T6
The standard and almost universal temper for 4032 forgings and pistons.
4032-T6 forgings combine the low thermal expansion and wear resistance of a 12 % silicon alloy with the soundness and grain flow of a forging. They are the standard material for forged pistons in aircraft piston engines, compressors and hydraulic pumps. Metline supplies 4032 forgings and forged piston blanks to ASTM B247, legacy AMS 4145 or your drawing, worldwide.

A piston sees combustion pressure, inertia loads and temperatures well above 200 °C at the crown, while sliding in a steel or cast-iron bore. It has to be light, strong when hot, resistant to wear and dimensionally steady as it heats up.
Cast pistons in Al-Si alloys handle most of those demands, but a forging adds strength, ductility and fatigue resistance because closed-die forging closes porosity and aligns grain flow with the piston's shape. 4032 brings the alloy advantages to the forging: about 12 % silicon for low expansion and wear resistance, nickel and copper for strength at temperature, and magnesium for a strong T6 temper.
The result is a piston that can run with tight skirt clearance, stays quiet when cold, seals well and resists scuffing. Aircraft piston engines, high-performance automotive engines, compressors and hydraulic pumps all use forged 4032 pistons for these reasons. Outside pistons, 4032 forgings are used for wear-resistant bushings, pump and valve parts and swashplates.
| Element | Minimum | Maximum | Role |
|---|---|---|---|
| Silicon (Si) | 11.0 | 13.5 | Low thermal expansion, wear resistance |
| Copper (Cu) | 0.50 | 1.3 | Strength and elevated-temperature strength |
| Magnesium (Mg) | 0.8 | 1.3 | Age hardening with Si |
| Nickel (Ni) | 0.50 | 1.3 | Strength retention at temperature |
| Iron (Fe) | — | 1.0 | Impurity |
| Chromium (Cr) | — | 0.10 | |
| Zinc (Zn) | — | 0.25 | Impurity |
| Others, each / total | — | 0.05 / 0.15 | |
| Aluminium (Al) | Remainder | About 82 – 87 % |
AMS 4145 describes the nominal composition as 12.2Si-1.1Mg-0.9Cu-0.9Ni. Some older listings give silicon as 6 – 12 % and omit nickel; those figures are wrong for 4032 and should not be accepted on a certificate.
ASTM B247 sets the specified minimums for 4032-T6 die forgings, including a tensile strength of about 360 MPa (52 ksi); yield and elongation minimums are given in the same table and depend on the forging type and test direction. Typical values sit somewhat higher.
| Property | Typical 4032-T6 |
|---|---|
| Tensile strength | about 380 MPa (55 ksi) |
| Yield strength (0.2 %) | about 315 MPa (46 ksi) |
| Elongation | about 5 – 9 % depending on direction and section |
| Brinell hardness | about 115 – 125 HB |
| Shear strength | about 260 MPa |
| Fatigue strength (5 × 10⁸ cycles) | about 110 MPa |
At piston operating temperatures, 4032 keeps a useful fraction of its room-temperature strength, more than 6xxx alloys but less than 2618, which was developed specifically for long exposure at high temperature. That trade-off drives the choice between the two forging alloys.
Forgings are solution heat-treated, quenched and artificially aged to T6. A typical cycle, consistent with AMS 2770 practice for wrought aluminium, is solution treatment at about 505 – 520 °C, water quench, then ageing at about 170 °C for around 10 hours. The exact cycle is fixed by the specification and qualified by the forge.
The standard and almost universal temper for 4032 forgings and pistons.
Forging stock may be supplied annealed (O) or as fabricated (F) for forging and later heat treatment.
Listed on some older pages for 4032 forgings, but not standard 4032 forging tempers. T73 is a 7xxx-alloy over-ageing temper. If your drawing shows them, ask the design authority to confirm.
Some piston makers apply a stabilising heat treatment so pistons do not grow when they first see engine temperature. Where this matters, state it on the order.
| Document | Scope | Status / note |
|---|---|---|
| ASTM B247 / B247M | Die, hand and rolled-ring forgings, including 4032-T6 | Current; normal commercial and many aerospace orders |
| SAE AMS 4145 | Forgings, 12.2Si-1.1Mg-0.9Cu-0.9Ni (4032-T6) | Cancelled by SAE in 1996 but still seen on legacy drawings; agree a replacement with the customer |
| AMS-QQ-A-367 / QQ-A-367 | Aluminium alloy forgings, general | Legacy federal / SAE document covering several alloys |
| AMS 2770 | Heat treatment of wrought aluminium parts | Process reference |
| AMS-STD-2154 | Ultrasonic inspection of wrought metals | Inspection on request |
| EN 586 / JIS H4140 | European and Japanese forging standards | For EN AW-4032 and A4032 forgings |
Near-net piston blanks with crown, skirt and pin bosses formed in the die, ready for machining.
Upset discs for machining pistons, pump parts and valve plates where volumes do not justify dedicated dies.
Forged and heat-treated bar for bushes, sleeves and wear parts.
Forged or rolled rings for wear sleeves and bearing housings, to drawing.
Size limits depend on the forging route and die; we confirm feasibility for each drawing rather than quoting a general size table.
| Factor | 4032-T6 | 2618-T61 |
|---|---|---|
| Silicon content | 11 – 13.5 % | 0.10 – 0.25 % |
| Thermal expansion | Lower (≈ 19.4 µm/m·°C) | Higher (≈ 22 µm/m·°C) |
| Cold clearance | Tighter; quieter cold start | Larger; more cold noise |
| Wear and scuff resistance | Better | Lower; often coated |
| Ductility and toughness | Lower | Higher; tolerates detonation better |
| Strength at sustained high temperature | Good | Better |
| Typical choice | Normally aspirated and moderate-output engines, compressors | High-boost, high-load and racing engines |
4032 forgings are not used for airframe structure, fuel pipes, landing-gear hubs or similar parts that older listings mention; those use 2xxx, 6xxx or 7xxx forgings.
Its 12 % silicon gives low thermal expansion and good wear resistance, so pistons run with tight clearances, quietly and with little scuffing. Forging adds strength and fatigue resistance over casting.
SAE lists AMS 4145 as cancelled (1996), although it still appears on legacy drawings. ASTM B247 covers 4032-T6 forgings and is the usual current reference; agree the replacement with your customer.
T6 is the standard temper for 4032 forgings. T73 is a 7xxx over-ageing temper and does not apply; T651 is a stretched temper for plate and bar. Confirm any such call-out with the design authority.
2618 is more ductile and better for very high cylinder pressures and detonation. 4032 suits engines where low noise, tight clearance and wear resistance matter more.
Chemistry, tensile and hardness results on a 3.1 certificate, with grain-flow macro-etch and ultrasonic inspection available on request.
Yes. Metline supplies 4032 forgings and piston blanks worldwide from Mumbai, with export packing and certificates.
Send the drawing, quantity, specification and inspection requirements. We will confirm feasibility and documentation.