SAE ARP 4404 : 2013
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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AIRCRAFT ELECTRICAL INSTALLATIONS
Hardcopy , PDF
14-10-2019
English
01-11-2013
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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
Specifies design recommendations that will provide a basis for satisfactory and safe electrical installations in transport aircraft.
| Committee |
AE-8A
|
| DocumentType |
Standard
|
| Pages |
111
|
| PublisherName |
SAE International
|
| Status |
Superseded
|
| SupersededBy | |
| Supersedes |
| SAE AIR 5451 : 2017 | A GUIDE TO LANDING GEAR SYSTEM INTEGRATION |
| FAA AC 25.1701-1 : 2007 | CERTIFICATION OF ELECTRICAL WIRING INTERCONNECTION SYSTEMS ON TRANSPORT CATEGORY AIRPLANES |
| MIL-HDBK-525 Base Document:2013 | ELECTRICAL WIRING INTERCONNECT SYSTEM (EWIS) INTEGRITY PROGRAM |
| SAE AIR 4004 : 2015 | GUIDE FOR INSTALLATION OF ELECTRICAL WIRE AND CABLE ON AIRCRAFT LANDING GEAR |
| SAE AS4373E | Test Methods for Insulated Electric Wire |
| MIL-DTL-5015 Revision H:2000 | CONNECTORS, ELECTRICAL, CIRCULAR THREADED, AN TYPE - GENERAL SPECIFICATION FOR |
| SAE ARP4101/5A | Aircraft Circuit Breaker and Fuse Arrangement |
| SAE ARP1199B | Selection, Application, and Inspection of Electric Overcurrent Protective Devices |
| MIL F 15160 : G | FUSE, INSTRUMENT, POWER, AND TELEPHONE, GENERAL SPECIFICATION FOR |
| MIL-STD-704 Revision F:2004 | AIRCRAFT ELECTRIC POWER CHARACTERISTICS |
| SAE AS8011B | Minimum Performance Standards for A-C Generators and Associated Regulators |
| SAE AIR 1329C : 2014 | ELECTRICAL CONNECTORS AND WIRING, COMPATIBILITY OF |
| MIL-STD-810 Revision G:2008 | ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS |
| SAE AIR1402A | Common Termination Method, Electrical Wiring System, Application Of |
| SAE AS1212A | Electric Power, Aircraft, Characteristics and Utilization of |
| ASTM D 3032 : 2016 : REDLINE | Standard Test Methods for Hookup Wire Insulation |
| SAE AS8028 | POWERPLANT FIRE DETECTION INSTRUMENTS THERMAL & FLAME CONTACT TYPES (RECIPROCATING AND TURBINE ENGINE POWERED AIRCRAFT) |
| SAE AS5363A | Electromechanical Power Controller/Relay, General Specification For |
| SAE AS24001A | FUSE HOLDER, BLOCK-TYPE, 1-, 2-, 3-POLE, 35- TO 60-AMPERE, AIRCRAFT |
| MIL-DTL-81381 Revision C:2005 | WIRE, ELECTRIC, POLYIMIDE-INSULATED, COPPER OR COPPER ALLOY |
| MIL-STD-1353 Revision C:2014 | ELECTRICAL CONNECTORS, PLUG-IN SOCKETS AND ASSOCIATED HARDWARE, SELECTION AND USE OF |
| MIL-E-7016 Revision F:1976 | ELECTRIC LOAD AND POWER SOURCE CAPACITY, AIRCRAFT ANALYSIS OF |
| MIL-STD-889 Revision C:2016 | DISSIMILAR METALS |
| SAE AS8023B | Minimum Performance Standards for Static Electric Power Inverters |
| MIL-STD-7080 Base Document:1994 | SELECTION & INSTALLATION OF AIRCRAFT ELECTRIC EQUIPMENT |
| MS21919 Revision E:1981 | CLAMP, LOOP TYPE, CUSHIONED, SUPPORT |
| MIL-C-85485 Revision A:1983 | CABLE, ELECTRIC, FILTER LINE, RADIO FREQUENCY ABSORPTIVE |
| MIL-STD-464 Revision C:2010 | ELECTROMAGNETIC ENVIRONMENTAL EFFECTS REQUIREMENTS FOR SYSTEMS |
| NEMA WC 27500 : 2015 | STANDARD FOR AEROSPACE AND INDUSTRIAL ELECTRICAL CABLE |
| SAE AS22759C | Wire, Electrical, Fluoropolymer-Insulated, Copper or Copper Alloy |
| SAE ARP4043B | Flight Line Grounding and Bonding of Aircraft |
| SAE ARP1870A | Aerospace Systems Electrical Bonding and Grounding for Electromagnetic Compatibility and Safety |
| SAE AS 4372 : 2014 | PERFORMANCE REQUIREMENTS FOR WIRE, ELECTRIC, INSULATED COPPER OR COPPER ALLOY |
| SAE AIR1557A | High and Extended Vibration Environment |
| SAE AS 4851 : 2012 | RELATIVE THERMAL LIFE AND TEMPERATURE INDEX FOR INSULATED ELECTRIC WIRE |
| SAE AS 1831 : 1997 | ELECTRICAL POWER, 270 V DC, AIRCRAFT, CHARACTERISTICS AND UTILIZATION OF |
| SAE ARP 1308 : 2014 | ELECTRICAL CONNECTORS FOR AEROSPACE, SHIPBOARD, GROUND VEHICLES AND ASSOCIATED EQUIPMENT |
| MIL F 5372 : D | FUSE, CURRENT LIMITER TYPE, AIRCRAFT |
| MIL-STD-461 Revision G:2015 | REQUIREMENTS FOR THE CONTROL OF ELECTROMAGNETIC INTERFERENCE CHARACTERISTICS OF SUBSYSTEMS AND EQUIPMENT |
| NAS557:2011 | GROMMET, PLASTIC, SPLIT |
| MIL W 25038 : F | WIRE, ELECTRICAL, HIGH TEMP, FIRE RESISTANT, AND FLIGHT CRITICAL, GENERAL SPECIFICATION FOR |
| SAE AS81044A | Wire, Electrical, Crosslinked Polyalkene, Crosslinked Alkane-Imide Polymer, or Polyarlyene Insulated, Copper or Copper Alloy |
| MS24000 Revision F:1992 | FUSE HOLDER, BLOCKTYPE 1- 2- AND 3-POLE, 1- TO 30 AMPERE AIRCRAFT |
| SAE J554_198708 | ELECTRIC FUSES (CARTRIDGE TYPE) |
| SAE AS50881F | Wiring Aerospace Vehicle |
| SAE AIR 4567 : 2014 | COMPOSITE ELECTRICAL CONNECTORS |
| SAE ARP1931B | Glossary of Terms With Specific Reference to Electrical Wire and Cable |
| SAE AS53731A | Fuse Holder, Block Type, Aircraft |
| SAE AS58091A | Circuit Breakers, Trip-Free, Aircraft General Specification For |
| SAE AIR1263 | TIN PLATED SOLDERLESS TERMINAL LUGS AND SPLICES ON NICKEL COATED HIGH TEMPERATURE WIRE |
| MIL-HDBK-221 Base Document:1965 | FIRE PROTECTION DESIGN HANDBOOK FOR U.S. NAVY AIRCRAFT POWERED BY TURBINE ENGINES |
| SAE AS 8020 : 1980 | MINIMUM PERFORMANCE STANDARDS FOR ENGINE DRIVEN D.C. GENERATORS/STARTER-GENERATORS AND ASSOCIATED VOLTAGE REGULATORS |
| MIL-STD-705 Revision D:2016 | MOBILE ELECTRIC POWER SYSTEMS |
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