Static Axial O-Ring Seal Applications Without Anti-Extrusion Devices for Engine and Engine Control Systems
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.