AVRO TOOLS manufactures countersinking and pneumatic tools including high performance pneumatic rivet hammers, drills, precision microstops and tungsten bucking bars.

The British Standards Institution (BSI) administers British Standards as the UK's National Standards body. British Standards L (BS-L) relate to different grades of aluminium alloys and light alloy materials such as magnesium and apply to different product forms (shapes) such as sheets/plates, bars and tubes.

Sourced from different manufacturers they are offered as their OEM parts or as parts of our own labelled (AVIATIONEU NEW ERA) product lines. They can be supplied in different Metric pre-cut ot cut-to-order (CTO) dimensions and heat treatments (tempers) and they are sold in pieces or bulk (tons). A brief overview of offered BS-L metal products commonly used in Aerospace with reference to the commercial (trade) name of the respective aluminum alloy, and their correlation to their US Standards' counterparts is included below (see table). Depending on application requirements,  certain US Standard metals can be used as alternatives to their BS-L counterparts.

2014/2014A(*)

Applicable forms: plates, sheets and strips, bars, tubes as per respective BS-L Standards.

The 2014 aluminum alloy is high-strength aerospace alluminum alloy alloyed with copper (3.90-5.00%). Often includes cladding with 1050A aluminium and heat treated to T3  or T4 conditions, as in the case of sheets, to meet respective BS L163, and BS L164 Standard specifications.  Clad sheets are typically used in aerospace and defense components, structural and high technology applications. Use of copper enables them to retain their high strength after their heat treatment while cladding, as part of the mill production process, enhances their corrosion resistance capabilities. 

2024/2024A(*)

Applicable forms: sheets.

The 2024 aluminum alloy (with copper as the primary alloying element) is also known as aerospace grade aluminum. It is commonly used in aircraft structural applications due to its high strength and fatigue resistance and those requiring high stress & strain resistance in aviation and industrial applications. This alloy is stronger but less versatile than 6061, which is more corrosion resistant, easier to weld, and more suited to machining, but less strong than the 7075.  2024A 1050A Alclad sheets relate to BS-L Standards BS L109 and BS L110.

7075

Applicable forms: plates, sheets and strips, bars.

7075 aluminium alloy is an aluminium alloy with zinc as the primary alloying element.  It is one of the most commonly used aluminium alloys for highly stressed structural applications such as aircraft structural parts. Respective BS-L Standards for different forms of 7075 aluminum include BS 2 L95 for T651 plates, BS 2 L88 for T6 clad sheets and strips, BS L160, BS L161, and BS L70 for bars.

For additional information, please refer to the supplied documentation or contact us for a quotation.

(*) The letter "A" in the alloy classification system indicates a modified version of the respective standard alloy with generally no distinction in material properties or performance betwwen the two.

AIRPRO INDUSTRY CORP. manufactures professional quality air tools, hand  & auto repair tools and accessories for professional applications under  the brand name AIRPROWU. AIRPROWU extensive product line ranges from aircraft tools to industrial, automotive/motorcycle ,tooling/molding, construction and auto body shop solutions and solutions for electronic assembly lines. AIRPROWU product line of Hydraulic Riveters include pneumatic, industrial hydraulic, air hydraulic riveter tools and others. Please refer to the specifications of individual riveters.

Cladding coils, strips & sheets produced by AUERHAMMER METALLWERK from clad materials with different properties including carbon steels, stainless steels, nickel and copper and FeNi alloys. Cladding process enables combination of a minimum of two different grades of metal (one base material and a layer material) to be joined and form a laminated rolled material with new desired properties, capabilities and functions. A wide range of metals can be combined using cold-rolled cladding process and resulting cladding products  can be furthered tailored to customer requirements by subsequent further cold-rolling and annealing production processes. Deliveries are possible in soft, deep drawing or cold-rolled quality depending on the intended use. Common material properties used for cladding and tested include yield strength,tensile strength, elongation, hardness, formability and grain size or other like electrical resistance. Please refer to the attached documentation for additional information.

The AL2024 aluminum alloy (with copper as the primary alloying element) also known as aerospace grade aluminum, is commonly used in aircraft structural applications due to its high strength and fatigue resistance.  It is suitable for applications requiring high stress and strain resistance. The AL2024 aluminum alloy is stronger but less versatile than AL6061 alloy, which is more corrosion resistant, easier to weld, and more suited to machining, but less strong than the AL7075 alloy.

AL2024 aluminum alloy sheets come as Annealed (O Temper) without heat treatment or as heat treated to attain their maximum strength. Heat treated sheets are available in vatious T tempers (such as T3,T4,T5,T6 and T651) for use in a range of aviation and industrial applications.

2024-O CLAD (ALCLAD) Aluminum alloy sheets(*) are offered as part of AVIATIONEU NEW ERA product lines and they consist an excellent choice when high corrosion resistance is needed. Sourced from quality producers, these sheets  are readily formed in the annealed condition and may be subsequently heat treated. They feature good machinability and can be machined to a high finish. They are offered in different thicknesses and specific widths and lengths in inches. They comply with AMS and ASTM specifications.

For additional information, please refer to our attached Brief Guide on Aluminum Grades & Temper Designations, the individual product presentations or contact us for quotation.

(*) ALCLAD is a corrosion-resistant aluminium sheet formed from high-purity aluminium surface layers metallurgically bonded (rolled onto) to high-strength aluminium alloy core material. As an enhanced sheet for fuselage applications, ALCLAD offers improved fracture toughness and fatigue crack growth while maintaining the strength characteristics of the alloy. ALCLAD also offers improved fracture toughness and fatigue crack growth while maintaining the strength characteristics of the alloy.

The 2024 aluminum alloy (with copper as the primary alloying element) is often referred to as aerospace grade aluminum due to its common use in aircraft structural applications requiring high strength and fatigue resistance. This alloy is stronger but less versatile than 6061, which is more corrosion resistant, easier to weld, and more suited to machining, but less strong than the 7075, also used in the aerospace industry.

2024 aluminum alloy sheets are offered as part of AVIATIONEU NEW ERA product lines. They come as Annealed (O Temper) without heat treatment or heat treated in various tempers (such as T3,T4,T5,T6 or T651) to attain their maximum strength (*). They can be supplied in different finishes (Untreated (Bare), Anodized or CLAD (referred to as ALCLAD). Anodization makes aluminum stronger, longer-lasting, and more durable in a wider variety of environments and applications. The surface becomes three times as hard as untreated aluminum, with increased resistance to abrasion, corrosion, and physical impact damage. CLAD sheets/plates are formed from high-purity aluminum surface layers metallurgically bonded to the aluminum alloy core material providing improved protection against fracture, fatigue crack growth & corrosion resistance.

Sourced from quality producers, AVIATIONEU NEW ERA 2024 aluminum sheets/plates can be supplied in pieces (see separate presentations) or in bulk in US or Metric Tons, consisting a cost effective solution when large quantities are demanded. Depending on the selected product & manufacturer they comply with different standards.

They are available in an extensive range of stocked thicknesses & standard or cut-to-order widths and lengths in inch or metric systems. If not in stock, approximate lead time for shipping is usually 1-2 months from the time of order placement, depending on the ordered quantity. Offered prices depend on selected products and quantities.  Prices and availability are subject to confirmation with our co-operating suppliers before order placement. Minimum Order Quantities (MOQ) depend on the required product.

Transport to customer destination can be arranged at additional cost. Small quantities are usually shipped by air transport while for bulk quantities sea/sea-surface transport is used.

All AVIATIONEU NEW ERA  metals are supplied free from oil stains, dents, inclusions, scratches, oxide discolorations, corrosion, or other defects, with PVC film cover, one/two side(s), depending on the producer & properly packaged for protection during the shipment.

For additional information, please contact us.

Notes: 

(*) All aluminum alloys, regardless of product form, are classified as either heat-treatable or non heat-treatable, depending upon the method used to attain their maximum strength. The modification methods applied to heat- and non heat-treatable alloys are listed in our attached Brief Guide on Aluminum Grades & Temper Designations.

Bars/rods from 2000 series aluminum alloys are offered in different shapes (cross sections) such as round, rectangular, hexagonal or square, as part of our own labelled (AVIATIONEU NEW ERA) product lines. They can be supplied in different Aluminum grades (e.g. 2014, 2024), with or without heat treatment (O) (see temper designators). Depending on the selected product and quality, 2000 series aluminum bars/rods comply with various aerospace or industrial standards / specifications (ASTM B209, AMS 4037, AMS-QQ-A-250/4, JIS, DIN) and others. They are intended for use in different industries, from packaging production, and mold making to aerospace, automotive, motorsports, shipbuilding, defense equipment,  and other applications.

Those from 2007 aluminum grade, made from a blend of high copper content, magnesium, and lead, are used mostly for machine parts, bolts and nuts, and threaded components.Those from 2014 grade (the second most popular alloy in its series, just after 2024) are known for their strength, toughness and machinability. Used in the manufacturing of machine and aerospace parts, and in buildings. The 2017 grade bars/rods are strong, easy to bend, and simple to shape, they can resist rust, and feature good ductility and machinability. Used for aircraft and construction parts. Their 2019 grade counterparts feature a high copper content, making them less resistant to corrosion compared to 5000 and 7000 series alloys while exhibiting high strength and good heat resistance. Used in applications in the aerospace industry and in buildings.  The 2024 alloy aluminium bars/rods, with copper as the primary alloying element, are used in applications requiring high strength to weight ratio, good fatigue resistance, weldablility and average machinability. Typical applications include structural and other components for the Aerospace, Defense, Automotive, Sports, Marine & other industries such as wing skins, body panels, wheel axles, bicycle frames, hulls & masts, railing, & fasteners.

AVIATIONEU NEW ERA bars/rods are offered in Aerospace quality with premium materials, rigorous processes, & extensive testing under strict quality management systems, and Commercial quality (separately listed), emphasizing on cost-effectiveness. Offered in different dimensions (sizes) & standard pre cut or cut to order lengths in inch/feet or mm (metric) systems. Sold in pieces or bulk quantities in US or Metric tons, with Minimum Order Quantity (MOQ) 1 ton. Air, sea or road transport options offered. If size(s) of ordered metals are not in stock, the approximate lead time is usually 1-2 months from ordering depending on the ordered quantity.

All AVIATIONEU NEW ERA metals are supplied free from oil stains, dents, inclusions, scratches, oxide discolorations, corrosion, or other defects and carefully packaged for protection during their transportation.

For additional information, please refer to our supplied documentation or contact us for a quotation.

AL5052 is an aluminium alloy, with magnesium and chromium as the primary alloying elements. It is  frequently used for general sheet metal work, heat exchangers, flooring panels, rivets and wires, chemical drums and other equipment, pressure vessels, treadplate, containers, and applications.  Alloy 5052 has a good marine atmosphere corrosion resistance of saltwater and excellent workability. Main features of this alloy include: non heat-treatable, excellent weldability, high corrosion resistance, smooth surface, lightweight, high-tensile strength.

Extruded bars/rods from 5052 aluminum alloy are offered as part of our own branded (AVIATIONEU NEW ERA) product lines. They come in different cross sections such as round, rectangular or square. Competitively priced, they are sourced from quality producers.

AVIATIONEU NEW ERA Aluminum 5052 H32 Temper round bars/rods are non-heat treatable, weldable, highly resistant to corrosion, used for marine, chemical and petrochemical applications. They are hardened by cold work and have good forming characteristics and corrosion resistance, including resistance to salt water. Although easily welded, they are not recommended for brazing and soldering applications. Main features of these bars/rods include their corrosion resistance, particularly in marine applications, adaptability to most mechanical and finishing processes although the heavier anodic films may take on a yellowish cast as well as fair machining with the proper set-up. They are offered in different thicknesses, widths and pre cut lengths in inches.

For additional information, please refer to our attached Brief Guide on Aluminum Grades & Temper Designations or contact us for quotation.

Note: AVIATIONEU NEW ERA metals are supplied free from oil stains, dents, inclusions, scratches, oxide discolorations, corrosion, or other defects. In certain cases, metals are additionally protected with PVC film.

Steel alloy 4130 (ST4130), also known as Chrome Moly after the 2 key elements of its composition, chromium, and molybdenum, is a general-purpose alloy steel widely used by the aviation and motorsports industries due to its weldability, fabrication, and mild hardenability in all offered forms (tubes, bars, sheets and plates). They are available in two different material states (Normalized and Annealed) depending on the process of how the material is heated and cooled.

The Normalized condition (sometimes referred to as "Condition N") is the harder and stronger condition and is best used when forming is not needed. Normalizing relieves internal stress on steel and improves toughness in steels that may harden after the cold working process.

The Annealed condition (sometimes referred to as "Condition A") is the softer and formable condition and is best used when forming is needed. Annealing relieves internal stresses, softens and makes the material more ductile.

4130 steel bars/rods are offered as part of our own branded (AVIATIONEU NEW ERA) product lines, featuring good strength and weldability without compromising steel abrasion or impact resistance. They do not require further heat treatment and are commonly used in structural applications, including gears, fasteners, and some aircraft exterior. Offered in Normalized condition and Cold Finished as indicated by the letters "NRZ" and  "CF" respectively in the product reference code (SKU). These bars/rods comply with ASTM -A108, AMS -6348, AMS -6370 & AMS/MIL -S-6758 specifications. Available in different diameters and lengths in inches. Unless otherwise mentioned, there is additional cost if manufacturing test reports are required.

For additional information, please refer to the supplied documentation, the individual product presentations or contact us.

SAE AISI(*) 1018 (G10180**) (separately presented) & 1020 (G10200**) mild/low carbon steel grades are are iron alloys with basically identical composition. Please refer to the supplied documentation for the comparison of SAE AISI 1018/1020 steel properties and additional information provided at the Product Description section. Technical data of supplied materials should be used ONLY FOR REFERENCE, NOT FOR DESIGN, and any decisions on their use remain entirely at the buyer discretion.

SAE AISI 1020 steel, aka C1020 steel in cold worked condition, is one of the most commonly used plain carbon steels. It is a low hardness and tensile strength carbon steel alloy with Brinell hardness ranging between  119 - 235 and tensile strength between 410 - 790 MPa. It features high machinability, high strength, high ductility and good weldability by most welding processes supporting its use in all industrial sectors. Due to its low carbon content, it is resistant to induction hardening or flame hardening but carburization or carbon nitriding can be applied to achieve a hardness value of more than  Rc65.  Normally used in turned and polished or cold drawn conditions.

Sourced from quality producers, SAE AISI 1020 steel tubes are offered as part of our own branded (AVIATIONEU NEW ERA) product lines. They can be furnished Normalized, Annealed or in other conditions, in different specifications, different shapes (cross sections), round, square, rectangular, etc. and dimensions in inches or millimeters (depending on the supplier) to meet project requirements. In the case of Metric round tubes, they are cold drawn seamless tubes available in different outer diameters and wall thicknesses in mm and pre cut or cut to order lengths in meters or centimeters. Those in inch system  are offered as DOM (Drawn Over a Mandrel***), with outer diameters and wall thicknesses in inches and lenghts in inches or feet.  Although they are welded tubes, the weld line becomes nearly undetectable during the manufacturing process and they are often referred to as seamless. Appearing prices for pre cut tubes are per piece in indicated dimensions.

(*) American Iron & Steel Institute (AISI), Society of Automotive Engineers (SAE).

(**)  Unified Numbering System ( UNS) Number, a designation system for Metals & Alloys.

(***) A process applied to tubing after its initial construction, allowing more exact ID/OD dimensions, a smoother finish, and a better alignment of the crystal lattice structure. 

The 2024 aluminum alloy (with copper as the primary alloying element) is also known as aerospace grade aluminum. It is commonly used in aircraft structural applications due to its high strength and fatigue resistance and those requiring high stress & strain resistance in aviation and industrial applications. This alloy is stronger but less versatile than 6061, which is more corrosion resistant, easier to weld, and more suited to machining, but less strong than the 7075. 

2024 aluminum alloy sheets/plates are offered as Annealed (O Temper, without heat treatment ) or Heat Treated in different tempers to attain their maximum strength, including the current listed T3 or others (such as T4,T5,T6 and T651) separately listed.

2024 T3 Alloy Aluminum sheets/plates are offered as part of AVIATIONEU NEW ERA product lines for a wide range of uses including aerospace, clock parts, computer parts, hydraulic parts, bolts, valves, nuts, pistons and gears. Sourced from quality producers, they are offered in different thicknesses & standard stocked or cut-to-order widths and lengths in inches. They can be furnished in different finishes, Untreated (Bare), Anodized or CLAD (sometimes referred to as ALCLAD) for improved corrosion resistance. 

Anodization makes aluminum stronger, longer-lasting, and more durable in a wider variety of environments and applications. The surface becomes three times as hard as untreated aluminum, with increased resistance to abrasion, corrosion, and physical impact damage. CLAD sheets/plates are formed from high-purity aluminum surface layers metallurgically bonded to the aluminum alloy core material providing improved protection against fracture, fatigue crack growth & improved corrosion resistance.

Depending on the selected product & manufacturer they comply with US SAE AMS, ASTM specifications or other standards.

AVIATIONEU NEW ERA 2024 T3 Alloy Aluminum sheets/plates are sold in pieces or in bulk with US or Metric Ton (as specified) as the unit of sale. Transport to customer destination can be arranged at additional cost. Small quantities are usually shipped by air transport while for bulk quantities sea/sea-surface transport is used. Minimum Order Quantities (MOQ) depend on the required product. Approximate time for shipping is usually 1-2 months from the time of order placement and payment receipt, depending on the ordered quantity. Appearing prices are indicative per unit of sale.  Prices and availability are subject to confirmation with our co-operating suppliers before order confirmation.

Note: All AVIATIONEU NEW ERA metals are supplied free from oil stains, dents, inclusions, scratches, oxide discolorations, corrosion, or other defects, with PVC film cover, one/two side(s), depending on the producer & properly packaged for protection during the shipment.

For additional information, please refer to the Product Description section, our attached Brief Guide on Aluminum Grades & Temper Designations, or contact us.

Steel alloy 4130 (ST4130), also known as Chrome Moly after the 2 key elements of its composition, chromium, and molybdenum, is a general-purpose alloy steel widely used by the aviation and motorsports industries due to its weldability, fabrication, and mild hardenability in all offered forms (tubes, bars, sheets and plates). They are available in two different material states (Normalized and Annealed) depending on the process of how the material is heated and cooled.

The Normalized condition (sometimes referred to as "Condition N") is the harder and stronger condition and is best used when forming is not needed. Normalizing relieves internal stress on steel and improves toughness in steels that may harden after the cold working process. The Annealed condition (sometimes referred to as "Condition A") is the softer and formable condition and is best used when forming is needed. Annealing relieves internal stresses, softens and makes the material more ductile.

4130 alloy steel (Chrome Moly) seamless round tubes are offered as part of our own branded (AVIATIONEU NEW ERA) product lines in Normalized (N )  or Annealed (A) conditions indicated by the letters "NRZ" and  "ANL" respectively in the product reference code (SKU). They have been for years the standard of the aircraft industry. These tubes offer good strength and weldability without compromising steel abrasion or impact resistance and can also be made even stronger through heat treatment. They are commonly used in in structural applications, gears, fasteners, and aircraft exteriors. Tensile Strength: 90,000 PSI. Available in a range of outer diameters, wall thicknesses and pre-cut lengths in inches or cut to order (CTO) lengths of 12 inches (1 foot)) or multiples. Apperating price of CTO tubes is per foot (12 inches). Depending on the supplier, they comply with different standards/specifications, such as MIL-T6736 standard or ASTM/A S1906 specifications. Unless otherwise mentioned, there is additional cost if manufacturing test reports are required. For additional information, please refer to the supplied documentation or contact us.

Steel alloy 4130 (ST4130), also known as Chrome Moly after the 2 key alloying elements, chromium, and molybdenum, is a general-purpose alloy steel widely used by the aviation and motorsports industries due to its weldability, fabrication, and mild hardenability in all offered forms (tubes, bars, sheets and plates). 

4130 alloy steel sheets are offered as part of AVIATIONEU NEW ERA product lines for a wide range of uses including structural applications, including gears, fasteners, and and aircraft exteriors. These sheets offer good weldability without compromising steel abrasion and impact resistance and can be made even stronger throough heat treatment.AVIATIONEU NEW ERA 4130 alloy steel sheets undergo a heat treating process and they are available in two different material states, Normalized or Annealed,  depending on the process of how the material is heated and cooled. The letters "NRZ" and "ANL" specify respectively Normalized or Annealed state in our Reference Codes (SKUs) for ordering of materials.  4130 Annealed steel sheets are produced to the aerospace specification AMS-6350 (sometimes referred to as "Condition A") while Normalized ones meet aerospace specification AMS-6345 (also known as "Condition N"). Annealed steel sheets are "softer" than their normalized steel counterparts and offer higher workability. Normalized steel sheets offer a higher strength tolerance.

Sourced from quality producers, these sheets are offered in different thicknesses and specific widths and lengths in inches. For additional information, please refer to our supplied documentation, the individual product presentations or contact us for quotation.

SAE AISI(*) 1018 (G10180**) and 1020 (G10200**) mild/low carbon steel grades are very similar. Both SAE AISI 1018 steel and SAE AISI 1020 (see separate product presentation) carbon steels are iron alloys with their alloy composition being basically identical. Please refer to the supplied documentation for the comparison of SAE-AISI 1018/1020 steel properties. An overview of AISI/SAE 1018 Carbon Steel properties and fabrication processes is provided at the Product Description section. Technical data of supplied materials should be used ONLY FOR REFERENCE, NOT FOR DESIGN, and any decisions on their use remain entirely at the buyer discretion.

SAE AISI 1018 mild/low carbon steel has excellent weldability and produces a uniform and harder case and it is considered as the best steel for carburized parts. This alloy offers a good balance of toughness, strength and ductility. Provided with higher mechanical properties, AISI 1018 hot rolled steel also includes improved machining characteristics and Brinell hardness. Also used in bending, crimping and swaging processes, fixtures, mounting plates and spacers, applications that do not need high strength of alloy steels and high carbon or to improve drilling, machining, threading and punching processes and prevent cracking in severe bends.

Sourced from quality producers, SAE AISI 1018 and 1020  low carbon steel tubes  are offered as part of our own branded (AVIATIONEU NEW ERA) product lines in different forms (cross sections), round, square, rectangular, etc. and dimensions in inches or millimeters (depending on the supplier) to meet project requirements.  In the case of round tubes, they can be furnished Normalized, Annealed or other conditions, in different specifications in pre cut or cut to order lengths. For those in Metric system outer diameters and wall thicknesses are specified in mm and lengths in meters or centimeters. For those in inch system outer diameters and wall thicknesses are in inches and lenghts in inches or feet.  Appearing prices for pre cut tubes are per piece in indicated dimensions.

(*) American Iron & Steel Institute (AISI), Society of Automotive Engineers (SAE).

(**)  Unified Numbering System ( UNS) Number. UNS is an alloy designation system for Metals & Alloys providing a means of correlating many internationally used metal and alloy numbering systems administered by their producers, societies, trade associations, and individual users.

Steel alloy 4130 (ST4130), also known as Chrome Moly after the 2 key alloying elements, chromium, and molybdenum, is a general-purpose alloy steel widely used by the aviation and motorsports industries due to its weldability, fabrication, and mild hardenability in all offered forms (tubes, bars, sheets and plates). 

4130 alloy steel sheets are offered as part of AVIATIONEU NEW ERA product lines for a wide range of uses including structural applications, including gears, fasteners, and and aircraft exteriors. These sheets offer good weldability without compromising steel abrasion and impact resistance and can be made even stronger throough heat treatment.AVIATIONEU NEW ERA 4130 alloy steel sheets undergo a heat treating process and they are available in two different material states, Normalized or Annealed,  depending on the process of how the material is heated and cooled. The letters "NRZ" and "ANL" specify respectively Normalized or Annealed state in our Reference Codes (SKUs) for ordering of materials.  4130 Annealed steel sheets are produced to the aerospace specification AMS-6350 (sometimes referred to as "Condition A") while Normalized ones meet aerospace specification AMS-6345 (also known as "Condition N"). Annealed steel sheets are "softer" than their normalized steel counterparts and offer higher workability. Normalized steel sheets offer a higher strength tolerance.

Sourced from quality producers, these sheets are offered in different thicknesses and specific widths and lengths in inches. For additional information, please refer to our supplied documentation, the individual product presentations or contact us for quotation.

AL5052 is an aluminium alloy, with magnesium and chromium as the primary alloying elements. Although It is non heat-treatable, it is the highest strength alloy of other non-heat-treatable grades also featuring an excellent weldability using most common techniques, high resistance to marine atmoshpere and salt water corrosion, smooth surface, lightweight and high-tensile strength. This alloy is comparable to the 6061 aluminum alloy (AL6061). 

AL5052-O CLAD (ALCLAD) tubes(*) are offered as part of our own branded (AVIATIONEU NEW ERA) product lines along with those from other grade aluminum and steel alloys. Sourced from quality producers, they are offered as Annealed in different outer diameters and wall thicknesses in inches and  cut to order lengths up to 5 ft (60 in.). They can be used for low and medium pressure hydraulic systems, fuel lines and oil lines. Tubing is sold by foot. There is additional cost if manufacturing test reports are required.

For additional information, please refer to our attached Brief Guide on Aluminum Grades & Temper Designations, the supplied documentation or contact us for quotation.

(*) ALCLAD is a corrosion-resistant aluminium sheet formed from high-purity aluminium surface layers metallurgically bonded (rolled onto) to high-strength aluminium alloy core material. As an enhanced sheet for fuselage applications, ALCLAD offers improved fracture toughness and fatigue crack growth while maintaining the strength characteristics of the alloy. ALCLAD also offers improved fracture toughness and fatigue crack growth while maintaining the strength characteristics of the alloy.

Note: AVIATIONEU NEW ERA metals are supplied free from oil stains, dents, inclusions, scratches, oxide discolorations, corrosion, or other defects. In certain cases, metals are additionally protected with PVC film.

Aluminum alloy 6061 (AL6061), with magnesium and silicon as its major alloying elements, is the most commonly used aluminum alloy in the world. It is a cold-treated aluminum forging product with the advantages of 4000 Series and 5000 Series. When heat-treated, 6061 aluminum alloys are a great choice for general purpose uses and find many applications in structural materials, electronics, chemical equipment, and others. This alloy features high strength, good corrosion resistance, weldability, and machinability. It comes in different tempers  such as O (annealed), or tempered grades, 6061-T4 and 6061-T6. Compared to AL2024, the so-called aircraft aluminum, 2024 should be generally selected if strength is a priority or for forming applications.  In terms of machinability, 6061 aluminum is one of the most popular machining alloys and therefore often preferred if machining procedures are necessary for a project.

AL6061 tubes/pipes are offered as part of our own branded (AVIATIONEU NEW ERA) product lines.Tubes are designed to act as structural support, whereas pipes are designed to carry liquids and gases. AL6061 tubing come in different shapes (round, square, orthogonal and others), tempers (T6 or T651 ), dimensions and pre cut or cut to order lenght options with the ability to be heat treated for even higher strength, all at an affordable price. 

The AVIATIONEU NEW ERA 6061 T6 aluminum round tubes are offered as Drawn or Extruded (indicated respectively by the words "DRW" and "EXTRD" in the product SKU). They are available in different outer diameters, wall thicknesses and pre cut lengths in inches. The drawn tubes meet ASTM -B210 and AMS -4082 specifications while the extruded tubes comply with AMS-QQ-A-200/8, ASTM-B221, ASTM-B429 specifications. For additional information, please refer to our Brief Guide on Aluminum Grades & Temper Designations  or contact us.

One of the most versatile metals in manufacturing today is Aluminum used to produce products in an almost limitless number of shapes for an almost limitless number of uses.

AL2024, the so-called aircraft aluminum, is an aluminium alloy, with copper as the primary alloying element. It is used in applications requiring high strength to weight ratio, as well as good fatigue resistance, weldablility and average machinability. The addition of copper to this alloy makes 2024 one of the strongest aluminum alloys. It comes in different tempers (O without heat treatment or T with heat treatment). It is non-magnetic and heat treatable but it also is more succeptible to corrosion than most other aluminum alloys. 

Due to the poor corrosion resistance of this alloy  it is often clad (specified as CLAD or ALCLAD) in which case high-purity aluminium surface layers are metallurgically bonded to the aluminium alloy core material. 2024-T3 is typically used in structures where a high strength to weight ratio is necessary, clock parts, computer parts, hydraulic parts, bolts, valves, nuts, pistons, and gears. 

Aluminum 2024 tubes/pipes are offered as part of our own branded (AVIATIONEU NEW ERA) product lines.Tubes are designed to act as structural support, whereas pipes are designed to carry liquids and gases. AL2024 tubing comes in different shapes (round, square, orthogonal and others), tempers, dimensions and pre cut or cut to order lenght options with the ability to be heat treated for even higher strength, all at an affordable price. 

Two of the most commonly used processes for shaping aluminum include the extrusion and the drawing process. In the drawn aluminum tubing process the aluminum is pulled, or drawn into the die cavity, during which it undergoes what is called plastic deformation where the aluminum is stretched to achieve the desired shape. Drawn aluminum is most often used to create products including pots, cans, tubes and other circular objects. In the extrusion tubing process the formed shape is achived by first heating the aluminum to a very high temperature until it is soft and malleable but not liquid. Then it is forced or pushed through a die which enables molding and shaping of the desired final product. After extrusion, the finished extruded tubing product  begins to cool and harden becoming strong and durable and holding the desired shape.

The AVIATIONEU NEW ERA Aluminum alloy round tubes 2024 T3 temper are frequently used for aerospace as they offer an excellent strength-to-weight ratio, high fatigue resistance, and average machinability. They are offered as drawn and are available in different outer diameters, wall thicknesses and pre cut lengths in inches. Depending on the producer they meet AMS -4088, AMS -WW-T-700/3 and ASTM B210 specifications. For additional information, please refer to our Brief Guide on Aluminum Grades & Temper Designations or contact us.

Steel alloy 4130 (ST4130), also known as Chrome Moly after the 2 key elements of its composition, chromium, and molybdenum, is a general-purpose alloy steel widely used by the aviation and motorsports industries due to its tensile strength of 90,000 psi, weldability, fabrication, and mild hardenability in all offered forms (tubes, bars, sheets and plates). They are available in two different material states (Normalized and Annealed) depending on the process of how the material is heated and cooled.

The Normalized condition (sometimes referred to as "Condition N") is the harder and stronger condition and is best used when forming is not needed. Normalizing relieves internal stress on steel and improves toughness in steels that may harden after the cold working process. The Annealed condition (sometimes referred to as "Condition A") is the softer and formable condition and is best used when forming is needed. Annealing relieves internal stresses, softens and makes the material more ductile.

4130 alloy steel (Chromoly) tubes exhibit an excellent strength to weight ratio, they are malleable, very easy to weld, resistant to scaling and oxidation and have a clean, smooth finish on both the inside and the outside of the tubing. Square tubes are offered in Normalized (N) condition as part of our own branded (AVIATIONEU NEW ERA) product lines and conform to SAE AMS-T 6736 & AMS 6360 M(*) specifications. They can be furnished in different wall thicknesses, widths and heights in inches and in different pre cut lengths from 1 foot to 12 feet. Appearing selling prices are per foot of cut length. Unless otherwise mentioned, there is additional cost if manufacturing test reports are required. For additional information, please refer to the supplied documentation or contact us.

(*) Aerospace Material Specifications (AMS) established by the Society of Automotive Engineers (SAE).

Steel alloy 4130 (ST4130), also known as Chrome Moly is a general-purpose alloy steel widely used by the aviation and motorsports industries due to its tensile strength, weldability, fabrication, and  hardenability. Sourced from quality producers AVIATIONEU NEW ERA 4130 Alloy Steel welded round tubes are cold drawn, offered in Normalized (N) condition and can be used in mechanical engineering, automotive applications and machinery. They conform to ASTM A513 specifications and they are offered in different wall thicknesses (1-12.5 mm), outer diameters (OD  6-350 mm) and cut to order lengths (max12000 mm/12 m), in various heat treatment processes (no final thermal treatment, stress relieved, annealed or normalized). Unit of sale is 1 Ton (US or Metric as specified) with Minimum Order Quantity (MOQ) 3 Tons. Sea/sea-surface transport to customer destination can be provided. Approximate time for shipping: usually 1-2 months from the time of order payment depending on the ordered quantity. Appearing price is indicative per unit of sale. Mechanical properties, depending on the selected heat treatment process, are summarized below. For additional information please refer to the attached chart or contact us.

Yield Strength: 55 ksi/ 379 Mpa - 50 ksi/ 345 Mpa - 85 ksi/ 586 Mpa - 80 ksi/ 552 Mpa

Ultimate Strength: 72 ksi/ 496 Mpa - 70 ksi/ 483 Mpa - 95 ksi/ 655 Mpa - 90 ksi/ 621 Mpa

Enlongation (%): 10% - 20% - 5% - 10%

Rockwell Hardness B Scale: 80 - 100 - 90- 87

AISI/SAE(*) 4130 and 4140 grade steels are low-alloy steels containing chromium and molybdenum as common composition elements. Both are are popular steel materials due to their properties. AISI 4130 grade steel shows good overall combinations of strength, toughness and fatigue strength with good atmospheric corrosion resistance while AISI 4140 grade steel features a high fatigue strength, abrasion and impact resistance, toughness, and torsional strength. Both alloys are weldable with the use of all conventional techniques (AISI 4130 alloy's lower carbon composition compared to AISI 4140 allows easier welding) and machinable in the annealed condition. To make them stronger they need to be subjected to heat treatment, such as annealing, cold working, etc. 4140 and 4130 grade steels are wideky used in aerospace, oil and gas, automotive, agricultural and defense industries.

Round bars from AISI 4130/4140 structural steel alloys are offered as part of AVIATIONEU NEW ERA product lines for a wide range of uses in different applications (gears, connection rods, stem assemblies, pump shafts, tool holders and others. Sourced from quality producers, they are competitively priced and offered in different diameters ( 5.5-500 mm), pre-cut (5.8m, 6m, 11.8m) and cut to order lengths, consisting a cost effective solution when large quantities of such sheets are demanded. Unit of sale is 1 kilogrram (kg)) with Minimum Order Quantity (MOQ) 300 kilograms. Sea/sea-surface transport to customer destinationcan be provided. Approximate time for shipping: usually 1-2 months from the time of order payment depending on the ordered quantity. Appearing price is indicative per unit of sale. For additional information, please refer to the attached comparison table of specifications for different steel alloys or contact us for quotation.

(*) American Iron & Steel Institute (AISI), Society of Automotive Engineers (SAE)

Seamless 4130/4140 alloy steel tubes/pipes are offered as part of AVIATIONEU NEW ERA product lines in rectangular or square shapes. Produced as cold drawn & cold rolling the tubes are intended for use in structural applications. These tubes can be delivered in different options (A.W.H.R. "as welded" from hot-rolled steel, A.W.C.R. "as welded" from cold-rolled steel, S.D.C.R.  "sink-drawn", cold-rolled steel, M.D. mandrel drawn or S.S.I.D. special smooth inside diameter). Sourced from quality producers, they conform to ASTM A519 specifications and can be furnished in the following ranges of wall thicknesses, outer dimensions and cut to order lengths:

Square Tubes  

Outer Dimesion (O.D.): 20-20 to 500-500 mm,

Wall Thickness  (W.T.): 1-24 mm,

Cut Length (L): Cut To Order - max12000 mm (12 m).

Rectangle Tubes 

Outer Dimesion (O.D.): 20-30 to 400-600 mm,

Wall Thickness  (W.T.): 1-24 mm,

Cut Length (L): Cut To Order - max12000 mm (12 m).

Unit of sale is 1 Ton (US or Metric as specified) with Minimum Order Quantity (MOQ) 3 Tons. Sea/sea-surface transport to customer destination can be provided. Approximate time for shipping: usually 1-2 months from the time of order payment depending on the ordered quantity. Appearing price is indicative per unit of sale. For additional information please refer to the attached chart or contact us.

Aluminum alloy 7075 (AL7075) is another "aircraft grade" aluminum with zinc and copper as its major alloying elements. Like aluminum alloy 2024 ((AL2024), AL7075 is a flexible and durable aluminum alloy extremely useful in highly stressed parts. Typically used in aerospace and defense, automotive, manufacturing and other applications requiring lighter weight and durable materials. This alloy is one of the strongest alloys available and is comparable to many types of steel featuring a high strength, low density (high strength-to-weight ratio), but also thermal properties and ability to be polished which makes AL7075 a preferred choice for the mold making industry. 

AL7075 aluminum alloy sheets are offered as part of AVIATIONEU NEW ERA product lines. Sourced from quality producers, they come in T6/T651 tempers (heat treated) and offered for cut to order in different thicknesses, widths and lengths, consisting a cost effective solution when large quantities of such sheets are demanded. Unit of sale is 1 Ton (US or Metric as specified) with Minimum Order Quantity (MOQ) 1 Ton. Sea/sea-surface transport to customer destinationcan be provided. Approximate time for shipping: usually 1-2 months from the time of order payment depending on the ordered quantity. Appearing price is indicative per unit of sale.  

For additional information, please refer to our attached Brief Guide on Aluminum Grades & Temper Designations, the individual product presentations or contact us for quotation.

AVIATIONEU NEW ERA round tubes from 5052 aluminum alloy are competitively priced, sourced from certified manufacturers, produced as per ASTM B210M specification and offered as Annealed (O-temper) or H112 tempered. Used in aviation and industrial applications (constructions, furniture, signs, etc). They are mill finished and available in outer diameters 5-650 mm, wall thicknesses 1-55 mm and lengths 1-13 m. Unit of measurement is 1 US Ton with Minimum Order Quantity (MOQ) 1 US Ton. Sea/sea-surface transport to destination. Appr. time for shipping: 1 month from the time of order payment. Appearing price is indicative per unit of sale. Please contact us for for additional information and quotation.

Our Quick Guide for Aluminum Alloys & Tempers is now available. Please see attached file.

AL6061 is an aluminium alloy, with magnesium and silicon as the primary alloying elements. It is one of the most common alloys of aluminum for general-purpose use. Commonly available in pre-tempered grades such as 6061-O (annealed) as well as tempered grades such as 6061-T6 or 6061-T651. It can be compared with AL5052 (the highest strength alloy of the more non-heat-treatable grades) as well as with AL6063 which  is similar in composition and mechanical properties. AL6061 main features include: heat-treatable, excellent machinability, excellent corrosion resistance, semi-smooth surface, lightweight, high-tensile strength. Commonly used in transportation components, recreation products, machinery and equipment, and consumer durables.

Extruded bars/rods from 6061 aluminum alloy are offered as part of our own branded (AVIATIONEU NEW ERA) product lines. They come in different cross sections such as round, rectangular or square. Competitively priced, they are sourced from quality producers, comply with ASTM specifications and offered as Fabricated (F) or H112 tempered. 

AVIATIONEU NEW ERA Aluminum 6061 H112 Temper round bars are offered in different diameters 6 mm (15/64'') -300 mm (11-13/16") and cut to order lengths up to 12000 mm (12 m), consisting a cost effective solution when large quantities are demanded. Unit of sale is 1 Ton (US or Metric as specified) with Minimum Order Quantity (MOQ) 1 Ton. Sea/sea-surface transport to customer destination can be provided. Approximate time for shipping: usually 1-2 months from the time of order payment depending on the ordered quantity. Appearing price is indicative per unit of sale.  For additional information, please refer to our attached Brief Guide on Aluminum Grades & Temper Designations or contact us for quotation.

Grade 5052 aluminium alloy, with magnesium and chromium as the primary alloying elements is frequently used for general sheet metal work, heat exchangers, flooring panels, rivets and wires, chemical drums and other equipment, pressure vessels, containers, and other applications.  5052 aluminium alloy exhibits a good marine atmosphere corrosion resistance of saltwater and excellent workability. Main features of this alloy include: non heat-treatable, excellent weldability, high corrosion resistance, smooth surface, lightweight, high-tensile strength.

Extruded bars/rods (*) from 5052 aluminum alloy are offered as part of our own labelled (AVIATIONEU NEW ERA) product lines. They come in different cross sections such as round, rectangular, hexagonal or square. Competitively priced, they are sourced from quality producers, comply with ASTM specifications and mostly offered as Fabricated (F) or H112 tempered. They are offered in Metric dimensions and cut to order lengths up to 12000 mm (12 m). AVIATIONEU NEW ERA Aluminum 5052 bars/rods consist a cost effective solution when large quantities are demanded. Unit of sale is 1 Ton (US or Metric as specified) with Minimum Order Quantity (MOQ) 1 Ton. Appearing price is indicative per unit of sale and can differentiate depending on the specifications of the ordered metals. 

In most cases, smaller quantities can be served by our suppliers' stocks within 10 days from order placement & payment. Availability for non stock sizes/quantities is  usually 1-2 months.

Packing includes waterproof paper, wooden boxes/pallets, steel band bundling etc. Sea/sea-surface transport to customer destination can be provided at additional cost.

Dimesion (size) ranges of offered AVIATIONEU NEW ERA Aluminum 5052 bars/rods per cross section:

Round: diameter from 4 to 650 mm

Square: dimensions from 4X4  to 200X200 mm

Rectangular: dimensions from  3X4 to 200X300 mm

Flat: dimensions from 3X4  to 10X675 mm

Hexagonal: A/F from 6 to 30 0mm

For additional information, please refer to our attached Brief Guide on Aluminum Grades & Temper Designations or contact us for quotation.

(*) Although the terms bars and rods are often used interchangeably and present general similarities, rods come in a smaller cross sections and are usually less strong and durable than bars. Due to their strength and durability, bars are often used in structural applications while rods are typically used in non-structural ones such as reinforcing, decorative and others.

AL6061 is an aluminium alloy, with magnesium and silicon as the primary alloying elements. It is one of the most common alloys of aluminum for general-purpose use. Commonly available in pre-tempered grades such as 6061-O (annealed) as well as tempered grades such as 6061-T6 or 6061-T651. It can be compared with AL5052 (the highest strength alloy of the more non-heat-treatable grades) as well as with AL6063 which  is similar in composition and mechanical properties. AL6061 main features include: heat-treatable, excellent machinability, excellent corrosion resistance, semi-smooth surface, lightweight, high-tensile strength. Commonly used in transportation components, recreation products, machinery and equipment, and consumer durables.

Extruded bars/rods from 6061 aluminum alloy are offered as part of our own branded (AVIATIONEU NEW ERA) product lines. They come in different cross sections such as round, rectangular or square. Competitively priced, they are sourced from quality producers, comply with ASTM specifications and offered as Fabricated (F) or H112 tempered. 

AVIATIONEU NEW ERA Aluminum 6061 H112 Temper square bars are offered in different dimensions 5 mm × 5 mm (13/64" x 13/64") up to 150 mm × 150 mm (5-29/32" x 5-29/32") and cut to order lengths up to 12000 mm (12 m), consisting a cost effective solution when large quantities are demanded. Unit of sale is 1 Ton (US or Metric as specified) with Minimum Order Quantity (MOQ) 1 Ton. Sea/sea-surface transport to customer destination can be provided. Approximate time for shipping: usually 1-2 months from the time of order payment depending on the ordered quantity. Appearing price is indicative per unit of sale.  For additional information, please refer to our attached Brief Guide on Aluminum Grades & Temper Designations or contact us for quotation.

AL6061 is an aluminium alloy, with magnesium and silicon as the primary alloying elements. It is one of the most common alloys of aluminum for general-purpose use. Commonly available in pre-tempered grades such as 6061-O (annealed) as well as tempered grades such as 6061-T6 or 6061-T651. It can be compared with AL5052 (the highest strength alloy of the more non-heat-treatable grades) as well as with AL6063 which  is similar in composition and mechanical properties. AL6061 main features include: heat-treatable, excellent machinability, excellent corrosion resistance, semi-smooth surface, lightweight, high-tensile strength. Commonly used in transportation components, recreation products, machinery and equipment, and consumer durables.

Extruded bars/rods from 6061 aluminum alloy are offered as part of our own branded (AVIATIONEU NEW ERA) product lines. They come in different cross sections such as round, rectangular or square. Competitively priced, they are sourced from quality producers, comply with ASTM specifications and offered as Fabricated (F) or H112 tempered. 

AVIATIONEU NEW ERA Aluminum 6061 H112 Temper rectangular bars are offered in different dimensions 3.0 mm (1/8') -100 mm (3-15/16") × 10 mm (25/64") -300 mm (11 13/16") and cut to order lengths up to 12000 mm (12 m), consisting a cost effective solution when large quantities are demanded. Unit of sale is 1 Ton (US or Metric as specified) with Minimum Order Quantity (MOQ) 1 Ton. Sea/sea-surface transport to customer destination can be provided. Approximate time for shipping: usually 1-2 months from the time of order payment depending on the ordered quantity. Appearing price is indicative per unit of sale.  For additional information, please refer to our attached Brief Guide on Aluminum Grades & Temper Designations or contact us for quotation.

AL7050 (known as a commercial aerospace alloy) is a heat-treatable aluminium alloy with zinc as the main alloying element, combining high mechanical strength, good stress corrosion cracking resistance and toughness at subzero temperatures. Typical mechanical properties of 7050 aluminum in metric and imperial systems include a tensile strength of 515 MPa (74695 psi), a yield strength of 455 MPa (65992 psi) and a fatigue strength of 240 MPa (34809 psi). Particularly suitable for heavy plate aerospace and other commercial and military applications, such as fuselage frames, bulkheads, wing skins and aircraft structures.

Extruded bars from 7050 aluminum alloy are offered as part of our own branded (AVIATIONEU NEW ERA) product lines. Competitively priced, they are sourced from quality producers, comply with ASTM specifications and offered in different shapes, (round, rectangular and square), tempers (e.g. as Fabricated (F) or H112 tempered), specifications, diameters/thicknesses and cut-to-oder lengths to meet order requirements. 

7070 aluminum alloy round bars are available in diameters 6 mm (15/64'') -300 mm (11-13/16") and cut to order lengths up to 12000 mm (12 m), consisting a cost effective solution when large quantities are demanded. Unit of sale is 1 Ton (US or Metric as specified) with Minimum Order Quantity (MOQ) 1 Ton. Sea/sea-surface transport to customer destination can be provided. Approximate time for shipping: usually 1-2 months from the time of order payment depending on the ordered quantity. Appearing price is indicative per unit of sale.  For additional information, please refer to our attached Brief Guide on Aluminum Grades & Temper Designations or contact us for quotation.

Note: AVIATIONEU NEW ERA metals are supplied free from oil stains, dents, inclusions, scratches, oxide discolorations, corrosion, or other defects. In certain cases, metals are additionally protected with PVC film. 

AL7050 (known as a commercial aerospace alloy) is a heat-treatable aluminium alloy with zinc as the main alloying element, combining high mechanical strength, good stress corrosion cracking resistance and toughness at subzero temperatures. Typical mechanical properties of 7050 aluminum in metric and imperial systems include a tensile strength of 515 MPa (74695 psi), a yield strength of 455 MPa (65992 psi) and a fatigue strength of 240 MPa (34809 psi). Particularly suitable for heavy plate aerospace and other commercial and military applications, such as fuselage frames, bulkheads, wing skins and aircraft structures.

Extruded bars from 7050 aluminum alloy are offered as part of our own branded (AVIATIONEU NEW ERA) product lines. Competitively priced, they are sourced from quality producers, comply with ASTM specifications and offered in different shapes, (round, rectangular and square), tempers (e.g. as Fabricated (F) or H112 tempered), specifications, diameters/thicknesses and cut-to-oder lengths to meet order requirements. 

7070 aluminum alloy square bars are available in different dimensions 5 mm × 5 mm (13/64" x 13/64") up to 150 mm × 150 mm (5-29/32" x 5-29/32") and cut to order lengths up to 12000 mm (12 m), consisting a cost effective solution when large quantities are demanded. Unit of sale is 1 Ton (US or Metric as specified) with Minimum Order Quantity (MOQ) 1 Ton. Sea/sea-surface transport to customer destination can be provided. Approximate time for shipping: usually 1-2 months from the time of order payment depending on the ordered quantity. Appearing price is indicative per unit of sale.  For additional information, please refer to our attached Brief Guide on Aluminum Grades & Temper Designations or contact us for quotation.

Note: AVIATIONEU NEW ERA metals are supplied free from oil stains, dents, inclusions, scratches, oxide discolorations, corrosion, or other defects. In certain cases, metals are additionally protected with PVC film. 

AL7050 (known as a commercial aerospace alloy) is a heat-treatable aluminium alloy with zinc as the main alloying element, combining high mechanical strength, good stress corrosion cracking resistance and toughness at subzero temperatures. Typical mechanical properties of 7050 aluminum in metric and imperial systems include a tensile strength of 515 MPa (74695 psi), a yield strength of 455 MPa (65992 psi) and a fatigue strength of 240 MPa (34809 psi). Particularly suitable for heavy plate aerospace and other commercial and military applications, such as fuselage frames, bulkheads, wing skins and aircraft structures.

Extruded bars from 7050 aluminum alloy are offered as part of our own branded (AVIATIONEU NEW ERA) product lines. Competitively priced, they are sourced from quality producers, comply with ASTM specifications and offered in different shapes, (round, rectangular and square), tempers (e.g. as Fabricated (F) or H112 tempered), specifications, diameters/thicknesses and cut-to-oder lengths to meet order requirements. 

7070 aluminum alloy rectangular bars are available in different dimensions 3.0 mm (1/8') -100 mm (3-15/16") × 10 mm (25/64") -300 mm (11 13/16") and cut to order lengths up to 12000 mm (12 m), consisting a cost effective solution when large quantities are demanded. Unit of sale is 1 Ton (US or Metric as specified) with Minimum Order Quantity (MOQ) 1 Ton. Sea/sea-surface transport to customer destination can be provided. Approximate time for shipping: usually 1-2 months from the time of order payment depending on the ordered quantity. Appearing price is indicative per unit of sale.  For additional information, please refer to our attached Brief Guide on Aluminum Grades & Temper Designations or contact us for quotation.

Note: AVIATIONEU NEW ERA metals are supplied free from oil stains, dents, inclusions, scratches, oxide discolorations, corrosion, or other defects. In certain cases, metals are additionally protected with PVC film. 

AVIATIONEU NEW ERA extruded round bars/rods from 7075 aluminum alloy are competitively priced, sourced from certified manufacturers, produced as per ASTM specification and offered as Fabriacted (F) or H112 tempered. Used in aviation and industrial applications (constructions, transportation tools, etc). They are available in outer diameters 6 mm (15/64'') -300 mm (11-13/16") and length up to 12000 mm (12 m). Unit of measurement is 1 US Ton with Minimum Order Quantity (MOQ) 1 US Ton. Sea/sea-surface transport to destination. Appr. time for shipping: 1 month from the time of order payment. Appearing price is indicative per unit of sale. Please contact us for for additional information and quotation.

Our Quick Guide for Aluminum Alloys & Tempers is now available. Please see attached file.

AVIATIONEU NEW ERA extruded square bars from 7075 aluminum alloy are competitively priced, sourced from certified manufacturers, produced as per ASTM specification and offered as Fabriacted (F) or H112 tempered. Used in aviation and industrial applications. They are available in dimensions 5 mm × 5 mm (13/64" x 13/64") up to 150 mm × 150 mm (5-29/32" x 5-29/32") and length up to 12000 mm (12 m). Unit of measurement is 1 US Ton with Minimum Order Quantity (MOQ) 1 US Ton. Sea/sea-surface transport to destination. Appr. time for shipping: 1 month from the time of order payment. Appearing price is indicative per unit of sale. Please contact us for for additional information and quotation.

Our Quick Guide for Aluminum Alloys & Tempers is now available. Please see attached file.

AVIATIONEU NEW ERA extruded rectangular bars from 7075 aluminum alloy are competitively priced, sourced from certified manufacturers, produced as per ASTM specification and  offered as Fabriacted (F) or H112 tempered. Used in aviation and industrial applications. They are available in dimensions 3.0 mm (1/8') -100 mm (3-15/16") × 10 mm (25/64") -300 mm (11 13/16") and length up to 12000 mm (12 m). Unit of measurement is 1 US Ton with Minimum Order Quantity (MOQ) 1 US Ton. Sea/sea-surface transport to destination. Appr. time for shipping: 1 month from the time of order payment. Appearing price is indicative per unit of sale. Please contact us for for additional information and quotation.

Our Quick Guide for Aluminum Alloys & Tempers is now available. Please see attached file.

AISI/SAE(*) 4130 and 4140 grade steels are low-alloy steels containing chromium and molybdenum as common composition elements. Both are are popular steel materials due to their properties. AISI 4130 grade steel shows good overall combinations of strength, toughness and fatigue strength with good atmospheric corrosion resistance while AISI 4140 grade steel features a high fatigue strength, abrasion and impact resistance, toughness, and torsional strength. Both alloys are weldable with the use of all conventional techniques (AISI 4130 alloy's lower carbon composition compared to AISI 4140 allows easier welding) and machinable in the annealed condition. To make them stronger they need to be subjected to heat treatment, such as annealing, cold working, etc. 4140 and 4130 grade steels are wideky used in aerospace, oil and gas, automotive, agricultural and defense industries.

AISI 4130/4140 alloy steel sheets/plates are offered as part of AVIATIONEU NEW ERA product lines for a wide range of uses. Sourced from quality producers, they are cold rolled to increase their strength and produced in accordance with ASTM specificatiions. Competitively priced and offered in different thicknesses (0.2-4 mm or 4-60 mm or 60-115 mm) and cut to order widths (500-1500 mm  or 600-3000 mm) and lengths, they consist a cost effective solution when large quantities of such sheets are demanded. Unit of sale is 1 Ton (US or Metric as specified) with Minimum Order Quantity (MOQ) 1 Ton. Sea/sea-surface transport to customer destinationcan be provided. Approximate time for shipping: usually 1-2 months from the time of order payment depending on the ordered quantity. Appearing price is indicative per unit of sale.  

For additional information, please refer to the attached comparison table of specifications for different steel alloys or contact us for quotation.

(*) American Iron & Steel Institute (AISI), Society of Automotive Engineers (SAE)

Stainless Steel alloy 13-8 PH (UNS S13800) is a martensitic precipitation-hardening stainless steel alloy featuring excellent strength, high hardness, superior toughness, and good corrosion resistance. Good transverse toughness properties are achieved by tight chemical composition control, low carbon content,and vacuum melting.

The chemical composition includes Chromium (Cr) 12.25-13.25%, Nickel (Ni) 7.5-8.5%, Molybdenum (Mo) 2.0-2.5%, Aluminum (Al) 0.90-1.35% as content weight with other metals covering the balance. This alloy is double melted in a Vacuum Induction Furnace followed by Consumable Electrode Vacuum Melt (VIM-VAR). In some cases, a second melting  by Electroslag Remelting (ESR) is implemented. It is weldable (inert gas shielding with Helium is preferred). Corrosion resistance is similar to 304 Stainless, with greatest resistance in the fully hardened conditions. Stainless Steel 13-8 PH comes in different shapes mostly in bars/rods, wires, forgings, rings and extrusions but also in sheets or plates.

Stainless steel 13-8 Mo is used in a range of applications including pins, valves, shafts, screws and bolts, missile components, fittings and fasteners, injection molding equipment, nuclear and petrochemical industry equipment as well as aircraft components such as engine, landing gear and structural sections.

Stainless Steel 13-8 PH grade round bars/rods are offered as part of AVIATIONEU NEW ERA product lines. Sourced by quality producers, these bars/rods are offered in Condition A (Annealed) and in different diameters in inches and pre cut lengths in inches or feet. They meet different specifications such as AMS -5629 or ASTM -A564. For additional information, please refer to the supplied documentation or contact us.

Aluminum alloys 6061 and 6063 (AL6061/AL6063), with magnesium and silicon as their major alloying elements, are both popular alloys used in extrusions for a variety of architectural, machinery, equipment, and consumer products. Similar in composition & mechanical properties they come as O (annealed), or in tempered grades. Their magnesium content provides increased strength, and silicon reduces their melting temperature. Their formability, weldability, corrosion resistance, and moderately high strength enhance their versatility. However, there are differences between them and factors affecting their suitability for different applications. 6061 aluminum is the most commonly used aluminum alloy in the world used in all kinds of applications ranging from electronics to welded assemblies. Compared to AL2024 (aka aircraft aluminum) 2024 aluminum’s higher yield strength makes it more suitable if strength is a priority. 6061 tubes, sheets, bars, and plates offer high- to moderate strength, excellent corrosion resistance, and superior machinability and weldability while 6063 aluminum tubes offer an excellent strength-to-weight ratio, superior corrosion resistance, and a fine appearance and finish.

AVIATIONEU NEW ERA seamless extruded round pipes from 6061/6063 aluminum alloy are competitively priced, produced as per ASTM B241 specification (also available in ASTM B209-04, B210M-05, B234M-04 & B221M-05a) and offered as T6 tempered. Available in outer diameters 12.7-1066.8 mm, wall thicknesses 1.5-150 mm and cut to order (CTO) lengths. Unit of sale is 1 Ton (US or Metric as specified) with Minimum Order Quantity (MOQ) 1 Ton. Sea/sea-surface transport to customer destination can be provided. Approximate time for shipping: usually 1-2 months from the time of order payment depending on the ordered quantity. Appearing price is indicative per unit of sale. For additional information, please refer to our attached Brief Guide on Aluminum Grades & Temper Designations or contact us.

2000 series aluminum alloys, with copper as the primary alloying element, are a set of "hard alloys". They typically contain between 2 to 10% copper, with smaller additions of other elements. The copper provides substantial increases in strength and facilitates precipitation hardening but can also reduce ductility and corrosion resistance. These alloys are known for high performance and excellent strength over a broad range of temperatures   but can be the most challenging to weld. They find use in many industries, including the aerospace sector. They are essential materials in various industries such as aerospace, marine, construction, and automobile. 

Extruded round tubes from 2011, 2014, 2017 and 2024 aluminum alloys in T351 & T651 tempers are offered as part of AVIATIONEU NEW ERA product lines. Sourced from quality producers, they conform with ASTM specifications. Competively priced these tubes are available in different diameters 1-360 mm, wall thicknesses and cut to order (CTO) lengths max 6 m. Also available in other shapes (square, rectangular, hexagonal tubes and ultra-thin tubes). Unit of sale is 1 Ton (US or Metric as specified) with Minimum Order Quantity (MOQ) 1 Ton. Sea/sea-surface transport to customer destination can be provided. Approximate time for shipping: usually 1-2 months from the time of order payment depending on the ordered quantity. Appearing price is indicative per unit of sale. For additional information, please refer to our attached Brief Guide on Aluminum Grades & Temper Designations or contact us.

AVIATIONEU NEW ERA Chrome Moly 4130 grade steel seamless round tubes are sourced from certified manufacturers, they are competitively priced and can be used in aerospace and industrial applications. They are offered in different wall thicknesses (2-200 mm), outer diameters (25-450 mm) and lengths, 10 mm (0.01 m) - 9000 mm (9 m). Depending on selected prroduct they comply with different AMS, ASTM or MIL specifications. Unit of measurement is 1 US Ton with Minimum Order Quantity (MOQ) 1 US Ton. They can be sea or sea/surface transported to the customer destination. Approximate time for shipping: 2 months from the time of ordering and payment receipt. Appearing price is indicative per unit of sale. Please contact us for quotation.

Aluminum alloy 6061 is the most commonly used aluminum alloy in the world due to its positive characteristics. It has magnesium and silicon as its main composition elements and is a cold-treated aluminum forging product with the advantages of 4000 Series and 5000 Series. Aluminum 6061, T6 or T651 tempered sheets exhibit above average corrosion resistance, excellent processability with no deformations, high strength, light weight, good weldability, and the ability to be heat treated for even higher strength, all at an affordable price. The difference between T6 and T651 tempers of an 6061 aluminum sheet is that the internal stress of T6 is relatively large and the processing will be deformed under normal circumstances; the suitable state for processing should be T651, which is based on T6 to stretch and eliminate internal stress. Both are typically used in aerospace, automotive, cameras, couplings, marine hardware, electrical components, decorative hardware, structural applications, pins, brakes, pistons, valves, and bicycle frames. Aluminum alloy 6061-T6 sheets from AVIATIONEU NEW ERA product lines are offered in different pre cut thicknesses, widths and lengths and they are PVC covered one side. They meet AMS 4027/ASTM B209 specifications.

AVIATIONEU NEW ERA cladding metal alloy strips combine two or more different cladding materials to achieve the optimum of the best characteristics of the individual materials. These strips intended for use in different industrial applications. They are offered in a range of combinations of cladding materials in different thicknesses, widths and lengths meeting order requirements, they are competitively priced, sourced from certified manufacturers and produced in accordance with international standards.  Unit of measurement is 1 kilogram (kg) with Minimum Order Quantity (MOQ) 250 kilograms unless otherwise stated. Sea/sea-surface transport to customer destination is most commonly used. Appr. time for shipping: 3 months from the time of order payment. Appearing prices are indicative per unit of sale. Please refer to any attached documentation  and contact us for additional information/clarifications and quotation.

AL5052 is an aluminium alloy, with magnesium and chromium as the primary alloying elements. Although It is non heat-treatable, it is the highest strength alloy of other non-heat-treatable grades also featuring an excellent weldability using most common techniques, high resistance to marine atmoshpere and salt water corrosion, smooth surface, lightweight and high-tensile strength. This alloy is comparable to the 6061 aluminum alloy (AL6061). 

AL5052-O aluminum alloy Annealed round tubes are offered as part of our own branded (AVIATIONEU NEW ERA) product and can be used for low and medium pressure hydraulic systems, fuel lines and oil lines. They withstand a higher pressure than 3003-0 tubing and can be gas, arc and resitance welded and coiled.  They meet WW-T-700/4, AMS 4070M and ASTM-B-210-12 specifications. Sourced from quality producers, they are offered in different outer diameters and wall thicknesses in inches and pre cut lengths of 6 feet and in 6 ft increments each. Cuts to smaller lenghts may be arranged with the supplier providing that minimum order quantity requirements are observed. They are also offered as ALCLAD for the enhancement of their corrosion-resistance (please refer to the separate product presentation). There is additional cost if manufacturing test reports are required. For additional information, please refer to our attached Brief Guide on Aluminum Grades & Temper Designations, the supplied documentation or contact us for quotation.

AL6061 is an aluminium alloy, with magnesium and silicon as the primary alloying elements. It is one of the most common alloys of aluminum for general-purpose use. Commonly available in pre-tempered grades such as 6061-O (annealed) as well as tempered grades such as 6061-T6 or 6061-T651. It can be compared with AL5052 (the highest strength alloy of the more non-heat-treatable grades) as well as with AL6063 which  is similar in composition and mechanical properties. AL6061 main features include: heat-treatable, excellent machinability, excellent corrosion resistance, semi-smooth surface, lightweight, high-tensile strength. Commonly used in transportation components, recreation products, machinery and equipment, and consumer durables.

Extruded bars/rods from 6061 aluminum alloy are offered as part of our own branded (AVIATIONEU NEW ERA) product lines. They come in different cross sections such as round, rectangular or square. Competitively priced, they are sourced from quality producers, comply with ASTM specifications and offered as  T6/T651 tempered in different dimensions. 

AVIATIONEU NEW ERA 6061 Aluminum square/rectangular bars are produced by extrusion and are offered in T6 or T651 Tempers, in different dimensions in inches and cut to order lengths in feet (in increments of one foot) to meet application requirements. They comply with ASTM-B221 and AMS-QQ-A-200/8 specifications. For additional information, please refer to our Brief Guide on Aluminum Grades & Temper Designations,  the individual product presentations or contact us.

Note: AVIATIONEU NEW ERA metals are supplied free from oil stains, dents, inclusions, scratches, oxide discolorations, corrosion, or other defects. In certain cases, metals are additionally protected with PVC film.

Steel alloy 4130 (ST4130),aka Chrome Moly,after the 2 key composition elements,chromium & molybdenum,is a general-purpose alloy steel widely used by the aviation and motorsports industries due to its weldability, fabrication and mild hardenability in all offered forms (tubes, bars/rods, sheets and plates). Available in two material states (Normalized and Annealed) depending on the process of how the material is heated and cooled.The Normalized condition (aka "Condition N") is the harder and stronger condition, best used when forming is not needed while the Annealed condition (aka "Condition A") is the softer and formable condition.

4130 steel bars/rods in round, rectangullar (flat), square and hexagonal shapes (cross sections) are offered as part of our own branded (AVIATIONEU NEW ERA) product lines. Sourced from quality producers, most of these bars/rods are produced, unless otherwise specified, as “Cold Finished Normalized” (aka “Condition D4”), indicated by the letters "NRZ" and  "CF" in the product SKUs.They are widely used in a variety of applications due to their excellent strength to weight ratio,weldability by all conventional methods and resistance to scaling and oxidation. 

AVIATIONEU NEW ERA 4130 Steel Alloy Rectangular (Flat) Bars/Rods are AMS S 6758 Condition D4 (Cold Finished Normalized) and Tempered MIL S 6758, unless otherwise specified. They are offered in different widths, thicknesses and pre-cut lengths in inches.  Also available in cut to order lengths (please refer to the respective product presentation).  It's best to keep the lengths under 5 feet for air shipping. Longer bars can only be shipped via standard sea/ground transportation.

Unless otherwise mentioned, there is additional cost if manufacturing test reports are required. For additional information, please refer to the supplied documentation, the individual product presentations or contact us.

Steel alloy 4130 (ST4130), also known as Chrome Moly after the 2 key elements of its composition, chromium, and molybdenum, is a general-purpose alloy steel widely used by the aviation and motorsports industries due to its weldability, fabrication, and mild hardenability in all offered forms (tubes, bars, sheets and plates). They are available in two different material states (Normalized and Annealed) depending on the process of how the material is heated and cooled.

The Normalized condition (sometimes referred to as "Condition N") is the harder and stronger condition and is best used when forming is not needed. Normalizing relieves internal stress on steel and improves toughness in steels that may harden after the cold working process. The Annealed condition (sometimes referred to as "Condition A") is the softer and formable condition and is best used when forming is needed. Annealing relieves internal stresses, softens and makes the material more ductile.

4130 alloy steel (Chrome Moly) seamless round tubes are offered in Normalized (N )  or Annealed (A) conditions as part of our own branded (AVIATIONEU NEW ERA) product lines. They have been for years the standard of the aircraft industry. These tubes offer good strength and weldability without compromising steel abrasion or impact resistance and can also be made even stronger through heat treatment. They are commonly used in in structural applications, gears, fasteners, and aircraft exteriors. Tensile Strength: 90,000 PSI. Available in a range of outer diameters, wall thicknesses and pre-cut lengths in inches or cut to order (CTO) lengths of 12 inches (1 foot)) or multiples. Apperating price of CTO tubes is per foot (12 inches). Depending on the supplier, they comply with different standards/specifications, such as MIL-T6736 standard or ASTM/A S1906 specifications. Unless otherwise mentioned, there is additional cost if manufacturing test reports are required. For additional information, please refer to the supplied documentation or contact us.

Steel alloy 4130 (ST4130), also known as Chrome Moly after the 2 key elements of its composition, chromium, and molybdenum, is a general-purpose alloy steel widely used by the aviation and motorsports industries due to its weldability, fabrication, and mild hardenability in all offered forms (tubes, bars, sheets and plates). They are available in two different material states (Normalized and Annealed) depending on the process of how the material is heated and cooled.

The Normalized condition (sometimes referred to as "Condition N") is the harder and stronger condition and is best used when forming is not needed. Normalizing relieves internal stress on steel and improves toughness in steels that may harden after the cold working process. The Annealed condition (sometimes referred to as "Condition A") is the softer and formable condition and is best used when forming is needed. Annealing relieves internal stresses, softens and makes the material more ductile.

4130 alloy steel (Chrome Moly) seamless round tubes are offered in Normalized (N )  or Annealed (A) conditions as part of our own branded (AVIATIONEU NEW ERA) product lines. They have been for years the standard of the aircraft industry. These tubes offer good strength and weldability without compromising steel abrasion or impact resistance and can also be made even stronger through heat treatment. They are commonly used in in structural applications, gears, fasteners, and aircraft exteriors. Tensile Strength: 90,000 PSI. Available in a range of outer diameters, wall thicknesses in millimeters (mm) and pre-cut lengths of one meter or multiples or cut to order (CTO) lengths in centimeters (cm). Depending on the supplier, they comply with different standards/specifications, such as ASTM A 519 or AMS MIL-T6737. Unless otherwise mentioned, there is additional cost if manufacturing test reports are required. For additional information, please refer to the supplied documentation or contact us.

AL6061 is an aluminium alloy, with magnesium and silicon as the primary alloying elements. It is one of the most common alloys of aluminum for general-purpose use. Commonly available in pre-tempered grades such as 6061-O (annealed) as well as tempered grades such as 6061-T6 or 6061-T651. It can be compared with AL5052 (the highest strength alloy of the more non-heat-treatable grades) as well as with AL6063 which  is similar in composition and mechanical properties. AL6061 main features include: heat-treatable, excellent machinability, excellent corrosion resistance, semi-smooth surface, lightweight, high-tensile strength. Commonly used in transportation components, recreation products, machinery and equipment, and consumer durables.

Extruded bars/rods from 6061 aluminum alloy are offered as part of our own branded (AVIATIONEU NEW ERA) product lines. They come in different cross sections such as round, rectangular or square. Competitively priced, they are sourced from quality producers and offered as T6/T651 tempered. 

AVIATIONEU NEW ERA Aluminum 6061 T6 Temper round bars/rods are produced by extrusion and offered in different diameters and pre-cut lengths in inches to meet application requirements. They comply with ASTM-B221 and AMS-QQ-A-200/8 specifications. For additional information, please refer to our Brief Guide on Aluminum Grades & Temper Designations,  the individual product presentations or contact us.

Note: AVIATIONEU NEW ERA metals are supplied free from oil stains, dents, inclusions, scratches, oxide discolorations, corrosion, or other defects. In certain cases, metals are additionally protected with PVC film.

AL2024 is an aluminium alloy, with copper as the primary alloying element. It is used in aircraft structural and other applications requiring high strength to weight ratio, as well as good fatigue resistance, weldablility and average machinability. This alloy  comes in  Annealed (O) condition  or different tempers and is readily formed and machined to a high finish in the annealed condition. It can be both hot and cold worked or forged, as well as welded through inert gas consumable electrode arc methods.

AL2024 extruded angles are produced by forcing a heated alumnium billet through a die of the proper shape by means of a hydraulic press. 

Sourced from quality producers they are offered in T3 or T3511 tempers but also in other tempers as part of our own branded (AVIATIONEU NEW ERA) product lines. The applicable temper is indicated in the product reference number (SKU). 

Both 2024-T3 aluminum and 2024-T3511 aluminum are variants of the same material. They share alloy composition and many physical properties, but develop different mechanical properties as a result of different processing (please refer to the respective property tables).

These angles are offered in different widths, heights  and thicknesses in inches and cut to order lengths in feet. Appearing sale price is per foot. If manufacturing test reports are required, additional charges are applied per order. For additional information, please refer to our attached Brief Guide on Aluminum Grades & Temper Designations or contact us for price on any unlisted size.

Note: AVIATIONEU NEW ERA metals are supplied free from oil stains, dents, inclusions, scratches, oxide discolorations, corrosion, or other defects. In certain cases, metals are additionally protected with PVC film.