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Data updated: 16 Jan 2026.
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Document ID:
MIL-G-83824
Scroll down to access document images
Overview
Title:
Gyroscope, Rate, Type I, Type II, and Type III (No S/S Document)
Scope:
This specification covers the design and performance requirements for a rate gyroscope used in the F-4 aircraft Automatic Flight Control System.
Status:
Canceled
Cancellation Date:
09-JAN-2012
FSC/Area:
6615
Doc Category:
Detail Specification
Responsibilities
Lead Standardization Activity:
71
Air Force Sustainment Center - Oklahoma City
Preparing Activity:
70
Air Force Sustainment Center - Ogden
Coordination:
Limited
Air Force Custodian:
70
Air Force Sustainment Center - Ogden
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.
Media
Document Part Description
Dist Stmt
Document Date
Pages
Size
Notice 3 - Cancellation
A
09-JAN-2012
1
50.8 KB
Notice 2 - Validation
A
07-OCT-2008
1
1.9 KB
Notice 1 - Inactivation
A
15-MAY-1997
1
3.3 KB
Base Document
A
04-OCT-1991
21
1009.8 KB
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Defense Standardization Program
WARNING: UNAUTHORIZED ACCESS TO THIS UNITED STATES GOVERNMENT COMPUTER SYSTEM AND SOFTWARE IS PROHIBITED BY PUBLIC LAW 99-474 (THE COMPUTER FRAUD AND ABUSE ACT OF 1986) AND CAN RESULT IN ADMINISTRATIVE, DISCIPLINARY OR CRIMINAL PROCEEDINGS.