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Cherry E-Z Buck

Cherry · Solid rivet

Composite-optimizedBoth sides needed

Lightweight ductile titanium rivet; Hollow-End variant sets in composite without delaminating.

aka E-Z Buck · Ti/Cb rivet · Hollow-End E-Z Buck

ACCESS SIDEBLIND SIDE

Schematic cross-section, not to scale. Bucked shop head — needs back-side access.

Shear

48–52 ksi

Blind bulb

n/a

Max service

≤ 600°F

Lead-time risk

Medium

Diameters

3/32, 1/8, 5/32, 3/16, 1/4"

Head styles

  • Protruding
  • 100° flush

Standards

  • NAS (Cherry E-Z Buck series)

Materials & galvanic compatibility vs CFRP

AlloyShearvs CFRPNotes
Titanium (Ti-6Al-4V)50 ksilowTi/Cb (titanium-niobium), ductile

Install tooling & training

Tool
Rivet gun + bucking bar (both sides)
Special / proprietary
Standard tooling
Training
Standard riveting; composite bucking needs care.
Inspection
Shop-head form; Hollow-End: soft bulge, no splitting.

Standard bucking; the Hollow-End variant uses a soft upset so it can be set in composite without splitting the laminate.

Sourcing

Lead-time risk: Medium

  • Peerless Aerospace Fastener

    Largest dedicated aerospace fastener inventory; approved source for major OEMs + DoD; multi-year fixed pricing, bonded storage, designated hold-shelf, min/max + safety-stock programs.

  • Incora

    Authorized distributor for 60+ manufacturers; AS9100 / EN9120 / FAA AC 00-56; strong vendor-managed-inventory (VMI) and kitting programs.

  • Boeing Distribution (Aviall / KLX)

    Formed from Aviall + KLX; broadest catalog coverage for OEM/MRO/airline; deep stock on commodity NAS/MS hardware.

Need a price or lead time?

Build a spec-complete RFQ and send it to distributors who stock Cherry E-Z Buck.

Strengths

  • +Light Ti/Cb (~33% lighter than Monel)
  • +Ductile — minimal sheet distortion
  • +Corrosion-resistant, no coating

Trade-offs

  • Needs back-side access (bucking)
  • Lower shear (~50 ksi)
  • Not removable

Typical applications

  • · Weight-critical riveted structure (lighter than Monel)
  • · Fatigue-critical, ductile joints
  • · Composite assemblies (Hollow-End soft-upset variant)

Sources