This test determines whether the equipment will accept frequence components of a magnitude normally expected when the equipment
is installed in the aircraft. These frequency components are normally harmonically related to the power source fundamental frequency.
The tests in this section are “susceptibility” tests, meaning the units being tested are the “victims” of the environment.
Our facilities have full DO-160G capability for categories B, Z, and K.
Our facilities include three 50 kHz DC, 100Amp Peak Power Techron Amplifiers