ATEQ ADSE 650 User manual

ADSE 650
USER MANUAL
REFERENCE V15-D2-0174-O / FEBRUARY 2023
INTERACTIVE NAVIGATION
ateq-aviation.com

ADSE 650 / USER MANUAL / Reference V15-D2-0174-0 / February 2023 2/79
Exhaustive Table of Content
Revision of the Manual
Contact
Safety Advisory
PRESENTATION
General
Applications
Characteristics
Units, Range and Precision
Domain Flight Option
Technical description
USER ACCESS
ADSE 650 RCU front panel
ADSE 650 EPU front panel
GETTING STARTED
Initial Procedures
OPERATOR INTERFACE
Starting software
Access to the ight domains
Measure/Manual Mode
Automatic program mode
File Manager
General Information
Help on line
Exiting the software
Keyboard conguration
Manual grounding
MAINTENANCE
Low Level Maintenance
Autotest Function
Maintenance Plan
Error and warning list
OPTIONS
1/ RCU link-serial Option
2/ EPR Option
3/ Cabin Pressure Option
4/ Outow Valve Option
SAFETY INFORMATION
EXHAUSTIVE TABLE OF CONTENT
Revision of the Manual...................................................................................................... 4
Contact ............................................................................................................................. 5
Safety Advisory................................................................................................................. 6
PRESENTATION 7
General ............................................................................................................................. 7
Applications ...................................................................................................................... 8
Characteristics.................................................................................................................. 9
Units, Range and Precision from 10°C to 40°C.................................................................. 9
Static pressure - Ps - Standard............................................................................................ 9
Total and differential pressures - Pt - ΔP - 650 kts ........................................................... 10
Rates of intrinsic leak ....................................................................................................... 10
Domain Flight Option from 10°C to 40°C........................................................................ 10
Total and differential pressures - Pt - Low speed option - 350 kts .................................... 10
Technical description ...................................................................................................... 11
Electro-pneumatic Unit.................................................................................................... 11
Front Panel.................................................................................................................. 11
Electro-pneumatic block .............................................................................................................................11
Pressure transducers ...................................................................................................................................11
Proportional Electrovalves ........................................................................................................................11
Synoptic ..............................................................................................................................................................11
Internal Battery ................................................................................................................................................. 12
Purpose...............................................................................................................................................................12
Charge Mode....................................................................................................................................................12
State of charge .................................................................................................................................................12
Remote Control Unit ....................................................................................................................................... 12
Software ............................................................................................................................................................... 13
Language ............................................................................................................................................................13
Pressure control..............................................................................................................................................13
Automatic Test programs............................................................................................................................13
Flight Domain ...................................................................................................................................................13
Self test ...............................................................................................................................................................13
USER ACCESS 14
ADSE 650 RCU front panel ............................................................................................. 14
ADSE 650 EPU front panel .............................................................................................. 15
GETTING STARTED 16
Initial Procedures ............................................................................................................ 16
ADSE 650 alternative power feeding ............................................................................... 16
Remote control link.......................................................................................................... 16
Pneumatic link ................................................................................................................. 16
Preparing for use ............................................................................................................. 16
Powering up..................................................................................................................... 16
Wi-Fi connection ............................................................................................................. 16
Interface software ........................................................................................................... 17
Shutting off...................................................................................................................... 17
OPERATOR INTERFACE 18
Starting software ............................................................................................................ 18
Connection established ................................................................................................... 19
Connection not established ............................................................................................. 19
.../...

ADSE 650 / USER MANUAL / Reference V15-D2-0174-0 / February 2023 3/79
Exhaustive Table of Content
Revision of the Manual
Contact
Safety Advisory
PRESENTATION
General
Applications
Characteristics
Units, Range and Precision
Domain Flight Option
Technical description
USER ACCESS
ADSE 650 RCU front panel
ADSE 650 EPU front panel
GETTING STARTED
Initial Procedures
OPERATOR INTERFACE
Starting software
Access to the ight domains
Measure/Manual Mode
Automatic program mode
File Manager
General Information
Help on line
Exiting the software
Keyboard conguration
Manual grounding
MAINTENANCE
Low Level Maintenance
Autotest Function
Maintenance Plan
Error and warning list
OPTIONS
1/ RCU link-serial Option
2/ EPR Option
3/ Cabin Pressure Option
4/ Outow Valve Option
SAFETY INFORMATION
EXHAUSTIVE TABLE OF CONTENT
.../...
Access to the ight domains............................................................................................ 20
Select a ight domain....................................................................................................... 20
Creating a ight domain ................................................................................................... 22
Editing, renaming and deleting a ight domain ................................................................. 23
Access to the Measure/Manual Mode............................................................................. 24
Changing the unit on th Ps and Pt channels ...................................................................... 25
Activating a channel......................................................................................................... 26
Generating on the Ps or Pt channel .................................................................................. 27
Outow indicators........................................................................................................... 28
Leak test .......................................................................................................................... 29
Return to the ground........................................................................................................ 30
Displaying the current ight domain ................................................................................ 31
Automatic program mode ............................................................................................... 32
Writing a new program .................................................................................................... 33
Editing, Renaming and deleting a program le.................................................................. 36
Executing a program ........................................................................................................ 37
Operating Mode......................................................................................................... 44
File format fo the data recorded by the semi-automatic program ............................... 45
File Manager.................................................................................................................... 46
General Information........................................................................................................ 47
Parameters ...................................................................................................................... 48
User settings............................................................................................................... 48
RS232 ......................................................................................................................... 48
Wi-Fi........................................................................................................................... 49
Ground ....................................................................................................................... 49
Reference ................................................................................................................... 50
Calibration .................................................................................................................. 50
Password ......................................................................................................................... 52
Enter a password ............................................................................................................. 54
Ground function .............................................................................................................. 55
Languages........................................................................................................................ 56
Help on line ..................................................................................................................... 57
Exiting the software........................................................................................................ 57
Keyboard conguration .................................................................................................. 58
Numerical keyboard......................................................................................................... 58
Alpha-Numeric Keyboard ................................................................................................ 58
Manual grounding ........................................................................................................... 59
MAINTENANCE 60
Low Level Maintenance................................................................................................... 60
Autotest Function ........................................................................................................... 60
Maintenance Plan............................................................................................................ 66
Error and warning list...................................................................................................... 67
OPTIONS 18
1/RCU link-serial Option................................................................................................. 69
2/EPR Option .................................................................................................................. 70
3/Cabin Pressure Option................................................................................................. 73
4/Outow Valve Option.................................................................................................. 75
SAFETY INFORMATION 77
Operating environment .................................................................................................. 77
Safety for lithium Polymer battery use ........................................................................... 77
Important instructions (for service personnel only) ....................................................... 78
Recycling ......................................................................................................................... 78

ADSE 650 / USER MANUAL / Reference V15-D2-0174-0 / February 2023 4/79
Exhaustive Table of Content
Revision of the Manual
Contact
Safety Advisory
PRESENTATION
General
Applications
Characteristics
Units, Range and Precision
Domain Flight Option
Technical description
USER ACCESS
ADSE 650 RCU front panel
ADSE 650 EPU front panel
GETTING STARTED
Initial Procedures
OPERATOR INTERFACE
Starting software
Access to the ight domains
Measure/Manual Mode
Automatic program mode
File Manager
General Information
Help on line
Exiting the software
Keyboard conguration
Manual grounding
MAINTENANCE
Low Level Maintenance
Autotest Function
Maintenance Plan
Error and warning list
OPTIONS
1/ RCU link-serial Option
2/ EPR Option
3/ Cabin Pressure Option
4/ Outow Valve Option
SAFETY INFORMATION
REVISION OF THE MANUAL
We continuously work on improving our products. This is why the information contained
in this manual, the device and the technical specications may be modied without prior
notication.
OBJECT JDATE EDITION REFERENCE
Creation
Revision
Revision
Revision
Revision
Revision
Revision
Revision
Revision
Revision
Revision
Revision
Revision
Revision
Revision
November 2014
June 2015
December 2015
February 2016
November 2016
July 2017
June 2018
October 2018
November 2018
January 2019
July 2019
February 2020
July 2020
February 2021
January 2023
01
02
03
04
05
06
06
07
08
09
10
12
13
14
15
D2-0174-A
D2-0174-B
D2-0174-C
D2-0174-D
D2-0174-E
D2-0174-F
D2-0174-G
D2-0174-H
D2-0174-I
D2- 0174-J
D2-0174-K
D2-0174-L
D2-0174-M
D2-0174-N
D2-0174-O
ATEQ Aviation Factories:
ATEQ - 15, rue des Dames, Z.I. - 78340 Les Clayes-Sous-Bois - France
Control Technology China, LTD - 98 Jian Peng Lu - Shanghai - China
Copyright © 2023 by ATEQ Inc. All rights reserved. The content of this manual may not be
reproduced in any form by any means, in part or in whole, without the prior written permis-
sion of ATEQ. Any reproduction of this document in any form whatsoever will be subject to
prosecution.
Pictures and gures in this manual are non-contractual.

ADSE 650 / USER MANUAL / Reference V15-D2-0174-0 / February 2023 5/79
Exhaustive Table of Content
Revision of the Manual
Contact
Safety Advisory
PRESENTATION
General
Applications
Characteristics
Units, Range and Precision
Domain Flight Option
Technical description
USER ACCESS
ADSE 650 RCU front panel
ADSE 650 EPU front panel
GETTING STARTED
Initial Procedures
OPERATOR INTERFACE
Starting software
Access to the ight domains
Measure/Manual Mode
Automatic program mode
File Manager
General Information
Help on line
Exiting the software
Keyboard conguration
Manual grounding
MAINTENANCE
Low Level Maintenance
Autotest Function
Maintenance Plan
Error and warning list
OPTIONS
1/ RCU link-serial Option
2/ EPR Option
3/ Cabin Pressure Option
4/ Outow Valve Option
SAFETY INFORMATION
CONTACT
With presence in 40 countries, ATEQ teams are knowledgable, professional and ready to
provide efcient service and support to customers worldwide.
A single procedure to get in touch with your ATEQ representative:
ateq-aviation.com
SUPPORT & SERVICES
Contact ATEQ Aviation Support & Services for calibration, follow-up, revision, trouble-
shooting and maintenance in real-time. Track the progress of your instrument’s service.
View quotation statuses and keep in contact with your local representative.
For urgent enquiries, please provide your phone number and wherever you are located, a
highly training technician will call you back promptly.
“You may be assured that we will do our utmost to look after your needs”.
ATEQ Team.

ADSE 650 / USER MANUAL / Reference V15-D2-0174-0 / February 2023 6/79
Exhaustive Table of Content
Revision of the Manual
Contact
Safety Advisory
PRESENTATION
General
Applications
Characteristics
Units, Range and Precision
Domain Flight Option
Technical description
USER ACCESS
ADSE 650 RCU front panel
ADSE 650 EPU front panel
GETTING STARTED
Initial Procedures
OPERATOR INTERFACE
Starting software
Access to the ight domains
Measure/Manual Mode
Automatic program mode
File Manager
General Information
Help on line
Exiting the software
Keyboard conguration
Manual grounding
MAINTENANCE
Low Level Maintenance
Autotest Function
Maintenance Plan
Error and warning list
OPTIONS
1/ RCU link-serial Option
2/ EPR Option
3/ Cabin Pressure Option
4/ Outow Valve Option
SAFETY INFORMATION
SAFETY ADVISORY
If the device is supplied with 100 / 264 VAC, it is mandatory to connect it to the ground with
a good link to the ground, to protect against electric hazard or electrocution.
It is dangerous to change the status of the Outputs.
They can control power actuators or other equipment (mechanical, pneumatic, hydraulic,
electrical or other) which can cause serious personal injury and damage to surrounding
material.
Recommendations for the test environment
Keep the test area as clean as possible.
Recommendations for operators
ATEQ recommends that the operators who use the devices have training and a level
of qualication that correspond to the job to perform.
General Recommendations
- Read the user manual before using the device.
- All electrical connections to the device must be equipped with safety systems (fuses,
circuit breakers, etc.) adapted to the needs and in accordance with the applicable stan-
dards and rules.
- To avoid electromagnetic interference, electrical connections to the device must be
shorter than 2 meters.
- Power supply plug must be grounded.
- Disconnect the device from the mains before performing any maintenance work.
- Shut off the compressed air supply when working on the pneumatic assembly.
- Do not open a connected device.
- Avoid splashing water on the device.
ATEQ is at your disposal for any information concerning the use of the device under maxi-
mum safety conditions.
We draw your attention to the fact that ATEQ cannot be held responsible for any accident
related to a misuse of the measuring instrument, the workstation or non-compliance of
the installation with safety rules.
In addition, ATEQ declines any responsibility for the calibration or the tting of its instru-
ments that is not done by ATEQ.
ATEQ also declines any responsibility for any modication (program, mechanical or elec-
trical) of the device done without its written consent.
“We are at your disposal for any information concerning the use of the device under
maximum safety conditions”.
ATEQ Team

ADSE 650 / USER MANUAL / Reference V15-D2-0174-0 / February 2023 7/79
Exhaustive Table of Content
Revision of the Manual
Contact
Safety Advisory
PRESENTATION
General
Applications
Characteristics
Units, Range and Precision
Domain Flight Option
Technical description
USER ACCESS
ADSE 650 RCU front panel
ADSE 650 EPU front panel
GETTING STARTED
Initial Procedures
OPERATOR INTERFACE
Starting software
Access to the ight domains
Measure/Manual Mode
Automatic program mode
File Manager
General Information
Help on line
Exiting the software
Keyboard conguration
Manual grounding
MAINTENANCE
Low Level Maintenance
Autotest Function
Maintenance Plan
Error and warning list
OPTIONS
1/ RCU link-serial Option
2/ EPR Option
3/ Cabin Pressure Option
4/ Outow Valve Option
SAFETY INFORMATION
PRESENTATION
GENERAL
The purpose of this manual is to provide the user with the information required to imple-
ment and operate the ADSE 650 Pitot Static Tester.
Exhibit 1: General view of ADSE 650 and Wi-Fi Touch Pad.
The ADSE 650 pressure controller is housed in a very robust housing box, able to be moved
directly to the aircraft on the tarmac or in the hangar to proceed "in situ" to test the equip-
ment tted to the aircraft.

ADSE 650 / USER MANUAL / Reference V15-D2-0174-0 / February 2023 8/79
Exhaustive Table of Content
Revision of the Manual
Contact
Safety Advisory
PRESENTATION
General
Applications
Characteristics
Units, Range and Precision
Domain Flight Option
Technical description
USER ACCESS
ADSE 650 RCU front panel
ADSE 650 EPU front panel
GETTING STARTED
Initial Procedures
OPERATOR INTERFACE
Starting software
Access to the ight domains
Measure/Manual Mode
Automatic program mode
File Manager
General Information
Help on line
Exiting the software
Keyboard conguration
Manual grounding
MAINTENANCE
Low Level Maintenance
Autotest Function
Maintenance Plan
Error and warning list
OPTIONS
1/ RCU link-serial Option
2/ EPR Option
3/ Cabin Pressure Option
4/ Outow Valve Option
SAFETY INFORMATION
The two parts of ADSE 650
- The Electro Pneumatic Unit (EPU) includes the computer, the pressure measurement
and regulation devices, the security systems as well as the pressure and vacuum pumps
necessary for independent safety operation in generation mode,
- The Remote Control Unit (RCU), located in the cover of the housing box, includes the
Human Machine Interface. It consists of a Tablet PC with Windows Pro tted with a
watertight touch sensitive plate displaying the static (Ps) and total (Pt) pressure parame-
ters (functions, measurement units, commands, rate of change, nominal values, program
number, ight limit number).
RCU and EPU are connected through the Wi-Fi. In case of problem with the Wi-Fi,
a cable can be connected between RCU and EPU.
The ergonomics of the ADSE 650 caters for:
- Excellent readability of the information,
- Easy programming of the conguration (interactive menus, with explanations and indi-
cation of potential handling errors).
APPLICATIONS
The ADSE 650 pressure generator/controller has been specially designed to simplify pres-
sure tests on equipment tted on the aircraft (altimeter, air speed indicator, rate of climb
indicator, air data computers...) in workshop, in hangar or directly on tarmac.
The computer manages the safety systems, the measurement and regulation devices
from the remote control unit with following operating functions:
1/ In "Measure" or "Manual" mode, independently or simultaneously on both static (Ps)
and total (Pt) pressure channels:
- Measurement or generation of static (Ps) pressures (altitude),
- Measurement or generation of total (Pt) pressures (air speed /MACH number),
- Chronometric measurement of leak rate.
2/ In "Program" mode, independently or simultaneously on both static (Ps) and total (Pt)
pressure channels:
- "Flight domains" writing,
- "Automatic test" programs writing,
- Execution of the written programs. In this mode, the operator can choose to enter at
each program step the actual data read on the equipment under test, or to let the pro-
gram run and to note manually the values read on the equipment under test.
3/ Security:
- Full time survey of all the ight domain limits parameters,
- Re-connection of the pressure circuits to the atmospheric pressure through manual ow
adjustable valves in case of power supply network cut-off,
- Self test of all the ADSE 650 internal functions each time the equipment gets switched on.

ADSE 650 / USER MANUAL / Reference V15-D2-0174-0 / February 2023 9/79
Exhaustive Table of Content
Revision of the Manual
Contact
Safety Advisory
PRESENTATION
General
Applications
Characteristics
Units, Range and Precision
Domain Flight Option
Technical description
USER ACCESS
ADSE 650 RCU front panel
ADSE 650 EPU front panel
GETTING STARTED
Initial Procedures
OPERATOR INTERFACE
Starting software
Access to the ight domains
Measure/Manual Mode
Automatic program mode
File Manager
General Information
Help on line
Exiting the software
Keyboard conguration
Manual grounding
MAINTENANCE
Low Level Maintenance
Autotest Function
Maintenance Plan
Error and warning list
OPTIONS
1/ RCU link-serial Option
2/ EPR Option
3/ Cabin Pressure Option
4/ Outow Valve Option
SAFETY INFORMATION
4/ Baro-setting:
The baro-setting (Ref) adjustment is performed by the operator himself and remains dis-
played permanently.
5/ Altitude difference (between the bench position and the equipment under test):
The operator can introduce in the measurement process the altitude difference between
the bench on the ground and the equipment tted in the aircraft cockpit.
CHARACTERISTICS
Power supply 90 to 264 VAC from 50 to 400 Hz
Normal operating temperature range -5°C to + 50°C (23°F to 122°F)
(Extanded Range on-demand)
Storage temperature -20°C to + 60°C (-4°F to 140°F)
(Extanded Range on-demand)
Overall dimensions
of the equipment
Length: 347 mm / 13.4 in.
Depth: 295 mm / 11.6 in.
Height: 146 mm / 5.9 in.
Outside dimensions
of the remote control unit
Width: 240 mm / 9.5 in.
Height: 142 mm / 5.6 in.
Depth: 14.5 mm / 0.6 in.
Total weight (without cables and tubes) 6 kg / 13.2 lbs
Weight of the RCU 0.6 kg / 1.3 lbs
Power consumption Less than 120 VA ~
UNITS, RANGE AND PRECISION FROM 10°C TO 40°C
Static pressure - Ps - Standard
CHANNEL UNIT RANGE PRECISION RESOLUTION
Ps hPa 72 to 1,100 hPa (1) ± 0.13 hPa 0.01 hPa
Ps InHg 2.1 to 32.5 inHg (1) ± 0.003 inHg 0.001 inHg
Altitude
Zp
ft -2,300 to 60,000 ft
± 3 ft at 0 ft
± 8 ft at 30,000 ft
± 32 ft at 60,000 ft
1 ft
m-700 to 18,000 m
± 1 m at 0 m
± 3 m at 10,000 m
± 10 m at 18,000 m
1 m
ΔZp / Δt
(VZ)
ft/min 100 to 6,000 ft/min ± 10 ft or ± 1 % (2) 5 ft/min
m/min 31 to 1,800 m/min ± 3 m or ± 1 % (2) 1 m/min
(1): Measure only (see ft unit for generation and calibration).
(2): On an integration time greater than 3 seconds, these performances are valid on a volume of 0 to 1000 cc.

ADSE 650 / USER MANUAL / Reference V15-D2-0174-0 / February 2023 10/79
Exhaustive Table of Content
Revision of the Manual
Contact
Safety Advisory
PRESENTATION
General
Applications
Characteristics
Units, Range and Precision
Domain Flight Option
Technical description
USER ACCESS
ADSE 650 RCU front panel
ADSE 650 EPU front panel
GETTING STARTED
Initial Procedures
OPERATOR INTERFACE
Starting software
Access to the ight domains
Measure/Manual Mode
Automatic program mode
File Manager
General Information
Help on line
Exiting the software
Keyboard conguration
Manual grounding
MAINTENANCE
Low Level Maintenance
Autotest Function
Maintenance Plan
Error and warning list
OPTIONS
1/ RCU link-serial Option
2/ EPR Option
3/ Cabin Pressure Option
4/ Outow Valve Option
SAFETY INFORMATION
Total and differential pressures - Pt - 650 kts
CHANNEL UNIT RANGE PRECISION RES.
ΔP DhPa 0 to 870 DhPa (1) ± 0.30 DhPa 0.01 DhPa
Airspeed
Vc
kts 0 to 650 kts ± 0.5 kt (2) at 50 kts
± 0.1 kts at 500 kts 0.1 kts
km/h 0 to 1,200 km/h ± 0.9 km/h (2) at 100 km/h
± 0.3 km/h at 900 km/h 0.1 km/h
ΔVc / Δt kts/min 40 to 300 kts/min ± 2 kts or ± 1 % (3) 1 kts/min
ΔVc / Δt km/h/min 75 to 555 km/h/min ± 3.7 km/h or ± 1 % (3) 1 km/h/min
Mach M0.1 to 3.0 M
± 0.0005 M at 0.8 M
at 25,000 ft
± 0.0003 M at 1.6 M
at 30,000 ft
0.001 M
EPR (4) -0.2 to 10 (5) < 0.005 0.001
(1): Measure only (see kts unit for generation and calibration).
(2): Accuracy after autozero function.
(3): On an integration time greater than 3 seconds, these performances are valid on a volume of 0 to 1000 cc.
(4): Optional.
(5): EPR values depend of Ps channel values.
Rates of intrinsic leak
The intrinsic leak of the ADSE 650 on the two channels is maximum 0.7 hPa/min at 500 hPa
with Ps and Pt hoses connected (test time: 15 minutes).
DOMAIN FLIGHT OPTION FROM 10°C TO 40°C
Total and differential pressures - Pt - Low speed option 350 kts
CHANNEL UNIT RANGE PRECISION RES.
ΔP DhPa 0 to 212 DhPa (1) ± 0.20 DhPa 0.01 DhPa
Airspeed
Vc
kts 0 to 350 kts ± 0.5 kt (2) at 50 kts
± 0.15 kt at 350 kts 0.1 kts
km/h 0 to 645 km/h ± 0.92 km/h (2) at 100 km/h
± 0.28 km/h at 645 km/h 0.1 km/h
ΔVc / Δt kts/min 40 to 300 kts/min ± 2 kts or ± 1 % (3) 1 Kts/min
ΔVc / Δt km/h/
min
75 to 555 km/h/min ± 3.7 km/h or ± 1 % (3) 1 km/h/min
Mach M0.1 to 2.5 M
± 0.0003 M at 0.8 M
at 25,000 ft
± 0.0002 M at 1.25 M
at 30,000 ft
0.001 M
(1): Measure only (see kts unit for generation and calibration).
(2): Accuracy after autozero function.
(3): On an integration time greater than 3 seconds, these performances are valid on a volume of 0 to 1000 cc.