P/N: 38349-018
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 |
|---|---|
| As Removed | 1 Available |
The 38349-018 is a forward tip-fin assembly for the dorsal fin on an aircraft's vertical stabilizer. This fairing component transitions aerodynamically at the fuselage junction while protecting fasteners and leading edge structure. Typically aluminum construction with smooth external surfaces to minimize airflow disruption.
Installed as a replacement during routine airframe maintenance and structural repairs. Verify compatibility with your aircraft's Illustrated Parts Catalog and follow the applicable maintenance manual for installation procedures and torque specifications.
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 38349-018 is a forward tip-fin assembly for the dorsal fin on an aircraft's vertical stabilizer. This fairing component transitions aerodynamically at the fuselage junction while protecting fasteners and leading edge structure.
The TIP-FIN, FORWARD ASSY 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: As Removed. 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 TIP-FIN, FORWARD ASSY. 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 38349-018.