Honeywell PRIMUS 1000 - Page 331

PRIMUSr 1000 Integrated Avionics System
A28--1146--112--00
Index
Index--21
Index (cont)
SG (symbol generator) button, 3-8
Reversionary modes, EICAS, 5-30
Loss of display guidance computer (DGC) symbol generator, 5-30
Loss of the display unit, 5-30
Roll hold mode, 8-2
S
Speed hold mode, 8-28
Engagement procedure, 8-30
Standby navigation display, 4-96
RMU backup navigation display, 4-98
ADF bearing pointer, 4-98
ADF pointer out of view right/left, 4-99
Aircraft symbol, 4-99
Course pointer with display, 4-100
Digital ADF bearing, 4-100
Digital heading, 4-98
Digital VOR bearing, 4-100
DME distance, 4-99
Glideslope pointer, 4-99
Glideslope scale, 4-99
Heading arc compass rose, 4-100
Heading compass, 4-99
Lateral deviation indicator, 4-100
Lateral deviation scale, 4-99
Marker beacon, 4-99
Selected course, 4-100
Standby navigation display failure indications, 4-100
TO/FROM indicator, 4-99
Tune box, 4-100
VOR bearing pointer, 4-98
VOR pointer out of view right/left, 4-99
VOR/ILS and ADF frequency display, 4-98
Supplemental pilot’s manuals, 1-1
System (SYS) on--off page, C--11
System description
Air data system (ADS), 2-5
Attitude heading and reference system (AHRS), 2-6
Electronic display system (EDS), 2-4
Flight guidance system (FGS), 2-3