P/N: 96-620005-630
Category: Flight Controls
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 96-620005-630 is a horizontal or vertical stabilizer assembly for aircraft empennage systems. This tail surface provides aerodynamic stability in pitch or yaw and supports elevator or rudder control surface attachments. Constructed from aluminum alloy for lightweight strength, the stabilizer maintains aircraft trim and damping characteristics during flight.
Installation follows aircraft maintenance manual procedures and 14 CFR Part 43 requirements. Verify compatibility with the aircraft's Illustrated Parts Catalog before return to service.
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 96-620005-630 is a horizontal or vertical stabilizer assembly for aircraft empennage systems. This tail surface provides aerodynamic stability in pitch or yaw and supports elevator or rudder control surface attachments.
The STABILIZER 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 STABILIZER. 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 96-620005-630.