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SAE AMS3267

Revision B, July 20, 2004

Complete Document

Sealing Compound, Low Adhesion, Corrosion Inhibiting for Removable Panels and Fuel Tank Inspection Plates

Includes all amendments and changes through Cancellation Notice , July 2004


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Superseded By: SAE AMS3284

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Additional Comments:
CNCL S/S BY SAE AMS3284*COMPLETE REPRINT W/NOTICE
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Product Details:

  • Revision: Revision B, July 20, 2004
  • Published Date: July 2004
  • Status: Superseded By:
  • Superseded By: SAE AMS3284
  • Document Language: English
  • Published By: SAE International (SAE)
  • Page Count: 14
  • ANSI Approved: No
  • DoD Adopted: No

Description / Abstract:

Form:

This specification and its supplementary detail specifications cover accelerated curing synthetic rubber compounds with corrosion inhibitors and low adhesive strength, supplied as a two-component system, curing at room temperature.

Application:

This product has been used typically for sealing aircraft access doors and accessories where gaskets are required, but usage is not limited to such applications. The sealing compounds are resistant to both jet fuels and high aromatic aviation gasolines and are usable from -55 to +120 °C (-67 to +248 °F).

Safety - Hazardous Materials:

While the materials, methods, applications, and processes described or referenced in this specification may involve the use of hazardous materials, this specification does not address the hazards which may be involved in such use. It is the sole responsibility of the user to ensure familiarity with the safe and proper use of any hazardous materials and to take necessary precautionary measures to ensure the health and safety of all personnel involved.

Classification:

The requirements specified herein and in the applicable detail specification define each sealing compound on the basis of property characteristics and application time, as shown in the title of each detail specification.

AIA/NAS Aerospace Standards