SAE AS1831A-1997
Electrical Power, 270 V DC, Aircraft, Characteristics and Utilization of

Standard No.

SAE AS1831A-1997

Release Date

1997

Published By

Society of Automotive Engineers (SAE)

Status

Be replaced

Replace By

SAE AS1831A-2017

Latest

SAE AS1831A-2023

Scope

This SAE Aerospace Standard establishes the characteristics and utilization of 270 V DC electric power at the utilization equipment interface and the constraints on the utilization equipment. These characteristics shall be applicable for both airborne and ground support power systems. This standard also defines the related distribution and installation considerations. Utilization equipment designed for a specific aircraft application may not deviate from these requirements without the approval of the procuring activity. The purpose of this standard is to assure compatibility between aircraft electrical systems or ground support electric systems and airborne utilization equipment.

SAE AS1831A-1997 Referenced Document

• SAE ARP4729-1992 DOCUMENT FOR 270 VOLTAGE DIRECT CURRENT (270 V DC) SYSTEM

SAE AS1831A-1997 history

• 2023 SAE AS1831A-2023 Electrical Power, 270 VDC, Aircraft, Characteristics and Utilization of
• 1970 SAE AS1831A-2017 Electrical Power, 270 V DC, Aircraft, Characteristics and Utilization of
• 1997 SAE AS1831A-1997 Electrical Power, 270 V DC, Aircraft, Characteristics and Utilization of
• 1987 SAE AS1831-1987 Electrical Power@ High Voltage Direct Current@ Aircraft@ Characteristics and Utilization of