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|  MIL-C-38418E(AS)
(Copies of specifications, standards, drawings, and publications required
by contractors in connection with specific procurement functions should
be obtained from the procuring activity or as directed by the contracting
officer.)
3.
REQUIREMENTS
3.1
First Article - When specified in 6.2, the contractor shall
furnish sample units for first article inspection and approval (see 4.4
and 6.2).
3.2
Components - The Attitude Gyroscope Control Assembly shall consist
of the following:
a.
A/A24G-39 Control Assembly
(1)
Gyroscope, Displacement, SBK-11A/A24G-26
(2)
Amplifier, Electronic Control,
ASK-32/A24G-39 (fixed wing aircraft)
or,
ASK-441A24G (rotary wing aircraft)
(3)
Controller, Compass System,
(white-lighted)
DCK-128/A24G
(red-lighted)
or,
DCK-129/A24G
(white-lighted, IPL)
or,
DCK-228/A24G
(moisture-sealed, white-lighted)
or,
DCK-234/A24G
(Moisture-sealed, red-lighted)
or,
DCK-235/A24G
(Moisture-sealed, white-lighted, IPL)
DCK-236/A24G
or,
3.2.1 Application Considerations - The A/A24G-39 Control Assembly shall
be supplied for installations requiring four heading outputs, a single
roll output, a single pitch output, and azimuth rate roll erection
The Compass System Controller is available in different
control.
configurations to meet various flight deck lighting requirements and
installation considerations (see 6.2). The Electronic Control Amplifier
is to be selected to meet the performance criteria of the applicable
aircraft (see 6.2).
3.2.2 Associated Equipment - The equipment shall operate properly with
the following associated equipment in accordance with 3.7:
4
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