Chemistry and potential.
Alloying elements establish the material family and its potential response: corrosion behavior, heat-treatability, weldability, conductivity, achievable strength, and finishing characteristics.
The alloy number tells you what the metal is. The temper suffix tells you what happened to it. You need both before strength, bendability, machining behavior, or finish can be specified.




In a designation such as 5052-H32 or 6061-T6, the four-digit number identifies the alloy family and chemistry. The suffix after the dash identifies the controlled condition created by fabrication, strain hardening, heat treatment, aging, or stress relief.
Aluminum-magnesium chemistry with its own registered composition limits.
The dash separates chemistry from condition.
Strain hardened, then stabilized.
Quarter-hard strain-hardening level.
Alloying elements establish the material family and its potential response: corrosion behavior, heat-treatability, weldability, conductivity, achievable strength, and finishing characteristics.
Processing determines how much of that potential has been developed and what condition arrives at the shop: soft, strain hardened, naturally aged, artificially aged, stabilized, or stress relieved.
For wrought aluminum, the first of four digits identifies the principal alloying family. That family is a useful first clue, but the complete four-digit designation defines the registered composition.
High aluminum content; often selected for conductivity, corrosion resistance, or forming.
Heat-treatable, high-strength family that includes 2024.
Non-heat-treatable sheet alloys with good forming and corrosion behavior.
Used in applications including filler metals; heat-treatability depends on the specific alloy.
Non-heat-treatable alloys such as 5052, strengthened mainly through cold work.
Heat-treatable family including versatile 6061 and architectural 6063.
Heat-treatable, high-strength family including 7075.
Specialized compositions not covered by the other principal families.
The second digit and final two digits have series-specific meanings. For 2xxx through 8xxx wrought alloys, the second digit generally indicates modification of the original alloy, while the last two identify the alloy registration. In 1xxx, the digits relate to purity and impurity control. Do not try to reconstruct exact chemistry from the number alone; use the registered composition and governing specification.
The basic temper letter describes the broad processing condition. Additional digits refine the treatment, degree of strain hardening, aging route, or stress-relief method.
No special control over strain hardening or thermal treatment after shaping. For wrought products, mechanical-property limits are not generally assigned to the F condition.
Process conditionApplied to wrought products annealed to obtain the lowest-strength condition. O tempers are often selected when maximum forming latitude is needed.
Softest conditionApplied to wrought products strengthened by cold work, with or without supplementary thermal treatment. Common for non-heat-treatable alloys.
Cold workAn unstable condition used only for alloys that naturally age after solution heat treatment. Time after heat treatment may be stated when it matters.
Unstable conditionStable conditions produced by thermal treatment, with or without supplemental strain hardening, other than F, O, or H.
Heat treatableH tempers normally use at least two digits. The first digit after H describes how strain hardening and supplementary treatment were combined. The second describes the degree of strain hardening.
Even-numbered degrees are commonly described as quarter-hard, half-hard, three-quarter-hard, and full-hard. These are standardized property positions relative to the annealed and full-hard conditions—not a statement that a specific percentage of forming capacity remains.
Odd second digits identify intermediate limits. A third H digit indicates a variation of the two-digit temper. Examples such as H111, H116, or H321 have definitions tied to alloy, product form, and registered requirements; they should be ordered by the complete designation rather than approximated from a nearby two-digit temper.
T tempers describe stable conditions achieved by controlled cooling, solution heat treatment, aging, and sometimes cold work. The order matters.
| Temper | Processing route | Practical reading |
|---|---|---|
| T1 | Cooled from an elevated-temperature shaping process, then naturally aged. | No deliberate cold work after cooling. |
| T2 | Cooled from elevated-temperature shaping, cold worked, then naturally aged. | Shaping heat + cold work + room-temperature aging. |
| T3 | Solution heat treated, cold worked, then naturally aged. | Common base route for 2024-T3 sheet. |
| T4 | Solution heat treated, then naturally aged. | More formable than a peak artificial-age condition in many alloy systems. |
| T5 | Cooled from elevated-temperature shaping, then artificially aged. | Often associated with press-quenched extrusions. |
| T6 | Solution heat treated, then artificially aged. | Common high-strength condition for 6061 and 7075. |
| T7 | Solution heat treated, then stabilized. | Overaged or stabilized to control properties such as corrosion response. |
| T8 | Solution heat treated, cold worked, then artificially aged. | Cold work occurs before artificial aging. |
| T9 | Solution heat treated, artificially aged, then cold worked. | Cold work occurs after artificial aging. |
| T10 | Cooled from elevated-temperature shaping, cold worked, then artificially aged. | Combines press cooling, cold work, and furnace aging. |
Additional digits can identify a registered variation of the basic temper or a stress-relief method. They often correlate with product form, so removing them can change both processing history and minimum properties.
Starts with the T6 route and adds stress relief by controlled stretching. Commonly specified for plate to reduce residual-stress movement during machining.
Stress relieved by stretching with minor straightening permitted after the stretching operation. Common for extruded rod, bar, profiles, and tube.
A compressive stress-relief route used for applicable products and registered tempers.
A 7075 condition combining a T73-class stabilized treatment with stress relief by stretching, selected when stress-corrosion resistance matters more than peak T6 strength.
Temper affects more than a tensile-property table. It can determine whether a bend cracks, a machined pocket moves, a welded region must be derated, or a finished part meets the drawing.
| Decision | Softer / annealed condition | Strain-hardened or heat-treated condition | What to verify |
|---|---|---|---|
| Bending | Usually more forming latitude and tighter achievable radii. | Higher crack risk and larger minimum bend radius; grain direction may matter more. | Alloy, temper, thickness, direction, inside radius, tooling, and bend test data. |
| Machining | May be gummy or less dimensionally stable depending on alloy and stock. | Often cuts more cleanly; stress-relieved plate can reduce movement. | Product form, residual stress, stock flatness, removal balance, and final tolerance. |
| Welding | Starting properties may be lower but forming is easier. | Heat can erase cold-work or precipitation-hardening benefits in the HAZ. | As-welded properties, filler, WPS, post-weld treatment, and structural calculation. |
| Laser cutting | Usually straightforward, but thin soft stock may be easier to distort. | Edge and flatness response vary with stress state and geometry. | Flatness, cut sequence, narrow webs, heat input, and downstream forming. |
| Anodizing | Temper can influence response, but alloy chemistry and surface condition usually dominate color and uniformity. | Alloy, finish type, pretreatment, cosmetic zone, rack marks, and approved sample. | |
Welding deserves special attention. Heat can locally anneal strain-hardened 5xxx material and reduce the precipitation-hardened strength of 6xxx or 7xxx material. The designation on incoming stock does not describe the final heat-affected-zone properties after welding.
Likewise, a stress-relieved temper helps control machining movement but does not guarantee a finished part will remain flat after aggressive, one-sided material removal. Toolpath strategy, workholding, thermal control, and roughing/rest cycles still matter.
A complete callout names the alloy, temper, product form, governing specification, stock size, finish, and certification requirements. The temper should never be guessed from the part description.
The temper designation is the letter-and-number suffix after the alloy number. It identifies the controlled mechanical or thermal processing condition, such as annealed, strain hardened, solution heat treated, naturally aged, artificially aged, or stress relieved.
Both are solution heat treated and artificially aged. T651 adds stress relief by controlled stretching, a condition commonly associated with plate. The applicable product form and governing specification must still be checked.
H3 means the product was strain hardened and then stabilized. The final 2 identifies a quarter-hard degree of strain hardening under the standard temper system.
Not automatically. Different tempers can have different minimum properties, residual stress, formability, corrosion behavior, conductivity, and product-form requirements. Any substitution should follow the controlling specification and engineering approval.
No. T6 describes a processing route, not a universal strength level. The resulting properties depend on alloy, product form, thickness, specification, and producer requirements.
This guide is educational. It does not replace the current ANSI standard, governing material or product specification, mill certification, approved design allowables, heat-treatment procedure, welding qualification, inspection plan, or engineering approval for the actual part.
Upload the CAD and drawing, choose the complete aluminum designation, and get manufacturing feedback before production begins.