Honeywell SPZ-8000 - Page 285

SPZ--8000 Digital Integrated Flight Control System
A28--1146--055
REV 2
Index
Index--4
Index (cont)
Electronic attitude director indicator
(EADI) (cont)
typi cal display present at i ons, 4-15
approach capture tracking
below DH, 4-19
climb to initial altitude, 4-16
enroute cruise, 4-17
setup for approach, 4-18
takeoff using go--around
mode, 4-15
Electronic flight instrument system
(EFIS), 2-4, 4-1
Electronic horizontal situation
indicator (EHSI), 4-37, 4-42
arc mode display, 4-47
arc mode with TCAS traffic
display (optional), 4-57
no bearing data, 4-58
range ring, 4-57
TCAS altitude display
submodes (optional), 4-58
traffic symbols, 4-57
composite display, 4-64
approach configuration, 4-66
crui se fl i ght configuration, 4-65
symbols, 4-64
displays and annunciators in the
FULL compass or ARC modes,
4-38
aircraft symbol, 4-42
approach (APP) annunciator
(FMS), 4-44
bearing pointer source
annunciators, 4-43
bearing pointers, 4-43
course deviation bar and
lateral deviation scale, 4-43
course preselect annunciator
(FMS), 4-43
course preselect pointer and
deviation bar, 4-42
course select/desired track
pointer and deviation bar,
4-41
course--desired track display,
4-41
distance display, 4-44
elapsed time display, 4-42
FMS drift bug, 4-41
FMS message annunciator,
4-41
fore and aft lubber lines, 4-38
glideslope deviation pointer,
4-42
groundspeed, 4-42
heading dial, 4-41
heading select bug and
display, 4-38
heading source annunciator,
4-41
navigation source
annunciator, 4-44
reci procal course point er, 4-43
reciprocal course preselect
pointer , 4-43
target alert annunciator, 4-41
time--to--go, 4-42
TO/FROM annunciator, 4-42
waypoint/DME identifier, 4-44
wind vector display, 4-38
EFIS reversion, 4-58
EFIS self--test, 4-66
test symbols, 4-67
failure warning flags, 4-61
glideslope failure, 4-62
heading failure, 4-61
navigation source failure,
4-62
symbol generator internal
failure, 4-63
TCAS failure, 4-63
heading comparison monitoring,
4-60
map mode with FMS s elected for
display, 4-52
map mode with VOR selected for
display, 4-49
NAV source reversions, 4-59