P/N: 27-41044-013
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 | 1 Available |
The 27-41044-013 is a lower stiffener reinforcing element for aircraft fuselage or wing lower skin panels. This structural component distributes aerodynamic and operational loads across the skin surface, reducing panel flexing and maintaining airframe integrity. Typically fabricated from aluminum alloy and installed using AN/MS fasteners with riveted joints per OEM specifications.
Installation follows aircraft maintenance manual procedures and IPC documentation, or FAA AC 43.13-1B acceptable methods when OEM data is unavailable. Common on general aviation and transport aircraft where skin stiffness is critical to structural performance.
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 27-41044-013 is a lower stiffener reinforcing element for aircraft fuselage or wing lower skin panels. This structural component distributes aerodynamic and operational loads across the skin surface, reducing panel flexing and maintaining airframe integrity.
The 27-41044-013 is currently available in the following conditions: New Surplus. Each condition reflects the part's maintenance history and certification status per FAA standards.
The 27-41044-013 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.