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MIL-C-38418 Revision E, July 30, 1981
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CONTROL ASSEMBLY,GYROSCOPE,ATTITUDE
Includes all amendments and changes through Interim Notice 1, March 31, 1998
Additional Comments: INAC FOR NEW DESIGN AFTER 3/31/98
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This specification covers the requirements for an Attitude Gyroscope Control Assembly, designated A/A24G-39, which provides pitch, roll, and heading angular displacements.

The equipment controlled by this specification shall consist of the following components in accordance with 3.2.
                         Type Designation

                     Control Assembly, Gyroscope
                     Attitude A/A24G-39 (see 3.5)

                     Gyroscope, Displacement (see 3.6)

                     Amplifier, Electronic Control (see 3.6)

                     Controller, Compass System (see 3.8)




This equipment shall operate with the associated equipment listed in 3.2.2. Beneficial comments (recommendations, additions, deletions, and any pertinent data which may be of use in improving this document) should be addressed to: Engineering Specifications and Standards Department (Code 93), Naval Air Engineering Center, Lakehurst, NJ 08733, by using the self-addressed Standardization Document Improvement Proposal (DD Form 1426) appearing at the end of this document or by letter.