SAE AS 47642 : 2017
Current
The latest, up-to-date edition.
VALIDATION METHODS FOR MIL-STD-1760C AIRCRAFT STATION INTERFACES
Hardcopy , PDF
English
28-06-2017
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1 SCOPE
2 REFERENCES
3 DEFINITIONS
4 GENERAL REQUIREMENTS
5 DETAILED REQUIREMENTS
6 NOTES
APPENDIX A - VALIDATION METHOD
Provides techniques for validating that an Aircraft Station Interface (ASI) complies with the interface requirements delineated in MIL-STD-1760C.
| Committee |
AS-1B
|
| DocumentType |
Standard
|
| Pages |
182
|
| PublisherName |
SAE International
|
| Status |
Current
|
| Supersedes |
| MIL-STD-704 Revision F:2004 | AIRCRAFT ELECTRIC POWER CHARACTERISTICS |
| MIL-STD-1760 Revision E:2007 | AIRCRAFT/STORE ELECTRICAL INTERCONNECTION SYSTEM |
| MIL C 38999 : J | CONNECTOR, ELECTRICAL, CIRCULAR, MINIATURE, HIGH DENSITY, QUICK DISCONNECT (BAYONET THREADED & BREECH COUPLING) ENVIRONMENT RESISTANT, REMOVABLE CRIMP & HERMETIC SOLDER CONTACTS |
| MIL-STD-1560 Revision C:2015 | INSERT ARRANGEMENTS FOR MIL-DTL-38999, MIL-DTL-27599 AND SAE-AS29600 SERIES A - ELECTRICAL CIRCULAR CONNECTORS |
| SAE AS 4113 : 1989 | VALIDATION TEST PLAN FOR THE DIGITAL TIME DIVISION COMMAND/RESPONSE MULTIPLEX DATA BUS BUS CONTROLLERS |
| MIL C 45662 : 0 | CALIBRATION SYSTEM REQUIREMENTS |
| STANAG 3350 : 0 | ANALOGUE VIDEO STANDARD FOR AIRCRAFT SYSTEM APPLICATIONS |
| MIL-STD-1553 Revision B:1978 | DIGITAL TIME DIVISION COMMAND/RESPONSE MULTIPLEX DATA |
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