Honeywell PRIMUS 1000 Pilot's Manual page 282

map view diagram, 3-97
mode messages, 3-99
no bearing readout, 3-97
off scale symbols, 3-98
range ring, 3-97
resolution advisories, 3-64
status messages, 3-65
traffic symbols, 3-100
typical display, 3-101
warning messages, 3-76
Trend vector, airspeed display, 3-57
Troubleshooting, 7-1, 7-25
AP FAIL indicator, 7-29
checklist loading, 7-28
combined mode problems, 7-20
digital avionics, 7-1
event codes, 7-6
ground maintenance test, 7-21
hardware/software ID pages, 7-4
lateral mode problems, 7-15
maintenance test mode, 7-2
operational notices, 7-29
pilot write–up, 7-31
technical support, 7-1
typical problems, 7-15
vertical mode problems, 7-18
True airspeed (TAS) display, 3-84
gain programming, 5-3
True north annunciator, 3-93
Typical PFD presentations, 3-67
approach capture tracking at
minimums, 3-71
climb to initial altitude, 3-68
comparison monitoring, 3-72
enroute cruise, 3-69
failures and warnings, 3-110
setup for approach, 3-70
takeoff in go–around mode, 3-67
Typical TCAS display, 3-101
U
UP annunciator, 4-4
A28–1146–134
REV 1 Jan/03
PRIMUS
Index (cont)
V
Variable gain display, 3-84
Vertical beam sensor (VBS), 5-3
Vertical deviation, 3-34, 3-79
Vertical gyro, 2-8
fast erect switch, 2-10
Vertical modes, 6-26
altitude hold (ALT HOLD), 6-38
altitude preselect (ASEL), 6-33
flight level change (FLC), 6-30
pitch hold, 6-26
problems, 7-18
vertical speed hold, 6-28
VNAV mode, 6-40
Vertical speed display, 3-63
failure displays, 3-78
hold mode, 6-28
Vertical track alert (VTA), 3-37
VNAV button, 4-2
VNAV,
FMS VNAV annunciators, 3-41
VNAV submenu, 3-8
VOR
after over station sensor, 5-4
approach (VAPP) mode, 6-14
capture, 5-4
course set knobs, 3-19
navigation mode, 6-4
NAV source lateral deviation,
over station sensor, 5-4
TO/FROM annunciator, 3-45
VOR button, 3-20
VS button, 4-3
V
SPEED
VSPEED submenu, 3-11
V
SPEED
V
STALL
R
1000 Integrated Avionics System
VNAV direct, 6-42
VNAV preselect, 6-45
3-44
bugs, 3-55
takeoff display, 3-57
bug (JAA), 3-57
Index
Index–11