BS EN 3197:2010
Current
The latest, up-to-date edition.
Aerospace series. Design and installation of aircraft electrical and optical interconnection systems
Hardcopy , PDF
English
31-01-2011
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Foreword
ORGANISATION OF THIS STANDARD (Detailed organisation may be
found in Annex A)
1 Scope
2 Normative references
3 Terms and definitions
4 Limitations
5 General requirements
6 Selection of EWIS and OFIS Components
7 EWIS Components Identification
8 Separation and principles to apply
9 Installation and manufacturing principles
10 Modification and repairs by STC applicants
11 EWIS and OFIS Safety
Annex A (informative) - EN 3197 detailed content
Annex B (normative) - Main normative references and ASD-STAN
Technical Reports per family of products
Annex C (informative) - Differences of electrochemical
potentials between some conductive materials (in mV)
Gives instructions on the methods to be used when designing, selecting, manufacturing, installing, repairing or modifying the aircraft electrical and optical interconnection networks, now called Electrical Wiring Interconnection System (EWIS), and Optical Fibre Interconnection Systems (OFIS), subjects to the limitations.
| Committee |
ACE/6
|
| DevelopmentNote |
Supersedes 09/30202200 DC. (01/2011)
|
| DocumentType |
Standard
|
| Pages |
112
|
| PublisherName |
British Standards Institution
|
| Status |
Current
|
| Supersedes |
This European standard provides instructions on the methods to be used when designing, selecting, manufacturing, installing, repairing or modifying the aircraft electrical and optical interconnection networks, now called Electrical Wiring Interconnection System (EWIS), and Optical Fibre Interconnection Systems (OFIS), subjects to the limitations defined in Clause 4 of this standard.
The general content of this standard is described in page 2.
A detailed content of this standard is given in Annex A.
This standard lists all the relevant European standards related to EWIS and OFIS in Annex B.
| Standards | Relationship |
| EN 3197:2010 | Identical |
| SAE AS83519C | Shield Termination, Solder Style, Insulated, Heat-Shrinkable, Environment Resistant General Specification For |
| IEC 60270:2000+AMD1:2015 CSV | High-voltage test techniques - Partial discharge measurements |
| ISO 4046-1:2002 | Paper, board, pulps and related terms Vocabulary Part 1: Alphabetical index |
| TR 9535 : 2008 | AEROSPACE SERIES - SUBSTANCE DECLARATION |
| ISO 2685:1998 | Aircraft — Environmental test procedure for airborne equipment — Resistance to fire in designated fire zones |
| EN 60270:2001/A1:2016 | HIGH-VOLTAGE TEST TECHNIQUES - PARTIAL DISCHARGE MEASUREMENTS (IEC 60270:2000/A1:2015) |
| MIL-T-43435 Revision B:1974 | TAPE, LACING, AND TYING |
| MIL-DTL-22520 Revision G:1997 | CRIMPING TOOLS, WIRE TERMINATION, GENERAL SPECIFICATION FOR |
| ASTM D 1868 : 2013 : REDLINE | Standard Test Method for Detection and Measurement of Partial Discharge (Corona) Pulses in Evaluation of Insulation Systems |
| ISO 7137:1995 | Aircraft — Environmental conditions and test procedures for airborne equipment |
| ISO 2574:1994 | Aircraft — Electrical cables — Identification marking |
| MIL-STD-202 Revision H:2015 | ELECTRONIC AND ELECTRICAL COMPONENT PARTS |
| SAE AS81824/1A | SPLICE, IN-LINE, ELECTRIC, CRIMP, SN/CU, ENVIRONMENTAL, HEAT-SHRINKABLE SLEEVE (150 °C), 1 × 1 SEALANT OPENING |
| TR 9536 : 2008 | AEROSPACE SERIES - DECLARABLE SUBSTANCES RECOMMENDED PRACTICE |
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