Aluminium 2017 Sheet Plate | AMS 4037 | UNS A92017 | DIN 3.1325

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PM Industries manufactures, supplies, and stocks AMS 4037 Aluminium 2017 Sheet Plate (UNS A92017) in a range of thicknesses and sizes. AMS 4037 covers Aluminium 2017 in sheet form to aerospace specification requirements. Aluminium 2017 belongs to the 2xxx series, with copper as the primary alloying element. It's a heat-treatable alloy that develops substantially higher strength than general-purpose grades like 1100 or 3003 after solution heat treatment and natural aging to the T4 temper.

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2017 is one of the older high-strength aluminium alloys and predates 2024 in the development of the 2xxx series. In many high-strength structural applications it has been succeeded by 2024, which provides higher strength and better fatigue resistance. However, 2017 retains a specific advantage over 2024 in machinability. The copper content and microstructure of 2017 produce chips that break more cleanly during high-speed machining, and the alloy holds tighter dimensional tolerances in precision turning and milling operations than 2024 in many production situations. For applications where machinability is the primary processing requirement and where 2024's incremental strength advantage isn't needed, 2017 remains the preferred specification.

Key characteristics:

• AMS 4037 covers Aluminium 2017 sheet to aerospace specification requirements
• 2xxx series copper-aluminium alloy, heat-treatable to develop high strength through natural aging
• Good tensile and yield strength in the T4 temper, higher than general-purpose aluminium grades
• Very good machinability, producing clean chips and holding tight tolerances in precision machining
• Good fatigue resistance under cyclic loading
• Lower corrosion resistance than 5xxx and 6xxx series alloys; cladding or protective treatment typically required for outdoor service
• Good rivet-driving characteristics in the naturally aged T4 condition, supporting its historical use in aircraft riveting
• Not typically welded by fusion welding; mechanical joining is the standard fastening method
• Available in T4 temper (solution heat-treated and naturally aged) as standard
• Also covered by ASTM B209 and equivalent international aluminium standards

Machinability in precision production is the current primary application driver for 2017. The alloy machines at high speeds with good surface finish and produces broken chips that clear easily from cutting zones, which keeps cutting forces and tool temperature lower than with alloys that produce long, stringy chips. In screw machine production, CNC turning, and high-volume precision part manufacturing, those machining characteristics translate to higher output rates, longer tool life, and better dimensional consistency between parts across a production run.

Rivet applications in aerospace were 2017's primary historical use, and it continues to be specified for rivets in certain aircraft applications where natural aging to T4 provides the required combination of strength and driven-head formation characteristics. Rivets in 2017 are driven in the soft condition shortly after quenching and naturally age to full strength in service, a process that has been standard in aerospace assembly for decades.

Corrosion resistance is the alloy's primary limitation. Like other 2xxx series alloys, 2017 is less corrosion-resistant than the 5xxx and 6xxx series due to copper-rich second phases at grain boundaries that create galvanic corrosion sites. For outdoor service, painting, anodizing, or cladding with a purer aluminium layer is standard practice. In controlled indoor and dry environments, 2017 performs without protective treatment for typical production and engineering applications.

Industries and typical applications:

• Aerospace: aircraft structural components, precision machined airframe fittings, and rivet stock for structural assembly
• Precision machining: high-volume turned and milled components, screw machine parts, hydraulic fittings, and precision hardware requiring good dimensional accuracy
• Automotive: precision machined components and lightweight structural parts where 2017's machinability supports efficient production
• General engineering: brackets, machine components, and structural parts requiring higher strength than general-purpose aluminium at manageable fabrication cost
• Defense: precision machined components and structural aerospace hardware in military aircraft and systems

Sheet and plate are available in T4 temper across a range of thicknesses and sizes with full material certification to AMS 4037 and applicable specifications including ASTM B209. Contact PM Industries for thickness, width, length, and pricing.

Specification Aluminium 2017 Sheet & Plate | AMS 4037 | UNS A92017 | DIN 3.1325

Specifications	ASME SA 240/ASTM A 240
Standard Sizes	1000 x 2000 mm, 1220 x 2440 mm, 1500 x 3000 mm, 2000 x 2000 mm, 2000 x 4000 mm
Width	10-2500mm
Length	2000mm, 2440mm, 3000mm, 5800mm, 6000mm, etc
Surface	2B, 2D, BA, NO.1, NO.4, NO.8, 8K, mirror, checkered, embossed, hairline, sand, blast, Brush, etching, etc
Thickness	0.1mm to 100 mm Thk
Hardness	Quarter Hard, Half Hard,Spring Hard, Soft, Hard
Stock available in form of	Shim Sheet, Rolls, Strip, Flats, Clad Plate, Plain Sheet, Plate, Sheet, Coils, Foils, Rolling Sheet, Rolling Plate, Flat Shim, Flat Sheet, Blank (Circle), soft annealed, sheared, annealed, tread plate,descaled, Checker Plate
Profiling	Plasma Plate Cutting
Value added services	Plasma cutting, Waterjet cutting, Laser cutting, welding, edge preparation, etc.
Test Certificates	EN 10204/3.1B, NACE MR0103, NACE MR0175
	Raw Materials Certificate
	100% Radiography Test Report
	Third Party Inspection Report, etc

Available Types of Aluminium 2017 Sheet & Plate

Aluminum 2017 Sheets & Plates – Equivalent Grades

European Standard	OLD	WNr	UNS	ISO	USA (AA)	GERMANY (DIN)
AW-AlCu4MgSi	AU4G	3.1325	A92017	AlCu4MgSi	2017	AlCuMg1

Aluminum 2017 Sheet & Plate – Chemical Composition

Grade	Al	Si	Fe	Cu	Mn	Mg	Cr	Zn	Ti	Others Each	Other Total
2017	Rem	0.20-0.8	0.7 max	3.5-4.5	0.40-1.0	0.40-0.8	0.10 max	0.25 max	0.15 max	0.05 max	0.15 max

Aluminum 2017 Sheets & Plates – Mechanical Properties

Material	Condition	Tensile Strength (N/mm²) min		Yield Strength		Elongation in 4D %
		ksi	Mpa	ksi	Mpa
2017	2017-T4 Bar	55	379	32	221	12