P/N: 390-110206-0002
Category: Circuit Breakers & Fuses
This product requires a custom quote. Please contact our sales team for pricing information or submit an RFQ (Request for Quote).
| Condition | Stock |
|---|---|
| Serviceable | 1 Available |
The 390-110206-0002 is a forward wing-to-fuselage link assembly that connects the wing root to the fuselage structure at the primary attachment point. This structural component transmits flight loads, landing loads, and bending forces between the wing and fuselage during all phases of operation. Installation requires standard AN/NAS/MS fasteners and follows aircraft maintenance manual procedures.
Verify part compatibility in the Illustrated Parts Catalog before installation. Used in general aviation and commercial aircraft where forward wing attachment reinforcement is required.
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 390-110206-0002 is a forward wing-to-fuselage link assembly that connects the wing root to the fuselage structure at the primary attachment point. This structural component transmits flight loads, landing loads, and bending forces between the wing and fuselage during all phases of operation.
Avionics compatibility depends on your aircraft model and existing installation. The LINK ASSEMBLY-WING TO FUSELAGE,FWD is available in: Serviceable. 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.