TOP HAT (P/N 6ca2541-45) - New Surplus
P/N: 6ca2541-45
Category: General Aircraft Parts
This product requires a custom quote. Please contact our sales team for pricing information or submit an RFQ (Request for Quote).
Available Inventory
| Condition | Stock |
|---|---|
| New Surplus | 1 Available |
Product Description
The 6ca2541-45 is a hat-section structural stiffener for aircraft fuselage panels. This aluminum profile features flanges and a web that create a rigid cap, increasing skin stiffness and distributing concentrated loads across the panel surface. Installed to locally reinforce fuselage skin areas subject to stress concentration or fatigue.
Installation requires approved fasteners, sealant per structural repair manual specifications, and adherence to maintenance data to maintain structural continuity and corrosion protection.
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.
Frequently Asked Questions
What is the TOP HAT (P/N 6ca2541-45)?
The 6ca2541-45 is a hat-section structural stiffener for aircraft fuselage panels. This aluminum profile features flanges and a web that create a rigid cap, increasing skin stiffness and distributing concentrated loads across the panel surface.
What conditions is the 6ca2541-45 available in?
The 6ca2541-45 is currently available in the following conditions: New Surplus. Each condition reflects the part's maintenance history and certification status per FAA standards.
How do I get pricing for the 6ca2541-45?
The 6ca2541-45 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.
Do you offer expedited shipping for the 6ca2541-45?
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.
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