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Military Rivets — Solid & Blind

Rivets are permanent mechanical fasteners essential for aircraft skin, aerodynamic surfaces, and heavy structural panel joining — installed by deforming one end of the fastener to clamp two or more sheets together without threads, welding, or adhesive.

Configurations: Solid, Blind Materials: Aluminum Alloy, Titanium-Columbium Governing Spec: MS20426 (Solid, Countersunk)

Rivet Configurations We Manufacture

Solid Rivets

Installed with access to both sides of the joint using a rivet gun and bucking bar — the traditional aircraft-skin and structural fastening method, offering the highest joint strength.

Blind Rivets

Installed from one side only using a pull-mandrel tool, used where the back side of the joint isn't accessible — common in enclosed structures and secondary assembly.

Overview

MS20426 covers solid rivets with a 100° countersunk "precision" head, allowing the installed rivet to sit flush with the surrounding surface — the standard choice for aerodynamically smooth aircraft skin panels. The most common material variant, "AD" (2117-T4 aluminum alloy), balances strength and workability, while a softer "A" (1100 pure aluminum) variant is available where greater ductility is needed during the driving/bucking process.

Solid rivets require access to both sides of the joint: one end is pre-formed with a factory head, and the protruding shank end is upset (bucked) into a second head using a rivet gun on one side and a bucking bar backing it up on the other. Blind rivets, by contrast, are engineered to be installed and set entirely from one side, using a mandrel that's pulled through the rivet body to form the back-side head — critical for closed-box structures, panels, or assemblies where the far side simply can't be reached.

  • MS20426 has been folded into the AIA/NAS-maintained NASM20426 document, though "MS20426" part numbers remain the universal industry callout.
  • A closely related family, MS20427, covers the same 100° countersunk head style in carbon steel, corrosion resistant steel, Monel, and copper for applications where aluminum isn't suitable.

Solid vs. Blind: Which Do You Need?

Both Sides Accessible: Solid rivets under MS20426 deliver the highest joint strength and are the standard for aircraft skin panels and primary structure — but require a bucking bar on the back side during installation.

Applicable Standards

Explore the individual military rivet specifications Ananka manufactures to.

Military Rivets — Frequently Asked Questions

What does the countersink angle on MS20426 rivets do?

The 100° countersink lets the installed rivet head sit flush with the surrounding surface once bucked, minimizing aerodynamic drag on aircraft skin panels compared to a protruding round head.

What's the difference between "AD" and "A" material codes?

"AD" denotes 2117-T4 aluminum alloy, the most common MS20426 rivet material for its balance of strength and workability. "A" denotes 1100 pure aluminum, a softer, more ductile option used where extra formability during installation is needed.

Are solid rivets stronger than blind rivets?

Generally yes — solid rivets, fully upset with a bucking bar, provide a more consistent and typically stronger joint than blind rivets, which is why solid rivets remain the standard for primary aircraft structure wherever both sides of the joint are accessible.

Need Military Rivets to Print?

Ananka Fasteners manufactures solid rivets to MS20426 with full material traceability and Mill Test Certification on every lot.

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