Age T73 (Aluminum)
Solution treat & age · Precipitation hardening
Age T73 (Aluminum) is a precipitation-hardening condition for 7075 and 7050 (alloy-specific overage condition).
Reference page — Al T73 is not in the instant-quote configurator. Upload the part, name the treatment in the notes with the call-out below, and an engineer quotes it with the part.
Al T73 at a glance
Four scores, each 0–100 against every heat treatment in this catalog. Hardness is derived from the HRC target (20 HRC = 0, 70 HRC = 100) — treatments without a hardness target (anneals, stress relief, HIP, cryo) are not rated. Toughness, dimensional stability and cost are FabDigit's engineering assessment.
What is Al T73?
Age T73 (Aluminum) is a precipitation-hardening condition for 7075 and 7050 (alloy-specific overage condition). It develops strength by solution treatment followed by controlled aging; the final condition, material specification, and acceptance test belong on the drawing.
How it works
Solution treatment dissolves strengthening constituents and establishes a controlled starting microstructure. Cooling retains a supersaturated or otherwise metastable matrix. During the prescribed age, diffusion forms a fine dispersion of strengthening precipitates that obstruct dislocation motion. Temperature and time control precipitate size, spacing, coherency, and grain-boundary chemistry: lower or shorter cycles generally favor peak strength, while overaging trades some strength for toughness, conductivity, or stress-corrosion resistance. The complete route, including the incoming material condition and cooling practice, is therefore part of the engineering definition.
Why specify it
- Produces 25–32 HRC across the stated grade set
- Provides 505 MPa or greater tensile capability where the cited product condition defines it
- Adds strength through precipitation rather than a carbon-steel temper
- Can be applied after near-net machining with less movement than a severe steel quench
Where it falls short
- Properties depend on alloy, product form, section size, and incoming condition
- Overaging or underaging can miss both strength and corrosion targets
- Solution treatment or quenching may distort thin and asymmetric parts
- A condition name does not replace material heat-lot traceability
The Al T73 cycle
Typical furnace parameters from the governing specifications and shop practice; the heat treater sets the exact recipe from the alloy, section size and required result.
| Temperature | 105–180 °C (221–356 °F) — Primary solution or age temperature window represented by the stages; use the alloy-specific specification. |
|---|---|
| Soak | 8–30 h — At-temperature time; load and section corrections may apply. |
| Cooling | Still air |
| Atmosphere | Air |
| Door to door | 18–40 h — Typical furnace cycle excluding queue and laboratory testing. |
Stages
- 1Solution heat treat and quench per alloy product specification
- 2Apply the specified two-step overaging cycle
- 3Air cool and verify conductivity plus mechanical properties where required
What Al T73 does to the part
| Hardness | 25–32 HRC (120–145 HB) — Condition and product-form range; Brinell is commonly reported as 120–145 HB. |
|---|---|
| Section affected | The whole section transforms. |
| Tensile strength | 505–540 MPa — Representative 7075-T73/T7351 product range; exact minimum depends on product form and thickness. |
| Toughness | Lower peak strength than T6 but substantially improved resistance to stress-corrosion cracking in 7000-series aluminum. |
| Distortion | Low risk. Overaging is stable; most distortion originates in the preceding solution quench. |
| Surface after treatment | No intended coating; light discoloration is cosmetic unless prohibited. |
| Machining sequence | Machine from T7351 plate for best stability; preserve grain-flow and short-transverse design allowables. |
Specifications for Al T73
The documents a drawing cites to define this treatment. Each links to a page explaining the standard, its classes and the tests it invokes.
Test and related methods: ASTM E18 (Standard Test Methods for Rockwell Hardness of Metallic Materials).
Drawing call-out
7075 ALUMINUM, TEMPER T73 PER AMS 2770; TENSILE STRENGTH 505 MPa MIN; VERIFY HARDNESS AND CONDUCTIVITYWhich alloys take Al T73?
Verdict per material family, with the grades that behave differently. Each family links to its datasheets in the material library. Typical grades: 7075, 7050 (alloy-specific overage condition).
| Material family | Verdict | Notes |
|---|---|---|
| Yes | Applicable to heat-treatable 2000 series, 6000 series, and 7000-series aluminum alloys as permitted by the product specification.
| |
| With care | Only for aluminum AM alloys with a qualified solution-and-age route.
| |
| No | This alloy category does not use the aluminum temper cycle. | |
| No | This alloy category does not use the aluminum temper cycle. | |
| No | This alloy category does not use the aluminum temper cycle. | |
| No | This alloy category does not use the aluminum temper cycle. | |
| No | This alloy category does not use the aluminum temper cycle. | |
| No | This alloy category does not use the aluminum temper cycle. | |
| No | This alloy category does not use the aluminum temper cycle. | |
| No | This alloy category does not use the aluminum temper cycle. | |
| No | This alloy category does not use the aluminum temper cycle. | |
| No | This alloy category does not use the aluminum temper cycle. | |
| No | This alloy category does not use the aluminum temper cycle. | |
| No | This alloy category does not use the aluminum temper cycle. | |
| No | This alloy category does not use the aluminum temper cycle. | |
| No | This alloy category does not use the aluminum temper cycle. |
Design rules for Al T73
What to decide on the drawing before the part goes to the heat treater.
- Complete forming before artificial aging unless the product route expressly permits forming in temper.The precipitation response depends on the material condition entering the age cycle.
- Control quench delay and transfer time to preserve solution treatment response.Uniform temperature and controlled transfer reduce property variation and distortion.
- State the alloy, product specification, final condition, and hardness-test method on the drawing.A condition name alone does not define material pedigree or acceptance sampling.
- Protect finished dimensions and verify critical fits after treatment.Precipitation aging is low-distortion but can still produce measurable contraction or growth.
Al T73 versus the alternatives
Treatments engineers weigh against Al T73, and when each wins.
| Treatment | Hardness | Toughness | Stability | Cost | Choose it when |
|---|---|---|---|---|---|
Al T73 this page | 17 | 72 | 78 | $$$ | — |
| 19 | 60 | 50 | $$ | when maximum static strength is required | |
| 19 | 60 | 72 | $$ | when a T6-strength stress-relieved plate temper is acceptable |
Cost, lead time and applications
Relative cost
Age T73 (Aluminum) is a premium-cost treatment ($$$) relative to the other heat treatments in this catalog.
Heat treatment is priced per lot with a furnace minimum. The exact figure appears on the instant quote once the part is uploaded.
Lead time
| Added lead time | 3–7 working days |
|---|---|
| Furnace time | 18–40 h |
What Al T73 is used for
- Aerospace structural hardware
- Precision shafts, fittings, and actuators
- High-strength tooling and fixtures
- Corrosion-resistant mechanical components
Al T73 — frequently asked
What does Al T73 mean?
Al T73 identifies a controlled solution-treatment and precipitation-aging condition, not a generic furnace temper. The drawing should also identify the alloy specification and acceptance hardness or tensile requirement.
Is this a quench-and-temper treatment?
No in the metallurgical sense. Strength comes primarily from fine precipitates formed during aging rather than tempering quenched carbon-steel martensite.
Will the part distort?
The expected risk is low. Aging is normally more stable than a hard steel quench, but residual stress, section changes, fixtures, and prior solution treatment still matter.
How should hardness be verified?
Use ASTM E18 for Rockwell hardness on a suitable flat section. The expected catalog range is 25–32 HRC; thin sections may require ASTM E384 microindentation and an approved conversion.
Can the condition be assigned after machining?
Usually yes when the starting material and process route are compatible. The purchase order must preserve traceability to the governing product specification and the heat treater must certify the complete cycle.