SAE ARP4729A
Current
The latest, up-to-date edition.
Document for 270 Voltage Direct Current (270 V DC) System
Hardcopy , PDF
English
11-30-2017
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.
| DocumentType |
Standard
|
| Pages |
36
|
| ProductNote |
This version is now stabilized.
|
| PublisherName |
SAE International
|
| Status |
Current
|
| Supersedes |
This SAE Aerospace Recommended Practice (ARP) provides technical design and application information related to the generation, distribution, control, and utilization of aircraft 270 V DC electrical power systems and support equipment. This document also provides references and definitions to permit comparisons of various electrical systems and components.
| MIL-C-81991 Base Document:1975 | Converter, Aircraft DC to DC, Boost General Specification for (No S/S Document) |
| MIL-I-8500 Revision D:1980 | Interchangeability and Replaceability of Component Parts for Aerospace Vehicles |
| SAE ARP926B | 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 AS1212A | Electric Power, Aircraft, Characteristics and Utilization of |
| SAE ARP935B | 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, Systems (S/S by MIL-STD-464) |
| MIL-E-7016 Revision F:1976 | Electric Load and Power Source Capacity, Aircraft, Analysis of |
| MIL-E-25499 Revision C:1970 | Electrical System, Aircraft, Design and Installation of, General Requirements for (No S/S Document) |
| MIL E 5400 : T | ELECTRONIC EQUIPMENT, AEROSPACE, GENERAL SPECIFICATION FOR |
| SAE ARP1870A | Aerospace Systems Electrical Bonding and Grounding for Electromagnetic Compatibility and Safety |
| 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 & SPECIFICATIONS, ORDER OF PRECEDENCE FOR THE SELECTION OF (S/S BY MIL-STD-970) |
| 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 (No S/S Document) |
| MIL-STD-462 Revision D:1993 | MEASUREMENT OF ELECTROMAGNTIC INTERFERENCE CHARACTERISTICS (S/S BY MIL-STD-461) |
| MIL-STD-1629 Revision A:1980 | PROCEDURES FOR PERFORMING A FAILURE MODE, EFFECTS AND CRITICALITY ANALYSIS (NO S/S DOCUMENT) |
| MIL-I-27273 Revision A:1965 | Inverter, Power, Static, General Specification for |
| MIL-B-5087 Revision B:1964 | Bonding, Electrical, and Lightning Protection, for Aerospace Systems (S/S by MIL-STD-464) |
| MIL-T-23103 Revision A:1971 | THERMAL PERFORMANCE EVALUATION, AIRBORNE ELECTRONIC EQUIPMENT AND SYSTEMS, GENERAL REQUIREMENT FOR (S/S BY MIL-STD-2218) |
| 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 Bus |
| SAE AS 486 : 1994 | AIRCRAFT CIRCUIT BREAKER AND FUSE ARRANGEMENT |
Access your standards online with a subscription
-
Simple online access to standards, technical information and regulations.
-
Critical updates of standards and customisable alerts and notifications.
-
Multi-user online standards collection: secure, flexible and cost effective.
Important note : All end users must be registered with an Account prior to user licenses being assigned.Logging out.