Do-160g [patched] - Rtca

DO-160G offers multiple (e.g., temperature extremes, vibration severity, lightning pin injection levels). The equipment manufacturer or airframer selects the appropriate level based on installation location (e.g., cockpit vs. unpressurized wing leading edge). Each section defines:

The primary goal of DO-160G is to simulate the extreme conditions an aircraft might encounter. Without these rigorous standards, equipment failure could lead to catastrophic accidents, which historically account for a significant portion of aviation safety incidents. By adhering to these procedures, manufacturers can demonstrate to regulatory bodies like the and EASA that their products are airworthy. Key Testing Categories rtca do-160g

Note: The absence of a letter means that test was not required or not performed. DO-160G offers multiple (e

Unlike commercial electronics (which use IP ratings or MIL-STD-810), Each section defines: The primary goal of DO-160G

The letter indicates the revision. DO-160 was first published in 1975. Revision G was released in 2010 (with Change 1 in 2014 and Change 2 in 2020). Each revision clarifies ambiguities and adds tests for new technologies, such as high-speed digital electronics and composite airframes.