Honeywell SPZ-8000 - Apr 15;93

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FZd30 FLIGHT GUIOANCE COMPUTER
10J 1B
f
r
—————
uam omc
I
1
ASCB “
2
I
ASCO “
L
—————
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ASCB ,
I
ASCB ~~
L
——— ——
1
——— ——
6E.JIA SG~ syMBoL GENERA70R
41
)
MIDDLE
42
ASCB ~~
MARKER
43
)
GS OEV?V
ASCB ,’
u
VALID
——— ——
C( MIDOLE MARKER ~ TO SH6
--@Et
TO SH7
I
TO SH6
lr
GS DEVN
TO SH6 ANO
FIG 259 (SH3)
--FEY
I NOTE 1 (SH1 )
NAV RECEIVER
ARINC 429
}
GS OEVIATION
● GS VALIO
● MIOOLE MARKER
I
(GS ARM. 1500 FT)
(GS CAP= 1S03 FT)
PITCH ATTITUOE
AND RATE
1(—
OUAL APP + GS TFIK
● MM PASSED . 250 FT
)
I
I
l—
C1OJ2A
—
37
- 38
r
—————— L
IIT-300RADIO ALTIMETER
- 2UJ1
I
PRIMAFW
{ 7 ‘-
+ w
OUTPUT
m
-40 mVOC/FT– N
I
w
28VOCRAVALIO
Y
.
%rl--
A/o
+J+&-n+
1 I
I 1
L ——— ——— Y
I
r
—.
RT-300 RADIO
I
I
——— —
ALTIMETER
C20J1
10J2A
PF!IMARY
OUTPUT
( 7 ‘=
+ w
b
36
40 mVOC!FT - N
m 37
28 vOC RA VALID ~
*
38
d
L
C1OJ2B
——— —
-
26
~
27
* 26
L
(
+
1
GS DEVN
BEAM FILTER
RATE
+
2 SECS
LIMITER
‘pRF2’’ER&FT0sH7
L ——
&
L
/
.—— — —.— ——— ——— ——— ——— ——— ——— —
——.. ___ _
GLIDESLOPE MODE
u
AO.13664 @) F13
F1ight Director/Autopilot
Pitch Channel Mode Flow Diagram
Figure 260 (Sheet 6)
22-14-00
Page 298.137/298.138
Apr 15/93
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