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TIP FIN (P/N 65345-803) - New Surplus

P/N: 65345-803

Category: Structural Components

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Available Inventory

Condition Stock
New Surplus 1 Available

Product Description

The 65345-803 is a tip fin aerodynamic surface installed at wing or stabilizer tips on Piper aircraft. This out-of-plane winglet influences vortex behavior and enhances directional stability during flight. Constructed from aluminum for lightweight durability, the fin mounts to lifting surface extremities per aircraft maintenance manual specifications.

Installation requires verification in the Illustrated Parts Catalog to ensure proper compatibility with your airframe configuration.

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 TIP FIN (P/N 65345-803)?

The 65345-803 is a tip fin aerodynamic surface installed at wing or stabilizer tips on Piper aircraft. This out-of-plane winglet influences vortex behavior and enhances directional stability during flight.

Is the 65345-803 a PMA or OEM part?

The TIP FIN 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 Surplus. Contact us for sourcing details.

Does the 65345-803 include installation hardware?

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 TIP FIN. We stock related hardware and can help identify companion parts.

Can the 65345-803 be shipped internationally?

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 65345-803.

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