RTCA DO-160 – Section 4.0 – Temperature and Altitude
The Temperature and Altitude tests determine the performance characteristics of equipment at the applicable categories for the temperatures and altitudes specified in Table 4-1 and at the pressures defined in Table 4-2.
Ground Survival Low Temperature Test and Short-Time Operating Low Temperature Test Operating Low Temperature Test
Ground Survival High Temperature Test and Short-Time Operating High Temperature Test
Operating High Temperature Test
In-Flight Loss of Cooling Test
Altitude, Decompression and Overpressure Tests
DO-160 is a standard for environmental test on avionics equipment published by RTCA, the Radio Technical Commission for Aeronautics. The DO 160 G was amended and now all guideline inside it are repleaced by the DO 357.