Aeronautical Standard
Rivet, Solid, Universal Head (2117-T4 Alloy) B0205016AD4-4S
Excludes freight, hazmat, and applicable taxes.
Available Alternates & Conditions
1 OptionsTechnical Description
Premium aerospace-grade solid aluminum alloy rivet (PN: B0205016AD4-4S) featuring a precision-engineered universal head profile. Manufactured from high-strength 2117-T4 aluminum alloy (AD material code) per strict airworthiness standards to provide optimal shear performance, high fatigue life, and absolute joint structural integrity. Designed with a close-tolerance straight cylindrical shank engineered for cold-working and compression bucking directly into pre-drilled aircraft structural sheets without requiring subsequent heat treatment or solution annealing. Features a passivated, corrosion-resistant surface finish perfectly optimized for internal airframe framing, fuselage skin attachment, and main structural bracket assemblies on civil and commercial aircraft.
Component Specifications
Logistics & Compliance
Ships globally from approved aerospace distribution centers. Items marked with EASA Form 1 or FAA 8130-3 dual release are guaranteed traceable. Subject to standard AOG dispatch times.
Available Inventory Conditions
Review specific stock levels, conditions, and available certifications for this component.
| Condition | Certifications | Stock Limit | Unit Price |
|---|---|---|---|
| NE | Trace Only | 1 EA | KES 450.00 |
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