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ISO 6858:2017

Current
Current

The latest, up-to-date edition.

Aircraft — Ground support electrical supplies — General requirements
Available format(s)

Hardcopy , PDF , PDF 3 Users , PDF 5 Users , PDF 9 Users

Language(s)

English

Published date

06-12-2017

ISO 6858:2017 specifies the electrical output characteristics and interface requirements between an aircraft and ground support electrical supplies. This includes all external electric power generation facilities, provided as part of a central source or in point-of-use application. Requirements for safety features are also included. Performance and safety issues under regional control are not addressed in this document. Requirements for ground traffic control purposes, such as towing points, identification and warning lights, etc. are also excluded.

The electrical characteristics relate to nominal 28 V DC and either 115/200 V or 230/400 V three-phase, 400 Hz AC outputs measured at the aircraft attaching connector as indicated in Figure 1.

Committee
ISO/TC 20/SC 1
DevelopmentNote
Supersedes ISO 223 (04/2001) Supersedes ISO/DIS 6858. (12/2017)
DocumentType
Standard
Pages
35
PublisherName
International Organization for Standardization
Status
Current
Supersedes

Standards Relationship
BS ISO 6858:2017 Identical
IS 7856 : 2023 Identical
BS ISO 6858:2017 Identical

ISO 1540:2006 Aerospace — Characteristics of aircraft electrical systems
IEC 60204-1:2016 Safety of machinery - Electrical equipment of machines - Part 1: General requirements
IEC 61558-2-6:2009 Safety of transformers, reactors, power supply units and similar products for supply voltages up to 1 100 V - Part 2-6: Particular requirements and tests for safety isolating transformers and power supply units incorporating safety isolating transformers
ISO 12100:2010 Safety of machinery — General principles for design — Risk assessment and risk reduction
ISO 461-2:1985 Aircraft — Connectors for ground electrical supplies — Part 2: Dimensions
ISO 461-1:2003 Aircraft Connectors for ground electrical supplies Part 1: Design, performance and test requirements
ISO 7137:1995 Aircraft — Environmental conditions and test procedures for airborne equipment
ISO 13850:2015 Safety of machinery Emergency stop function Principles for design
IEC 61140:2016 Protection against electric shock - Common aspects for installation and equipment
ISO 12384:2010 Aerospace — Requirements for digital equipment for measurements of aircraft electrical power characteristics

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