GE Druck ADTS 405 R/F Mk2 Instruction Manual

Druck ADTS 405 R/F Mk2

Air Data Test Set

Instruction Manual

ADTS HAND TERMINAL

GE Data Classification: Public

500VA

POWERSUPPLY24-30V

FUSES

T32A

T20A

POWERSUPPLY

100/120/230V~50/60Hz500VA

115~400Hz500VA

FUSES

T5.0A250VHRC

www.gemeasurement.com

INTRODUCTION

This technical manual provides operating instructions for the Druck Air Data Test System ADTS 405 Mk 2 series.

SCOPE

This technical manual contains a brief description, operation and testing procedures for the user of this equipment.

SAFETY

The manufacturer has designed this equipment to be safe when operated using the procedures detailed in this manual:

• Do not use this equipment for any other purpose than that stated. the protection given by the equipment from working.

• See Product Safety and Installation Guide 124M8686, also supplied, for essential operating and Safety instructions that must be followed to ensure safe operation.

• Use suitably qualified Technicians and good engineering practice for all procedures in this publication.

*A qualified technician must have the necessary technical knowledge, documentation, special test equipment and tools to carry out the required work on this equipment.

Incorrect use can prevent

PRESSURE

Do not apply pressure greater than the maximum safe working pressure specified in this manual when using the ADTS405 Mk 2 series.

TOXIC MATERIALS

There are no known toxic materials used in this equipment.

MAINTENANCE

The equipment must be maintained using the manufacturer’s procedures and should be carried out by authorized service agents or the manufacturer’s service departments.

For technical advice contact GE or subsidiary manufacturer of this product.

MARKS AND SYMBOLS ON THE EQUIPMENT

Symbol Description

This equipment meets the requirements of all relevant European safety directives. The equipment carries the CE mark.

This symbol on the equipment indicates that the user should refer to the user manual.

This symbol on the equipment indicates a warning and that the user should refer to the user manual.

This symbol warns the user of the danger of electric shock.

Do not dispose of this product as household waste. Use an approved organization that collects and/or recycles waste electrical and electronic equipment. For more information contact your Customer Service using the details shown at the back, or your local Government Office.

For the list of approved GE service centers go to: www.gemeasurement.com

ASSOCIATED PUBLICATIONS

The following table lists the Druck publications referenced in this manual:

Safety and Installation Guide - Air Data Test Systems ADTS 405F/ 405R 124M8686

Calibration Manual -

IEEE 488 OPT 2 Manual -

SCPI IEEE 488 Manual -

User Manual -

Operating and Communications Manual -

Altimeter Encoder Option K0170

Line Switching Unit LSU 100/101

Air Data Test System ADTS 405

Line Switching Unit LSU Series

K0199

K0154

K0157

K0220

K0223

ABBREVIATIONS

The following abbreviations are used in this manual; the abbreviations are the same in the singular and plural.

Abbreviation Description

A Ampere

abs Absolute

a.c. Alternating current

ALT Altitude

CAS Calibrated airspeed

d.c. Direct current

e.g. For example

EOC End of conversion

EPR Engine pressure ratio

EPROM Electrically programmable read only memory

etc. And so on

Fig. Figure

ft Foot

g Gauge

Hg Mercury

Hz Hertz

IAS Indicated airspeed

i.e. That is

IEEE 488 Institute of Electrical and Electronic Engineers standard 488 data

in inch

kg Kilogram

LED Light emitting diode

(M) Magnesium alloy

m Meter

mA Milliampere

max Maximum

mbar Millibar

mV Millivolts

No. Number

N.m. Newton meter

Para. Paragraph

Ps Static pressure

psi Pounds per square inch

Abbreviation Description

Pt Total pressure (pitot)

Qc Differential pressure Pt-Ps

QFE Local atmospheric pressure

QNH Barometric pressure at sea level

ROC Rate of climb

Vc Calibrated velocity

Vt True velocity

+ve Positive

-ve Negative

°C Degrees Celsius

GLOSSARY

The terminology used in this manual is specific and individual interpretation must not be introduced. The terms are defined as follows:

Item Description

Adjust To bring to a more satisfactory state; to manipulate controls, levers, linkages, etc. to

return equipment from an out-of-tolerance condition to an in-tolerance condition.

Align To bring into line; to line up; to bring into precise adjustment, correct relative

position or coincidence.

Assemble To fit and secure together the several parts of; to make or form by combining parts.

Calibrate To determine accuracy, deviation or variation by special measurement or by

comparison with a standard.

Check Make a comparison of a measure of time, pressure, temperature, resistance,

dimension or other quality with a known figure for that measurement.

Disconnect To detach the connection between; to separate keyed or matched equipment parts.

Dismantle To take apart to the level of the next smaller unit or down to all removable parts.

Ensure To confirm that a proper condition exists; to find out with certainty.

Examine To perform a critical visual observation or check for specific conditions; to test the

condition of.

Fit Correctly attach one item to another.

Inspect Review the work carried out by Specialists to ensure it has been performed

satisfactorily.

Install To perform operations necessary to properly fit an equipment unit into the next

larger assembly or system.

Maintain To hold or keep in any particular state or condition especially in a state of efficiency

or validity.

Operate Ensure that an item or system functions correctly as far as possible without the use

of test equipment or reference to measurement.

Readjust To adjust again; to move back to a specified condition; to bring back to an in-

tolerance condition.

Reconnect To rejoin or refasten that which has been separated.

Refit Fit an item which has previously been removed.

Remove To perform operations necessary to take an equipment unit out of the next larger

assembly or system. To take off or eliminate. To take or move away.

Repair To restore damaged, worn out or malfunctioning equipment to a serviceable, usable

or operable condition.

Replace Remove an item and fit a new or a serviced item.

Reset To put back into a desired position, adjustment or condition.

Service To perform such operations as cleaning, lubricating and replenishing to prepare for

use.

Test Ascertain by using the appropriate test equipment that a component or system

functions correctly.

RETURNED GOODS PROCEDURE

If the unit is unserviceable and requires a repair return to a GE Service Centre. Contact the GE Service Centre, either by 'phone, fax or e-mail to obtain a Returned Goods Authorization (RGA) number, providing the following information:

• Product (i.e. ADTS 405)

• Pressure medium (i.e. air, nitrogen)

• Serial number

• Details of defect/work to be undertaken

• Operating conditions

SAFETY PRECAUTIONS

See Safety and Installation Guide 124M8686

Note: Do not use unauthorized sources to service this equipment as this will affect the

warranty and may not guarantee further performance.

PRESSURE UNITS AND CONVERSION FACTORS

Pressure units Factor (hPa) Pressure units Factor (hPa)

mbar 1.0 cmH

bar 1000.0 mH

Pa (N/m2)0.01 kg/m

hPa 1.0 kg/cm

kPa 10.0 torr 1.333223684

MPa 10000.0 atm 1013.25

mmHg @ 0°C 1.333223874 psi 68.94757293

cmHg @ 0°C 13.33223874 lb/ft

mHg @ 0°C 1333.223874 inH

inHg @ 0°C 33.86388640341 inH2O @ 20°C 2.486413

mmH

O @ 4°C 0.0980665 inH2O @ 60°F 2.487641558

O @ 20°C 0.978903642

O @ 20°C 97.8903642

O @ 4°C 2.4908891

0.0980665

980.665

0.4788025898

O @ 4°C 0.980665 ftH2O @ 4°C 29.8906692

cmH

O @ 4°C 98.0665 ftH2O @ 20°C 29.836983

mmH

O @ 20°C 0.097890364 ftH2O @ 60°F 29.8516987

Unit Conversion

To convert FROM pressure Value 1(in pressure Units)1 TO pressure Value 2 in pressure Units: Calculate as follows:

Value 2 = Value 1 x Factor 1 ÷ Factor 2

Contents

1. DESCRIPTION 1

1.1 Introduction 1

1.2 Operating Range and Performance 1

1.3 Operating Limits 2

2. INSTALLATION 5

2.1 List of Parts 5

2.2 Packaging for Storage or Transportation 5

2.3 Power Supply 9

2.3.1 405R Rack-mounted version 9

2.3.2 405F Flightline version 9

2.4 Positioning of the ADTS 10

2.4.1 405R Rack-mounted version 10

2.4.2 405F Flightline version 10

3. OPERATION 15

3.1 Preparation 15

3.2 Start-up 15

3.2.1 Connections 15

3.2.2 Power-up 16

3.2.3 Units of Measure 18

3.3 Operation quick reference 19

3.4 Operating modes 20

3.5 Operating Procedures 24

3.5.1 Control or Measure Parameter 24

3.5.2 Aim 28

3.5.3 Leak Measure 29

3.5.4 Aircraft system protection 31

3.5.5 Limit Checking 31

3.5.6 Changing Parameters 33

3.5.7 Engine Pressure Ratio (EPR) 34

3.6 Testing Aircraft Systems or UUT 35

3.6.1 Go To Ground and Shut-down 35

3.6.2 SETUP and CONFIGuration options 36

3.7 Communications panel options 45

3.7.1 Ethernet System 45

3.7.2 Access ADTS files 47

3.7.3 Connection of the IEEE 488 Facility 48

3.8 Enabling the Altimeter Encoder Option 49

4. MAINTENANCE 51

4.1 Introduction 51

4.2 Materials 51

4.3 Maintenance Tasks 52

4.4 Routine Maintenance 53

4.4.1 Servicing Procedures 53

4.4.2 Replacing the output connector o-ring 53

4.4.3 Fuse Replacement 53

4.5 Cable tests 56

5. TESTING AND FAULT FINDING 59

5.1 Introduction 59

5.2 Error messages 59

5.3 Standard Serviceability Test 60

5.3.1 Procedure 60

5.3.2 Fault Finding 61

5.4 Fault Diagnosis 62

5.5 Ventilating after Overpressure 63

5.6 Further Testing 65

5.6.1 Environmental and preliminary operations 65

5.6.2 Pressure Leak check 65

5.6.3 Vacuum leak check 66

5.6.4 Range Check 66

5.6.5 Controller Stability 66

5.6.6 Testing of Standard and Optional External Communication Ports 67

5.6.7 Testing of IEEE 488 Facility 68

5.6.8 Testing the Altimeter Encoder Option 69

6. REFERENCE AND SPECIFICATION 71

6.1 Introduction 71

6.2.1 F1 - F4 72

6.2.2 ALT/Ps 72

6.2.3 SPEED/Qc 72

6.2.4 MACH/Pt 73

6.2.5 EPR 73

6.2.6 ROC/Ps RATE 73

6.2.7 RATE TIMER 73

6.2.8 HOLD 74

6.2.9 RATE 75

6.2.10 LEAK MEASURE/CONTROL 75

6.2.11 GROUND 76

6.2.12 [GO TO GROUND] 76

6.2.13 [DISPLAY QFE] 76

6.2.14 [DISPLAY QNH] 77

6.2.15 PORT 77

6.2.16 REMOTE 77

6.2.17 PRINT 77

6.2.18 EXECUTE TEST PROGRAM 78

6.2.19 HELP 79

6.2.20  or (Nudge Keys) 79

6.2.21 Number 0 to 9 79

6.2.22 -000 80

6.2.23 CLEAR/QUIT 80

6.2.24 ENTER 80

6.2.25 CLEAR + ENTER (ABORT) 80

6.2.26 SETUP 81

6.2.27 FULL SET-UP 81

6.2.28 SETUP, [UNITS] 81

6.2.29 SETUP, [LIMITS] 82

6.2.30 SETUP, [OSC] 82

6.2.31 SETUP, [MORE], [CONTROL], [Ps Pt DUAL] 83

6.2.32 SETUP, [MORE], [DISPLAYS/OPTIONS], [DISPLAY TYPE] 83

6.2.33 SETUP, [MORE], [DISPLAYS/OPTIONS], [OPTIONS] 85

6.2.34 SETUP, [MORE], [CLOSE OUTPUT VALVES] 85

6.2.35 SETUP, [MORE], [OPEN OUTPUT VALVES] 85

6.2.36 SETUP, [MORE], [SYSTEM SELF TEST] 85

6.2.37 SETUP, ALT (Figures 6-5 and 6-6) 86

6.2.38 SETUP, SPEED, [AUTO ZERO] 86

6.2.39 SETUP, SPEED, [CAS/TAS] 86

6.2.40 SET-UP, SPEED, [Pt TEMPERATURE] 87

6.2.41 SET-UP, MACH 87

6.2.42 SET-UP, RATE TIMER 88

6.2.43 SET-UP, RATE 88

6.2.44 SETUP, LEAK MEASURE CONTROL, [AUTO LEAK] 88

6.2.45 SETUP, LEAK MEASURE CONTROL, [AUTO LIMIT] 88

6.2.46 SETUP, GROUND 88

6.2.47 SETUP, [PORT] 88

6.2.48 SETUP, PRINT, [DATE/TIME] 88

6.2.49 SETUP, EXECUTE TEST PROGRAM 89

6.2.50 SETUP, HELP 89

6.2.51 SETUP, or  (Nudge keys) 89

6.2.52 MINIMUM SETUP 89

6.2.53 SETUP, [UNITS], [AERO] 89

6.2.54 SETUP, [UNITS], [PRESS] 89

6.2.55 SETUP, [LIMITS] 90

6.2.56 SETUP, HELP 90

6.2.57 CONFIGURATION 90

6.2.58 CONFIG, [UNITS] 91

6.2.59 CONFIG, [LIMITS], [EDIT LIMITS], [EDIT EXISTING] 91

6.3 ADTS 405R/F Specification 97

6.4 Measurement and Control Range Specifications 99

Figures

Figure Page

2-1 Equipment and Parts 7 2-2 ADTS 405R Altitude Reference 10 2-3 ADTS 405F Altitude Reference 11 2-4 ADTS 405R Front Panel View 11 2-5 ADTS 405R Rear Panel 12 2-6 ADTS 405F General View 13 3-1 Front Panel 18 3-2 Single Display 25 3-3 Dual Display 25 3-4 Triple Display 26 3-5 Rate Timer Display Aeronautical Units 26 3-6 Rate Timer Display Pressure Units 27 3-7 Pt Only Display 27 3-8 Set-up example 36 3-9 Configuring Windows For ADTS Subnet IP Address 45 3-10 Ping Test From Windows Command Prompt 46 3-11 PuTTY Configuration 46 3-12 Changing the default password 47 3-13 WinSCP Login Screen 47 3-14 ADTS File System Directories Screen 48 4-1 Output Connector O ring Seal 53 4-2 ADTS 405F AC Fuse Positioning 54 4-3 ADTS 405F DC Fuse Positioning 55 4-4 ADTS 405R AC Fuse Positioning 56 5-1 Fault Finding Chart 62 5-2 External Communications 67 6-1 Altitude Correction Rack Mounting 87 6-2 ALTITUDE CORRECTION ON-AIRCRAFT 87 6-3 ARINC 565 OPERATING LIMITS 93

Tables

Table Page

2-1 ADTS MK2 SPARES AND ACCESSORIES LIST 8 2-2 DC Input Connector 10 3-1 Units of Measure 18 3-2 Warning Messages 32 3-3 IEEE 488 facility 49 4-1 Maintenance Chart 51 4-2 Materials List 51 4-3 Tool and Test Equipment Requirements 52 4-4 AC Input Connector 57 4-5 DC Input Connector 57 5-1 Error Messages 59 5-2 Fault Advice and Action 63 5-3 Optional cable (AAU-32 units) 69 6-1 Aeronautical Units Dual Display 83 6-2 Pressure Units Dual Display 84 6-3 Aeronautical units triple display 84 6-4 Pressure units triple display 85

Introduction

1. DESCRIPTION

1.1 Introduction

There are two versions of this Air Data Test System, a 19", 6U high (10½”) rack-mounted unit (ADTS 405R) and a flight line unit (ADTS 405F).

The ADTS 405R is a rack-mounted system and, with external pressure and vacuum supplies connected, provides measurement and control of pitot and static systems and components. The unit can be used for leak checks, calibration accuracy checks and functional tests of air data instruments, components and systems.

The ADTS 405F is a self-contained flight-line air data test system providing complete pitot and static measurement and control. The unit can be used for on-aircraft sense and leak testing, calibration accuracy checks and functional tests of air data instruments, components and systems. The ADTS 405F comprises an electronics rack and pump rack enclosed in a high density, polyethylene case.

The ADTS 405 displays and operates in either units of pressure measurement or aeronautical units. In the control mode, the rate that the pressures change towards new set-points can be controlled in true aeronautical rate units.

There are two independent pneumatic channels connect to the aircraft or instrument systems, one for static and one for pitot. They can be operated as measure only channels with leak testing facility or each can be control channels producing true pressure conditions for altitude and airspeed.

To protect sensitive instruments and equipment a “ground” facility automatically and safely controls both channels to atmospheric pressure at the previously entered rates of change and then informs the operator when both channels are safely at “ground”.

The operator interface is either a hand terminal connected to the front panel or the key pad and display on the front panel. Both provide information and control selections for the user through the keys and display. The keypad has a back-light for improved operation in poor light conditions. The unit can also be controlled remotely using the IEEE488 communications interface. The front panel contains the operate switch and a mimic panel with LED indicators showing the operation of the solenoid-operated pneumatic valves.

The pump rack, on the ADTS 405F, produces pressure and vacuum supplies for the electronics rack and for external services. Located on the front panel, the external connectors provide for external pressure and vacuum supplies (EXT PRESSURE and EXT VACUUM) and an auxiliary static (vacuum) output (AUX). The rack is cooled by a fan located under a protective cover on the front panel. The power supply connection for the ADTS 405F is located on the front panel.

1.2 Operating Range and Performance

The ADTS 405 is supplied in one of two full-scale ranges (850 knots or 1000 knots) for measurement and control of the pitot pressure channel.

Operating limits are set, pre-defined tabular limits known as STANDARD, CIVIL and MAX these can be selected through the SETUP menu (see Reference section 6). Operators may also configure the display to aeronautical or pressure units but should be aware that when units of pressure are selected, wider full-scale pressure limits will be enabled for some parameters.

Chapter 1. DESCRIPTION

1.3 Operating Limits

The following sets of operating limits are supplied with the ADTS 405.

850 knot range operating limits

Parameter Max Limits Standard Limits Civil Limits

Min Alt -3,000 ft -2,000 ft -1,000 ft

Max Alt 105,000 ft 80,000 ft 50,000 ft

Min CAS -100 kts 0.0 kts 0 kts

Max CAS 850 kts 850 kts 450 kts

Min Ps 3.0 mbar 27.615 mbar 115.972 mbar

Max Ps 1355.00 mbar 1088.657 mbar 1050.406 mbar

Min Qc -1,352.00 mbar 0.0 mbar 0.0 mbar

Max Qc 1,700.00 mbar 1688.00 mbar 368.01 mbar

Max Mach 12.35 2.5 1

Max ROC 100,000 ft/min 9,000 ft/min 6,000 ft/min

Max Rate CAS 2,000 kts/min 600 kts/min 600 kts/min

Max Rate Ps 10,000.00 mbar/min 200.00 mbar/min 100.00 mbar/min

Max Rate Qc 10,000.00 mbar/min 200.00 mbar/min 100.00 mbar/min

ARINC Limits OFF OFF OFF

Alt Correction 0 ft 0 ft 0 ft

Operating Limits

1000 knot range operating limits

Parameter Max Limits Standard Limits Civil Limits

Min Alt -3,000 ft -3,000 ft -1,000 ft

Max Alt 105,000 ft 80,000 ft 50,000 ft

Min CAS -100 kts 0.0 kts 0 kts

Max CAS 1,000 kts 1,000 kts 450 kts

Min Ps 3.0 mbar 27.615 mbar 115.972 mbar

Max Ps 1355.00 mbar 1,128.029 mbar 1050.406 mbar

Min Qc -1,352.00 mbar -16.303 mbar 0 mbar

Max Qc 2,500.00 mbar 2,490.50 mbar 368.01 mbar

Max Mach 14.97 5 1

Max ROC 1000,000 ft/min 15,000 ft/min 6,000 ft/min

Max Rate CAS 2,000 kts/min 700 kts/min 600 kts/min

Max Rate Ps 10,000.00 mbar/min 200.00 mbar/min 100.00 mbar/min

Max Rate Qc 10,000.00 mbar/min 200.00 mbar/min 100.00 mbar/min

ARINC Limits OFF OFF OFF

Alt Correction 0 ft 0 ft 0 ft

Chapter 1. DESCRIPTION

List of Parts

2. INSTALLATION

Special request

Please keep the special packing boxes so that the ADTS can be safely shipped for calibration, repair or storage.

2.1 List of Parts

On receipt of the ADTS 405 check the contents of the packaging against the following lists:

Standard Packaging List - ADTS 405F Standard Packaging List - ADTS 405R

i) Flight line ADTS 405F i) Rack ADTS 405R

ii) Accessory bag ii)

Power supply cable 2m or 10m (regional plug

iii)

as per order)

iv) Hand terminal (optional) iv) Input, hose, 15m, green, AN6 - open

v) Hand terminal cable - 2 m (optional) v) Input, hose, 15m, yellow, AN4 - open

vi) Hand terminal cable - 18 m (optional) vi) Kit, fuse/o-ring

vii) User Manual K0572 (this publication) vii) Plug, expansion port

viii) Kit, fuse/o-ring viii) Safety and Installation Guide 124M8686

Power supply cable 2.5m (regional plug as per order)

iii) User Manual K0572 (this publication)

ix) Safety and Installation Guide 124M8686

2.2 Packaging for Storage or Transportation

WARNING THE FLIGHT-LINE UNIT CAN BE MOVED BY USE OF THE HANDLE AND

WHEELS, BUT IF IT IS TO BE LIFTED, IT IS A TWO PERSON LIFT.

Environment The optimum conditions for ADTS405 Mk2 equipment during transit, preparation for calibration and

repair and when being storage are detailed as below. Items in storage are defined as being nonoperational. If the ADTS becomes exposed to moisture or very high humidity, dry as soon as possible and temporarily store in a low humidity area. The following conditions apply for storage or shipping:

Temperature Range -51° to 70°C (-60° to +158°F) Altitude Up to 50,000 feet (15,240 metres)

Procedure

1. The unit should be at zero/ambient pressure.

2. Disconnect all hose assemblies and stow them in the shoulder bag.

3. Switch power OFF and disconnect from the electrical power supply.

4. Disconnect the power supply cable and the hand terminal cable.

5. Disconnect the hand terminal cable from the hand terminal.

Chapter 2. INSTALLATION

When using packing materials other than the original, proceed as follows:

1. Wrap unit in polyethylene sheeting.

2. Select a double-wall cardboard container. Inside dimensions must be at least 15 cm greater than the equipment. The carton must meet test strength requirements of >125 kg.

3. Protect all sides with shock-absorbing material to prevent equipment movement within the container.

4. Seal carton with approved sealing tape.

5. Mark carton “FRAGILE” on all sides, top, and bottom of shipping container.

Note: For ADTS 405R rack units loose or peripheral items should be placed in a sealed polythene bag. For ADTS 405F stow the power supply cable, hand terminal cable and the hand terminal in the ADTS 405F lid. Fit the lid to the unit.

SHOULDER BAG

Packaging for Storage or Transportation

HAND TERMINAL

ADTS 405F

ADTS 405R

4a-h

5a-p

REGIONAL LINE PLUG

AC CABLE (ADTS 405F)

HAND TERMINAL CABLES

2.5mREGIONAL LINE PLUG

AC CABLE (ADTS 405R)

2m or 10m

18m

IEC

ACCESSORIES

EXPANSION PORT DONGLE

(ADTS 405R ONLY)

9a-d

OPTIONAL CONFIGURABLE

ORDER ITEMS

AIRCRAFT HOSES (Ps / Pt, RED / BLUE)

ALTIMETER ENCODER CABLE (OPTION)

SERVICE KIT

SERVICES HOSES (ADTS 405R ONLY) PRESSURE / VACUUM, YELLOW / GREEN

15m

DC CABLE (OPTION)

Figure 2-1: Equipment and Parts

Chapter 2. INSTALLATION

Table 2-1: ADTS MK2 SPARES AND ACCESSORIES LIST

Item Part Number Description Used On

1 - FLIGHTLINE ASSEMBLY (configured order item) 2 AS405-111-1728M0 3 AS505-57-3124M0 Accessory Bag 4a

†4b* †4c* †4d*

†4e* †4f †4g*

†4h* 5a

5b 5c 5d 5e 5f 5g 5h 5i 5j 5k 5l 5m 5n 5o 5p

6 7* 8 9a 9b 9c

9d 10 11 12

AA405F-23 AA405F-24 AA405F-25 AA405F-26

AA405F-27 AA405F-28 AA405F-29

AA405F-30 AA405F-1

AA405F-2 AA405F-3 AA405F-4 AA405F-5 AA405F-6 AA405F-7 AA405F-8 AA405F-9 AA405F-10 AA405F-11 AA405F-12 AA405F-13 AA405F-14 AA405F-15 AA405F-16

AS405-33-1891M0 AS405-34-1891M0 AS405-22-1891M0 EXPANSION PORT DONGLE ADTS 405R AA500F-19 AA500F-20 AA500F-22

AA500F-23 AS405-60-1891M0 AS405-82-1891M0 AS405-53-1729M0 /

AS405-54-1729M0

AS405-31-1891M0 POWER CABLE DC (OPTION) ADTS 405F * not illustrated † option

HAND TERMINAL ASSEMBLY ADTS 405F/R

IEC 60320 to UK Style, BS1363 IEC 60320 to USA/Canada style, NEMA 5-15P IEC 60320 to European style, Schuko CEE 7/7 IEC 60320 to Australia/New Zealand style, AS/NZS4417 (AS3112) IEC 60320 to India style, IS 1293 (IA16A3, BS546) IEC 60320 to China style, GB 15934 (GB 2099, GB1002) IEC 60320 to South Africa style, SANS 164-1 (SANS 60799, BS546) IEC 60320 to Japan style, JIS 8303 (NEMA 5-15P)

LEAD, AC POWER, UK, 2m LEAD, AC POWER, UK, 10m LEAD, AC POWER, USA, 2m LEAD, AC POWER, USA, 10m LEAD, AC POWER, EUROPE, 2m LEAD, AC POWER, EUROPE, 10m LEAD, AC POWER, NEW ZEALAND, 2m LEAD, AC POWER, NEW ZEALAND, 10m LEAD, AC POWER, INDIA, 2m LEAD, AC POWER, INDIA, 10m LEAD, AC POWER, CHINA, 2m LEAD, AC POWER, CHINA, 10m LEAD, AC POWER, SOUTH AFRICA, 2m LEAD, AC POWER, SOUTH AFRICA, 10m LEAD, AC POWER, JAPAN, 2m LEAD, AC POWER, JAPAN, 10m

LEAD, HAND TERMINAL 2 M LEAD, HAND TERMINAL 18 M

HOSE, RED (state length in metres) HOSE, BLUE (state length in metres)

CONNECTOR, HOSE, AN4 FEMALE CONNECTOR, HOSE, AN6 FEMALE ALTIMETER ENCODER CABLE FUSE/O-RING KIT

HOSE SET, PRESS. / VAC. YELL. / GRN.

ADTS 405F

ADTS 405R

ADTS 405F

ADTS 405F/R ADTS 405F/R

ADTS 405F/R ADTS 405F/R ADTS 405F/R

ADTS 405R

Examine all equipment to be used, paying particular attention to electrical leads and connectors and pneumatic pipes and connectors.

CAUTION DO NOT USE ANY EQUIPMENT THAT IS KNOWN TO BE OR SUSPECTED TO BE

DAMAGED OR FAULTY.

2.3 Power Supply

See Safety and Installation Guide 124M8686 for full details.

AC Input

AC power supply

100 / 120 / 230V ~ 50 / 60Hz

115V ~ 400Hz 500VA

DC Input (Option ADTS405 F only)

DC power supply

24 - 30V

500VA

2.3.1 405R Rack-mounted version

Power Supply

1. The unit must be connected to the correct electrical power supply as stated, beside the power connectors on the rear panel.

2. Install an easily accessible isolator in the power supply circuit.

3. The power supply connector on the rear panel of the unit will not be accessible when fitted in the equipment rack.

Note: The power supply switch on the front panel is not classified as a disconnecting device.

On the ADTS 405R, two 20mm High Breaking Capacity fuses are located in the holder mounted on the power input connector on the rear of the rack and protect the entire unit. The fuses are connected in the live and neutral supply circuit and are: T5A/250V HRC type. Only replace the fuses with the correct type, see Figure 2-1 item 11 section 4-4.

2.3.2 405F Flightline version

1. The power switch on the front panel is not a power isolator as defined by EN61010. To isolate the power supply disconnect the power supply connector.

Fuses AC Power

The fuses fitted in the fuse holders on the front panel are: T5A/250V HRC type. Only replace a fuse with the correct type, see Figure 2-1, item 11. To replace a fuse see Section 4-4.

Fuses DC Power

The fuses fit in the fuse holders on the front panel are either: T20.0A/250V HRC type (on the left) or T32A/250V HRC type (on the right). The DC power option (nominal 28 V DC), can be an alternative power supply using an additional connector located on the pump front panel. Only replace a fuse with the correct type, see Figure 2-1, item 11 To replace a fuse see, Section 4-4.

Chapter 2. INSTALLATION

Table 2-2: DC Input Connector

ADTS Pin Cable Colour Function

1 Grey + 28V 2 White 0V Return

EARTH Green Protective Ground

CAUTION A protective EARTH connection must also be made for DC operation or

specified EMC performance may be impaired.

2.4 Positioning of the ADTS

2.4.1 405R Rack-mounted version

It is important that the position of the ADTS 405 in relation to the UUT is known. An altitude correction must be made to allow for the difference in height between the reference level, indicated on the mimic panel, and the UUT. The Reference section contains details of altitude correction (SETUP, ALTITUDE).

WARNING OBSERVE THE APPROPRIATE SAFETY INSTRUCTIONS AND PROCEDURES

DETAILED IN THE AIRCRAFT MAINTENANCE MANUAL AND COMPONENT MAINTENANCE MANUALS.

rack-mounted ADTS 405R

ADTS panel marked reference level

requires negative

UUT

Corrected altitude output = true altitude output increased by height difference

Figure 2-2: ADTS 405R Altitude Reference

altitude correction value entered when below ADTS

UUT reference level

2.4.2 405F Flightline version

It is important that the position of the ADTS 405F in relation to the aircraft altitude sensors is known. An altitude correction must be made to allow for the difference in height between the reference level and the aircraft's altitude sensors. The Reference section contains details of altitude correction (SETUP ALTITUDE).

Positioning of the ADTS

WARNING THE ADTS SHOULD NOT BE PLACED IN CONTACT WITH HAZARDOUS FUEL

VAPOUR CONCENTRATIONS.

Instruments

Aircraft reference level

requires positive altitude correction value entered when above ADTS

ADTS reference level

Air Data

Computer

Corrected altitude output = true altitude output decreased by height difference

Figure 2-3: ADTS 405F Altitude Reference

STATIC

PITOT

Cover plate for communications connectors

Hand terminal connector

Altimeter encoder connector (option)

Static output connector

Altitude sensor datum height

Key-pad and display

Solenoid valve status indicator

Pitot output connector

Figure 2-4: ADTS 405R Front Panel View

Power connection indicators

System status indicator

Calibration enable switch

Power supply switch

Chapter 2. INSTALLATION

AC fuses holder

DC power supply Connector (option)

AC power supply connector

Pressure regulator

Source Pressure Input connector

INPUT

24-30V

400VA

INPUT

100/120/230V~50/60Hz

115V~400Hz

400VA

FUSED2x

T5A250VHRC

Source Vacuum Input connector

Cooling fan air intake

Expansion port (used with GE PV103R pump unit)

Figure 2-5: ADTS 405R Rear Panel

Pitot output connector

IEEE 488 interface

Static output connector

Note:

When port not used with other equipment the Expansion Port Plug

connector

MUST

be fitted.

+ 92 hidden pages

GE Druck ADTS 405 R/F Mk2 Instruction Manual

Specifications and Main Features

Frequently Asked Questions

User Manual

1. DESCRIPTION

1.1 Introduction

1.2 Operating Range and Performance

1.3 Operating Limits

2. INSTALLATION

2.1 List of Parts

2.2 Packaging for Storage or Transportation

2.3 Power Supply

2.3.1 405R Rack-mounted version

2.3.2 405F Flightline version

2.4 Positioning of the ADTS

2.4.1 405R Rack-mounted version

2.4.2 405F Flightline version