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Aluminum 2219-T351

Temper

AA 2219 · UNS A92219 · EN AW-2219, AW 2219 · GB 2A16, LY16

T351 = t3, stress relieved by stretching

Low-residual-stress plate/bar version of T31 for machined parts that will later be aged or used as-is.

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Values for the T351 condition

Other 2219 tempers and conditions

2219 is listed in 13 conditions; see the grade overview at 2219.

Compare all 13 conditionsHide
Condition · open for datasheetBest forYield MPaTensile MPaElong. %HardnessConductivity
Annealed
Softest, most formable condition for deep forming or before re-solution treatment; annealed at ~415 °C with slow cool.761721845 HB44 % IACS
Solution heat treated and naturally aged by the user
User-performed solution treatment plus natural aging, used when parts are formed in O temper and then heat treated.1853602090 HB28 % IACS
Solution heat treated, cold worked ~1 %, naturally aged
Intermediate condition for forming/welding of sheet and plate before final T81 artificial aging.24836017100 HB28 % IACS
Solution heat treated, cold worked and naturally aged
Solution-treated, cold-worked and naturally aged 2219 — moderate strength with good ductility and formability, the usual pre-weld/pre-age condition for sheet and plate.25036017100 HB28 % IACS
T351This page
T3, stress relieved by stretching
Low-residual-stress plate/bar version of T31 for machined parts that will later be aged or used as-is.25036015100 HB28 % IACS
T6, heat treated by the user
Pick when parts are formed or welded soft and then given a full user solution + aging cycle; slightly lower strength than T81/T87.29041410115 HB30 % IACS
Solution heat treated and artificially aged
Standard peak-aged temper for 2219 die forgings, hand forgings and extrusions (AMS 4143).29041510115 HB30 % IACS
Solution heat treated and cold worked ~7 %
Heavily stretched pre-temper used as the starting stock for T87 tank plate; higher strength than T31 with lower ductility.31539311110 HB28 % IACS
Solution treated, mechanically stress-relieved (cold compressed),…
Forging temper (AMS 4144) with low residual stress and good short-transverse properties for machined cryogenic hardware.3454406128 HB30 % IACS
Solution heat treated, cold worked and artificially aged
Peak-aged 2219 after cold work — highest usable strength with retained cryogenic toughness and weldability, the standard aerospace tankage condition.35045510130 HB30 % IACS
T8, stress relieved by stretching
Low-residual-stress thick plate and rolled bar temper for machined structural fittings.3504558132 HB30 % IACS
Solution treated, cold worked, artificially aged
Final aged temper of T31 sheet/plate: high strength with better SCC resistance than naturally aged tempers.35245510134 HB30 % IACS
T87Default
T8 with 7 % cold work
The classic launch-vehicle cryogenic tank plate temper: highest 2219 strength with good weld and cryogenic performance.39347610130 HB30 % IACS

What is 2219-T351?

2219-T351 is 2219 in the T351 temper — low-residual-stress plate/bar version of T31 for machined parts that will later be aged or used as-is. 2219-T351 has a yield strength of 250 MPa (36.3 ksi) and a tensile strength of 360 MPa (52.2 ksi) — stronger than 65% of aluminum grades. Elongation at break is 15% and the elastic modulus is 73.8 GPa (10.7 Msi). 2219-T351 has a density of 2.84 g/cm³ (0.103 lb/in³), heavier than 93% of aluminum grades. It melts at 543°C (1,009 °F). T87 is the default condition FabDigit quotes; T351 is available on request or by drawing note.

Advantages

  • Tough — resists crack growth — 45 MPa·√m (41 ksi·√in), better than 100% of aluminum grades
  • Ductile — tolerates forming and impact — 15%, better than 82% of aluminum grades
  • Readily welded — 85/100, better than 79% of aluminum grades

Limitations

  • Needs corrosion protection — 28/100, worse than 99% of aluminum grades
  • Low electrical conductivity — 28 % IACS, worse than 82% of aluminum grades
  • Poor heat conductor — 121 W/m·K (69.9 BTU/hr·ft·°F), worse than 76% of aluminum grades

2219-T351 properties

Typical room-temperature values for 2219-T351; 22 are specific to this condition. Other listed values are 2219 reference data and may not represent this condition. Bars are the position among aluminum grades.

Physical3

2219-T351 has a density of 2.84 g/cm³ (0.103 lb/in³), heavier than 93% of aluminum grades. It melts at 543°C (1,009 °F).

Density2.84 g/cm³0.1 lb/in³
Melting Point (Solidus)543°C1,009 °F
Liquidus Temperature643°C1,189 °F

Mechanical12

2219-T351 has a yield strength of 250 MPa (36.3 ksi) and a tensile strength of 360 MPa (52.2 ksi) — stronger than 65% of aluminum grades. Elongation at break is 15% and the elastic modulus is 73.8 GPa (10.7 Msi).

Elastic (Young's) Modulus73.8 GPa10.7 Msi
Shear Modulus27 GPa3.9 Msi
Bulk Modulus73 GPa10.6 Msi
Poisson's Ratio0.33
Tensile Strength (Ultimate)360 MPa52.2 ksi
Yield Strength (0.2% offset)250 MPa36.3 ksi
Elongation at Break15%
Compressive Strength255 MPa37 ksi
Shear Strength230 MPa33.4 ksi
Fatigue Strength (Endurance Limit)115 MPa16.7 ksi
Fracture Toughness (K_IC)45 MPa·√m41 ksi·√in
Hardness, Brinell100 HB

Thermal6

2219-T351 is rated for continuous service to 150°C (302 °F). It conducts heat at 121 W/m·K (69.9 BTU/hr·ft·°F), worse than 76% of aluminum grades. Thermal expansion is 22.3 µm/m·K (12.4 µin/in·°F).

Thermal Conductivity121 W/m·K69.9 BTU/hr·ft·°F
Specific Heat Capacity864 J/kg·K0.21 BTU/lb·°F
Thermal Expansion (CTE, 20–100 °C)22.3 µm/m·K12.4 µin/in·°F
Latent Heat of Fusion390 J/g168 BTU/lb
Max Service Temperature (continuous)150°C302 °F
Min Service Temperature-269°C-452 °F

Electrical3

2219-T351 conducts electricity at 28 % IACS, worse than 82% of aluminum grades.

Electrical Conductivity28 % IACS
Electrical Resistivity6.16×10⁻⁸ Ω·m2.43 µΩ·in
Magnetic Responsenon-magnetic

Chemical & Environmental3

Corrosion resistance is poor (28/100), worse than 99% of aluminum grades.

Galvanic Potential (seawater, vs SCE)-0.64 V
Corrosion ResistancePoor28/100
Chemical Resistance SummaryGood in dry atmospheres and neutral organics/fuels; poor in chlorides, seawater and acids/alkalis — Cu-rich phases cause pitting, intergranular and exfoliation attack; T8x tempers markedly more SCC-resistant than T31/T37; always clad, anodize or prime for service.

Sustainability4

Producing a kilogram of 2219-T351 takes about 205 MJ of energy and emits 12.5 kg of CO₂ — more than 76% of aluminum grades. Typical recycled content is 5%.

Embodied Energy (primary production)205 MJ/kg88,134 BTU/lb
Embodied Carbon (primary production)12.5 kg CO₂/kg
Embodied Water1,200 L/kg144 gal/lb
Typical Recycled Content5%

Manufacturability8

2219-T351's machinability is good (62/100, better than 55% of aluminum grades); weldability excellent (85/100); formability fair (40/100).

MachinabilityGood62/100
Machinability Rating (AISI 1212 = 100 %)60%
WeldabilityExcellent85/100
Formability (cold)Fair40/100
CastabilityPoor30/100
Brazeability / SolderabilityPoor15/100
PolishabilityGood55/100
Anodizing Responsefair — high Cu content gives darker, less uniform and less protective films; chromic-acid or thin sulfuric anodize per MIL-A-8625 is used for aerospace corrosion protection rather than decoration

Values are nominal handbook figures for design screening. Confirm any required mill or lot documentation when quoting.

Working with 2219-T351

Is 2219 easy to machine?

Machines well in T8x tempers with sharp carbide tools, high speed and flood coolant; gummy and prone to built-up edge in O/T42.

Can 2219 be welded?

Best weldable 2000-series alloy — GTAW/GMAW/EBW/FSW with 2319 filler; welds are quench-sensitive, expect ~60–70 % of parent strength unless post-weld solution + age is possible.

Can 2219 be formed, bent or molded?

Form in O or T31/T42; T87 plate has low cold formability and should be brake-formed with generous radii or hot-formed 150–200 °C.

What surface finishes work on 2219?

Use chromic or thin sulfuric anodize plus primer for corrosion protection (Cu content darkens film); alkaline cleaning must be short to avoid intergranular attack; not suitable for bright decorative anodizing.

2219 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
Cumain strengthening addition5.8 – 6.86.3
Mn0.2 – 0.40.3
Si≤ 0.2—
Fe≤ 0.3—
Mg≤ 0.02—
Zn≤ 0.1—
Tigrain refiner0.02 – 0.10.06
Velevated-temperature stability0.05 – 0.150.1
Zrgrain-structure control, weld crack resistance0.1 – 0.250.18
Others (each)each≤ 0.05—
Others (total)total≤ 0.15—
Albalance—

2219-T351 — frequently asked

What is 2219-T351 used for?

2219-T351 is typically used for cryogenic propellant tanks, missile and launch-vehicle structures, welded cryogenic pressure vessels, supersonic airframe structures, machined aerospace forgings and elevated-temperature structural fittings. In short: weldable + cryogenic; aerospace tank.

What is the yield strength of 2219-T351?

2219-T351 has a typical yield strength of 250 MPa (36.3 ksi) and a tensile strength of 360 MPa (52.2 ksi) — stronger than 65% of aluminum grades. Strength varies by condition: see the 13 listed tempers.

Is 2219-T351 easy to machine?

Reasonably — machinability is rated good (62/100, better than 55% of aluminum grades). Machines well in T8x tempers with sharp carbide tools, high speed and flood coolant; gummy and prone to built-up edge in O/T42.

Can 2219-T351 be welded?

Yes — weldability is rated excellent (85/100). Best weldable 2000-series alloy — GTAW/GMAW/EBW/FSW with 2319 filler; welds are quench-sensitive, expect ~60–70 % of parent strength unless post-weld solution + age is possible.

What surface finishes work on 2219-T351?

Use chromic or thin sulfuric anodize plus primer for corrosion protection (Cu content darkens film); alkaline cleaning must be short to avoid intergranular attack; not suitable for bright decorative anodizing.

Can 2219-T351 be formed, bent or molded?

Form in O or T31/T42; T87 plate has low cold formability and should be brake-formed with generous radii or hot-formed 150–200 °C.

What is the maximum service temperature of 2219-T351?

2219-T351 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.

What is the difference between 2219-T87 and 2219-O?

T87 is the default condition — the classic launch-vehicle cryogenic tank plate temper: highest 2219 strength with good weld and cryogenic performance. O: softest, most formable condition for deep forming or before re-solution treatment; annealed at ~415 °C with slow cool. Yield strength is 393 MPa in T87 versus 76 MPa in O.

Can FabDigit make parts in 2219-T351?

Yes — 2219-T351 is available for CNC machining and sheet metal; every part is priced by an engineer rather than instantly. Upload a STEP file to get a price and a DFM check.

Sources

  1. Aluminum Association Teal Sheets — International Alloy Designations and Chemical Composition Limits — The Aluminum Association (2018)
  2. ASTM B209 / B209M — Aluminum Sheet and Plate — ASTM (2021)
  3. AMS-QQ-A-250/30 — 2219 Aluminum Alloy Plate and Sheet — SAE (2016)
  4. AMS 4143 / AMS 4144 — 2219 Forgings (T6, T852) — SAE (2017)
  5. ASM Handbook Vol. 2 — Properties and Selection: Nonferrous Alloys — ASM International (1990)
  6. MMPDS-2023 Metallic Materials Properties Development and Standardization — FAA/Battelle (2023)
  7. MatWeb alloy data sheets — Aluminum 2219 tempers — MatWeb LLC (2024)

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.