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CPA8001 Flight Data Calibrator



Flight data calibrator

Reference pressure sensor

Replaceable pressure reference pressure sensor
Apps
Height and Height Rate of Change Calibration
Airspeed calibration
Flight data computer calibration
Military, commercial, helicopter
R&D Lab

Features
Replace the sensor by removing the panel
Large-size touch screen for relevant information
Control stability is 0.001% of range
Accuracy up to 0.009% IS-50 (IntelliScale)

Description
Apps
Flight Data Calibrator CPA8001 (ADTS) is a pressure controller developed specifically for flight data science. The CPA8001 can be used to calibrate altitudes, climb rates, speedometers, digital sensors or flight data computers. Due to the modular design of the CPA8001, it can be flexibly configured according to customer needs.
Design
Flight Data Calibrator CPA8001 can be used as a desktop instrument or can be installed in a 19-inch cabinet. The device has two channels, each with a reference sensor CPR8001.
The sensor can be replaced by removing the front plate without having to disassemble the entire controller.
Features
Flight Data Calibrator CPA8001 has a large, high resolution touch screen. The menu logic is clear, the interface is easy to operate, and the convenience of operation is guaranteed to the greatest extent. Can support multiple languages.
On the screen you can display all the necessary parameters, such as the current measured value, height set point, airspeed, acceleration, etc. (pressure unit is optional). Customers can also set up their own test procedures through the device.
Users can remotely control the controller through the serial interface. Therefore, in addition to the current settings, other ADTS instruments have a series of virtual operational commands.
Complete Test Calibration System
can be equipped with mobile or static test systems according to customer needs. The product can be connected to other instruments via IEEE-48.8.2, RS-232, USB and Ethernet ports, allowing the corresponding instrument to be integrated into the current system.