Honeywell PRIMUS 1000 Pilot's Manual page 275

R
PRIMUS 1000 Integrated Avionics System
EMER button, 3-95
Enhanced ground proximity warning
system (EGPWS) (optional), 2-9,
3-66, 3-102
color scheme, 3-103
messages, 3-102
pop–up display, 3-106
TEST mode, 3-105
Enroute cruise, 3-69
ENT (enter) button, 3-21
Equipment list, 1-1
cockpit mounted, 1-1
optional, 1-2
remote mounted, 1-2
software, 1-4
ET button, 3-15
Event codes, sample forms, 7-31
Event codes (ECs), 7-6
Excessive attitude, 3–31, 3-74
Excessive lateral deviation, 3-43
Exchange/rental centers, 1-8
F
Failure displays
attitude reference system, 3-78
AOA, 3-56
course deviation data, 3-79
course select, 3-79
display controller, 3-111
distance display, 3-79
DU, 2-5
EFIS, 3-111
flight director, 3-79
EGPWS modes, 3-66
heading, 3-79
IAS, 3-78
MADC, 3-78
MFD, 3-107
displays, 3-110
DU wraparound, 3-108
FMS, 3-108
heading select, 3-108
IC fan, 3-109
Index
Index–4
Index (cont)
radio altimeter, 3-79
TCAS messages, 3-76
vertical deviation, 3-79
vertical speed, 3-78
Fans, IC, failure warning, 3-109
Fast erect switch, 2-10
FD transfer switch, 2-10
FLC button, 4-3
Flight director (FD), 2-6
ALT button, 4-2
APR button, 4-2
BC button, 4-2
command bars, 3-35
couple arrow, 3-36
failure displays, 3-79
FLC button, 4-3
HDG (heading) button, 4-2
mode annunciators, 3-28
mode selector, 4-1
modes of operation, 6-38
NAV button, 4-2
VNAV button, 4-2
VS button, 4-3
Flight guidance system (FGS), 2-5,
4-1
autopilot controller, 2-6, 4-3
flight director, 2-6
mode selector, 4-1
yaw damper, 2-6
Flight level change (FLC) mode,
6-30
Flight management system (FMS)
accuracy/crosstrack, 3-46
failure warning, 3-108
LNAV annunciators, 3-46
message flag, 3-42
source annunciator, 3-37
status annunciators, 3-47
VNAV annunciators, 3-41
VNAV submenu, 3-9
IC overheat, 3-109
MADC, 3-108
MENU INOP, 3-109
TAT, 3-108
weather radar, 3-109
A28–1146–134
REV 1 Jan/03