AS4052A Gland Design: Scraper, Landing Gear, Installation

Reaffirmed

08/02/2006

Features
Issuing Committee
Scope
Content
This SAE Aerospace Standard (AS) covers an alternate gland design for the installation of scraper/wiper rings in the lower end of landing gear shock struts for the purpose of contaminant exclusion.
The defined scraper gland covered by this document, as shown in Table 1, is a variant of AS4716, the accepted gland standard for MS28775, O-ring packing seals. Piston diameters, gland internal diameters, groove sidewall angles and the surface finish are all defined by AS4716, but the gland outer retaining wall diameter is changed.
AS4088 is similar to this document, but was developed by SAE A-6 for flight control and general-purpose cylinders. It differs from this document primarily by the clearance between the rod (piston) and outer gland wall. Since landing gears are more susceptible to dirt contamination, the additional clearance provides a larger path to allow excessive dirt accumulation to exit the gland.
Rationale
Content
This document has been reaffirmed to comply with the SAE 5-year Review policy.
Meta TagsDetails
DOI
https://doi.org/10.4271/AS4052A
Pages
5
Citation
SAE International Technical Standard, Gland Design: Scraper, Landing Gear, Installation, SAE Standard AS4052A, Reaffirmed August 2006, Revised April 2001, Issued April 1994, https://doi.org/10.4271/AS4052A.
Additional Details
Publisher
Published
Aug 2, 2006
Product Code
AS4052A
Content Type
Technical Standard
Status
Reaffirmed
Language
English

Revisions