P/N: hl10vf6-4
Category: Fasteners & Hardware
This product requires a custom quote. Please contact our sales team for pricing information or submit an RFQ (Request for Quote).
| Condition | Stock |
|---|---|
| New Surplus | 19 Available |
The HL10VF6-4 is a titanium alloy Hi-Lok rivet pin engineered for structural airframe clamping applications. This protruding-head shear fastener delivers precise preload control when installed with a compatible Hi-Lok collar, typically HL70 series. Material conforms to AMS4928/AMS4967 specifications, ensuring high strength-to-weight performance in aircraft assembly.
Installation requires torquing per the aircraft structural repair manual to achieve controlled clamp load across fuselage, wing, and empennage joints. Used where repeatable fastening accuracy and vibration resistance are critical.
Please note: Product descriptions are provided for informational purposes. Always refer to your aircraft's Illustrated Parts Catalog (IPC) to verify part compatibility and specifications.
The HL10VF6-4 is a titanium alloy Hi-Lok rivet pin engineered for structural airframe clamping applications. This protruding-head shear fastener delivers precise preload control when installed with a compatible Hi-Lok collar, typically HL70 series.
Aircraft hardware is manufactured to military and aviation specifications. The RIVET conforms to its applicable AN (Air Force-Navy), MS (Military Standard), or NAS (National Aerospace Standard) specification. Contact us for specific specification details.
Aviation hardware is available in various materials including cadmium-plated steel, stainless steel, aluminum alloy, and titanium depending on the application. Contact us for material certification and specifications for the hl10vf6-4.
Yes, we sell hardware in various quantities from single units to bulk lots. The RIVET is available in: New Surplus. Submit an RFQ for volume pricing or call (904) 998-9101 for quantity availability.