SAE ARP 4729 : 2017
Current
The latest, up-to-date edition.
DOCUMENT FOR 270 VOLTAGE DIRECT CURRENT (270 V DC) SYSTEM
Hardcopy , PDF
English
30-11-2017
Important note : Users cannot be edited or removed once added to your Multi user PDF.
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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