P/N: 45a22002-642
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 45a22002-642 is an elevator assembly serving as the primary pitch-control surface on the horizontal stabilizer. This hinged surface responds to control-column inputs to adjust aircraft nose attitude during flight. Installed on the empennage for longitudinal control, the assembly requires rigging and balance verification per maintenance manual specifications.
Commonly found on Hawker 400 series aircraft. Before installation, verify compatibility with your aircraft's Illustrated Parts Catalog and follow FAA AC 43.13-1B accepted practices for proper alignment and secure attachment.
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 45a22002-642 is an elevator assembly serving as the primary pitch-control surface on the horizontal stabilizer. This hinged surface responds to control-column inputs to adjust aircraft nose attitude during flight.
The ELEVATOR ASSEMBLY 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 ELEVATOR ASSEMBLY. 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 45a22002-642.