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The electric load and power source capacity analyses report shall consider all aircraft or equipment operating conditions in order to ascertain or maintain robustness of each electric power system in the aircraft or equipment. DID DI-SESS-82282 may be applied to analyses requirements of special-purpose electric systems (e.g. electrical systems in backup mode, independent engine ignition and control generator systems, general-purpose electric systems, etc.).

This DID contains the format, content, and intended use information for the data product resulting from the work task described by the contract statement of work (SOW).