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.
Start here. The temper you specify depends on your part geometry and service environment, not on what the supplier stocks.
| Your Situation | Use This | Why |
|---|---|---|
| CNC machining from plate — removing material from one side | T651 | Stress-relieved by stretching. Won't warp when you machine pockets or features on one face. |
| CNC machining bar stock (uniform cross-section) | T6 is fine | Round bar has symmetric stress distribution. Distortion risk is low. T6 is cheaper and more available. |
| 7075 part in humid or marine environment under load | T73 or T7351 | T6 will crack via stress corrosion. T73 loses ~12% strength but eliminates SCC risk entirely. |
| Need to bend or form before machining | O (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 T351 | Naturally aged for best fatigue resistance. T6 would reduce fatigue life. |
| Maximum strength, no corrosion concern | T6 | Peak-aged. Highest tensile and yield. Fine for dry indoor environments. |
| Welding 6061 (weldment assembly) | T4 or T6 | Weld HAZ drops to T4-level properties regardless. No benefit specifying T6 for the weld zone. |
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.
| Designation | Process | Key Properties | Typical Use |
|---|---|---|---|
| F | As-fabricated, no thermal treatment | No guaranteed properties. May vary across the piece. | Raw stock for re-heat-treating. Not for finished parts. |
| O | Annealed (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. |
| T3 | Solution treated + cold worked + natural aged | Improved strength vs T4 due to cold work. Good fatigue resistance. | 2024-T3 aircraft skins. Rivet holes benefit from cold-worked strength. |
| T4 | Solution 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. |
| T6 | Solution treated + artificially aged (elevated temp) | Maximum strength (peak-aged). Contains residual quench stress. | Default for most CNC parts. 6061-T6, 7075-T6. |
| T651 | T6 + 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. |
| T73 | Solution treated + overaged (two-stage aging) | 12% lower strength than T6. Excellent SCC resistance. | 7075-T73 aerospace and marine fittings. No SCC risk. |
| T7351 | T73 + stress-relieved by stretching | Same as T73 but with low residual stress for machining. | 7075 plate for marine/aerospace CNC parts. |
| T8 | Solution treated + cold worked + artificially aged | Higher strength than T6 for some alloys. Reduced ductility. | 2024-T81, 2024-T86. High-strength aerospace fittings. |
| T9 | Solution treated + artificially aged + cold worked | Extra strength from cold work after aging. Rare in machining. | Extrusions requiring high strength. Not common in plate stock. |
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.
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.
| Scenario | T6 Result | T651 Result |
|---|---|---|
| 200mm plate, machine a 10mm deep pocket on one face | Plate 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 diameter | Usually fine — symmetric removal. | No practical benefit over T6 for bar stock. |
| Thin plate (3mm), machine flat | Significant bowing. May be unfixable. | Stays flat if clamping is proper. |
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.
The most common aluminum alloy. The temper difference is subtle in the spec sheet but significant on the machine.
| Property | 6061-T6 | 6061-T651 |
|---|---|---|
| Tensile strength | 310 MPa | 310 MPa (identical) |
| Yield strength | 275 MPa | 275 MPa (identical) |
| Elongation | 12% | 12% (identical) |
| Hardness (HB) | 95 | 95 (identical) |
| Thermal conductivity | 167 W/mK | 167 W/mK (identical) |
| Residual stress | High (from quenching) | Low (stretched after quench) |
| Distortion after machining | Moderate to high | Minimal |
| Available forms | Plate, bar, tube, sheet, extrusion | Plate, flat bar, thick sheet |
| Cost (China market) | Baseline | +5–10% |
Same mechanical property story as 6061 — identical on paper. But 7075 has an additional risk that makes temper selection even more critical.
| Property | 7075-T6 | 7075-T651 | 7075-T73 | 7075-T7351 |
|---|---|---|---|---|
| Tensile strength | 572 MPa | 572 MPa | 503 MPa | 503 MPa |
| Yield strength | 503 MPa | 503 MPa | 434 MPa | 434 MPa |
| Elongation | 11% | 11% | 13% | 13% |
| Hardness (HB) | 150 | 150 | 135 | 135 |
| Residual stress | High | Low | Low | Low |
| SCC resistance | Poor | Poor | Excellent | Excellent |
| Distortion after machining | Moderate | Minimal | Minimal | Minimal |
| Cost premium vs T6 | Baseline | +5–10% | +15–20% | +20–25% |
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.
| Application | Environment | Recommendation | Reason |
|---|---|---|---|
| Aircraft structural fittings | Altitude (condensation possible) | T73 or T7351 | Industry standard for 7075 structural parts. |
| Marine hardware (brackets, mounts) | Saltwater spray | T7351 | SCC immunity + machining stability. |
| Outdoor equipment (tropical climate) | High humidity, 30–40°C | T73 | Humidity alone is enough to trigger SCC in T6. |
| Indoor equipment (climate controlled) | Dry, 20–25°C | T6 is fine | SCC risk is minimal in dry environments. |
| Tooling plates, jigs (no service stress) | Any | T6 is fine | Without sustained tensile stress, SCC won't initiate. |
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 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.
| Situation | Approach | Detail |
|---|---|---|
| Need to bend or form 6061 plate | Start with O-temper, form, then re-heat-treat | 6061-T6 has ~12% elongation and will crack at tight bend radii. O-temper gives ~25% elongation. |
| Deep drawing aluminum | O-temper is mandatory | You cannot deep-draw T6. It will tear. |
| Complex sheet metal fabrication | Form in O, then solution treat + age to T6 | Common workflow: O-temper blank → form → T6 heat treat → machine final features. |
| Welding prep (pre-heating) | Not needed | O-temper doesn't help with welding. The weld HAZ will overheat regardless of starting temper. |
After forming O-temper material, you can restore full T6 properties by solution treating and artificial aging. The process:
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.
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.
| Temper | Process | Tensile (MPa) | Yield (MPa) | Key difference |
|---|---|---|---|---|
| 2024-T3 | Solution + cold worked (~2%) + natural age | 483 | 345 | Higher strength from cold work. Best for aircraft skins with rivet holes. |
| 2024-T4 | Solution + natural age only | 469 | 324 | Slightly lower strength, better ductility. Better for bulk machined parts. |
| 2024-T351 | T4 + stress relieved by stretching | 469 | 324 | Same as T4 but stable for plate machining. |
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.
Always include the full alloy-temper designation. The correct format is ALLOY-TEMPER. Examples:
| Material | Availability | Lead Time | Common Suppliers |
|---|---|---|---|
| 6061-T6 | Stock item everywhere | Same day | Southwest Aluminum, Mingtai, Nanshan |
| 6061-T651 | Widely available | 1–3 days | Southwest Aluminum, Alcoa China |
| 7075-T6 | Available | 3–7 days | Southwest Aluminum, CNMC |
| 7075-T651 | Check stock | 1–2 weeks | Southwest Aluminum, import from Alcoa/Constellium |
| 7075-T73 / T7351 | Often made-to-order | 3–6 weeks | May need to import. Plan ahead. |
| 2024-T351 | Check stock | 1–3 weeks | Southwest Aluminum, import |
| 6061-O | Limited stock | 1–2 weeks | Most mills can produce on request |
| Form | Common Thickness | Common Width | Common Length |
|---|---|---|---|
| Plate (T651) | 6, 8, 10, 12, 15, 20, 25, 30, 40, 50, 60, 80, 100mm | 1000, 1220, 1500, 2000mm | 2000, 2500, 3000mm |
| Flat bar (T651) | 3, 5, 6, 8, 10, 12, 15, 20, 25mm | 50–300mm | 2000, 3000mm |
| Round bar (T6) | 5–200mm dia. | — | 1000, 2000, 3000mm |
| Sheet (T6, T4) | 0.5, 1.0, 1.5, 2.0, 2.5, 3.0mm | 1220, 1500mm | 2440, 3000mm |
| Material | Price Range (CNY/kg) | Relative to 6061-T6 |
|---|---|---|
| 6061-T6 | 22–28 | 1.0x (baseline) |
| 6061-T651 | 24–32 | 1.05–1.10x |
| 6061-O | 24–30 | 1.05–1.10x |
| 7075-T6 | 45–70 | 1.8–2.5x |
| 7075-T651 | 50–80 | 2.0–2.8x |
| 7075-T7351 | 60–100 | 2.5–3.5x |
| 2024-T351 | 40–65 | 1.6–2.3x |
| Mistake | What Happens | Correct Approach |
|---|---|---|
| Ordering T6 plate, machining deep pockets on one face | Plate warps. Scrap rate increases. Extra skim passes add cycle time. | Order T651 plate. Always. |
| Using 7075-T6 outdoors under load | Stress corrosion cracking. Sudden, catastrophic failure with no visible warning. | Specify T73 or T7351 for any sustained-load outdoor application. |
| Writing "6061" on drawing without temper | Supplier 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 bend | Cracking at the bend radius. Wasted material. | Start with O-temper, form, then re-heat-treat to T6. |
| Specifying T73 for indoor, non-structural parts | Paying 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-treat | Finished 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 strengths | Overpaying 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 job | Project 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 finish | T73 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. |