BS G 260:1996
Current
The latest, up-to-date edition.
Environmental tests for aircraft equipment. Steady-state acceleration
Hardcopy , PDF
English
15-06-1996
Committees responsible
National foreword
Introduction
Specification
1 Scope
2 Normative reference
3 Apparatus
4 Equipment mounting
5 Classification of tests
6 Test sequence
7 Acceleration severity grades
8 Procedures
9 Information to be included in the relevant
equipment specification
Tables
1 Equipment severity grades
2 Classification of tests
3 Equipment categories
4 Acceleration severity grades (functional tests)
5 Acceleration severity grades (structural tests)
A.1 Additional accelerations
Figure
1 Direction of aircraft acceleration
Annex
A (normative) Additional accelerations
Describes two types of steady-state acceleration test and five severity grades of acceleration forces used for simulation of a gradually changing acceleration environment simulating that encountered by civil aircraft equipment in operational use.
| Committee |
ACE/58
|
| DevelopmentNote |
Supersedes 89/75587 DC. Also numbered as ISO 2669. (06/2005)
|
| DocumentType |
Standard
|
| Pages |
16
|
| PublisherName |
British Standards Institution
|
| Status |
Current
|
This International Standard specifies two types of steady-state acceleration test and establishes five severity grades of acceleration forces used to simulate a gradually changing acceleration environment representative of that which civil aircraft equipment can encounter in operational use.
The emergency landing case is not within the scope of this International Standard; reference should be made to ISO 7137 for this case.
| BS 4G 229:1996 | Schedule for environmental conditions and test procedures for airborne equipment |
| BS 4G 229:1996 | Schedule for environmental conditions and test procedures for airborne equipment |
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