Honeywell PRIMUS 1000 - Page 332

PRIMUSr 1000 Integrated Avionics System
A28--1146--112--00
Index
Index--22
Index (cont)
Flight management system (FMS) (Option), 2-9
Other switches and controls, 2-9
AP (autopilot) disconnect switch, 2-9
External AHRS switches, 2-9
GA (go--around) button, 2-9
Joystick (option), 2-10
Master warning/master caution switches, 2-10
N2 override switch, 2-10
TCS (touch control steering) button, 2-9
PRIMUS
â
660 Weather Radar System, 2-6, B--1
PRIMUS
â
880 Weather Radar System (Option), 2-8
PRIMUS
â
II Integrated Radio System, 2-7, C--1
Radio altimeter system, 2-7
Traffic alert and collision avoidance system (TCAS), 2-8
System description, 2-1, 2-2
System display failure annunciation, 4-95
Display controller failures, 4-95
Both pilot’s and copilot’s DC fail, 4-96
Copilot’s DC fails, 4-96
Pilot’s DC fails, 4-95
Display system reversionary modes, 4-95
EFIS 1 (pilot normal) failure, 4-95
EFIS 2 (copilot normal) failure, 4-95
System file, 1-1, 1-2
System limits, 7-1, 7-2
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
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
System performance and operating limits, 7-5