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BS ISO 20949 - AIRCRAFT - SMART CONTACTOR - GENERAL REQUIREMENTS
Hardcopy , PDF
English
Foreword
Introduction
1 Scope
2 Normative references
3 Terms and definitions
4 General Requirements
5 Design characteristics
6 Design characteristics
7 Environmental conditions and test procedures
8 Test
Bibliography
BS ISO 20949.
Committee |
ACE/6
|
DocumentType |
Draft
|
Pages |
31
|
PublisherName |
British Standards Institution
|
Status |
Current
|
ISO 1540:2006 | Aerospace — Characteristics of aircraft electrical systems |
ISO 5867-1:1996 | Aircraft — Electromagnetic relays and contactors — Part 1: General requirements |
ISO 2678:1985 | Environmental tests for aircraft equipment — Insulation resistance and high voltage tests for electrical equipment |
ISO 8816:1993 | Aircraft — Solid-state remote power controllers — General requirements |
ISO 7137:1995 | Aircraft — Environmental conditions and test procedures for airborne equipment |
ISO 10296:1992 | Aircraft — Hybrid remote power controllers — General requirements |
ISO 263:1973 | ISO inch screw threads General plan and selection for screws, bolts and nuts Diameter range 0,06 to 6 in |
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