P/N: s2226-2
Category: Lighting
This product requires a custom quote. Please contact our sales team for pricing information or submit an RFQ (Request for Quote).
| Condition | Stock |
|---|---|
| New | 10 Available |
The s2226-2 is a loop clamp designed to secure wire bundles and small conduits to aircraft structure. This steel clamp restrains lighting harnesses along frames, bulkheads, and fuselage sections, preventing movement during flight vibration and maintenance access. Installation uses standard aerospace fasteners with appropriate spacing per FAA AC 43.13-1B guidelines.
Verify your aircraft's Illustrated Parts Catalog for specific configuration and mounting requirements. The loop design accommodates various bundle diameters while maintaining secure retention in cockpit, cabin, and exterior lighting circuits.
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 s2226-2 is a loop clamp designed to secure wire bundles and small conduits to aircraft structure. This steel clamp restrains lighting harnesses along frames, bulkheads, and fuselage sections, preventing movement during flight vibration and maintenance access.
The CLAMP may be available as an OEM (Original Equipment Manufacturer) or PMA (Parts Manufacturer Approval) part depending on condition and source. Both carry FAA certification for airworthiness. Currently available in: New. Contact us for sourcing details.
Installation hardware requirements vary by application. Check your aircraft's Structural Repair Manual (SRM) or Illustrated Parts Catalog (IPC) for the complete installation kit requirements for the CLAMP. We stock related hardware and can help identify companion parts.
Yes, we ship airframe components worldwide. International orders typically arrive within 3-14 business days depending on destination. Export documentation and customs forms are included. Contact us for international shipping quotes on the s2226-2.