Closed-die forgings
Near-net-shape parts pressed in matched dies: fittings, brackets, hubs, wheels and housings. Least machining and best grain flow.
6061 aerospace forgings are die forgings, open-die (hand) forgings and rolled rings in 6061, heat-treated to T6 or T652 and certified to specifications such as AMS 4127, AMS 4248 and ASTM B247. Forging aligns the grain with the part shape and closes internal porosity, giving better toughness and ductility in all directions than a part machined from plate or bar. Metline supplies 6061 forgings to drawing, worldwide.

A forging is shaped by pressing or hammering a hot billet, so the metal's grain flows along the contour of the part. For a fitting, hub or ring that carries load in several directions, this gives more consistent ductility and fatigue behaviour than the same shape cut from plate, where properties in the thickness direction are weakest.
6061 is one of the easiest aluminium alloys to forge. It flows well at forging temperature, takes intricate die shapes and, after heat treatment to T6, gives a strong, weldable and corrosion-resistant part. It is chosen for moderately loaded fittings, wheels and hubs, rings, housings and valve bodies where 2014, 7050 or 7075 forgings would be stronger than needed and harder to protect from corrosion.
| Specification | Scope | Temper |
|---|---|---|
| SAE AMS 4127 | Die forgings (up to 4 in / 102 mm thick at heat treatment), hand forgings, forged and rolled rings, and forging stock | T6 |
| SAE AMS 4248 | Hand forgings and rolled rings, stress-relieved by compression | T652 |
| AMS-QQ-A-367 | General aluminium alloy forgings (former federal specification) | T6, T652 and others |
| ASTM B247 / B247M | Die, hand and rolled-ring forgings, commercial and industrial | O, T4, T6, T652 |
| EN 586-2 / -3 | European forgings: mechanical properties and tolerances (EN AW-6061) | T6 |
Forging specifications set maximum section thicknesses for each temper. For thick or heavy parts, check the limit before finalising the design.
Forgings use the standard 6061 composition. Copper is 0.15 – 0.40 % and chromium 0.04 – 0.35 %; tables that list copper as 0.15 % maximum or chromium as 0.04 % maximum are incorrect.
| Element | Minimum | Maximum | Role in the alloy |
|---|---|---|---|
| Silicon (Si) | 0.40 | 0.80 | Forms the strengthening Mg2Si phase with magnesium |
| Iron (Fe) | — | 0.70 | Impurity; held low for toughness and surface quality |
| Copper (Cu) | 0.15 | 0.40 | Adds strength; a small penalty in corrosion resistance |
| Manganese (Mn) | — | 0.15 | Grain structure control |
| Magnesium (Mg) | 0.80 | 1.20 | Main strengthening element with silicon |
| Chromium (Cr) | 0.04 | 0.35 | Limits recrystallisation, improves stress-corrosion resistance |
| Zinc (Zn) | — | 0.25 | Impurity |
| Titanium (Ti) | — | 0.15 | Grain refiner |
| Others, each / total | — | 0.05 / 0.15 | |
| Aluminium (Al) | Remainder | About 95.8 – 98.6 % |
Guaranteed properties for forgings are lower than for plate or bar in the same temper, because a forging is tested in several directions and thick sections cool more slowly when quenched. Values below are representative; the exact minimums depend on forging type, thickness and test direction in the governing specification.
| Condition | Tensile strength | Yield strength (0.2 %) | Elongation |
|---|---|---|---|
| T6 die forging, minimum (longitudinal, typical spec level) | About 260 MPa / 38 ksi | About 240 MPa / 35 ksi | About 7 % |
| T6 / T652, typical | 310 MPa / 45 ksi | 276 MPa / 40 ksi | 12 % |
| T4, typical | 240 MPa / 35 ksi | 145 MPa / 21 ksi | 22 % |
| O, typical | 125 MPa / 18 ksi | 55 MPa / 8 ksi | 25 % |
Typical Brinell hardness is about 95 HB in T6 and about 65 HB in T4. T451 is a plate and rolled-bar temper and is not normally used for forgings.
Near-net-shape parts pressed in matched dies: fittings, brackets, hubs, wheels and housings. Least machining and best grain flow.
Blocks, discs, shafts and bars shaped between flat or simple tools. Used for prototypes, low quantities and large parts machined to shape.
Seamless rings rolled from a pierced blank, for flanges, bearing housings, adaptor rings and launch-vehicle joints.
Solution treated, quenched and artificially aged. The standard temper for 6061 forgings.
T6 with 1 – 5 % cold compression after quenching to relieve stress. Chosen for large hand forgings and rings that will be heavily machined.
As-forged, annealed or naturally aged conditions, for parts that will be further worked or heat-treated by the user.
For highly loaded primary structure such as wing-to-fuselage fittings or landing-gear parts, 7050-T7452 or 7075-T73 forgings are normally specified. 6061 suits parts where the design stress is moderate and corrosion resistance or weldability is important.
AMS 4127 covers 6061-T6 die forgings, hand forgings and forged or rolled rings. AMS 4248 covers T652 hand forgings and rolled rings that are stress-relieved by compression.
Typical strength is similar, but forgings give more uniform properties in all directions and better fatigue behaviour at features such as lugs and bosses, because the grain follows the part shape.
T6 with a controlled cold compression of about 1 – 5 % after quenching, which reduces residual stress so large forgings and rings distort less when machined.
Yes. 6061 forgings weld with 4043 or 5356 filler, which is one reason they are chosen over 2xxx and 7xxx forgings. The heat-affected zone loses some strength unless re-heat-treated.
Closed-die forging suits larger quantities and gives near-net shape with the best grain flow. Open-die forging suits prototypes, small quantities and large parts that will be machined.
Yes. Forgings can be supplied with ultrasonic inspection to AMS-STD-2154 or ASTM B594 and an EN 10204 3.1 certificate, shipped worldwide.
Send your drawing, temper, quantity and specification. Our team will propose a forging route and a delivered price.