P/N: 212-030-388-019s
Category: Plates, Doublers & Reinforcements
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 | 2 Available |
The 212-030-388-019s is a structural doubler plate designed to reinforce aircraft airframe sheet metal around cutouts and high-load areas. This aluminum reinforcement component distributes concentrated stresses and supports damage containment in fuselage, wing, and control surface repairs. Typically riveted to parent structure using standard aerospace fasteners, the doubler transfers loads across a wider area to prevent crack propagation.
Installation follows FAA AC 43.13-1B acceptable methods and the aircraft's Structural Repair Manual. Verify applicability through the Illustrated Parts Catalog before use.
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 212-030-388-019s is a structural doubler plate designed to reinforce aircraft airframe sheet metal around cutouts and high-load areas. This aluminum reinforcement component distributes concentrated stresses and supports damage containment in fuselage, wing, and control surface repairs.
The 212-030-388-019s is currently available in the following conditions: New Surplus. Each condition reflects the part's maintenance history and certification status per FAA standards.
The 212-030-388-019s requires a custom quote. Submit a Request for Quote (RFQ) through our website or call our sales team at (904) 998-9101 for immediate pricing assistance.
Yes, we offer same-day processing on in-stock items and provide 24/7 AOG (Aircraft on Ground) support for urgent needs. Standard, expedited, and overnight shipping options are available.