GE Druck ADTS 405

Druck ADTS 405
Air Data Test Systems
User Manual K114
GE
Sensing
DRUCK ADTS 405
ATEX COMPLIANT
HAND TERMINAL
DO NOT DISCONNECT WHEN
ENERGIZED IN THE HAZARDOUS AREA
Ps
1013. 25 mbar
Aim
1013. 25<
Pt
3199. 91 mbar
Aim
3200. 00
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GE Druck ADTS 405 Specifications

General

Type	Air Data Test Set
Power Supply	100 to 240 VAC, 50/60 Hz
Airspeed Range	0 to 650 knots
Operating Temperature	0 to 50°C
Communication	RS232, IEEE-488
Housing	Rugged case

Summary

1 DESCRIPTION

1.1 Introduction

Provides an overview of the ADTS 405 and its versions.

2 INSTALLATION

2.1 Packaging

Details the contents of the packaging for ADTS 405 and 405F units.

2.2 Packaging for Storage or Transportation

Outlines procedures for packing the unit for storage or repair.

2.3 Electrical Connection

Explains how to connect the unit to electrical power supplies safely.

2.4 Pneumatic Pressure Connections

Describes pneumatic connections for ADTS 405 rack and flight line units.

2.6 Positioning of the ADTS 405 F

Covers safe positioning of ADTS 405F in hazardous areas.

3 OPERATION

3.1 Preparation

Details pre-operation checks and connections for the ADTS 405.

3.2 Display Functions and Units of Measure

Explains display options and unit conversions for data.

3.3 Quick Reference

Provides a quick reference to key-pad functions and commands.

3.4 First Time Operators

Guides new users through the initial power-up and system checks.

3.6 Power-up

Describes the power-up sequence and initial system status checks.

3.7 Control or Measure Parameter

Explains how to select parameters and set target values (aims).

3.8 Leak Testing the ADTS 405

Outlines the procedure for performing leak tests on the ADTS 405.

3.13 Changing the Units

Explains how to change between pressure and aeronautical units.

3.14 Limit Checking

Describes how the system checks data against set minimum and maximum limits.

Aircraft System Protection

Explains features for protecting aircraft systems against errors and leaks.

3.16 Options

SCPI IEEE 488 Option

Details the SCPI IEEE 488 interface for remote control.

Altimeter Encoder Option

Explains the Altimeter Encoder Option for displaying encoded altimeter data.

ARINC 429 Option

Describes the ARINC 429 interface for transmitting aeronautical data.

3.17 SETUP and CONFIGuration

FULL SET-UP

Provides complete access to all secondary functions and unit selections.

SETUP, [UNITS]

Allows configuration of default aeronautical and pressure units.

SETUP, [LIMITS]

Allows selection and programming of aircraft limit sets.

SETUP, [MORE], [CONTROL], [Ps Pt DUAL]

Configures dual channel operation and single channel testing modes.

SETUP, [MORE], [DISPLAYSOPTIONS], [DISPLAY TYPE]

Allows configuration of display types: single, dual, or triple.

SETUP, [MORE], [SYSTEM SELF TEST]

Initiates a system self-test routine.

SETUP, ALT

Allows changing the altitude correction value.

SETUP, SPEED, [AUTO ZERO]

Enables or disables the auto zero function for airspeed accuracy.

SETUP, SPEED, [CASTAS]

Switches airspeed display between CAS and TAS.

SET-UP, MACH

Allows changing or disabling the Mach limit.

SET-UP, RATE TIMER

Allows setting Wait/Time values for the RATE TIMER function.

SET-UP, RATE

Selects automatic airspeed rate control ON or OFF.

SETUP, LEAK MEASURE CONTROL, [AUTO LEAK]

Enables or disables the auto leak recovery facility.

SETUP, LEAK MEASURE CONTROL, [AUTO LIMIT]

Enables or disables the auto limit recovery facility.

SETUP, EXECUTE TEST PROGRAM

Sets up the results file options for printing or saving.

4 Maintenance

4.1 Introduction

Introduces operator maintenance tasks and their periodicity.

4.3 Maintenance Tasks

Details specific maintenance tasks (A-J) and their procedures.

5 TESTING AND FAULT FINDING

5.1 Introduction

Introduces the built-in self-test and diagnostic system.

5.2 Standard Serviceability Test

Provides a procedure to check the functions and facilities of the ADTS 405.

5.3 Self-Test Errors

Explains how self-test errors are displayed with error codes.

5.4 Venting after Overpressure

Details the procedure to vent pressure after an overpressure event.

5.6 Further Testing

Describes additional tests for pneumatic leaks or controller instability.

5.7 Testing an Option Facility

Explains how to test optional facilities like IEEE 488, Altimeter Encoder, ARINC 429.

5.8 Fault Finding

Introduces fault diagnosis and lists error messages.

5.8.2 Warning Messages

Lists warning messages, their causes, and recommended actions.

6 REFERENCE AND SPECIFICATION

6.1 Introduction

Introduces key functions and references to associated functions.

ALTPs

Describes the altitude and static pressure (Ps) display functions.

SPEEDQc

Explains airspeed (CAS/TAS) and dynamic pressure (Qc) display functions.

MACHPt

Describes Mach display and total pressure (Pt) display functions.

EPR

Explains the Engine Pressure Ratio (EPR) check and display.

LEAK MEASURECONTROL

Explains switching between Control and Leak Measure modes.

GROUND

Describes ground pressure display and controlling pressures to atmospheric.

REMOTE

Details entering Remote Mode for external control of the unit.

PRINT

Describes the facility to print displayed readings and user entries.

EXECUTE TEST PROGRAM

Explains using the Test Program Manager for aircraft and component testing.

6.3 SETUP

Introduces SETUP and CONFIGuration modes for system customization.

6.4 CONFIGURATION

Details how to change default settings and lock parameters.

6.5 Specification

Details physical, power, and performance specifications.

Control Performance

Covers stability, rate control, and control response characteristics.

Zone 2 Hazardous Area Definition

Defines Zone 2 hazardous areas and safety precautions for ATEX equipment.