SAE ARP4404C
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
Aircraft Electrical Installations
Hardcopy , PDF
02-11-2024
English
19-09-2019
1. SCOPE
2. APPLICABLE DOCUMENTS
3. CIRCUIT PROTECTION
4. FAIL-SAFE FEATURES IN ELECTRIC CIRCUITS
5. CIRCUITS FOR ESSENTIAL EQUIPMENT
6. MULTI-ENGINE RELIABILITY
7. CONNECTORS AND OTHER TERMINATIONS
8. GROUNDING AND BONDING
9. WIRE SELECTION AND ROUTING
10. ALUMINUM WIRE AND CONNECTIONS
11. WIRE AND CABLE IDENTIFICATION
12. MAINTENANCE OF ELECTRIC EQUIPMENT
13. OPERATION AND INSPECTION OF ELECTRIC EQUIPMENT
14. PROVISIONS FOR ADDITIONAL ELECTRIC EQUIPMENT
15. EQUIPMENT SELECTION AND INSTALLATION
16. CORROSION PREVENTION IN ELECTRICAL EQUIPMENT
17. SYSTEM LOAD DISTRIBUTION
18. ELECTRIC SYSTEM TESTS
19. EMERGENCY CONTROLS AND PROCEDURES
20. AUXILIARY POWER PLANTS
APPENDIX A - DEFINITIONS
APPENDIX B - EVALUATION CHECK-OFF LIST FOR ELECTRIC
EQUIPMENT
APPENDIX C - MINIMUM AIR SPACINGS FOR VARIOUS
VOLTAGES AND ALTITUDES
It is the purpose of this document to present design recommendations that will provide a basis for satisfactory and safe electrical installations in transport aircraft.
DocumentType |
Standard
|
Pages |
111
|
PublisherName |
SAE International
|
Status |
Superseded
|
SupersededBy | |
Supersedes |
It is the purpose of this document to present design recommendations that will provide a basis for satisfactory and safe electrical installations in transport aircraft. This document is not intended to be a complete electrical installation design handbook. However, the requirements for safety extend so thoroughly throughout the electric systems that few areas of the installation are untouched by the document. It is recognized that individual circumstances may alter the details of any design. It is, therefore, important that this document not be considered mandatory but be used as a guide to good electrical application and installation design.Transport aircraft electric systems have rapidly increased in importance over a number of years until they are now used for many functions necessary to the successful operation of the aircraft. An ever increasing number of these functions are critical to the safety of the aircraft and its occupants. The greatly increased power available in electric systems is another factor in aircraft safety. These considerations make it essential that aircraft electrical design practices be carefully considered from the standpoint of safety and reliability. It is believed that this document will be of value in pointing out potential difficulties and in solving many of the problems.
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