Honeywell PRIMUS 1000 - Page 186

PRIMUSr 1000 Integrated Avionics System
A28--1146--112--00
System Limits
7-6
Mode ValueParameter
Control or
Sensor
VOR,
VORAPR, or
FMS (cont)
On Course
Roll Angle Limit
Roll Rate Limit
Crosswind Correction
Over Station
Course Change
Roll Angle Limit
Roll Rate Limit
±12_
1_/sec
Up to ±45_Course Error
in VOR, ±30_ in VAPP
Up to ±90_
±7_ of Roll
3_/sec
LOC, APR, or
BC
Course Knob
and Nav
Receiver and
Radio Altimeter
LOC Capture
Beam Intercept
Roll Angle Limit
Roll Rate Limit
Capture Point
LOC Track
Roll Angle Limit
Crosswind Correction
Limit
Gain Programming
Up to±90_
±27.5_
5.5_/sec
Function of Beam, Beam
Rate and Course Error
Max. trip point 175 µA
Min. trip point 60 µA
±17_ roll
±30_ of course error
Starts at 1200 ft. radio
altitude gain reduction =
1 to 0.5
GS GS Receiver, Air
Data Computer
and Radio
Altimeter or MLS
Receiver
GS Capture
Beam Capture
Pitch Command Limit
Path Damping
Pitch Rate Limit Gain
Programming (First
Stage)
Gain Programming
(Second Stage)
Function of beam and
beam rate
±10_
Vertical Acceleration
f (TAS)
Starts at 1200 ft radio
altitude, gain reduction
= 1 to 0.33
Starts at 250 ft. radio
altitude, gain reduction =
0.33 at 250 ft.= 0 at 0 ft.
GA Control Switch
on Throttle
Fixed Pitch--up
Command,
Wings Level
12_ Pitch up
System Performance/Operating Limits
Table 7--1 (cont)