Honeywell SPZ-8000 Maintenance Manual page 543

Digital automatic flight control system for gulfstream iv
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-———
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—-
I FZ-S20FLIGNT GUIDANCE COMPUTER
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30sEcfi
vOR CAP+VOR
AOSS 2
LATERAL OEVIATION
RATE ~
< 50/SEC
BANK ANGLE<
I
COURSE
CHANGE
>
3 DEG
=
GA
vOR TRACK
HDG SEL
LNAV SEL
0ss
PFD CMD SEL
CLR
NAV SOURCE CHANGE
TKOD
AP ENG
SG VALID
FOR COUPLED
PFD
FGC ~
IRS MISCOMPARE
IRS 3 VALID
-3
SDADC VALID
SEL LAT GUIDANCE
VALID
5 SEC
CPL=.
2 SEC
TTL
'-T
'OR 'RACK
"
'SEC --l--&
I
~~~;~?i!!-v
s
a
'oRoss
>75
mV . RATE
>8
mV/SEC.
w
R
DME VALID
GA
3
CLR
+
DME HOLD
HDG SEL
LNAV SEL
vOR AOSS 1
PfD CMD SEL
NAV SOURCE
CHANGE
TKOD
AP SNG Yld
%Jr+
R
GA
CLR
HDG SEL
LNAV SEL
vOR AOSS 2
PFD CMD SEL
NAV SOURCE
CHANGE
TKOD
AP ENG 3
'ORAO:M:=-tF
GA
Y
h
CLR
HDG SEL
LNAV SEL
VOR TRACK
PFD CMD SEL
NAV SOURCE CHANGE
TKOD
AP ENG
vOR AOSS 2
D
L ——— ——— ——— ——— ———
LATERAL/ROLL
MODES
F1
iqht
Director
Mode select Diagram
Figure 255 (Sheet 3)
3
J
;
.——
-1
AO.13e63 @) -R3
22-14-00
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d
10J 1W1OJ2B
1
ASCB OUTPUT
"A
2
TO SYMBOL
PROCESSOR
GENERATOR
TO
4
DISPLAY SELECTED
MODE ON PFD
l-'
5
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Page 298.60
Aug 15/91
Use or disclosure of information on this page is subject to the restrictions on the title page of Ihts document.

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