INVERTER,STATIC (P/N pc-50) - As Removed

The pc-50 is a solid-state static inverter that converts 28 VDC aircraft bus power into 115 VAC, 400 Hz output for avionics and instrument systems. This inverter supplies AC power to flight instruments, navigation equipment, and cabin accessories that require alternating current on DC-powered aircraft. Installation follows aircraft wiring manual specifications and FAA AC 43.13-1B practices.

Verify compatibility with your aircraft's Illustrated Parts Catalog before installation to ensure proper voltage and frequency requirements are met.

What is the INVERTER,STATIC (P/N pc-50)?

The pc-50 is a solid-state static inverter that converts 28 VDC aircraft bus power into 115 VAC, 400 Hz output for avionics and instrument systems. This inverter supplies AC power to flight instruments, navigation equipment, and cabin accessories that require alternating current on DC-powered aircraft.

Is the pc-50 compatible with my aircraft's avionics suite?

Avionics compatibility depends on your aircraft model and existing installation. The INVERTER,STATIC is available in: As Removed. We recommend checking your aircraft's wiring diagrams and STC documentation, or contact our avionics team for compatibility assistance.

Does the pc-50 come with an 8130-3 airworthiness tag?

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.

Do you offer bench testing for the pc-50?

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.