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.

AN hex head bolts in different series are offered under AVIATIONEU NEW ERA product series. Sourced from quality vendors, these bolts are manufactured to the US Army-Navy (AN) standard, predecessor to Mil-Spec (MS), superseded by the National Aerospace Standard (NAS). Commonly used in aviation for either tensile/shear load applications. Made from high-strength type 4037 or 8740 alloy steel or 431 Stainless Steel (CRES) and cadmium plated for superior corrosion resistance (compared to commercial grade zinc plated bolts) they are offered with shank drilled for cotter pin or undrilled for stop nut application, and with a drilled head for safety wire or without. Minimum Tensile Strength (Steel and CRES) - 125,000psi. The length of AN aircraft bolts is measured from under the head to the end of the shank. The "grip" is the unthreaded portion of the shank. Threads are pressed into the steel, not cut, thus maintaining strength throughout the entire shank. The surface under the head of AN bolts is designed to be a bearing surface to reduce non-uniform stress as the bolt is torqued thus reducing premature fatigue. The following letters are used in the product part  numbers.

"A" after the dash number for bolts with undrilled shank

"C"  for bolts made of 431 Stainless Steel (CRES)

"H" after the AN number for bolts with drilled head (eg. AN8H-15)

 AN3 through AN20 Series bolts are superseded by NASM3 through 20 Series. The part numbers in both series have not been changed. 

Specification Details:

AN3 through AN20 (REV. 12), Military Specification Sheet: Bolt -Machine, Aircraft [superseded by NASM3 through 20]. This specification covers aircraft machine bolts part numbers, AN3, AN4, AN5, AN6, AN7, AN8, AN9, AN10, AN14, AN16, AN17, AN18, and AN20. AN3 THRU AN20  is canceled and superseded by NASM3 THRU NASM20. The Part Identification Number (PIN) for AN3 THRU AN20 REV. 12 and the part number for NASM3 THRU NASM20 are identical. The part numbers have not been changed.

AL2024 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. It comes in different tempers, O (Annealed)without heat treatment or T (heat treated). Since corrosion resistance is relatively low, 2024 is commonly used with an anodized finish or in clad form (specified as CLAD or ALCLAD) with a thin surface layer of high purity aluminum metallurgically bonded to the aluminium alloy core material.

AL2024 bars/rods are offered as part of our own branded (AVIATIONEU NEW ERA) product lines along with those from other aluminum and steel alloys (e.g. AL5052, AL6061, AL7050, AL7075, ST4130, ST4140 etc.). Like other AL2024 products these bars/rods can be used in an extensive list of applications in aerospace, automotive and many other industrial sectors such as aircraft structural components, aircraft fittings, hardware, truck wheels and parts for the transportation industry.

AVIATIONEU NEW ERA 2024-T351 aluminum rectangular bars/rods are sourced from quality producers and offered either in different dimensions and pre-cut lengths in inches or cut to order (CTO) lengths in feet  to meet application requirements. The pre-cut bars/rods are cold finished and comply with ASTM -B211, AMS -4120 & AMS -QQ-A-225/6 specifications while those with cut to order lengths meet AMS-OQ-A-225/5, AMS 4120, ASTM B211 and UNS A92024 specifications.  Appearing prices are per piece for pre-cut bars/rods and per foot for those cut to order. 

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.

AN818 Series of coupling nuts are offered as part of our own (AVIATIONEU NEW ERA) portfolio of fittings. Sourced from quality producers these fittings can be furnished in steel, aluminum or stainless steel and in different outer tube diameters and sizes in inches. 

Aluminum and Stainless Steel fittings are designated by the letters "D" and "J" respectively after the suffix number of the product reference number (SKU).

AL2024 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. It comes in different tempers (O without heat treatment or T with heat treatment). 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. 

AL2024 bars/rods are offered as part of our own branded (AVIATIONEU NEW ERA) product lines along with those from other aluminum and steel alloys (e.g. AL5052, AL6061, AL7050, AL7075, ST4130, ST4140 etc.). Like other AL2024 products these bars/rods can be used in an extensive list of applications in aerospace, automotive and many other industrial sectors.

AVIATIONEU NEW ERA 2024-T351 aluminum round bars/rods are sourced from quality producers. They are heat treated, cold finished and available in different diameters and pre-cut lengths in inches to meet application requirements.  They comply with ASTM -B211, AMS -4120 & AMS -QQ-A-225/6 specifications. For additional information, please refer to our Brief Guide on Aluminum Grades & Temper Designations,  the individual product presentations or contact us.

These AVIATIONEU NEW ERA hexagon locking nuts comform with ASTM A194 standard specification for carbon, alloy and stainless steel nuts used in high pressure, temperature or other special-purpose applications. They can be indicatively used in the process industries, such as petroleum and chemicals for pressure vessels, valves, flanges, and fittings. Sourced by certified manufacturers these nuts are competitively priced and offered in metric (M3 - M36 diameter) or inch (3/16" - 1.1/2") sizes, different thread types and grade range to meet respective design, service conditions, mechanical properties, and high temperature requirements. Please refer to ASTM A194  specification table for additional information. Sold in packs of 100 pcs each.  Appearing price is for reference only per pack. Please contact us for a quotation.

NAS1922/NAS1924 series clamps are light-weight, aircraft application clamps from 300-series stainless steel available with either a 1/4" round slotted screw or a 1/4" slotted hex-head screw. 

NAS1922/NAS1924 series clamps are included as part of our own branded (AVIATIONEU NEW ERA) product lines. They are available in different sizes (NAS1924 clamps are available in sizes 48 & above). Both screw styles can be supplied with optional lock wire hole for tamper resistance. NAS1922 series clamps are sold in increments of 100 pieces with Minimum Order Quantity 100 pieces. Appearing price is per piece. Black Oxide coated band versions (designated by the letter "L" in the part number) are also offered for increased wear resistance.

The following designators in the product reference number (SKU) indicate the different versions:

-1 Clamp with round slotted screw

-3 Clamp with slotted hex-head screw

-1H Clamp with round slotted screw & lock wire hole

-3H Clamp with slotted hex-head screw & lock wire hole

Please refer to the attached documentation of the effective diameter range for different part numbers.

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. NAS Standard Machine Screws meet aerospace standards and come in different types and sizes structured in different series including NAS1101, NAS1102, NAS1189, NAS1190, NAS1191, NAS1635, NAS1801, NAS1802, NAS220, NAS229, NAS333, NAS514, NAS517, NAS560, NAS583, NAS600, NAS623 and NAS662.

AVIATIONEU NEW ERA NAS333/NAS334 series of machine (non structural) screws (also termed as bolts) are aeronautical standard 100 Deg. standard flush head, shear close tolerance screws. They are made from alloy steel per MIL-S-6049 with a Cadmium finish per QQ-P-416 Type II. They are both offered in different thread sizes, grips and lengths in inches and sold in pieces. CPA indicates a plated Phillips recess. The length and grip of the screw are indicated by numbers after the last dash in the product part number. For more information, please refer to the supplied documentation or contact us. 

NAS machine bolts are commonly used in aircraft, space shuttles, military vehicles, drones, and other high-performance applications. They are offered in different series to meet application requirements. NAS6203 through NAS6210 series include hex head, close tolerance, alloy steel, short thread, self-locking & non-locking bolts.

Sourced from quality producers, NAS6203 through NAS6210 series are offered as part of our own branded (AVIATIONEU NEW ERA) product lines. These fine-threaded, dimpled-head hex bolts have a minimum tensile strength of 160,000 psi and a minimum shear strength of 95,000 psi. Thread length is consistent within each diameter (1103/6203 series have a shorter thread), and grips are available in 1/16” increments beginning at 1/16”. Used in applications where a premium-quality, high strength bolt is necessary. They come in different nominal diameters: NAS6203: 3/16 in. (0.1875"), NAS6204: 1/4 in. (0.25"), NAS6205: 5/16 in. (0.3125"), NAS6206: 3/8 in. (0.375"), NAS6208: 1/2 in. (0.500"), NAS6210: 5/8 in. (0.625").

NAS6208 series shear hexagon head bolts with a 1/2-20" thread supercede NAS1108 high strength bolts. Their shearing feature is used to minimize damage to critical components of the application. They are made from alloy steel with cadmium or chromium finishes and offered in different grips and lengths in inches with undrilled or drilled head and/or shank. They are sold in pieces.

The following letters after the basic part numbers specify the material, finish and drilling condition of these bolts. More than one code letters may be used in sequence.

No Finish Code for cadmium plated bolts

"C" for chromium plated bolts

"L" for self-locking bolts

Grip Dash Number indicating grip in .0625 increments. The following letters after this number indicate:

"D"/"H" drilled thread/ drilled head

"X"/"Y" replacement oversized repair bolts 

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

National Aerospace Standard (NAS) bolts come in a large variance of lengths, thread types, head type, and materials. NAS bolts are suitable for high strength applications. They are the same as Army-Navy (AN) bolts, except they may be either raised or recessed.

NAS bolts are offered as part of our own branded (AVIATIONEU NEW ERA) product lines. They are sourced from quality producers and structured in different series. 

AVIATIONEU NEW ERA NAS428 series of machine (non structural) bolts are fully threaded, crowned hexagon head bolts made from cadmium plated steel or corrosion resistant steel (CRES). These bolts are offered with drilled or undrilled head or thread in different thread sizes, diameters and lengths in inches and sold in pieces. The number after NAS428 ( - ) denotes the thread size in 1/16th inch increments.The number after the last dash ( - ) is the overall length under the head. If this number is a single digit it is 1/8 of an inch. If it is a two digit number, the first is whole inches, the second is additional 1/8ths. For more 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 applications requiring high strength to weight ratio, as well as good fatigue resistance, weldablility and average machinability. It comes in different tempers (O without heat treatment or T with heat treatment).

AL2024 bars/rods are offered as part of our own branded (AVIATIONEU NEW ERA) product lines along with those from other aluminum and steel alloys (e.g. AL5052, AL6061, AL7050, AL7075, ST4130, ST4140 etc.). They come in different cross sections such as round, rectangular,hexagonal or square. Like other AL2024 products, these bars/rods can be used in an extensive list of applications in aerospace, automotive and many other industrial sectors.

AVIATIONEU NEW ERA heat treated aluminum hexagonal bars from 2024 alloy are sourced from quality producers. They are offered in T3/T4/T6/T651 tempers for use in a range of aviation and industrial applications, consisting a cost effective solution when large quantities are demanded. They comply with ASTM specifications and they are available for cut to order in different dimensions and surface finishes. 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.

Clevis pins are used as a quick and secure fastener in place of bolts and rivets. Clevis pins can be partially threaded or unthreaded. Unthreaded Clevis pins have a domed head at one end and a cross-hole at the other end. A Clevis pin is inserted through the holes at the pronged ends of a Clevis and is kept in place by a cotter pin. Threaded Clevis pins are partially threaded on one end with a formed head on the other.

MS20392 series Clevis pins are straight, headed pins with a drilled shank. They supersede those of AN392 to AN396 series and those of AN400, AN402, AN404, and AN406 series. MS20392 series Clevis pins are produced in different materials (steel alloy, corrosion resistant steel (CRES), titanium alloy) and surface finishes (cadmium plated, chrome plated, titanium alloy - aluminum coated) with a drilled hole for cotter pin. The following letters in the part number specify materials and finishes:

“C”  Steel alloy, 4037 4130 8630 or 8740 cadmium plated

“S”  Steel alloy, 8740 cadmium plated

“R” Corrosion resistant steel, PH13-8Mo chrome plated

“P” Corrosion resistant steel, PH13-8Mo cleaned descaled and passivated

“A” Titanium alloy Ti-6AI-4V, aluminum coated and lubricated with solid film lubricant

“T” Titanium alloy, Ti-6AI-4V, no finish

MS20392 series Clevis pins are offered as part of our own branded (AVIATIONEU NEW ERA) product lines in different materials, head, shank diameters and effective lengths. They are used with clevis forks and in secondary controls which are not subjected to continuous operation. For more information, please refer to the supplied documentation or contact us.

AVIATIONEU NEW ERA ASTM A193 Grade B6 Series stainless steel stud bolts are manufactured from the ferritic grade AISI 410 stainless steel and can be heat-treated and machined to minimum of 110-ksi or 760 Mpa tensile strength. Like other fasteners in this seies, apart from their high tensile strength, they exhibit excellent resistance to corrosion, durability as well as a long functional work life. They can be used in different applications in industries that demand high tensile strength and corrosion resistance. Sourced by certified manufacturers they are competively priced and offered in different diameters and lengths. Sold by the piece (pc.) in increments of 10 pieces with Minimum Order Quantity (MOQ) 100 pieces. Appearing price is for reference only and differentiates based on wanted bolt sizes. Please contact us for a quotation.

AVIATIONEU NEW ERA ASTM A324 Grade 10.9 Series high tensile hexagonal head threaded bolts are produced from medium carbon steel, medium carbon steel alloy and low carbon boron steel with heat treatment by both quenching and tempering.  They meet ASTM A324 Grade BD and SAE J429 standards. These bolds feature high tensile strength and good wear resistance and are used in automotive applications and for bolting large and forged parts. 

Nominal Tensile Strength: 1.000 Megapascal (MPa) or 1.000 N/sqr. mm , Yield Stress: 900 Megapascal (MPa) or 900 N/sqr. mm 

They are offered in different finishes (zinc plated, plain or hot dip galvanised) and different standard, coarse and fine thread sizes (diameter M20 to M100 mm / 3/4" to 3.1/2").  Sold by the piece (pc.) in increments of 10 pieces with Minimum Order Quantity (MOQ) 100 pieces. Appearing price is for reference only and differentiates based on wanted bolt sizes. Please contact us for a 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.

The AL2024 aluminum alloy (with copper as the primary alloying element) is often referred to as aerospace grade aluminum as it is often 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, also commonly used in the aerospace industry.

AL2024 aluminum alloy sheets are offered as part of AVIATIONEU NEW ERA product lines. They 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 (*). Sourced from quality producers, AVIATIONEU NEW ERA heat treated AL2024 alloy aluminum sheets are mostly 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 and quotation.

(*) 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 the Temper Designation System.

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.

Structural screws are made of alloy steel, are properly heat treated, and can be used as structural bolts. Those commonly used in aircraft applications are manufactured to aerospace/military standards/specifications. They are offered as part of our own branded (AVIATIONEU NEW ERA) product lines in different materials and finishes, structured in different series based on the standard of their conformance.

AVIATIONEU NEW ERA MS27039 Series structural screws are pan head cross recessed screws equivalent to those of NAS 220 Series. Other structural screws of NAS204 through NAS235 and AN509/AN525 series are also available (see individual product presentations). MS27039 Series screws are fabricated from alloy steel and cadmium plated per specification QQ-P-416A, Type II, Class 3 or Stainless Steel unplated  to MIL-S-6050 or MIL-8695 specifications (designated by the letter "C" in the product part number after MS27039 and before the size number). These screws have 125,000 to 145,000 psi tensile strength. Sourced from quality suppliers, they are offered in different thread sizes and lengths in inches and sold in pieces. For more 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, 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.

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.