Honeywell PRIMUS 1000 - Page 330

PRIMUSr 1000 Integrated Avionics System
A28--1146--112--00
Index
Index--20
Index (cont)
Controls and annunciations, C--20
General, C--20
Built--in--test (BIT), C--28
ADF PAST, C--32
ATC transponder and TCAS PAST, C--30
General, C--28
Pilot--activated self--test (PAST), C--28
VHF COM past, C--29
VOR/ILS/marker/DME PAST, C--31
Cross--side operation, C--27
General, C--7
Maintenance, C--32
Memory pages, C--11
Navigation receiver operation, C--17
Basic NAV tuning, C--17
DME hold, C--18
Single DME installation, C--18
VHF communications transceiver operation, C--13
Basic COM tuning, C--13
COM messages, C--15
Radio management unit (RMU) operation, C--7
Controls, C--8
Cursor, C--8
Function keys, C--9
Line select keys, C--8
Transfer key, C--8
Tuning knobs, C--8
System (SYS) on--off page, C--11
Remote autopilot switches and annunciators, 6-5
AP disconnect switch, 6-5
Go--around button, 6-5
Pitch wheel and Turn knob controls, 6-5
TCS button, 6-5
Remote mounted equipment, 1-2
Reversionary controllers and dimming panel, 3-7
Data acquisition unit (DAU) reversionary panel, 3-8
EDS dimming panel, 3-8
System reversionary panel, 3-7
ADC button, 3-7
AHRS button, 3-8
MDF knob, 3-7