PO)
PARALLEL
STR09E
OUTPUTS
CLOCK
cm
I
I
\
I
I
+—
>
-
ANN
I
LATCHESl
-
LAMP
ORIVERS
TEST 2
I
( P
#
I
+
w
I
NOTES
LAMP TEST
TEST2+
1 THE INPUTIS LEVEL SHIFTED TO
ANNVLD
+
ORIVE2
PROVIDE A5 VDC PARALLELINPUT
I
TO THE PISO
END AROUND
2 THE GP-820 COPILOTS SIOE (CH2) IS
SHOWN
THE COPILOTS SIDE (CH1 )
I
IS SHOWN ON SHEET I
3. ALL CIRCLED LETTERS DENOTE TIE
-9
CLOCK
I
POINTS ON SHEET 1.
-
STROBE
+
PARALLEL IN-
1
*
CLEAR
SERIAL OUT
OEVICE (PISO)
ANN VLD
.;
1
'b
11J2
SERIAL
(H)
7
PARALLEL
DATA OUT
INPUTS
(C)
8
5V
I
(5
o
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1
I
PULSE WIDTH
CONVERTER
k
I
T
A
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I
J
Ao 12462
~
F1 ight
Director
Mode Select Diagram
Figure 255 (Sheet 1.1)
22-14-00
Page 298.57/298.58
Aug 15/91
Use or dwclosure of Intormallon on
this
page
IS subject
10 the
restrictions
on
Ihe
htle page of thm document.

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