P/N: nas1352c04-16
Category: Connectors
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 | 52 Available |
The NAS1352C04-16 is a socket head cap screw with internal hex drive and 4-40 UNRC class 3A threads. Manufactured from corrosion-resistant 18-8 stainless steel per FF-S-86 aerospace standards, this fastener provides reliable fastening in aircraft avionics brackets and access panels where low head clearance is critical. The compact socket head design allows installation in tight spaces without protruding fastener heads.
Installation requires verification of thread size and length against the aircraft Illustrated Parts Catalog and adherence to maintenance manual procedures.
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 NAS1352C04-16 is a socket head cap screw with internal hex drive and 4-40 UNRC class 3A threads. Manufactured from corrosion-resistant 18-8 stainless steel per FF-S-86 aerospace standards, this fastener provides reliable fastening in aircraft avionics brackets and access panels where low head clearance is critical.
Avionics compatibility depends on your aircraft model and existing installation. The SCREW: SOCKET HD is available in: New Surplus. We recommend checking your aircraft's wiring diagrams and STC documentation, or contact our avionics team for compatibility assistance.
Availability of an FAA 8130-3 tag depends on the part condition. Overhauled and repaired units typically include 8130-3 documentation. As-removed units may include a removal tag with trace history. Contact us for specific documentation on the condition you need.
We can arrange bench testing through our network of FAA-certified repair stations. Call (904) 998-9101 for testing availability and turnaround times, or submit an RFQ with your specific requirements.