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.
aircraft:bt-67:pt100 (6943)
| Manufacturer | Goodrich |
|---|---|
| Model | 102E |
| Serial No. | n/a |
| Type | temperature sensor |
Contacts
No contacts available.
Available Devices and Specifications
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
| Info | Temperature sensors are installed in the nose compartment as well as within the Turbulence Nose Boom. |
Data logging, storage and archiving
Logged parameter
| Parameter | Sensor Output Type | Unit |
|---|---|---|
| temperature analogue signal | temperature | Ohm |
Rawdata storage on board
Data archiving on land
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.