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Attention:

The  differential pressure transducer setra 239 with a pressure range of 0-30 INWC (inch water column) is permantly installed in both aircraft as part of the Basic Meteorology module. Additionally, the pressure transducer setra 239 with a pressure range of +/- 7.5 INWC is installed in nose booms used for turbulence measurements.

Summary

The setra 239 model is used for measuring differential pressure for the basic meteorology at the nose of the aircraf. Additionally, it is used with the Turbulence Noseboom where setra239 transducers are connected to a 5-whole probe. The Model 239 is a transducer designed for extremely low pressure ranges (+/- 2.7 inch WC) and a wide temperature range (-18 to +80°C).


Manufacturersetra
Model239
Serial No.n/a
Typepressure sensor
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Contacts

NameInstitutionRole

Available devices and Specifications

NameModelType
Differential pressure transducer239 (0-30 INWC)pressure sensor
Differential pressure transducer239 (0-30 INWC)pressure sensor
Differential pressure transducer239 (0-30 INWC)pressure sensor
Differential pressure transducer239 (0-30 INWC)pressure sensor
Differential pressure transducer239 (0-30 INWC)pressure sensor
Differential pressure transducer239 (0-30 INWC)pressure sensor
Differential pressure transducer239 (0-30 INWC)pressure sensor
Differential pressure transducer239 (+/- 7,5 INWC)pressure sensor
Differential pressure transducer239 (+/- 7,5 INWC)pressure sensor
Differential pressure transducer239 (+/- 7,5 INWC)pressure sensor
Differential pressure transducer239 (+/- 7,5 INWC)pressure sensor
Differential pressure transducer239 (+/- 7,5 INWC)pressure sensor
Differential pressure transducer239 (+/- 7,5 INWC)pressure sensor
Differential pressure transducer239 (+/- 7,5 INWC)pressure sensor
Differential pressure transducer239 (+/- 7,5 INWC)pressure sensor

Specifications of setra 239 (without mounting)

Dimension (L x W x H)

83 x 50 x 79 mm

Weight

0.3 kg

Power Supply

22 - 30 VDC

Data interface

analogue data (V)

Position

Origin Description:Setra 239 differential pressure transducer are installed in the nose pylon of the aircraft for the basic meteorology module as well as in the turbulence nose boom used for turbulence measurements.

Data logging, storage and archiving

Logged parameter

ParameterSensor Output TypeUnit
differential pressurepressureV

Rawdata storage on board

During flight setra 239 data are stored within the aircraft onboard DMS system.

Data archiving on land

After the flight setra 239 data are accessible via the land system of the aircraft data managment system (DMS).

DMS

Module name

B712 Basic Meteorology, B719 Turbulence Noseboom 1, B851 Turbulence Noseboom 2

Device name

Static Pressure Slow

Parameters

ErrorText; Static Pressure Slow; Status


Documentation


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