BS G 240:1988 - Specification for pressure transducers for use on aircraft

BS G 240:1988

Specification for pressure transducers for use on aircraft

Status : Current, Under review   Published : February 1988



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.

Standard NumberBS G 240:1988
TitleSpecification for pressure transducers for use on aircraft
StatusCurrent, Under review
Publication Date29 February 1988
Confirm Date01 July 2014
Normative References(Required to achieve compliance to this standard)No other standards are normatively referenced
Informative References(Provided for Information)No other standards are informatively referenced
DescriptorsCalibration, Leak tests, Electrical measurement, Quality, Performance testing, Thermal testing, Aircraft components, Measuring instruments, Designations, Voltage, Temperature, Endurance testing, Type testing, Pressure testing, Air transport engineering, Response time, Signals, Burst tests, Electrical equipment, Design, Pressure, Transducers, Pressure measurement (fluids), Classification systems, Accuracy, Aircraft instruments
Title in FrenchCapteurs de pression utilisés à bord des aéronefs. Spécifications
Title in GermanDruckwandler fuer Luftfahrzeuge
ISBN0 580 16294 X
File Size279.9 KB

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