P/N: 96-620005-629
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 |
Part 96-620005-629 is a stabilizer assembly for the aircraft empennage, comprising aluminum skins, spars, and ribs that form the tail structure. This assembly maintains pitch or yaw stability during flight by providing aerodynamic surfaces for elevator or rudder attachment. Installed in the tail section per aircraft maintenance manual specifications, the stabilizer assembly is verified against the Illustrated Parts Catalog before fitment and rigging.
Critical for directional and pitch control in general aviation aircraft.
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.
Part 96-620005-629 is a stabilizer assembly for the aircraft empennage, comprising aluminum skins, spars, and ribs that form the tail structure. This assembly maintains pitch or yaw stability during flight by providing aerodynamic surfaces for elevator or rudder attachment.
The STABILIZER ASSEM 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 ASSEM. 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 96-620005-629.