Honeywell PRIMUS 1000 - Page 328

PRIMUSr 1000 Integrated Avionics System
A28--1146--112--00
Index
Index--18
Index (cont)
Yaw damper annunciations, 4-26
STD (standard) button, 4-5
Vertical speed (VS) display, 4-51
Flight director VS target display and bug, 4-51
TCAS II resolution advisory display, 4-52
TCAS status message, 4-52
Vertical speed analog scale, 4-52
Vertical speed digital display, 4-52
PRIMUS
â
660 Weather Radar System, 2-6, B--1, B--2
Description, B--1
Introduction, B--1
Maximum permissible exposure level (MPEL), B--12
Tilt management
Radar beam illumination high altitude -- 12--inch radiator,
B--11
Radar beam illumination low altitude --12--inch radiator, B--11
Weather radar controller, B--2
Controls and indicators, B--2
Normal operation, B--8
PRIMUS
â
880 Weather Radar System (Option), 2-8
PRIMUS
â
II Integrated Radio System, 2-7
PRIMUS
â
II Radio System, C--1, C--5, C--6
Audio panel operation, C--33
Controls, C--33
General, C--33
Introduction, C--1
Radio management unit (RMU) operation, C--7
ADF operation, C--24
ATC transponder and TCAS operations, C--20
Built--in--test (BIT), C--28
Controls, C--8
Cross--side operation, C--27
General, C--7
Memory pages, C--11
Navigation receiver operation, C--17
System (SYS) on--off page, C--11
VHF communications transceiver operation, C--13
System description, C--5
Audio Panel, C--6
General, C--5
Integrated communication unit, C--6