AVIATIONEU NEW ERA aircraft wheel axle jack falls under our product lines of Aircraft MRO Equipment. It is mainly used for tire change in aircraft. It includes a pneumatic hydraulic mode and features a lift weight capability of 50T for use in commercial aircraft like A320 and B737. The cylinder block is made of high-quality manganese steel and the surface from high-quality carbon steel, chromium plated, galvanized and plastic sprayed. The minimum height of the hydraulic cylinder is 245mm and the maximum height is 565mm. With a robust construction ensuring a long service life, versitile use and competitive price, AVIATIONEU NEW ERA aircraft wheel axle jack is an indispensable equipment for any Maintenance, Repair and Overhaul (MRO) facility. For more information and a quotation please contact us.

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 come in different dimesions in inches and cut to order (CTO) lengths in feet (*) and meet several AMS specifications, most common being AMS-S-6758 and AMS- 6348. 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. 

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.

(*) As per vendors' requirements, certain 4130 steel bars/rods are ONLY SOLD in 3 feet increments, i.e. cut lengths can only be set to 3, 6, 9 feet etc. as mentioned in the respectivel product presentations. In this case, appearing prices are per 3 feet length and the Minimum Order Quantity (MOQ) is 3 pieces for each of selected rod/bar. Required cut lengths should be specified at the time of ordering.

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 come in different dimesions in inches and cut to order (CTO) lengths in feet (*) and meet several AMS specifications, most common being AMS-S-6758 and AMS- 6348. 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. 

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.

(*) As per vendors' requirements, certain 4130 steel bars/rods are ONLY SOLD in 3 feet increments, i.e. cut lengths can only be set to 3, 6, 9 feet etc. as mentioned in the respectivel product presentations. In this case, appearing prices are per 3 feet length and the Minimum Order Quantity (MOQ) is 3 pieces for each of selected rod/bar. Required cut lengths should be specified at the time of ordering.

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 come in different dimesions in inches and cut to order (CTO) lengths in feet (*) and meet several AMS specifications, most common being AMS-S-6758 and AMS- 6348. 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. 

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.

(*) As per vendors' requirements, certain 4130 steel bars/rods are ONLY SOLD in 3 feet increments, i.e. cut lengths can only be set to 3, 6, 9 feet etc. as mentioned in the respectivel product presentations. In this case, appearing prices are per 3 feet length and the Minimum Order Quantity (MOQ) is 3 pieces for each of selected rod/bar. Required cut lengths should be specified at the time of ordering.

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)

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.

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 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.

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.

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.

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

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.

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).

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)

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.

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.

Grade 410 is a basic general-purpose hardenable martensitic stainless steel alloy for highly stressed requirements, providing good corrosion resistance. Martensitic stainless steels are fabricated using techniques requiring final heat treatment. These grades are less resistant to corrosion when compared to those of austenitic. Their operating temperatures are often affected by their loss of strength at high temperatures, due to over-tempering and loss of ductility at sub-zero temperatures. Quenching and tempering can harden grade 410 steels while their corrosion resistance can be further enhanced by hardening, tempering and polishing. 

410 is a very common grade used in many industries such as aerospace, power generation, and general industry. Generally used for applications requiring mild corrosion, heat resistance and high strength and ductility. Indicative examples include steam / gas turbine blades and buckets, bushings, valve components, fasteners, nuclear reactor control rod mechanisms, petrochemical equipment and machine parts.

Grade 410 round bars/rods are offered as part of AVIATIONEU NEW ERA product lines. Sourced by quality producers, these bars/rods are available in different diameters and pre cut lengths in inches. They meet AMS -QQ-S-763, AMS -5612, AMS -5613, AMS -2303, ASTM -A276, ASTM -A479 specifications. For additional information, please refer to the supplied documentation or contact us.

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.

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.

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.

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.

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.

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.

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.

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.

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.

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.

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.

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.

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.

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 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.

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.

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. 

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 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. 

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.

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 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.

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.

Stainless steel strips feature high hardness, toughness, corrosion resistance and low maintenance making them suitable in different industries. AVIATIONEU NEW ERA stainless steel strips are offered in strips/strip coils in different grades (201,202,301,304/304L, 309S,310S,316L,316Ti,317L,321,347,444,904L & 2507) in a range of  thicknesses, widths and pre-cut or cut to order lengths meeting application requirements. A brief description of each grade and respective applications is included in the Product Description section.

AVIATIONEU NEW ERA stainless steel strips are sourced from quality producers and they are competitively priced. Unit of measurement for pre-cut strips is each (ea.) while for the cut to order strips can be kilograms or tons as specified by our suppliers. Appearing prices are  per unit of sale. Sea/sea-surface transport to customer destination is most commonly used. Appr. time for shipping: within 3 months from the time of order payment, depending on the ordered quantity. Please refer to the attached documentation of the various offered grades or contact us for additional information.

Incoloy® is a registered trademark of Special Metals Corporation (SMC) for a family of super austenitic stainless steels.They do not have to be heat treated after welding to restore the corrosion resistance. Like other SMC superalloys,  Incoloy® alloys come in different grades (variations) listed in the Product Description and are used in the manufacturing of different products such as pipes, tubes, sheets, strips, plates, round and flat bars, etc. Incoloy® products are mostly chromium-based and mostly nickel-based, and designed for corrosion resistance as well as strength at high temperatures.

AVIATIONEU NEW ERA Inconel® strips are intended for use in different industrial applications. They are offered in strips/strip coils in different Incoloy® variations  in a range of  thicknesses, widths and pre-cut or cut to order lengths meeting application requirements. Sourced from quality producers these strips are competitively priced. Unit of measurement for pre-cut strips is each (ea.) while for the cut to order strips is 1 kilogram (kg) unless otherwise stated. Appearing prices are  per unit of sale. Sea/sea-surface transport to customer destination is most commonly used. Appr. time for shipping: within 3 months from the time of order payment, depending on the ordered quantity. Please refer to any attached documentation  and contact us for additional information/clarifications and quotation.

Inconel® is a registered trademark of Special Metals Corporation (SMC) for a family of austenitic nickel-chromium-based superalloys. Inconel® suitability for extreme pressure and heat environments and corrosion resistance allow its use in most demanding operating conditions. Even compared to stainless steel, Inconel® has an incredibly high tolerance for extreme heat, and doesn’t lose as much tensile strength at 2,000°F as most steel alloys.  Inconel® alloy comes in different grades (variations) such as 600, 601, 617, 625, 686, 690, 693, 718, 725, 751, 783 and others. It also used in the production of pipes, tubes, sheets, strips, plates, round and flat bars, etc. but also in the manufacturing of other products including fittings, flanges or fasteners. Some typical sectors/fields of use of Inconel® alloy include:

Oil and gas extraction industries due to its high temperature resistance and oxidation resistant properties,

Heat treat applications, due to its resistance to extreme temperatures,

Saltwater (Marine) Applications, because of its extraordinary resistance to sodium chloride (salt) at a variety of temperatures,

Jet engines and turbines where they need to withstand extreme temperatures (low or high). At a passenger jet’s standard cruising altitude of 36.000 ft., the average air temperature is -56.3°C (-69.3°F), but the combustion process can exceed temperatures of 1.150°C (2120°F).

AVIATIONEU NEW ERA Inconel® strips are intended for use in different industrial applications. They are offered in strips/strip coils in different Inconel® variations  in a range of  thicknesses, widths and pre-cut or cut to order lengths meeting application requirements. Sourced from quality producers these strips are competitively priced. Unit of measurement for pre-cut strips is each (ea.) while for the cut to order strips is 1 kilogram (kg) unless otherwise stated. Appearing prices are  per unit of sale. Sea/sea-surface transport to customer destination is most commonly used. Appr. time for shipping: within 3 months from the time of order payment, depending on the ordered quantity. Please refer to any attached documentation  and contact us for additional information/clarifications and quotation.

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.

The 15CDV6 (1.7734) grade is a chromium-molybdenum-vanadium (CrMoV) heat treatable low carbon steel, a trully multifunctional material that excels in various areas such as mechanical strength, toughness, machinability, thermal stability, lightweight properties, and compatibility with a wide range of materials. Highly regarded & used in aerospace, motorsports and other industries due to its high tensile and compressive mechanical strength for structural components aimed to endure high stresses, its robustness and resistance to fracture or cracking under various load conditions for applications where safety cannot be compromised.Common uses in aerospace include aircraft chassis and fuselage structures, landing gear components (struts, wheel axles, and others) but also  for bolts, screws, and other fasteners like rivets. Also used for rocket engines, parts for electric motors, racing vehicle frames, pressure vessels, suspensions, or vital components in the nuclear and defense industries. 

The 15CDV6:

- combines a high yield strength (superior to SAE 4130) with good toughness and weldability with very little loss of its properties and without the need for further heat treatment. 

- is  low weight. For similar mechanical performance, it offers a more favorable strength-to-weight ratio than many other steels.

- has excellent machinability. Whether for cutting, forming, or welding, 15CDV6 suitability to various processing methods, results in ease of handling and reduces production costs.

- has excellent thermal stability making this alloy a material of choicel in aerospace, where components are subjected to extreme temperature ranges, from very cold to very hot, without compromising their performance.

- is compatible with other metals and composite materials frequently used in the aerospace industry. This compatibility facilitates its integration into complex systems, making it a preferred choice for engineers and aircraft designers. 

Metal products from 15CDV6 (1.7734) grade alloy steel are now offered in different forms/shapes (bars, sheets/plates, pipes/tubes, strips/coils, wires) for use in aerospace and industrial applications as part of OEM or our own labelled (AVIATIONEU NEW ERA) product lines. Depending on the selected product, they are available in different diameters, thicknesses, widths and pre-cut or cut-to order lengths in Metric system and specifications  (*)  to meet the application requirements. Priced per piece or unit weight (kg or ton for substantial quantities). Please refer to the supplied documentation or send us your RFQ for a quotation.

(*) Indicative Norms/Specifications: DIN WL 1.7734-1 (1982) Aerospace | 15CrMoV6 | AECMA FE-PL63 S / FE-PL1505 | AIR 9160C | LN 668 / MN 1013 (round bars) | ASNA 3108 / DIN 65389 / DIN 65390 (sheets and plates) | TE014 / LN 9369  (seamless tubes).

Machine screws are one of the more widely used products among dozens of standard fastener types. They can be either coarse-threaded or fine-threaded, and are usually available with a wide range of head types. Usually stronger than many other screw types, they are used for fastening metal parts and panels securely together in a range of construction and other applications including aerospace, machinery, vehicles, engines, tool assemblies, electronic devices, and large-scale industrial equipment. 

Sourced from quality producers,  machine screws are offered as part of our own branded (AVIATIONEU NEW ERA) product lines conforming to aerospace/military or industrial standards/specifications. They come in different sizes, head types, materials and thread gradings.

Machine sccrews meeting National Aerospace Standards (NAS), developed and maintained by the US Aerospace Industries Association (AIA), are offered in different series.  

AVIATIONEU NEW ERA AIA NAS 623 Series are aeronautical standard non structural pan head cross recess short thread machine screws. They are made from alloy steels 4140 (UNS G41400)  per MIL-S-5626, 4340 (UNS G43400)  per MIL-S-5000 or 8740 (UNS G87400 per MIL-S-6049. They are cadmium plated per QQ-P-416 Type II, Class 2. Heat treatment 160,000 to 180,000 psi ultimate tensile streangth in accordance with SPEC-MIL-H-6875.They are offered in different thread sizes, grips and lengths in inches and sold in pieces or convenient packs of specified number of screws per pack indicated by the number after the letters "PK" in the product reference number (SKU).

For more information, please refer to the supplied documentation or contact us.

Close tolerance bolts, designed with a greater emphasis on measurement accuracy than other types of bolts, are commonly used in the aerospace manufacturing industry. They are threaded fasteners with a shank and head and a tolerance of just +0.000, -0.0005 inch as an acceptable range of variance. The shank is threaded, thus allowing them to be driven into a threaded hole. They intend to eliminate problems appearing when using traditional bolts which have a greater acceptable range of variance. Close tolerance bolts have closer shank tolerances than that of traditional bolts and fit more securely in threaded holes. For some fastening applications, traditional bolts may suffice. For sensitive fastening applications in which precision is required, close tolerance bolts are typically used. When selecting close tolerance instead of traditional bolts the drive type should be considered. Most close tolerance bolts have a recess within their head that supports a specific bit, such as a Phillips head bit. Regarding their threading, all close tolerance bolts, as well as traditional bolts, have threading. But the way in which the threading is designed may vary. Some bolts have more threading on their shank than others, and some bolts have finer threading than others.

Close tolerance bolts are offered in different materials with high-carbon steel being a common material used in their construction. 

Army & Navy (AN) close tolerance bolts are offered as part of our own labelled (AVIATIONEU NEW ERA) lines of fasteners. They are sourced from quality manufacturers and structured in different series (AN 173/174/175/176/178/180).

The following letters after the basic part numbers specify the material, finish and drilling condition of these bolts.

First Number after AN Basic designates the Diameter. 

"-" for Steel, Cad II plated, no head hole

"C" in place of (-) for Corrosion Resistant Steel (CRES)

"H" in place of (-) or after (C) for bolts with a head hole

"A" In the end of the PN  for bolts with no shank hole

European Standards (EN) and other deliverables are developed in a large number of sectors by the CEN National Standardization Bodies and CENELEC's National Committees (NCs) of the EU and EFTA countries. Together with the European Telecommunications Standards Institute (ETSI) they are the three European Standardisation Organisations operating under the Regulation (EU) No 1025/2012 to produce European harmonised standards in support of EU legislation and policies.

EN 6114 & EN 6115 Standards relate to short thread countersunk & protruding head bolts respectively for aerospace applications. EN6114 & EN 6115 Standard bolts are commonly used on Airbus commercial aircraft platforns such as A320, A330, A350 and A380. Airbus A320/ A330 aicraft commonly use the alloy steel versions of the EN6114 Standard bolts and those of the Titanium series indicated by the V and T surface coding. The Airbus A350 and A380 models incorporate those from INCONEL®  nickel-chromium-based superalloy. Several HLT, HST, NSA, and VL fasteners can be used as alternates to those of EN6114 Standard (see the supplied documentation).

Sourced from various manufacturers in different materials (steel, titanium or INCONEL® alloys), coatings and sizes, the EN 6114 & EN 6115 Standard bolts are offered as OEM parts of their respective suppliers or as part our own labelled (AVIATIONEU NEW ERA) product lines. Different material letter codes in the part number indicate the material used (e.g. " V" and "T" for Titanium or "L" and "M" for Inconel®). They are sold in packs with the number of bolts included in each pack designated after the letters "PK" in the product reference number (SKU). For additional information please refer to our brochure in our Attachment section