Menu
Aerospace forgings

6A02-T6 Aerospace Aluminium Forgings

6A02 (formerly LD2) is a heat-treatable aluminium-magnesium-silicon-copper forging alloy with excellent hot plasticity, good corrosion resistance and medium strength in T6. It is specified on drawings made to GB, HB and GJB standards, and is close to 6151 and 6061 in other systems. Metline supplies 6A02 die forgings, free forgings, rings and forged bar to HB 5204 and GJB 2351, certified and shipped worldwide.

Forging of 6A02 aluminium alloy aerospace parts
Alloy
6A02 (Al-Mg-Si-Cu)
Temper
T6 (O, T4 on request)
Standards
HB 5204 · GJB 2351 · GB/T 3190
Forms
Die & free forgings, rings, bar
Overview

What is 6A02 aluminium?

6A02 belongs to the 6xxx family. Its magnesium and silicon form Mg2Si, while 0.2–0.6 % copper adds strength beyond 6061-level and either manganese or chromium controls grain growth. The alloy is valued above all for its plasticity when hot, which lets it be forged into complex shapes at modest pressure.

In T6 temper 6A02 offers medium strength, good fatigue behaviour and better corrosion resistance than the 2xxx forging alloys. It also stays ductile at low temperatures. These qualities made it a standard choice for moderately loaded aircraft forgings, engine accessory housings and helicopter parts, especially where complex shapes with thin webs are required.

For buyers working in other standards, 6A02 sits between 6061 and 6151: it has a little more copper than 6061 and less silicon and chromium than 6151. It is not formally identical to any AA alloy, so substitution must be approved by the design authority.

Chemical composition

6A02 chemical composition (wt %)

Limits per GB/T 3190. The certificate for each lot reports the actual analysis.

ElementMinimumMaximumRole
Silicon (Si)0.501.20Forms Mg2Si; aids hot workability
Iron (Fe)—0.50Impurity
Copper (Cu)0.200.60Raises strength more than in 6061
Manganese (Mn) or chromium (Cr)0.150.35Either element may be used for grain control
Magnesium (Mg)0.450.90Main strengthening element with Si
Zinc (Zn)—0.20Impurity
Titanium (Ti)—0.15Grain refiner
Others, each / total—0.05 / 0.10
Aluminium (Al)Remainder
Mechanical properties

Mechanical properties of 6A02-T6 forgings

Forging standards set minimums by direction: longitudinal (L, along the grain flow), long-transverse (LT) and short-transverse (ST). Values below are the minimums commonly quoted for T6 forgings under the two main aviation standards; always confirm against the current edition named on your drawing.

Standard and productDirectionTensile strength RmYield Rp0.2Elongation AHardness
GJB 2351, free and die forgings, T6L≥ 275 MPa—≥ 10 %≈ 85 HB
HB 5204, die forgings, T6L≥ 295 MPa≥ 215 MPa≥ 12 %≈ 85 HB
HB 5204, die forgings, T6LT≥ 265 MPa—≥ 4 %—

Physical properties (T6)

Density
≈ 2.70 g/cm³
Modulus of elasticity
≈ 70 GPa
Thermal conductivity
≈ 155 – 175 W/m·K
Thermal expansion
≈ 23 µm/m·°C (20 – 100 °C)
Melting range
≈ 595 – 650 °C
Heat treatment

Tempers and heat treatment

T6

Solution heat-treated at about 515–530 °C, water quenched and artificially aged. The standard delivery temper for aerospace forgings.

T4

Solution treated and naturally aged; more ductile. Used where parts are formed or straightened before final ageing.

O / as-forged

Supplied for customers who carry out their own heat treatment after rough machining.

Quench delay and water temperature have a strong effect on thick forgings. For sections over about 75 mm, ask for properties to be tested at mid-thickness, not only near the surface.

Standards & equivalents

Specifications and equivalent grades

SpecificationScope
HB 5204Aviation standard for aluminium alloy die forgings
GJB 2351Specification for aluminium alloy forgings for aerospace use
GB/T 3190Chemical composition of wrought aluminium alloys
GB/T 16865 / GB/T 228.1Tensile test specimens and methods
ASTM B594 or AMS-STD-2154Ultrasonic inspection, when called up by the buyer
SystemDesignationComment
GB/T 31906A02Current national designation
Former designationLD2Still seen on older drawings
GOST 4784AV (АВ)Russian equivalent, very close in composition
Nearest AA grades6151, 6061Similar Mg-Si-Cu-Cr base; not identical
Nearest EN gradeEN AW-6061Used as a substitute on European drawings
Supply range

Forging types we supply

TypeTypical partsNotes
Closed-die forgingsHousings, brackets, levers, fittingsNear-net shape to drawing
Free (open-die) forgingsBlocks, bars, step shaftsMachining allowance agreed per order
RingsFlanges, casings, bearing housingsSeamless rolled or forged rings
Discs and hubsWheel hubs, covers, rotorsUpset for radial grain flow
Back-extruded tubesHollow cylinders and sleevesSeamless, heavy wall

Maximum sizes depend on shape and forging route and are confirmed against each drawing.

Quality

Inspection and documents

  • Chemical analysis of each cast
  • Tensile tests in L, LT or ST directions as the standard and drawing require
  • Hardness check on every heat-treatment lot
  • Ultrasonic inspection and macro-etch grain-flow checks on request
  • Dimensional report against the forging drawing
  • EN 10204 3.1 certificate; third-party inspection on request
Applications

Where 6A02 forgings are used

  • Airframe: moderately loaded fittings, hinge brackets and frame joints
  • Engine accessories: gearbox and pump housings, mounting brackets
  • Helicopters: complex forgings with thin ribs and webs
  • Instruments and avionics: structural housings and chassis
  • Industrial: pneumatic and hydraulic bodies, machine parts that need good corrosion resistance

6A02 is not used for turbine blades or hot-section engine parts: like all aluminium alloys, it loses strength rapidly above about 150 °C.

Comparison

6A02 compared with other forging alloys

Property6A02-T66061-T66151-T62A50 / 2014-T6
Typical tensile strength≈ 320 – 340 MPa≈ 310 MPa≈ 330 MPa≈ 420 – 485 MPa
Hot plasticityExcellentGoodExcellentGood
Corrosion resistanceGoodVery goodVery goodFair
Typical drawing standardGB / HB / GJBASTM / AMSAMS 4125GB / ASTM / AMS
Ordering

How to order 6A02 forgings

  1. SpecifyDrawing, alloy and temper, forging standard (HB 5204, GJB 2351 or equivalent), test directions and quantity.
  2. ReviewWe confirm forging route, test locations, documentation and delivery terms (EXW, FOB, CIF or DAP).
  3. InspectMechanical, dimensional and any NDT checks are completed and recorded.
  4. ShipForgings are protected and export-packed for sea or air freight with the 3.1 certificate.
Sources

References and standards

  1. GB/T 3190 – Wrought aluminium and aluminium alloys: chemical composition
  2. HB 5204 – Aluminium alloy die forgings (aviation industry standard)
  3. GJB 2351 – Specification for aluminium alloy forgings for aeronautics and astronautics
  4. GOST 4784 – Aluminium and wrought aluminium alloys: grades
  5. The Aluminum Association – International Alloy Designations and Chemical Composition Limits (Teal Sheets)
FAQ

6A02 aerospace forgings: frequently asked questions

What is the international equivalent of 6A02?

There is no exact match. The Russian grade AV is very close, and among AA alloys 6151 and 6061 are the nearest. Any substitution needs approval from the design authority.

What is the old name for 6A02?

LD2. Older drawings and specifications often still use it.

What strength does 6A02-T6 reach?

Die forgings to HB 5204 are commonly quoted at a minimum of 295 MPa tensile and 215 MPa yield in the longitudinal direction, with typical values somewhat higher.

Is 6A02 weldable?

It can be welded by TIG or MIG with 4043-type filler, but the heat-affected zone loses T6 strength. Forgings are usually joined mechanically.

Can you supply 6A02 forgings to a European or US specification?

Where the design authority allows it, we can offer 6061 or 6151 forgings to ASTM B247, AMS or EN 586 as an alternative.

Need 6A02 forgings?

Send the drawing, standard and quantity. We will reply with the forging route, certification and a delivered price.