Honeywell PRIMUS 1000 Pilot's Manual page 318

PRIMUSr1000 Integrated Avionics System
GS capture (CAP), 7-2
GS gain programming as a RA and vertical speed (VS) function,
7-2
Lateral beam sensor (LBS), 7-2
Lateral gain programming, 7-3
Localizer/back course (BC) track, 7-3
True airspeed (TAS) gain programming, 7-3
Vertical beam sensor (VBS), 7-4
VOR after over station sensor (AOSS), 7-4
VOR capture (CAP), 7-4
VOR over station sensor (OSS), 7-4
Go--around (GA) mode (wings level), 8-40
Ground initialization, A--9
Abnormal operations, A--10
Flight operations in basic mode, A--11
Flight operations in DG mode, A--11
In--air initialization, A--11
Takeoff in basic mode, A--10
Takeoff in DG mode, A--10
Ground maintenance test, 9-9
Test procedure, 9-9
Guidance controller (GC), 6-1
Autopilot (AP)/yaw damper (YD)/couple (CPL) buttons, 6-1
AP button, 6-1
AP disengage, 6-2
CPL button, 6-2
YD button, 6-2
YD disengage, 6-2
Autopilot power--up test, 6-5
FGS caution and advisory messages, 6-5
Amber (caution) flight guidance system messages, 6-6
Red (warning) flight guidance system messages, 6-5
Flight director (FD) mode selection, 6-3
ALT (altitude) button, 6-3
AP OFF, 6-4
APR (approach) button, 6-3
CRS (course) knob, 6-4
FD1/FD2 buttons, 6-4
FD1/FD2 switch operation, 6-4
FLC (flight level change) button, 6-3
HDG (heading) button, 6-3
Index
Index--8
Index (cont)
A28--1146--112--00