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

Integrated avionics system for the citation encore
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SYSTEM PERFORMANCE AND OPERATING LIMITS

Table 5–1 lists the system performance limits for the Citation Encore
aircraft.
Control or
Sensor
Mode
Yaw
Yaw Engage
Damper
Autopilot
AP Engage
Engage
Basic
Touch Control
Autopilot
Steering (TCS)
TURN Knob
PITCH Wheel
Heading Hold
Heading
Heading
Select
Select Button
VOR or
VORAPR
System Performance and Operating Limits
A28–1146–134
REV 1 Jan/03
R
PRIMUS
Parameter
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 5–1 (cont)
1000 Integrated Avionics System
Value
Up to 45_ left or right bank
Roll: Up to ±45_
Pitch: Up to ±30_
Roll: Up to ±45_
Pitch: Up to ±30_
±30_
5.5_/sec.
±15° Pitch
±35.5_
5.5_/sec.
±27_
±14_
±4.0_/sec.
Up to ±90_
±27.5_
4_/sec
±45_ Course
Function of beam, beam rate,
course error, DME distance.
Maximum trip point 13.3_
Minimum trip point 1_
System Limits
5-5

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