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|  MIL-N-81497A(AS)
Electrical Connectors - The Computer, Navigation
3.5.5.15
shall have the following connectors:
Function
Type
Designation
Power Supply
Cable to:
MS3122-22E-55PX
4J1
Aircraft
Cable to:
MS3122-24E-61SZ
4J2
Cable to: Control,
MS3122-24E-61SN
4J3
Gyroscope Assembly
Aircraft
Cable to:
MS3122-24E-61PW
4J4
MS3122-24E-55SY
Cable to: Aircraft
4J5
Test Connector
M81511/01E16-55S2
4J6
Test Connector
M81511/01E16-55S1
4J7
Color - The Computer, Navigation shall be lusterless
3.5.5.16
gray 36231 as specified in FED-STD-595.
Mounting - Computer, Navigation mounting shall be
3.5.5.17
in accordance with MS91403.
Power Supply PP-4964/ASN-84 - The Power Supply shall
3.5.6
meet the following requirements.
Function - The Power Supply shall generate the reg-
3.5.6.1
ulated DC voltages required by the INS. It shall include a battery
capable of maintaining critical equipment operation, as defined in
3.4.1.3
during temporary loss of aircraft power. The Power Supply
shall also distribute aircraft 400 Hz power as required. BITE shall
be provided as part of the Power Supply unit to determine its GO or
NO-GO status. The battery shall be considered as a separate LRU.
Form Factor - Form factor of the equipment shall con-
3.5.6.2
form to EI-554. Maximum envelope dimensions shall be 15 inches by
11.5 inches by 7.625 inches,
The weight of the Power Supply shall not
Weight -
3.5,6.3
exceed 23.6 pounds.
48
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