P/N: 394300-3-1
Category: Carburetors & Fuel Injection
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 394300-3-1 is a flow divider for aircraft fuel-injection systems on piston engines. This component meters fuel from the fuel control unit and distributes it equally to individual injector nozzles, ensuring balanced cylinder-to-cylinder fuel flow. The divider maintains positive fuel cutoff during engine shutdown and idle operation.
Installed between the fuel control and injector manifold on RSA-type fuel-injected engines, it stabilizes combustion and prevents lean-running conditions. Follow engine manufacturer maintenance manual and FAA-approved data for installation and torque 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 394300-3-1 is a flow divider for aircraft fuel-injection systems on piston engines. This component meters fuel from the fuel control unit and distributes it equally to individual injector nozzles, ensuring balanced cylinder-to-cylinder fuel flow.
Depending on condition, the 394300-3-1 may include an FAA 8130-3 Airworthiness Approval Tag, a yellow serviceable tag, or manufacturer documentation. Currently available in: As Removed. Contact us for specific documentation details on the condition you need.
Yes, the FLOW DIVIDER can be used in engine overhauls and maintenance events. Always verify part compatibility against your engine's Type Certificate Data Sheet (TCDS) and Illustrated Parts Catalog (IPC) before installation.
In-stock items ship same business day when ordered before 3 PM EST. We also offer 24/7 AOG (Aircraft on Ground) support at (904) 998-9101 for urgent engine part needs.