Honeywell SPZ-8000 Pilot's Manual page 284

map mode with FMS selected
for display, 4-52
map mode with VOR selected
for display, 4-49
NAV source reversion, 4-59
weather radar displays, 4-54
multifunction display (MFD), 5-1
checklist display, 5-22
controller, 5-3
system information, 5-2
Dual couple approach mode, 8-36
automatic cancellation, 8-37
manual cancellation, 8-37
Dual flight guidance system, 2-5
E
Electronic attitude director indicator
(EADI), 4-6
CAT 2 annunciators, 4-28
excessive deviation
monitoring, 4-28
failure, 4-28
comparison monitoring, 4-29
attitude, 4-29
glideslope, 4-30
IAS, 4-30
localizer, 4-30
displays and annunciators, 4-9
aircraft symbol, 4-11
altitude preselect display, 4-11
AP engage annunciator, 4-10
attitude sphere, 4-13
decision height display and
annunciator, 4-9
FD couple arrow, 4-10
flight director mode
annunciators, 4-9
FMS speed bug, 4-13
IAS acceleration trend, 4-14
IAS display scale, 4-13
IAS/Mach reference bug and
display, 4-12
inclinometer, 4-12
A28--1146--055
REV 2
SPZ--8000 Digital Integrated Flight Control System
Index (cont)
EFIS reversion, 4-20
EFIS self--test, 4-66
excessive attitude display, 4-31
failure warning flags, 4-32
localizer pointer, localizer scale,
and rising runway, 4-12
Mach display, 4-13
marker beacon, 4-11
maximum velocity indicator,
4-14
pitch and roll command cue,
4-12
radio altitude display, 4-12
roll attitude pointer and scale,
4-10
TCAS resolution advisory
(optional), 4-14
vertical speed display
(optional), 4-14
vertical or glideslope
deviation pointer, 4-11
vertical track alert
annunciator, 4-11
cockpit reversion switching
locations, 4-20
flight director reversions, 4-26
IAS reversions, 4-24
IRS reversions, 4-22
NAV source reversions, 4-27
reversion annunciators, 4-21
symbol generator reversions,
4-24
altitude preselect failure, 4-34
attitude failure, 4-33
cross--side data failure, 4-34
flight director failure, 4-33
glideslope failure, 4-35
indicated airspeed failure, 4-34
localizer failure, 4-35
radio altitude failure, 4-35
symbol generator internal
failure, 4-35
TCAS messages and failure
annunciators, 4-36
vertical speed failure, 4-35
Index
Index--3