AS5440: Hydraulic Systems, Aircraft, Design and Installation Requirements For - Technical Standard

Features

Scope

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

Meta Tags

Topics: Hydraulic systems
Fixed-wing aircraft
Seals and gaskets
Fluid power systems
Valves
Fittings
Flight control actuators
Electric motors
Valve trains
Corrosion resistant alloys

Details

DOI: https://doi.org/10.4271/AS5440

Pages: 56

Citation: SAE International Technical Standard, Hydraulic Systems, Aircraft, Design and Installation Requirements For, SAE Standard AS5440, Issued April 1998, https://doi.org/10.4271/AS5440.

Additional Details

Publisher: SAE International

Published: Apr 1, 1998

Product Code: AS5440

Content Type: Technical Standard

Status: Current

Language: English

Historical