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BS G 240:1988

Current
Current

The latest, up-to-date edition.

Specification for pressure transducers for use on aircraft
Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

02-29-1988

Publisher

British Standards Institution

Foreword
Committees responsible
Specification
1. Scope
2. Definitions
3. Information to be supplied in the individual
     transducer specification
4. Classification
5. Construction
6. Output signal
7. Electrical supplies
8. Performance
9. Type tests
10. Production test
Table
1. Limits of long-term drift

Specifies requirements for transducers used in pressure systems, that convert a fluid pressure into an electrical signal for transmission to aircraft indicators or systems, embracing gauge, absolute and differential pressure units.

This British Standard specifies requirements for pressure transducers used in aircraft pressure systems, to convert a fluid pressure into an electrical signal for transmission to aircraft indicators or systems. It is applicable to transducers capable of measuring gauge, absolute or differential pressure, that have an accuracy in the range 0.25 % to 2.0 % of full scale output at reference conditions, and are capable of working over the ambient temperature range − 54 °C to + 85 °C.

NOTE The titles of the publications referred to in this standard are listed on the inside back cover.

Committee
ACE/1
DevelopmentNote
Supersedes 85/78805 DC. (06/2005) Reviewed and confirmed by BSI, January 2009. (12/2008)
DocumentType
Standard
Pages
12
PublisherName
British Standards Institution
Status
Current

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Hardcopy - English
PDF - English
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