P/N: 600-75102-21
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 600-75102-21 is a Power Control Unit (PCU) for elevator pitch control on Bombardier Challenger 600/601 series aircraft. This hydraulic actuator converts pilot control inputs into commanded elevator surface movement within the tailplane flight-control assembly. The unit integrates with the aircraft's hydraulic system to modulate pressure and control elevator deflection during flight operations.
Installation requires verification against the Illustrated Parts Catalog and functional testing per the Aircraft Maintenance Manual.
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 600-75102-21 is a Power Control Unit (PCU) for elevator pitch control on Bombardier Challenger 600/601 series aircraft. This hydraulic actuator converts pilot control inputs into commanded elevator surface movement within the tailplane flight-control assembly.
The PCU, ELEVATOR 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 PCU, ELEVATOR. 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 600-75102-21.