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Aluminum 7049 · precip hard

Aluminum 7049-T7352

Properties of the T7352 condition, compared with the other 7049 tempers.

Hand and die forgings that will be extensively machined; compression stress relief minimises distortion.

CNC machiningSheet metalPremium cost $$$

What is 7049-T7352?

7049-T7352 is 7049 in the T7352 condition — hand and die forgings that will be extensively machined; compression stress relief minimises distortion. 7049-T7352 has a yield strength of 460 MPa (66.7 ksi) and a tensile strength of 530 MPa (76.9 ksi) — stronger than 92% of aluminum grades. Elongation at break is 10% and the elastic modulus is 71.7 GPa (10.4 Msi). 7049-T7352 has a density of 2.84 g/cm³ (0.103 lb/in³), heavier than 93% of aluminum grades. It melts at 477°C (891 °F).

Advantages

  • High strength — 460 MPa (66.7 ksi), better than 92% of aluminum grades
  • Tough — resists crack growth — 33 MPa·√m (30 ksi·√in), better than 88% of aluminum grades
  • Easy to machine — 72/100, better than 80% of aluminum grades

Limitations

  • Difficult to weld — 15/100, worse than 96% of aluminum grades

7049-T7352 properties

Typical room-temperature values for 7049-T7352 — 8 properties are specific to this condition; the rest are grade-level values shared by every 7049 temper. Each bar shows where the value sits among the aluminum grades in FabDigit's library — further right is higher.

Physical3

7049-T7352 has a density of 2.84 g/cm³ (0.103 lb/in³), heavier than 93% of aluminum grades. It melts at 477°C (891 °F).

Density2.84 g/cm³0.1 lb/in³
Melting Point (Solidus)477°C891 °F
Liquidus Temperature635°C1,175 °F

Mechanical14

7049-T7352 has a yield strength of 460 MPa (66.7 ksi) and a tensile strength of 530 MPa (76.9 ksi) — stronger than 92% of aluminum grades. Elongation at break is 10% and the elastic modulus is 71.7 GPa (10.4 Msi).

Elastic (Young's) Modulus71.7 GPa10.4 Msi
Shear Modulus26.9 GPa3.9 Msi
Bulk Modulus71 GPa10.3 Msi
Poisson's Ratio0.33
Tensile Strength (Ultimate)530 MPa76.9 ksi
Yield Strength (0.2% offset)460 MPa66.7 ksi
Elongation at Break10%
Reduction in Area22%
Compressive Strength490 MPa71.1 ksi
Shear Strength325 MPa47.1 ksi
Fatigue Strength (Endurance Limit)160 MPa23.2 ksi
Fracture Toughness (K_IC)33 MPa·√m30 ksi·√in
Hardness, Brinell132 HB
Hardness, Vickers150 HV

Thermal6

7049-T7352 is rated for continuous service to 150°C (302 °F). It conducts heat at 154 W/m·K (89 BTU/hr·ft·°F), better than 68% of aluminum grades. Thermal expansion is 23.4 µm/m·K (13 µin/in·°F).

Thermal Conductivity154 W/m·K89 BTU/hr·ft·°F
Specific Heat Capacity960 J/kg·K0.23 BTU/lb·°F
Thermal Expansion (CTE, 20–100 °C)23.4 µm/m·K13 µin/in·°F
Latent Heat of Fusion390 J/g168 BTU/lb
Max Service Temperature (continuous)150°C302 °F
Min Service Temperature-196°C-321 °F

Electrical3

7049-T7352 conducts electricity at 40 % IACS, better than 72% of aluminum grades.

Electrical Conductivity40 % IACS
Electrical Resistivity4.3×10⁻⁸ Ω·m1.69 µΩ·in
Magnetic Responsenon-magnetic

Chemical & Environmental3

Corrosion resistance is fair (48/100), worse than 58% of aluminum grades.

Galvanic Potential (seawater, vs SCE)-0.84 V
Corrosion ResistanceFair48/100
Chemical Resistance SummaryGood in neutral atmospheres and fresh water; the T73/T74 overaged condition gives high resistance to stress-corrosion cracking and exfoliation. Attacked by strong acids and alkalis, and prone to galvanic and pitting attack in chloride environments — protect with anodize/primer and insulate from steel or graphite composites.

Sustainability4

Producing a kilogram of 7049-T7352 takes about 215 MJ of energy and emits 13.5 kg of CO₂ — more than 92% of aluminum grades. Typical recycled content is 10%.

Embodied Energy (primary production)215 MJ/kg92,433 BTU/lb
Embodied Carbon (primary production)13.5 kg CO₂/kg
Embodied Water1,200 L/kg144 gal/lb
Typical Recycled Content10%

Manufacturability8

7049-T7352's machinability is very good (72/100, better than 80% of aluminum grades); weldability poor (15/100); formability poor (22/100).

MachinabilityVery good72/100
Machinability Rating (AISI 1212 = 100 %)70%
WeldabilityPoor15/100
Formability (cold)Poor22/100
CastabilityPoor20/100
Brazeability / SolderabilityNot recommended10/100
PolishabilityGood60/100
Anodizing Responsegood — hard and sulfuric anodizing accepted; coatings take a grey/bronze cast from the Zn-Cu content, chromic anodize preferred for aerospace parts

Values are nominal handbook figures for design screening. Certified mill or lot data ships with every FabDigit order on request.

Other 7049 tempers and conditions

7049 is also supplied in 4 other conditions. The full side-by-side table is on the 7049 overview.

Working with 7049-T7352

Is 7049 easy to machine?

Machines well in the overaged tempers with sharp carbide tools, high speed and flood coolant; chips are tough so use polished flutes and generous rake to avoid built-up edge.

Can 7049 be welded?

Not weldable by fusion processes (hot cracking and loss of SCC resistance); join by fasteners, adhesive bonding or friction stir with qualified procedures.

Can 7049 be formed, bent or molded?

Hot-work / forge at about 350–440 °C; cold forming in T73-type tempers is very limited — form in the solution-treated (W) state or before ageing.

What surface finishes work on 7049?

Chromic or sulfuric anodize plus primer for aerospace corrosion protection; keep parts insulated from steel and carbon composites, and shot-peen critical machined surfaces for fatigue life.

7049 chemical composition (wt %)

Limits by weight percent from the governing specification, written the way the spec states them — a single maximum for impurities, a range for alloying elements, and the base element as balance. Nominal is the typical mid-range value.

ElementSpec limit (wt %)Nominal
Zn7.2 – 8.27.7
Mg2 – 2.92.45
Cu1.2 – 1.91.55
Crgrain-boundary/quench-sensitivity control0.1 – 0.220.16
Fe≤ 0.35
Si≤ 0.25
Mn≤ 0.2
Ti≤ 0.1
Others (each)0.15 total≤ 0.05
Albalance

7049-T7352 — frequently asked

What is 7049-T7352 used for?

7049-T7352 is typically used for aircraft landing gear forgings, airframe fittings and lugs, support arms and links, thick-section closed-die forgings, hand (open-die) forgings and thick plate for machined structural parts. In short: high-strength aerospace forging.

What is the yield strength of 7049-T7352?

7049-T7352 has a typical yield strength of 460 MPa (66.7 ksi) and a tensile strength of 530 MPa (76.9 ksi) — stronger than 92% of aluminum grades. Strength varies by condition: see the 5 listed tempers.

Is 7049-T7352 easy to machine?

Yes — machinability is rated very good (72/100, better than 80% of aluminum grades). Machines well in the overaged tempers with sharp carbide tools, high speed and flood coolant; chips are tough so use polished flutes and generous rake to avoid built-up edge.

Can 7049-T7352 be welded?

Not readily — weldability is rated poor (15/100). Not weldable by fusion processes (hot cracking and loss of SCC resistance); join by fasteners, adhesive bonding or friction stir with qualified procedures.

What surface finishes work on 7049-T7352?

Chromic or sulfuric anodize plus primer for aerospace corrosion protection; keep parts insulated from steel and carbon composites, and shot-peen critical machined surfaces for fatigue life.

Can 7049-T7352 be formed, bent or molded?

Hot-work / forge at about 350–440 °C; cold forming in T73-type tempers is very limited — form in the solution-treated (W) state or before ageing.

What is the maximum service temperature of 7049-T7352?

7049-T7352 is rated for continuous use to about 150°C (302 °F). Strength falls off well before that limit — check the elevated-temperature data for load-bearing parts.

Can FabDigit make parts in 7049-T7352?

Yes — 7049-T7352 is available for CNC machining and sheet metal with instant online pricing. Upload a STEP file to get a price and a DFM check.

Sources

  1. International Alloy Designations and Chemical Composition Limits for Wrought Aluminum (Teal Sheets)The Aluminum Association (2018)
  2. ASM Handbook Vol. 2 — Properties and Selection: Nonferrous Alloys and Special-Purpose MaterialsASM International (1990)
  3. ASM Handbook Vol. 19 — Fatigue and FractureASM International (1996)
  4. MMPDS — Metallic Materials Properties Development and StandardizationFAA/Battelle (2023)
  5. AMS 4111 / AMS-QQ-A-367 aluminium forging specificationsSAE International (2019)

Property data is compiled from published supplier and standards handbooks and normalised for comparison. Nothing on this page is a certification — request mill certs, CoC or material test reports with your order.