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|  MIL-T-63536(AR)
Component Assembly,
A2
11830988
Torque Command
A4
11830798
Component Assembly,
Depression Limit
11830724
A5
Component Assembly
Coincidence Sensor
A6
11830797
Component Assembly
Interconnection
3.1.2 Government furnished property list. See 6.2c.
3.1.3 Electrical power supply. The LCU shall operate from power sources
with characteristics conforming to MIL-STD-704. The power supplies for all
acceptance tests shall be as specified in Table II.
TABLE II. Electrical power.
Input Power
Function
Pin
115 Vac (5%), 400 Hz (5%), 200 mA
J2-e
115 Vac
J2-f
115 Vac Return
115 Vac Return
28 (+0.5, -O) Vdc, Current of 1.5
J2-h
28 Vdc
amps
Ground
J2-g
Return for all dc
and 26 Vac supplies
26 Vac
26 Vac (5%), 400 Hz (5%), 8mA
J2-U
3.1.3.1 Ground. When the LCU is installed in the helicopter, the
enclosures mounting provisions shall be electrically bonded in accordance
with MIL-B-5087.
3.2 Material. Materials shall be in accordance with applicable drawings,
specifications, and standards.
3.3 Assembly. The Logic Control Unit Assembly shall comply with all
requirements specified on Drawing (Dwg) 11830922, all associated drawings, and
with all requirements specified in applicable specifications, and standards.
4
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