P/N: 6231100-8
Category: Terminals & Splices
This product requires a custom quote. Please contact our sales team for pricing information or submit an RFQ (Request for Quote).
| Condition | Stock |
|---|---|
| As Removed | 2 Available |
The 6231100-8 is a splice plate designed to join adjacent aircraft structural members and restore load continuity at repair joints. This component supports sheet-metal repairs and splices performed according to FAA AC 43.13-1B standards. Installed during airframe stringer splice maintenance, the plate transfers loads across the joint while maintaining structural integrity.
Installation requires approved rivet or bolt patterns with proper edge distances per the aircraft structural repair manual. Commonly fabricated from aluminum alloy stock, the splice plate reinforces the joint area and prevents stress concentration at the repair interface.
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 6231100-8 is a splice plate designed to join adjacent aircraft structural members and restore load continuity at repair joints. This component supports sheet-metal repairs and splices performed according to FAA AC 43.
Avionics compatibility depends on your aircraft model and existing installation. The SPLICE PLT is available in: As Removed. 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.