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SAE AS4299

Revision B, July 1, 2018

Complete Document

Rings, Retaining - Spiral Wound, Uniform Section Corrosion and Heat Resistant, UNS S66286



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Product Details:

  • Revision: Revision B, July 1, 2018
  • Published Date: July 2018
  • Status: Active, Most Current
  • Document Language: English
  • Published By: SAE International (SAE)
  • Page Count: 22
  • ANSI Approved: No
  • DoD Adopted: Yes

Description / Abstract:

Type

This procurement specification covers retaining rings of the spiral wound type with uniform rectangular cross-section, made of a corrosion and heat resistant age hardenable iron base alloy of the type identified under the Unified Numbering System as UNS S66286, work strengthened and heat treated to a tensile strength of 185 to 240 ksi at room temperature.

Application

Intended for use on aerospace propulsion systems for retaining parts on shafts and in housing bores where high strength at temperatures up to approximately 900 °F is required.

Dimensions and Tolerances

Unless otherwise specified herein, dimensions and tolerances are in inches.
AIA/NAS Aerospace Standards