Honeywell PRIMUS 1000 Pilot's Manual page 317

Equipment
Air data system, 2-5
Attitude and heading reference system, 2-6, A--1
Cockpit mounted, 1-2
Electronic display system, 2-4, 3--1
Flight guidance system (FGS), 2-3, 6--1
Flight management system, 2-9
Integrated radio system, 2-7
List, 1-2
Optional, 1-3
Optional list, 2-1
Other switches and controls, 2-9
Radio altimeter system, 2-7
Remote mounted, 1-2
Standard list, 2-1
Traffic alert and collision avoidance system, 2-8
Weather Radar System, 2-6, 2-8
F
Flight guidance system (FGS), 2--3, 6-1, 6-2
Autopilot controller, 6-6
PITCH wheel, 6-6
TURN knob, 6-7
Guidance controller (GC), 6-1
Autopilot (AP)/yaw damper (YD)/couple (CPL) buttons, 6-1
Autopilot power--up test, 6-5
FGS caution and advisory messages, 6-5
Flight director (FD) mode selection, 6-3
Remote autopilot switches and annunciators, 6-5
Flight level change (FLC) mode, 8-31
Descend and climb parameters, 8-31
Flight management system (FMS) (Option), 2-9
Flight management system (FMS) navigation mode (option), 8-10
Engagement procedure, 8-10
G
Glossary of terms, 7-1
Attitude director indicator (ADI) command cue, 7-1
Glideslope (GS) gain programming as a radio altitude (RA)
function, 7-2
A28--1146--112--00
PRIMUSr1000 Integrated Avionics System
Index (cont)
Index
Index--7