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").

NAS6205 series shear hexagon head bolts with a 5/16-24" thread supercede NAS1105 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. 

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

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.

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.

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.

Flush type head grease nipples comply with  DIN 3405 standard.They are made from different materials,  EN 1AL(free cutting steel), 1SMnPb30+C or SAE 12L13 and  zinc plated. Available with parallel threads in different sizes:

Metric: from M5x0.8 to M12x1.5

British Standard Pipe (BSP): 1/8", 1/4" & 3/8"

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

Sold by the piece (pc.) with Minimum Order Quantity (MOQ) 500 pcs.  Appearing price is for reference only per pc. Please contact us for a quotation.

Sourced from quality producers, AVIATIONEU NEW ERA general purpose brass check valves with nylon cover are suitable for use in hydraulic, heating, air conditioning and pneumatic installations in vertical, horizontal or oblique positions. They are manufactured in accordance with ISO 228 standard and they are available in different sizes. Sold in pieces.

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.

Aluminum alloys 6061 and 6063 (AL6061/AL6063), with magnesium and silicon as their major alloying elements, are both popular alloys used in extrusions for a variety of architectural, machinery, equipment, and consumer products. Similar in composition & mechanical properties they come as O (annealed), or in tempered grades. Their magnesium content provides increased strength, and silicon reduces their melting temperature. Their formability, weldability, corrosion resistance, and moderately high strength enhance their versatility. However, there are differences between them and factors affecting their suitability for different applications. 6061 aluminum is the most commonly used aluminum alloy in the world used in all kinds of applications ranging from electronics to welded assemblies. Compared to AL2024 (aka aircraft aluminum) 2024 aluminum’s higher yield strength makes it more suitable if strength is a priority. 6061 tubes, sheets, bars, and plates offer high- to moderate strength, excellent corrosion resistance, and superior machinability and weldability while 6063 aluminum tubes offer an excellent strength-to-weight ratio, superior corrosion resistance, and a fine appearance and finish.

AVIATIONEU NEW ERA seamless extruded round pipes from 6061/6063 aluminum alloy are competitively priced, produced as per ASTM B241 specification (also available in ASTM B209-04, B210M-05, B234M-04 & B221M-05a) and offered as T6 tempered. Available in outer diameters 12.7-1066.8 mm, wall thicknesses 1.5-150 mm and cut to order (CTO) lengths. Unit of sale is 1 Ton (US or Metric as specified) with Minimum Order Quantity (MOQ) 1 Ton. Sea/sea-surface transport to customer destination can be provided. Approximate time for shipping: usually 1-2 months from the time of order payment depending on the ordered quantity. Appearing price is indicative per unit of sale. For additional information, please refer to our attached Brief Guide on Aluminum Grades & Temper Designations or contact us.

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.

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.

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

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").

NAS6204 series shear hexagon head bolts with a 1/4-28" thread supercede NAS1104 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" for self-locking bolts

"P" for 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. 

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

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

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

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

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

AL5052-O CLAD (ALCLAD) tubes(*) are offered as part of our own branded (AVIATIONEU NEW ERA) product lines along with those from other grade aluminum and steel alloys. Sourced from quality producers, they are offered as Annealed in different outer diameters and wall thicknesses in inches and  cut to order lengths up to 5 ft (60 in.). They can be used for low and medium pressure hydraulic systems, fuel lines and oil lines. Tubing is sold by foot. There is additional cost if manufacturing test reports are required.

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

(*) ALCLAD is a corrosion-resistant aluminium sheet formed from high-purity aluminium surface layers metallurgically bonded (rolled onto) to high-strength aluminium alloy core material. As an enhanced sheet for fuselage applications, ALCLAD offers improved fracture toughness and fatigue crack growth while maintaining the strength characteristics of the alloy. ALCLAD also offers improved fracture toughness and fatigue crack growth while maintaining the strength characteristics of the alloy.

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

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.

Aircraft cables are stranded wires used in a wide variety of applications on or around the aircraft including flight control surfaces and tie-downs or other purposes. The term "wire rope" is also used when the diameter is larger than 3/8 inch (9.52 mm), with smaller gauges designated as cables or cords. They are specified by the number of strands times the number of wires in each strand. For example, “7x19” means the cable has seven (7) strands, with 19 wires in each strand. 7x19 is the most flexible aircraft cable construction, approximately twice as flexible as 7x7 construction.

AVIATIONEU NEW ERA aircraft ropes/cables feature smooth finish, corrosion resistance and high load bearing strength. They feature a tensile strength of 1570-1960 MPA, are sourced by certified manufacturers, competitively priced and offered in the common construction types (1X7, 7x17, 1x19, 7x19 ) in Galvanized or Stainless Steel, different diameters ( 9 -12mm for cables, 5-52 mm for ropes) and cut to order lengths in meters. Unit of measure and sale is the meter and the Minimum Order Quantity (MOQ) is 500 meters.  Appearing price is for reference only per meter. Please contact us for a quotation.

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).

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.