MIL-STD-704 Aircraft Electrical Power Specifications Standard, prepared by the United States (US) Department of Defense, is a military standard that covers issues such as voltage, frequency, phase, fluctuation and maximum current in a military aircraft and its equipment. The most current version of the standard is MIL-STD-704F_CHG-1, published in 2016. However, this standard is not a standard that only covers the US military and its subcontractors, but is a globally accepted standard for evaluating the suitability of military aircraft and systems. It is converted to the voltage levels required for the operation of the equipment used in the aircraft power system, which comes with a power source that complies with the MIL-STD-704 standard. In order for a piece of equipment to operate in accordance with the MIL-STD-704 standard, it must pass MIL-STD-704 tests to see its effects under difficult conditions and to verify its conformity.

The LDC105 Normal Voltage Transitions Test is performed to verify that 28V DC power handling equipment operates and maintains specified performance when subjected to steady-state voltage rises or falls within the fraction of seconds specified in MIL-STD-704.

The LDC105 Normal Voltage Transitions Test indicates that the operating equipment is successful if it operates and maintains performance as specified in the operating equipment performance specification document for normal aircraft electrical conditions when subjected to transient voltage fluctuations within the normal limits of the applicable version(s) of MIL-STD-704. It is considered to be MIL-STD-704-8 and as stated in the table. LDC105 Normal Voltage Transitions Test use equipment must maintain specified performance during and after voltage transients. The equipment used in the LDC105 Normal Voltage Transitions Test must not be damaged or cause an unsafe situation.