Honeywell SPZ-8000 Maintenance Manual page 545

Digital automatic flight control system for gulfstream iv
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——.
————
.——
——.
.—
I
I
I
I
I
I
w
R
LOC TRACK 2
CLR
HDG SEL
LNAV SEL
BC SEL
GA
PFD CMD SEL
NAV SOURCE
CHANGE
TKOD . AP ENG
l—–
SG VALID FOR COUPLED
PFD
FGC vALID
I
IRS MISCOMPARE
IRS 3 VALID
SDADCVALID
l–
CPL VALID . 2SEC
"wF
I
"-4
SEL LAT GuIDANCE
=.5
SEC
I
OC TRACK
1
-
(NOTE)
LOC TRACK
1
vERT VEL <-2°
(TAS/57.3)
LOC TRACK 2
r-ii
(NOTE)
R
Cl
E?.-l
HDG SEL ~
II
4
.
NAV SOURCE
CHANGE
10J2B
TKOD . AP ENG 3
r
IJ1
NAV.
LOC SEL
s
7 +
100 e
SERIAL IN
BC ARM
o
PARALLEL OUT
T
8
+
101 +
DEVICE
~
R
TTL
CLR
3s +
106
2
BC CAP1 4
!
BC SWITCH
INPUT
(REF SH1)
Y
APP SEL
LNAV SEL
GA
I
PFD CMD SEL
NAV SOURCE
CHANGE
TKOD
AP ENG
I
P
I
FGC VALID
IRS MISCOMPARE*
lRS3~
I
SDADC=
CPL =
2 SEC
1
K
'w
F1iqht Director
I
I
I
I
I
I
I
I
I
I
a
,,w
loJIB/loJ2B
PROCESSOR
1
Ascs
ouTPuT
,,A,,
2
TO SYMBOL
PROCESSOR
GENERATOR
TO
4
DISFIAY SELECTED
MODE ON PFD
5
I
I
I
I
I
I
I
I
I
1
I
I
I
I
I
I
L——————
———————
———
-1
LATERAUROLL
MODES
Mode ~elect Diagram
Figure 255 (Sheet 5)
NOTE:
IF BOTH DADCS ARE INVALID,
THE FGC WILL USE DEFAULT
AIR DATA VALUES
WHEN
IN
APPROACH
TRACK
MODE.
THE
DEFAULT
VALUES
ARE:
DYNAMIC
PRESSURE
75 La/F?
TAS
160 KNOTS
AD-136S2 @
-R3
22-14-00
Page 298.62
Aug 15/91
use
or
disclosure
of
information
on
this
page
is
subject
to
the
restrictions
on
the
title
page
of
this
document.

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