P/N: 407-704-027-113
Category: Structural Components
This product requires a custom quote. Please contact our sales team for pricing information or submit an RFQ (Request for Quote).
| Condition | Stock |
|---|---|
| New | 1 Available |
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.
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.
The STIFFENER may be available as an OEM (Original Equipment Manufacturer) or PMA (Parts Manufacturer Approval) part depending on condition and source. Both carry FAA certification for airworthiness. Currently available in: New. Contact us for sourcing details.
Installation hardware requirements vary by application. Check your aircraft's Structural Repair Manual (SRM) or Illustrated Parts Catalog (IPC) for the complete installation kit requirements for the STIFFENER. We stock related hardware and can help identify companion parts.
Yes, we ship airframe components worldwide. International orders typically arrive within 3-14 business days depending on destination. Export documentation and customs forms are included. Contact us for international shipping quotes on the 407-704-027-113.