Abstract: Systems and methods for an overheating control system for an electrical power harness disposed within an enclosure of an aircraft. The system includes a temperature sensor disposed within the enclosure and communicatively coupled to an electronic processor. The electronic processor is configured to monitor, via the temperature sensor, a temperature within the enclosure, compare the temperature to a predetermined threshold, and adjust a power output provided to one or more supply lines of the harness based on an amount in which the temperature exceeds the predetermined threshold.

Abstract: A durable knockdown cabinet and kit for making the same includes, a bottom panel, a top panel, a left panel, a right panel and a plurality of clips. When assembled the left side panel with a lower interior portion of the left panel is aligned by and detachably connected to a left exterior region of the bottom panel with at least one of the clips and an upper interior portion of the left panel is aligned by and detachably connected to a left interior region of the top panel with at least one of the clips. The right side panel with a lower interior portion of the right panel is aligned by and detachably connected to a right exterior region of the bottom panel with at least one of the clips and an upper interior portion of the right panel is aligned by and detachably connected to a right interior region of the top panel with at least one of the clips. The clips each include a first and second clip section and a C-shaped locking plate.