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Aerospace sheet & plate · 2xxx series

2014 / 2014A Aerospace Aluminium Sheet & Plate

2014 sheet and plate gives the highest strength of the common 2xxx rolled products: about 480 MPa tensile and 410 MPa yield in T6 and T651. It is used for machined fittings, frames and heavy-duty structure where strength and machinability matter more than corrosion resistance. Metline supplies bare and Alclad 2014 and 2014A sheet and plate, certified to AMS, ASTM and EN standards, to customers worldwide.

Stack of 2014-T651 aerospace aluminium plates with protective film
Alloy
2014 / 2014A
Tempers
O, T4, T6, T651
Thickness
Sheet 0.5 – 6 mm; plate to about 150 mm
Standards
AMS 4029 · ASTM B209 · EN 485
Overview

What is 2014 aerospace sheet and plate?

2014 is an aluminium-copper-silicon-magnesium alloy (AlCu4SiMg). In sheet and plate form it is chosen when a part needs higher yield strength than 2024 can give, and when the part will be machined or formed and then protected by cladding, anodising or paint.

Two families of product are supplied. Bare 2014 plate in T651 is the machining grade: it is stretched after quenching so it stays flat as material is removed, and it is cut into fittings, frames, ribs and test hardware. Alclad 2014 sheet carries a thin layer of 6003 aluminium alloy on each face; the cladding is anodic to the core and corrodes sacrificially, protecting the 2014 underneath. Alclad sheet is used for formed skins and panels where the surface stays exposed.

2014A is the European version of the alloy, with tighter silicon and iron limits. It is called up in European aerospace standards and British "L" specifications, while US programmes use 2014 to SAE AMS and ASTM documents. For most designs the two are interchangeable only with the approval of the design authority, so always order the designation shown on your drawing.

Chemical composition

2014 and 2014A composition (wt %)

The table gives registered limits. Alclad 2014 has a 2014 core with 6003 cladding on both sides; the certificate reports the core chemistry.

Element2014 (AA / ASTM)2014A (EN AW-2014A)Role
Copper (Cu)3.9 – 5.03.9 – 5.0Main strengthening element (Al2Cu precipitates)
Silicon (Si)0.50 – 1.20.50 – 0.9Speeds the ageing response; the "Si" in AlCu4SiMg
Manganese (Mn)0.40 – 1.20.40 – 1.2Grain control and toughness
Magnesium (Mg)0.20 – 0.80.20 – 0.8Adds to precipitation hardening
Iron (Fe)0.7 max0.50 maxImpurity; lower Fe improves toughness
Chromium (Cr)0.10 max0.10 maxImpurity
Nickel (Ni)—0.10 maxImpurity
Zinc (Zn)0.25 max0.25 maxImpurity
Titanium (Ti)0.15 max0.15 max (Ti + Zr 0.20)Grain refiner
Others, each / total0.05 / 0.150.05 / 0.15
Aluminium (Al)RemainderRemainder
Mechanical & physical properties

Mechanical properties by temper

Typical values describe what the material normally achieves. Specified minimums are what the standard guarantees; they fall slightly as plate thickness rises and are lower for Alclad sheet, because the soft cladding carries little load.

TemperTensile strengthYield strength (0.2 %)ElongationBrinell hardness
O (annealed)186 MPa / 27 ksi97 MPa / 14 ksi18 %45 HB
T4, T451427 MPa / 62 ksi290 MPa / 42 ksi20 %105 HB
T6, T651, T6511483 MPa / 70 ksi414 MPa / 60 ksi13 %135 HB
Product (ASTM B209, approximate minimums)Tensile strengthYield strengthElongation
2014-T4 bare sheet~400 MPa / 58 ksi~250 MPa / 36 ksi14 %
2014-T6 bare sheet, 1 – 6 mm~455 MPa / 66 ksi~400 MPa / 58 ksi6 – 7 %
Alclad 2014-T6 sheet, 1 – 6 mm~440 MPa / 64 ksi~395 MPa / 57 ksi7 – 8 %
2014-T651 plate, 6 – 50 mm~450 – 460 MPa~405 MPa4 – 7 %

Minimums vary by thickness band; the governing values are those in the order specification and on the mill certificate.

Physical properties of 2014 (T6 unless noted)

Density
2.80 g/cm³ (0.101 lb/in³)
Modulus of elasticity
about 73 GPa (10.6 Msi)
Melting range
about 507 – 638 °C
Thermal conductivity
about 154 W/m·K (T6); about 190 W/m·K (O)
Electrical conductivity
about 40 % IACS (T6); about 50 % IACS (O)
Coefficient of thermal expansion
about 23 µm/m·°C (20 – 100 °C)
Tempers

Which 2014 temper fits your part?

O (annealed)

Softest condition for stretch forming, deep drawing and tight bends. The formed part is then solution treated and aged to T4 or T6.

T4 / T451

Solution treated and naturally aged. Good formability with useful strength; T451 plate is stretched to relieve stress. Often formed in T4 and aged to T6 (T62) afterwards.

T6

Solution treated and artificially aged for full strength. The usual temper for sheet in finished structure.

T651

Solution treated, stretched 1.5 – 3 % and aged. The standard plate temper for machined parts, because residual stresses are low.

T62

Aged to T6 by the user after heat treatment from O or F. Specify T62 properties when you heat-treat parts yourself.

Alclad tempers

Alclad 2014 is supplied in O, T3, T4 and T6; the core is heat-treated in the same way as bare material.

Standards & equivalents

2014 plate specifications and equivalents

Sheet and plate specifications

ASTM B209 / ASME SB-209
Bare and Alclad 2014 sheet and plate, all tempers
AMS 4029
2014-T651 plate (and T6 sheet) for aerospace
AMS-QQ-A-250/3
Alclad 2014 sheet and plate (former federal QQ-A-250/3)
EN 485-1/-2/-4, EN 573-3
EN AW-2014 and EN AW-2014A sheet, strip and plate
EN aerospace series and BS "L" specifications
Specific 2014A tempers, bare and clad, for European programmes
SystemDesignationNote
Aluminum Association / UNS2014 / A92014Basis of ASTM and AMS specifications
European (EN)EN AW-2014 (AlCu4SiMg); EN AW-2014A (AlCu4SiMg(A))2014A has tighter Si and Fe limits
German Werkstoff3.1255AlCuSiMn in older DIN usage
ISOAlCu4SiMgISO 209
Japan (JIS)A2014JIS H4000 / H4040 / H4140
France (old NF)AU4SGStill seen on older drawings
China (GB)2A14 (close equivalent)Similar chemistry; check limits before substituting
Supply range

Sizes, weights and supply range

Supply range

Thickness
Sheet 0.5 – 6 mm; plate 6 – about 150 mm (heavier sections on enquiry)
Width
1000, 1220, 1250, 1500 mm; wider plate on request
Length
2000 – 4000 mm standard; long lengths and cut blanks to order
Surface
Mill finish, PVC-film protected; Alclad sheet with clad faces
Processing
Saw cutting and waterjet profiling to drawing

2014 weighs 2.80 kg per square metre per millimetre of thickness, about 4 % more than 6061. The plate weight calculator handles any size.

Thickness (mm)kg per m²1220 × 2440 mm (kg)1500 × 3000 mm (kg)
0.82.246.710.1
12.808.312.6
1.64.4813.320.2
25.6016.725.2
38.4025.037.8
411.2033.350.4
616.8050.075.6
1028.0083.4126.0
1233.60100.0151.2
1644.80133.4201.6
2056.00166.7252.0
2570.00208.4315.0
3084.00250.1378.0
40112.00333.4504.0
50140.00416.8630.0
60168.00500.1756.0
80224.00666.81008.0
100280.00833.51260.0
Tolerances & inspection

Tolerances, testing and documentation

Dimensional tolerances follow ANSI H35.2 for ASTM and AMS orders and EN 485-3/-4 for EN orders. Aerospace plate is commonly ultrasonically inspected to AMS-STD-2154 or ASTM B594, with the class stated on the order. Each lot is tested for tensile properties in the directions the specification requires, and electrical conductivity and hardness are used to confirm correct heat treatment.

  • EN 10204 3.1 certificate with chemistry, tensile results and lot traceability
  • Ultrasonic inspection report where specified
  • Flatness and dimensional checks; cut pieces inspected to drawing tolerance
  • Cladding thickness confirmation for Alclad sheet on request
Working with 2014

Machining, forming and protection

Machining

T651 machines cleanly with short chips. Remove material evenly from both faces of thick plate and keep coolant flowing to control heat.

Forming

Form in O or freshly quenched (W) condition, then age. T6 sheet tolerates only generous bend radii, typically 3 – 6 × thickness depending on gauge.

Joining

Riveting, bolting and adhesive bonding are standard. Fusion welding is avoided because of hot cracking and strength loss.

Corrosion protection

Anodise or conversion-coat and prime all bare surfaces after machining. Alclad sheet protects itself unless the cladding is machined away.

Heat exposure

Do not hold 2014 above about 150 °C for long periods; over-ageing reduces strength.

Inspection after forming

Check formed parts for orange peel and cracking at bends, and confirm properties after re-heat treatment.

Applications

Applications of 2014 sheet and plate

  • Airframe fittings and frames machined from T651 plate
  • Lower-wing and fuselage skins on older and light aircraft, usually Alclad
  • Ribs, brackets and stiffeners formed from O or T4 sheet and aged
  • Missile and space structure where high static strength is needed
  • Truck frames and heavy-duty structures needing high strength in bolted designs
  • Tooling and test rigs that require an aerospace-grade, high-strength plate
Comparison

2014 plate compared with 2024 and 7075

Property2014-T6512024-T3517075-T651
Typical tensile strength~483 MPa~469 MPa~572 MPa
Typical yield strength~414 MPa~324 MPa~503 MPa
Fatigue crack growth resistanceFairVery goodFair
Fracture toughnessModerateGoodModerate
Corrosion resistance (bare)LowLowLow–moderate
Typical useFittings, framesTension skins, damage-tolerant partsHighly stressed machined parts

Choose 2024-T351 for tension-loaded, fatigue-critical structure and 7075-T651 or 7050-T7451 for the highest strength. 2014-T651 sits between them, giving high yield strength with excellent machinability.

Ordering

How to order 2014 sheet and plate

  1. SpecifyAlloy (2014 or 2014A), bare or Alclad, temper, thickness, width, length or cut size, and quantity.
  2. Name the standardASTM B209, AMS 4029, AMS-QQ-A-250/3, EN 485 or your customer specification, plus any ultrasonic class.
  3. QuoteWe confirm availability, tolerance, test scope, certification and delivery terms (EXW, FOB, CIF or DAP) for your port or site.
  4. Process and inspectPlates are cut, film-protected where needed and checked for dimensions, flatness and surface.
  5. Document and shipEach lot ships with an EN 10204 3.1 mill test certificate traceable to the heat and lot, plus a packing list. Material is packed in seaworthy wooden cases with moisture protection; third-party inspection can be arranged on request.
Sources

References and standards

  1. ASTM B209 – Standard Specification for Aluminum and Aluminum-Alloy Sheet and Plate
  2. SAE AMS 4029 – Aluminum Alloy Sheet and Plate, 2014-T651
  3. EN 485-2 – Aluminium and aluminium alloys: sheet, strip and plate, mechanical properties
  4. The Aluminum Association – International Alloy Designations and Chemical Composition Limits
  5. ASM Handbook, Vol. 2 – Properties and Selection: Nonferrous Alloys (2014)
FAQ

2014 aerospace aluminium (aluminum) plate: FAQ

What is Alclad 2014?

Alclad 2014 is 2014 sheet or plate with a thin metallurgically bonded layer of 6003 alloy on each face. The cladding corrodes in preference to the core, protecting it. It slightly lowers strength, so Alclad minimums are a little below bare values.

Is 2014-T651 stronger than 2024-T351?

Yes in yield strength: about 414 MPa against about 324 MPa typical. 2024-T351 has better fatigue crack-growth resistance and toughness, so it is preferred for tension skins and damage-tolerant parts.

Can I form 2014-T6 sheet?

Only with generous bend radii. For tight forming, use O or T4 temper, or form immediately after quenching, and then age the part to T6 (reported as T62).

What is the difference between 2014 and 2014A plate?

2014A has tighter limits on silicon and iron and is the designation used in European standards. Mechanical properties are similar, but substitution needs approval from the design authority.

Does 2014 plate need corrosion protection?

Yes. Bare 2014 has low corrosion resistance. Anodise or conversion-coat and paint after machining, or use Alclad sheet for exposed formed parts.

What certification comes with 2014 plate?

An EN 10204 3.1 mill test certificate with chemistry and mechanical results for the lot, plus ultrasonic and dimensional reports when the order specifies them.

Need 2014 or 2014A plate?

Tell us the temper, thickness, size, specification and quantity. We will reply with availability, certification and a delivered price.