Honeywell PRIMUS 1000 Pilot's Manual page 13

Integrated avionics system for embraer 145
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Table of Contents (cont)
Section
7. SYSTEM LIMITS (CONT)
Glideslope (GS) Gain Programming as a Radio
Altitude (RA) Function
GS Gain Programming as a RA and Vertical
Speed (VS) Function
GS Capture (CAP)
Lateral Beam Sensor (LBS)
Lateral Gain Programming
Localizer/Back Course (BC) Track
True Airspeed (TAS) Gain Programming
Vertical Beam Sensor (VBS)
VOR Capture (CAP)
VOR Over Station Sensor (OSS)
VOR After Over Station Sensor (AOSS)
System Performance and Operating Limits
8. MODES OF OPERATION
Heading (HDG) Hold Mode, Wings Level
Roll Hold Mode
Heading Select Mode
VOR Navigation (NAV) Mode
VOR Approach (VAPP) Mode
Flight Management System (FMS) Navigation
Mode (Option)
Localizer (LOC) Mode
Back Course (BC) Mode
Instrument Landing System (ILS) Approach Mode
Pitch Hold Mode
Pitch Hold Mode Operation, AP Engaged
Pitch Hold Mode Operation, AP Not Engaged
TakeOff Mode
Vertical Speed Hold Mode
Speed Hold Mode
Flight Level Change (FLC) Mode
Altitude Preselect (ASEL) Mode
Altitude Hold (ALT HOLD) Mode
Windshear (WDSHEAR) Mode
Go--Around (GA) Mode (Wings Level)
A28--1146--112--00
PRIMUSr1000 Integrated Avionics System
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Table of Contents
Page
7-2
7-2
7-2
7-2
7-3
7-3
7-3
7-4
7-4
7-4
7-4
7-5
8-1
8-1
8-2
8-3
8-4
8-9
8-10
8-12
8-17
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8-20
8-25
8-25
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8-25
8-26
8-27
8-28
8-31
8-32
8-37
8-38
8-40
TC--3

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