P/N: 600-75102-21
Category: Actuators
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 600-75102-21 is currently available in the following conditions: As Removed. Each condition reflects the part's maintenance history and certification status per FAA standards.
The 600-75102-21 requires a custom quote. Submit a Request for Quote (RFQ) through our website or call our sales team at (904) 998-9101 for immediate pricing assistance.
Yes, we offer same-day processing on in-stock items and provide 24/7 AOG (Aircraft on Ground) support for urgent needs. Standard, expedited, and overnight shipping options are available.