EUROLAB Laboratory performs the Boeing D6-16050-4 electromagnetic compatibility tests, includes electromagnetic compatibility requirements of selected electrical/electronic equipment for installation on Boeing commercial transport aircraft. Transient, audio frequency and radio frequency emission and sensitivity limits are specified for the equipment. Test procedures, typical test setups, approved measuring equipment, and test provisions are included with the designer's notes to aid in the correct interpretation of the design and test requirements.
EMC Test Procedure and Test Report data requirements are also specified in the Boeing D6-16050-4. Various testing procedures have been updated and clarified, with more attention given to supporting documentation requirements.
Electromagnetic compatibility requires that each aircraft system perform its intended function in the aircraft electromagnetic environment and that the operation of a particular system does not degrade the performance of other aircraft systems. Aircraft electromagnetic compatibility requires proper aircraft structural design, equipment installation, wiring installation, and equipment qualification. The emission limits and sensitivity thresholds contained in this document are a way to ensure that design goals will be met when compatible equipment is installed on an aircraft.
Boeing D6-16050-4 contains electromagnetic compatibility qualification and documentation requirements for electrical/electronic equipment to be installed on Boeing commercial transport aircraft. Transient, audio frequency and radio frequency emission and sensitivity limits are specified for the equipment. Test procedures, typical test setups, approved measuring equipment, and test provisions are included with the designer's notes to aid in the correct interpretation of the design and test requirements. EMC Test Procedure and Test Report data requirements are also specified.
Each supplier has full responsibility for the EMC design, construction and testing of the furnished equipment. This effort will comply with the applicable procurement specification and Boeing D6-16050-4. This will include responsibility for designing all circuits and associated packaging proven and effective techniques for the control of emissions and sensitivities.
While the test procedures and methods detailed here are standardized, each supplier has the responsibility to demonstrate that the performance of each unit has been tested and implemented with hardware, interfaces, software and operating modes that represent the actual in-service installation. Test equipment and load simulation units will be designed for RF immunity and non-sensitivity monitoring to ensure the accuracy of measurements.
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