PRIMUS
r
1000 Integrated Avionics System
A28--1146--112--00
Index
Index--6
Index (cont)
E
Electronic display system (EDS), 2--4, 3-1, 3-5, 3-6
Introduction, 3-1
MFD bezel controller basic operation, 3-5
Bezel controls, 3-5
Controller conventions, 3-6
Map range control, 3-6
Reversionary controllers and dimming panel, 3-7
Data acquisition unit (DAU) reversionary panel, 3-8
Dimming panel, 3-8
System reversionary panel, 3-7
Electronic flight instrument system (EFIS), 4-1, 4-5, 4-6
Controls, 4-5
Display controller (DC), 4-20
EFIS preflight self--test, 4-23
Guidance controller course and heading controls, 4-22
Multifunction display (MFD) bezel controller, 4-6
Primary flight display (PFD) bezel controller, 4-5
Displays, 4-25
MFD system displays, 4-86
Multifunction display (MFD), 4-68
PFD caution and failure display, 4-61
Primary flight display (PFD), 4-25
Standby navigation display, 4-96
System display failure annunciation, 4-95
Typical PFD presentations, 4-53
Introduction, 4-1
Engine instrument and crew alerting system (EICAS), 5-1
Controls, 5-5
EICAS bezel controller, 5-5
Master warning and caution annunciation switches, 5-5
Displays, 5-6
Backup EICAS display, 5-31
Backup EICAS display failure indications, 5-34
Crew alerting system (CAS), 5-22
EICAS display, 5-6
EICAS reversionary modes, 5-30
Primary engine displays, 5-7
Introduction, 5-1