P/N: pc251-3a
Category: Batteries & Power Supply
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 |
| Serviceable | 2 Available |
The pc251-3a is a static inverter that converts DC bus power to regulated AC output for aircraft electrical systems. This unit supplies AC power to avionics, cabin equipment, and other onboard systems requiring alternating current. The inverter operates within FAA TSO-C73 standards and RTCA DO-160 qualification parameters.
Installation requires integration into the aircraft power distribution network per the maintenance manual and manufacturer's wiring instructions. Suitable for general aviation and corporate aircraft electrical architectures.
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 pc251-3a is a static inverter that converts DC bus power to regulated AC output for aircraft electrical systems. This unit supplies AC power to avionics, cabin equipment, and other onboard systems requiring alternating current.
Avionics compatibility depends on your aircraft model and existing installation. The INVERTER is available in: As Removed, Serviceable. We recommend checking your aircraft's wiring diagrams and STC documentation, or contact our avionics team for compatibility assistance.
Availability of an FAA 8130-3 tag depends on the part condition. Overhauled and repaired units typically include 8130-3 documentation. As-removed units may include a removal tag with trace history. Contact us for specific documentation on the condition you need.
We can arrange bench testing through our network of FAA-certified repair stations. Call (904) 998-9101 for testing availability and turnaround times, or submit an RFQ with your specific requirements.