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Aluminum T-Tempers

The temper designation (T6, T651, T73, etc.) is not optional — it determines whether your part warps on the machine table, cracks in service, or costs 2x what it should. Most engineers just write "6061-T6" and hope for the best. This page tells you when that's wrong.

T6 vs T651 — Which Do You Need?

Start here. The temper you specify depends on your part geometry and service environment, not on what the supplier stocks.

Your SituationUse ThisWhy
CNC machining from plate — removing material from one sideT651Stress-relieved by stretching. Won't warp when you machine pockets or features on one face.
CNC machining bar stock (uniform cross-section)T6 is fineRound bar has symmetric stress distribution. Distortion risk is low. T6 is cheaper and more available.
7075 part in humid or marine environment under loadT73 or T7351T6 will crack via stress corrosion. T73 loses ~12% strength but eliminates SCC risk entirely.
Need to bend or form before machiningO (annealed)Softest condition. Form it, then re-heat-treat to T6. Trying to form T6 plate causes cracking.
Aerospace 2024 structure (fatigue-critical)T4 or T351Naturally aged for best fatigue resistance. T6 would reduce fatigue life.
Maximum strength, no corrosion concernT6Peak-aged. Highest tensile and yield. Fine for dry indoor environments.
Welding 6061 (weldment assembly)T4 or T6Weld HAZ drops to T4-level properties regardless. No benefit specifying T6 for the weld zone.

Understanding T-Temper Designations

The Aluminum Association designation system uses prefixes (F, O, H, T, W) followed by digits. For CNC machining, you mainly deal with F, O, and the T-series.

DesignationProcessKey PropertiesTypical Use
FAs-fabricated, no thermal treatmentNo guaranteed properties. May vary across the piece.Raw stock for re-heat-treating. Not for finished parts.
OAnnealed (heated to ~415°C, slow cooled)Lowest strength, maximum ductility. Tensile drops 50–60% vs T6.Deep forming, bending. Then re-heat-treat to desired temper.
T3Solution treated + cold worked + natural agedImproved strength vs T4 due to cold work. Good fatigue resistance.2024-T3 aircraft skins. Rivet holes benefit from cold-worked strength.
T4Solution treated + naturally aged (room temp, 96+ hrs)Partial strength (~75–80% of T6). Excellent fatigue and fracture toughness.2024-T4 structural parts. Formable before full aging.
T6Solution treated + artificially aged (elevated temp)Maximum strength (peak-aged). Contains residual quench stress.Default for most CNC parts. 6061-T6, 7075-T6.
T651T6 + stress-relieved by stretching (1–3% permanent set)Same mechanical properties as T6. Near-zero residual stress.Plate and flat bar for CNC machining. Prevents distortion.
T73Solution treated + overaged (two-stage aging)12% lower strength than T6. Excellent SCC resistance.7075-T73 aerospace and marine fittings. No SCC risk.
T7351T73 + stress-relieved by stretchingSame as T73 but with low residual stress for machining.7075 plate for marine/aerospace CNC parts.
T8Solution treated + cold worked + artificially agedHigher strength than T6 for some alloys. Reduced ductility.2024-T81, 2024-T86. High-strength aerospace fittings.
T9Solution treated + artificially aged + cold workedExtra strength from cold work after aging. Rare in machining.Extrusions requiring high strength. Not common in plate stock.
What the digits mean The first digit after T indicates the basic treatment sequence. Additional digits modify it: 5 = stress-relieved by stretching (plate/flat bar), 4 = stress-relieved by compressing (forgings/rod), 2 = cold worked after heat treatment, 3 = cold worked + naturally aged.

Why T651 Matters for CNC Machining

This is the single most important section on this page. If you machine aluminum plate, you need to understand why T651 exists and when T6 will cause problems.

The distortion problem

When aluminum is solution-treated and quenched (the first steps of T6), the rapid cooling locks in thermal gradients. The outside of the plate cools and contracts faster than the inside. This creates residual stresses — the internal layers are in tension, the surface layers are in compression (or vice versa, depending on geometry).

As long as the plate is intact, these forces balance out. The plate appears flat. But when you start machining — especially removing material from one side — you break that balance. The remaining stressed material pulls the part out of shape.

ScenarioT6 ResultT651 Result
200mm plate, machine a 10mm deep pocket on one facePlate bows upward (convex on machined side). Typical distortion: 0.1–0.5mm.Stays flat. Distortion under 0.02mm.
50mm plate, machine thin ribs (wall 2mm)Ribs deflect during machining. Dimensional scatter between parts.Ribs hold position. Consistent dimensions.
100mm plate, machine features on both faces (symmetric)Less distortion than single-sided, but still some warpage.Negligible distortion.
Round bar, turning down diameterUsually fine — symmetric removal.No practical benefit over T6 for bar stock.
Thin plate (3mm), machine flatSignificant bowing. May be unfixable.Stays flat if clamping is proper.

How T651 fixes this

Between quenching and aging, the T651 process applies a controlled permanent stretch of 1–3% to the plate. This plastic deformation exceeds the yield point and allows the residual stresses to redistribute and partially cancel out. The result is a plate with the same mechanical properties as T6, but with residual stresses reduced by roughly 80–90%.

The stretching is done by the mill (Alcoa, Aleris, Southwest Aluminum, etc.) on the full-size plate before it's cut to size. You can't convert T6 to T651 in your shop — it has to be ordered that way.

Rule of thumb If you're machining plate or flat bar and removing more than ~15% of the thickness from one side, specify T651. The cost premium is 5–10%, but it eliminates scrap from warping and reduces machining time (fewer skim passes to clean up distortion). For bar stock and tube, T6 is generally fine.

6061-T6 vs 6061-T651

The most common aluminum alloy. The temper difference is subtle in the spec sheet but significant on the machine.

Property6061-T66061-T651
Tensile strength310 MPa310 MPa (identical)
Yield strength275 MPa275 MPa (identical)
Elongation12%12% (identical)
Hardness (HB)9595 (identical)
Thermal conductivity167 W/mK167 W/mK (identical)
Residual stressHigh (from quenching)Low (stretched after quench)
Distortion after machiningModerate to highMinimal
Available formsPlate, bar, tube, sheet, extrusionPlate, flat bar, thick sheet
Cost (China market)Baseline+5–10%
When T6 is correct T6 is fine for bar stock (round, hex, square) where material removal is roughly symmetric around the centerline. It's also fine for extrusions, thin sheet, and tubing. You only need T651 when machining thick plate or flat bar with asymmetric material removal.

7075-T6 vs 7075-T651

Same mechanical property story as 6061 — identical on paper. But 7075 has an additional risk that makes temper selection even more critical.

Property7075-T67075-T6517075-T737075-T7351
Tensile strength572 MPa572 MPa503 MPa503 MPa
Yield strength503 MPa503 MPa434 MPa434 MPa
Elongation11%11%13%13%
Hardness (HB)150150135135
Residual stressHighLowLowLow
SCC resistancePoorPoorExcellentExcellent
Distortion after machiningModerateMinimalMinimalMinimal
Cost premium vs T6Baseline+5–10%+15–20%+20–25%
7075-T6 SCC warning 7075-T6 is susceptible to stress corrosion cracking in humid or marine environments. SCC is catastrophic and invisible — the part shows no signs of damage, then fails suddenly under tensile load. If a 7075 part will experience sustained stress in any environment above 50% relative humidity, do not use T6. Specify T73 or T7351. This is not optional for aerospace, marine, or outdoor structural applications.

T73: Over-Aging for SCC Resistance

T73 is a two-stage overaging process specifically developed for 7xxx series alloys. The first aging step is at a lower temperature than T6, the second at a higher temperature. This produces a coarser, more evenly distributed precipitate structure that is far less susceptible to stress corrosion cracking.

When to specify T73

ApplicationEnvironmentRecommendationReason
Aircraft structural fittingsAltitude (condensation possible)T73 or T7351Industry standard for 7075 structural parts.
Marine hardware (brackets, mounts)Saltwater sprayT7351SCC immunity + machining stability.
Outdoor equipment (tropical climate)High humidity, 30–40°CT73Humidity alone is enough to trigger SCC in T6.
Indoor equipment (climate controlled)Dry, 20–25°CT6 is fineSCC risk is minimal in dry environments.
Tooling plates, jigs (no service stress)AnyT6 is fineWithout sustained tensile stress, SCC won't initiate.

The tradeoff

T73 costs more and gives less strength. For 7075, the numbers are:

If your design can accommodate the lower strength (redesign with slightly thicker sections), T73 is the safer choice. If the part is non-structural or used indoors, T6 is fine and cheaper.

O-Temper and Annealed

O-temper is the fully annealed condition. The material is heated to ~410–430°C (depending on alloy) and slow-cooled. This dissolves all precipitates and produces the softest, most ductile state.

When to use O-temper

SituationApproachDetail
Need to bend or form 6061 plateStart with O-temper, form, then re-heat-treat6061-T6 has ~12% elongation and will crack at tight bend radii. O-temper gives ~25% elongation.
Deep drawing aluminumO-temper is mandatoryYou cannot deep-draw T6. It will tear.
Complex sheet metal fabricationForm in O, then solution treat + age to T6Common workflow: O-temper blank → form → T6 heat treat → machine final features.
Welding prep (pre-heating)Not neededO-temper doesn't help with welding. The weld HAZ will overheat regardless of starting temper.

Re-heat-treating after forming

After forming O-temper material, you can restore full T6 properties by solution treating and artificial aging. The process:

  1. Solution treat: Heat to 530°C (6061) or 480°C (7075), hold 1 hour. Dissolves alloying elements into solid solution.
  2. Quench: Rapid water quench within 10 seconds of removal from furnace. Traps elements in supersaturated solid solution.
  3. Age: 6061 at 175°C for 8 hours. 7075 at 120°C for 24 hours. This produces the precipitation hardening.

If you need T651 after forming, specify T351 as the starting temper instead of O-temper. T351 is T4 + stress relieved. It's formable enough for moderate bends (not as soft as O) and can be aged to T6 after forming.

Dimensional change after heat treatment Re-heat-treating will cause dimensional changes — typically 0.05–0.15% shrinkage or warpage depending on geometry. Machine rough features before heat treat, finish-machine after. If you're outsourcing heat treatment, plan for this in your tolerance stackup.

T4: Natural Aging

T4 means the alloy has been solution-treated and then allowed to age at room temperature. It reaches ~75–80% of T6 strength after 4–5 days and continues to slowly strengthen for months.

2024-T4 vs 2024-T3

TemperProcessTensile (MPa)Yield (MPa)Key difference
2024-T3Solution + cold worked (~2%) + natural age483345Higher strength from cold work. Best for aircraft skins with rivet holes.
2024-T4Solution + natural age only469324Slightly lower strength, better ductility. Better for bulk machined parts.
2024-T351T4 + stress relieved by stretching469324Same as T4 but stable for plate machining.

When to specify T4

T4 is used almost exclusively with 2xxx series alloys (2024, 2014) for applications where fatigue resistance and fracture toughness matter more than absolute strength. T6 would give higher static strength but worse fatigue performance. The naturally aged microstructure has a coarser precipitate that resists crack propagation better than the fine precipitates in T6.

If you're machining 2024 parts, use T351 plate for the same distortion reasons as 6061-T651.

Practical Procurement Guide

What to specify on drawings

Always include the full alloy-temper designation. The correct format is ALLOY-TEMPER. Examples:

Availability in China

MaterialAvailabilityLead TimeCommon Suppliers
6061-T6Stock item everywhereSame daySouthwest Aluminum, Mingtai, Nanshan
6061-T651Widely available1–3 daysSouthwest Aluminum, Alcoa China
7075-T6Available3–7 daysSouthwest Aluminum, CNMC
7075-T651Check stock1–2 weeksSouthwest Aluminum, import from Alcoa/Constellium
7075-T73 / T7351Often made-to-order3–6 weeksMay need to import. Plan ahead.
2024-T351Check stock1–3 weeksSouthwest Aluminum, import
6061-OLimited stock1–2 weeksMost mills can produce on request

Common stock sizes (China domestic market)

FormCommon ThicknessCommon WidthCommon Length
Plate (T651)6, 8, 10, 12, 15, 20, 25, 30, 40, 50, 60, 80, 100mm1000, 1220, 1500, 2000mm2000, 2500, 3000mm
Flat bar (T651)3, 5, 6, 8, 10, 12, 15, 20, 25mm50–300mm2000, 3000mm
Round bar (T6)5–200mm dia.1000, 2000, 3000mm
Sheet (T6, T4)0.5, 1.0, 1.5, 2.0, 2.5, 3.0mm1220, 1500mm2440, 3000mm

Cost comparison (approximate, China market, 2026)

MaterialPrice Range (CNY/kg)Relative to 6061-T6
6061-T622–281.0x (baseline)
6061-T65124–321.05–1.10x
6061-O24–301.05–1.10x
7075-T645–701.8–2.5x
7075-T65150–802.0–2.8x
7075-T735160–1002.5–3.5x
2024-T35140–651.6–2.3x
Prices fluctuate Aluminum prices track the LME (London Metal Exchange) and domestic Chinese market rates. The above ranges are approximate. Get current quotes from your supplier. Large orders (>500kg) can typically negotiate 5–15% off list price. Import material (Alcoa, Constellium, Kobe) carries a 20–40% premium over domestic but often has tighter tolerance control.

Common Mistakes

MistakeWhat HappensCorrect Approach
Ordering T6 plate, machining deep pockets on one facePlate warps. Scrap rate increases. Extra skim passes add cycle time.Order T651 plate. Always.
Using 7075-T6 outdoors under loadStress corrosion cracking. Sudden, catastrophic failure with no visible warning.Specify T73 or T7351 for any sustained-load outdoor application.
Writing "6061" on drawing without temperSupplier ships whatever they have. Could be O, T4, T6, or even F. Properties vary wildly.Always write "6061-T651" (or appropriate temper) on the drawing.
Forming T6 plate into a tight bendCracking at the bend radius. Wasted material.Start with O-temper, form, then re-heat-treat to T6.
Specifying T73 for indoor, non-structural partsPaying 25% more for material you don't need. Longer lead time.T73 only when SCC is a real risk (sustained stress + moisture). Use T6 otherwise.
Not accounting for dimensional change after re-heat-treatFinished parts out of tolerance after heat treatment cycle.Rough machine before heat treat, finish-machine after. Allow 0.05–0.15% dimensional change.
Assuming T6 and T651 have different strengthsOverpaying for T651 thinking it's "stronger," or avoiding T651 thinking it's "weaker."They are identical in mechanical properties. T651 just has lower residual stress.
Importing T7351 with 2-week lead time for a rush jobProject delayed. Could have used T6 for indoor application.Check if SCC is actually a risk. If not, use T651 or T6 and ship on time.
Anodizing 7075-T73 and expecting bright cosmetic finishT73 still has copper content — anodize comes out dark and uneven.Use 6061-T6 if cosmetic anodizing matters. 7075 is a structural alloy, not a cosmetic one.