P/N: 100-525-0100
Category: Valves & 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 100-525-0100 is an electromechanical pitch trim actuator that provides linear motion to position the elevator trim tab. This unit operates within the aircraft's longitudinal control system to relieve control forces and maintain pitch attitude during flight. The actuator drives the elevator trim linkage through coordinated electrical and mechanical action.
Installation requires verification against the aircraft's Illustrated Parts Catalog and rigging per the maintenance manual and FAA AC 43.13-1B guidance.
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 100-525-0100 is an electromechanical pitch trim actuator that provides linear motion to position the elevator trim tab. This unit operates within the aircraft's longitudinal control system to relieve control forces and maintain pitch attitude during flight.
Hydraulic component compatibility depends on the aircraft system design. Common aviation hydraulic fluids include MIL-PRF-5606 (mineral-based), MIL-PRF-83282 (synthetic), and Skydrol (phosphate ester). Verify the ACTUATOR, PITCH TRIM against your aircraft maintenance manual for fluid compatibility.
Overhauled and repaired hydraulic components are pressure-tested per manufacturer specifications and include 8130-3 documentation. The ACTUATOR, PITCH TRIM is available in: As Removed. Contact us for test documentation on your selected condition.
In-stock hydraulic components ship same business day before 3 PM EST. We provide 24/7 AOG support at (904) 998-9101 for urgent hydraulic system needs. RFQ submissions are typically quoted within 24 hours.