Aluminum Designation Field Guide

Alloy + Temper

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.

ANSI H35.1 SystemUpdated August 202614 minute read
Decode the complete designation
6061T6511
6061Alloy chemistry: magnesium + silicon series
T6Solution heat treated + artificially aged
511Stress relieved by stretching; minor straightening permitted
Mill-finish 1100-H14 aluminum
1100-H14
Commercially pure · Half hard
Mill-finish 5052-H32 aluminum
5052-H32
Strain hardened · Stabilized
Mill-finish 6061-T6 aluminum
6061-T6
Solution treated · Artificially aged
Mill-finish 7075-T6 aluminum
7075-T6
High strength · Heat treatable
01 Basics02 Alloy Families03 F O H W T04 H Tempers05 T Tempers06 Suffixes07 Fabrication08 Drawings09 FAQ
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01 / Read the Whole Code

Alloy and temper answer different questions.

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.

Alloy
5052

Aluminum-magnesium chemistry with its own registered composition limits.

Separator

The dash separates chemistry from condition.

Basic temper
H3

Strain hardened, then stabilized.

Degree
2

Quarter-hard strain-hardening level.

The alloy controls

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 temper controls

Delivered condition.

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.

T6 is not a strength grade.T6 describes a processing route. 6061-T6 and 7075-T6 have very different properties because their chemistries respond differently. Always look up values for the complete alloy, temper, product form, and thickness.
02 / Wrought Alloy Families

The first digit points to the alloy family.

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.

1xxx

Unalloyed aluminum

High aluminum content; often selected for conductivity, corrosion resistance, or forming.

2xxx

Copper

Heat-treatable, high-strength family that includes 2024.

3xxx

Manganese

Non-heat-treatable sheet alloys with good forming and corrosion behavior.

4xxx

Silicon

Used in applications including filler metals; heat-treatability depends on the specific alloy.

5xxx

Magnesium

Non-heat-treatable alloys such as 5052, strengthened mainly through cold work.

6xxx

Magnesium + silicon

Heat-treatable family including versatile 6061 and architectural 6063.

7xxx

Zinc

Heat-treatable, high-strength family including 7075.

8xxx

Other elements

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.

03 / Five Basic Temper Designations

Start with the first letter.

The basic temper letter describes the broad processing condition. Additional digits refine the treatment, degree of strain hardening, aging route, or stress-relief method.

F

As fabricated

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 condition
O

Annealed

Applied to wrought products annealed to obtain the lowest-strength condition. O tempers are often selected when maximum forming latitude is needed.

Softest condition
H

Strain hardened

Applied to wrought products strengthened by cold work, with or without supplementary thermal treatment. Common for non-heat-treatable alloys.

Cold work
W

Solution heat treated

An unstable condition used only for alloys that naturally age after solution heat treatment. Time after heat treatment may be stated when it matters.

Unstable condition
T

Thermally treated

Stable conditions produced by thermal treatment, with or without supplemental strain hardening, other than F, O, or H.

Heat treatable
“Temper” does not simply mean hardness.The code records a controlled processing history. Two conditions can have similar hardness while differing in residual stress, conductivity, corrosion response, stability, or minimum-property requirements.
04 / Strain-Hardened H Tempers

H codes use process + degree.

H 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.

H1
Strain hardened only
Cold worked to obtain the required strength without a supplementary thermal treatment.
H2
Strain hardened + partially annealed
Cold worked beyond the final requirement, then partially annealed back to the specified strength.
H3
Strain hardened + stabilized
Cold worked, then stabilized at a relatively low temperature to reduce later softening. 5052-H32 is a common example.
H4
Strain hardened + coated
Cold worked, then subjected to heat during painting or lacquering; applicable to coated sheet products.

The second digit: 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.

Code
Relative strain-hardening degree
Common name
Hx2
Quarter hard
Hx4
Half hard
Hx6
Three-quarter hard
Hx8
Full hard
Hx9
Extra hard

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.

05 / Thermally Treated T Tempers

The first T digit records the route.

T tempers describe stable conditions achieved by controlled cooling, solution heat treatment, aging, and sometimes cold work. The order matters.

TemperProcessing routePractical reading
T1Cooled from an elevated-temperature shaping process, then naturally aged.No deliberate cold work after cooling.
T2Cooled from elevated-temperature shaping, cold worked, then naturally aged.Shaping heat + cold work + room-temperature aging.
T3Solution heat treated, cold worked, then naturally aged.Common base route for 2024-T3 sheet.
T4Solution heat treated, then naturally aged.More formable than a peak artificial-age condition in many alloy systems.
T5Cooled from elevated-temperature shaping, then artificially aged.Often associated with press-quenched extrusions.
T6Solution heat treated, then artificially aged.Common high-strength condition for 6061 and 7075.
T7Solution heat treated, then stabilized.Overaged or stabilized to control properties such as corrosion response.
T8Solution heat treated, cold worked, then artificially aged.Cold work occurs before artificial aging.
T9Solution heat treated, artificially aged, then cold worked.Cold work occurs after artificial aging.
T10Cooled from elevated-temperature shaping, cold worked, then artificially aged.Combines press cooling, cold work, and furnace aging.
Definitions are condensed for manufacturing use. Refer to ANSI H35.1/H35.1M, Aluminum Standards & Data, and the governing material specification for the formal definition and applicable product forms.
Natural aging and artificial aging are different.Natural aging develops properties at room temperature over time. Artificial aging uses a controlled elevated-temperature cycle. That difference is why T4 and T6 are not interchangeable even when the alloy number is identical.
06 / Stress Relief & Registered Variants

Extra digits carry real requirements.

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.

T651

Stretched plate condition

Starts with the T6 route and adds stress relief by controlled stretching. Commonly specified for plate to reduce residual-stress movement during machining.

T6511

Extrusion-specific detail

Stress relieved by stretching with minor straightening permitted after the stretching operation. Common for extruded rod, bar, profiles, and tube.

T52

Stress relieved by compression

A compressive stress-relief route used for applicable products and registered tempers.

T7351

Stabilized + stretched

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.

T651 is not shorthand for T6511.The Aluminum Association has specifically cautioned that these designations refer to different processing parameters and product forms and may have different mechanical or physical properties. A near-looking suffix is not an automatic substitute.
07 / What Temper Changes in the Shop

The suffix can change the manufacturing plan.

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.

DecisionSofter / annealed conditionStrain-hardened or heat-treated conditionWhat to verify
BendingUsually 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.
MachiningMay 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.
WeldingStarting 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 cuttingUsually 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.
AnodizingTemper 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.

08 / Drawings, Quotes & Purchase Orders

Specify the complete material identity.

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.

Example callouts — adapt to the actual product and specification
SHEET: ALUMINUM 5052-H32, ASTM B209, 0.063 IN
PLATE: ALUMINUM 6061-T651, ASTM B209, 0.500 IN
EXTRUSION: ALUMINUM 6061-T6511, ASTM B221, PROFILE PER DRAWING
CERTIFICATION: MATERIAL TEST REPORT REQUIRED
SUBSTITUTION: NO ALLOY, TEMPER, OR PRODUCT-FORM SUBSTITUTION WITHOUT WRITTEN APPROVAL
Alloy + temper
State both. “6061 aluminum” does not define delivered properties or stress-relief condition.
Product form
Sheet, plate, bar, extrusion, tube, and forging can use different temper variants and property requirements.
Governing spec
Use the current standard that applies to the purchased form and end-use requirements.
Geometry controls
Add exact thickness, grain direction, flatness, straightness, or machining stock where function requires them.
Verification
Request traceability and MTRs when chemistry, temper, source, or certified properties are material to acceptance.
09 / Frequently Asked Questions

Temper questions worth asking early.

What is an aluminum temper designation?

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.

What is the difference between 6061-T6 and 6061-T651?

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.

What does H32 mean in 5052-H32?

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.

Can one aluminum temper replace another?

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.

Does T6 mean the same strength for every aluminum alloy?

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.

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