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|  MIL-C-62204B(AR)
3.3.4 Replies display count. - With tthe logical one digital type - A signal
item 3.1 of table I, present at pins P1-13A, -28A, -29A, -30A and -32A and
with the signal input conditions of table III established in any item order,
the output replies data waveform of figure 5 shall appear at pins as specified
in table III. (See 4.6.2.4)
3.3.5 Malfunction display count. - With the logical one digital type - A
signal item 3.1 of table I, present at pins P1-lA, -2A, -3B, -4A, -5B, -6A,
-7B, -8A, -9A, -10A, -11B and -12A, with the logical zero digital type-A
signal item 3.1 of table I, present at pins P1-14A, -17A, -18A and -20A and
with the signal input conditions if table IV established in any item order,
the output malfunction data waveform of figure 6 shall appear at pins as
specified in table IV. (See 4.6.2.5)
3.3.6 Lamp test. - With the logical one digital type-A signal, item 3.1
of table I, present at pins P1-28A, P1-29A, P1-30A, P1-32A and P1-30B, the
output condition at pin P1-25A shall be 1.8 0.3 Vdc. With the logical zero
digital type - A signal, item 3.1 of table I, present at pin P1-30B, the output
condition at pin P1-25A shall be 14.0 0..5 Vdc. (See 4.6.2.6)
3.3.7 Blanking test. - With the logical digital type-A signal, item 3.1
of table I, present at pins P1-29A, P1-30A, P1-32A and-P1-30B and a logical
zero type - A signal present at pin p1-28A and with a RANGE signal applied in
accordance with figure 7, the blanking output and MALF LIGHT RET output shall
be as specified in figure 7. (See 4.6.2.7)
3.4 Environmental.
3.4.1 Shock. The assembly shall be capable of operating as specified
herein after exposure under the conditions of 3.1.3 to three half sine wave
shock pulses of 40 4 gravity units (g) for a duration of 18 3 milliseconds
(msec) applied in each direction along three mutually perpendicular axes. In
addition, the assembly shall be capable of withstanding three half sine wave
shock pulses of 100.0 10.0 g for a duration of 1.5 0.2 msec applied in
each direction along three mutually perpendicular axes. (See 4.6.3.1)
3.4.2 Vibration. The assembly shall be capable of operating as specified
herein after exposure under the conditions of 3.1.3 to the vibration profile
of figure 8. Duration of exposure shall be not less than 80 minutes in each
of three mutually perpendicular axes. (See 4.6.3.2)
3.4.3 Operating temperature. The assembly shall be capable of operating
as specified herein over the operating temperature range of -25F to
+140F. (See 4.6.3.3, 4.6.3.4 and 4.6.3.5)
3.4.4 Storage temperature. The assembly shall be capable of operating as
specifies herein after exposure to storage temperatures ranging from -65F
to +160F. (See 4.6.3.3, 4.6.3.4 and 4.6.3.5)
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