AS5440A: Hydraulic Systems, Military Aircraft, Design and Installation, Requirements For - Technical Standard

Features

Issuing Committee: A-6A2 Military Aircraft Committee

Scope

Content: This specification covers the design and installation requirements for Types I and II military aircraft hydraulic systems.

Meta Tags

Topics: Fixed-wing aircraft
Flight control actuators
Flight control systems
Hydraulic systems
Hydraulic fluids
Hydraulic control
Military aircraft

Details

DOI: https://doi.org/10.4271/AS5440A

Pages: 44

Citation: SAE International Technical Standard, Hydraulic Systems, Military Aircraft, Design and Installation, Requirements For, SAE Standard AS5440A, Revised January 2011, Issued April 1998, https://doi.org/10.4271/AS5440A.

Additional Details

Publisher: SAE International

Published: Jan 3, 2011

Product Code: AS5440A

Content Type: Technical Standard

Status: Revised

Language: English

Historical