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Attention:

Temperature sensors are permantly installed in a de-iced Rosemount housing in both aircraft as part of the Basic Meteorology module. Additionally, temperature sensors are installed in nose booms used for turbulence measurements. Here two sensors are used - one in a de-iced and one in a not de-iced Rosemount housing.

Summary

Temperature sensors are used for measuring the air temperature at the nose of the aircraft or within the Turbulence Nose Boom. The Turbulence Nose Boom comprises de-iced as well as non-deiced sensors while the basic meteorology only uses de-iced sensors.

Sensor-Info: aircraft:bt-67:pt100, 6943


ManufacturerGoodrich
Model102E
Serial No.n/a
Typetemperaturesensor



Contacts


Available Devices and Specifications

NameModelSerialNumber
PT100 Temperature Sensors102EB10807
PT100 Temperature Sensors102E14658E
PT100 Temperature Sensors102E14663E
PT100 Temperature Sensors102E70511
PT100 Temperature Sensors102EB10530
PT100 Temperature Sensors102EB10682

Specifications of temperature sensor (without mounting)

Dimension (max. diameter x W x H)

64 x 65 x 128 mm

Weight

~0.6 kg (incl. sensor)

Power Supply

28 VDC

Data interface

analogue data (Ohm)

Position


Temperature sensors are installed in the nose compartment as well as within the Turbulence Nose Boom.

Data logging, storage and archiving

Logged parameter

ParameterSensor Output TypeUnit
temperature analog signaltemperatureOhm

Rawdata storage on board

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

Data archiving on land

After the flight temperature 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

Humicap

Parameters

ErrorText; Relative Humidity Raw [A]; Status; Temperature raw [A]


Documentation

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


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