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SAE AMS1640

Revision C, December 1, 2011

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Corrosion Removing Compound for Aircraft Surfaces



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Product Details:

  • Revision: Revision C, December 1, 2011
  • Published Date: December 2011
  • Status: Active, Most Current
  • Document Language: English
  • Published By: SAE International (SAE)
  • Page Count: 6
  • ANSI Approved: No
  • DoD Adopted: Yes

Description / Abstract:

Form

This specification covers a corrosion-removing compound in the form of a liquid concentrate.

Application

This method is primarily concerned with the removal of pitting corrosion and heavy surface oxidation from exterior aluminum surfaces of aircraft.

Precautions

Compounds meeting the requirements of this specification may cause hydrogen embrittlement of high-strength steels and will remove cadmium plate.

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.

AIA/NAS Aerospace Standards