P/N: 8295-1
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 | 2 Available |
The 8295-1 is an electromechanical actuator that positions the oil cooler flap to regulate airflow and engine oil temperature. This unit converts electrical input into linear motion, driving linkage that modulates the cooler door under cockpit command or automatic temperature control. Mounted in the engine cooling system, it maintains optimal oil temperatures during varying flight conditions.
Installation requires verification against the aircraft's Illustrated Parts Catalog and compliance with the applicable maintenance manual specifications.
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 8295-1 is an electromechanical actuator that positions the oil cooler flap to regulate airflow and engine oil temperature. This unit converts electrical input into linear motion, driving linkage that modulates the cooler door under cockpit command or automatic temperature control.
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 OIL COOLER FLAP ACTUATOR 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 OIL COOLER FLAP ACTUATOR 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.