SAE AMS3697 Aerodynamic Fairing Compound, -55 to +150Mdc (-65 to +300Mdf)
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时间:2024-05-22 07:00:57
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Product Code:SAE AMS3697
Title:Aerodynamic Fairing Compound, -55 to +150Mdc (-65 to +300Mdf)
Issuing Committee:Ams G9 Aerospace Sealing Committee
Scope: This specification covers a two-component air-curing, aluminum-powder -filled, epoxy-resin-base material in the form of a paste or putty, suitable for application by spatula or putty-knife. Primarily for filling small holes, crevices, and gaps or for smoothing areas requiring thin layers of material to produce the required smoothness on aerodynamic surfaces subject to service temperatures from -55 to +150 degrees C (-65 to +300 degrees F).
Rationale: This specification covers a two-component air-curing, aluminum-powder -filled, epoxy-resin-base material in the form of a paste or putty, suitable for application by spatula or putty-knife. Primarily for filling small holes, crevices, and gaps or for smoothing areas requiring thin layers of material to produce the required smoothness on aerodynamic surfaces subject to service temperatures from -55 to +150 degrees C (-65 to +300 degrees F).
Title:Aerodynamic Fairing Compound, -55 to +150Mdc (-65 to +300Mdf)
Issuing Committee:Ams G9 Aerospace Sealing Committee
Scope: This specification covers a two-component air-curing, aluminum-powder -filled, epoxy-resin-base material in the form of a paste or putty, suitable for application by spatula or putty-knife. Primarily for filling small holes, crevices, and gaps or for smoothing areas requiring thin layers of material to produce the required smoothness on aerodynamic surfaces subject to service temperatures from -55 to +150 degrees C (-65 to +300 degrees F).
Rationale: This specification covers a two-component air-curing, aluminum-powder -filled, epoxy-resin-base material in the form of a paste or putty, suitable for application by spatula or putty-knife. Primarily for filling small holes, crevices, and gaps or for smoothing areas requiring thin layers of material to produce the required smoothness on aerodynamic surfaces subject to service temperatures from -55 to +150 degrees C (-65 to +300 degrees F).
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