AS838: 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.

Meta Tags

Topics: Seals and gaskets
Fasteners
Flight control systems
Throttles
Turboprop engines
Hydraulic fluids
Aluminum alloys
Copper alloys
Nuts

Details

DOI: https://doi.org/10.4271/AS838

Pages: 12

Citation: SAE International Technical Standard, Aircraft Hydraulic Starter/Pumps, SAE Standard AS838, Reaffirmed April 2005, Issued January 1968, https://doi.org/10.4271/AS838.

Additional Details

Publisher: SAE International

Published: Apr 26, 2005

Product Code: AS838

Content Type: Technical Standard

Status: Reaffirmed

Language: English

Historical