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|  MIL-PJ-81497A(AS)
3.4.3.2.3 (Continued)
Dual Equipment Interface - The interface
(9)
between the equipment and the altimeter shall
be designed to permit operation when either
1 or 2 identical ASN-84 equipments are connected
in parallel to the altimeter.
-3.4.3.2.4
Power On Signal - The equipment shall receive an
external Power On signal of aircraft DC ground potential and current
rating of 0.5 ampere. Absence of this signal, open circuit condition,
shall be supplied to shut off the equipment and shall be provided
when aircraft power interruption exceeds 10 SEC in duration.
3.4.3.3
Displays - The INS shall have the following visual
outputs as specified in 3.5.
Magnetic Synchronization Indicator
On Lamp
Align indicators
2 MIN to GO indicator
Test Mode Indicators
System Fail indicators
Mode indicators
LRU Fail indicators
Doppler Available indicator
Damping ON indicator
Battery in Use indicator
Present Latitude and Longitude
Present Position Insertion and Update indicators
3.4.3.4
Electrical Outputs -
20
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