National Aerospace Standard (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.

NAS 6603 Series Steel Cadmium Plated Shear Hex Head Machine Bolts are offered as part of our own labelled (AVIATIONEU NEW ERA) lines of  fasteners. Sourced from quality manufacturers, AVIATIONEU NEW ERA NAS6604 series shear hexagon head bolts conform to the respective U.S. National Aerospace Standard of the Aerospace Industries' Association. They have a 10-32 thread and a nominal grip diameter of 0.1900 inch. NAS6603 series forms part of NAS family of bolts (NAS6603 through NAS6610 series) which includes hex head, close tolerance, alloy steel, long thread, self-locking & non-locking bolts. Their shearing feature is used to minimize damage to more critical components within 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. Used in applications where a premium-quality, high strength bolt is necessary. The following letters after the basic part numbers specify the material, finish and drilling condition of these bolts.

No Finish Code for cadmium plated bolts

"C" for chromium plated bolts

"D" for drilled shank bolts

"L" for self-locking bolts

"P" for self-locking bolt with patch type locking element

"H" for bolts with drilled head

More than one code letters may be used in sequence.

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. 

AVIATIONEU NEW ERA NAS860/NAS870 series of machine (non structural) screws (also termed as bolts) are aeronautical standard high strength, close tolerance, short thread, Philips head recess screws.   Both series are made from 8616 alloy steel, heat treated to 160-180 KSI and Cadmium plated per QQ-P-416 Type II. Also offered from 8716 A286 corrosion resistant steel (CRES), heat treated to 160-180 KSI.They are offered in different thread sizes and grip lengths in inches with undrilled or drilled shanks and sold in pieces. Screw size number is after the basic part number (e.g. NAS8602 for size 2 screws). Grip Length in 1/16ths inches after the dash. The following letters are also used:

"D" after the dash number indicates a drilled shank

"A" after the basic part number prefix and the letter "D", if applicable, indicates an aluminum coating

"U" after the basic part number prefix and the letter "D", if applicable, indicates unplated and passivated

 For more information, please refer to the attached reference table or contact us. 

Apart from aerospace & defense, hinges of different types are commonly used in many other industries for cabinets, enclosures or other applications in the automotive, transportation, construction, furniture, marine, food, and others. Types of these hinges include among others continuous (aka piano) and butt hinges, corner, concealed, latching and other hinges depending on the intended application. These industrial hinges are sourced from quality manufacturers and/or their distributors and are marketed and sold  as part of our own labelled (AVIATIONEU NEW ERA) product lines. They are offered in different materials (including steel, aluminum, and stainless steel alloys), various finishes, in inch or metric dimensions depending on their manufacturer and selected product.

AVIATIONEU NEA ERA Continuous & Butt hinges come with their respective corrosion resistance hinge pins and without mounting holes (intended for welding) unless otherwise specified. The hinge pin diameter will vary depending on the open width size, and material the hinge is made from. Their  common materials include steel, aluminum, and stainless steel alloys but other material options are also available. Continuous hinges are typically stocked & sold in 3 ft (915 mm) and 6 ft (1830 mm) hinge lengths but they can be cut to smaller lengths. The length is indicated by the number  after the dash in the product reference code (SKU). For example "-3" denotes a hinge 3 feet 3 (36 inches) long. Sold in pieces.

Manufacturer C of C and material certifications are available upon request for all our supplied hinges. Their requirement must be specified at order placement as additional charges may apply.

Screws, bolts and nuts are standard fastening hardware widely used in a range of applications. 

Internal wrenching (also known as Allen) fasteners are threaded fasteners. Screws and bolts have a drive recess within the head allowing the insertion of an internal wrench for their installation or removal. Allen socket set screws are blind (headless) fasteners with an internal hex drive offered in different styles (regular cap screw and flat and button type) while Allen nuts are cylindrical nuts internally threaded on one side with an Allen socket on the other. These fasteners are produced by different manufacturers and come in different styles, inch or Metric sizes, materials, finishes,  and coarse or fine threadings. They are offered as OEM parts or parts of AVIATIONEU NEW ERA product lines. Sold in pieces or packs of specified number of pieces per pack as designated by the number after the letters "PK" in the product reference code (SKU). 

Internal wrenching fasteners for aerospace applications are designed and intended for use in aircraft construction and repair and conform to Military or Aerospace Standards. Aerospace Industries Association Standard NASM 20004 through 20024 internal wrenching bolts supersede respective part numbers of MS 20004 through 20024 which in turn have superseeded those of older National Aerospace Standard NAS NAS 144 to 158 series. Fabricated from 160-180 ksi high-strength steel they are intended for use in both tension and shear applications. 

Socket screws for aerospace and military uses come in different sizes and meet aerospace/military standards including AN565 (superseded by NASM565), NAS1081, MS18063, MS18064, MS51021, MS51023, MS51029, MS51031, MS51038, MS51045, MS51963, MS51964, MS51965, MS51966. Those of AN565 (NASM565) standard are headless hex and fluted socket set screws while their MS51963 standard counterparts are cup point hex socket set screws.  Both are made of high-quality steel and they are designed to deliver maximum holding pressure Typically used to bind parts onto shafts. Available in cup or cone point styles, in different thread sizes and lengths in inches.

81791 internal wrenching  nuts are self-locking, high-strength, corrosion and oxidation resistant nuts made of nickel-chromium alloy with cadmium plating. These nuts are catalogued and supplied in different sizes as part numbers of TEXTRON AVIATION (separately listed).

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

Anchor nuts (aka nutplates or anchor plates) are terms used interchangeably and relate to stamped sheet metal fasteners with an internally threaded tube and a plate with two clearance holes for rivets. They are used in blind mounted panel applications in aerospace and other industrial sectors where hex nuts cannot be used or an attached nut is required for ease of maintenance. 

Anchor nuts can be Fixed or Floating, the latter being easier to use due to their built-in nut (threaded hole) able to "float" slightly thus providing a convenient connection point for threaded rods, such as bolts, from the backside. In the case of Fixed anchor nuts, the built-in nut is static (i.e. without the capability to “float”) and the threaded rod must be positioned perfectly over the hole. Self-locking anchor nuts are those with a built-in locking mechanism preventing them from loosening over time from vibrations. They are extensively used in aerospace, automotive, and construction industries.

Depending on their intended application, nutplates conform to different military, aerospace, ISO or other industrial standards such as the German DIN, U.S. (ASME & ASTM, IFI, ANSI), British BS, Japanese JIS and others. They are offered as OEM parts under their respective brands or under our own labelled (AVIATIONEU NEW ERA) product lines intended as cost-effective alternatives to the respective OEM products. Listed in accordance with their standard of compliance, Fixed and Floating nutplates come in different materials (such as steel or CRES & finishes),  in single/double lug configurations and Metric ISO οr Unified thread sizes. There is currently no U.S. Military Standard (MS) specification for Metric nutplates.Depending on the selected product and availability, nutplates can be supplied with a dry film lube specified by the letter "L" in the respective part number. Those with countersunk rivet holes are specified by the letter "K" at the end of the part number.

Sourced from quality manufacturers, AVIATIONEU NEW ERA MS21047 series nutplates are fixed self locking elastic insert 2-lug anchor nuts made of cadmium plated steel with nylon insert and plain rivet holes. They replace those of AN366F series and are available in different Unified thread sizes to meet application requirements and replace respective nut plates. Sold in pieces but also in packs where the specified number of nuts per pack is indicated after the letters "PK" in the product reference number (SKU). Appearing prices are always for the units of measurement used each time. Matching rivets are sold separately.

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

A. RAYMOND TINNERMAN® & PALNUT® (aka PAL) of TINNERMAN PALNUT ENGINEERED PRODUCTS, INC. are leading brands in specialty clip-type fasteners including the world's largest selection of spring steel, stainless steel, and plastic engineered fasteners.Their fasteners replace traditional fastening methods with innovative solutions combining aesthetics and functionality. They are quick and easy to install, and do not require mounting tools. 

TINNERMAN®  & PALNUT® equivalent (style) fasteners, corresponding to respective OEM popular part numbers, and other specialty fastening products are sourced from different quality manufacturers and offered as part of our own labelled (AVIATIONEU NEW ERA) product lines (*). Depending on the selected products, they can be supplied in inch or metric systems in different design variations (impression types), materials, finishes and screw sizes to comply with panel thicknesses. Sold in pieces mostly in packs of specified number of fasteners according to the selected part number. The number of pieces per pack is indicated after the letters "PK" in the product SKU. Parts are all in NEW Condition unless otherwise specified and are accompanied by our own and Manufacturer's Certificate of Conformance.

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

(*) TINNERMAN® & & PALNUT® are registered trademarks of A. RAYMOND & CIE and TINNERMAN PALNUT ENGINEERED PRODUCTS, INC. respectively. AVIATIONEU GROUP companies DO NOT manufacture these fasteners. They are sourced from their respective manufacturers and/or authorized distributors.

Extending the range of nutplates (*) complying with different Military Specifications, anchor nuts for industrial (also known as commercial anchor nuts) for non military uses are offered as  part of AVIATIONEU NEW ERA product lines. They are offered in Standard and Miniature versions, different types (fixed or floating, one lug, two lugs, corner, etc.) in both in Metric (M2 - M24 diameters) and Unified thread types (**).

Common materials used are Steel and Carbon Steel Alloys such as 30CrMnSiA high-strength, low-alloy structural steel, 42CrMo4 steel and C1050 heat treated carbon steel , CRES (stainless steel) A-286 alloy, Brass,  Aluminum, INCONEL alloy or other alloys depending on the manufacturer.

Different offered surface finishes include anodizing, brushing, polishing, resin spraying, powder and black oxide coating, rust preventive oil, sandblasting, painting, different platings (laser engraving Zn, blue black Zn, Ni, Cr, Tin, Copper, titanium alloy galvanized, silver plating, electroplating, etc.)

Depending on the the anchor nut type and the manufacturer, the AVIATIONEU NEW ERA industrial anchor nuts meet ISO and different other standards such as the German DIN, U.S. (ASME & ASTM, IFI, ANSI), British BS, Chinese GB, Japanese JIS and others.

Competitively priced, AVIATIONEU NEW ERA industrial nutplates are cost effective alternatives to the respective OEM parts and commonly used in aerospace, automotive, machinery manufacturing and other industries but also in certain military equipment. 

They are sold in pieces but packs are also used where the number of anchor nuts per pack is indicated after the letters "PK" in the product SKU. Appearing prices are always for the used units of measurement each time. Please refer to product specifications or contact us.

(*) Anchor nuts (aka nut plates or anchor plates) are stamped sheet metal fasteners used in blind mounted panel applications, where hex nuts cannot be used or an attached nut is required for ease of maintenance. They are usually riveted to a workpiece and have an internally threaded tube and a plate with two clearance holes for rivets. These terms are used interchangeably to describe the respective fasteners. 

(**) Metric ISO thread used in Europe. Designated by the letter "M" followed by the value of the thread nominal diameter and pitch in millimeters. Unified form thread designations, such as UNC (unified coarse) or UNF (unified fine),have a fixed number of threads per inch with the thread major diameter preceding the designation.

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 labelled (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), come in different types and sizes structured in different series, including:

NAS 1101, 1102, 1189, 1190, 1191, 1635, 1801, 1802, 220, 229, 333,  514,  517, 560, 583, 600, 623 και NAS 662.

The NAS 583 series are non structural machine screws are flush head close tolerance machine screws made of aeronautical 100 deg. alloy steel and cadmium plated.  Offered in different thread sizes and lengths in inches as OEM parts of respective manufacturers or as parts of AVIATIONEU NEW ERA product lines. Sold mostly in packs with number of pieces per pack specified after the letters "PK" in the product reference number (SKU). For more information, please refer to the supplied documentation or contact us. 

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 labelled (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), come in different types and sizes structured in different series, including:

NAS 1101, 1102, 1189, 1190, 1191, 1635, 1801, 1802, 220, 229, 333,  514,  517, 560, 583, 600, 623 και NAS 662.

The NAS 584 series are non structural machine screws are flush head close tolerance machine screws made of aeronautical 100 deg. alloy steel and cadmium plated.  Offered in different thread sizes and lengths in inches as OEM parts of respective manufacturers or as parts of AVIATIONEU NEW ERA product lines. Sold mostly in packs with number of pieces per pack specified after the letters "PK" in the product reference number (SKU). For more information, please refer to the supplied documentation or contact us. 

Nuts are extensively used in a wide range of aerospace and industrial applications. Self-locking nuts are those containing a locking feature as an integral part. 

Hexagon self-locking nuts of both low (thin pattern) and regular height (pattern) used in aerospace and defense applications comform to different Standards and they are designed for use in high temp installations (up to 250°F or 1200°F for those from silver-plated stainless steel). Low height self-locking nuts complied with Army & Navy AN 364 superseded by Mil Standard MS 20364 which was in turn superseded by the newer Mil Standard MS 21083. Similarly, Army & Navy AN 365 Standard relating to regular height nuts was superseded by Mil Standard MS 20365 and this in turn by MS21044. Furthermore, MS Standards have been replaced by NASM National Aerospace Standards with their part identification numbers remaining the same. For example, nuts with PNs MS21083 and NASM21083 are identical.

Regular height NASM/MS 21044 self-locking nuts and their low-height NASM/MS 21083 counterparts replace the superseeded MS 20365  / AN 365 & MS 20364 / AN 364 for respective materials and sizes but their older Standard part numbers (although cancelled) are still commonly used in the market. Sourced from quality manufacturers, these nuts are offered as part of own labelled (AVIATIONEU NEW ERA) product lines in different materials and finishes (e.g. cadmium plated alloy steel, corrosion resistant steel passivated,copper cadmium plated, aluminum alloy anodized), and different dimensions and thread sizes in inches. Cadmium plated nuts are furnished to military specifications while stainless steel nuts are supplied to military specification and commercial grade. These nuts come either with all metal or non metallic inserts (often termed as fiberlock or elastic stop to create friction and prevent loosening from vibration) designated by the letters "C" and "A" respectively after the dash number. No letter indicates an all metal or a non metallic insert nut. They are reliable and economical fastening devices with their inserts providing a friction grip on the threads of the bolt  holdsing it securely.

The following letters after the dash in their part number indicate their materials and finishes:

"B" Copper alloy - Cadmium plated

"C" Corrosion resistant steel (stainless steel) - passivated

"D" Aluminum alloy - Anodised

"N" Steel alloy - Cadmium plated

For example, MS21044C3 is a corrosion resistance steel self-locking nut with a thread size of 10-32, while MS21044N3 is a steel alloy nut with the same thread size.

Sold in pieces or packs. 

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

The NAS1630 Series screws are pan head, short thread, offset cruciform machine screws offered as part of our own branded (AVIATIONEU NEW ERA) product lines. These screws use PHILLIPS Screw-Torq-Set® drive system with significant benefits outlined below. Sourced from quality manufacturers they are offered in alloy steel or corrosion resistant steel (CRES) and different thread sizes and legths in inches. Sold in packs each containing a specified number of screws. The number of screws in each pack is specified after the letters "PK" in the product reference code (SKU).

PHILLIPS Screw-Torq-Set® Drive System Features & Benefits

Offset cruciform shape with straight wing walls for greater torque transfer.

Removal walls larger than drive walls. Facilitates disassembly without drill outs.

Specific driver for each diameter fastener. Assures optimum torque for each size and strong head configuration.

Compatible with standard PHILLIPS ACR® ribbed TORQ-SET® drivers. Allows use of ribbed tools with standard screws

PSC quality inspections. Assures global system quality and compatibility.

AVIATIONEU NEW ERA Screw Extraction Kit is intended for use as a removal tool of stuck or broken screws, bolts or studs.

The kit consists of a 6-piece standard screwdriver set and a T Type steel single sided ratchet wrench adjustable to handle fasteners of M3 to M8 sizes. 

It is a high quality, versatile, convenient, efficient and long service life kit that can be used for home and professional applications in bikes, cars, electronics, household appliances, mobile repairs and other uses.

The 6-piece standard screwdriver set and the ratchet wrench can be bought separately although the kit provides a cost effective solution.

MS20604 and MS20605 Standard pull-thru rivets are unique blind rivets typically used in nut plate applications. MS20604 and MS20605 series blind rivets are superseded by those of NASM20604 and NASM20605 respectively.They are both non structural blind rivets with universal head (MS20604) or 100 deg. flush head (MS20605). These rivets are ideal in circumstances with very limited clearance while allowing for a secure set on both sides of the application. The symmetrical insertion allows for access and installation on either side while retaining its blind rivet capacity of one-sided installation. NASM/MS 20604 rivets come with a Universal Head, allowing for ease of installation while retaining strength and security. 

Sourced from quality manufacturers, NASM20604/MS20604 and NASM20605/MS20605 blind rivets are offered either as part of our own label (AVIATIONEU NEW ERA) product lines or as OEM parts of PCC CHERRY® AEROSPACE and other manufacturers (separately listed). They are available in different mil-spec approved materials, such as 2117-T4 grade Aluminum or 5056 Grade Aluminum, finishes and sizes. They are sold in packs of specified number of rivets per pack indicated after the letters "PK" in the product reference code (SKU).

Specialty fasteners such as eye bolts, rod ends, clevis rod ends, shaped bolts, anchors and others are offered as part of our own branded (AVIATIONEU NEW ERA) product lines for use in different aerospace and industrial applications.

Eye bolts are threaded bolts with a loop or eye at one end. They come in different types and have a shank for anchoring to structures or equipment and a ring at the top for attaching rope, hooks, or other hardware. They're used to anchor a cable, rope or chain.  

Rod ends are threaded swing bolts. They connect and support loads and allow motion control and hinge movements. They are used in an array of applications: steering, tensioning, and controlling movement at pivot points.

Clevis rod ends are either machined or folded pieces molded into a clevis. At its base, the end is fitted with a hole. Here, a rod is attached. The hole is typically threaded in machined pieces. They are frequently used to secure loads in a variety of applications including automobiles, aircraft, boats, machinery, construction equipment and others.

Sourced from quality producers, AVIATIONEU NEW ERA eyebolts & rod ends are made from different materials, including carbon steel, steel alloys and stainless steel, and can be furnished in different inch or metric sizes,coatings/finishes in different specifications. Sold in pieces or in packs of specified fasteners per pack indicated by the letters "PK" after the product reference number (SKU).

For additional information please refer to the Product Description section and the supplied documentation.

National Aerospace Standards (NAS) are voluntary standards developed and maintained by committees and working groups of subject matter experts from member companies of the U.S. Aerospace Industries Association (AIA).

These standards have served as the foundation for the development of aircraft, spacecraft, watercraft, ground vehicles, machinery, and electronics.

NAS parts are most well-known for state-of-the-art, high-strength, precision fasteners, electrical connectors, splices and terminations, rod end bearings, and many other types of hardware and components. The NA prefix relates to metric standards. 

NA-0027/NA-0028 Series Metric Self-Locking Floating Two-Lug Nutplates (*) form part of NAS high-strength, precision fasteners. Sourced from quality manufacturers they are offered as part of our own labelled (AVIATIONEU NEW ERA) product lines in different materials, finishes, thread sizes and dimensions in Metric system. Usually sold in pieces but packs are also used where the number of anchor nuts per pack is indicated after the letters "PK" in the product SKU. Appearing prices are always for the used units of measurement each time. For additional information, please refer to the product specifications or contact us.

(*) also termed as plate nuts, anchor nuts or anchor plates. These terms are used interchangeably to describe the respective fasteners. 

The 12LiS Cordless Screw Gun from AVIATIONEU NEW ERA product line is an irreplaceable assistant both in life, and on production. This easy, compact screw gun with a rated voltage of 12 V features:

- a speed of 0-350/1200 rpm, 

- boss size: 10 mm, 

- torque 15 nanometers, 

- 2 accumulators with capacity 2 Ach providing long time to perform required works, 

- battery built-in indicators to show when the accumulator needs to be charged

- rubberized handles. 

- one year manufacturer's guarantee

AVIATIONEU NEW ERA 12LiS Cordless Screw Gun is delivered in a convenient plastic case, with a set of 2 Li-ion accumulators, the accumulator charging device and a trial nozzle. 

AVIATIONEU NEW ERA pneumatic drills provide cost-effective solutions for drilling, boring or other works on different materials to cover the needs of a wide range of applications in aviation and other industrial sectors.They are robust, durable, powerful  and reliable tools, offered in pistol or other types, in various rotation speeds and drilling diameters capacities. Depending on the model, AVIATIONEU NEW ERA pneumatic drills are intended for use with high or medium hardness materials as well as for specific uses.  Some drills are also suitable  for working on hard-to-reach surfaces and confined spaces. Please refer to the technical specifications of individual drill or contact us for additional information.

AVIATIONEU NEW ERA drill type pneumatic sanders provide cost-effective solutions for stripping and grinding of metals in a wide range of applications. They are robust, durable, powerful  and reliable tools, offered as pistol (PM-33-140) or direct sanders (PMZ-31-250, MP-006,  PMZ-01-17000) and they can operate with different sander attachments such as abrasive wheels, burrs, metal brushes and others.

The PM-33-140 pistol sander was developed for the aerospace industry and is designed to work on high-strength steels, cast iron and non-ferrous metals.

The PMZ-31-250 direct sander has been designed for stripping and grinding of metal parts during assembly and repair works.  

The MP-006 direct sander can be used for processing and grinding of molds and dies as well as for cleaning and surface finishing of parts and welds. This lightweight comfortable pneumatic direct sander with rotation speed 30000 rpm provides high quality processing. 

The PMZ-01-17000 direct sander is intended for use in cleaning metal surfaces, for the treatment of weld seams and edges while it can also be used for the processing of solid wood and plastic. This easy and compact direct pneumatic sander is useful for working on hard-to-reach surfaces and confined spaces.

An aircraft elevator removal installation sling is the supporting frame which, together with the car platform, guide shoes, elevator car safety, hoisting ropes (or sheaves) and/or associated equipment, are used to as to remove or install the elevator from an aircraft. AVIATIONEU NEW ERA slings are offered as part of our own label product portfolio of Aircraft MRO Equipment. The PN: -C55001-1 elevator sling is intended for use on BOEING  737-300 thru -500 and 737-200 series airplanes with composite elevators. For more information and a quotation please contact us.

AVIATIONEU NEW ERA frames for storage of aircraft engine pylons are offered as part of our own label product portfolio of Aircraft MRO Equipment and they are indispensable equipment for any Maintenance, Repair and Overhaul (MRO) facility. 

Different pylon storage frames are offered corresponding to diffent aircraft engines. The PN: 460007240 98A54003003000 frame is intended for use to handle and store pylons of GENERAL ELECTRIC (GE) and PRATT & WHITTNEY (PW) aircraft engines.  For more information and a quotation please contact us.

AVIATIONEU NEW ERA aircraft tolleys are offered as part of our own label product portfolio of Aircraft MRO Equipment and they are indispensable equipment for any Maintenance, Repair and Overhaul (MRO) facility. 

Aircraft Build Trolley PN: 460007240 is intended for use in AIRBUS A320 Series aircraft to handle and support the MLG shock absorber after it has been removal. For more information and a quotation please contact us.

The landing gears and doors used in commercial airplanes are moved by a set of actuating cylinders. For each door, a cylinder opens and closes the door. Landing gear door locks offered as  part of our own label  AVIATIONEU NEW ERA product portfolio of Aircraft MRO Equipment are high strength steel clamping tools which retain the door actuator in closed position. They fit around the actuator and secure two tension rods to the door Iinkage. For more information and a quotation please contact us.

Aircraft waste leak testing equipment are used to plug the waste system and provide leak detection. AVIATIONEU NEW ERA aircraft waste leak testing equipment are offered as  part of our own label product portfolio of Aircraft MRO Equipment. For more information and a quotation please contact us.

All aircraft develop fuel leaks at one time or another which can ground an aircraft for unspecified time intervals. Fuel leaks are considered to be one of the most time consuming maintenance tasks required on an aircraft. Fuel line leak testers are intended to check leakages in fuel lines and assist maintenance personnel of Maintenance, Repair and Overhaul (MRO) facilities to detect and repair them. AVIATIONEU NEW ERA fuel line leak testers are offered as  part of our own label product portfolio of Aircraft MRO Equipment. For more information and a quotation please contact us.

AVIATIONEU NEW ERA engine/IDG oil servicing carts are offered as part of our own label product portfolio of Aircraft MRO Equipment and they are indispensable equipment for any Maintenance, Repair and Overhaul (MRO) facility. These carts are intended for use as fillers of oil in the aircraft engine and the Integrated Drive Generator system, or IDG, a key power system found on aircraft that controls all of the engine hydraulic systems. For more information and a quotation please contact us.

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.

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

For additional information, please contact us.

Notes: 

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

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.

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.