DC FLAP CONTROLLER (P/N 6238400-1a) - As Removed

The 6238400-1a is a DC flap controller that regulates electrical power to wing flap actuators. This component coordinates flap extension and retraction commands from cockpit switches to the actuator motors, managing current flow and sequencing in electrically driven flap systems. Installed between the flap control switch and actuator in the aircraft's electrical distribution network, it ensures synchronized flap movement across wing stations.

Installation follows aircraft maintenance manual procedures and FAA AC 43.13-1B electrical guidance. Verify compatibility with the aircraft's Illustrated Parts Catalog before integration.

What is the DC FLAP CONTROLLER (P/N 6238400-1a)?

The 6238400-1a is a DC flap controller that regulates electrical power to wing flap actuators. This component coordinates flap extension and retraction commands from cockpit switches to the actuator motors, managing current flow and sequencing in electrically driven flap systems.

Is the 6238400-1a compatible with my aircraft's avionics suite?

Avionics compatibility depends on your aircraft model and existing installation. The DC FLAP CONTROLLER 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 6238400-1a 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 6238400-1a?

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.