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SAE AS692

Revision A, April 3, 1972

Complete Document

Igniter, Spark, Aeronautical Engine (High Tension)

Includes all amendments and changes through Reaffirmation Notice , November 1992


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Product Details:

  • Revision: Revision A, April 3, 1972
  • Published Date: November 1992
  • Status: Active, Most Current
  • Document Language: English
  • Published By: SAE International (SAE)
  • Page Count: 4
  • ANSI Approved: No
  • DoD Adopted: No

Description / Abstract:

SCOPE

Scope: This specification establishes the performance, qualification, acceptance limits, and identification for aeronautical engine high tension spark igniters.

Classification: Spark igniters of the following gap types and outline configurations are covered by this specification.

OUTLINE CONFIGURATIONS

Class A - Flange mounted, right angle termination

Class B - Flange mounted, straight termination

Class C - Thread mounted

GAP TYPES

Type I - High voltage, air

Type II - High voltage, surface

Type III - High voltage, air surface

AIA/NAS Aerospace Standards