Honeywell SPZ-8000 Maintenance Manual page 662

Digital automatic flight control system for gulfstream iv
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1-
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————
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1 PZ-800 PERFORMANCE
COMPUTER
1
I
I
I
I
I
I
I
I
I
I
I
I
I
I
I
I
I
I
I
I
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I
I
SELECTED ENGINE RATING
/
\
ENGINE
RATING
CALCULATION
————
————
————
—,———
————
——,
1
-i
EPR
EPR
EPR
RATING
FLCH EPR
COMMAND
+
COMMAND
K
PROCESSOR
&
FLIGHT PATH ANGLE
)
I
I
I
>3
SECONDS
<30
SECONDS
P-J
~THRusT
I
b
REDUCTION
INERTIAL ACCELERATION
( ENGINE PRESSURE RATlO )
I
I
I
I
I
LEFT OR RIGHT
FLIGHT LEVEL
CHANGE PLA
COMMAND
SPEED
COMPLIMENTARY
FILTER
4
LEFT OR RIGHT
EPR
. SPEED HOLD PLA
SPEED
v
+
SELECTED AIRSPEED
ERROR
COMMAND
COMMAND
*
K
PROCESSOR
";
&=~~s
[
ENGINE PRESSURE RATIO ~
PRIMARY
EPR
EPR
RATE
LEFT OR RIGHT
COMMAND
+
TAKEOFFIGO AROUND PLA COMMAND
I
I
I
L-
MODE SELECTION LOGIC
II
ENGINE PRESSURE RATIO
d
~
'ATE
EON
'ATE
I
TAKER
TAKER
L ———
———
———
———
—,——
———
———
———
———
———
—___
_, J
AD-xM15 @
RI#
I
I
I
Autothrottle
Mode
F1OW
Diagram
Figure
270
(Sheet
2)
22-14-00
Page
298.207/298.208
Apr
15/93
Use of disclosure
of information
on
this
page
is
subject
to
the
restrictions
on
the
title
page
of this
document,

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