AS4775A Aircraft Maintenance Jacks - General Requirements

Reaffirmed

01/14/2011

Features
Issuing Committee
Scope
Content
This document covers the general requirements for hydraulic aircraft jacks. It can be applied to tripod, unipod, and axle jacks that may be used on open ramp areas as well as in the aircraft hanger.
Throughout this Aerospace Standard, the minimum essential criteria are identified by the key word “shall”. Recommended criteria are identified by use of the key word “should”. Deviation from recommended criteria should only occur after careful consideration and thorough service evaluation have shown alternate methods to provide an equivalent level of safety.
The term “vertical load” throughout this Aerospace Standard is defined as the force imposed on the aircraft jack at the airframe jack point.
Meta TagsDetails
DOI
https://doi.org/10.4271/AS4775A
Pages
17
Citation
SAE International Technical Standard, Aircraft Maintenance Jacks - General Requirements, SAE Standard AS4775A, Reaffirmed January 2011, Revised December 2004, Issued July 1994, https://doi.org/10.4271/AS4775A.
Additional Details
Publisher
Published
Jan 14, 2011
Product Code
AS4775A
Content Type
Technical Standard
Status
Reaffirmed
Language
English

Revisions