Honeywell PRIMUS 1000 - Page 312

PRIMUSr 1000 Integrated Avionics System
A28--1146--112--00
Index
Index--2
Index (cont)
Operation, A--7
Reduced performance operation, A--8
Standard operation, A--7
Pilot self--test, A--9
Pilot initiated self--test annunciations, A--9
Power--up test, A--8
Pilot self--test annunciations, A--8
Audio panel, C--6
Audio panel operation, C--33
Controls, C--33
Audio source (COM, HF, NAV, ADF, and DME) controls,
C--34
BOOM/MASK switch, C--34
COM1, COM2, COM3, and HF microphone switches, C--34
Emergency (EMER) microphone switch, C--34
ID/VOICE control, C--34
Marker (MKR) beacon volume control, C--35
Marker beacon MUTE and HI SENS/LO SENS sensitivity
controls, C--35
Passenger address (PAX) microphone switch, C--34
S.T. level control, C--35
SPKR and HDPH controls, C--35
General, C--33
Autopilot controller, 6-6
PITCH wheel, 6-6
TURN knob, 6-7
Autopilot power--up test, 6-5
B
Back course (BC) mode, 8-17
Flight procedure, 8-17
Backup EICAS display, 5-31
Backup EICAS display failure indications, 5-34
Built--in--test (BIT), C--28
ADF PAST, C--32
Procedure, C--32
ATC transponder and TCAS PAST, C--30
Procedure, C--30
General, C--28
Pilot--activated self--test, C--28