TM 55-1510-219-10
(3) Test procedure.
1.
Function switch TEST.
2.
RANGE switches Press and
release as required to obtain
80 mile display.
3.
BRT control As required.
4.
Screen Verify proper display.
(The test display consists of
two green bands, two yellow
bands, and a red band on a
120-degree scan. The word
TEST will be displayed in the
upper right corner. The
operating mode selected by
the MODE switches, either
MAP, WX, or WXA, will be
displayed in the lower left
corner. If WXA has been
selected, the red band in the
test pattern will flash on and
off.
The
range
will
be
displayed in the upper right
corner
beneath
the
word
TEST and appropriate range
mark distances will appear
along the right edge of the
screen.)
(a)
Weather
observation
operating
procedure:
1.
Function switch ON.
2.
MODE switches Press and
release as required to select
WX.
3.
BRT control As required.
4.
TILT
control
Adjust
until
weather pattern is displayed.
Include the areas above and
below the rainfall areas to
obtain a complete display.
5.
MODE switches Press and
release to select WXA. Areas
of intense rainfall will appear
as flashing red. These areas
must be avoided.
6.
TRACK switches Press to
move track line through area
of least weather intensity.
Read
relative
position
in
degrees in upper left corner of
screen.
NOTE
Refer to TM 1-230 for weather
observation,
interpretation
and
application.
(b)
Ground
mapping
operating
procedure: 1. Function switch ON.
2.
MODE switches Press and
release as required to select
MAP.
3.
BRT control As required.
4.
GAIN control As required to
present usable display.
(4)
Standby procedure. Function switch
STBY.
d.
Shutdown procedure: Function switch OFF.
e.
Emergency operation. Not applicable.
3-30. TRANSPONDER SET (APX-100).
a.
Description. The transponder system receives,
decodes, and responds to interrogations from Air Traffic
Control (ATC) radar to allow aircraft identification,
altitude reporting, position tracking, and emergency
tracking. The system receives a radar frequency of
1030 MHz and transmits preset coded reply pulses on a
radar frequency of 1090 MHz at a minimum peak power
of 200 watts. The range of the system is limited to line-
of-sight.
The transponder system consists of a combined
receiver/transmitter/ control panel (fig. 3-25) located on
the pedestal extension; a pair of remote switches, one
on each control wheel; and two antennas, located on the
underside and top of the fuselage. The system is
protected by the 3-ampere TRANSPONDER and the 35-
ampere AVIONICS MASTER PWR #1 circuit breakers
on the overhead circuit breaker panel (fig. 2-26).
b.
Transponder Control Panel fig. 3-25).
CONTROL
FUNCTION
TEST/GO
Illuminates
to
indicate
successful
indicator
completion of built-in-test (BIT).
TEST/MON
Illuminates to indicate system indicator
malfunction or interrogation by a ground
station.
ANT switch
Selects desired antenna for signal input.
TOP
Selects upper antenna.
DIV
Selects diverse (both) antennas.
BOT
Selects lower antenna.
RAD TEST
Enables reply to TEST mode in-
OUT switch
terrogations from test set.
3-74