P/N: 311851201a
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 311851201a is a flow divider valve for aircraft fuel-injected piston engines. This component splits metered fuel from the servo into balanced outlets feeding individual injector nozzles, ensuring even cylinder delivery across the engine. Commonly called a fuel manifold or spider, it mounts between the fuel servo and injection system.
The valve provides positive fuel cutoff during engine shutdown. Installation requires strict adherence to engine maintenance manual specifications and IPC compatibility verification. Proper rigging ensures consistent fuel distribution and reliable engine performance.
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 311851201a is a flow divider valve for aircraft fuel-injected piston engines. This component splits metered fuel from the servo into balanced outlets feeding individual injector nozzles, ensuring even cylinder delivery across the engine.
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, FLOW DIVIDER 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, FLOW DIVIDER 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.