GOEBEL® is leading manufacturer of high quality fasteners with product lines extending from blind Rivets, self-tapping/drilling screws, and sealing washers, to drill bits, nut drivers, toggle latches, hand & power tools, PPE equipment, and many more innovative specialty products. GOEBEL® blind rivets, much like other GOEBEL® fastening products, are widely recognized used by leading companies in nearly every industry including oil & gas, automotive, HVAC, railroad, aerospace, telecommunications, and construction.

Blind rivets are offered in different product families in different materials, finishes head styles and sizes to meet intended application requirements. They include Standard, Multi-Grip, Semi Structural & Structural, Tri-Folding & Load Spreading as well as Specialty blind rivets. More information on GOEBEL® Structural Blind Rivets is included in the Product Description. Additional information on GOEBEL® Blind Rivers is also available in the documentation in the Attachment section.

Blind rivets (also commonly referred to as POP Rivets) are mainly used in applications where there is no access to the rear (blind side) of the joint. They are two-piece fasteners consisting of the rivet body (aka shell, or hat) and the stem or mandrel, pre-assembled and ready to use. They are not material specific and therefore they can be used to join two different material types together.

Rivets are installed by using a riveting tool to draw the mandrel which causes the body to deform and clamp down on the joint. Upon reaching the designed clamping force, the mandrel snaps and is discarded. 

They come in different materials, sizes, military or industrial standards, and cover a wide range of structural and non structural applications.

Non structural blind rivets are those designed for applications where the connection doesn't need to withstand significant load-bearing forces. They are offered by different  manufacturers under their respective brands, such as STANLEY® Engineered Fastening AVDEL® & POP®, and others but also as part of our own labelled (AVIATIONEU NEW ERA) product lines, sourced by quality suppliers and intended as cost-effective alternatives to OEM parts. Depending on the rivet, they are made of different materials such as steel, stainless steel,  alluminum alloys, or combinations, and supplied in different head styles, in Inch or Metric (M) diameters, lengths and grip ranges.

Blind rivets conform to national and international military, aerospace and industrial standards such as MS, AIA/NAS, DIN, ISO and others.

Non structural blind rivets produced in accordance with the German DIN 7337 Standard or respective replacing ISO Standards (ISO 15983 for Protruding Head, and ISO 15977 for Flat/Countersunk Head blind rivets) are offered as part of AVIATIONEU NEW ERA product lines.

Sold in pieces but mostly in packs with the number of rivets per pack indicated in the product SKU after the letters "PK". Appearing sale prices are per unit of sale used each time. Depending on the selected rivet & prevailing stock conditions alternate part numbers of the same rivet may be supplied in lieu of the ordered, meeting or exceeding Standard specifications. For additional information on different products please refer to the Product Description section, the supplied documentation or contact us.

Jo-Bolt is a trade name for an internally threaded three-piece rivet. A Jo-Bolt consists of three factory preassembled parts, a threaded steel alloy bolt, a threaded steel nut, and an expandable stainless steel sleeve. During installation the bolt is turned while the nut is held. This causes the sleeve to expand over the end of the nut, forming the blind head and clamping against the work. When driving is complete, a portion of the bolt breaks off. The high shear and tensile strength of the Jo-Bolt  fasteners makes them suitable for use in high-stress applications where some of the other blind fasteners would not be practical. Other advantages include their excellent resistance to vibration, weight saving, and fast installation by one person. Jo-Bolts are often encountered in the permanent structure of late model aircraft, in areas which are not often subjected to replacement or servicing. Manufactured to different aerospace standards such as NAS 1669, 1670, 1750, or 1751 they are offered as OEM parts of their respective producers or as respective Standard part numbers under our own labelled (AVIATIONEU NEW ERA) product lines.

Blind rivets (also commonly referred to as POP Rivets) are mainly used in applications where there is no access to the rear (blind side) of the joint. They are produced in accordance with different standards specifying their properties, sizes/dimensions, materials, finishes, installation methods & other information for their application. A benefit of blind rivets is that they are not material specific and therefore they can be used to combine two different material types together. 

This listing relates to those manufactured in accordance with National Aerospace Standards NAS 1919 & 1921, U.S. industry standards for the aerospace industry created and maintained by the Aerospace Industries Association (AIA).

NAS 1919 & NAS 1921 rivets are general-purpose, mechanically-locked blind rivets used in aerospace and industrial applications for creating permanent and strong joints. They feature a self-plugging, serrated stem and a protruding (NAS 1919) or 100° (NAS 1921) flush head style. Produced by different manufacturers (such as PCC CHERRY AEROSPACE or HOWMET AEROSPACE HUCK) they are offered in different materials (aluminum, corrosion resisting A286 stainless steel or Monel) and finishes, different nominal shank diameter sizes & corresponding grip ranges in inches. 

NAS 1919 / 1921 rivets are sold under OEM brands and part numbers or as  Standard part numbers under our own branded (AVIATIONEU NEW ERA) product lines, in pieces or packs where the specified number of fasteners per pack is indicated after the letters "PK" in the product reference number (SKU). 

Depending on the selected size & stock conditions alternate part numbers of the same fastener may be supplied in lieu of the ordered, meeting or exceeding Standard specifications. For more information please refer to the attached documentation or contact us.

AIRPRO INDUSTRY CORP. manufactures professional quality air tools, hand  & auto repair tools and accessories for professional applications under  the brand name AIRPROWU. AIRPROWU extensive product line ranges from aircraft tools to industrial, automotive/motorcycle ,tooling/molding, construction and auto body shop solutions and solutions for electronic assembly lines. AIRPROWU compression riveters include different models covering different capacity requirements for aluminum and steel. They come in different dimensions and are  offered with matching yokes to cover various application needs. Please refer to the specifications of individual compression riveters.

The MS21141 Series of blind fasteners are high srength pull type protruding head blind bolts (or otherwise termed as rivets) made of corrosion resisting steel (typically A286 stainless steel) with a 95 KSI shear strength. These fasteners are produced by different manufacturers and sold uder their respective brands and part numbers. Indicative examples include PCC CHERRY AEROSPACE CR7621 Series of Maxibolt® Blind Bolts or  HOWMET AEROSPACE Unimatic® UBP-EU Blind Bolt Fasteners. These blind bolts are offered in different nominal diameter sizes & corresponding grip ranges in inches, passivated or cadmium plated and with or without lubrication. They can be installed with the use of single action tools and they are supplied either as OEM part numbers of their respective manufacturer or MS21141 Standard part numbers under our own branded (AVIATIONEU NEW ERA) product lines. In the case of OEM parts, these are listed separately. Sold in pieces or packs where the specified number of fasteners per pack is indicated after the letters "PK" in the product reference number (SKU). 

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

For more information please refer to the attached 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.

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.

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).

European Standards (EN) and other deliverables are developed in a large number of sectors by the CEN National Standardization Bodies and CENELEC's National Committees (NCs) of the EU and EFTA countries. Together with the European Telecommunications Standards Institute (ETSI) they are the three European Standardisation Organisations operating under the Regulation (EU) No 1025/2012 to produce European harmonised standards in support of EU legislation and policies.

EN 6114 & EN 6115 Standards relate to short thread countersunk & protruding head bolts respectively for aerospace applications. EN6114 & EN 6115 Standard bolts are commonly used on Airbus commercial aircraft platforns such as A320, A330, A350 and A380. Airbus A320/ A330 aicraft commonly use the alloy steel versions of the EN6114 Standard bolts and those of the Titanium series indicated by the V and T surface coding. The Airbus A350 and A380 models incorporate those from INCONEL®  nickel-chromium-based superalloy. Several HLT, HST, NSA, and VL fasteners can be used as alternates to those of EN6114 Standard (see the supplied documentation).

Sourced from various manufacturers in different materials (steel, titanium or INCONEL® alloys), coatings and sizes, the EN 6114 & EN 6115 Standard bolts are offered as OEM parts of their respective suppliers or as part our own labelled (AVIATIONEU NEW ERA) product lines. Different material letter codes in the part number indicate the material used (e.g. " V" and "T" for Titanium or "L" and "M" for Inconel®). They are sold in packs with the number of bolts included in each pack designated after the letters "PK" in the product reference number (SKU). For additional information please refer to our brochure in our Attachment section

National Aerospace Standard (NAS) machine bolts are commonly used in aircraft, space shuttles, military vehicles, drones, and other high-performance applications. They are offered in different series to meet application requirements.

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

No Finish Code for cadmium plated bolts

"C" for chromium plated bolts

"D" for drilled shank bolts

"L" for self-locking bolts

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

"H" for bolts with drilled head

More than one code letters may be used in sequence.

National Aerospace Standard (NAS) machine bolts are commonly used in aircraft, space shuttles, military vehicles, drones, and other high-performance applications. They are offered in different series to meet application requirements.

NAS 6604 Series Steel Cadmium Plated Shear Hex Head Machine Bolts are offered as part of our own labelled (AVIATIONEU NEW ERA) lines of  fasteners. Sourced from quality manufacturers, AVIATIONEU NEW ERA NAS6604 series shear hexagon head bolts conform to the respective U.S. National Aerospace Standard of the Aerospace Industries' Association. They have a 1/4-28 thread and a nominal grip diameter of 0.2500 inch. NAS6604 series forms part of NAS family of bolts (NAS6603 through NAS6610 series) which includes hex head, close tolerance, alloy steel, long thread, self-locking & non-locking bolts. Their shearing feature is used to minimize damage to more critical components within the application. They are made from alloy steel with cadmium or chromium finishes and offered  in different grips and lengths in inches with undrilled or drilled head and/or shank. Used in applications where a premium-quality, high strength bolt is necessary. The following letters after the basic part numbers specify the material, finish and drilling condition of these bolts.

No Finish Code for cadmium plated bolts

"C" for chromium plated bolts

"D" for drilled shank bolts

"L" for self-locking bolts

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

"H"for bolts with drilled head

More than one code letters may be used in sequence.

National Aerospace Standard (NAS) machine bolts are commonly used in aircraft, space shuttles, military vehicles, drones, and other high-performance applications. They are offered in different series to meet application requirements.

Those of NAS 6203 through NAS 6220 series, superseding their NAS 11(xx) counterparts, are tension hexagon head high strength close tolerance short-thread alloy steel bolts with a minimum tensile strength of 160,000 psi and a minimum shear strength of 95,000 psi. 

They are made from different steel alloys such as 4140 (UNS G41400) or  4340 (UNS G43406) with either Cadmium Plate  Type II, Class 2 or Chromium Plate on shank only with all other surfaces cadmium plated.

Depending on the series they come in different nominal diameters in inches (e.g. NAS 6203 0.1875" (3/16"), NAS 6204 0.25" (1/4"), NAS 6205  0.3125" (5/16"), NAS 6206 0.375" (3/8"), NAS 6208 0.500" 1/2") or NAS 6210 0.625" (5/8") grips (in 1/16” increments beginning at 1/16”), thread and overall fastener lengths. They can be supplied undrilled or with drilled head and/or thread and with or without locking elements (nylon or equivalent). Sourced from quality manufacturers, these bolts are listed according to their series, and offered either as OEM parts or as parts of our own labelled (AVIATIONEU NEW ERA) product lines (see the respective listings). Sold in pieces or packs of specified number of bolts per pack designated by the number after the letters "PK" in the product reference code (SKU).

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

No Finish Code for Cadmium II plated bolts

"C" for Chromium plated bolts (shank only)

"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.

PN Examples:

NAS6204-10 - NAS 6204 Series Bolt, .2500-28 Thread, .625 Grip, Undrilled, Non-locking, Alloy Steel Cadmium II Plated.

NAS6204-10D - Same bolt as above with Drilled Thread.

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

National Aerospace Standard (NAS) machine bolts are commonly used in aircraft, space shuttles, military vehicles, drones, and other high-performance applications. They are offered in different series to meet application requirements.

Those of NAS 6203 through NAS 6220 series, superseding their NAS 11(xx) counterparts, are tension hexagon head high strength close tolerance short-thread alloy steel bolts with a minimum tensile strength of 160,000 psi and a minimum shear strength of 95,000 psi. 

They are made from different steel alloys such as 4140 (UNS G41400) or  4340 (UNS G43406) with either Cadmium Plate  Type II, Class 2 or Chromium Plate on shank only with all other surfaces cadmium plated.

Depending on the series they come in different nominal diameters in inches (e.g. NAS 6203 0.1875" (3/16"), NAS 6204 0.25" (1/4"), NAS 6205  0.3125" (5/16"), NAS 6206 0.375" (3/8"), NAS 6208 0.500" 1/2") or NAS 6210 0.625" (5/8") grips (in 1/16” increments beginning at 1/16”), thread and overall fastener lengths. They can be supplied undrilled or with drilled head and/or thread and with or without locking elements (nylon or equivalent). Sourced from quality manufacturers, these bolts are listed according to their series, and offered either as OEM parts or as parts of our own labelled (AVIATIONEU NEW ERA) product lines (see the respective listings). Sold in pieces or packs of specified number of bolts per pack designated by the number after the letters "PK" in the product reference code (SKU).

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

No Finish Code for Cadmium II plated bolts

"C" for Chromium plated bolts (shank only)

"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.

PN Examples:

NAS6204-10 - NAS 6204 Series Bolt, .2500-28 Thread, .625 Grip, Undrilled, Non-locking, Alloy Steel Cadmium II Plated.

NAS6204-10D - Same bolt as above with Drilled Thread.

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

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

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

AVIATIONEU NEW ERA NAS 428 series of machine (non structural) bolts are fully threaded, crowned hexagon head bolts made from cadmium plated steel or corrosion resistant steel (CRES). These bolts are offered with drilled or undrilled head or thread in different thread sizes, diameters and lengths in inches and sold in pieces. The number after NAS428 ( - ) denotes the thread size in 1/16th inch increments. The number after the last dash ( - ) is the overall length under the head. If this number is a single digit it is 1/8 of an inch. If it is a two digit number, the first is whole inches, the second is additional 1/8ths. For more information, please refer to the supplied documentation or contact us. 

National Aerospace Standard (NAS) machine bolts are commonly used in aircraft, space shuttles, military vehicles, drones, and other high-performance applications. They are offered in different series to meet application requirements.

Those of NAS 6203 through NAS 6220 series, superseding their NAS 11(xx) counterparts, are tension hexagon head high strength close tolerance short-thread alloy steel bolts with a minimum tensile strength of 160,000 psi and a minimum shear strength of 95,000 psi. 

They are made from different steel alloys such as 4140 (UNS G41400) or  4340 (UNS G43406) with either Cadmium Plate  Type II, Class 2 or Chromium Plate on shank only with all other surfaces cadmium plated.

Depending on the series they come in different nominal diameters in inches (e.g. NAS 6203 0.1875" (3/16"), NAS 6204 0.25" (1/4"), NAS 6205  0.3125" (5/16"), NAS 6206 0.375" (3/8"), NAS 6208 0.500" 1/2") or NAS 6210 0.625" (5/8") grips (in 1/16” increments beginning at 1/16”), thread and overall fastener lengths. They can be supplied undrilled or with drilled head and/or thread and with or without locking elements (nylon or equivalent). Sourced from quality manufacturers, these bolts are listed according to their series, and offered either as OEM parts or as parts of our own labelled (AVIATIONEU NEW ERA) product lines (see the respective listings). Sold in pieces or packs of specified number of bolts per pack designated by the number after the letters "PK" in the product reference code (SKU).

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

No Finish Code for Cadmium II plated bolts

"C" for Chromium plated bolts (shank only)

"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.

PN Examples:

NAS6204-10 - NAS 6204 Series Bolt, .2500-28 Thread, .625 Grip, Undrilled, Non-locking, Alloy Steel Cadmium II Plated.

NAS6204-10D - Same bolt as above with Drilled Thread.

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

National Aerospace Standard (NAS) machine bolts are commonly used in aircraft, space shuttles, military vehicles, drones, and other high-performance applications. They are offered in different series to meet application requirements.

Those of NAS 6203 through NAS 6220 series, superseding their NAS 11(xx) counterparts, are tension hexagon head high strength close tolerance short-thread alloy steel bolts with a minimum tensile strength of 160,000 psi and a minimum shear strength of 95,000 psi. 

They are made from different steel alloys such as 4140 (UNS G41400) or  4340 (UNS G43406) with either Cadmium Plate  Type II, Class 2 or Chromium Plate on shank only with all other surfaces cadmium plated.

Depending on the series they come in different nominal diameters in inches (e.g. NAS 6203 0.1875" (3/16"), NAS 6204 0.25" (1/4"), NAS 6205  0.3125" (5/16"), NAS 6206 0.375" (3/8"), NAS 6208 0.500" 1/2") or NAS 6210 0.625" (5/8") grips (in 1/16” increments beginning at 1/16”), thread and overall fastener lengths. They can be supplied undrilled or with drilled head and/or thread and with or without locking elements (nylon or equivalent). Sourced from quality manufacturers, these bolts are listed according to their series, and offered either as OEM parts or as parts of our own labelled (AVIATIONEU NEW ERA) product lines (see the respective listings). Sold in pieces or packs of specified number of bolts per pack designated by the number after the letters "PK" in the product reference code (SKU).

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

No Finish Code for Cadmium II plated bolts

"C" for Chromium plated bolts (shank only)

"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.

PN Examples:

NAS6204-10 - NAS 6204 Series Bolt, .2500-28 Thread, .625 Grip, Undrilled, Non-locking, Alloy Steel Cadmium II Plated.

NAS6204-10D - Same bolt as above with Drilled Thread.

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

National Aerospace Standard (NAS) machine bolts are commonly used in aircraft, space shuttles, military vehicles, drones, and other high-performance applications. They are offered in different series to meet application requirements.

Those of NAS 6203 through NAS 6220 series, superseding their NAS 11(xx) counterparts, are tension hexagon head high strength close tolerance short-thread alloy steel bolts with a minimum tensile strength of 160,000 psi and a minimum shear strength of 95,000 psi. 

They are made from different steel alloys such as 4140 (UNS G41400) or  4340 (UNS G43406) with either Cadmium Plate  Type II, Class 2 or Chromium Plate on shank only with all other surfaces cadmium plated.

Depending on the series they come in different nominal diameters in inches (e.g. NAS 6203 0.1875" (3/16"), NAS 6204 0.25" (1/4"), NAS 6205  0.3125" (5/16"), NAS 6206 0.375" (3/8"), NAS 6208 0.500" 1/2") or NAS 6210 0.625" (5/8") grips (in 1/16” increments beginning at 1/16”), thread and overall fastener lengths. They can be supplied undrilled or with drilled head and/or thread and with or without locking elements (nylon or equivalent). Sourced from quality manufacturers, these bolts are listed according to their series, and offered either as OEM parts or as parts of our own labelled (AVIATIONEU NEW ERA) product lines (see the respective listings). Sold in pieces or packs of specified number of bolts per pack designated by the number after the letters "PK" in the product reference code (SKU).

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

No Finish Code for Cadmium II plated bolts

"C" for Chromium plated bolts (shank only)

"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.

PN Examples:

NAS6204-10 - NAS 6204 Series Bolt, .2500-28 Thread, .625 Grip, Undrilled, Non-locking, Alloy Steel Cadmium II Plated.

NAS6204-10D - Same bolt as above with Drilled Thread.

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

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

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

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

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.

AVIATIONEU NEW ERA high tensile stainless steel threaded bolts are manufactured from AISI 410 stainless steel and heat-treated and machined to minimum of 110-ksi or 760 Mpa tensile strength. They are dual ASTM & ASME certified (ASTM A193 B6: Class 1 Stainless Steel, ASME B1.1 2A/3A Inch Unified Threads and B1.13M 6h Metric Coarse Threads). In addition to their high tensile strength, they exhibit excellent resistance to corrosion, good dimensional stability, durability as well as a long functional work life. They can be used in different industries demanding high tensile strength and corrosion resistance like marine, chemical & petrochemical etc. Sold in in packs (pk) of 25 bolts/pk in different head, body diameters and thread lengths in inches with Minimum Order Quantity (MOQ) 10 packs. Please refer to the attached specifications table. Appearing price is for reference only and differentiates based on wanted bolt sizes. Please contact us for a quotation.

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

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.

Close tolerance bolts, designed with a greater emphasis on measurement accuracy than other types of bolts, are commonly used in the aerospace manufacturing industry. They are threaded fasteners with a shank and head and a tolerance of just +0.000, -0.0005 inch as an acceptable range of variance. The shank is threaded, thus allowing them to be driven into a threaded hole. They intend to eliminate problems appearing when using traditional bolts which have a greater acceptable range of variance. Close tolerance bolts have closer shank tolerances than that of traditional bolts and fit more securely in threaded holes. For some fastening applications, traditional bolts may suffice. For sensitive fastening applications in which precision is required, close tolerance bolts are typically used. When selecting close tolerance instead of traditional bolts the drive type should be considered. Most close tolerance bolts have a recess within their head that supports a specific bit, such as a Phillips head bit. Regarding their threading, all close tolerance bolts, as well as traditional bolts, have threading. But the way in which the threading is designed may vary. Some bolts have more threading on their shank than others, and some bolts have finer threading than others.

Close tolerance bolts are offered in different materials with high-carbon steel being a common material used in their construction. 

Army & Navy (AN) close tolerance bolts are offered as part of our own labelled (AVIATIONEU NEW ERA) lines of fasteners. They are sourced from quality manufacturers and structured in different series (AN 173/174/175/176/178/180).

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

First Number after AN Basic designates the Diameter. 

"-" for Steel, Cad II plated, no head hole

"C" in place of (-) for Corrosion Resistant Steel (CRES)

"H" in place of (-) or after (C) for bolts with a head hole

"A" In the end of the PN  for bolts with no shank hole

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.

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. 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.

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.  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).

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.

HOWMET® AEROSPACE Inc. (formerly ARCONIC Inc.) develops and manufactures high performance, engineered products and solutions for the aerospace, industrial gas turbine, commercial transportation and oil and gas markets. HOWMET® FASTENING SYSTEMS product range under different brands offers the greatest breadth and depth of fastening solutions available including self-locking nuts, quick-release fasteners, draw latches, threaded inserts, lock-bolts, and structural blind fasteners.

HOWMET FASTENING SYSTEMS structural blind fasteners and lockbolts (including those under HUCK® brand) are designed to provide permanent, vibration-resistant, superior-quality joining solutions for use in aerospace and industrial applications. Suited for applications where the joints are integral to the structure, they offer high tensile, shear & clamp properties.  For additional information please refer to the Product Description section and the supplied documentation. Installation tool systems (separately listed) are also offered.

HI-SHEAR Fasteners are patented fasteners of HI-SHEAR CORPORATION (Patent Holder), subsidiary of LISI AEROSPACE, a manufacturer of advanced aerospace fasteners and installation equipment used in space, military and commercial vehicles. Depending on the fastener, they are made by quality fastener manufacturers (licensees) in different  countries including but not limited to LISI AEROSPACE companies, HOWMET ALCOA / SIMMONDS / FAIRCHILD, PCC  SPS, and others. 

The HI-SHEAR rivet pin range offers a versatile solution for most of structural assemblies. They consist a very common type of threaded fastener used for clearance, transition and low interference fit throughout the airframe (metallic and composite), from wings to fuselage, in engine fairings, and more. Easily installed from one side, by one person with conventional tooling.

HI-SHEAR rivet pin product portfolio includes the original HI-LOK™ (HL™) system, the latest HI-LITE™ (HST™) pins with an improved recess and HI-TIGUE™ (HLT™) pins with improved fatigue benefits. They can be used in shear and/or tension applications on plain or sloped surfaces and feature controlled preload, a wide range of sizes and variety of materials and coatings for installation in all structures.

Most fasteners are mainly loaded in shear. That should be the only way for rivets as their tension capability is relatively low. Whenever there is a substantial tension load in a fastener, a threaded bolt should be used.

Additional information is available in Product Description section and the supplied documentation.

These bolts are for use in Textron Lycoming aircraft engines. Supplied with our own Certificate of Conformance. If additional certification is required, please contact us as a respective charge may apply.

Blind Rivets are multi-piece rivet assemblies, capable of being installed from one side of the workpiece.Traditionally, blind rivets were used on aircraft leading edges, trailing edges, and close out areas which are limited to access to one side of the structure.  Current blind rivet usage has expanded to many additional areas of the aircraft in an effort to decrease labor expense and to address the ergonomic issues of solid riveting.

The CherryMAX® locked spindle blind rivets by CHERRY® AEROSPACE are the most reliable, high strength structural fasteners with visual inspectability in the world today. They are also known as "bulbed" fasteners due to their large blind side bearing surface, developed during the installation process. They feature a a visibly inspectable  "Safe-lock" locking collar for more reliable joint integrity, and their own installation washers, which eliminate the problems resulting from worn tool anvils. CherryMAX® rivets are used in thin sheet applications and in materials that may be damaged by other types of blind rivets. They meet the requirements of PS-CMR-3000 and can be supplied in 1/8" through 1/4" diameters in both nominal (CR3212 and CR3213 Series) and 1/64" oversize diameters (CR3242 and CR3243 Series). 

Please refer to the supplied documentation and the Product Description section for detailed information on CherryMAX® rivet and other blind rivets manufactured by CHERRY® AEROSPACE. 

Blind Rivets are multi-piece rivet assemblies, capable of being installed from one side of the workpiece.Traditionally, blind rivets were used on aircraft leading edges, trailing edges, and close out areas which are limited to access to one side of the structure.  Current blind rivet usage has expanded to many additional areas of the aircraft in an effort to decrease labor expense and to address the ergonomic issues of solid riveting.

The CherryLOCK® blind rivets by CHERRY® AEROSPACE come in below  mentioned types, and in different sizes, materials and strength levels. A complete range of recommended power tools, hand tools and pulling heads are also available.

CherryLOCK® ‘A’ Code “non-shift”, self-plugging blind rivets 

Single action, mechanically locked, wire-drawing fasteners providing excellent hole-fill and sheet take-up capability. They conform to the Procurement Specification NAS 1400 and Standards Pages NAS 1398 and NAS 1399.These rivets are offered in aluminum, monel and A-286 stainless steel materials in a wide variety of diameters and grip ranges. CherryLOCK® ‘A’ Code  "Wiredraw"  rivets are locked spindle flush fracturing structural rivets manufactured in 3/32", 1/8", 5/32", 3/16" and 1/4" diameters in 100° flush head and protruding head style configurations and offer grip ranges from .020 in the smaller diameters to 1.073 in the larger diameters. The 3/32" diameter rivet is available in A-286 only with grips ranging from .020 to .562. Rivets 1/8" diameter and larger have head markings to identify grip, material and manufacturer for ready inspection. The flush fracturing spindle eliminates the need for shaving and meets the flushness requirement of the NAS 1400 specification. These rivets are especially suited for sealing applications and joints requiring excellent sheet take-up and allow simple installation with a wide variety of Cherry® nonshifting and shifting tools. 

Both CherryLOCK® ‘A’ & Wiredraw Rivets rivets are designed to provide strong, reliable fastening solutions, but the choice between them may depend on specific application requirements, such as material compatibility, strength needs, and installation conditions. Both offer a wide grip range, making them versatile for different thicknesses.

Bulbed CherryLOCK® locked spindle and flush fracturing structural rivets

They consist a complete shear fastening system.  Their features can be utilized for optimum strength and performance in both thick and thin sheets. They provide the highest possible design integrity, particularly in double dimple or thin backside sheet applications. CherryLOCK® hydroshift installation tool systems are required for installation. They conform to Procurement Specification NAS1740 and Standards Pages NAS1738 and NAS1739.

For additional information on CherryLOCK® rivets and other blind rivets manufactured by CHERRY® AEROSPACE (separately listed) please refer to the supplied documentation and the Product Description section. 

The CHERRY® Nut-Plate family of fasteners offers an extensive range of head styles in a low cost, pull through style rivet. Rivet heads include the CCR/CCMR274, “Universal”, CCR/CCMR264, 100° Flush, and the CCR/CCMR244, 100° Reduced Flush head (NAS 1097). Sleeve materials include C1018 steel or A-286 CRES stainless steel. Single action installation tools are all that is required to complete this low cost fastening system. Recommended installation tools include the G29 hand tool, which is sold complete with pulling head, or the G902/G902-15 lightweight power tool with pulling heads sold separately.

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

CHERRY® AEROSPACE MAXIBOLT® Blind Bolts (also termed as rivets) are multi-piece assemblies, capable of being installed from one side of the workpiece. Typically used in higher strength aircraft structural areas they are offered as Maxibolt®,  Maxibolt® Plus and Titanium Maxibolt® Blind Bolts. They can be installed with the use of CHERRY® tools for a most reliable installation performance.

CHERRY® Maxibolt® Blind Bolts are supplied in alloy steel and A-286 CRES materials. They conform to MS90353/MS90354, and MS21140/MS21141 Standards, meet MIL-F-81177 and MIL-F-8975 requirements, and are listed in QPL81177 and QPL8975. Shear strength for the steel version is 112 KSI and  95 KSI for the A286 CRES version.  CHERRY® Maxibolt® Plus Blind Bolts are available in -5, -6, and -8 diameters and stainless steel, and titanium materials. One tool and pulling head installs all three diameters. Creating a larger blind side footprint, they provide excellent performance in thin sheet and non-metallic applications. The flush breaking stem eliminates shaving while the extended grip range accommodates different application thicknesses. CHERRY® Titanium Maxibolt® Blind Bolts feature expanded performance capabilities for metallic and composite blind fastening applications. They provide a flush, burr- free installation with no shaving required. The Titanium Maxibolt® bolts offer fast and consistent installation by utilizing single action tooling with a unique shift washer design. The all-titanium sleeve and stem are compatible with exotic composite materials. They cause no delamination of the exit side of the structure during installation, and offer a blind-side slope tolerance up to 7°.

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

RAPCO produces quality FAA-PMA approved replacement organic and metallic brake linings for Cleveland and McCauley brake assemblies on most general aviation aircraft. Organic linings are actually made from a semi metallic mix. RAPCO combines brass, copper and Kevlar fibers with a high temperature binding compound to provide outstanding performance and long service life. Most RAPCO organic linings have a built in wear indicator, which reduces the risk of damage to the brake disc and helps to optimize lining life. RAPCO organic linings are available in boxes of 10 or in organic lining kits containing the proper number of linings and rivets necessary for replacement on Cleveland or McCauley brake assemblies. They are convenient to have on hand when the need for relining occurs. Metallic lining replacements for the Cleveland brake assemblies are made of sintered steel, a specially developed process that fuses metallic particles to a steel carrier plate. RAPCO metallic linings offer long life and excellent braking performance.

RAPCO Brake Rivets are FAA-PMA approved quality tubular rivets produced from plated steel for mounting aircraft brake linings. The RAPCO RA825 Rivet Tool Kit is recommended for proper installation.

Please refer to the attached Application Guide for additional information.

SKYBOLT® stainless cowling fastener kits replace the old parts from other manufacturers originally installed on aircraft cowlings and access panels with exclusive SKYBOLT® CLoc®, ZLoc®, or ALoc® style stainless steel fasteners manufactured by SKYBOLT®. SKYBOLT® Cloc style fasteners are compatible with Camloc and are available in 2000 and 4000 series. ZLoc fasteners are compatible with Dzus and Aloc fasteners with Airloc ones. In addition SKYBOLT® SK2003 plate mounts upgrades those of J 7444 series commonly used in Cessna aircraft. SKYBOLT® kits for different aircraft models and year of construction are offered to cover all panels or certain portions of the engine cowling. The SKYBOLT® Cowling Fastener Kits will usually contain more of a selection than the aircraft may actually require so that a replacement project can efficiently move from start to finish. Other kits like the Trim and Fuel Tank Kit are also available.

Note: Alternative kits from competition may include less fasteners than those required for the replacement project. It is recommended that kit evaluations and price comparisons should be made on the basis of the hardware included in each kit.

ATI® TOOLS 107A series flush straight drive rivets are manufactured from S2 high-grade shock-resistant steel and machined in accordance with MIL-STD GGG-R-425. Large radii at critical points enable these rivets to withstand continuous rugged use.They are slightly crowned with a highly polished face designed for rapid flush riveting where a smooth skin surface is essential and feature large radii at critical points to prevent breakage, protection with plastic coating to prevent damage during shipment and storage, blended radius between cup and chamfer with no sharp edges, which coin or mar skin, highly polished precision cup, free of machine marks and ridges and chamfered corners. Shank diameter 0.401".  Different sizes are available serve specification requirements for face diameters and lengths.

ATI® TOOLS 110C series flush straight drive rivets with rubber guard are manufactured from S2 high-grade shock-resistant steel and machined in accordance with MIL-STD GGG-R-425. They feature protection with plastic coating to prevent damage during shipment and storage, blended radius between cup and chamfer with no sharp edges, which coin or mar skin, highly polished precision cup, free of machine marks and ridges and chamfered corners. Shank diameter 0.401".  Different sizes are available serve specification requirements for face diameters and lengths.

ATI® TOOLS 100A series (straight drive) and 101A series (offset drive) AN470/MS20470 universal-head cup shaped  rivets are manufactured from S2 high-grade shock-resistant steel and machined in accordance with MIL-STD GGG-R-425. Respective flush head rivets of ATI® TOOLS 100A/101A series are designated by the letter "F" after the series number (i.e. 100AF/101AF respectively. They feature protection with plastic coating to prevent damage during shipment and storage, blended radius between cup and chamfer with no sharp edges, which coin or mar skin, highly polished precision cup, free of machine marks and ridges and chamfered corners. Shank diameter 0.401". Available in different rivet sizes, body diameters and lengths in inches.

ATI® TOOLS 106A series flush swivel type rivets are manufactured from S2 high-grade shock-resistant steel and machined in accordance with MIL-STD GGG-R-425. They feature protection with plastic coating to prevent damage during shipment and storage, blended radius between cup and chamfer with no sharp edges, which coin or mar skin, highly polished precision cup, free of machine marks and ridges and chamfered corners. Rivet Type: Flush Swivel Type. Shank diameter 0.401".  

ATI® TOOLS 105A series AN470/MS20470 universal-head cup shaped double offset drive rivets are manufactured from S2 high-grade shock-resistant steel and machined in accordance with MIL-STD GGG-R-425. They feature protection with plastic coating to prevent damage during shipment and storage, blended radius between cup and chamfer with no sharp edges, which coin or mar skin, highly polished precision cup, free of machine marks and ridges and chamfered corners. Rivet Type: AN470/MS20470 universal-head. Shank diameter 0.401".  Available in different rivet sizes, body diameters and lengths in inches.

ATI® TOOLS ATIST1111BK3 anti-slip rivet set, H13 magnetic particle tested. Manufactured to Boeing® specifications. It features polyurethane rim to prevent slipping and damage to skin surfaces. Shank diameter 0.401". Length 2-1/2″. Face diameter 1-1/4″.

Different bolts used on Textron Aviation Cessna, Beechcraft and Hawker aircraft. Also available as FAA-PMA approved parts from other manufacturers.

Different pins, rivet pins & collars used on Textron Aviation Cessna, Beechcraft and Hawker aircraft. Also available are alternative respective parts from other manufacturers. HI-SHEAR HI-LOK™ pins and collars are catalogued as TEXTRON AVIATION part numbers but the alternative HI SHEAR part number is also included in the product reference number (SKU). When fasteners are sold in packs the specified number of pieces per pack is designated after the letters "PK" in the product SKU.

MONOGRAM AEROSPACE FASTENERS® is part of TRIMAS AEROSPACE™ which serves the world’s markets with industry leading products including specialty fasteners, temporary fasteners for fixturing and alignment, fastener installation tools, finishing and removal tools and the design of innovative fastening solutions for the aerospace industry. The blind rivet portfolio of MONOGRAM AEROSPACE FASTENERS® includes:

The Visu-Lok® family of high strength fasteners available to 112 KSI shear. Designed for use in metal structures they address the need for cost-effective one-sided fastener installation as they are fully installed and verified from one side of the structure. Features: High strength. ease of installation, self-locking resisting loosening in severe vibration, available in a wide range of materials, unified or metric sizes, head styles, including oversize and close tolerance interference fit configurations, compliance with NAS standards, easily adapted to robotic or automated installation.

Composi-Lok® fasteners, industry's standard for blind fastening of composite laminates but equally well-suited to metal structures, they  provide superior joint integrity. Approved on virtually all composite airframe programs throughout the world. Features: large blind upset eliminating composite damage, easy, labor-saving one-sided installation, controlled clamp-up, compatible with graphite, available in titanium or CRES materials to resist galvanic corrosion, visual locking, fuel-tight sealing capability.

Radial-Lok® unique hole-filling, high strength blind fasteners. With their uniform radial expansion throughout the entire fastener grip, they are uniquely suited to offer both enhanced fatigue strength & lightning strike damage protection. Uniform radial expansion throughout the entire length of the clearance fit hole. Features: interference fits to .006″, enhanced fatigue life, eliminate costly hole preparation, clearance fit before installation, easy one-sided installation, high clamp-up,  large blind-side upset, tighter joints, ideal for aluminum and composite applications, available in 3/16″ through 3/4″ diameters, including oversizes, .100″ grip accommodation, 7-deg. blind slope capability.

OSI-Bolt®, the only blind bolts capable of equivalent usage with solid shank bolts offering a full 1.5D bearing area. Direct replacement for solid shank pin-and-collar systems. Suited for primary structures they deliver strength with the added advantages of simple one-sided installation & a flush break-off for installed cost savings in both metal and composite structures. The updated titanium Ti-OSI® combines all these advantages in a weight-saving configuration. Features: availability in 95 & 112 KSI shear and a variety of hex, tension, shear, and protruding head styles, diameters from 5/32″ to 1/2”, 1/64” and 1/32” oversize availability, 1/16” grip with +/- .015” capability, “Vise-like” sheet take-up, flat, uniform blind-side footprint ...