Becker DVCS6100 User manual

Becker
Brand
Becker
Model
DVCS6100
Type
User manual
Becker Avionics GmbH • Baden-Airpark B108 • 77836 Rheinmünster • Germany
 +49 (0) 7229 / 305-0 • Fax +49 (0) 7229 / 305-217
http://www.becker-avionics.com • E-mail: info@becker-avionics.com
Installation and Operation
Manual DV64460.03
Issue 12 June 2019
Article-No. 0589.829-071
Remote
Electronic Unit
REU6100
Installation and Operation
Becker Avionics
2 REU6100 DV64460.03 Issue 12 June 2019
Approved Production and Maintenance Organization
Certificates see: http://www.becker-avionics.com/company-about/ →Certificates
Contact data for:
Europe, Asia,
Oceania and
Africa
Becker Avionics GmbH
Baden-Airpark B108
77836 Rheinmünster (Germany)
Tel.: + 49 (0) 7229 / 305-0
Fax: + 49 (0) 7229 / 305-217
Internet: www.becker-avionics.com
Email: info@becker-avionics.com
Customer Service:
Email: support@becker-avionics.com
Contact data for:
America,
Australia, Japan
Becker Avionics Inc
Email: info@beckerusa.com
WARNING - USER RESPONSIBILITY
FAILURE OR IMPROPER SELECTION OR IMPROPER USE OF THE PRODUCTS DESCRIBED
HEREIN OR RELATED ITEMS CAN CAUSE DEATH, PERSONAL INJURY AND PROPERTY
DAMAGE.
This document and other information from Becker Avionics provide product or system options for
further investigation by users having technical knowledge.
The user is responsible for making the final selection of the system and components. The user has to
assure that all performance, endurance, maintenance, safety requirements of the application are met
and warnings be obeyed.
For this the user has to include all aspects of the application to be compliant with the applicable
industry standards and the requirements of the responsible aviation authority. The product
documentations from Becker Avionics have to be obeyed.
To the extent that Becker Avionics provide component or system options based upon data or
specifications provided by the user, the user is responsible for determining that such data and
specifications are suitable and sufficient for all applications and reasonably foreseeable uses of the
components or systems.
Term definition: User in the sense of user, installer, installation company.
Becker Avionics
Installation and Operation
DV64460.03 Issue 12 June 2019 REU6100 3
Preface
Dear Customer,
Thank you for purchasing a Becker Avionics product. We are pleased that you have chosen our
product and we are confident that it will meet your expectations.
For development and manufacturing of our product, the guidelines for highest quality and reliability
have been borne in mind, supplemented by selection of high-quality material, responsible production
and testing in accordance to the standards.
Our competent customer support department will respond on any technical question you may have.
Please do not hesitate to contact us at any time.
Remote Electronic Unit*
Remote Control Unit REU6100
(front- rear view)
* design depends on variant.
*
Some figures in this manual are for basic understanding and can be different to the actual design.
Installation and Operation
Becker Avionics
4 REU6100 DV64460.03 Issue 12 June 2019
List of Effective Pages and Changes
Only technical relevant modifications are described in this table.
Document: DV64460.03 / issue 12 Article Number 0589.829-071
Cover Page 06/2019
Introduction 06/2019
Chapter 1 - 4 06/2019
Issue Page No.:
Section /
Chapter
Description
12
1-106 all Changed: Editorial adjustments.
-- 1.9.2 Updated: Order code, accessories.
-- 2.6.1 Updated: Table for connector P1.
--
--
--
--
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--
--
--
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© by Becker Avionics GmbH / all rights reserved
Becker Avionics
Installation and Operation
DV64460.03 Issue 12 June 2019 REU6100 5
Table of Contents
1 General Description .................................................................................................................... 13
1.1 Introduction.................................................................................................................................. 14
1.2 Purpose of Equipment ................................................................................................................. 15
1.3 Variants Overview ....................................................................................................................... 15
Software Status ................................................................................................................. 15
1.4 Associated Devices ..................................................................................................................... 15
Examples of System Block Diagram ................................................................................. 16
1.5 Scope of Functionality ................................................................................................................. 18
Audio Channel In/Outputs ................................................................................................. 18
Intercom Function ............................................................................................................. 19
Signal Tones ..................................................................................................................... 19
Discrete In/Outputs ........................................................................................................... 19
Special Features ............................................................................................................... 20
Features for Special Mission Operation ............................................................................ 21
Communication Interfaces ................................................................................................ 21
Memory Device EM6100................................................................................................... 21
1.6 Safety-Conscious Utilization ....................................................................................................... 22
1.7 Restriction for Use ....................................................................................................................... 22
1.8 Technical Data ............................................................................................................................ 23
Power Supply .................................................................................................................... 23
Monitoring ......................................................................................................................... 23
Fixed Inputs ...................................................................................................................... 23
Tone Generator ................................................................................................................. 24
Speaker Amplifier .............................................................................................................. 24
Headphone Amplifier ........................................................................................................ 24
Mike Amplifier ................................................................................................................... 25
Transceiver Modulation..................................................................................................... 25
Cockpit Voice Recorder (CVR .......................................................................................... 25
Control In/Outputs ............................................................................................................. 26
Intercom Operation ........................................................................................................... 27
Build In Test Equipment (BITE) ........................................................................................ 27
Back-up Operation ............................................................................................................ 28
Control Data Interface REU - ACU ................................................................................... 28
Control Data Interface REU - Glass Cockpit..................................................................... 28
Control Data Interface REU - REU ................................................................................... 28
Dimensions & Weight........................................................................................................ 28
Device Connectors ............................................................................................................ 29
Software ............................................................................................................................ 29
Hardware .......................................................................................................................... 29
Continued Airworthiness ................................................................................................... 29
Environmental Conditions ................................................................................................. 30
Certifications ..................................................................................................................... 31
1.9 Order Code.................................................................................................................................. 32
Remote Electronic Unit - REU6100 .................................................................................. 32
Accessories ....................................................................................................................... 32
Documentation .................................................................................................................. 33
2 Installation .................................................................................................................................... 35
2.1 Packaging, Transport, Storage ................................................................................................... 36
2.2 Device Assignment ..................................................................................................................... 37
Scope of Delivery .............................................................................................................. 37
State of Delivery ................................................................................................................ 37
Additional Required Equipment ........................................................................................ 37
Type Plate ......................................................................................................................... 38
Software/Firmware Status - Functionality ......................................................................... 38
2.3 Serial Interface Description ......................................................................................................... 38
2.4 Installation Requirements ............................................................................................................ 39
2.5 Dimensions.................................................................................................................................. 40
REU6100 .......................................................................................................................... 40
Mounting Tray MT519-1.................................................................................................... 41
REU6100 with Mounting MT519-1 and Connectors ......................................................... 42
2.6 Connector Pin Assignments ........................................................................................................ 43
Installation and Operation
Becker Avionics
6 REU6100 DV64460.03 Issue 12 June 2019
Connector P1 .................................................................................................................... 44
Connector P2 .................................................................................................................... 45
Connector P3 .................................................................................................................... 46
Connector P4 .................................................................................................................... 48
Connector P5 - not for variant -(3XX) ............................................................................... 49
Connector P5 - REU6100-X-(3XX) ................................................................................... 50
Connector J6 ..................................................................................................................... 50
Address Coding ................................................................................................................. 51
2.7 Aircraft Wiring .............................................................................................................................. 51
Electrical Bonding and Grounding..................................................................................... 51
REU6100-X-(3XX) - RS422 / RS232 / CAN Connections ................................................. 52
REU6100 - Power Supply Connections ............................................................................ 52
REU6100 - Headset Audio and PTT Connections ............................................................ 53
REU6100 - Transceiver Connections ............................................................................... 54
REU6100 - Receiver and CVR Connections .................................................................... 55
REU6100 - FIX Audio, Alert Tones and IC Ring Connections .......................................... 56
REU6100 - Speaker, Back-up Act., Control and other Connections ................................ 57
CANbus Connector ........................................................................................................... 58
Wiring - REU6100 & ACU610X ......................................................................................... 59
Wiring - REU6100 & ACU610X with Service Connector (Option) .................................... 61
Wiring - REU6100 & ACU6100 (Fixed-Wing Version) with Service Connector (Option) .. 63
Wiring - REU6100-X-(3XX) & ACU610X ........................................................................... 65
Wiring - REU6100-X-(3XX) & ACU610X & Glass Cockpit with Service Connector .......... 67
2.8 Configuration ............................................................................................................................... 69
Configuration Software (CSW6100) .................................................................................. 69
EM6100 ............................................................................................................................. 69
2.9 Communication Interfaces ........................................................................................................... 69
CANbus Protocol for REU6100 ......................................................................................... 69
RS232/RS422 Protocol for REU6100 ............................................................................... 69
2.10 REU6100 Functions .................................................................................................................... 70
Headset ............................................................................................................................. 70
PTT Key ............................................................................................................................ 70
Output Level TX-Devices .................................................................................................. 70
Input Level TX-Devices ..................................................................................................... 70
Input Level RX-Devices ..................................................................................................... 70
Sidetone ............................................................................................................................ 70
Forced Monitoring ............................................................................................................. 70
Audio Muting ..................................................................................................................... 70
FIX Input Channels (Warning Audio Tones) ..................................................................... 71
Speaker ............................................................................................................................. 71
Cockpit Voice Recorder (CVR) ......................................................................................... 71
Alert Tones ........................................................................................................................ 71
Signal Tones ..................................................................................................................... 72
Activation Signal Tones ..................................................................................................... 72
Activation - Selective Call .................................................................................................. 72
Winchman Operation ........................................................................................................ 72
Intercom Circuits ............................................................................................................... 73
IC-Indications - Cockpit Call, Cabin Call, 3
rd
-IC-Circuit ..................................................... 73
Muting Signal..................................................................................................................... 75
Marker Mute Function ....................................................................................................... 75
Back-up Mode and Slave Mode ........................................................................................ 75
2.11 Special Functions ........................................................................................................................ 76
Double Transmit and Multi Transmit (Simulcast) Mode .................................................... 76
Guard Radio PTT Function ............................................................................................... 76
Relay Mode ....................................................................................................................... 77
Operation "Headset without ACU610X" ............................................................................ 78
Operation "Headset connected to ACU" ........................................................................... 78
Operation "3rd-IC-circuit" .................................................................................................. 78
Alternative Use of Alert Tones Activation Inputs ............................................................... 79
Data Interchange in Multi-REU Applications (RS232/RS422) .......................................... 81
2.12 Service Connector ....................................................................................................................... 82
Service Connector inside the Aircraft ................................................................................ 82
Service Cable Kit ............................................................................................................... 82
Becker Avionics
Installation and Operation
DV64460.03 Issue 12 June 2019 REU6100 7
2.13 Block Diagram - DVCS6100 with Ground Crew.......................................................................... 83
2.14 Block Diagram - DVCS6100 with Intercom Amplifier .................................................................. 85
2.15 Block Diagram - DVCS6100 with Glass Cockpit Application ...................................................... 87
2.16 Block Diagram - DVCS6100 with Electronic Display Application................................................ 89
2.17 Block Diagrams - DVCS6100 with Multi-REU Application .......................................................... 91
Block Diagrams - DVCS6100 with Multi-REU Application ................................................ 91
Block Diagram - DVCS6100 with Multi-REU & Glass Cockpit Application ....................... 92
2.18 Warning and Failure Indications ................................................................................................. 92
2.19 Post Installation Check ................................................................................................................ 93
Mechanical Installation and Wiring Check ........................................................................ 93
Power Supply .................................................................................................................... 93
Power On Check ............................................................................................................... 93
3 Operation ...................................................................................................................................... 95
3.1 General ........................................................................................................................................ 95
3.2 Device Description ...................................................................................................................... 96
Device Assignment ........................................................................................................... 96
Packing, Transport, Storage ............................................................................................. 96
Scope of Delivery .............................................................................................................. 96
State of Delivery ................................................................................................................ 96
Additional Required Equipment ........................................................................................ 96
Type Plate ......................................................................................................................... 96
3.3 Operation..................................................................................................................................... 97
Operating with Becker Avionics Controller ACU610X ...................................................... 97
Operating with Glass Cockpit ........................................................................................... 97
3.4 Start-Up ....................................................................................................................................... 97
3.5 Headset ....................................................................................................................................... 97
3.6 PTT Key ...................................................................................................................................... 97
PTT Stuck Detection ......................................................................................................... 97
3.7 Audio Muting ............................................................................................................................... 97
3.8 Speaker ....................................................................................................................................... 98
3.9 Cockpit Voice Recorder (CVR) ................................................................................................... 98
3.10 Alert Tones .................................................................................................................................. 98
3.11 Signal Tones ............................................................................................................................... 98
3.12 Activation Signal Tones ............................................................................................................... 98
3.13 Activation - Selective Call ............................................................................................................ 98
3.14 Winchman Operation .................................................................................................................. 99
3.15 Intercom Circuits ......................................................................................................................... 99
3.16 IC-Indications - Cockpit Call, Cabin Call, 3
rd
-IC-Circuit ............................................................. 100
IC-Ring Line connected to the Cabin (Standard Configuration) ..................................... 100
IC-Ring Line connected to the Cockpit ........................................................................... 100
3rd-IC-Circuit for Special Mission Operation .................................................................. 101
3.17 Muting Signal ............................................................................................................................ 101
3.18 Operation "Headset without ACU610X" .................................................................................... 101
3.19 Operation "Headset connected to ACU" ................................................................................... 101
3.20 Operation "3rd-IC-Circuit" ......................................................................................................... 102
3.21 Marker Mute Function ............................................................................................................... 102
3.22 Back-up Mode and Slave Mode ................................................................................................ 102
3.23 Double Transmit and Multi Transmit (Simulcast) Mode ............................................................ 102
3.24 Guard Radio PTT Function ....................................................................................................... 102
3.25 Relay Mode ............................................................................................................................... 103
3.26 Contact Data ............................................................................................................................. 104
4 Index ........................................................................................................................................... 106
Installation and Operation
Becker Avionics
8 REU6100 DV64460.03 Issue 12 June 2019
List of Figures
Some figures in this manual are for basic understanding and can be different to the actual design.
Figure 1: REU6100 with CANbus Interface (Glass Cockpit possible) .................................................................... 16
Figure 2: REU6100-X-(3XX) with CANbus and RS232 / RS422 Interface ............................................................. 16
Figure 3: Multi-REU6100-X-(3XX) with CANbus and RS232 / RS422 Interface ..................................................... 17
Figure 4: External Memory Module - EM6100 ........................................................................................................ 21
Figure 5: Type Plate (Example) .............................................................................................................................. 38
Figure 6: Dimensions REU6100 ............................................................................................................................. 40
Figure 7: Dimensions Mounting Tray MT519-1 ...................................................................................................... 41
Figure 8: Dimensions REU6100 with Mounting MT519-1 and Connectors ............................................................ 42
Figure 9: REU6100: Connector Pin Assignment - Overview .................................................................................. 43
Figure 10: Wiring REU6100-X-(3XX) - RS422 / RS232 / CAN ................................................................................ 52
Figure 11: Wiring - Power Supply ........................................................................................................................... 52
Figure 12: Wiring - Headset Audio and PTT ........................................................................................................... 53
Figure 13: Wiring - Transceiver .............................................................................................................................. 54
Figure 14: Wiring - Receiver and CVR ................................................................................................................... 55
Figure 15: Wiring - FIX Audio, Alert Tones and IC Ring ......................................................................................... 56
Figure 16: Wiring - Speaker, Back-up Act., Control and other ................................................................................ 57
Figure 17: Wiring - REU6100 & ACU610X ............................................................................................................. 59
Figure 18: Wiring - REU6100 & ACU610X with Service Connector (Option) ......................................................... 61
Figure 19: Wiring - REU6100 & ACU6100 (Fixed-Wing Version) with Service Connector (Option) ....................... 63
Figure 20: Wiring - REU6100-X-(3XX) & ACU610X ............................................................................................... 65
Figure 21: Wiring - REU6100-X-(3XX) & ACU610X & Glass Cockpit with Service Connector ............................... 67
Figure 22: Example - Intercom Configuration ......................................................................................................... 73
Figure 23: Intercom Circuits - Standard Configuration ............................................................................................ 74
Figure 24: Intercom Circuits - IC-Ring Line connected to the Cockpit .................................................................... 74
Figure 25: Intercom Circuits - 3
rd
-IC-Circuit for Special Mission Operation ............................................................. 75
Figure 26: Relay Mode ........................................................................................................................................... 77
Figure 27: Table - Alert Tone Inputs ....................................................................................................................... 79
Figure 28: Discrete
In-/Outputs
............................................................................................................................ 80
Figure 29: Service Connector inside the Aircraft .................................................................................................... 82
Figure 30: Service Connector with Service Cable Kit SCK6100-1 ......................................................................... 82
Figure 31: Block Diagram - DVCS6100 with Ground Crew .................................................................................... 83
Figure 32: Block Diagram - DVCS6100 with Intercom Amplifier ............................................................................. 85
Figure 33: Block Diagram - DVCS6100 with Glass Cockpit Application ................................................................. 87
Figure 34: Block Diagram - DVCS6100 with Electronic Display Application........................................................... 89
Figure 35: Table - Cable Types for Multi-REU Application ..................................................................................... 91
Figure 36: Block Diagram - DVCS6100 with Multi-REU Application ....................................................................... 91
Figure 37: Block Diagram - DVCS6100 with Multi-REU & Glass Cockpit Application ............................................ 92
Figure 38: Example - Intercom Configuration ......................................................................................................... 99
Figure 39: Intercom Circuits - Standard Configuration .......................................................................................... 100
Figure 40: Intercom Circuits - IC-Ring Line connected to the Cockpit .................................................................. 100
Figure 41: Intercom Circuits - 3
rd
-IC-Circuit for Special Mission Operation ........................................................... 101
Figure 42: Relay Mode ......................................................................................................................................... 103
Becker Avionics
Installation and Operation
DV64460.03 Issue 12 June 2019 REU6100 9
List of Abbreviations
List of Abbreviations
ACU
Audio Control Unit
ATR
Air Transport Rack
CBIT
Continuous Build-In Test
CSW
Configuration Software
CVR
Cockpit Voice Recorder
EASA
European Aviation Safety Agency
FAA
Federal Aviation Administration
HS
Headset
IBIT
Initiated Build-In Test
IC
Intercom
PAX
Passenger
PBIT
Power-on Build-In Test
PTT
Push-To-Talk
REU
Remote Electronic Unit
SPKR
Speaker
TF
TufLok®, self-locking screws and threads
VOX
Voice Operated Switch
Units
Units
A
Ampere
mA
Milliampere
°C
Degree Celsius
dBm
Power Ratio In Decibel referenced to 1 mW
dB
Decibel
g
Gram
kg
Kilogram
kHz
Kilohertz
MHz
Megahertz
mm
Millimeter
Ohm (Ω)
Resistance
s
Second
V
Volt
mV
Millivolt
W
Watt
mW
Milliwatt
"
Inch
Installation and Operation
Becker Avionics
10 REU6100 DV64460.03 Issue 12 June 2019
General Safety Definitions
Indicates a hazardous situation which, if not avoided, will result in death or
serious injury.
Indicates a hazardous situation which, if not avoided, could result in death or
serious injury.
Indicates a hazardous situation which, if not avoided, could result in minor or
moderate injury.
Is used to address practices not related to physical injury.
Safety instructions (or equivalent) signs indicate specific safety-related
instructions or procedures.
Becker Avionics
Installation and Operation
DV64460.03 Issue 12 June 2019 REU6100 11
Disposal
The packaging material is inflammable, if it is disposed of improperly by
burning, toxic fumes may develop.
This product contains materials that fall under the special disposal regulation. We recommend the
disposal of such materials in accordance with the current environmental laws.
• Dispose circuit boards by a technical waste dump which is approved to take on e.g.
electrolytic aluminium capacitors. Do under no circumstances dump the circuit boards with
normal waste dump.
Warranty Conditions
The device(s) may be installed on an aircraft only by an approved aeronautical
company (e.g. Part 145) which shall also examine the installation.
Any change made by the user excludes any liability on our part (excluding the work described in this
manual).
• The device must not be opened.
• Do not make any modifications to the device, except for those described in the manual.
• Make connections to the inputs, outputs and interfaces only in the manner described in
the manual.
• Install the devices according to the instructions.
We cannot give any guarantee for other methods.
Conditions of Utilization
General introductory notes
With this device you bought a product which was manufactured and tested before delivery with the
utmost care.
Please take your time to read the notes which you ought to follow closely during installation and
operation.
Otherwise, all claims under the warranty will become void and a decreased service life or even
damages must be expected.
The user is responsible for protective covers and/or additional safety measures
in order to prevent damages to persons and electric accidents.
Additional Conditions of Utilization
Please refer to "Safety-Conscious Utilization", page 22.
Non-Warranty Clause
We checked the contents of this publication for compliance with the associated hard and software. We
can, however, not exclude discrepancies and do therefore not accept any liability for the exact
compliance. The information in this publication is regularly checked, necessary corrections will be part
of the subsequent publications.
Installation and Operation
Becker Avionics
12 REU6100 DV64460.03 Issue 12 June 2019
Blank Page
Becker Avionics
General Description
Introduction
DV64460.03 Issue 12 June 2019 REU6100 13
1 General Description
In this chapter you can read about:
1.1 Introduction.................................................................................................................................. 14
1.2 Purpose of Equipment ................................................................................................................. 15
1.3 Variants Overview ....................................................................................................................... 15
Software Status ................................................................................................................. 15
1.4 Associated Devices ..................................................................................................................... 15
Examples of System Block Diagram ................................................................................. 16
1.5 Scope of Functionality ................................................................................................................. 18
Audio Channel In/Outputs ................................................................................................. 18
Intercom Function ............................................................................................................. 19
Signal Tones ..................................................................................................................... 19
Discrete In/Outputs ........................................................................................................... 19
Special Features ............................................................................................................... 20
Features for Special Mission Operation ............................................................................ 21
Communication Interfaces ................................................................................................ 21
Memory Device EM6100................................................................................................... 21
1.6 Safety-Conscious Utilization ....................................................................................................... 22
1.7 Restriction for Use ....................................................................................................................... 22
1.8 Technical Data ............................................................................................................................ 23
Power Supply .................................................................................................................... 23
Monitoring ......................................................................................................................... 23
Fixed Inputs ...................................................................................................................... 23
Tone Generator ................................................................................................................. 24
Speaker Amplifier .............................................................................................................. 24
Headphone Amplifier ........................................................................................................ 24
Mike Amplifier ................................................................................................................... 25
Transceiver Modulation..................................................................................................... 25
Cockpit Voice Recorder (CVR) ......................................................................................... 25
Control In/Outputs ............................................................................................................. 26
Intercom Operation ........................................................................................................... 27
Build In Test Equipment (BITE) ........................................................................................ 27
Back-up Operation ............................................................................................................ 28
Control Data Interface REU - ACU ................................................................................... 28
Control Data Interface REU - Glass Cockpit..................................................................... 28
Control Data Interface REU - REU ................................................................................... 28
Dimensions & Weight........................................................................................................ 28
Device Connectors ............................................................................................................ 29
Software ............................................................................................................................ 29
Hardware .......................................................................................................................... 29
Continued Airworthiness ................................................................................................... 29
Environmental Conditions ................................................................................................. 30
Certifications ..................................................................................................................... 31
1.9 Order Code.................................................................................................................................. 32
Remote Electronic Unit - REU6100 .................................................................................. 32
Accessories ....................................................................................................................... 32
Documentation .................................................................................................................. 33
This manual describes the Becker Remote Electronic Unit REU6100. The type plate on your device
shows the part number for identification purposes (see "Type Plate", page 38).
Before starting operation of the device(s) please read this manual carefully, with particular attention to
the description referring to your device(s).
General Description
Becker Avionics
Introduction
14 REU6100 DV64460.03 Issue 12 June 2019
1.1 Introduction
The technical information in this document applies to the product REU6100 and variants of it.
The Remote Electronic Unit REU6100 is part of the Digital Voice Communication System DVCS6100
and is for installation in aircraft.
• We use also the term REU6100 for descriptions instead writing the complete model
number.
• If a description refers to only one of the product variants it is specified accordingly.
The manuals "Maintenance and Repair" (M&R) and "Installation and Operation (I&O) contain the
sections:
Section
DV64460.04
M&R
DV64460.03
I&O
General
X
X
Installation
X
X
Operation
X
X
Theory of Operation
X
N/A
Maintenance and Repair
X
N/A
Illustrated Parts List
X
N/A
Modification and Changes
X
N/A
Circuit Diagrams
X
N/A
Certifications
X
N/A
Attachments
X
N/A
Becker Avionics
General Description
Associated Devices
DV64460.03 Issue 12 June 2019 REU6100 15
1.2 Purpose of Equipment
The Remote Electronic Unit REU6100 is part of the Digital Voice Communication System DVCS6100
and it is for installation in aircraft. Together with audio control devices (ACU6100, ACU6101 or Glass
cockpit) the Remote Electronic Unit REU6100 is the intercom system of the aircraft.
• For variant REU6100-3-(XXX):
o A maximum of six audio control devices (6x ACU610X) can be connected to the
Remote Electronic Unit.
• For variant REU6100-2-(XXX):
o A maximum of four audio control devices (4x ACU610X) can be connected to the
Remote Electronic Unit.
• For variant REU6100-3-(3XX):
o A maximum of six audio control devices (2x Glass cockpit and 4x ACU610X) can
be connected to the Remote Electronic Unit.
o This variant is also applicable for Multi-REU installations.
1.3 Variants Overview
Within the part number, the meaning of "-X-(XXX) " is:
REU
6100
-
X
-
(X
X
X)
Identifier
0= Standard Config
uration Data
1=
Customized Configuration Data
Model Number
1= Standard
*
2= 4 Headset Connections
2= Extended Short Time Temp.85 °C
3= 6 Headset Connections
0= Standard (no EM6100 is used)
1= EM6100 is used
3= with RS422 Interface + EM6100
* max. number of operators per REU6100.
Software Status
Descriptions see "Software/Firmware Status - Functionality", page 38.
1.4 Associated Devices
These devices can operate together with REU6100:
Device
Function
ACU6100
Becker Avionics Audio Control Unit
ACU6101
Becker Avionics Audio Control Unit
Glass cockpit
Audio Control Device via Serial Interface
This manual describes the REU6100 with ACU610X from Becker Avionics. For other devices please
refer to the related manuals.
General Description
Becker Avionics
Associated Devices
16 REU6100 DV64460.03 Issue 12 June 2019
Examples of System Block Diagram
Figure 1: REU6100 with CANbus Interface (Glass Cockpit possible)
Figure 2: REU6100-X-(3XX) with CANbus and RS232 / RS422 Interface
Becker Avionics
General Description
Associated Devices
DV64460.03 Issue 12 June 2019 REU6100 17
Figure 3: Multi-REU6100-X-(3XX) with CANbus and RS232 / RS422 Interface
• You can also use ACU6101 as control devices.
• A REU6100-X-(3XX) is not interchangeable with other REU6100 variants.
• The variant REU6100-X-(3XX) has a different pin assignment on
connector P5 (see table 2.6.5 and 2.6.6).
ACU6100
ACU610
0
ACU6100 ACU6100 ACU6100 ACU6100
Audio Control Units
CANbus
CANbus
REU6100-X-(
3XX)
ACU
6100 AC
U610
0 ACU
6100
ACU610
0 ACU
610
0 ACU61
00
Audio Control Units
CANbus
CANbus
REU6100-X-(3XX)
RS232 / RS422
General Description
Becker Avionics
Scope of Functionality
18 REU6100 DV64460.03 Issue 12 June 2019
1.5 Scope of Functionality
The REU6100 is for installation in the avionics compartment of an aircraft.
• It is a device in a standard ATR ¼ short case.
• The device connectors are on the front and back side of the REU6100.
o The connectors are coded to prevent misconnection.
• The REU6100 receives the commands from the audio control devices and accordingly
influences and processes all incoming and outgoing audio signals.
• The REU6100 supplies the logical functions necessary to operate the transceivers and for
aircraft intercommunication.
• The REU6100 supplies up to 10 different tone signals.
o The tone signals can be managed through discrete control lines.
• The audio processing circuits are in a modular design.
o Each external control device (e.g. ACU610X) is connected to an individual
processing module inside the REU6100.
o From electrical and mechanical points of view the modules are identical for easy
upgrade and interchange work.
Audio Channel In/Outputs
• The device has 22 balanced audio inputs, as follows:
o 8 transceivers or 7 transceivers and PA amplifier.
o 8 receivers.
o 6 fixed inputs.
• The input sensitivity for each transceiver and receiver is in the range of 2.5…20 V. The
input sensitivity is programmable with the configuration software.
• The input sensitivity for the fixed input 1…3 is in the range of 5…40 V. The input
sensitivity is programmable with the configuration software.
• The input sensitivity for the fixed input 4…6 is in the range of 2.5…20 V and under main-
volume control. The input sensitivity is programmable with the configuration software.
• Control of monitoring volume of the TX and RX channels connected in the range of
0...-48 dB.
• Main volume control by 0…-48 dB for headphone and, if enabled, for speaker amplifier.
• Supply of mike audio to 100…250 mV into 150 Ω (standard carbon mike) or 0.5…4 mV
into 20 Ω (dynamic mike):
o Automatic Gain Control (AGC).
o Providing the standard mike supply.
• Supply of a balanced audio output of 0.07…1.5 V into 150 Ω and distribution to 8 TX
modulation lines (configurable).
• Distribution of the PTT to 8 key lines. Keying logic to ensure transmission priority over
IC operation and to mute speaker outputs as well as non-desired RX and fixed inputs
during transmission.
• Supply of forced monitoring for all TX-channels with mike line selection.
• PTT priority for each operator (configurable high / low).
• PTT stuck detection.
• Generation of an artificial sidetone from the mike signal for radio transceivers which do not
feature a built-in sidetone during transmission (e.g. FM radios).
o Natural sidetone.
o Duplex sidetone.
o The sidetone can be individually programmed for every of the 8 transceivers by
configuration software from system integrator.
• Muting of receiver audio during transmission.
• Phone amplification of summed audio signal to 250 mW into 300 Ω or 500 mW into 8 Ω.
Becker Avionics
General Description
Scope of Functionality
DV64460.03 Issue 12 June 2019 REU6100 19
Intercom Function
• Supply of mike audio for intercom operation:
o Interconnection and separation of 3 IC circuits.
o Intercommunication VOX control.
o HOT MIKE activation.
o Addition of an incoming IC audio signal to the summed-up monitor audio;
adjustment of the IC audio via the ACU panel control by 0…-48 dB.
o Enhancing to IC-ring line level 0.775 V into 600 Ω.
o Extension of intercommunication by the IC-ring line audio in/out for external
devices like EB3100 (Ground Crew) or IC3100 (Intercom Amplifier).
o IC-ring line can be connected to the cockpit or cabin intercom circuit.
Signal Tones
• The REU6100 supplies up to 10 different tone signals in the frequency spectrum of
800…4800 Hz.
o 1x signal "Intercom request" (1600 Hz / 1200 Hz intermitted).
o 1x signal "E-call" (2400 Hz / 800 Hz / 1200 Hz intermitted).
o 8x alert signals (1x continuous, 3x pulsed, 4x intermittent) in the frequency
spectrum of 1200…4800 Hz.
• The signal tones are connected through 8 discrete control lines (active LO ≤ 1 V).
• It is possible to give different states to the signal tones:
o Muted during transmission.
o Set at the priority level (high, low, medium).
o Set at cancellation possibility.
Discrete In/Outputs
• 4 control outputs for specific logical external activations (all active low).
o DF-blanking (when a PTT is pushed).
o Cockpit call activation (if call is on).
o Cabin call activation (if cabin is isolated).
o Third intercom circuit status.
• 6 control inputs for specific logical DVCS-action (all active low).
o Winchman VOX-level selection.
o Winchman volume-level selection.
o Intercom request call input.
o E-call activation.
o Selective call activation.
o Warning tone cancellation.
General Description
Becker Avionics
Scope of Functionality
20 REU6100 DV64460.03 Issue 12 June 2019
Special Features
• The winchman connection facility in parallel to the related headset (ACU610X).
o Individual VOX level and volume level adjustment is possible through discrete
control lines.
• Turn on and off the speaker amplifiers and supply of an output of 12 W into 4 Ω.
• Muting of the cockpit speakers during transmission and intercom operation to avoid
acoustic feedback (configurable).
• By a "VOICE-filter", an incoming 1020 Hz tone can be attenuated at least 26 dB for
listening to the NAV voice modulation without disturbance. The filter function can be
connected to each of the eight receiver channels during factory or system integration
setup.
• Detection of a selective call signal by a discrete input from one of the 8 com radios
(configurable).
o Supply of a visual indication on the audio control device.
• Forced monitoring of the audio signal (configurable).
1.5.5.1 Built-in Tests
• The REU6100 device has different built-in tests.
• The tests monitor the system equipment and some internal circuits.
o PBIT: A system self-test starts after power-on.
o CBIT: A background test routine runs continuously during normal operation.
o IBIT: An additional test can be manually started.
1.5.5.2 Marker Mute Function
• If set by the operator the marker channel is muted for 30 seconds.
• The marker mute function can be individual enabled for each receiver channel and
operator in the configuration setup.
1.5.5.3 Emergency Operation (Back-Up Operation)
• Relay controlled fall back in case of emergency operation (back-up): Assignment of radios
and receivers to their operators.
o Headset 1 (normally the pilot) is connected to TX1 and FIX1,
o Headset 2 (copilot) to TX2 and FIX2.
• Back-up operation is started either manually through the hard-wired BACK-UP switches
on the ACU610Xs (if connected), or automatically upon power supply failure to the
REU6100, or if the internal power supply of the REU6100 itself is defective (this function
with pilot’s and copilot’s audio control devices only).
1.5.5.4 Slave Operation
• Relay controlled activation of slave operation to connect one operator headset in parallel
to others (this function with pilot’s and copilot’s audio control devices only).
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Becker DVCS6100 User manual

Becker
Brand
Becker
Model
DVCS6100
Type
User manual
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