MS20819/AN819 Series of coupling sleeves are offered as part of our own (AVIATIONEU NEW ERA) portfolio of fittings. Sourced from quality producers these fittings can be furnished in steel, aluminum or stainless steel and in different outer tube diameters and sizes in inches. Aluminum and Stainless Steel fittings are designated by the letters "D" and "J" respectively after the suffix number of the product reference number (SKU).

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

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

Sourced from quality producers,  machine screws are offered as part of our own branded (AVIATIONEU NEW ERA) product lines conforming to aerospace/military or industrial standards/specifications.  They come in different sizes, head types, materials and thread gradings. NAS Standard Machine Screws meet aerospace standards and come in different types and sizes structured in different series including NAS1101, NAS1102, NAS1189, NAS1190, NAS1191, NAS1635, NAS1801, NAS1802, NAS220, NAS229, NAS333, NAS514, NAS517, NAS560, NAS583, NAS600, NAS623 and NAS662.

AVIATIONEU NEW ERA NAS583 series of machine (non structural) screws are aeronautical 100 deg. alloy steel cadmium plated flush head close tolerance machine screws  offered in different thread sizes and lengths in inches and sold 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. 

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

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

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.

Adel (aka MS21919) aircraft clamps, are key components used in line support, vibration dampening and maintaining proper clearance for lines or harnesses running throughout the aircraft structure. The Adel clamp is a metal band, constructed from aluminum, corrosion-resistant steel and low-carbon steel, covered by a white rubber lining or cushion, made from silicone.

Adel MS21919 Series cushioned loop aerospace clamps are offered as part of AVIATIONEU NEW ERA product lines in different sizes with their bands (straps) and cushions manufactured from different materials.

The High Temperature MS21919WH and MS21919WCH clamps feature  "silicone" white rubber cushions rated for 400 degrees for use in the aerospace industry. Cushion material enables elevated temperature usage in phosphate ester based fluid and other synthetic fluid contaminated areas. They are unaffected by ozone. Not resistant to petroleum based fluids. The extra rubber wedge at one end of the rubber cushion assures a tight fit, helps avoid pinching wires or lines when closing the clamp and helps reduce vibration when used on lines. 

The “WCH” series clamps have a corrosion resistant steel (stainless steel) strap while the “WH” series clamps have an aluminum strap. 

The MS21919WDF Series clamps have an aluminum strap and a nitrile cushion while the MS21919WDG Series clamps have have an aluminum strap and a chloroprene cushion.

Clamps and Cushioned Loops can be slipped over a tube or wire and closed with a bolt at assembly and have one round hole and one slot for ease of alignment and a developed shape for proper closing.

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

With a modern design, a rigid full composite structure, spacious cabin and a panel equipped with advanced avionics and instruments, PICA 2 Ultralight/LSA single engine low wing aeroplane from H.F DORNA stands out from competition. However, what cathes the eye on the ground becomes an unforgettable flying experience due to the PICA 2 high performance as a result of the aeroplane construction, the powerful BPR-ROTAX 912 UL S2 100 HP engine and the 3-blade SR200B ground adjustable WOODCOMP propeller.  Designed and built in strict conformance with ASTM International standard, with a MTOW of 600 kg, PICA 2 aeroplane qualifies for Ultralight certification under present national rules in the EU countries where the previous 450 kg weight limit has been replaced by a 600 kg (1,320 pounds) MTOW. It also qualifies for operations in the U.S. or other countries accepting FAA Light Sport Aircraft (LSA) certification regulations. Running on MOGAS (95 octane unleaded) or AVGAS 100LL fuel and exhibiting a Low Direct Operating Cost, the PICA 2 Ultralight aeroplane is offered under AVIATIONEU NEW ERA Lease or Buy Programs as a multi purpose aircraft for recreational and business flying, pilot training, aeroclub operations, surveillance or other missions. Depending on the leasing or buy option, a range of support services (*) are also offered including initial airworthiness certification in the country of operations, user training on aircraft operations, supply of spare parts and consummables, aircraft maintenance, insurance etc. For additional information please refer to the supplied documentation or contact us.

(*) Some of these services are prerequisites in the leasing option. 

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

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

NAS6206 series shear hexagon head bolts with a 3/8-24" thread supercede NAS1106 high strength bolts. Their shearing feature is used to minimize damage to critical components of the application. They are made from alloy steel with cadmium or chromium finishes and offered in different grips and lengths in inches with undrilled or drilled head and/or shank. They are sold in pieces.

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

No Finish Code for cadmium plated bolts

"C" for chromium plated bolts

"L" / "P" for self-locking bolts/self-locking bolts with patch type locking element only

Grip Dash Number indicating grip in .0625 increments

"D" after the grip dash number for drilled thread bolts

"H" after the grip dash number for bolts with drilled head

More than one code letters may be used in sequence.

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

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

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

Copper wires are conductors of electricity and they are used for a wide range of applications including power generation, power transmission, power distribution, telecommunications, electronics circuitry and others. Apart from the high conductivity copper features durability, tensile strength and corrosion resistance.

AVIATIONEU NEW ERA copper round wire product range includes bare copper, copper, paper insulated copper wires as well as double cotton covered and silver or tinned plated copper wires. 

They are offered in rolls in different wire gauges (*). Sold in kilograms except the double cotton covered wire which is sold by the meter. Appearing prices is for reference only per UOM. Please contact us for a quotation.

Bare Copper Wire, Gauge 0-5

Paper Insulated Stranded Wire, Gauge 0-5

Tinned Plated Copper Wire (Temperature 120 deg. C), Gauge 0.2-2

Silver Plated Copper Wire (Voltage up to 1000 V, Flame Retardant), Gauge 0-5

Double Cotton Covered Copper Wire, Gauge 0-5

(*) Wire gauge is a measurement of wire diameter. This determines the amount of electric current a wire can safely carry, as well as its electrical resistance and weight. Please refer to the respective table.

MS internal wrenching bolts (superseding  NAS series) are offered as part of AVIATIONEU NEW ERA product lines. Sourced from quality producers, they are fabricated from 160-180 ksi high-strength steel and are intended for use in both tension and shear applications. Standard AN hex head bolts and washers cannot be substituted for them as they do not have the required strength. NAS 144 to 158 series are supeseded by MS 20004 to MS 20024 series. Refer to the supersedure chart provided. 

These bolts are available in different total and grip lengths, thread pitches and diameters in inches as well as with drilled or undrilled heads and shanks. The head of the internal wrenching bolt is recessed to allow the insertion of an internal wrench when installing or removing the bolt. When they are used in steel parts, the bolt hole must be slightly countersunk to seat the large corner radius of the shank at the head. In Dural material, a special heat-treated washer must be used to provide an adequate bearing surface for the head. They should always be used with the designed companion washer MS20002C(size) under the head as these bolts have a noticeable radius at the head to shank juncture. Special high-strength nuts are used on these bolts. To develop full tension use an NAS1804-(size) 180ksi, or an MS21042-(size) 160ksi nut according to your requrements. 

Unless specified by the following letters in the part numbers, internal wrenching bolts come with an Undrilled Shank and Undrilled Head.

"A"  Drilled Shank (NAS series)

"DH"  Drilled Head (NAS series)

"ADH"  Drilled Shank, Drilled Head (NAS series)

"H" Drilled Head (MS series)

Use these bolts with companion washers MS20002C(size) under the head and NAS1804-(size) 180ksi, or MS21042-(size) 160ksi high-strength nuts according to requrements.

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.

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.

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.

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

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

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

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

AVIATIONEU NEW ERA ASTM A324 Grade 8.8 Series high tensile hexagonal head threaded bolts are produced from medium carbon steel with heat treatment by both quenching and tempering.  They comply with ASTM A324, ASME SA324 standards. Medium carbon steel is less expensive  than other grades and features good ductile and malleable qualities but a lower tensile strength. 

Grade 8 Class bolt capabilities: Yield (strech): 4354 lbs min, Tension (failure): 5024 lbs min, Tensile Strength: 150.000 lbs per square inch.

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

AL2024 is an aluminium alloy, with copper as the primary alloying element. It is used in applications requiring high strength to weight ratio, as well as good fatigue resistance, weldablility and average machinability. It comes in different tempers, O (Annealed)without heat treatment or T (heat treated). Since corrosion resistance is relatively low, 2024 is commonly used with an anodized finish or in clad form (specified as CLAD or ALCLAD) with a thin surface layer of high purity aluminum metallurgically bonded to the aluminium alloy core material.

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

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

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

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

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

AVIATIONEU NEW ERA hydraulic grease nipples are sourced from certified manufacturers and they available in different types (conical, button or flush head, drive-in or self-forming). Please refer to the respective product presentations.

Conical head type grease nipples comply with DIN 71412, SAE J534 & IS 4009-2 standards. Hardness for nipple head: Min.550 HV. They are made from different materials,  EN 1AL(free cutting steel), 1SMnPb30+C,SAE 12L13 or stainless steel  303 & 316 with different surface finishes (clear/yellow/olive green zinc plated). Available with straight or angled nipples, tapered or parallel threads in different sizes:

Metric: from M5x0.8 to M16x1.5

British Standard Pipe (BSP): from 1/8"-28 to 3/8"-19

U.S. National Pipe Thread (NPT/PTF): from 1/8"-27 to 1/4"-18

U.S. ANSI/ASME B1.1 Unified National Thread - UNC Coarse series and UNF Fine series: from 1/4"-28 to 3/8"-24

Sold by the piece (pc.) with Minimum Order Quantity (MOQ) 1000 pcs.  Appearing price is for reference only per pc. Please contact us for a quotation.