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Data updated: 12 Jan 2026.
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Document ID:
MIL-T-5522
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Overview
Title:
Test Requirements and Methods for Aircraft Hydraulic and Emergency Pneumatic Systems (S/S By MIL-STD-5522)
Scope:
This specification establishes requirements for tests and methods for the testing of aircraft hydraulic systems deisgned in accordance with requirements of MIL-H-5440, MIL-H-8891, and of aircraft pneumatic systems designed in accordance with requirements of MIL-P-5518.
Status:
Canceled
Cancellation Date:
26-SEP-2000
FSC/Area:
1650
Doc Category:
Detail Specification
Responsibilities
Lead Standardization Activity:
AS
Naval Air Systems Command
Preparing Activity:
AS
Naval Air Systems Command
Coordination:
Full
Army Custodian:
AV
Combat Capabilities Development Command, Aviation and Missile Center
Navy Custodian:
AS
Naval Air Systems Command
Air Force Custodian:
99
Air Force Life Cycle Management Center - Item Reduction Support
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 D Notice 2 - Cancellation
A
26-SEP-2000
1
2.8 KB
Revision D Notice 1 - Validation
A
25-AUG-1987
1
2.2 KB
Revision D Amendment 1
A
28-SEP-1979
1
3.1 KB
Revision D
A
30-SEP-1975
51
1568.4 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.