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MIL-N-81604C(AS)
Appendix I
Para 30.5.9.2
(cont)
a set (no-go) state, a ground shall be supplied. *
The relay contacts shall have a 28-volt d-c,
*
0.5-ampere capacity.  The common contact shall
be connected to ground.
e.
CAU No-Go - This discrete output from the CAU
to the SCRAM shall be provided to indicate that
the CAU malfunction flag has been set.  When
the flag is in a reset (go) state, an open
relay contact shall be supplied.  When the flag
is in a set (no-go) state, a ground shall be
*
supplied.  The relay contacts shall have a
28-volt d-c, 0.5-axnpere capacity.  The common
*
contact shall be connected to ground.
f.
INS No-Go - This discrete output from the CAU
to the CP shall go to the true (high) state to
indicate than AN/ASN-92(V) velocity data are
not valid.  The CAU line driver shall be a
Type 3 circuit.
INS Mode - This discrete output from the CAU
g.
to the SCRAM shall go to the true (high) state
to indicate that the AN/ASN-92(V) is in the
inertial mode of navigation.  The CAU line
driver shall be a Type 3 circuit.
h.
Doppler-INS Mode - This discrete output from
the CAU to the SCRAM shall go to the true (high)
state to indicate that the AN/ASN-92(V) is in
the doppler-inertial mode of navigation.  The
*
CAU line driver shall be a Type 3 circuit.
*
i.
MAG SLV or Free Mode - This discrete output
from the CAU to the SCRAM shall go to the true
(high) state to indicate that the AN/ASN-92(V)
is in the magnetic slave or free attitude refer- *
ence mode.  The CAU line driver shall be a
Type 3 circuit.
Vertical Reliability No. 1 - This discrete output
from the CAU to the AFCS shall be provided to
indicate the validity of the pitch and roll
outputs from the CAU.  When the attitude outputs
are valid, a Pair Of closed relay contacts shall *
be supplied.  When the attitude outputs are not
valid, a Pair of normally open relay contacts
*
shall be supplied.  The relay contacts shall have
a 28-volt d-c, 3-ampere capacity.
*
178

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