
Do you have a question about the GE Druck ADTS 2 Series and is the answer not in the manual?
| Pneumatic pressure range | -15 to 300 psi |
|---|---|
| Pneumatic pressure units | psi, kPa, bar, mbar, inH2O, ftH2O, inHg, mmHg |
| Power | 100-240 VAC, 50/60 Hz |
| Interfaces | RS232, Ethernet |
| Pressure Range | -15 to 300 psi |
Describes the probe used for pressure measurements, calculating altitude and airspeed.
Details checking the ADTS 2XX contents against the packaging list upon receipt.
Provides procedures for packing the tester for storage or return for calibration/repair.
Covers warnings, power supply, and cable connections for the ADTS 2XX.
Details the pneumatic connections for Ps1, Ps2, and Pt using expansion ports.
Advises on safe placement, environmental considerations, and altitude correction.
Explains different configurations for connecting the ADTS 2XX with hand terminals and PCs.
Details essential pre-use checks, including safety, connections, and leak testing.
Guides through the process of powering on the ADTS 2XX and checking initial displays.
Explains the main operation menu, key selections, and navigation controls.
Instructions for creating and editing custom test sequence files in CSV format.
Explains SCPI syntax for external control, commands, and queries via RS232.
Details daily, weekly, and periodic maintenance tasks for the ADTS 2XX.
Covers replacing o-rings, fuses, and AHT repair guidelines.
A procedure to verify if the unit is serviceable and check its functions.
Procedures for performing pressure and vacuum leak checks on the ADTS 2XX.
Lists error codes and messages displayed at power-up, with probable causes and actions.
Provides tables of error messages, probable causes, and recommended actions for troubleshooting.
Details the general specifications of the ADTS 2XX, including weight, power, and environment.
Lists the air data measurement ranges, resolutions, and accuracies for Ps1, Ps2, and Pt ports.
Defines default and alternative operating limits for various parameters like altitude, airspeed, and pressure.











