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Page Title:
Control-Indicator C-9863/ASN-124 |
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|  MIL-N-85005A(AS)
Input Power
3.5.11.7
Aircraft Power - The equipment shall utilize air-
3.5.7.11.7.1
craft power in accordance with Paragraph 3.3.12 as follows:
(1) 26 VAC, 400 Hz, 1 0, 0.8 Amp
(2) 0-26 VAC, 400 Hz, 1 0, 0.4 Amp
System Power - The equipment shall utilize system
3.5.11.7.2
power as follows:
(1) 5 VDC, 0.4 Amp, regulated, from the SDC
(2) 5 VDC, 0.1 Amp, regulated, from the PP-4964/ASN-84
Inertial Power Supply.
Panel Illumination - The Controller shall incorporate
3.5.11.8
an integrally illuminated information panel per MIL-P-7788, Class 1-R,
Type V. The panel shall utilize 26 V, 400 Hz aircraft dimmable power.
*3.5.11.9
Electrical Connections - Electrical connections to
external circuits shall be as listed:
Reference
Function
Receptacle Type
Designation
SJTP02RE14-35PB(023)
Logic Power and
J1
Discretes
Lighting Power
SJTP02RE10-98P(023)
J2
Mounting - The Controller shall be a console mounted
3.5.11.10
unit in accordance with MIL-C-6781, Type 1.
Color - The Controller shall be painted lusterless
3.5.11.11
black, No. 37038, in accordance with FED-STD-595.
Control-Indicator C-9863/ASN-124 - The Control-
3.5.12
Indicator shall meet the following requirements:
Function - The Control-Indicator shall provide
3.5.12.1
selection of radio navigation aids or the Navigation-Display Set as the
source of data for the HSI. It shall also provide an
annunciator to indicate when True Heading data is being displayed. The
front panel shall conform to Figure 37.
Form Factor - The Control-Indicator, excluding front
3.5.12.2
panel protrusions, but including the rear connector, shall be formed
within the following maximum dimensions (inches).
Depth
Width
Height
2.200 (behind mounting
2.500
1.500
surface)
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