AS838A Aircraft Hydraulic Starter/Pumps

Stabilized

10/28/2013

Features
Issuing 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 TagsDetails
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
Published
Oct 28, 2013
Product Code
AS838A
Content Type
Technical Standard
Status
Stabilized
Language
English

Revisions