System Performance And Operating Limits - Honeywell PRIMUS 1000 Pilot's Manual

SYSTEM PERFORMANCE AND OPERATING LIMITS

Table 7--1 lists the system performance limits for the aircraft. Table 7--2
defines the units of measure and their data range for this aircraft.
Mode
Yaw Damper Yaw Engage
Autopilot A/P Engage
Engage
Basic Touch Control
Autopilot Steering (TCS)
TURN Knob
PITCH Wheel
Heading Hold
Heading Heading Knob
Select
VOR, Course Knob,
VORAPR, or NAV Receiver,
FMS DME Receiver,
FMS
System Performance/Operating Limits
A28--1146--112--00
Control or
Sensor
Engage Limit
Engage Limit
Roll Control Limit
Pitch Control Limit
Roll Angle Limit
Roll Rate Limit
Pitch Angle Limit
Roll Angle Limit
Roll Rate Limit
Roll Angle Limit
Low Bank
Roll Rate Limit
Capture
Beam Angle
Intercept (HDG
SEL)
Roll Angle Limit
Roll Rate Limit
Course Cut Limit
at Capture
Capture Point
Table 7--1 (cont)
PRIMUSr1000 Integrated Avionics System
Parameter
No limit
Roll: Up to ±45_
Pitch: Up to ±30_
Roll: Up to ±45_
Pitch: Up to ±30_
±30_
3_ /sec.
±15_Pitch
±30° /sec
5.5_ /sec.
±27_
±14_
±4.0_ /sec.
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
Value
System Limits
7-5