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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 setra 239 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).

Sensor-Info: aircraft:bt-67:setra239, 6868



Manufacturer setra
Model 239
Serial No. n/a
Type pressure sensor

Contacts

 

Available devices and Specifications

Name Model Serial Number
Differential pressure transducer 239 (0-30 INWC) 6608170
Differential pressure transducer 239 (0-30 INWC) 4995087
Differential pressure transducer 239 (0-30 INWC) 4995089
Differential pressure transducer 239 (0-30 INWC) 4995088
Differential pressure transducer 239 (0-30 INWC) 4995086
Differential pressure transducer 239 (0-30 INWC) 6937824
Differential pressure transducer 239 (0-30 INWC) 7554970
Differential pressure transducer 239 (+/- 7,5 INWC) 4995080
Differential pressure transducer 239 (+/- 7,5 INWC) 4995081
Differential pressure transducer 239 (+/- 7,5 INWC) 4995082
Differential pressure transducer 239 (+/- 7,5 INWC) 4995083
Differential pressure transducer 239 (+/- 7,5 INWC) 6937826
Differential pressure transducer 239 (+/- 7,5 INWC) 6937827
Differential pressure transducer 239 (+/- 7,5 INWC) 7554969
Differential pressure transducer 239 (+/- 7,5 INWC) 7554968

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

Parameter Sensor Output Type Unit
differential pressure pressure V

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

Also see https://sensor.awi.de/ for calibration certificates of the sensors.


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