Honeywell PRIMUS 1000 - System Performance and Operating Limits

PRIMUSr 1000 Integrated Avionics System
A28--1146--112--00
7-5
System Limits
SYSTEM PERFORMANCE AND OPERATING LIMITS
Table 7--1liststhe system performance limits for theaircraft. Table7--2
defines the units of measure and their data range for this aircraft.
Mode
Control or
Sensor Parameter Value
Yaw Damper Yaw Engage Engage Limit No limit
Autopilot
Engage
A/P Engage Engage Limit Roll: Up to ±45_
Pitch: Up to ±30_
Basic
Autopilot
Touch Control
Steering (TCS)
TURN Knob
PITCH Wheel
Heading Hold
Roll Control Limit
Pitch Control Limit
Roll Angle Limit
Roll Rate Limit
Pitch Angle Limit
Roll Angle Limit
Roll Rate Limit
Roll: Up to ±45_
Pitch: Up to ±30_
±30_
3_/sec.
±15_ Pitch
±30°/sec
5.5_/sec.
Heading
Select
Heading Knob Roll Angle Limit
Low Bank
Roll Rate Limit
±27_
±14_
±4.0_/sec.
VOR,
VORAPR, or
FMS
Course Knob,
NAV Receiver,
DME Receiver,
FMS
Capture
Beam Angle
Intercept (HDG
SEL)
Roll Angle Limit
Roll Rate Limit
Course Cut Limit
at Capture
Capture Point
Up to ±90_
±27.5_
5.5_/sec VORAPR
3_/sec VOR
3_/sec VOR or FMS
±45_ Course
Function of beam, beam
rate, course error, DME
distance. Maximum trip
point 175 µA
Minimum trip point
30 µA
System Performance/Operating Limits
Table 7--1 (cont)