Honeywell SPZ-8000 Maintenance Manual page 547

Digital automatic flight control system for gulfstream iv
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LNAV SWITCI
INPuT
(REF SH1)
e————
—————
—————
———w
I FZ-820FLIGHTGUIDANCE
COMPUTER
I
I
FMS VALID—
1OJ2B
lJ1
SQ
FMS ARM
*
7
+
100 *
SERIAL IN
B
PARALLEL
T
+
101 -
OUT DEVICE
-
R
CLR
FMS SELECTED—
)
J-'-IG=JG=J
I
MOVING
AWAY
FROM DES TRK
WITHIN
I
2.5 MILES OF
DES TRK
T
l;:~~D~::.
I
DIFFERENCE
BETWEEN
ACTUAL A C TRK
I
DES AC TRK)
I
I
I
I
I
I
I
I
I
I
I
LNAVARMJ
LNAV SEL
HDG SEL
APP CAP
BC CAP L
-J
r
SQ
FMS CAP
R
CLR
GA
PFD CMD SEL
TKOD
AP ENG
Y
5J3 a
FOR
COUPLEO
PFD
FMS VALID
-u
FGC ~D
IRS MISCOMPARE
lRS3~
_
SDADCVALID
CPL VALID.
2 SEC 4
I
SELLAT
GUIDANCE
I
~.5SEC
i
I
I
I
I
I
=%
"A"
PROCESSOR
I
10J1
B/l OJ2B
1
ASCB OUTPUT
2
TO SYMBOL
PRO&SOR
GENERATOR
TO
4
DISPLAY SELECTED
5
MODE ON PFD
I
I
I
I
I
I
I
I
I
I
I
I
I
I
I
I
I
—.——
———— ———— ————
A
Flight Director
Mode Select Diagram
Figure 255 (Sheet 7)
AO-13SS2@.R4
22-14-00
Page 298.64
Aug 15/91
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