SAE ARP1234C
Static Axial O-Ring Seal Applications Without Anti-Extrusion Devices for Engine and Engine Control Systems
Historical
Standard by SAE International, 2020-11-09
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About This Item
This document establishes standard gland design criteria and dimensions for static axial O-ring seal applications without anti-extrusion devices specifically for engines and engine control systems operating at a maximum pressure of 1500 psi (10345 kPa).
NOTE: The criteria herein are similar, but not identical, to those in AS4716 and the legacy standard MIL-G-5514.
This standard has been reformatted for ease of use, with no technical changes.
NOTE: This standard was transferred from E-25 General Standards for Aerospace and Propulsion Systems Committee to the A-6C Seals Committee.
Please request information about the document. Contact Page
Standard Details
- Publication Date: 2020-11-09
- Standard Status: historical
- Publisher: SAE International
- Document Type: Aerospace Standard
- Subject: Engine control systems, Seals and gaskets, , , , , , ,
- Official SAE: Doi link
