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Data updated: 22 Nov 2024.
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Document ID:
MIL-I-81683
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Overview
Title:
Indicator, Attitude Reference Self-Contained, 3-Inch, ID-1791/A
Scope:
The equipment covered by this specification is a Self-Contained Vertical Gyro Indicator System for Military Aircraft.
Status:
Inactive
Document Date:
11-JUL-2024
Next Review Due:
09-JUL-2034
FSC/Area:
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.
Media
Document Part Description
Dist Stmt
Document Date
Pages
Size
Revision A Notice 3 - Validation
A
11-JUL-2024
1
1.9 KB
Revision A Notice 2 - Inactivation
A
04-APR-1998
1
2.1 KB
Revision A Notice 1 - Validation
A
07-DEC-1987
1
20.4 KB
Revision A
A
17-SEP-1979
62
1942.1 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.
