(R) Lubricant, Solid Film, Heat Cured, Corrosion Inhibiting Procurement Specification
|Publication Date:||1 July 2005|
This SAE Aerospace Standard (AS) establishes the requirements for heat cured solid film lubricants. For other general or high temperature applications, see AS1701.
For applications where temperatures may range from -90 to 400 °F (-68 to 204 °C).
This specification establishes the following types:
Type I: A lubricant capable of being cured within 60 minutes at 302 °F ± 27 °F (150 °C ± 15 °C) with an endurance life of 250 minutes minimum. See 6.4 for related product information.
Type II: A lubricant capable of being cured within 60 minutes at 400 °F ± 27 °F (204 °C ± 15 °C) with an endurance life of 450 minutes minimum. See 6.4 for related product information.
Type III: A low volatile organic compound (VOC) content lubricant capable of being cured within 120 minutes at 302 °F ± 27 °F (150 °C ± 15 °C) or within 60 minutes at 400 °F ± 27 °F (204 °C ± 15 °C) with an endurance life of 450 minutes minimum. Type III shall be used when performance is satisfactory for the desired application to meet VOC emission regulations.
Color 1 - Natural product color.
Color 2 - Black color. See 3.7.
See 6.4 for related product information.
Safety - Hazardous Materials:
While the materials, methods, applications, and processes described or referenced in this specification may involve use of hazardous materials, this specification does not address the hazards which may be involved in such use. The product manufacturer shall prepare Materials Safety Data Sheets (MSDS) in accordance with AMS 2825 and abide by MSDS requirements to ensure familiarity with the safe and proper handling of hazardous materials used and take necessary precautionary measures to ensure the health and safety of all personnel involved.