AFGS�87219B
DEPARTMENT OF DEFENSE STANDARDS
MIL-STD-704 Aircraft Electric Power Characteristics
MIL-STD-1796 Avionics Integrity Program (AVIP)
MIL-STD-1798 Mechanical Equipment and Subsystems Integrity Program
MIL-STD-2161 Paint Schemes and Exterior Markings for U.S. Navy and
Marine Corps Aircraft
(Copies of these documents are available online at https://assist.dla.mil/quicksearch/ or from the Standardization Document Order Desk, 700 Robbins Avenue, Building 4D, Philadelphia, PA
19111-5094.)
2.3 Non�Government publications.
The following documents form a part of this document to the extent specified herein. Unless otherwise specified, the issues of these documents are those cited in the solicitation or contract.
SAE INTERNATIONAL
SAE AS35061 Connector, Receptacle External Electric Power, Aircraft, 28
Volt DC Operating Power
SAE AS90362 Connector, Receptacle, External Electric Power, Aircraft,
115/200 Volt, 400 Hertz
(This standard is available from SAE International, 400 Commonwealth Drive, Warrendale, PA
15096-0001 or online at https://www.sae.org.)
2.4 Order of precedence.
Unless otherwise noted herein or in the contract, in the event of a conflict between the text of this document and the references cited herein, the text of this document takes precedence. Nothing in this document, however, supersedes applicable laws and regulations unless a specific exemption has been obtained.
3. REQUIREMENTS
3.1 System description.
The electrical power system (EPS) shall provide for the on-board generation, conversion, storage, distribution, diagnostics, and control of the electric power required for all phases of vehicle operation, including ground maintenance.
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