Honeywell SPZ-8000 - Page 288

SPZ--8000 Digital Integrated Flight Control System
A28--1146--055
REV 2
Index
Index--7
Index (cont)
pitch attitude hold mode, 8-40
presel ected course appr oach, 8-28
roll hold mode, 8-2
vertical navigation modes, 8-50
altitude hold , 8-50
altitude select, 8-50
flight level change, 8-50
vertical path mode, 8-51
vertical speed hold mode, 8-41
VOR (NAV) mode, 8-4
DIRECT TO function, 8-12
over station operation, 8-11
VOR approach mode, 8-11
Multifunction display controller, 5-3
checklist, 5-5
control buttons, 5-6
EMER button, 5-5
NORM button, 5-5
designator control, 5-5
ENT button, 5-5
joystick, 5-5
RCL button, 5-5
SKP button, 5-5
DIM control knob, 5-7
mode selector switch, 5-7
navigation, 5-3
APT button, 5-4
DAT button, 5-4
INC/DEC RNG switch, 5-4
MAP/PLAN button, 5-3
SRC button, 5-3
VOR button, 5-4
WX button, 5-3
Multifunction display system (MFD),
2-5, 5-1
changing a waypoint, 5-16
checklist display, 5-22
map mode, 5-8
map mode flight plan displays,
5-11
plan mode, 5-13
plan mode flight plan data, 5-14
system information, 5-2
TCAS mode traffic display
(optional), 5-18
weather radar, 5-20
N
Navigation display unit, A--9
P
Pilot writeup, 9-10
Pitch attitude hold mode, 8-40
Power--on/alignment operation, A--6
Preselected course approach, 8-28
PRIMUS
R
650 Weather Radar
System,2-8,B--1
controller, B--3
GAIN knob, B--7
LSS k nob, B-- 5
RADAR mode select switch,
B--6
RANGE buttons, B-- 3
RCT button, B--3
SECT button, B--5
SLV annunciator, B--5
STAB button, B--4
TGT button, B-- 4
TILT knob, B--5
description, B--2
introduction, B--1
maximum permissible exposure
level, B--14
operating procedures, B--8
in--flight compensation
adjustment, B--12
powerup, B--8
precautions, B--8
preliminary control settings,
B--8
radar mode -- ground
mapping, B--9
radar mode -- weather, B--9
self--test, B--10
standby, B--9
tilt management, B--13