DOCUMENT FOR 270 VOLTAGE DIRECT CURRENT (270 V DC) SYSTEM

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

11-30-2017

Publisher

SAE International

1. SCOPE
2. APPLICABLE DOCUMENTS
3. 270 V DC SYSTEM
4. QUALITY ASSURANCE REQUIREMENTS
5. SHIPPING AND HANDLING
6. GENERAL NOTES
APPENDIX A

Gives technical design and application information related to the generation, distribution, control, and utilization of aircraft 270 VDC electrical power systems and support equipment.

Committee	AE-7C
DocumentType	Standard
Pages	36
ProductNote	This version is now stabilized.
PublisherName	SAE International
Status	Current
Supersedes	SAE ARP 4729 : 2010

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MIL-I-8500 Revision D:1980	INTERCHANGEABILITY AND REPLACEABILITY OF COMPONENT PARTS FOR AEROSPACE VEHICLES
SAE ARP 926 : 1997	FAULT/FAILURE ANALYSIS PROCEDURE
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SAE AIR 1221 : 1971	ELECTROMAGNETIC COMPATIBILITY (EMC) SYSTEM DESIGN CHECKLIST
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SAE AIR 1406 : 1993	LIGHTNING PROTECTION AND STATIC ELECTRIFICATION
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SAE AS 1212 : 2012	ELECTRIC POWER, AIRCRAFT, CHARACTERISTICS AND UTILIZATION OF
SAE ARP 935 : 2013	CONTROL PLAN/TECHNICAL CONSTRUCTION FILE
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