RTCA DO-160
Section 4.0 Temperature and Altitude
RTCA DO-160G, Section 4.0
What It Evaluates
Select the category that matches the equipment’s installation location, temperature control, pressurization, and maximum aircraft altitude. Categories A–F establish the applicable temperature and altitude conditions, while the numbered subcategories identify the specific thermal environment. Categories V, W, P, Y, and Z separately define the required in-flight loss-of-cooling duration.
When It Applies
Applicability depends on the airborne equipment installation, declared category, aircraft environment, and program requirements.
Likely Procedures
Typical Ranges / Conditioning
This tool provides preliminary planning information only. Final MIL-STD-810H, MIL-STD-461, and RTCA DO-160 requirements must be reviewed and tailored by qualified engineers based on the product, lifecycle, platform, environment, and contract requirements.
