N/A
Carbon .38/.43 |
N/A Intended for use in the manufacturing of highly stressed aircraft parts requiring good hardenability as well as parts requiring high ultimate tensile strength. |
N/A This material in thicknesses up to 3/4" shall withstand being bent 90° around a diameter equal to its nominal thickness, both perpendicular and parallel to the direction of rolling. |
N/A
To develop the highest strength (260,000 psi minimum ultimate) with the best combination of mechanical properties in both transverse and longitudinal directions, the following thermal treatment is recommended:
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