Honeywell PRIMUS 660 Pilot's Manual page 160

R
PRIMUS 660 Digital Weather Radar System
System configurations, 2-1
dual configuration, 2-1
dual control mode truth table, 2-3
equipment list, 2-4
cockpit mounted options, 2-4
remote mounted, 2-4
stand–alone, 2-1
T
Test mode, 4-6
color bands, 4-6
dedicated radar indicator, 4-6
EFIS/MFD/ND, 4-6
Test mode with TEXT FAULTS
enabled, 8-2
Thunderstorms, A–3
Cancellation, A–3
general, A–3
hazards, A–4
do's and don'ts of
thunderstorm flying, A–8
effect on altimeters, A–7
hail, A–6
icing, A–5
lightning, A–7
low ceiling and visibility, A–7
schematic cross section of a
thunderstorm, A–6
squall lines, A–4
tornadoes, A–4
turbulence, A–5
weather radar, A–7
national severe storms laboratory
(NSSL) thunderstorm research,
A–10
extrapolation to different
climbs, 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
Index
Index–6
Index (cont)
purpose, A–3
related reading material, A–3
Tilt management, 5-5
tilt setting for minimal ground
Tornadoes, A–4
Trim adjustments, 7-1
Turbulence
above storm tops, A–11
and echo intensity on NWS radar
below cloud base, A–12
in relation to distance from storm
in relation to distance from the
relationship between turbulence
relationship between turbulence
relationship between
turbulence and altitude,
A–10
relationship between
turbulence and reflectivity,
A–10
turbulence above storm tops,
A–11
turbulence and echo intensity
on NWS radar (WSR–57),
A–11
turbulence below cloud base,
A–12
turbulence in relation to
distance from the storm
edge, A–11
turbulence in relation to
distance from storm core,
A–11
use of airborne radar, A–13
visual appearance of storm
and associated turbulence
with them, A–12
target display, 5-8
12–inch radiator, 5-8
18–inch radiator, 5-9
(WSR–57), A–11
core, A–11
storm edge, A–11
and altitude, A–10
and reflectivity, A–10
A28–1146–111
REV 2