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Consider also that a prop is an e=ADssential
non-redundant monolithic structure, which if aluminum, is ma=ADde of a material (2024-T3) that has good tensile, but mediocre fract=ADure toughness properties. Lightplane props are universally made of 2025T6, according to my Sensenich prop manual. 2024T3 is used mostly for aircraft skins. The 2025 lacks the manganese and magnesium of the 2024, but has silicon that the 2024 doesn't have. The yield and tensile strengths of 2025T6 are a bit less than 2024T3, but the metal isn't as hard, likely reducing crack tendencies somewhat. The copper is still present, making the prop corrosion-prone, and in Canada, at least, we have to remove the prop, strip it and inspect it for corrosion at least every five years. Corrosion pits can be as bad as nicks for starting cracks. Dan |
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