DI-SESS-82282
Electric Load and Power Source Capacity Report
Specifies requirements for an electric load and power source capacity analysis report to ensure robustness of electric power systems in aircraft or equipment.
Approval DateAugust 7, 2019
AMSC NumberN10064
Preparing ActivityAS
Project NumberSESS-2019-031
OPR—
DTIC Applicable—
GIDEP Applicable—
Limitation—
Applicable Forms—
Approval Limitation—
Form Version—
DID Formatfree_text
963C CompliantYes
DISTRIBUTION STATEMENT A: Approved for public release; distribution is unlimited.
Application & Interrelationship
—
Use & Relationship
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. This Data Item Description (DID) 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).
Preparation Instructions
1Reference DocumentsThe applicable issue of the documents cited herein, including their approval dates of any applicable amendments, notices, and revisions, shall be as specified in the contract.
2FormatThe report format shall be prepared in accordance with latest version of detail specification, Electric Load and Power Source Capacity, Aircraft, Analysis of, MIL-E-7016, section 3.3, 3.4, and its subsections.
3ContentThe report content shall be prepared in accordance with latest version of detail specification, Electric Load and Power Source Capacity, Aircraft, Analysis of, MIL-E-7016, section 3.5 and its subsections.
Schema v3.0Community-maintained · Verify against ASSIST