P/N: 394408-10-1
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 |
|---|---|
| New Surplus | 1 Available |
| As Removed | 1 Available |
| Serviceable | 2 Available |
| Overhauled | 1 Available |
Part 394408-10-1 is a flow divider for aircraft fuel systems that splits metered fuel from the fuel control unit into primary and secondary manifolds. Located between the fuel control and nozzle manifolds, it proportions fuel flow across the engine's operating range and purges residual fuel during shutdown. This component supports stable engine starts and positive cutoff at engine termination.
Installation and testing must follow the applicable engine 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.
Part 394408-10-1 is a flow divider for aircraft fuel systems that splits metered fuel from the fuel control unit into primary and secondary manifolds. Located between the fuel control and nozzle manifolds, it proportions fuel flow across the engine's operating range and purges residual fuel during shutdown.
Depending on condition, the 394408-10-1 may include an FAA 8130-3 Airworthiness Approval Tag, a yellow serviceable tag, or manufacturer documentation. Currently available in: New Surplus, As Removed, Serviceable, Overhauled. 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.