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Page Title:
Controller, Mode C-10422/ASN-124 |
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|  MIL-N-85005A(AS)
Appendix
Input Power - No input power shall be required from the INS.
30.5.1.3
Controller, Mode C-10422/ASN-124 - The Controller shall meet
30.5.2
the following requirements:
30.5.2.1
Function - The Controller shall provide ON/OFF power control
of the NC, SDC, and the OR-90/ARN-99(V)1 Receiver-Converter. The con-
figuration of the front panel shall conform to Figure 42.
30.5.2.2
Form Factor - The Controller, exclusive of front panel
protrusions and attachment points, but including connector projections,
shall be formed within the following maximum dimensions (inches):
Width
Height
Depth
4.500 (behind mounting surface)
2.630
5.750
Weight - The weight of the Controller shall not exceed 2
30.5.2.3
pounds.
30.5.2.4
Controls - The Controller shall provide the following control:
Power - A two-position rotary switch shall control the
30.5.2.4.1
state of output discretes to the ASN-124, and shall switch power to the
OR-90/ARN-99. It shall be necessary to lift the switch in order to
change position.
30.5.2.5
Displays - The Controller shall provide the fallowing display:
30.5.2.5.1
Auto-Pilot Engage - The Controller shall provide an indicator
lamp to signal when the auto-pilot is engaged. The lamp shall be illum-
inated amber when the +28 VDC lamp power is supplied to the Controller.
Lighting Power - The equipment shall utilize aircraft lighting
30.5.2.6
power in accordance with paragraph 3.3.12 as follows:
0-26 VAC, 400 Hz, 1 0, 0.4 Amp.
Panel Illumination The Controller shall incorporate an
30.5.2.7
integrally illuminated information panel per MIL-P7788, Class 2W, Type
V. The panel shall utilize 26V, 400 Hz, aircraft dimmable power.
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