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|  MIL-N-85005A(AS)
Appendix
INS Warn - The Control-Indicator shall provide an indicator
30.5.3.5.2
lamp to signal when the INS annunciates INS Master Warning on the INS
Control Display Unit. The Control-Indicator shall include a lamp driver
circuit when shall present a load of 20,000 or more ohms referenced to
aircraft ground and shall operate according to the following logic:
Greater than 17 VDC = WARN
= NOT WARN
Less than 3.5 VDC
The lamp shall be illuminated amber when the INS signals WARN. The lamp
shall provide integral push-to-test function and adjustable brightness
control.
Aircraft Power - The equipment shall utilize aircraft power
30.5.3.6
as follows:
(1) 0 - 26 VAC, 400 Hz, 1 0, 0.6 amp.
(2) 28 VDC, 4 watts
Panel Illumination - The Control-Indicator shall incorporate
30.5.3.7
an integrally illuminated information panel per MIL-P-7788, Class 1R,
type V. The panel shall utilize 26V, 400 Hz, aircraft dimmable power.
Electrical Connections - Connections to external circuits
30.5.3.8
shall be as listed.
Reference
Function
Receptacle Type
Designation
To aircraft and system
SJTP02RE10-35PB(023)
J1
Mounting - The Control-Indicator shall meet the requirements
30.5.3.9
of MIL-C-6781 for Type II control panels, and shall utilize the mounting
dimensions of MS33638.
30.5.3.10
Color - The Control-Indicator shall be painted lusterless
black, No. 37038, in accordance with FED-STD-595.
40.
NOTES
Associated Equipment - Inertial Navigation Set per ARINC 561-8.
40.1
U.S. GOVERNMENT PRINTING OFFICE : 1978-703-122/3598
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