Lubricant, Solid Film, Heat Cured, Corrosion Inhibiting; Procurement Specification
|Publication Date:||1 March 1997|
This SAE Aerospace specification establishes the requirements for heat cured solid film lubricants for aerospace fastener/threaded applications only. For other general or high temperature applications, see AS1701.
For aerospace fastener applications where temperatures may range from −68 to 204°C (−90 to 400°F).
This specification establishes the following types:
Type I: A cure temperature of 150 ± 15°C (302 ± 27 °F) and endurance life of 250 min. Replaces MIL-L-46010, Type I.
Type II: A cure temperature of 204 ± 15°C (400 ± 27 °F) and endurance life of 450 min. Replaces MIL-L-46010, Type II.
1.3 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.