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Aerospace · Structural sheet and plate

6082 Aerospace Aluminium Sheet & Plate (T6, T651)

6082 is the strongest of the widely stocked European 6xxx plate alloys and, as BS L113 sheet and BS L115 plate, an established material for aerospace fittings, tooling, ground support equipment and machined parts. T651 plate is stretched to stay flat during heavy machining, and the alloy welds, anodises and resists corrosion well. Metline supplies 6082 sheet and plate in O, T4, T6 and T651, cut to size and certified to aerospace, EN or ASTM standards, worldwide.

6082-T651 aluminium plates stacked for machining into aerospace fittings
Alloy
6082 (Al-Si-Mg-Mn)
Tempers
O, T4, T6, T651
Thickness
Sheet 0.5 – 6 mm; plate 6 – 250 mm
Standards
BS L113 · L115 · EN 485
Overview

What 6082 aerospace plate is used for

6082 is an aluminium-silicon-magnesium-manganese alloy. Its silicon content is higher than the Mg2Si ratio requires, and the excess raises strength after ageing; manganese controls the grain structure and adds a little strength of its own. With copper held at 0.10 % maximum, corrosion resistance is better than 6061.

The alloy was developed in Europe and replaced the older British grade HE30/H30, which is why it is sometimes still called "H30" in workshops. For aerospace use, the British L-series covers 6082 in all main forms: BS L113 for T6 sheet and strip, BS L115 for T651 plate, L111 for bar and sections, L112 for forgings and L114 for tube. Many European aerospace suppliers and MRO shops use these specifications for parts where 6061-class strength is enough.

Typical aerospace plate applications are machined brackets, mounting plates and fittings in secondary structure, avionics and equipment trays, cargo-system and seat components, assembly jigs and tooling plates, and a very wide range of ground support equipment such as stairs, platforms, towbars and engine stands. Primary structure such as wing skins, spars and fuselage frames uses 2024, 7075, 7050 or aluminium-lithium plates, which offer far higher strength and damage tolerance, so treat claims that 6082 is used for wings or fuselage skins with caution.

In general engineering 6082 is sometimes described as having replaced 6061 because of its higher strength. In reality the two are very close: 6082-T651 plate is slightly stronger in thick sizes and more corrosion resistant, while 6061 is more widely stocked outside Europe and has more US aerospace specifications. The choice usually follows the standards system of the drawing.

Chemical composition

6082 chemical composition (wt %)

Limits follow EN 573-3 for EN AW-6082 and the Aluminum Association registration. BS L113 and L115 call the same composition. Note that the magnesium minimum is 0.60 %; data sheets showing 0.06 % contain a typing error.

ElementMinimumMaximumRole in the alloy
Silicon (Si)0.701.30Excess Si over the Mg2Si ratio raises aged strength
Iron (Fe)—0.50Impurity
Copper (Cu)—0.10Kept low for corrosion resistance
Manganese (Mn)0.401.00Suppresses recrystallisation and coarse grain; adds strength
Magnesium (Mg)0.601.20Main strengthening element with Si
Chromium (Cr)—0.25Grain control
Zinc (Zn)—0.20Impurity
Titanium (Ti)—0.10Grain refiner
Others, each / total—0.05 / 0.15
Aluminium (Al)RemainderAbout 95.2 – 98.3 %

The manganese range is wide. Plate producers usually target the upper half to suppress recrystallisation during solution treatment, which keeps a fine grain structure and higher strength in thick plate.

Mechanical & physical properties

Mechanical properties of 6082 sheet and plate

Values below are minimums from EN 485-2 by thickness band. Minimums fall as plate gets thicker because the centre cools more slowly during quenching. BS L113 sheet quotes 295 MPa tensile and 255 MPa proof stress up to 3 mm and 295 / 240 MPa from 3 to 25 mm; L115 plate follows a similar pattern. Design to the minimums printed on the certificate.

Temper / thicknessTensile strength (min)0.2 % proof stress (min)Elongation (min)
O, 0.4 – 25 mm≤ 150 MPa (max)≤ 85 MPa (max)14 – 18 %
T4, 0.4 – 12.5 mm205 MPa110 MPa12 – 14 %
T6, 0.4 – 1.5 mm310 MPa260 MPa6 % (A50)
T6, 1.5 – 3 mm310 MPa260 MPa7 % (A50)
T6, 3 – 6 mm310 MPa260 MPa10 % (A50)
T6 / T651, 6 – 12.5 mm300 MPa255 MPa9 % (A50)
T651, 12.5 – 60 mm295 MPa240 MPa8 % (A)
T651, 60 – 100 mm295 MPa240 MPa7 % (A)
T651, 100 – 150 mm275 MPa240 MPa6 % (A)
T651, 150 – 175 mm275 MPa230 MPa4 % (A)

Values summarised from EN 485-2; the edition on your order governs. Typical T651 values are about 320 – 340 MPa tensile, 280 – 300 MPa proof stress and 95 – 100 HB.

Physical properties

Density
2.70 g/cm³ (0.0975 lb/in³)
Modulus of elasticity
about 70 GPa
Thermal conductivity (T6)
about 170 – 180 W/m·K
Electrical conductivity (T6)
about 40 – 45 % IACS (24 – 26 MS/m)
Coefficient of thermal expansion
about 23.4 µm/m·°C (20 – 100 °C)
Melting range
about 575 – 650 °C
Shear strength (T6, typical)
about 210 MPa
Fatigue strength (T6, typical, 5 × 10⁸ cycles)
about 95 MPa
Tempers

Which 6082 temper to order

6082-T651 (BS L115)

Solution treated, stretched 1.5 – 3 % and aged. The standard for plate above about 6 mm that will be machined: residual stress is low, so parts stay flat.

6082-T6 (BS L113)

Solution treated and aged without stretching. Normal for sheet up to about 6 mm, used flat or lightly formed.

6082-T4

Solution treated and naturally aged. Bend or form, then age to T6 if needed.

6082-O

Annealed for the deepest forming. Strength is restored by full heat treatment after forming.

T5 and T6511

These are extrusion tempers. If a plate enquiry mentions them, it usually means T6 or T651; we confirm before quoting.

Cast tooling plate

If flatness matters more than strength, consider cast and milled tooling plate alongside 6082-T651.

Standards & equivalents

6082 plate standards and international designations

Standard / designationScope
BS L1136082-T6 sheet and strip, British aerospace series
BS L1156082-T651 plate, British aerospace series
EN 485-1 / -2 / -3 / -4Sheet, strip and plate: delivery conditions, properties and tolerances
EN 573-3Chemical composition (EN AW-6082, AlSi1MgMn)
ASTM B209 / ASME SB-209Sheet and plate; 6082 is registered and can be certified to ASTM on request
BS 1470 (legacy)HS30 (sheet) and HP30 (plate); superseded by EN 485
Werkstoff / DIN (legacy)3.2315, AlMgSi1
UNSA96082
ISOAlSi1MgMn (ISO 6361 for sheet and plate)

If your drawing quotes HP30 or HS30, those are the older British plate and sheet designations for the same alloy, and EN AW-6082 to EN 485 is the modern replacement. For aerospace parts, keep to the specification named on the drawing; substitution between BS L-series, EN and ASTM certification needs written approval.

Supply range

6082 sheet and plate sizes and weights

Supply range

Sheet
0.5 – 6 mm thick (0.020 – 0.236 in)
Plate
6 – 200 mm standard; up to about 250 mm by enquiry (0.25 – 9.8 in)
Width
1000, 1250, 1500 mm standard; wider plate to about 2500 mm, and very wide plate by enquiry
Length
2000 – 6000 mm standard; longer lengths and cut-to-size blanks on request
Imperial sizes
48 × 96 in, 48 × 144 in and 60 × 120 in sheets; 1/8 – 6 in thickness
Surface
Mill finish; PE or PVC film (one or both sides); brushed, anodised or precision-milled on request
Processing
Saw cutting, waterjet and CNC profiling to drawing

Very wide or very thick plate is made to order; send the size early so we can confirm the supply route.

6082 weighs 2.70 kg per square metre for every millimetre of thickness. Metric reference weights:

Thickness (mm)kg per m²1250 × 2500 mm (kg)1500 × 3000 mm (kg)
12.708.412.2
1.54.0512.718.2
25.4016.924.3
38.1025.336.5
410.8033.848.6
513.5042.260.8
616.2050.672.9
821.6067.597.2
1027.0084.4121.5
1232.40101.2145.8
1643.20135.0194.4
2054.00168.8243.0
2567.50210.9303.8
3081.00253.1364.5
40108.00337.5486.0
50135.00421.9607.5
60162.00506.3729.0
80216.00675.0972.0
100270.00843.81215.0
150405.001265.61822.5
200540.001687.52430.0

Imperial reference weights (density 0.0975 lb/in³):

Thickness (in)lb per ft²48 × 96 in sheet (lb)48 × 144 in sheet (lb)
0.1251.7656.284.2
0.253.51112.3168.5
0.3755.27168.5252.7
0.57.02224.6337.0
0.7510.53337.0505.4
114.04449.3673.9
1.2517.55561.6842.4
1.521.06673.91010.9
228.08898.61347.8
2.535.101123.21684.8
342.121347.82021.8
456.161797.12695.7
570.202246.43369.6
684.242695.74043.5
Tolerances & quality

Tolerances, flatness and inspection

Unless the drawing states otherwise, dimensional tolerances follow EN 485-3 for hot-rolled plate and EN 485-4 for cold-rolled sheet, or ANSI H35.2 when ordered to ASTM B209. Cut-to-size blanks are typically held to ±0.5 – 1 mm; precision-milled plate can be held much tighter.

Inspection and documentation

Dimensions and flatness
Checked on every plate against the order standard
Surface
Visual inspection for scratches, roll marks, corrosion and handling damage
Ultrasonic testing
For thick aerospace plate on request, for example to AMS-STD-2154 Class A or B
Mechanical testing
Tensile tests per lot, with hardness and conductivity checks where required
Certification
EN 10204 3.1 mill certificate with chemistry and mechanical results, traceable to the lot
Machining

Machining 6082 plate for aerospace parts

6082-T651 machines well with carbide tooling at high spindle speeds and flood coolant. Because it contains almost no copper, chips are a little longer and stringier than with 6061, so chip-breaker geometries, high-pressure coolant and good evacuation help on deep pockets.

The main risk in machining plate is distortion. Quenching leaves the surface in compression and the core in tension; removing material unbalances those stresses. T651 stretching reduces them to a low level, so specify T651 for any plate that will lose a large share of its weight to machining. For thin-walled parts, rough-machine both sides, let the part relax, then finish-machine.

  • Use sharp, polished carbide tools with high positive rake and large flute volume
  • Machine symmetrically from both faces to keep residual stress balanced
  • Leave about 1 – 2 mm finishing stock after roughing on large or thin parts
  • Avoid clamping distortion: use vacuum or distributed clamping on thin plate
  • Deburr and clean before anodising to avoid marks in the finished coating
Working with 6082

Welding, forming, finishing and corrosion

Welding

Weldable by TIG, MIG and friction stir welding. Use ER4043 for crack resistance or ER5356 / ER5183 for higher strength and better colour match after anodising. The heat-affected zone falls to roughly 50 – 60 % of T6 strength unless re-heat-treated.

Forming

Bend O or T4 sheet tightly; T6 needs inside radii of about 1.5 – 3 × thickness. Bend across the rolling direction where possible.

Anodising

Takes sulphuric, hard and, for aerospace process specifications, chromic or boric-sulphuric anodising. The film is slightly less bright than on 6063.

Corrosion

Very good resistance to atmospheric and marine exposure. Isolate from carbon fibre and stainless or titanium fasteners with sealant and primer.

Temperature

Keeps useful strength up to about 100 – 150 °C; prolonged exposure above that over-ages the alloy.

Cryogenic service

Like other 6xxx alloys, strength and toughness hold up well at low temperature.

Applications

Typical aerospace uses of 6082 plate

  • Machined fittings and brackets in secondary structure and systems installations
  • Avionics trays, equipment shelves and mounting plates
  • Cargo and seat systems: base plates, rails and machined components
  • Assembly tooling: jigs, fixtures, drilling templates and base plates for aircraft assembly
  • Ground support equipment: maintenance platforms, stairs, towbars, engine stands and trolleys
  • Space and UAV: structural panels, brackets and mounting plates in small satellites and drones
  • Test rigs: frames and fixtures for structural and systems testing

A typical example is an assembly fixture for a fuselage panel: the base and uprights are cut from 6082-T651 plate, machined flat and anodised, giving a stiff, light fixture that resists corrosion in a humid hangar.

Comparison

6082 plate compared with 6061, 5083, 2024 and 7075

Property6082-T6516061-T6515083-H1112024-T3517075-T651
Typical tensile strength320 – 340 MPa310 MPa290 MPa470 MPa570 MPa
Typical yield strength280 – 300 MPa276 MPa145 MPa325 MPa505 MPa
MachinabilityVery goodVery goodFairVery goodExcellent
WeldabilityGoodGoodExcellentPoorPoor
Corrosion resistanceVery goodGoodExcellentPoorFair
Typical aerospace roleFittings, tooling, GSEFittings, tooling, GSEWelded GSE, tanksDamage-tolerant structureHigh-strength structure

In practice, 6082 and 6061 are close substitutes, but substitution needs approval because they are different designations. Choose 2024 or 7075 when strength or fatigue dominates and the part will not be welded, and 5083 for welded structures that must keep their strength. See our 6061 vs 6082 comparison.

Ordering

How to order 6082 aerospace plate

  1. SpecifyAlloy and temper, thickness, width and length or a cutting drawing, surface protection, quantity and the governing specification with its revision (BS L113, BS L115, EN 485 or ASTM B209).
  2. ConfirmWe confirm the specification can be met, the tolerance class, any extra tests and the delivery terms (EXW, FOB, CIF or DAP).
  3. InspectMaterial is checked for dimensions, straightness and surface condition; tests named on the order are carried out or arranged with a third party.
  4. DocumentEach lot ships with a mill test certificate to EN 10204 3.1 showing chemistry and mechanical results, traceable to the cast or lot number.
  5. Pack and shipExport packing in sealed, moisture-protected wooden cases or on pallets, shipped by sea or air to your port or door.
Sources

References and standards

  1. BS L113 – Aluminium Alloy 6082-T6 Sheet and Strip (British aerospace series)
  2. BS L115 – Aluminium Alloy 6082-T651 Plate (British aerospace series)
  3. EN 485-2 – Aluminium and aluminium alloys: sheet, strip and plate, mechanical properties
  4. ASTM B209 – Standard Specification for Aluminum and Aluminum-Alloy Sheet and Plate
  5. EN 573-3 – Aluminium and aluminium alloys: chemical composition and form of wrought products
  6. The Aluminum Association – International Alloy Designations and Chemical Composition Limits (Teal Sheets)
FAQ

6082 aerospace aluminium (aluminum) plate: FAQs

What are BS L113 and BS L115?

They are British aerospace specifications for 6082: L113 covers T6 sheet and strip and L115 covers T651 plate. Both use the standard 6082 chemistry with minimum properties set by thickness.

Is 6082 plate stronger than 6061?

Slightly, in most thicknesses: EN 485-2 gives 6082-T651 a minimum of 295 – 300 MPa tensile up to 60 mm, against about 290 MPa for 6061-T651 under ASTM B209. 6082 also resists corrosion better because of its low copper.

Should I order T6 or T651?

Order T651 for plate over about 6 mm that will be machined, because stretching relieves quench stresses and prevents warping. T6 is normal for thinner sheet.

Is 6082 used for aircraft wing skins or fuselage?

No. Primary structure uses 2024, 7075, 7050 or aluminium-lithium alloys. 6082 plate is used for fittings, equipment mounts, tooling and ground support equipment.

Can 6082 plate be welded?

Yes, by TIG, MIG or friction stir welding with ER4043, ER5356 or ER5183 filler. The weld zone loses part of its T6 strength, so welded designs use reduced allowables or post-weld heat treatment.

How much does 6082 plate weigh?

It weighs 2.70 kg per m² per millimetre of thickness. A 1250 × 2500 × 10 mm plate weighs about 84.4 kg.

Do you cut 6082 plate to size and ship internationally?

Yes. Metline cuts 6082 plate to size by saw or waterjet, protects it with film on request and ships worldwide with an EN 10204 3.1 certificate.

Need 6082 plate for aerospace parts or tooling?

Send the temper, size, quantity, specification and destination. We will reply with availability, certification and a delivered price.