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Aerospace · Al-Mn sheet

3103 / 3103A Aircraft Aluminium Sheet

3103 is the European aluminium-manganese sheet alloy, a close relative of 3003, used in aircraft for formed, lightly loaded parts such as fairings, ducting, tanks and heat-exchanger components. It is non-heat-treatable, forms and welds easily and resists corrosion well. Metline supplies 3103 and 3103A sheet to EN 485 and British aerospace specifications, worldwide.

Stack of 3103 aluminium sheet with protective interleaving
Alloy
EN AW-3103 / 3103A (AlMn1)
Tempers
O, H12, H14, H16, H18, H2x
Standards
EN 485 · EN 573-3 · BS L59/L60/L61
Thickness
0.5 – 6 mm sheet; plate on request
Overview

What 3103 is, and why British and European drawings call for it

3103 (AlMn1) carries about 1 % manganese with no required copper. It is the standard Al-Mn sheet alloy in Europe, in the same way that 3003 is in North America.

Like every 3xxx alloy, 3103 gains strength only from cold work. It is supplied annealed (O) for heavy forming, or strain-hardened to quarter, half, three-quarter or full hard. Because no solution treatment or ageing is involved, formed parts keep their properties without further heat treatment, and welding does not cause the large strength loss seen in heat-treated alloys beyond the return to annealed strength in the heat-affected zone.

British aircraft programmes adopted 3103 under the old BS 1470 designation N3 (NS3 for sheet) and the BS aerospace L-series. It remains a common choice for formed secondary parts on aircraft and helicopters designed or maintained to UK and European documentation, and for ground support equipment, ducting and heat exchangers.

Chemical composition

3103 chemical composition (wt %)

Limits below follow EN 573-3 for EN AW-3103. 3103A is a separately registered variant with slightly different limits; a mill certificate states which one the material meets, and the two should not be swapped without the design authority agreeing.

Element3103 (EN AW-3103)3003, for comparison
Silicon (Si)≤ 0.50≤ 0.6
Iron (Fe)≤ 0.7≤ 0.7
Copper (Cu)≤ 0.100.05 – 0.20
Manganese (Mn)0.9 – 1.51.0 – 1.5
Magnesium (Mg)≤ 0.30—
Chromium (Cr)≤ 0.10—
Zinc (Zn)≤ 0.20≤ 0.10
Zirconium + titanium (Zr + Ti)≤ 0.10—
Others, each / total0.05 / 0.150.05 / 0.15
Aluminium (Al)RemainderRemainder

The practical differences are small: 3103 allows a little magnesium and no minimum copper, while 3003 requires 0.05 % copper. Strength and formability are essentially the same, which is why most non-critical applications treat them as alternatives.

Mechanical & physical properties

3103 sheet properties by temper

Values below are the EN 485-2 tensile limits for 3103 sheet in mid thickness bands (roughly 0.5 – 3 mm). Limits shift slightly with thickness, and the governing specification on your order always takes precedence.

TemperConditionTensile Rm (MPa)Proof Rp0.2 min (MPa)
O / H111Annealed90 – 13035
H12Quarter hard115 – 15585
H14Half hard140 – 180120
H16Three-quarter hard160 – 200145
H18Full hard185 min165
H22Quarter hard, partially annealed115 – 15580
H24Half hard, partially annealed140 – 180110
H26Three-quarter hard, partially annealed160 – 200135

Physical properties (typical)

Density
2.73 g/cm³
Melting range
about 640 – 655 °C
Modulus of elasticity
about 69 GPa
Thermal conductivity
about 155 – 190 W/m·K depending on temper
Thermal expansion
about 23 µm/m·°C (20 – 100 °C)

Some older data sheets for this product mix up the rows of the property table, listing elongation in MPa and shear strength in per cent. The values above are arranged correctly.

Tempers

Which 3103 temper to order

O

For deep drawing, spinning and stretch forming. Parts can be formed to very tight radii and stiffen slightly as they work-harden.

H14

The most commonly ordered temper. Stiff enough for panels and covers while still bending well in thin gauges.

H12 / H22

Light cold work for parts that need a little more stiffness than O but still see heavy forming. Associated with the BS L60 sheet document.

H16 / H26

Higher strength for flat or lightly formed parts that must resist denting. Associated with the BS L59 sheet document.

H18

Full hard, for flat parts, fins and feedstock that will not be bent much.

H2x vs H1x

H2x tempers reach the same strength band with more elongation, so they tolerate bending after blanking better than the matching H1x temper.

Standards

3103 standards and equivalent designations

The British aerospace sheet documents for 3103 are the L-series: BS L59, BS L60 and BS L61, which cover 3103 sheet in different temper conditions (harder, half-hard and annealed respectively). Always check the current issue of the document named on the drawing to confirm the exact temper and test requirements before ordering.

SystemDesignationDocument
EuropeanEN AW-3103 / EN AW-AlMn1EN 573-3, EN 485-1/-2/-4
European variantEN AW-3103AEN 573-3
British aerospace3103 sheet, by temperBS L59, BS L60, BS L61
British (legacy general)N3 / NS3BS 1470 (withdrawn, replaced by EN 485)
German Werkstoff3.0515 (AlMn1)DIN EN 485
ISOAlMn1ISO 209, ISO 6361
North American near-equivalent3003ASTM B209 (not identical; confirm before substituting)
Supply range

Sizes and weights

3103 / 3103A supply range

Thickness
0.5 – 6 mm sheet; thicker plate in H112 or O on request
Sheet sizes
1000 × 2000, 1250 × 2500, 1500 × 3000 mm; cut blanks to drawing
Coil and strip
Slit strip for fins, tube stock and formed parts
Tempers
O, H12, H14, H16, H18, H22, H24, H26
Surface
Mill finish; PVC film, paper interleaving or pre-painted on request

H14 is the most commonly stocked temper; others are ordered to requirement.

At 2.73 g/cm³, 3103 sheet weighs 2.73 kg/m² per millimetre of thickness.

Thickness (mm)kg/m²1000 × 2000 mm sheet (kg)1250 × 2500 mm sheet (kg)
0.51.362.74.3
0.82.184.46.8
12.735.58.5
1.23.286.610.2
1.54.098.212.8
25.4610.917.1
2.56.8313.721.3
38.1916.425.6
410.9221.834.1
513.6527.342.7
616.3832.851.2
821.8443.768.2
1027.3054.685.3
1232.7665.5102.4
1643.6887.4136.5
Working with 3103

Forming, joining and finishing

Forming

Excellent in O and H2x. Anneal at roughly 350 – 410 °C to restore ductility between deep-draw stages.

Welding

TIG and MIG with 4043A or 1050A filler. The HAZ returns to annealed strength, so design H14 welded parts to O values near the weld.

Brazing

Very good; 3103 and 3003 are the usual cores for clad brazing sheet in radiators and heat exchangers.

Machining

Soft and gummy in O; H14 and harder tempers machine more cleanly with sharp, polished tools.

Finishing

Accepts conversion coating, primer and paint; anodising gives a slightly grey film.

Corrosion

Very good in atmosphere and fresh water; no stress-corrosion or exfoliation problems.

Applications

Where 3103 sheet is used in aerospace

  • Fairings and closures: formed covers, trailing-edge closures and access-panel skins that carry no primary load
  • Ducting: air-conditioning, ventilation and avionics-cooling ducts and transitions
  • Tanks and containers: water and fluid reservoirs, drip trays and covers
  • Heat exchangers: fins, tube stock and headers in oil and air coolers
  • Interior parts: galley and cabin panels, trims and closeouts
  • Ground equipment: panels, steps, guards and enclosures for tugs, carts and maintenance stands

Primary structure such as skins, frames and fittings uses heat-treatable alloys. Where a formed part needs more strength or better fatigue performance than 3103 offers, 5251 or 5052 is the usual next step.

Ordering

How to order 3103 sheet

  1. SpecifyAlloy and temper, thickness, sheet size or blank drawing, quantity and the governing specification with its revision (EN 485 with EN 573-3 chemistry, BS L59 / L60 / L61, or your OEM document).
  2. ConfirmWe confirm the specification can be met, the tolerance class, test requirements and delivery terms (EXW, FOB, CIF or DAP).
  3. InspectMaterial is checked for dimensions and surface condition; any extra tests named on the order are carried out or arranged.
  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 cases or on pallets, shipped by sea or air to your port or door.
Sources

References and standards

  1. EN 573-3 – Aluminium and aluminium alloys: chemical composition and form of wrought products
  2. EN 485-2 – Aluminium and aluminium alloys: sheet, strip and plate, mechanical properties
  3. EN 485-4 – Aluminium and aluminium alloys: sheet, strip and plate, tolerances on shape and dimensions for cold-rolled products
  4. BS L59, L60, L61 – Aerospace series: aluminium alloy 3103 sheet (British Standards Institution)
  5. ASM Handbook, Vol. 2 – Properties and Selection: Nonferrous Alloys and Special-Purpose Materials
FAQ

3103 aircraft aluminium (aluminum) sheet: buyer questions

Is 3103 the same as 3003?

Not exactly, but very close. 3103 allows up to 0.30 % magnesium and has no minimum copper; 3003 requires 0.05 – 0.20 % copper. Strength and formability are almost identical, so they are alternatives for most non-critical parts once the design authority agrees.

What is the difference between 3103 and 3103A?

3103A is a separately registered variant in EN 573-3 with slightly different composition limits. Order the one your drawing names; the certificate will state which it is.

Can 3103 sheet be heat-treated to T4 or T6?

No. It is non-heat-treatable. Strength comes only from cold work (H tempers), and annealing gives the O temper.

Which temper is best for deep drawing?

O temper. If the part needs more stiffness after forming but must still bend well, H22 or H24 is a good compromise.

What does the BS L-series cover?

BS L59, L60 and L61 are British aerospace sheet documents for 3103 in different temper conditions. Check the issue named on your drawing for the exact temper and test requirements.

Do you ship 3103 sheet worldwide?

Yes. Metline supplies 3103 and 3103A sheet from Mumbai to customers worldwide, with EN 10204 3.1 certificates and export packing.

Need 3103 sheet for an aircraft or ground-equipment part?

Send the temper, thickness, size, quantity and specification. We will confirm availability and certification.