Honeywell PRIMUS 660 Pilot's Manual page 157

L
Level flight stabilization check, 5-17,
7-3
stabilization in straight and level
flight check
procedure, 5-17, 7-3
Lightning, A–7
Line configurations, 5-52
avoid bow–shaped line of echoes
by 20 miles, 5-54
avoid line echo wave patterns
(LEWP) by 20 miles, 5-53
avoid thunderstorm echoes at the
south end of a line or at a break
in a line by 20 miles, 5-52
Low ceiling and visibility, A–7
M
Maximum permissible exposure
level (MPEL), 6-1
Maximum storm tops, A–12
Modification of criteria when severe
storms and rapid development are
evident, A–13
N
National severe storms laboratory
(NSSL) thunderstorm
research, A–10
extrapolation to different climbs,
A–13
desert areas, A–13
tropical–humid climates, A–13
hail in thunderstorms, A–12
maximum storm tops, A–12
modification of criteria when
severe storms and rapid
development are evident, A–13
relationship between turbulence
and altitude, A–10
A28–1146–111
REV 2
R
PRIMUS
Index (cont)
relationship between turbulence
turbulence above storm tops,
turbulence and echo intensity on
turbulence below cloud base,
turbulence in relation to distance
turbulence in relation to distance
use of airborne radar, A–13
visual appearance of storm and
Normal operation, 4-1
preliminary control settings, 4-1
test mode, 4-6
O
Offset adjustment, 7-5
pitch, 7-8
roll, 7-5
Operating controls, 3-1
weather radar controller
660 Digital Weather Radar System
and reflectivity, A–10
A–11
NWS radar (WSR–57), A–11
A–12
from storm core, A–11
from the storm edge, A–11
associated turbulence with
them , A–12
power–up procedure, 4-1
radar mode –– ground
mapping, 4-5
radar mode –– weather, 4-4
standby, 4-4
color bands, 4-6
dedicated radar indicator, 4-6
EFIS/MFD/ND, 4-6
adjustment procedure, 7-8
adjustment procedure, 7-5
operation, WC–660, 3-10
GAIN, 3-16
LSS (lightning sensor system)
(optional), 3-13
RADAR, 3-14
rainfall rate color coding, 3-14
RANGE, 3-11
Index
Index–3