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Honeywell SPZ-8000 - System Performance;Operating Limits

Honeywell SPZ-8000
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SPZ--8000 Digital Integrated Flight Control System
A28--1146--055
REV 2
7-7
System Limits
D VOR AOSS 2 occurs when the following conditions are all satisfied:
VOR AOSS 1 has tripped plus 3 seconds
Beam deviation is less than 2 dots
Once VOR AOSS 2 trips, beam deviation is again part of the control
signal.
SYSTEM PERFORMANCE/OPERATING LIMITS
Table 7--1 lists the system performance and operating limits.
Mode
Control or
Sensor
Parameter Value
A
P
A
Pen
a
e En
a
e limit Roll: U
to 75_
A
P
A
P
E
l
i
m
i
t
R
l
l
:
U
t
Pitch: Up to 50_
Basic AP TCS released
r
A
P
Roll control limit Up to 45_ roll
or
A
P engage
Pitch control limit Up to 20_ pitch
Pitch angle limit 20 pitch
P
i
t
c
c
m
m
l
i
m
i
t
m
x
i
m
m
P
i
tc
g
comman
l
i
m
i
t .
gma
x
i
mum
H
i
H
i
S
E
R
l
l
l
l
i
m
i
t
_
H
i
select
H
i
S
E
knob
R
l
l
l
l
i
m
i
t
_
17_ low bank switched on
s
l
c
t
k
l
w
k
s
w
i
t
c
the flight guidance
c
t
r
l
l
r
r
t
m
t
i
c
l
l
y
controller or automatically
Roll rate limit 4_/second
VOR Course knob
N
A
V
VOR Capture:
and N
A
V
receiver
Beam intercept angle
(HDG SEL)
Up to 90_
Capture point Function of beam, beam
closure
rate, and course error
Minimum trip point: 20 mV
dc
Maximum trip point: 180
mV dc
Roll angle limit 24_
17_ (low bank switched)
Roll rate limit 5.5/second
Course cut limit during
capture
45_ course
System Performance and Operating Limits
Table 7--1 (cont)

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