•
T1- cooled from an elevated temperature shaping process and naturally
aged to a substantially stable condition.
•
T2- cooled from an elevated temperature shaping process, cold
worked, and naturally aged to a substantially stable condition.
•
T3- solution heat-treated, cold worked, and naturally aged to
a substantially stable condition.
•
T4- solution heat-treated and naturally aged to a substantially
stable condition.
•
T5- cooled form an elevated temperature shaping process and then
artificially aged.
•
T6- solution heat treated and then artificially aged
•
T7- solution heat treated and stabilised
•
T8- solution heat treated, and then artificially aged.
•
T9- solution heat-treated, artificially aged, and then cold worked.
•
T10- cooled from an elevated temperature shaping process, cold
worked and then artificially aged. Some additional digits have been
assigned for specific conditions such as stress-relieved tempers,
as follows.
•
T51- stress relieved by controlling stretching. This applies to
plate. For extrusions there are two subdivisions.
•
T510- for products that receive no further straightening after
stretching.
•
T511- for products that may receive minor straightening after
stretching, to comply with tolerances.
Among
the commonly used T-51 conditions are:
•
T351- solution heat treated, cold worked, controlled stretching
and naturally aged.
•
T651- solution heat treated, controlled stretched and artificially
aged.
•
T851- solution heat treated, cold worked, controlled stretched
and artificially aged.
•
T7351- solution heat treated, controlled stretched and artificially
aged to provide optimum stress corrosion resistance but with 15-20%
lower tensile properties than T6.
•
T7651- solution heat treated, controlled stretched and artificially
aged to achieve optimum exfoliation resistance corrosion resistance
but with about 10% lower tensile properties than T6.
•
T52- stress relieved by compressing.
•
T54- stress relieved by combining stretching and compressing.