TM 1-1510-225-10
3B-196
3. At the end of test sequence an aural
message "TCAS System Test Okay"
or "TCAS System Test Fail" will be
annunciated. If the FAIL light stays
on
it
denotes
a
failure
in
the
transponder or units monitored by the
transponder. FAIL illuminates for one
second to verify operation of the light
and test mode in the transponder.
Transponder code digits will display
8888 for 1 second to verify that all
digit segments will illuminate.
q. Normal/In-Flight Operation. By selecting
TA/RA mode, the system automatically inhibits RA
displays when the aircraft if below 900 feet AGL on
approach or 1100 feet AGL on climbout. When flying
in close proximity to other aircraft during takeoff and
landing this may be desirable.
(1) Takeoff.
1. Immediately before beginning takeoff,
select TA/RA and 1 or 2.
2. Select short range (6 nm) to reduce
clutter.
(2) Cruise.
1. Select desired display range.
2. Select normal or pop-up mode as
desired.
(3) Descent and Landing.
1. Select short range display.
2. Select TA to eliminate RA displays
caused by other aircraft in close
proximity.
(4) Post
Flight.
The
recommended
procedure is to place the TCAS in STBY mode as
soon as practical after a landing is completed.
r. Alternate Operating Procedures. The
following
are
suggested
alternate
operating
procedures for use in event a TCAS flag is displayed
on the vertical speed indicator, or the FAIL indicator
on the transponder/TCAS control panel is lit. RA's
cannot be displayed so the RA flag will also be
displayed.
(1) V/S and RA Flags Displayed.
1. Select TA ONLY.
2. Traffic display will provide information,
including TA's relative to intruders in
your area.
Do not maneuver the aircraft solely with
reference to information on the traffic
display.
(2) RA Flag Displayed. Appearance of this
flag on the vertical speed indicator indicates failure of
the RA functions of the TCAS. Follow the same
procedure as in r(1) above.
(3) TCAS Flag Displayed. Appearance of
this flag indicates failure of some part of the TCAS
system. This includes the associated display systems
as well as the units generating the major TCAS
functions and signals.
1. Verify that ATC FAIL indicator is not
lit. If lit, refer to ATC FAIL indicator
procedures. If not, continue with the
following procedures.
2. Select TA ONLY.
Do not maneuver the aircraft solely with
reference to information on the traffic
display.
3. If TCAS flag is replaced by TA ONLY
message, continue TCAS operation in
TA mode.
4. If TCAS FAIL flag remains, select
XPDR or STBY as TCAS is no longer
available.
3B-35. LIGHTNING
DETECTION
SYSTEM
(WX-1000E).
a. Description.
The
Stormscope
system
consists of three components that defect, locate, and
map areas of vertical electrical discharge activity
contained within thunderstorms. The antenna mounts
externally to the aircraft and detects electrical
discharges associated with thunderstorms over a
125,000 square mile area around the aircraft. The
processor
analyzes
this
information
to
aid
in
identification
of
valid
electrical
discharges
from
lightning and to determine range and azimuth for
display in the cockpit. The analysis is completed in
milliseconds. The location of a vertical electrical
discharge associated with thunderstorm is plotted on
WARNING
WARNING