Honeywell PRIMUS 1000 Pilot's Manual page 161

Integrated avionics system for the citation encore
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R
PRIMUS
1000 Integrated Avionics System
Control or
Sensor
Mode
VOR or
VORAPR
VOR or
VORAPR
LOC or
Course Knob,
APR
NAV Receiver,
and Radio
Altimeter
LOC or
APR
System Performance and Operating Limits
System Limits
5-6
Parameter
On Course
Roll Angle Limit
Roll Rate Limit
Crosswind Correction
Over Station
Course Change
Roll Angle Limit
Roll Rate Limit
Localizer/Azimuth Capture
Beam Intercept
Roll Angle Limit
Roll RateLimit
Capture Point
Localizer On Course
Roll Angle Limit
Crosswind Correction
Limit
Gain Programming
Table 5–1 (cont)
Value
12_
1_/second
Up to 45_
Course Error in VOR,
±30_ in VOR APR
Up to ±90_
12_
4_/sec
Up to ±90_
27.5_
5.0_/sec
Function of Beam, Beam
Rate, and Course Error.
Max. trip point 175 ma
Min. trip point 60 ma
12_
30_
Starts at 1200 ft radio altitude,
gain reduction = 1 to 0.5
A28–1146–134
REV 1 Jan/03

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