PRIMUS
r
1000 Integrated Avionics System
A28--1146--112--00
7-5
System Limits
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
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
µ
A
Minimum trip point
30
µ
A
System Performance/Operating Limits
Table 7--1 (cont)
