Honeywell PRIMUS 1000 - Page 313

PRIMUSr 1000 Integrated Avionics System
A28--1146--112--00
Index
Index--3
Index (cont)
VHF COM PAST, C--29
Procedure, C--29
VOR/ILS/marker/DME PAST, C--31
VOR/ILS/marker/DME PAST procedure, C--31
C
Cockpit mounted equipment, 1-2
Controls, 4-5, 5-5
Display controller (DC), 4-20
EFIS preflight self--test, 4-23
Self--test, 4-23
Instrument test, 4-24
Switching test, 4-24
EICAS bezel controller, 5-5
Guidance controller course and heading controls, 4-22
Multifunction display (MFD) bezel controller, 4-6
Checklist menu, 4-15
Map/plan, 4-19
MFD main menu, 4-8
MFD menu, 4-10
System menu, 4-8
TCAS, 4-17
WX (weather), 4-18
Primary flight display (PFD) bezel controller, 4-5
Crew alerting system (CAS), 5-22
CAS display failure indications, 5-29
EICAS test, 5-29
Symbol generator failure, 5-29
CAS messages, 5-23
Advisory messages (Cyan), 5-28
Caution messages (Amber), 5-24
Computed advisory messages, 5-29
Computed caution (AMBER) messages, 5-27
Warning messages (RED), 5-23
Cross--side operation, C--27
Customer support centers -- North America, 10-2