AS838A: Aircraft Hydraulic Starter/Pumps - Technical Standard

Features

Issuing Committee: A-6C4 Power Sources Committee

Scope

Content: This specification established (1) the common requirements for hydraulic units capable of functioning as starters and as pumps suitable for use in aircraft and missiles and (2) the methods to be used for demonstrating compliance with these requirements.

Rationale

Content: This document has been determined to contain basic and stable technology which is not dynamic in nature.

Meta Tags

Topics: Flight control systems
Hydraulic fluids
Aluminum alloys
Copper alloys
Automatic pilots
Pumps
Magnesium alloys

Details

DOI: https://doi.org/10.4271/AS838A

Pages: 13

Citation: SAE International Technical Standard, Aircraft Hydraulic Starter/Pumps, SAE Standard AS838A, Stabilized October 2013, Reaffirmed April 2005, Issued January 1968, https://doi.org/10.4271/AS838A.

Additional Details

Publisher: SAE International

Published: Oct 28, 2013

Product Code: AS838A

Content Type: Technical Standard

Status: Stabilized

Language: English

Historical