Titanium fasteners are best known for their strength,  lightweight, and corrosion resistance. They feature an excellent strength to weight ratio and significant mechanical properties but perhaps their most notable attribute is their superior corrosion resistance to salt water / seawater operating conditions. Titanium fasteners are used in aerospace, automotive and motorsports but also in many other industries including chlor alkali, marine, off-shore oil & gas, desalination, medical, and pulp and paper. They come in different types (like bolts, screws and nuts), sizes, titanium grades and standards/specifications (e.g. ANSI/ASME, DIN/ISO, ASTM, ASME, MIL specifications etc.) to meet application requirements. Compared to respective fasteners made of steel and aluminum, as a rule of thumb, titanium fasteners are about half the weight of their steel counterparts while aluminum fasteners are about half the weight of titanium ones.

Sourced from quality producers, a wide range of titanium fasteners are offered as part of AVIATIONEU NEW ERA product lines (please refer to the individual product presentations). 

AVIATIONEU NEW ERA Titanium nuts are available in both inch and metric systems. Their typicals uses include aerospace, marine, motorsports and many other applications. Manufactured from 6AL-4V grade titanium, CNC machined, heat treated with hexagonal heads and rolled threads these nuts come in diffrent types including locking and flange nuts(*), sizes, thread pitches, flange diameters and lengths. They are sold in pieces. For more information or unlisted fasteners please contact us.

(*) Appearing dimensions for Flange Nuts: Hex Size, Flange Diameter, Height (Hex or Total).

Titanium fasteners are best known for their strength,  lightweight, and corrosion resistance. They feature an excellent strength to weight ratio and significant mechanical properties but perhaps their most notable attribute is their superior corrosion resistance to salt water / seawater operating conditions. Titanium fasteners are used in aerospace, automotive and motorsports but also in many other industries including chlor alkali, marine, off-shore oil & gas, desalination, medical, and pulp and paper. They come in different types (like bolts, screws and nuts), sizes, titanium grades and standards/specifications (e.g. ANSI/ASME, DIN/ISO, ASTM, ASME, MIL specifications etc.)  to meet application requirements. 

Compared to respective fasteners made of steel and aluminum, as a rule of thumb, titanium fasteners are about half the weight of their steel counterparts while aluminum fasteners are about half the weight of titanium ones.

Sourced from quality producers, a wide range of titanium fasteners are offered as part of AVIATIONEU NEW ERA product lines (please refer to the individual product presentations). 

AVIATIONEU NEW ERA Titanium nuts are available in both inch and metric systems. Their typicals uses include aerospace, marine, motorsports and many other applications. Manufactured from aerospace grade titanium, CNC machined, heat treated with hexagonal heads and rolled threads these nuts come in diffrent types including locking and flange nuts, sizes, thread pitches, flange diameters and lengths. They are sold in pieces. For more information or unlisted fasteners please 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 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. Countersunk screws allow the head of the screw to sit flush with or below the surface of the surrounding material. They may also be used to remove the burr left from a drilling or tapping operation thereby improving the finish of the product and removing any hazardous sharp edges.

AVIATIONEU NEW ERA MS35206 and MS35207 series of machine (non structural) screws are mil spec pan head cross recessed (Phillips) screws, manufactured from carbon steel and are cadmium plated to specification QQ-P-416, Type 2, Class 3. MS35206 series machine screws feature 60,000 psi min. tensile strength and can be used as replacements for AN526 truss head & AN515 round head screws. MS35207 series machine screws are fine threaded have a minimum tensile strength of 55,000 psi and replace the AN507R series. Both MS35206 and MS35207 series machine screws are offered in different diameters, thread sizes and lengths in inches and they are sold in pieces. For more information, please refer to the individual product presentations, the supplied documentation or contact us.

Cotter pins are used to secure bolts, screws, nuts, and pins. Military standard MS24665 split cotter pins are made from cadmium plated steel, replacing those of AN380 series or passivated corrosion resistant steel (CRES), replacing those of AN381 series. The CRES cotter pins are more resistant to corrosion and also used where heatresisting attributes are desired, such as forward of firewall or  in locations where nonmagnetic material is required. Regardless of their shape or material, all cotter pins serve the same general purpose - safetying. MS24665 split cotter pins are superseded by respective part numbers of NASM24665 series.

MS24665 Series split cotter pins are offered as part of our own branded (AVIATIONEU NEW ERA) product lines in cadmium plated steel or passivated corrosion resistant steel and in different diameters and lengths. Sold in pieces. 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 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. Countersunk screws allow the head of the screw to sit flush with or below the surface of the surrounding material. They may also be used to remove the burr left from a drilling or tapping operation thereby improving the finish of the product and removing any hazardous sharp edges.

AVIATIONEU NEW ERA MS35206 and MS35207 series of machine (non structural) screws are mil spec pan head cross recessed (Phillips) screws, manufactured from carbon steel and are cadmium plated to specification QQ-P-416, Type 2, Class 3. MS35206 series machine screws feature 60,000 psi min. tensile strength and can be used as replacements for AN526 truss head & AN515 round head screws. MS35207 series machine screws are fine threaded have a minimum tensile strength of 55,000 psi and replace the AN507R series. Both MS35206 and MS35207 series machine screws are offered in different diameters, thread sizes and lengths in inches and they are sold in pieces. For more information, please refer to the individual product presentations, the supplied documentation or contact us.

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 structured in different series based on the standard of their conformance. Some of the screws commonly used include NAS204 through NAS235 and AN509/AN525 series. 

MS24694 Series structural screws have a 100° countersunk Phillips head. They replace the respective AN509 series structural screws of materials and finishes. Minimum tensile strength for steel is 125,000 psi. They are fabricated from alloy steel and cadmium plated per specification QQ-P-416A, Type II, Class 3 or 300 Series Stainless Steel unplated designated by the letters "S" and "C" respectively in the product part number after MS24694 and before the size number.

Sourced from quality suppliers, AVIATIONEU NEW ERA MS24694 series structural screws are offered in different thread sizes and lengths in inches and sold in pieces or packs of specified number of screws designated after the letters "PK" in the product reference number (SKU). For more information, please refer to the individual product presentations, the supplied documentation or contact us.

The AN363 series regular height all-metal stop nuts are similar to those of MS21042 series except that MS21042 nuts are shorter than the AN363 but develop the same tensile strength. The AN363 series nuts are fabricated from carbon steel & cadmium plated as per specification QQ-P-416C or stainless steel, in which case the letter "C" is included after the series number (e.g. AN363 cadmium plated steel, AN363C stainless steel). Both are designed for use in high temp installations (AN363 up to 450°F, AN363C up to 800°F).  The AN363/ AN363C series nuts have been replaced by those of MS21045/MS21046C respectively which in turn are superseded by NASM21045/NASM21046C.  The Part Identification Number (PIN) for MS21045/MS21046C  and the part number for NASM21045/NASM21046C nuts are identical. The part numbers have not been changed (eg. AN363-1032 to MS21045-3 to NASM21045-3).

Sourced from quality producers, MS21045/MS21046C all-metal stop nuts are offered as part of AVIATIONEU NEW ERA product lines which also include nuts from other AN, MS/NASM series (please refer to the individual product presentations). Sold in pieces. Please refer to product specifications or contact us.

Note: Depending on availability,these parts part may be supplied without or with Dry-Film Lubricant indicated by letter "L" in the SKU.

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 MS21069/MS21070 series nutplates are fixed self-locking, two-lug, reduced rivet spacing low height miniature anchor nuts.  MS21069 series nutplates are made from cadmium plated steel while those of MS21070 series from corrosion resistant steel (CRES). They come in different Unified Thread sizes with plain or countersunk rivet holes on each side,  with or without a dry film lube. 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.

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.

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

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

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

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

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

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.  AN3 through AN20 Series bolts are superseded by NASM3 through 20 Series. The part numbers in both series have not been changed. 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. AN10H-15)

AN10 bolts have a 5/8-18 thread with a 5/8" shank diameter. All AN10 bolts have a 0.955 thread length regardless of grip length. They can be torqued  to 92-108 lb-ft with AN365 or AN310 full-height nuts, or 50-65 lb-ft with AN364 or MS21042 half-height nuts. Indicated lengths are UHL: Under Head Length (aka Full Shank Length or Overall Length not including bolt head).

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. Countersunk screws allow the head of the screw to sit flush with or below the surface of the surrounding material. They may also be used to remove the burr left from a drilling or tapping operation thereby improving the finish of the product and removing any hazardous sharp edges.

AVIATIONEU NEW ERA AN507 series screws are mil spec threaded 100 degree countersunk non structural screws with Phillips head. They have been replaced by the respective screws of MS24693 series of materials and finishes. These screws are made of carbon steel and cadmium plated, stainless steel unplated or brass with chemical black finish. They are sold in pieces and offered in different sizes in the following materials and finishes with the corresponding notations after MS24693 and before the size number:

Carbon Steel Cadmium plated (letter "S") 

300 Series Stainless Steel unplated (letter "C")

Brass with chemical black finish, (letter "BB")

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

Tapping screws eliminate the need for drilled holes, as they are designed to cut their own hole as it is screwed into the materials. They are commonly used  in cases when the material is too thin (e.g. sheet metals), there is no rear access for installation of  a nut or when disassembly is required at a later stage and therefore blind rivets can not be an alternative. Sourced from quality producers, tapping screws are offered as part of our own labelled (AVIATIONEU NEW ERA) product lines conforming to aerospace/military or industrial standards/specifications. 

AVIATIONEU NEW ERA AN530 series screws are mil spec tapping screws offered in different sizes and sold in packs. Those with a Philips recessed head are indicated by the letter "R" in the product part number. Tapping screws conforming to ASME specifications are also available as part of AVIATIONEU NEW ERA product portfolio (see separate product presentation). The number of screws per package is indicated after the letters "PK" in the product reference number (SKU). For more information, please refer to the individual product presentations, 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.

AVIATIONEU NEW ERA AN526 series screws are mil spec truss-head non-structural machine screws made of carbon steel and cadmium plated. Minimum tensile strength 55,000 psi. Available in slot head or Phillips recessed head indicated by the letter "R" in the product part number. They are available in different sizes and lengths in inches and sold in packs. The number of screws per package is indicated after the letters "PK" in the product reference number (SKU). For more information, please refer to the individual product presentations, the supplied documentation or contact us.

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 structured in different series based on the standard of their conformance. Some of the screws commonly used include NAS204 through NAS235 and AN509/AN525 series. 

AN525/AN525R Series high-strength structural washer head (AN525) and cross-recessed (Phillips) head (AN525R) screws, fabricated from alloy steel per specification QQ-S-689. Tensile strength 125,000 PSI. Cadmium plated per QQ-P-416A, Type II, Class 3.  

The AN525 washer head structural screws provide a large contact area. The AN509R (100° countersunk) Phillips head screws are used in countersunk holes where a flush surface is necessary. These have been replaced by MS24694 Series structural screws of the respective materials and finishes.

Structural screws have a definite grip and the same shear strength as a bolt of the same size. Shank tolerances are similar to AN hex head bolts, and the threads are National Fine. Structural screws are available with round, brazier, or countersunk heads. The recessed head screws are driven by either a Phillips or a Reed and Prince screwdriver. Sourced from quality suppliers, these structural screws are offered as part of our own labelled (AVIATIONEU NEW ERA) product lines in different thread sizes and lengths in inches and sold in pieces. For more information, please refer to the individual product presentations, the supplied documentation or contact us.

Solid shank rivets are relatively low-cost,  permanently installed fasteners used as structural parts in aircraft and other applications where reliability and safety consist a priority.  These rivets are produced in accordance with military and other international standards such as US Army-Navy (AN) standard and Mil-Spec (MS) that followed. AN426/MS20426 and AN470/MS20470 Series rivets are solid aluminum rivets with countersunk head or universal head respectively. Sourced from quality suppliers they are offered as part of our own labelled (AVIATIONEU NEW ERA) product lines. They are  available in different diameters and lengths and sold by the pound (lb). Those designated by the letter "A" in their part numbers are "soft" rivets fabricated from 1100-grade aluminum with a tensile strength of 16,000 PSI while rivets designated by the letters "AD" are fabricated from 2117 aluminum and heat treated to the T4 condition. They have a shear strength of 26,000 PSI and a tensile strength of 38,000 PSI. For additional information please refer to the article on an overview of our fasteners, other 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.

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. AN6H-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.

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.

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. AN5H-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.

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. AN4H-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.

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. 

NAS 1794 Series self-locking counter bore replaceable nut elements are produced by various manufacturers. They are offered as OEM parts or parts falling under our own labelled (AVIATIONEU NEW ERA) product lines in different materials, finishes, thread sizes and dimensions in inches. Please refer to the supplied documentation.

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.

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. AN3H-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.

AN310/NASM310 and AN320/NASM320 Series castlellated nuts are manufactured from steel and cadmium plated. AN310/320 nuts have been superseded by NASM310/320 Series.  The Part Identification Numbers (PIN) for AN310/AN320 and those for NASM310/NASM320 are identical.

Castellated nuts are of similar style and shape as castle nuts but they are not as thick (deep) as the castle nuts (they consist the thin version of standard castle nuts). The thin design makes castlellated nuts weaker than the castle nuts and are used only where shear stress forces are encountered. Fabricated from steel and cadmium plated per QQ-P-416A, Type II, Class 3. AN310/NASM310 castle nuts are used with drilled-shank bolts, clevis bolts, eye bolts and studs. The slots in the nut accommodate a cotter pin for safety purposes. The thinner AN320/NASM320 series castellated shear nuts, with half the tensile rating of the AN310/NASM310 series nuts, are used with clevis bolts and threaded taper pins which are subject to shearing stress only.

Both AN310/NASM310 and AN320/NASM320 Series castlellated nuts are sourced from quality producers and offered as part of AVIATIONEU NEW ERA product lines. For additional information please consult the supplied documentation or contact us.

AN316/NASM316 Series hexagonal steel cadmium plated  thin non-locking check nuts are Military Specification versions of non-locking jam nuts used typically to lock in adjustments where a male threaded part screws only partway into a female threaded part (rod ends, grub screws, bulkhead fittings, etc). AN316/NASM316 Series jam nuts are thinner than the AN315 specification nuts for use in tighter installations but the AN316/NASM316 hex check nuts can carry half the tension load of the AN315 nuts.

Sourced from quality producers, the AN316/NASM316 Series check nuts are offered as part of AVIATIONEU NEW ERA product lines in steel cadmium plated or corrosion resistant steel (CRES) passivated (indicated by the letter "C" replacing the dash number) in different thicknesses and thread sizes in inches.  Letters "R" and "L" after the dash number indicate a Right or Left Hand thread respectively. For additional information please consult the supplied documentation or contact us.

Certification Details:

AN316 (REV. 11)., AIR FORCE-NAVY AERONAUTICAL STANDARD: Nut, Jam, Hexagon (25 Feb 1991). Superseded by NASM316. The Part Identification Number (PIN) for AN316 and the part number for NASM316 are identical. The part numbers have not been changed.

AN315/NASM315 Series hex plain nuts are manufactured from steel and cadmium plated per QQ-P-416A, Type II, Class 3, corrosion resistance steel or aluminum alloys. The AN315 nuts have been superseded by NASM315 Series. Similar to common nuts  but with a rugged construction they are designed and built with aviation grade materials and to specific aviation design specifications. They can carry the same high tension load as the AN310 castle nuts and require an auxiliary locking device such as a check nut or lock washer. 

Sourced from quality producers, the AN315/NASM315 Series hex plain nuts are offered as part of AVIATIONEU NEW ERA product lines in different thicknesses and thread sizes in inches. The following letters are used to designate specific types of airframe nuts:

"C" before dash number for corrosion resistance steel nuts

"D" before dash number for aluminum-alloy nuts

"L" after dash number for left-hand thread

"R" after dash number for right-hand thread

For additional information please consult the supplied documentation or contact us.

Certification Details:

AN315 (REV. 10) (NOTICE 2)., AIR FORCE-NAVY AERONAUTICAL STANDARD: Nut, Plain, Castellated, Airframe (23 SEP 2002) [S/S BY NASM315]., AN315 REV. 10, dated 29 DECEMBER 1972, is hereby canceled and superseded by NASM315. The Part Identification Number (PIN) for AN315 REV. 10 and the part number for NASM315 are identical. The part numbers have not been changed.

NAS1291 Series Nuts

The NAS1291 series lock-nuts are widely used throughout the aerospace industry. They are thin-walled, self-locking nuts with a reduced height and are made of silver plated corrosion resisting (stainless) steel for maximum temperatures 800°F or cadmium plated alloy steel for maximum temperatures 450°F, and offered with or without dry film lubricant The NAS1291 series of nuts ranges in size from 02 to 10 corresponding to thread diameters of .086 to .6250 inches. The following designators indicate the material and the dry film lubrication of these nuts:

- No letter after NAS1291 indicates nuts made of cadmium plated alloy steel with dry film lubrication,

- The letter "X" after NAS1291 is used to designate nuts made of cadmium plated alloy steel without dry film lubrication,

- The letter "C" after NAS1291 indicates nuts made of silver plated corrosion resisting steel (CRES) for use at max temperature 800°F.When the letter "M" is included in the end of the part number, dry film lubrication is included & max temperature is 450°F.

Nuts NAS1291-02 thru -6, NAS1291X02 thru X6, NAS1291C04 thru C6 are inactive for new design. They have been superseded by respective nuts of NASM21042/MS21042 and NASM21043/MS21043 series.

NASM21042/MS21042 and NASM21043/MS21043 Series Nuts 

The MS21042 series (superseded by NASM21042 series) are all-metal hexagon reduced height self-locking nuts, rated at 160,000 psi tensile strength, made of cadmium plated steel. They are shorter than the AN363 nut but develop the same tensile strength. They are also  lighter than AN365 nylon lock nuts (an average of 63% lighter for sizes -3 through -6).The NASM21042/MS21042 lock nuts are widely used throughout the aerospace industry together with those of MS21043 series (superseded by NASM21043) all-metal reduced hexagon, reduced height self-locking nuts with a ring base made of corrosion resistance steel and silver plated. Because of their reduced hex dimension, they are widely used in limited space applications where wrench access is a problem. Both are designed for use in high temperature installations (up to 450°F for MS21042 series  and up to 800°F for MS21043 series nuts). They both come without or with or  a dark grey dry film lubricant, indicated by the letter "L" in their part number.

Sourced from quality producers, NAS1291, NASM/MS 21042 and 21043 series nuts are offered as part of our AVIATIONEU NEW ERA product lines. Sold in pieces or packs with the number of nuts per pack indicated after the letters "PK" at the product reference code (SKU).

Depending on the selected nut  & stock conditions alternate part numbers of the same fastener may be supplied in lieu of the ordered, meeting or exceeding standard specifications of ordered parts. 

For more information please refer to the supplied documentation.

A castellated nut, also referred to as a castle nut or slotted nut, is a nut with slots (notches) cut into one end. Although castellated nuts are frequently referred to as slotted nuts, there are slight differences. Castellated nuts are formed with a round section at the top where the slots are located. Slotted nuts do not have this rounded modification. The flat sides of slotted nuts extend fully from the top to the bottom of the nut. Both castellated and slotted nuts are designed to use a pin (usually a split pin) that fits through the slots and through a hole in the screw to which the nut is attached. This pin prevents the nut from turning and loosening. Compared with slotted nuts, castellated nuts allow the cotter pin to be confined closer to the margins of the nut itself, providing added secureness.

MS17825 Series nuts are slotted hexagon style lightweight castellated self locking nuts manufactured  from cadmium plated steel to standard castle or shear nut specifications with a nylon insert added for positive safety. They are offered as part of our own labelled (AVIATIONEU NEW ERA) product lines and can be used throughout the control system. In case the cotter pin used with castle nuts is overlooked, the nut cannot work loose. The nylon insert will act as a stop nut.

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.

The NAS1581 Series screws  (also termed as bolts) are high strength, close tolerance, reduced (shear) head, countersunk screws offered as part of our own branded (AVIATIONEU NEW ERA) product lines. They come in different materials and finishes designated by the following letters in their product reference number (SKU) which is formed as a combination of the material, diameter, drive style, grip length and option of the screw:

Materials

(A) or (F) = Alloy Steel, 4140,4340 or 8740, Heat treated to 160-180ksi. Cad 2 plated. Material Code (A) has been superseded by Code (F)

(C) = Corrosion Resistant (A286) Steel, Heat treated to160-190ksi. Cad 2 (optional)

(V) = Titanium (6al-4v) Heat treated to 160-180ksi. No finish. Material Code (V) has been cancelled Dec.1991

Diameters: Numbers 3 to 10

Drive Styles

(R)= Offset Cruciform, (Torq-set) R, for diameters 3,4 & 5.

(T) = Offset Cruciform, (Torq-set) R for diameters 6 and up.

(H) = Dovetail Slot

Grip Lengths

The grip length  for Countersunk Head Fasteners (T in the supplied table) includes the head and extends to the full cylindrical portion of the shank. The Grip Length for NAS1581 Series screws is measured in 1/16ths of an inch. + or - .010

AVIATIONEU NEW ERA NAS1581 Series screws are offered in pieces or kits for convenience and economy. 

For more 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.

AS81820 Standard bearings are Plain Self-Aligning, Self-Lubricating ,Low Speed bearings with a -65 TO +325 °F temperature operating range offered in different specifications with those of SAE AS Standard superseding the Military Standard  respective parts.  AS81820 Standard bearings include AS14101/MS14101 narrow, grooved race, AS14102/MS14102 wide, chamfered race, AS14103/MS14103 wide, grooved race, and AS14104/MS14104 narrow, chamfered race.

SAE-AS14102 and SAE-AS14103 (included in this presentation) supersede those of MS14102 and MS14103 specifications. They are both are wide plain spherical bearings, self lubricating self aligning, and low speed, designed for operation in high temperature environments  (-65°F to +325°F  or -53.9°C to +162.8°C). Their inner and outer rings are made from Corrosion Resistant Steel (CRES). AS14102/MS14102 series bearings come with a chamfered outer ring while those of AS14103/MS14103 series come with a grooved outer ring. They are offered as either OEM parts from RBC® BEARINGS or as part of our own label (AVIATIONEU NEW ERA) product lines sourced from quality manufacturers. 

Narow Series AS14101/MS14101 and AS14104/MS14104 bearings (separately listed) are offered as OEM parts by different manufacturers including RBC® BEARINGS, NEW HAMPSHIRE BALL BEARINGS® (NHBB), AURORA BEARING COMPANY® and others as well as their replacements by NATIONAL PRECISION BEARING® (NPB).

For additional information and specifications please refer to the supplied documentation.

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.

Extending our present product range, our new AVIATION NEW ERA extruded aluminum alloy angles are offered in Metric (mm) dimensions and cut to oder lengths in meters to cover a wide range of application requirements.These angles are sourced mostly from Asian producers with a ISO9001:2008 quality management system and production process control while some are also holders of Approved Supplier Certificates from major aerospace companies. They comply, according to the selected angle,  with SAE AMS-QQ-A-200/3  (*) or ASTM B211M specifications (**).

Like the other AVIATION NEW ERA extruded aluminum profiles, these angles are offered in different aluminum alloys and tempers and are competitively priced to provide aviation quality but also economical solutions to our angles in inches produceed as per SAE AMS-QQ-A-200/3 specifications (**).

Aluminum Alloy Options: 2011,2014,2017,2024,5052,5083,5086,5454,5754,6061, 6063,6082,7003,7022,7050,7055,7075. 

Temper Options: T3,T351,T4,T451,T5,T6,T651,T6511,T7351,H111,H114,O.

Wide range of dimensions (mm). Custom dimensions also possible with an additional mold charge

Cut To Order (CTO) Lengths (m). Range: 1000mm - 6000mm.

Standard sizes in stock for quick deliveries. Custom dimensions also possible with an additional mold charge

 Manufacturer Test Reports (MTRs) can be supplied at additional charge

Applications: widely used to contain, protect, reinforce and support various surfaces whether in ceramic, glass, plaster, plastic, stone, wood or other metals.

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

(*) AMS stands for Aerospace Material Specifications established by the SAE International (formerly, the Society of Automotive Engineers or SAE). AMS specifications are compiled in a comprehensive database of individual directives that standardize procedures, equipment and processes related to aerospace material processing. These are continuously updated and revised to stay up-to-date with advances in material science and processes technologies.

(**) ASTM International is a standards organization developing and publishing “voluntary consensus technical standards for a wide range of materials, products, systems, and services.”ASTM’s aerospace material standards are instrumental in evaluating materials, components, and devices primarily used in aerospace and aircraft industries.

MIL-DTL 6000D Soft Flexible Aircraft Fuel (*), Oil, Water & Alcohol Rubber Hoses (superseeding MIL-DTL-6000C hoses) are offered as part of our own labeled (AVIATIONEU NEW ERA) product lines. They replace the respective MIL-DTL 6000C hoses.

These hoses are designed to handle oil, alcohol, coolant, and water.  The tube of these hoses is oil resistant with a black cover reinforced with high strength mildew resistant yarns. It withstands extreme temperature conditions from -40 deg. F to +250 deg. F.  Lightweight, flexible and easy-to-handle, they meet or exceed U.S. military specs and consist the right choice for hard-to-get-to spots in tight engine compartments. Their burst pressure is 1000 PSI (400 PSI for the hose with ID 2-1/2 in.). 

AVIATIONEU NEW ERA MIL-DTL 6000D hoses are available in different internal and outer diameters in inches. Priced and sold in feet in one foot increments. The last part of our product reference code (SKU) indicates the inner diameter of the hose in inches.

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

(*) MIL-DTL 6000D hoses are not recommended for use as fuel lines.

Aluminum alloy products consist a significant product cateory within our AVIATIONEU NEW ERA offered portfolio of metal products.

Sourced from quality producers worldwide, they are widely used in different applications in Aerospace & Defense as well as many other industries. Extending our Aerospace quality aluminum product portfolio, (separately listed) manufactured from premium materials, through rigorous processes & extensive testing under strict quality management systems, our new Commercial quality product lines  for industrial applications emphasize on cost-effectiveness. Without sacrificing quality, they conform to industrial standards (many of which are the same with those of their Aerospace quality counterparts) and can be supplied in different aluminum alloys and tempers to select for specific project requirements. Produced through extrusion, cold rolling (aka cold drawing or cold finishing) or hot rolling  manufacturing processes (*), they are competitively priced and offered in different finishes (mill finish, polished, etc.) in a wide range of dimensions in inches or millimeters (Metric system) with pre cut or cut to order lengths in feet or meters. Custom dimensions also possible with an additional mold charge. Standard sizes are maintained in stock with our suppliers for quick deliveries. Available shape options include round, rectangular, hexagonal, square bars/rods, angles, and different profiles for architectural and other applications. They are typicaly  used in automotive industry (vehicle body building), transport equipment, equipment components, frame building and general constructions, reinforcement and support of various surfaces (in the case of angles) and many others.

For further information please refer to the Product Description section and the respective documentation.

(*) Extrusion is a common forming process for producing a variety of metal parts and other materials. Extruded aluminium is made by heating the aluminium and pushing it through a die to form the finished product, and subsequently cooled, stretched, and hardened at room temperature or in heated spaces for rapid tempering. A common product example for this process is aluminium tubing. In cold drawing or cold rolling forming process (sometimes referred as cold finishing) the aluminum material is pulled into a draw die or rollers, shaping the metal at room temperature. In hot rolling, the material is heated before shaping. Cold drawing improves the metal’s mechanical properties and gives a captivating finish to the finished product.

In general, the extrusion process is considered of lower cost to cold processing which involves a greater set of instruments and materials to finish.

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

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

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

AN840 series of pipe thread hose nipple fittings are offered as part of our own (AVIATIONEU NEW ERA) portfolio of fittings. Sourced from quality producers these fittings can be furnished in aluminum or brass in different tube internal diameters and thread sizes in inches.Aluminum are designated by the letter "D" after the suffix number of the product reference number (SKU).

When battery terminals with heavy current capacity and high conductivity are required AVIATIONEU NEW ERA SC HEAVY DUTY lug type battery terminals are recommended. Similar to the AVIATIONEU NEW ERA SC brass battery terminals except that they are are produced from pure copper  and tin plated, they are available in three versions: SC(JGA), SC(JGY) and SC(JGB). Please refer to the specifications table. They can be used with wire sizes 1.5-1000mm2 (16AWG - 777MCM). Sold in packs of 20 pieces each with Minimum Order Quantity (MOQ) 5 packs. The appearing price is for reference only. Please contact us for quotation.

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).

Solid shank rivets are relatively low-cost,  permanently installed fasteners used as structural parts in aircraft and other applications where reliability and safety consist a priority.  These rivets are produced in accordance with military and other international standards such as US Army-Navy (AN) standard and Mil-Spec (MS) that followed. AN426/MS20426 and AN470/MS20470 Series rivets are solid aluminum rivets with countersunk head or universal head respectively. Sourced from quality suppliers they are offered as part of our own labelled (AVIATIONEU NEW ERA) product lines. They are  available in different diameters and lengths and sold by the pound (lb). Those designated by the letter "A" in their part numbers are "soft" rivets fabricated from 1100-grade aluminum with a tensile strength of 16,000 PSI while rivets designated by the letters "AD" are fabricated from 2117 aluminum and heat treated to the T4 condition. They have a shear strength of 26,000 PSI and a tensile strength of 38,000 PSI. For additional information please refer to the article on an overview of our fasteners, other 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.

Countersinking is used to ensure that flat head screws or fasteners sit flush against the workpiece. Countersinks used in aerospace and industrial applications are made of durable materials such as High Speed Steel (HSS) known for its hardness, toughness, and ability to withstand high temperatures. High Speed Steel (HSS) countersinks are well suited for cutting aluminum sheet metals. When combined with Cobalt, an alloying agent in steels to improve the hardenability, strength, and wear resistance in machining applications but also due to its ability to resist wear at higher temperatures, the  respective countersinks are often used for cutting stainless steel and other aluminum alloys.

Sourced from quality suppliers, integral (fixed) pilot Microstop countersink cutters are offered as part of our own labeled (AVIATIONEU NEW ERA) product lines. Made from HSS or HSS Steel with Cobalt, they consist ideal tools for aircraft manufacturers, aircraft maintenance/ repair stations or  industrial manufacturers for precise and accurate countersinking, cost-effective alternatives to other OEM products and and stocked by our suppliers for fast deliveries. 

Offered in different flutes, body and pilot diameters and sold  either separately (*) or in custom sets to address specific customer needs in machining applications.

Because of the difference in composition between HSS and Cobalt, main strengths of HSS countersinks are their high hardness and wear resistance. Therefore, as a general rule, they consist a better choice when you want your countersinks to retain their strength even when exposed to extreme wear or abuse. For higher hardenability, strength, and wear resistance and in applications when when countersinks are to be exposed to extremely high temperatures, cobalt countersinks should best be used.

AVIATIONEU NEW ERA countersinks can be used with popular adjustable or Microstop countersinking units utilizing a threaded shank drive (sold separately). For additional information please consult the supplied documentation or contact us.

(*) Minimum Order Quantities apply depending on the selected countersinks or their sets.

High-Speed Steel (HSS) is a metal alloy made up primarily of iron, tungsten, and carbon. It's known for its hardness, toughness, and ability to withstand high temperatures without losing its strength or shape. It also has excellent abrasion resistance properties, which make it useful for cutting tools. HSS drill bits are extremely hardwearing and particularly well designed for drilling into relatively hard metal surfaces and wood, as they are much more resistant to the heat generated from the fast speed operation. The front edges cut the material, whilst the spirals remove debris from the hole. Apart from HSS, Cobalt is often used as an alloying agent in steels to improve the hardenability, strength, and wear resistance in machining applications but also due to its ability to resist wear at higher temperatures while still maintaining its strength and shape. Cobalt-based alloys are typically harder than HSS alloys but are also more prone to cracking or chipping if not handled properly. Compared to HSS drill bits which are more elastic and, as such, don't break easily, those containing cobalt are more brittle and chip quickly.

Sourced from quality suppliers, threaded hex shank drill bits are offered as part of our own labeled (AVIATIONEU NEW ERA) product lines. Made from HSS or HSS Steel with Cobalt, these drill bits consist ideal tools for aircraft manufacturers, aircraft maintenance/repair stations or  industrial manufacturers, cost-effective alternatives to other OEM products and and stocked by our suppliers for fast deliveries. Offered in different types (stub, short or long), flute and overall lengths they are sold either separately (*) or in custom sets to address specific customer needs in machining applications.

Because of the difference in composition between HSS and Cobalt, main strengths of HSS drill bits are their high hardness and wear resistance. Therefore, as a general rule, they consist a better choice when you want your drill bits to retain their strength even when exposed to extreme wear or abuse. For higher hardenability, strength, and wear resistance and in applications when when drill bits are to be exposed to extremely high temperatures, cobalt drill bits should best be used.

For additional information please consult the supplied documentation or contact us.

(*) Minimum Order Quantities apply depending on the selected drill bits or their sets.

United States Military Standard RG58 Coaxial Cables are flexible and lightweight coaxial cable with a solid 20 American Wire Gauge (AWG) conductor, a 50-ohm characteristic impedance and maximum voltage rating of 1,900 volts. They feature a low-density polyethylene dielectric insulation with a dielectric constant of 2.3 and a diameter of 0.116 inches (2.9mm), a tinned copper braided shield and a PVC jacket. The outside diameter of the cable is 0.195' (4.95 mm), which makes it suitable for indoor and vehicular use where size matters. It is best for signal frequencies up to 1GHz, where its attenuation is 14.5 decibels per 100 feet. Above that frequency, attenuation increases, and at 5GHz it is approximately 60 dB/100 ft. RG58 coaxial cable supports 10Base2 Ethernet.

These cables come in different versions (types) corresponding to different conductors including RG58 (pure annealed copper conductor), RG58/U (single solid core copper conductor), RG58A/U (multi-core tinned copper conductor with generally low loss foamed insulation)  or RG58C/U (multi-strand tin-plated copper conductor and polyethylene solid core). RG58 A/U Coaxial Cables with PVC jacket are ones most used in WiFi, Wireless LAN, GSM, and Monitoring and Control of Network Infrastructure Sites. Also they are standard cables for avionics installations in experimental (non-certified) aircraft.

The mil-spec coaxial specification version of RG58 is the M17/28-RG58 Coaxial Cables. These cables are like their standard RG58 counterparts except that they feature a stranded tinned copper conductor and the outer conductor is a 36 AWG tinned copper braid.

RG58 Coaxial Cables are offered as part of our own labelled (AVIATIONEU NEW ERA) product lines. Sourced from quality manufacturers they priced and sold by the foot or meters (depending on the manufacturer). They can be furnished in standard or cut to order lengths.

Connectors compatible with RG58 coaxial cables are also offered and include BNC bayonet connectors, Low-Profile screwed TNC connectors and screwed FME connectors.

(*) The letter "U" means indicates that the conductor of the cable is copper while letters "A", "B", "C" are used when the conductor is aluminum thin.

A castellated nut, also referred to as a castle nut or slotted nut, is a nut with slots (notches) cut into one end. Although castellated nuts are frequently referred to as slotted nuts, there are slight differences. Castellated nuts are formed with a round section at the top where the slots are located. Slotted nuts do not have this rounded modification. The flat sides of slotted nuts extend fully from the top to the bottom of the nut. Both castellated and slotted nuts are designed to use a pin (usually a split pin) that fits through the slots and through a hole in the screw to which the nut is attached. This pin prevents the nut from turning and loosening. Compared with slotted nuts, castellated nuts allow the cotter pin to be confined closer to the margins of the nut itself, providing added secureness.

MS17826 Series nuts are slotted hexagon style lightweight castellated self locking nuts. They are similar to MS17825 Series nuts but they have a reduced height. They are manufactured  from cadmium plated steel to standard castle or shear nut specifications with a nylon insert added for positive safety. They are offered as part of our own labelled (AVIATIONEU NEW ERA) product lines and can be used throughout the control system. In case the cotter pin used with castle nuts is overlooked, the nut cannot work loose. The nylon insert will act as a stop nut.

Aircraft braking systems serve a vital function during takeoff, landing and taxiing. Along with landing gear, aircraft wheels and brakes are critical to ensure safe and reliable aircraft ground operations under extreme forces, stress, as well as wear and tear from general operation and the environment. Commercial aircraft brakes are arranged in multiple disk pairs commonly referred to as Heat Sinks or Heat Packs (as they convert the kinetic energy of the moving airplane to heat energy). Initially made metal (steel) heat sinks are gradually replaced by those from carbon fibres (particularly on larger, long-haul commercial airplanes) due to their higher efficiency in braking applications, longer life-span, lower weight and resulting less fuel consumption and lower CO2 emission by the engines. 

Carbon and steel heat packs and parts are offered as part of our own labelled (AVIATIONEU NEW ERA) product lines. Sourced from quality suppliers these heat packs  feature high quality, safety, improved design, significant cost savings and fast deliveries. They can be used as  cost effective alternatives in many commercial aircraft platforms equalling or exceeding standards of  respective OEM products by leading manufacturers such as Honeywell Aerospace, Collins Aerospace/Goodrich Wheels & Brakes, Parker Meggitt Aircraft Braking Systems and Safran Landing Systems (formerly Messier-Bugatti-Dowty). They are  PMA approved (*) parts by the Civil Aviation Administration of China (CAAC) for use on an extensive list of Western and Eastern commercial (civil ) aircraft platforms including Boeing, Airbus, McDonnell Douglas, Ilyushin and others and are currently installed in aircraft operating by different air transport operators in China and other countries in the Middle-East, South and Central Asia and Africa.

Typical Aircraft Applications for steel and carbon heat packs include Boeing 737 / 757, Airbus A318 / A319 / A320 / A330 , McDonnell Douglas: MD82 /MD90  Xian MA60 etc. 

(*)  Parts Manufacturer Approval (PMA) is a combined design and production approval granted by a competent Civil Aviation Authority (CAA) to a manufacturer of aircraft parts for modification and replacement. Use of Civil Aviation Administration of China (CAAC) approved parts in other countries depends on existing bilateral agreements between CAAC and respective competent authorities in these countries.

For additional information please contact us.