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-——. ——— ——— —.— .—— ——— —.— .—— _
1
FZ-S20 FLIGHT GUIDANCE COMPUTER (PILOT’S)
1
2
3
4
5
6
M
rT
71
66
78
m
rs
9
10
15
16
w
46
49
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l-+
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(c)
SERIAL
DATA IN
{H)
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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
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(c)
—
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8
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- DISENGAGE
HORN
1’
- &ENGAGE
ANN
o-
a
p
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I
(
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@
a
PFD-CMD
+
@
-@
1
I
1
20 Voc
YD OISENG -
MACH TRIM
DISENG -
L
1
I
(
3
ASCBOUTPUT
TOSYMBOL
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.