SAE AIR 5575 : 2017
Current
The latest, up-to-date edition.
HOT STAMP WIRE MARKING CONCERNS FOR AEROSPACE VEHICLE APPLICATIONS
Hardcopy , PDF
English
24-01-2017
Important note : Users cannot be edited or removed once added to your Multi user PDF.
1. SCOPE
2. REFERENCES
3. DISCUSSION
4. CONCLUSIONS
Describes overlooked relationship between hot stamp marking and the environmental conditions that contribute aircraft wiring problems and discusses current beliefs of military service experts, regulatory agencies and industry standard writing bodies about the potential hazards imposed by the hot stamping process.
| Committee |
AE-8A
|
| DocumentType |
Standard
|
| Pages |
15
|
| ProductNote |
This version is now stabilized.
|
| PublisherName |
SAE International
|
| Status |
Current
|
| Supersedes |
| FAA AC 25.1701-1 : 2007 | CERTIFICATION OF ELECTRICAL WIRING INTERCONNECTION SYSTEMS ON TRANSPORT CATEGORY AIRPLANES |
| SAE ARP 5369 : 2016 | GUIDELINES FOR WIRE IDENTIFICATION MARKING USING THE HOT STAMP PROCESS |
| ASTM D 3032 : 2016 : REDLINE | Standard Test Methods for Hookup Wire Insulation |
| SAE ARP 5369 : 2016 | GUIDELINES FOR WIRE IDENTIFICATION MARKING USING THE HOT STAMP PROCESS |
| SAE ARP 5607 : 2013 | LEGIBILITY OF PRINT ON AEROSPACE WIRES AND CABLES |
| BS G 244:1989 | Code of practice for installation/repair of aircraft electrical interconnection systems |
| SAE AS 50881 : 2015 | WIRING AEROSPACE VEHICLE |
| PREN 3838 : 200P2 | AEROSPACE SERIES - REQUIREMENTS AND TESTS ON USER-APPLIED MARKINGS ON AIRCRAFT ELECTRICAL CABLES |
| FAA AC 43.13-1 : 0 | ACCEPTABLE METHODS, TECHNIQUES, AND PRACTICES - AIRCRAFT INSPECTION AND REPAIR |
| MIL-W-5088 Revision L:1991 | Wiring, Aerospace Vehicle (Future Design Should Refer to SAE-AS50881) |
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