P/N: 0753011-1
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 0753011-1 is a heat valve assembly for aircraft engine thermal management systems. This valve regulates coolant or fluid flow through engine cooling passages based on temperature changes, maintaining optimal operating temperatures during flight. Commonly installed in piston and turboprop engine installations where precise temperature control prevents overheating and ensures consistent engine performance.
The valve opens and closes automatically as engine temperature fluctuates, directing fluid through bypass or primary cooling circuits. Used in general aviation and corporate aircraft cooling systems.
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 0753011-1 is a heat valve assembly for aircraft engine thermal management systems. This valve regulates coolant or fluid flow through engine cooling passages based on temperature changes, maintaining optimal operating temperatures 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 VALVE HEAT 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 VALVE HEAT 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.