Honeywell SPZ-8000 - System Performance;Operating Limits

MAINTENANCE
MANUAL
GULFSTRE4M IV
Mode
Control or Sensor
Parameter
Value
LOC or BC
(cent)
APR
GA
I
GP-820
APR Button,
CRS Knob,
and NAV
Receiver
Control Switches
on Throttles
(DisengageA/P)
Roll Angle Limit
Roll Rate Limit
Course Cut Limit
During Capture
LOC Track:
Roll Angle Limit
Roll Rate Limit
Crosswind
Correction
LOC Gain Programming
Glideslope Capture:
Capture Point
Pitch Command Limit
Glideslope Damping
Pitch Rate Limit
GS Gain Programming
Fixed Flight Director
Pitch-Up Command;
Wings Level in Roll
~30
deg
7.0 deg/sec
*45 deg Course
224
deg
5.5 deg/sec
Up to t45 deg
Course Error
Function of Radio
Altitude, TAS
and
GS Deviation
Function of Beam
and Beam Closure
Min Trip Point,
20 mV dc
Max Trip Point,
37.5 mVdc
+10 deg, -15 deg
Error
Rate
Vertical Acceleration
Preset 0.2 g maximum
Function of Radio
Altitude, TAS and
Vertical Speed
15.0 deg noseup
(12.0 deg noseup
-906/907 FGC)
System Performance/OperatingLimits
Table 205 (cent)
22-14-00
Page 298.39
Apr 15/93
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