Honeywell PRIMUS 1000 Pilot's Manual page 329

Integrated avionics system for embraer 145
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Integrated navigation unit, C--5
Radio management unit (RMU), C--6
Tuning backup control head, C--7
Tuning backup control head operation, C--35
Controls and annunciations, C--37
Emergency mode, C--36
General, C--35
Normal mode, C--36
Procedures
ADF PAST procedure, C--32
Altitude hold mode engagement procedure, 8-37
Altitude preselect mode engagement procedure, 8-32
Altitude preselect mode procedure, 8-34
ATC transponder and TCAS PAST procedure, C--30
Back course flight procedure, 8-17
Designating a new waypoint procedure, 4-81
DME function key operating procedure, C--20
FMS mode engagement procedure, 8-10
Ground maintenance test procedure, 9-9
ILS approach mode procedure, 8-21
Localizer mode engagement procedure, 8-12
MFD checklist upload procedure, 9-11
Speed mode engagement procedure, 8-30
Troubleshooting procedure, 9-13
VHF COM PAST procedure, C--29
VOR approach mode engagement procedure, 8-9
VOR navigation mode engagement procedure, 8-4
VOR/ILS/marker/DME PAST procedure, C--31
Publication ordering information, 10-4
R
Radio altimeter system, 2-7
Radio management unit (RMU), C--6
ADF operation, C--24
ADF operation with HF transmitters, C--26
Controls, C--25
General, C--24
Single ADF installation, C--27
ATC transponder and TCAS operations, C--20
ATC failure warnings, C--24
A28--1146--112--00
PRIMUSr1000 Integrated Avionics System
Index (cont)
Index
Index--19

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