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SAE ARP 4729 : 2017

Current
Current

The latest, up-to-date edition.

DOCUMENT FOR 270 VOLTAGE DIRECT CURRENT (270 V DC) SYSTEM
Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

30-11-2017

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

MIL-C-81991 Base Document:1975 CONVERTER, AIRCRAFT DC TO DC, BOOST GENERAL SPECIFICATION FOR
MIL-I-8500 Revision D:1980 INTERCHANGEABILITY AND REPLACEABILITY OF COMPONENT PARTS FOR AEROSPACE VEHICLES
SAE ARP 926 : 1997 FAULT/FAILURE ANALYSIS PROCEDURE
MIL-STD-704 Revision F:2004 AIRCRAFT ELECTRIC POWER CHARACTERISTICS
SAE AIR 1221 : 1971 ELECTROMAGNETIC COMPATIBILITY (EMC) SYSTEM DESIGN CHECKLIST
MIL-P-81653 Revision B:1980 POWER CONTROLLER, SOLID STATE, GENERAL SPECIFICATION FOR
MIL-STD-810 Revision G:2008 ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS
SAE AIR 1406 : 1993 LIGHTNING PROTECTION AND STATIC ELECTRIFICATION
MIL G 21480 : A GENERATOR SYSTEM, 400 HERTZ ALTERNATING CURRENT, AIRCRAFT GENERAL SPECIFICATION FOR
SAE AS 1212 : 2012 ELECTRIC POWER, AIRCRAFT, CHARACTERISTICS AND UTILIZATION OF
SAE ARP 935 : 2013 CONTROL PLAN/TECHNICAL CONSTRUCTION FILE
DOD STD 1686 : 0 ELECTROSTATIC DISCHARGE CONTROL PROGRAM FOR PROTECTION OF ELECTRICAL AND ELECTRONIC PARTS ASSEMBLIES AND EQUIPMENT (EXCLUDING ELECTRICALLY INITIATED EXPLOSIVE DEVICES)(METRIC)
MIL-E-6051 Revision D:1967 ELECTROMAGNETIC COMPATIBILITY REQUIREMENTS, SYSTEM
MIL-E-7016 Revision F:1976 ELECTRIC LOAD AND POWER SOURCE CAPACITY, AIRCRAFT ANALYSIS OF
MIL-E-25499 Revision C:1970 ELECTRICAL SYSTEMS, AIRCRAFT, DESIGN AND INSTALLATION OF, GENERAL REQUIREMENTS FOR
MIL E 5400 : T ELECTRONIC EQUIPMENT, AEROSPACE, GENERAL SPECIFICATION FOR
SAE ARP1870A:1987(S2012) Aerospace Systems Electrical Bonding and Grounding for Electromagnetic Compatibility and Safety(STABILIZED Aug 2012)<br>
SAE AIR 1277 : 2005 COOLING OF MILITARY AVIONIC EQUIPMENT
MIL C 7115 : F CONVERTER, AIRCRAFT, GENERAL SPECIFICATION FOR
SAE AS 1831 : 1997 ELECTRICAL POWER, 270 V DC, AIRCRAFT, CHARACTERISTICS AND UTILIZATION OF
MIL-STD-143 Revision B:1969 STANDARDS, AND SPECIFICATIONS ORDER OF PRECEDENCE FOR THE SELECTION OF
MIL-STD-461 Revision G:2015 REQUIREMENTS FOR THE CONTROL OF ELECTROMAGNETIC INTERFERENCE CHARACTERISTICS OF SUBSYSTEMS AND EQUIPMENT
MIL R 6106 : J RELAYS, ELECTROMAGNETIC [INCLUDING ESTABLISHED RELIABILITY [ER] TYPES
MIL-Q-9858 Revision A:1963 QUALITY PROGRAM REQUIREMENTS
MIL-STD-462 Revision D:1993 MEASUREMENT OF ELECTROMAGNETIC INTERFERENCE CHARACTERISTICS
MIL-STD-1629 Revision A:1980 PROCEDURES FOR PERFORMING A FAILURE MODE, EFFECTS AND CRITICALITY ANALYSIS
MIL-I-27273 Revision A:1965 INVERTER, POWER, STATIC, GENERAL SPECIFICATION FOR
MIL-B-5087 Revision B:1964 BONDING, ELECTRICAL AND LIGHTING PROTECTION, FOR AEROSPACE SYSTEMS
MIL-T-23103 Revision A:1971 THERMAL PERFORMANCE EVALUATION, AIRBORNE ELECTRONIC EQUIPMENT AND SYSTEMS, GENERAL REQUIREMENTS FOR
MIL-STD-785 Revision B:1980 RELIABILITY PROGRAM FOR SYSTEMS AND EQUIPMENT DEVELOPMENT AND PRODUCTION
MIL STD 2073 : 1978 DOD MATERIEL, PROCEDURES FOR DEVELOPMENT AND APPLICATION OF PACKAGING REQUIREMENTS
MIL-E-81910 Revision A:1977 ELECTRICAL POWER GENERATING AND CONTROL EQUIPMENT, AIRCRAFT, GENERAL SPECIFICATIONS FOR
MIL-STD-1553 Revision B:1978 DIGITAL TIME DIVISION COMMAND/RESPONSE MULTIPLEX DATA
SAE AS 486 : 1994 AIRCRAFT CIRCUIT BREAKER AND FUSE ARRANGEMENT

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