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This document defines the method to establish an electrical load analysis which is used to compare the supply capacity of an electrical power generation system with the power demand of the connected electrical utilisation equipment. It shall prove that the power sources are capable of supplying these loads under all electrical power system states and aircraft operating conditions and that specified growth capacity for future requirements is ensured.

 

Document History

  1. DANSK DSF/FPREN 3830


    Aerospace series – Electrical system – Load analysis

    • Historical Version
  2. DANSK DS/EN 3830

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    Aerospace series – Electrical system – Load analysis

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