Honeywell SPZ-8000 - Page 159

SPZ--8000 Digital Integrated Flight Control System
A28--1146--055
REV 2
7-9
System Limits
Mode V a lueParameter
Control or
Sensor
APR or
B
C
Course knob
a
n
d
N
A
V
LOC Track:
B
C
and N
A
V
receiver
Roll angle limit 24_
Roll rate limit 5.5_/second
Crosswind correction Up to 45_ course error
LOC
g
ain
p
ro
g
rammin
g
Function o
f
radio altitude,
L
O
C
g
a
i
n
p
r
o
g
r
a
m
m
i
n
g
F
u
n
c
t
i
o
n
o
f
r
a
d
i
o
a
l
t
i
t
u
d
e
,
TAS, and VS
APR NAV receiver Glideslope Capture:
Capture point <150 mV glideslope beam
deviation
P
i
t
c
h
c
o
m
m
a
n
d
l
i
m
i
t
+
1
0
_
-
-
1
5
_
P
i
tc
h
comman
d
l
i
m
i
t +
1
0
_,--
1
5_
glideslope damping Vertical acceleration
Pitch rate limit .2g maximum
Glideslope gain
programming
Function of radio altitude,
TAS, and VS
GA Control
s
w
i
t
c
h
e
s
o
n
Fixed flight director
p
i
t
c
h
u
p
a
n
d
w
i
n
g
s
10.0_ nose up
switches on
throttles
(
d
i
s
e
n
g
a
g
e
pitch--up and wings
level command
(
d
i
sengage
A/P)
Pitch hold Pitch wheel or Pitch attitude command 20_ ma
x
imum
P
i
t
c
h
h
o
l
d
P
i
t
c
h
w
h
e
e
l
o
r
TCS release
P
i
t
c
h
a
t
t
i
t
u
d
e
c
o
m
m
a
n
d

2
0
m
a
x
i
m
u
m
ALT hold DADC AL T hold engage range 0 to 60,000 feet
ALT hold engage error 40 feet
Pitch limit 20_
Pitch rate limit .3g maximum
Bank
select
Turn knob Bank limit 30_
V
S hold D
A
DC
V
Sen
g
a
g
e 0 to +6000
f
eet
/
min, --8000
V
S
h
o
l
d
D
A
D
C
V
S
e
n
g
a
g
e
0
t
o
+
6
0
0
0
f
e
e
t
/
m
i
n
,
8
0
0
0
feet/min
V
S
h
o
l
d
e
n
g
a
g
e
e
r
r
o
r

1
0
0
f
e
e
t
/
m
i
n
V
S
h
o
l
d
engage error 
1
0
0
f
eet
/
m
i
n
Pitch limit 20_
Pitch rate limit .1g maximum
System Performance and Operating Limits
Table 7--1 (cont)