Document ID:	MIL-STD-5522       Scroll down to access document images

Overview

Title:  Test Requirements and Methods for Aircraft Hydraulic and Emergency Pneumatic Systems Scope:  This standard establishes test and test method requirements for aircraft and weapons hydraulic and emergency pneumatic systems design and installation with operating pressure ranges from 3,000 psi to 8,000 psi and temperature ranges from -65 deg. F to + 450 deg. F. Status:  Active Document Date:  04-JUN-2024         Next Review Due:  03-JUN-2029 FSC/Area:  1650 Doc Category:   Military Standard -Test Method Standard

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

Changes to military standards or handbooks issued after August 1, 2003 are incorporated in the modified document.

Revision History

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