Honeywell SPZ-8000 - Page 289

SPZ--8000 Digital Integrated Flight Control System
A28--1146--055
REV 2
Index
Index--8
Index (cont)
PRIMUS
R
870 Weather Radar
System,2-8,C--1
controller, C--3
GAIN knob, C--11
GCR button, C-- 4
LSS s elect switch (optional),
C--7
mode select switch, C--7
RANGE buttons, C-- 3
SECT button, C--6
SLV annunciator, C--7
TGT button, C-- 5
TILT knob, C--6
TRB button, C--3
description, C--2
introduction, C--1
maximum permissible exposure
level, C--18
operating procedures, C--12
in--flight compensation
adjustment, C--16
powerup, C--1 2
precautions, C--12
preliminary control settings,
C--12
radar mode -- ground
mapping, C--13
radar mode -- weather, C--13
self--test, C--14
standby, C--13
receiver transmitter antenna
(RTA), C--2
tilt management, C--17
Procedures:
altitude hold mode, 8-47
altitude preselect mode, 8-45
changing a waypoint, 5-16
dual couple approach, 8-36
flight level change mode, 8-43
in--flight roll compensation
adjustment, B--12
in--flight roll offset adjustment,
C--16
localizer NAV mode, 8-17
power--on alignment, A--6
VOR (NAV) mode engage, 8-4
VOR DIRECT TO function, 8-12
Publication ordering information,
10-4
R
Radio altimeter system, 2-7
Roll hold mode, 8-2
S
Setup for approach, 4-18
System description, 2-1
air data system, 2-3
dual flight guidance system, 2-5
electronic flight instrument
system (EFIS), 2-4
flight management system
(FMS), 2-6
LASEREF
R
Inertial Reference
System (IRS), 2-9
LASERTRAK
R
Switch (Serial No.
5087 and later), 2-9
lightning sensor system (LSS)
(optional), 2-10
multifunction display system
(MFD), 2-5
PRIMUS
R
650 Weather Radar
System, 2-8
PRIMUS
R
870 Weather Radar
System, 2-8
radio altimeter system, 2-7
switches and controls, 2-11
traffic alert and collision
avoidance system (TCAS II)
(optional), 2-10
Systemlimits,7-1,7-2
glossary of terms, 7-1
performance/operating limits, 7-7