- Section
15: Magnetic Effects
Ensures aircraft equipment can operate properly within the magnetic
field of another aircraft system or equipment.
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- Section
16: Power Input
Performs
various tests that could be susceptibility causes to the AC
or DC power inputs to aircraft systems or equipment.
|
- Section
17: Voltage Spike
Determines
whether the aircraft systems or equipment can withstand the
effects of voltage spikes arriving at the equipment power leads.
|
- Section
18: Audio Frequency Conducted Susceptibility
Determines
whether the equipment will accept frequency components of a
magnitude normally expected when the equipment is installed
in the aircraft.
|
- Section
19: Induced Signal Susceptibility
Determines
whether the equipment interconnect circuit configurations will
accept a level of induced voltages caused by the installation
environment.
|
- Section
25: Electrostatic Discharge (ESD)
Determines
the immunity or the ability of the equipment to perform its
intended function without permanent degradation of performance
as a result of an air-discharged electrostatic pulse.
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The
Susceptibility Test Lab opened in May 2007. Equipped with the latest technology,
the lab is capable of providing DO-160 certification for the following
sections: 
