6061-T6 vs T651: What the Extra Digit Means for Machining
Same alloy, same strength, same hardness — yet one version warps when you pocket it and the other stays flat. The difference between 6061-T6 and 6061-T651 is a 1.5–3% stretch at the mill, and it decides whether your plate part holds tolerance.

IsoCNC Engineering Team
CNC Machining & DFM Engineers · Updated · 13 min read

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Quick Answer
6061-T6 and 6061-T651 are the same alloy at the same strength — about 45 ksi tensile and 40 ksi yield in both tempers. T651 simply adds one step after quenching: the plate is stretched 1.5–3% to relieve the residual stress that quenching locks in. That stress is what makes T6 plate warp when you remove material unevenly. Specify T651 for thick plate, heavy pocketing, and flatness-critical parts; plain T6 is fine for thin sheet, small parts, and light machining. T651 costs a small premium and is the default for tooling plate, fixtures, and aerospace machined plate per ASTM B209 / AMS 4027.
What T6 and T651 Actually Mean
The temper code is a process history, not a strength grade. In the Aluminum Association designation system, T6 means solution heat treated and artificially aged: the alloy is heated until the magnesium and silicon dissolve, quenched to trap them in solution, then aged at elevated temperature to precipitate the strengthening phase. That is where 6061 gets its 40-ksi-class yield strength, and it is why 6061 dominates machined aluminum work in the first place — the trade-offs against stronger alloys like 7075 are covered in our 6061 vs 7075 comparison.
The appended digits 51 add exactly one operation: stress relief by stretching. So T651 reads as T6 plus a controlled permanent stretch, applied after quenching. Everything else — chemistry, aging response, hardness, anodizing behavior, weldability — is identical between the two tempers. When a drawing says 6061-T651, it is not asking for a better material. It is asking for the same material with the internal stress taken out before it ships. Full alloy background lives on our aluminum CNC machining materials page.
How the Stretch Works: 1.5–3% of Permanent Set
To understand why the stretch matters, start with where the stress comes from. After solution heat treatment, the plate is quenched — and the surface cools and contracts faster than the core. That temperature gradient leaves the plate in a self-balanced state of residual stress: typically compression near the surface, tension in the core. The plate looks flat and measures flat. The stress is invisible until you start cutting it.
The T651 stretch is the fix, done at the mill. The quenched plate is gripped at both ends and pulled past its yield point — a permanent set of 1.5–3% for plate, 0.5–3% for sheet, and 1–3% for rolled or cold-finished rod and bar — then aged. That small plastic deformation yields every fiber of the cross-section past the point where the quench stresses were sitting, collapsing the stress gradient to a low, uniform level. The plate loses almost nothing in the process: strength and hardness specs are unchanged, and a couple of percent of length is irrelevant. There is also a compression-based cousin, T652, used where stretching is impractical. What the mill cannot do is relieve the stress after you have bought unstretched plate — once T6 plate is in your shop, the stress is yours to manage.
T6 vs T651: The Specs Are Identical
Engineers regularly assume the extra digit buys strength. It does not. Because both tempers share the same solution treatment, quench, and aging cycle, every mechanical property on the datasheet matches — typical values and the ASTM B209 minimums alike. Choosing between them is never a structural calculation; it is a machining-stability calculation.
| Property | 6061-T6 | 6061-T651 |
|---|---|---|
| Ultimate tensile strength (typical) | 310 MPa (45 ksi) | 310 MPa (45 ksi) |
| Yield strength, 0.2% offset (typical) | 276 MPa (40 ksi) | 276 MPa (40 ksi) |
| ASTM B209 minimums (plate) | 290 MPa tensile / 240 MPa yield | 290 MPa tensile / 240 MPa yield |
| Brinell hardness | ~95 HB | ~95 HB |
| Elongation | ~12% (thin gauges) | ~12% (thin gauges) |
| Residual stress after quench | Locked in — released when you cut | Relieved by 1.5–3% stretch before aging |
| Machining distortion risk | Moderate to high in plate and heavy-removal parts | Low — the reason the temper exists |
| Material cost | Baseline | Small premium over T6 |
If the part fails a strength check in T6, T651 will not save it — step up to 7075 or 2024 instead. And if the alloy decision itself is still open, our comparisons of 6061 vs 5052 and 6061 vs 6063 cover where 6061 sits against the non-heat-treatable and extrusion-grade alternatives.
Why Machining Turns the Difference Into Real Money
Residual stress is balanced inside the plate — until it is not. Every chip you remove carries stress out of the part with it. Machine a pocket on one face, take a heavy skim off one side, or cut a thin floor into thick plate, and the remaining stress field is no longer symmetric. The part physically moves to rebalance itself: faces bow, edges curl, walls lean, and the flat datum you just machined is not flat anymore. With T6 plate this can happen mid-cycle — operators watch a part spring away from the fixture as the last pocket finishes.

The classic casualties are exactly the parts plate gets bought for: fixture plates and tooling plates that must stay flat, mold bases with deep cavities, aerospace ribs and brackets where 80% of the billet becomes chips, and any wide thin part with a flatness callout. Thicker sections are worse, because the quench gradient that created the stress grows with section thickness. Shops can fight it with symmetric roughing, multiple unclamp-and-reseat cycles, and skim passes — but every one of those tactics is cycle time and scrap risk you are spending to compensate for material that cost slightly less. T651 removes the problem at the source, which is why it is the default temper for machining plate. The cutting side of the equation — speeds, tooling, chip control — is covered in our aluminum milling guide.
T651, T6510, T6511: Plate, Rod, and Extrusions
The 51 suffix extends across product forms with two extra digits for extrusions. Rolled plate, sheet, and rolled or cold-finished rod and bar carry plain T651 — stretched, with no straightening permitted afterward. Extrusions get their own codes because an extruded shape often cannot meet straightness tolerances from stretching alone: T6510 means the extrusion was stretched and receives no further straightening, while T6511 permits minor straightening after stretching so the shape can comply with standard tolerances.
| Temper | Product Form | Permanent Stretch | Straightening After Stretch |
|---|---|---|---|
| T651 (plate) | Rolled plate | 1.5–3% | Not allowed |
| T651 (sheet) | Rolled sheet | 0.5–3% | Not allowed |
| T651 (rod/bar) | Rolled or cold-finished rod and bar | 1–3% | Not allowed |
| T6510 | Extruded rod, bar, shapes, tube | 1–3% | Not allowed |
| T6511 | Extruded rod, bar, shapes, tube | 1–3% | Minor straightening allowed to meet standard tolerances |
For the buyer, the practical point is simple: if the part is being machined from extruded bar or shapes and the drawing says T651, T6511 is what the mill will actually supply, and it is the correct callout. The stress relief is the same either way.
When T6 Is Enough — and How to Call Out the Temper
T651 is not free, and it is not always needed. Plain T6 is the right call for thin sheet parts, small components, light or balanced material removal, and near-net-shape work — anywhere the locked-in stress never gets the chance to move the part. A small bracket skimmed equally on both sides from 1/8-inch sheet does not care which temper you bought. Save the premium for the parts that do: thick plate, deep pockets, thin floors, wide flat parts, fixtures, and anything with a flatness or position tolerance that must survive machining.
On the drawing or purchase order, call out alloy, temper, form, and specification in one line: 6061-T651 aluminum plate per ASTM B209, or AMS 4027 for aerospace sheet and plate programs (it replaces the legacy QQ-A-250/11 spec). Request mill certificates with the order so the temper is traceable to the actual plate. And keep flatness as its own drawing requirement — stress relief stops the part from moving during machining, but it is not a delivered-flatness guarantee. If you would rather not arbitrate temper questions on every RFQ, that is normal — as a China CNC machining supplier we review material callouts on every quote and flag it when a T6 callout is going to warp on a flatness-critical plate part.
FAQ: 6061-T6 vs T651
Is 6061-T651 stronger than 6061-T6?
No. Both tempers carry the same specified and typical mechanical properties — about 310 MPa (45 ksi) ultimate tensile, 276 MPa (40 ksi) yield, and roughly 95 HB hardness — because they are the same alloy put through the same solution heat treatment and artificial aging. The only extra step in T651 is a controlled stretch that relieves residual stress. Strength is a chemistry-and-aging question; the 51 suffix is a stress question. If your calculation needs more strength, the answer is a different alloy (7075, 2024) or a different temper family, not a different stress-relief suffix on 6061.
What does the 51 in T651 stand for?
In the Aluminum Association temper designation system, the digits 51 appended to a T temper mean stress-relieved by stretching. T651 therefore reads as: T6 (solution heat treated and artificially aged) plus 51 (stress relieved by a controlled permanent stretch — 1.5 to 3% for plate). Related suffixes exist for other relief methods: T652 means stress relieved by compressing the plate, and T6510/T6511 apply the same stretching concept to extrusions. The stretch is small and permanent, and it is done before the material ever reaches your machine.
Why does 6061-T6 warp during machining?
The warp is baked in at the mill. After solution heat treatment, plate is quenched rapidly, and the surface cools and contracts faster than the core — that differential locks residual stress into the plate. The stress sits there quietly until you start removing material. Cut an asymmetric pocket, machine one face thinner than the other, or slot down the middle of a plate, and the stress field you removed material from is no longer balanced. The part moves to find a new equilibrium: faces bow, edges curl, and flat datums are suddenly not flat. T651 removes most of that stored energy before the plate ships, so the part has nothing left to redistribute.
When should I specify 6061-T651 instead of T6?
Specify T651 whenever the part is plate-based and the machining is heavy or asymmetric: thick plate over about 1/4 inch, large pockets or deep cavities, thin floors or webs, wide flat parts with flatness callouts, fixture plates, mold bases, and tooling plate work. Also specify it when tight dimensional tolerances must survive a second operation or anodizing. T6 is fine for thin sheet parts, small parts with light and balanced material removal, and near-net-shape work — anywhere the locked-in stress never gets a chance to move the part. When in doubt on a flatness-critical plate part, T651 is the cheap insurance.
What is the difference between 6061-T651 and 6061-T6511?
Form, mostly. T651 applies to rolled plate, sheet, and rolled or cold-finished rod and bar — products that receive no straightening after the stress-relieving stretch. T6510 and T6511 are the extrusion equivalents: the extrusion is stretched the same way, and T6511 additionally permits minor straightening after stretching so the extrusion can meet standard straightness tolerances. For the machinist the practical read is identical — the material has been stress relieved. If your drawing says T651 but the part is being cut from extruded bar, T6511 is the correct callout, and any competent mill will supply it that way.
How do I call out 6061-T651 on a drawing or purchase order?
Call out the alloy, temper, product form, and specification in one line: for example, 6061-T651 aluminum plate per ASTM B209. Aerospace programs typically reference AMS 4027, which covers 6061-T651 sheet and plate and replaces the older QQ-A-250/11 federal specification. Ask for mill certificates with the order so the temper is traceable to the plate, not just the PO. If flatness matters, add the flatness requirement to the drawing itself rather than assuming the temper covers it — stress relief prevents movement during machining, but it is not a flatness tolerance on the as-delivered plate.
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Plate Parts That Stay Flat, Machined Right the First Time
IsoCNC machines 6061-T651 plate and T6511 bar daily — fixtures, tooling plates, mold bases, and structural parts with full mill certs to ASTM B209 or AMS 4027. Not sure whether your part needs the stress-relieved temper? Send the drawing; an engineer reviews every RFQ, typically within 1–2 business days.