P/N: 25-8te3-1a
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 25-8te3-1a is a port elevator tab assembly for horizontal tail pitch control. This component mounts on the left-side elevator tab linkage and provides aerodynamic trim or balance adjustment during flight. The assembly interfaces with standard AN/MS fasteners per aircraft design documentation.
Installation requires rigging in accordance with the aircraft maintenance manual and verification against the Illustrated Parts Catalog for your specific airframe. Proper tab assembly alignment ensures coordinated pitch control and maintains elevator effectiveness.
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 25-8te3-1a is a port elevator tab assembly for horizontal tail pitch control. This component mounts on the left-side elevator tab linkage and provides aerodynamic trim or balance adjustment during flight.
The TAB ASSEMBLY PORT - ELEVATOR TAB 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 TAB ASSEMBLY PORT - ELEVATOR TAB. 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 25-8te3-1a.