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Page Title: IDENT Function
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IFF TRANSPONDER RESPONSE.
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Aviation Electronics Technician 1 (Organizational)
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Interrogator Set Major Components

airspeed-altitude   computer. All  framing  and information reply pulses are 0.45 (±0.1) microsecond wide.  All  modes  are  transmitted  by  the  RT  at  a frequency of 1090 MHz. Mode 1.— The reply pulse train consists of from zero to five information pulses framed by two framing pukes.  The  spacing  between  the  information  pulses  is in  multiples  of  2.9  (±0.05)  microseconds  from  the initial framing pulse.    The position where the sixth information   pulse   would   be   (17.4   [±0.05]   micro- seconds from the initial framing pulse) is not used. There are 32 different codes available for use from the specified five information pulses. Mode 2 and 3/A.— When transmitted, these reply trains contain from zero to 12 information pulses, plus the  two  framing  pulses.  The  information  pulse spacing is in multiples of 1.45 (±0.05) microseconds from the initial framing pulse. The position where the seventh  information  pulse  would  be  (10.5  [±0.05] microseconds  from  the  initial  framing  pulse)  is normally   not   used. There   are   a   possible   4,096 different  codes  available  from  the  specified  12 information  pulses. Mode  C.—  When  the  Airspeed-Altitude  Com- puter  is  connected  in  the  system,  the  reply  train consists  of  from  1  to  11  information  pulses  and  2 framing  pulses.  The  information  pulses  are  spaced  in multiples   of   1.45   (±0.05)   microseconds   from   the initial   framing   pulses. The  positions  where  the seventh  and  the  ninth  pulses  are  normally  located (10.5  [±0.05]  and  13.05  [±0.05]  microseconds  from the initial framing pulse) are not used. When there is a  pulse  in  the  thirteenth  position  (18.85  [±0.05] microseconds  from  the  initial  framing  pulse),  there  is a special position indicator pulse also generated in the train.  This  pulse  is  located  24.65  (±0.05)  micro- seconds  from  the  initial  framing  pulse.  There  is  a total   of   2,048   possible   codes   available   from   the specified   11   information   pulses.   When   the airspeed-altitude computer is not on-line, the reply train will be the framing pulses only. Mode 4.— This reply train is determined by the KIT-1A/TSEC. IDENT   Function.—   The    identification-of- position (IDENT) function is used in modes 1, 2, and 3/A. The IDENT function, which can be selected by the   pilot   for   transmission   for   approximately 20-second  intervals,  is  used  to  distinguish  between aircraft  displaying  the  same  coding.  When  used  in mode 1, the reply pulse train containing the code in use is transmitted twice for each trigger puke received. The second train is 24.65 (±0.05) microseconds from the  leading  edge  of  the  first  framing  pulse  of  the  first reply train. The IDENT function in modes 2 and 3/A uses the special position indicator (SPI) pulse. The reply pulse train containing the code in use is followed by a pulse for each trigger received. This SPI pulse is 24.65 (±0.05) microseconds from the leading edge of the first framing pulse of the reply train. Emergency  Function.—  The   EMERGENCY signals are selected by the pilot to indicate an in-flight emergency.  The  emergency  function  is  used  with modes  1,  2,  and  3/A.  For  modes  1  and  2,  the  reply pulse train containing the code in use is transmitted once  for  each  trigger  pulse  received,  followed  by three sets of framing pulse pairs with no information pukes. The three sets of framing pulses are located 24.65   (±0.1),   44.95   (±0.15),   49.30   (±0.20),   69.60 Figure 3-21.-Normal reply pulse characteristics. 3-19

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