Honeywell SPZ-8000 Pilot's Manual page 159

Control or
Sensor
Mode
APR or Course knob
BC BC and NAV and NAV
receiver
APR NAV receiver
GA Control
switches on switches on
throttles
(disengage (disengage
A/P)
Pitch hold Pitch hold Pitch wheel or Pitch wheel or
TCS release
ALT hold DADC
Bank Turn knob
select
VS hold VS hold DADC DADC
System Performance and Operating Limits
A28--1146--055
REV 2
SPZ--8000 Digital Integrated Flight Control System
Parameter
LOC Track:
Roll angle limit
Roll rate limit
Crosswind correction
LOC gain programming LOC gain programming
Glideslope Capture:
Capture point
Pitch command limit Pitch command limit
glideslope damping
Pitch rate limit
Glideslope gain
programming
Fixed flight director
pitch--up and wings pitch up and wings
level command
Pitch attitude command Pitch attitude command
ALT hold engage range
ALT hold engage error
Pitch limit
Pitch rate limit
Bank limit
VS engage VS engage
VS hold engage error VS hold engage error
Pitch limit
Pitch rate limit
Table 7--1 (cont)
Value
24_
5.5_/second
Up to 45_ course error
Function of radio altitude, Function of radio altitude,
TAS, and VS
<150 mV glideslope beam
deviation
+10_, --15_ +10_ --15_
Vertical acceleration
.2g maximum
Function of radio altitude,
TAS, and VS
10.0_ nose up
20 maximum 20_ maximum
0 to 60,000 feet
40 feet
20_
.3g maximum
30_
0 to +6000 feet/min, --8000 0 to +6000 feet/min, 8000
feet/min
100 feet/min 100 feet/min
20_
.1g maximum
System Limits
7-9