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Data updated: 09 Jan 2026.
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Document ID:
MIL-A-23622
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Overview
Title:
Actuator, Aircraft, Electro-Mechanical, Linear, Direct Current
Scope:
This specification defines the requirements for the design and testing of linear electro-mechanical actuators which are electrically reversible and mechanically irreversible with adjustable limit switches, operable from a 20 volt direct current system.
Status:
Inactive
Document Date:
30-JUL-2019
Next Review Due:
27-JUL-2029
FSC/Area:
1680
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
Notice 3 - Validation
A
30-JUL-2019
1
1.9 KB
Amendment 1
A
21-JUN-2001
2
4.1 KB
Notice 2 - Inactivation
A
15-JUL-1993
1
7.2 KB
Notice 1 - Inactivation
A
03-DEC-1990
1
22.4 KB
Base Document
A
15-APR-1963
19
259.7 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.