STIFFENER (P/N 407-704-027-113) - New
P/N: 407-704-027-113
Category: Plates, Doublers & Reinforcements
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Available Inventory
| Condition | Price | Stock |
|---|---|---|
| New | $240.00 | 1 Available |
Product Description
The 407-704-027-113 is a structural stiffener designed to reinforce airframe skins and panels in aircraft cowling assemblies. This OEM component reduces panel flex, local buckling, and vibration transmission under flight loads. Typically fabricated from aluminum alloy, the stiffener attaches via riveted joints following aircraft maintenance manual specifications.
Installation requires verification of serial-number applicability and proper alignment with existing airframe structure. Used in general aviation and business aircraft cowling reinforcement.
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 STIFFENER (P/N 407-704-027-113)?
The 407-704-027-113 is a structural stiffener designed to reinforce airframe skins and panels in aircraft cowling assemblies. This OEM component reduces panel flex, local buckling, and vibration transmission under flight loads.
What conditions is the 407-704-027-113 available in?
The 407-704-027-113 is currently available in the following conditions: New. Each condition reflects the part's maintenance history and certification status per FAA standards.
How do I get pricing for the 407-704-027-113?
The 407-704-027-113 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 407-704-027-113?
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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