P/N: 25-8gf-227-1a
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 | 2 Available |
The 25-8gf-227-1a is a tail cone assembly that closes the aft fuselage and streamlines airflow over the empennage. This structural-aerodynamic component reduces base drag while maintaining aerodynamic efficiency during flight. Constructed to OEM specifications, the tail cone integrates with the fuselage skin and empennage structure.
Installation follows the Aircraft Maintenance Manual (AMM), Structural Repair Manual (SRM), or FAA AC 43.13-1B guidance. Verify compatibility with your aircraft's Illustrated Parts Catalog before installation.
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 25-8gf-227-1a is a tail cone assembly that closes the aft fuselage and streamlines airflow over the empennage. This structural-aerodynamic component reduces base drag while maintaining aerodynamic efficiency during flight.
The TAIL CONE 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 TAIL CONE. 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 25-8gf-227-1a.