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.

LDC101 Load Measurements Test is carried out within the scope of MIL-STD-704 Standard. The LDC101 Load Measurements Test is performed to verify that 28V DC power usage equipment meets the load limits, instantaneous limits, current distortion limits and current spectrum limits that may be required by the usage equipment performance specification document. The equipment used in the LDC101 Load Measurements Test must not be damaged or cause a malfunction.

If the equipment used in the LDC101 Load Measurements Test requires a performance specification document; If the usage equipment is within the load limits, inrush current limits, current distortion limit and current spectrum limits specified in the usage equipment performance specification document, the usage equipment is considered to pass. As noted in the table, load limits, inrush current limits, current distortion limit, and current spectrum limits are not specified in versions A through F of MIL-STD-704. Use with the LDC101 Load Measurements Test must not damage equipment or cause an unsafe situation.