SAE AS47642B
Current
The latest, up-to-date edition.
Validation Methods for MIL-STD-1760C Aircraft Station Interfaces
Hardcopy , PDF
English
28-06-2017
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.
| DocumentType |
Standard
|
| Pages |
182
|
| PublisherName |
SAE International
|
| Status |
Current
|
| Supersedes |
This document establishes techniques for validating that an Aircraft Station Interface (ASI) complies with the interface requirements delineated in MIL-STD-1760C. For validation of aircraft designed to MIL-STD-1760A Notice 2 AS4764 Issued 1995-04 applies. For validation of aircraft designed to MIL-STD-1760B Notice 3 AS47641 Issued 1999-08 applies.
| 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 |
| 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 Bus |
Please Login or Create an Account so you can add users to your Multi user PDF Later.
Important note : All end users must be registered with an Account prior to user licenses being assigned.
Users cannot be edited or removed once added to your Multi user PDF.