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   Data updated: 26 Feb 2026. Home |  About Quick Search |  ASSIST |  ASSIST Updates Document Details
Document ID:   MIL-C-38418       Scroll down to access document images

Overview
Title:  Control Assembly, Gyroscope, Attitude A/A24G-39
Scope:  This specification covers the requirements for an Attitude Gyroscope Control Assembly, designated A/A24G-39, which provides pitch, roll, and heading angular displacements.
Status:  Inactive Document Date:  16-JUL-2024      
  Next Review Due:  14-JUL-2034
6610 Doc Category:   Detail Specification  

Responsibilities
Lead Standardization Activity:  71  Air Force Sustainment Center - Oklahoma City  
  Preparing Activity: AS  Naval Air Systems Command
Coordination:  Limited  
Navy Custodian:  AS   Naval Air Systems Command  

Amendments to military specifications or specification sheets issued after August 1, 2003 are incorporated in the modified document.
Revision History Click on column headings for a description of column content.
MediaDocument Part DescriptionDist StmtDocument DatePagesSize
Document ImageRevision E Notice 2 - ValidationA16-JUL-202411.9 KB
Document ImageRevision E Notice 1 - InactivationA31-MAR-199812.6 KB
Document ImageRevision E Amendment 2 A12-MAR-1985842.6 KB
Document ImageRevision E A30-JUL-198193563.1 KB

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