UNIVERSAL AVIONICS UL-801 Airborne datalink Installation Manual
Below you will find brief information for Airborne datalink UL-801. The UL-801 Airborne Datalink provides an air-to-ground two-way digital datalink that meets the need for specific air-to-ground communications. UniLink communicates with multiple ground-based Datalink Service Providers (DSP) using a VHF radio and/or SatCom telephony-based system. The UL-801 contains an internal VHF Data Radio (VDR) and supports connections with up to three FMSs and one remote CDU, and connections to a VDR; and peripheral devices, such as UASC multifunction displays (MFDs) (including the MFD-640 and Electronic Flight Instrument-890R (EFI-890R) displays) and a printer. UniLink capabilities include: Future Air Navigation System (FANS), Controller-Pilot Datalink Communications (CPDLC) messaging, Automatic Dependent Surveillance - Contract (ADS-C), CVR/CVFDR Output for datalink recording, OOOI (Out-Off-On-In) reporting, Automatic position reporting, Fight planning route uplinks, Aircraft triggered events, Clearances/Requests, Textual and graphical color weather maps or depictions in both low and high resolution formats, Digital Automatic Terminal Information System (D-ATIS, which is sometimes referred to as ATIS), Terminal Weather Information for Pilots (TWIP), Free Text messaging, Special Status reports (for example, delays, ETA updates, and diversions).
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UL-801
Installation Manual
The information contained herein is subject to the Export Administration Regulation
(“EAR”), 15 C.F.R. Parts 730-774. Diversion contrary to U.S. law is prohibited.
This publication is available at www.uasc.com.
© 2011 UNIVERSAL AVIONICS SYSTEMS CORPORATION
ALL RIGHTS RESERVED
3260 East Universal Way
Tucson, AZ 85756-5097
(520) 295-2300 • (800) 321-5253
23-20-06
15 December 2011
UL-801 Installation Manual
Record of Revisions
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Initials
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Title Page
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Table of Contents
Introduction
Description and
Operation
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Appendix 2
Appendix 3
Appendix 1
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UL-801 Installation Manual
Table of Contents
Record of Revisions ............................................................................................................. 1
Record of Temporary Revisions ........................................................................................... 1
List of Effective Pages .......................................................................................................... 1
Table of Contents ................................................................................................................. 1
Introduction ........................................................................................................................... 1
1. Makeup and Use of This Manual ............................................................................... 1
A. Application ......................................................................................................... 1
B. Organization ...................................................................................................... 1 and Terminology ................................................................................. 1
Description and Operation .................................................................................................... 1
1. Description ................................................................................................................. 1
A. General ............................................................................................................... 2
B. Future Air Navigation System (FANS 1/A+) ........................................................ 3
E. UniLink Customer, ATC, and Geographic Databases ........................................ 5
F. UASC
429
Serial Ports .................................................................................. 18
K. Ethernet ........................................................................................................... 22
Media Management ................................................................... 22
O. SatCom-based
P. ACARS
Q. Advisory Alerts, Device Status, and Error Messages ....................................... 29
R. COCKPIT Voice Recorder (CVR) .................................................................... 29
S. Printers ............................................................................................................ 30
T. Transmission Media Interfaces – Configuration Option ................................... 31
Message
V. Media
Leg
Data Reproting Option ............................................................. 32
AA. ARINC 741 using Iridium or Inmarsat .............................................................. 32
2. Operation ................................................................................................................. 32
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UL-801 Installation Manual
FAA Approval .................................................................................................................... 101
A. Applicable TSOs .............................................................................................. 101
Deviations ................................................................................................ 101
C. Equipment Classes .......................................................................................... 102
D. Reference Documents ..................................................................................... 102
2. Software Criticality .................................................................................................. 105
3. Instructions for Continued Airworthiness ................................................................ 106
B. Compliance ...................................................................................................... 107
4. Environmental Qualification Forms ......................................................................... 108
5. Sample Airplane Flight Manual Supplement ........................................................... 112
Equipment Specifications .................................................................................................. 201
1. UniLink Equipment Specifications .......................................................................... 201
A. UniLink Part Number Matrix ............................................................................. 201
Installation Kit ...................................................................................... 202
C. Power Specifications ........................................................................................ 202
D. Equipment Weights .......................................................................................... 202
E. VHF Antenna Specifications ............................................................................ 202
G. Equipment Drawings ........................................................................................ 204
H. Signal Specifications ........................................................................................ 207
I. HS-429-1 Bus – UniLink ................................................................................... 211
J. Configurable LRUs ........................................................................................... 212
Installation and Wiring ....................................................................................................... 301
1. Installation Considerations for UniLink Mounting .................................................... 301
Mounting ............................................................................................. 301
2. Wiring Diagrams ..................................................................................................... 301
A. UL-801 without FANS to UNS-1C .................................................................... 302
B. UL-801 without FANS to UNS-1C+ .................................................................. 304
C. UL-801 without FANS to UNS-1E .................................................................... 306
D. UL-801 without FANS to UNS-1Csp ................................................................ 308
E. UL-801 without FANS to UNS-1Esp................................................................. 310
F. UL-801 without FANS to UNS-1D .................................................................... 312
G. UL-801 without FANS to UNS-1D+ .................................................................. 314
H. UL-801 without FANS to UNS-1F .................................................................... 316
I. UL-801 without FANS to UNS-1K .................................................................... 318
J. UL-801 without FANS to UNS-1K+ .................................................................. 320
K. UL-801 without FANS to UNS-1L ..................................................................... 322
L. UL-801 without FANS to UNS-1Ew .................................................................. 323
M. UL-801 without FANS to UNS-1Espw .............................................................. 325
N. UL-801 without FANS to UNS-1Lw .................................................................. 327
O. UL-801 without FANS to UNS-1Fw .................................................................. 329
P. UL-801 FANS Discretes (WAAS FMS SCN 1000.5/1100.5 or later) ................ 331
Q. UL-801 to EFI-890R – High Resolution ............................................................ 332
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UL-801 Installation Manual
R. UL-801 to MFD-640 – High Resolution (MFD SCN 1011.4.8 or later) ............. 333
S. UL-801 to Remote CDU (RCDU) - Low Resolution ......................................... 334
T. UL-801 to MFD-640 – Low Resolution (MFD SCN 1011.4.7 or earlier) ........... 335
U. UL-801 to CVR/CVFDR ................................................................................... 336
W. UL-801 to SSDTU ........................................................................................... 337
X. UL-801 to Portable DTU-100 ........................................................................... 338
Y. UL-801 to Portable SSDTU ............................................................................. 338
Z. UL-801 to Airborne-based Telephony SatCom Systems ............................... 339
AA. UL-801 to ARINC740/744/744A Printer ......................................................... 341
BB. UL-801 to PC Printer ..................................................................................... 342
CC. UL-801 to Generic Parallel Printer ................................................................. 342
3. UL-801 Connector Pin Identification ...................................................................... 343
Plug .......................................................................................................... 343
C. Bottom Plug ..................................................................................................... 346
4. UL-801 Connectors ................................................................................................ 347
System Data Installation ................................................................................................... 401
1. International Civil Aviation Organization (ICAO) Aircraft Type Designators ........... 401
2. Configuration Worksheets ..................................................................................... 405
A. Customer/Aircraft Information.......................................................................... 406
B. System
C. SYS CONFIG 2/4 ............................................................................................ 424
D. SYS CONFIG 3/4 ............................................................................................ 426
3. Configuration Procedures ...................................................................................... 428
B. FANS Block Data Transmission ...................................................................... 431
C. Storing UniLink Options ................................................................................... 432
D. Configuration Edit Mode .................................................................................. 433
F. Clearances ...................................................................................................... 436
G. Alerts ............................................................................................................... 437
H. System Configuration 3/4 ................................................................................ 438
Configuration ............................................................................................. 439
Configuration ........................................................................................... 446
Configuration ....................................................................................... 448
M. Telephony (TEL) Configuration ....................................................................... 449
N. Position Report Configuration.......................................................................... 450
O. Configuration Review ...................................................................................... 451
Maintenance, Checkout, and Troubleshooting ................................................................. 501
1. UniLink Ground Checkout Procedures .................................................................. 501
Installation Test ....................................................................................... 501
B. Return to Service ............................................................................................. 501
C. UniLink to FMS/MCDU Communications ........................................................ 501
D. Version Check ................................................................................................. 502
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UL-801 Installation Manual
F. UniLink to Display Processor RS-422 Communications................................... 502
G. UL-801 VHF Communications ......................................................................... 503
H. OOOI Sensor Test ........................................................................................... 503
J. Checking the UL-801 FANS ALERTS Output Discretes .................................. 504
K. Checking the UL-801 Self-Test (Optional) ....................................................... 504
L. Checking the UL-801 Weather Graphics using a SatCom-based
Telephony System ........................................................................................... 504
M. Checking the UL-801 ARINC 741 SatCom (SAT) ............................................ 505
2. Error Messages ...................................................................................................... 506
A. Pop-up Window Error Messages ..................................................................... 506
Error Messages .................................................................................. 507
C. Configuration Error Messages ......................................................................... 512
D. Hidden Error/Status Messages ........................................................................ 519
Appendix 1 ...................................................................................................................... A1-1
1. Acronyms, Abbreviations, and Terms ................................................................... A1-1
Appendix 2 ...................................................................................................................... A2-1
1. UniLink Menus and Submenus – without FANS ................................................... A2-1
A. UniLink Menu 1/2 ........................................................................................... A2-1
B. UniLink Menu 2/2 ........................................................................................... A2-3
C. Maintenance Menu ........................................................................................ A2-4
D. Configuration Menu ........................................................................................ A2-5
2. UniLink Menus and Submenus – with FANS ........................................................ A2-6
A. UniLink Menu 1/2 ........................................................................................... A2-6
B. Maintenance Menu ...................................................................................... A2-10
C. Ops Menu .................................................................................................... A2-12
Appendix 3 ...................................................................................................................... A3-1
1. Datalink Service Providers ................................................................................... A3-1
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UL-801 Installation Manual
Introduction
1. Makeup and Use of This Manual
A. Application
This manual provides installation information pertaining to the UL-801.
B. Organization
This manual provides information about:
•
Description of the components of the UL-801
•
Environmental qualification forms
•
UniLink equipment specifications
•
Installation and wiring requirements
•
Worksheets and procedures for installing system data including configuring the UL-801
Configuration Module
2. Abbreviations and Terminology
This manual contains no abbreviations or terms that have varying interpretations throughout the industry. Refer to Appendix 1 for a list of acronyms, abbreviations, and terms that are used throughout this manual.
The front panel of the Control Display Unit/Multi-function Control Display Unit
(CDU/MCDU), part of the FMS, contains an array of push buttons or keys that are used by the crew to operate the system. Instructions in this manual refer to specific keys by name. We bracket the legend on the key in the text. Examples: [ENTER], [A]. Line Select Keys (LSK) are referred to by numerical order (top to bottom) and side. Text appearing on the display may be included. Example: RETURN [5R].
Please submit comments, suggestions, errors or other concerns about this manual to our
Technical Publications Department at [email protected].
To order copies or request changes in address and distribution information, contact [email protected].
For technical questions, please contact [email protected]
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UL-801 Installation Manual
Description and Operation
1. Description
The UL-801 Airborne Datalink provides an air-to-ground two-way digital datalink that meets the need for specific air-to-ground communications. UniLink communicates with multiple ground-based Datalink Service Providers (DSP) using a VHF radio and/or SatCom telephony-based system. The UL-801 contains an internal VHF Data Radio (VDR).
NOTE: Both DSP and DLSP are used as acronyms for Datalink Service Providers.
The Datalink system consists minimally of an FMS, a CDU/MCDU, the UL-801, a transmission medium, such as a VDR or SatCom, and a configuration module. The UL-801 supports connections with up to three FMSs and one remote CDU, and connections to a
VDR; and peripheral devices, such as UASC multifunction displays (MFDs) (including the
MFD-640 and Electronic Flight Instrument-890R (EFI-890R) displays) and a printer.
This Installation Manual applies to both FANS-enabled and non-FANS-enabled UniLink systems unless otherwise noted.
UniLink capabilities include:
•
Future Air Navigation System (FANS)
•
Controller-Pilot Datalink Communications (CPDLC) messaging
•
Automatic Dependent Surveillance - Contract (ADS-C)
•
CVR/CVFDR Output for datalink recording
•
OOOI (Out-Off-On-In) reporting
•
Automatic position reporting
•
Fight planning route uplinks
•
Aircraft triggered events
•
Clearances/Requests
−
Pre-departure
−
Oceanic
−
Pushback
−
Expected Taxi
•
Textual and graphical color weather maps or depictions in both low and high resolution formats
•
Digital Automatic Terminal Information System (D-ATIS, which is sometimes referred to as ATIS)
•
Terminal Weather Information for Pilots (TWIP)
•
Free Text messaging
•
Special Status reports (for example, delays, ETA updates, and diversions).
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The communication links used to exchange data are Very High Frequency (VHF), including:
•
The legacy Aircraft Communications Addressing and Reporting system (ACARS)
•
Next-generation VHF digital link (VDL) Mode 2
•
Satellite Communications (SatCom).
The UL-801 is designed to be interfaced with, and controlled through, a variety of Universal
Avionics Control Display Units (CDUs) or Multi-function Control Display Units (MCDUs) that are integrated with a Universal Avionics Flight Management System (FMS). The
UL-801 can also be controlled via an MCDU with ARINC 702 FMS or 743/743A GNSS.
Uplink text messages are displayed on Universal’s CDU/MCDUs. Color graphical weather maps may be displayed on Universal’s CDUs, MCDUs, Multi-Function Displays (MFD), and Flat Panel Integrated Display (FPID), as well as UASC’s EFI-890Rs.
High resolution graphics ports support up to two high-resolution display devices, such as a capable EFI-890R ND and/or an MFD-640.
UniLink is capable of simultaneously transmitting and or receiving messages on more than one transmission link at a time (VHF and SatCom, which includes SAT and TEL). Messages may be generated on the ground and sent to the aircraft (uplink message) or messages can be generated from the aircraft and sent to the ground (downlink message). Downlink messages are generated by the crew, internally by the UniLink, or any one of the peripheral units may generate a message to be passed on to the UniLink for transmission. When UniLink receives an uplink message, it determines if the message should be processed internally or be sent to a peripheral device specified by a message sub-label. Messages can be predefined as ARINC
Aircraft Communications Addressing and Reporting System (ACARS) messages or UniLink supported messages, such as specialized weather requests or graphical weather maps, or text messages routed to a printer.
The communications link connects the UniLink-equipped aircraft directly to a DSP. This provides a general purpose communications link between the aircraft and ground computers utilizing such first party service providers such as ARINC, SITA, and/or AVICOM. It is the user’s decision which DSP is selected. The decision may also be based on the second-party
DSP to which the user subscribes.
In order to aid in potential incident/accident investigations, UniLink supports the transmission of datalink records to an ARINC Characteristic 757 Cockpit Voice Recorder
(CVR) and a Cockpit Voice Flight Data Recorder (CVFDR).
A. General
The UL-801 provides two-way datalink for air-to-ground communications which allows communication with a DSP for a variety of available services. In order for UniLink to be utilized, a DSP subscription is required. Each DSP may not support all UniLink services.
Contact your DSP for a list of supported services. A list of available UniLink DSPs can be found in Appendix 3.
UniLink communicates via one or more communication systems: VHF and/or Satellite
SatCom systems. It supports an RS-232 serial or ARINC 429 (740, 744/744A) cockpit printer to print various uplink messages, such as a textual weather report. The UniLink also connects to a DTU/SSDTU to allow future software and database updates.
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SatCom weather graphic uplinks via circuit mode data and text weather uplinks via Short
Burst Data (SBD) or packet data mode may or may not be available, based on your selected
DSP and the SatCom equipment installed. In addition, some functions/features may only be available through specific communications systems as described in the following table.
Supported Applications
1
Communication System
2
AOC Text, and
Text, Weather, and
D-ATIS
ACARS Air
Traffic Services excluding FANS
Flight
Information
Services (FIS)
3
ATC FANS
1/A+
Weather
Graphics
4
VHF (VDL Mode 2 and POA)
SatCom (UASC Aero-I)
Yes
Yes
Yes
Yes
Yes
Yes
Yes
No
No
No
SatCom (UASC Aero-M) Yes No No No
Iridium SatCom ARINC 741 Yes Yes Yes Yes
4
Yes
No
Iridium SatCom RS-232
Inmarsat SatCom ARINC 741
Inmarsat SatCom RS-232
Yes
Yes
Yes
No
Yes
No
No
Yes
No
No
Yes
4
Yes
No
No Yes
1. Check with the DSP for applicable supported applications.
2. Communication Systems must meet DO-178B Level D to be used for FANS applications.
3. The following Flight Information Services are available thru the internal VHF radio or a capable and approved Packet Mode Data or Short Burst Data SatCom system. Contact your DSP and SatCom manufacturer for more information.
• Pre-departure
• Oceanic
• D-ATIS
• TWIP
• Pushback
• Expected taxi clearance
4. Check with the Iridium or Inmarsat SatCom manufacturer for current FANS approvals.
5. Graphical weather information is available only when the UniLink is interfaced to a circuit mode data
SatCom system via the RS-232 connection and supported by the DSP. The older tip and ring circuit mode data interface that was available on all previous UniLink models, UL-60X and UL-70X, has been removed.
B. Future Air Navigation System (FANS 1/A+)
UniLink system functionality is greatly enhanced by a Future Air Navigation System
(FANS) 1/A+ implementation, which is intended to improve safety of flight, enhance efficiency, and increase air traffic capacity by replacing voice transmissions between crews and ATC with datalink messages during flight in oceanic and remote areas that have no or limited radar coverage. Voice transmissions will continue to be used as a reversionary means of communication. UniLink provides a FANS-1/A+ implementation as defined in
RTCA/DO-258A and A622. FANS-1/A+ features include AFN, ADS, and CPDLC text data transmissions.
At least one UASC FMS must be installed and operating with SCN 1000.5/1100.5 or later for the UniLink FANS-1/A+ implementation. The FMS must be configured to enable FANS data transmission and must be configured to transmit to UniLink over the UNS HS-429-1 bus.
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FANS-1 is the original version of FANS developed by Boeing and FANS-A is the corresponding version developed by Airbus. Both of these versions are interoperable with worldwide ATC facilities and use the Aircraft Communications Addressing and Reporting
System (ACARS) network. UniLink’s FANS-1/A+ implementation is designated as such because it is functionally equivalent to, and combines many of the best features of both
Boeing’s FANS-1 and Airbus’ FANS-A implementations.
Future Air Navigation System (FANS) is principally comprised of three applications:
•
Air Traffic Services ATS Facilities Notification (AFN)
AFN allows the aircraft and an ATS provider on the ground to exchange addresses, as well as information about which FANS applications they support.
•
Automatic Dependent Surveillance-Contract (ADS-C)
ADS-C allows multiple ATS providers to command position reports and other situational data at regular intervals or in response to events specified by the ATS provider, such as a change in altitude or lateral deviation. ADS-C requires no crew interaction.
•
Controller-Pilot Datalink Communications (CPDLC)
CPDLC provides capabilities to substitute for traditional voice communications for routine communications between a pilot and an air traffic controller. CPDLC messages can be used to request and grant clearances, to inform the ground of the aircraft’s position and situation, and to provide instructions to the crew, such as “Climb To Reach FL390
By 2200” or “Proceed Direct To TUNTO”.
C. Field-Loadable Software and Databases
The UniLink application software, Customer, ATC, and Geographic databases are loadable in the field or at an authorized Universal Avionics dealer. During the software loading process, automatic and manual version number verification procedures are performed to ensure the compatibility of the software and database. A separate manual, 23-20-08, provides the Field Loading procedures.
Detection of Corrupted or Partially Loaded Software
All loadable software and databases contain a 32-bit Cyclic Redundancy Check (CRC). The data-loading software function calculates a CRC upon receipt of a file and compares it to the
CRC included with the loaded data file thus rejecting any files whose contents have changed during the loading process.
Determination of the Effects of Loading the Inappropriate Software
The system has been designed to guard against inappropriate software or database loading based on version numbering. Loadable application software only functions with versions of the hardware and boot software that supports the version type of software loaded. If an incompatibility is detected during power-up checks, the system is placed into a state in which no normal functions can occur. Only appropriate loadable databases and applications will function with compatible versions of the main application software.
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Hardware/Software Compatibility
The hardware versions are made available to the application software and are verified for compatibility during power-up checks and during application software loading.
Restricted Access to the Field-Loading Function
The field-loading function is only enabled when the aircraft is on the ground and after a password has been entered successfully.
UniLink Databases
The UniLink databases, consist of multiple database components including the Aeronautical
Operational Control (AOC) and Air Traffic Control (ATC) databases (required for FANS operations) components, contains the definitions of nearly all user-interface screens, nearly all uplink and downlink messages, a flight database that defines how data is formatted and stored, and event triggers used for responses to system events. Database integrity is verified by means of a 32-bit CRC at loading and during UniLink initialization.
D. Field-Loadable Software Interface
UniLink provides an interface to load the following databases and application software via the UASC Data Transfer Unit (DTU-100) or UASC Solid State Data Transfer Unit
(SSDTU). Access to the software and database loading functions are password protected and the aircraft must be on the ground. The UASC DTU physical interface is 10BaseT Ethernet.
The UniLink hardware contains a 10/100BaseT Ethernet port.
•
Datalink application software
•
VDR application software
•
Customer database, which includes the AOC database
•
ATC database
•
Geographic database
UniLink provides user-interface screens that allow the user to command and monitor the loading progression.
E. UniLink Customer, ATC, and Geographic Databases
The Field Loadable Software database system provides flexibility in response to the changing communications, navigation, and surveillance/air traffic management environment for current and future regulations. The Customer Database (CDB)-driven user interface and message set can be customized by UASC to match airline or business operator’s requirements. Each database is described below.
All UniLink systems include three databases: the Customer Database, the Air Traffic Control
(ATC) Database, and the Geographic Database, and contains the definitions of the following:
•
User interface screens
•
Line Select Key functions
•
Message definitions for uplink and downlink messages
•
A flight database, which defines how data is formatted and stored
•
Event triggers used for OOOI event reporting and other responses to system events
Page 5 23-20-06
UL-801 Installation Manual
The Customer Database (CDB)-driven user interface and message set can be customized to match airline or business operator’s operational requirements. Each database is described below.
•
Customer Database
Contains screen and message definitions for Aeronautical Operational Communications
(AOC) and Air Traffic Services (ATS) applications. Contains user definitions for uplink and downlink messaging, and a flight database that defines how data is formatted and stored, and event triggers used for responses to system events.
A 32-bit CRC is employed to confirm database integrity at loading, initialization, and during flight. The customer database also has a version number that is checked upon loading for compatibility with the application software. If the customer database CRC check fails, UniLink annunciates the error and provides a screen for reloading the customer database.
NOTE: The loading of the customer database erases the ATC database from UniLink memory. Following a load of the customer database, the ATC database must be reloaded.
•
Air Traffic Control (ATC) Database
Contains screen and message definitions for ATC applications, including the Future Air
Navigation Systems (FANS).
The system provides flexibility in response to the changing communications, navigation, and surveillance/air traffic management environment for current and future regulations.
This database is used to define the UniLink ATC screens and message sets and is very similar in function and purpose as the customer database.
A 32-bit CRC is employed to confirm database integrity at loading, initialization, and during flight. The ATC database also has a version number that is checked upon loading for compatibility with the application software and the customer database. If the ATC database CRC check fails, UniLink annunciates the error and allows the user to continue to access the functions defined by the customer database.
NOTE: Loading the ATC database does not affect the currently loaded customer database or Geographic database.
•
Geographic Database
Contains aircraft communications addressing and reporting system (ACARS) ground station locations and corresponding ACARS VHF frequency information.
The geographic database has a 32-bit CRC that is verified upon database loading. It also has a version number that determines its compatibility with the application software. If the geographic database CRC check fails, UniLink annunciates the error and prevents the user from operating UniLink with a corrupted database.
NOTE: The Customer, ATC, and Geographic databases can be installed by UASC and can also be field-loaded using a UASC DTU-100 or SSDTU. It is recommended that this connection be installed as updates to these databases may be required from time to time.
Page 6 23-20-06
F. UASC FMS Interface
UL-801 Installation Manual
The UniLink provides concurrent user interface access for up to three UASC Flight
Management Systems. The ARINC 429 interface uses the ARINC 739 protocol for display control and ARINC 619 bit oriented file transfer protocol for file exchange between the devices. Each UASC FMS provides a high-speed ARINC 429 channel as inputs to UniLink.
The specific channel will be specified by the configuration module, based on aircraft wiring.
Any of the general purpose ARINC 429 output buses can be configured as output bus to the
FMS. However, ARINC TX port #1 is hard set to low speed and is required by the number 1
FMS. UniLink provides an RS-422 proprietary graphics display bus interface between the unit and each UASC CDU for low resolution graphics.
Page 7 23-20-06
UL-801 Installation Manual
(1) UniLink interface capabilities
SATCOM-BASED
AIRBORNE
TELEPHONY
VHF ANTENNA
RS-232
A741
AIRBORNE
TELEPHONE SYSTEMS
IRIDIUM / INMARSAT SATCOM
A741
/
A739 MCDU A739 MCDU A739 MCDU
14 DISCRETE
OUTPUT DEVICES
/
UNILINK
UL-801
ARINC
A429
A429
UNIVERSAL AVIONICS
FLIGHT MANAGEMENT
SYSTEMS
CONFIGURATION
MODULE
ETHERNET
SUPPORTS
UP TO 3
UASC FMSs
OR
ARINC 702A
FMC
STANDARD
SOLID STATE DATA
TRANSFER UNIT (SSDTU)
*
RS-422
GRAPHIC SUPPORT FOR UP TO 4 DISPLAYS
A740/744/744A
PRINTER
A429
SERIAL PRINTER
RS-232
A604 CMC
A429
RS-422
GRAPHIC
SUPPORT
FOR TWO
DISPLAYS
I/Os
/ 14 OUT
/ 8 OUT
RS-232/422: 6 IN / 6 OUT
ETHERNET: 3 10 / 100 BASE-T
RS-422
MFD-640
HI-RES
NAV
DISPLAY
EFI-890R
HI-RES
NAV
DISPLAY
A429
DATA INPUT
ONE A743 GPS RECEIVER
OR A743A GNSS SENSOR
A429 A429
D ATA
RECORDING
DIGITAL ADC
*
DTU-100 MAY ALSO BE USED
A757 CVFDR/CVR
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UL-801 Installation Manual
(2) UL-801 to UNS-1E/UNS-1C+ Block Diagram – non FANS-enabled
UNS-1E/UNS-1C+ #1 UNS-1E/UNS-1C+ #2
UNIVERSAL
DA
FU
NA
F
VN DT
PE TU
LI
MEN
PR
NE
A B C D E F G
H I J K L M N
O P Q R S T
U V W X Y Z
1 2 3
4 5 6
7 8 9
BA
0
±
MS
ENT
UNIVERSAL
DA
FU
NA
F
VN DT
PE TU
LI PR
MEN NE
A B C D E F G
H I J K L M N
O P Q R S T
U V W X Y Z
1 2 3
4 5 6
7 8 9
BA
0
±
MS
ENT
ARINC 429 LS
ARINC 429 HS
VHF ANTENNA
ARINC 429 HS
RS-422
UL-801
CONFIGURATION MODULE
AIRCRAFT
PRINTER:
ARINC 740.
ARINC 744, OR
SERIAL
RS-232
ARINC 741
SATCOM-BASED
AIRBORNE
TELEPHONY
SSDTU*
UNIVERSAL
* THE DTU-100 MAY BE USED BUT IS NOT RECOMMENDED IN NEW INSTALLATIONS.
CVR/CVFDR
Page 9 23-20-06
UL-801 Installation Manual
(3) UL-801 to UNS-1Esp/UNS-1Csp+ Block Diagram – non FANS-enabled
UNS-1Esp/
UNS-1Csp+ #1
UNS-1Esp/
UNS-1Csp+ #2
UNIVERSAL UNIVERSAL
DA NA VN DT LI PR
FU F PE TU MEN NE
A B C D E F G
H I J K L M N
O P Q R S T
U V W X Y Z
1 2 3
4 5 6
7 8 9
BA
ON/
OFF
0
±
MS
ENT
DA NA VN DT LI PR
FU F PE TU MEN NE
A B C D E F G
H I J K L M N
O P Q R S T
U V W X Y Z
1 2 3
4 5 6
7 8 9
BA
ON/
OFF
0
±
MS
ENT
ARINC 429 LS
ARINC 429 HS
VHF ANTENNA
UL-801
ARINC 429 HS
CONFIGURATION MODULE
RS-422
AIRCRAFT
PRINTER:
ARINC 740.
ARINC 744, OR
SERIAL
RS-232
ARINC 741
SATCOM-BASED
AIRBORNE
TELEPHONY
SSDTU*
UNIVERSAL
* THE DTU-100 MAY BE USED BUT IS NOT RECOMMENDED IN NEW INSTALLATIONS.
CVR/CVFDR
Page 10 23-20-06
UL-801 Installation Manual
(4) UL-801 to UNS-1F/UNS-1D+ Block Diagram – non FANS-enabled
UNIVERSAL
DA NA VN DT LI PR
FU F PE TU MEN NE
A B C D E F G
H I J K L M N
O P Q R S T
U V W X Y Z
1 2 3
4 5 6
7 8 9
BA
0
MS
ON/
OFF
±
ENT
4/5" FPCDU 4/5" FPCDU UNIVERSAL
DA
FU
NA
F
VN
PE
DT
TU
LI PR
MEN NE
A B C D E F G
H I J K L M N
O P Q R S T
U V W X Y Z
1 2 3
4 5 6
7 8 9
BA
0
MS
ON/
OFF
±
ENT
NCU #1
UNS-1F/UNS-1D+
NCU #2
UNS-1F/UNS-1D+
UNI UNI
ARINC 429 LS
ARINC 429 HS
VHF ANTENNA
UL-801
ARINC 429 HS
RS-422
CONFIGURATION MODULE
AIRCRAFT
PRINTER:
ARINC 740.
ARINC 744, OR
SERIAL
RS-232
ARINC 741
SATCOM-BASED
AIRBORNE
TELEPHONY
SSDTU*
UNIVERSAL
* THE DTU-100 MAY BE USED BUT IS NOT RECOMMENDED IN NEW INSTALLATIONS.
CVR/CVFDR
Page 11 23-20-06
UL-801 Installation Manual
(5) UL-801 to UNS-1L/UNS-1K+ Block Diagram – non FANS-enabled
UNIVERSAL
MSG
DAT
FUE
TUN
PRE
NEX
PWR
DIM
A B C D E F G
H I J K L M N
O P Q R S T U
V W X Y Z
ENTE
1 2
4
7
5
8
BACK
0
3
6
9
NA
DT
FP
VNA
LI
MENU
PER
4 FPCDU
UNIVERSAL
MSG
DAT
FUE
TUN
PRE
NEX
PWR
DIM
A B C D E F G
H I J K L M N
O P Q R S T U
V W X Y Z
ENTE
1 2
4
7
5
8
BACK
0
3
6
9
NA
DT
FP
VNA
LI
MENU
PER
4 FPCDU
NCU #1
UNS-1L/UNS-1K+
NCU #2
UNS-1L/UNS-1K+
UNI UNI
ARINC 429 LS
ARINC 429 HS
VHF ANTENNA
ARINC 429 HS
CONFIGURATION MODULE
UL-801
AIRCRAFT
PRINTER:
ARINC 740.
ARINC 744, OR
SERIAL
RS-232
ARINC 741
SATCOM-BASED
AIRBORNE
TELEPHONY
SYSTEM
SSDTU*
UNIVERSAL
* THE DTU-100 MAY BE USED BUT IS NOT RECOMMENDED IN NEW INSTALLATIONS.
CVR/CVFDR
Page 12 23-20-06
UL-801 Installation Manual
(6) UL-801 to UNS-1Ew Block Diagram - FANS-enabled (FMS SCN 1000.5/1100.5 and later)
UNS-1Ew #1
UNIVERSAL
UNS-1Ew #2
UNIVERSAL
DA NA
FU F
VN
PE
DT LI
TU MEN
PR
NE
A B C D E F G
H I J K L M N
O P Q R S T
U V W X Y Z
1 2 3
4 5 6
7 8 9
BA
ON/
OFF
0
±
MS
ENT
DA
FU
NA VN
F PE
DT LI
TU MEN
PR
NE
A B C D E F G
H I J K L M N
O P Q R S T
U V W X Y Z
1 2 3
4 5 6
7 8 9
BA
ON/
OFF
0
±
MS
ENT
ARINC 429 LS
ARINC 429 HS ARINC 429 HS
RS-422
1
FANS UL-801
CONFIGURATION MODULE
VHF ANTENNA
7
5
7
I
N
A
R
C
AIRCRAFT
PRINTER:
ARINC 740.
ARINC 744, OR
SERIAL
RS-232
ARINC 741
SATCOM-BASED
AIRBORNE
TELEPHONY
1
SSDTU*
UNIVERSAL
* THE DTU-100 MAY BE USED BUT IS NOT RECOMMENDED IN NEW INSTALLATIONS.
1 VISUAL, AURAL ALERTING, AND DATALINK RECORDING ARE REQUIRED FOR FANS.
CVR/CVFDR
Page 13 23-20-06
UL-801 Installation Manual
(7) UL-801 to UNS-1Espw Block Diagram - FANS-enabled (FMS SCN 1000.5/1100.5 and later)
UNS-1Espw #1
UNIVERSAL
UNS-1Espw #2
UNIVERSAL
DA NA
FU F
VN
PE
DT LI
TU MEN
PR
NE
A B C D E F G
H I J K L M N
O P Q R S T
U V W X Y Z
1 2 3
4 5 6
7 8 9
BA
ON/
OFF
0
±
MS
ENT
DA
FU
NA VN
F PE
DT LI
TU MEN
PR
NE
A B C D E F G
H I J K L M N
O P Q R S T
U V W X Y Z
1 2 3
4 5 6
7 8 9
BA
ON/
OFF
0
±
MS
ENT
ARINC 429 LS
ARINC 429 HS
1
FANS
AIRCRAFT
PRINTER:
ARINC 740.
ARINC 744, OR
SERIAL
UL-801
ARINC 429 HS
CONFIGURATION MODULE
VHF ANTENNA
RS-422
7
5
7
I
N
A
R
C
RS-232
ARINC 741
SATCOM-BASED
AIRBORNE
TELEPHONY
1
SSDTU*
UNIVERSAL
* THE DTU-100 MAY BE USED BUT IS NOT RECOMMENDED IN NEW INSTALLATIONS.
1
VISUAL, AURAL ALERTING, AND DATALINK RECORDING ARE REQUIRED FOR FANS.
CVR/CVFDR
Page 14 23-20-06
UL-801 Installation Manual
(8) UL-801 to UNS-1Fw Block Diagram - FANS-enabled (FMS SCN 1000.5/1100.5 and later)
UNIVERSAL
DA NA VN DT LI PR
FU F PE TU MEN NE
A B C D E F G
H I J K L M N
O P Q R S T
U V W X Y Z
1 2 3
4 5 6
7 8 9
BA
0
MS
±
ENT
4/5" FPCDU 4/5" FPCDU
UNIVERSAL
DA NA VN DT LI PR
FU F PE TU MEN NE
A B C D E F G
H I J K L M N
O P Q R S T
U V W X Y Z
1 2 3
4 5 6
7 8 9
BA
0
MS
±
ENT
NCU #1
UNS-1Fw
NCU #2
UNS-1Fw
UNI UNI
ARINC 429 LS
ARINC 429 HS
1
FANS
UL-801
ARINC 429 HS
RS-422
CONFIGURATION MODULE
VHF ANTENNA
AIRCRAFT
PRINTER:
ARINC 740.
ARINC 744, OR
SERIAL
7
5
7
I
N
A
R
C
RS-232
ARINC 741
SATCOM-BASED
AIRBORNE
TELEPHONY
1
SSDTU*
UNIVERSAL
* THE DTU-100 MAY BE USED BUT IS NOT RECOMMENDED IN NEW INSTALLATIONS.
1 VISUAL, AURAL ALERTING, AND DATALINK RECORDING ARE REQUIRED FOR FANS.
CVR/CVFDR
Page 15 23-20-06
UL-801 Installation Manual
(9) UL-801 to UNS-1Lw Block Diagram - FANS-enabled (FMS SCN 1000.5/1100.5 and later)
UNIVERSAL
MSG
DAT
FUE
TUN
PRE
NEX
PWR
DIM
A B C D E F G
H I J K L M N
O P Q R S T U
V W X Y Z
ENTE
1 2
4 5
7
BACK
8
0
3
6
9
NA
DT
FP
VNA
LI
MENU
PER
4/5" FPCDU
UNIVERSAL
MSG
DAT
FUE
TUN
PRE
NEX
PWR
DIM
A B C D E F G
H I J K L M N
O P Q R S T U
V W X Y Z
ENTE
1 2
4 5
7
BACK
8
0
3
6
9
NA
DT
FP
VNA
LI
MENU
PER
4/5" FPCDU
NCU #1
UNS-1Lw
NCU #2
UNS-1Lw
UNI UNI
ARINC 429 LS
ARINC 429 HS
1 FANS
UL-801
ARINC 429 HS
CONFIGURATION MODULE
VHF ANTENNA
7
5
7
I
N
A
R
C
AIRCRAFT
PRINTER:
ARINC 740.
ARINC 744, OR
SERIAL
RS-232
ARINC 741
SATCOM-BASED
AIRBORNE
TELEPHONY
SYSTEM
1
SSDTU*
UNIVERSAL
* THE DTU-100 MAY BE USED BUT IS NOT RECOMMENDED IN NEW INSTALLATIONS.
1 VISUAL, AURAL ALERTING, AND DATALINK RECORDING ARE REQUIRED FOR FANS.
CVR/CVFDR
Page 16 23-20-06
UL-801 Installation Manual
The configuration module, an electrically erasable, programmable read-only memory
(EEPROM) device, is mounted on the rear of the mounting tray and connected via a dedicated interface to the UniLink. The configuration module stores information specific to the installation.
The user can view and retrieve the aircraft configuration through specially designed pages that can be accessed through the keypad on the CDU or MCDU. The UniLink retrieves the configuration data during each power up cycle. Modifications to the configuration are possible only on the ground and are restricted through software interlocks.
H. ARINC 429 Channels
UniLink provides sixteen ARINC 429 receivers and eight ARINC 429 transmitters.
(1) ARINC 429 Receivers
The sixteen ARINC 429 receivers can be independently configured for supported
ARINC devices. The receiver bus speed (high or low) is determined by the ARINC device selected during configuration.
(2) ARINC 429 Transmitters
ARINC 429 transmitter, Port #1, is set to low speed by default. The remaining seven
ARINC 429 transmitters can be independently configured for bus speed (high or low). Multiple ARINC devices of the same bus speed can be connected in parallel by each transmitter configuration selection. Do not exceed 15 receive devices on one
ARINC transmitter port.
Device UniLink TX Speed (NOTE 1) UniLink RX Speed
UASC FMS/CDU 1
UASC FMS/CDU 2
UASC FMS/CDU 3
739 MCDU 1
739 MCDU 2
739 MCDU 3
702 FMS 1
702 FMS 2
702 FMS 3
740/744/744A Printer
741 SDU
Voice Tune Bus
Vibro-Meter CMC
604 CMC
750 VDR
LOW
LOW
LOW
LOW
LOW
LOW
LOW or HIGH
LOW or HIGH
LOW or HIGH
LOW
LOW
NOTE 6 LOW
LOW
LOW
NOTE 6 HIGH
HIGH
HIGH
HIGH
LOW
LOW
LOW
NOTE 2
NOTE 2
NOTE 2
LOW
LOW
Not Applicable
HIGH
LOW
HIGH
DHC8 IOP 1 Not Applicable LOW
DHC8 IOP 2 Not Applicable LOW
Page 17 23-20-06
UL-801 Installation Manual
Device
Test Device (NOTE 3)
ARINC 743A GNSS Receiver
DADC1
DADC2
Generic 429 Device (1 – 4)
757 CVR HIGH
UniLink TX Speed (NOTE 1)
LOW or HIGH
Not Applicable
Not Applicable
Not Applicable
LOW or HIGH
HIGH
UniLink RX Speed
HIGH
HIGH or LOW (NOTE 4)
HIGH or LOW (NOTE 5)
HIGH or LOW (NOTE 5)
NOTE 2
Not Applicable
NOTE 1: Device TX speed supported by UniLink.
NOTE 2: The customer database specifies the data speed of this configurable device.
NOTE 3: The test device is not used in aircraft installations.
NOTE 4: References to an ARINC 743A GNSS receiver also include ARINC 743 Global Positioning
System (GPS) receivers. UniLink automatically detects the transmission speed (high/low) of the GNSS or GPS and configures the interface accordingly.
NOTE 5: UniLink automatically detects the transmission speed (high/low) of the Digital ADC and configures the interface accordingly.
NOTE 6: Does not apply to UL-801.
I. RS-232/422 Serial Ports
UniLink provides six general purpose RS-232/422 transmitters and six general purpose
RS-232/422 receivers. These ports are available to perform as six full duplex channels. The ports are capable of operating up to a 19.2 kilobaud rate. The serial port type selection
(RS-232 or RS-422) is determined by the type of serial device selected during configuration.
UniLink RS-422 serial ports support the interface between the UniLink and various combinations of CDU/MCDU display processors (DPs), flat-panel multifunction displays
(MFDs), and EFI-890R displays to accomplish display of uplinked graphic images.
UniLink can be connected to up to three CDUs and one remote CDU/MCDU via ARINC
739 protocol over an ARINC 429 physical layer providing UniLink with control of the
CDU/MCDU text display. The user selects graphics to acquire and display from text menus rendered by UniLink on the CDU/MCDU via this interface.
EFI-890R and high-resolution MFD (SCN 1011.4.8) displays are connected to UniLink via an RS-422. UniLink supports two high-resolution connections.
If the device assigned to a serial port is a low-resolution display, UniLink sets up that port as an RS-422 port at a baud rate specified by configuration item CDU/MFD Baud Rate, options
9801 BPS or 19.2 KBS.
Other devices supported by UniLink RS-232/422 serial ports include a serial printer and
SatCom telephony functions
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UL-801 Installation Manual
UniLink provides 10 general purpose discrete input connections and 14 general purpose discrete output connections.
Discrete Inputs
5 VDC
3.3 VDC
DISCRETE
INPUT
NOTE: THE TRANSITION VOLTAGE VALUE IS 3.8 VDC.
THE ABOVE CIRCUIT IS INTERNAL TO UNLINK.
Basic UniLink Discrete Input
Configurable Discrete Inputs
The discrete input signal types and active states (in other words, whether the signal state is active when the input is open or connected to a ground) are configurable.
The following discrete input types are selectable from the UniLink Discrete Input
Configuration menu:
Park Brake Set
Active State
Ground
Open
Strut Comp
Park Brake Set Options
Active
Park Brake Set
Park Brake Set
Inactive
Park Brake Released
Park Brake Released
Active State
Ground
Open
Strut Comp Options
Active
Strut Compressed
Strut Compressed
Inactive
Strut Not Compressed
Strut Not Compressed
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UL-801 Installation Manual
Door n Closed
Active State
Door n Closed Options
Active Inactive
Ground
Open
Door n is closed
Door n is closed
Door n is open
Door n is open
NOTE: If more than one door discrete input is wired and configured, the inputs are logically
AND’ed together by UniLink to determine approximately when "all doors are closed".
Discrete Outputs
UniLink provides 14 discrete outputs. Each discrete output is capable of current sinking up to
500mA, to drive relays, lights, and trigger a variety of aural warning generators.
12 VDC
V
CC
DISCRETE
OUTPUT
ENABLE
IN
N
THERMAL
LIMIT
<<1
NOTE: THE ABOVE CIRCUIT IS INTERNAL TO UNLINK.
Basic UniLink Discrete Output
Configurable Discrete Outputs
The discrete output signal types and active states (in other words, whether the signal state is active when the input is open or ground) are configurable.
FANS Visual (when FANS is enabled)
Active State
FANS Visual
Active Inactive
Ground
(Recommended Configuration)
Open
FANS ATC annunciator on FANS ATC annunciator off
FANS ATC annunciator off FANS ATC annunciator on
NOTE: 1. The ATC Annunciator power is connected to the aircraft 28 VDC.
2. This annunciator is used to alert the crew of an incoming FANS ATC message.
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UL-801 Installation Manual
FANS Aural (when FANS is enabled)
Active State
FANS Aural
Active Inactive
Ground
(Recommended Configuration)
Open
FANS alerter on
FANS alerter off
FANS ATC annunciator off
FANS ATC annunciator on
NOTE: The aural alerting devices must be connected to the aircraft 28 VDC power.
CPDLC Connect
Active State
CPDLC Connect
Active
Ground
Open
CPDLC connection active
No CPDLC connection
NOTE: Use of this discrete is optional.
Inactive
No CPDLC connection
CPDLC connection active
New Message
Active State
New Message n
Active Inactive
Open received
No new/unread messages
No new/unread messages New/unread message/graphic received
NOTE: This discrete is intended to drive a visual annunciator. Not associated with FANS advisories.
Chime
Active State
Chime n
Active Inactive
Open received
No new/unread messages
No new/unread messages New/unread message/graphic received
NOTE: This discrete is intended to drive an aural annunciator.
Media NOCOMM
Active State
Ground
Open
VHF NOCOMM/SAT NOCOMM/TEL NOCOMM
Active
Media link failed
Media link established/idle
NOTE: These discretes are intended to drive visual annunciators.
Inactive
Media link established/idle
Media link failed
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UL-801 Installation Manual
K. Ethernet
The UASC DTU-100/SSDTU physical interface is 10BaseT Ethernet. The UniLink hardware contains a 10/100BaseT Ethernet port. All UniLink interfaces to the UASC DTU-100 can be directly applied to the UASC SSDTU without any modifications to the UniLink.
L. Transmission Media Management
UniLink is capable of managing multiple links (VHF, TEL, and SAT) so that simultaneous transmission and receipt of messages is possible on several different links. UniLink provides individual management of the VDR radio and satellite communications equipment.
VHF Digital Link (VDL) Mode 2 Capability
The internal VDR is capable of supporting both the D8PSK modulation of the VDL Mode 2 channel and the current ACARS MSK modulation of the POA ACARS channel (which is used when the aircraft is outside of the VDL Mode 2 coverage area) or directed by the DSP.
POA, in conjunction with VDL Mode 2, supports the Future Air Navigation System (FANS) applications that include ATS Facilities Notification (AFN), Controller-Pilot Datalink
Communications (CPDLC), and Automatic Dependent Surveillance-Contract (ADS-C).
The aircraft’s 24-bit International Civil Aviation Organization (ICAO) address is required for
VDL Mode 2 communications. This address is obtained from the selected DSP and is entered during the configuration process and is stored in the configuration module.
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The UniLink contains an internal VHF radio for its data communication. UniLink will only attempt to transmit if the radio has successfully tuned to the selected frequency. VHF
Management requires that UniLink perform the following tasks in order to manage the VHF air-ground link:
•
Acquire a frequency - UniLink acquires a frequency by the Automatic selection method or a frequency is provided by Autotune or manual crew selection/entry or recall from previously established frequency from Non Volatile Memory at power up.
•
Establish a frequency - UniLink establishes the acquired frequency by transmitting a downlink block and receiving a necessary Positive Acknowledgment response.
•
Maintain the frequency - UniLink maintains the established frequency until signal loss on the frequency or until subsequent new frequency selection or entry.
The UniLink VHF Communication Status is displayed on the COMM STATUS page and is explained by the table below.
VHF Media Status Reason
COMM/IDLE
COMM/SENDING
NOCOMM/NO FREQ
Communications have been established with the ground and datalink messages can be transmitted over VHF. No data is currently being transmitted.
A message is currently in the process of being transmitted over VHF and
UniLink is waiting for acknowledgement from the ground.
UniLink has not selected a frequency for tuning due to invalid FMS lat/long or no radio type
NOCOMM/SCANNING
NOCOMM/CONNECTING UniLink has sent communication to the ground and is awaiting a reply.
NOCOMM/NO DSP All DSPs have been manually selected OFF.
NOCOMM/VOICE
UniLink is automatically selecting a frequency for tuning in current region with enabled DSP.
The VDR is in VOICE mode.
NOTE: Does not apply to UL-801 with internal VDR.
NOCOMM/VDR INOP
NOCOMM/VDR FAULT
VDR inoperative.
VDR is reporting a fault.
NOCOMM/VDR UNAVAIL UniLink has not set the VDR’s protocol state.
NOCOMM/MONITORING UniLink has not detected a viable VDL Mode 2 ground station.
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N. SatCom-based Airborne Telephony (TEL)
A dedicated standard telephone modem is designed into UniLink. This modem is used to transfer data between a supported ground station and the aircraft subsystems. For example, the airborne telephone modem is initially used for uploading messages, text weather, and graphical weather data from a DSP via a dial-up connection. UniLink manages only one
RS-232 port for this use.
SatCom-based Airborne Telephony is supported by Iridium and Inmarsat systems that include an integral air phone modem which UniLink accesses via an RS-232 interface. The airborne telephony modem uploads messages, text weather, and graphical weather from a
DSP.
It is important to note that the UniLink does not support the MagnaStar Digital Airborne
Telephone System and the UASC Aero-I. There is no UniLink tip and ring interface as was the case with previous UL-60X/70X products. However, the legacy use of the word TEL, which is used to abbreviate telephony, remains unchanged and continues to indicate the use of a configured RS-232 UniLink port in support of such systems.
If TEL is configured to be used in the priority rotation, the request is then routed to an available SatCom system via a configured RS-232 port.
The available options for RS-232-capable air phone configurations are UASC T-T Aero-M or Iridium. The Iridium selection supports a variety of RS-232 available Iridium SatCom products.
The UniLink Telephony Communications Status is displayed on the COMM STATUS page and is explained in the following table.
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Up to four low-resolution display devices can be connected to a single low-resolution bus and one high-resolution device each can be connected to two high-resolution graphic ports.
TEL Media Status Reason
COMM/MDM TIMEOUT
COMM/DIALING
UniLink has dialed the phone but a timeout occurred prior to a connection being established.
NOTE: Sequential, excessive timeouts will result in the NOCOMM/AUTO
DELAY message displaying.
UniLink has provided the phone with the dial string command and is waiting for the phone to answer.
COMM/CONNECTING
COMM/IDLE
COMM/CONNECTED
COMM/PLEASE WAIT
The ground has answered the phone and UniLink is communicating with the
DSP.
The phone is hung up and no attempt is currently being made to use it and
SatCom (TEL) is not suspended or waiting to retry.
The phone line is connected and messages can or are currently being transferred.
TEL SUSPEND has been manually activated. UniLink is in the process of shutting down the connection.
NOCOMM/SUSPENDED SatCom (TEL) has been suspended, either by the crew or automatically due to excessive failed attempts.
NOCOMM/AUTO DELAY UniLink is waiting for the configurable AUTO-DELAY timer to expire before trying again
NOCOMM/CONFIG FAIL While CONNECTING with the ground server, a message is received saying the configuration sent by UniLink is invalid. The SatCom (TEL) system is permanently shut down. Cycling UniLink power is required to exit this state.
NOCOMM/INIT FAIL
NOCOMM/DIALING
The SatCom (TEL) system is not available for operation. One or both of the following configuration items are invalid: Aircraft Registration Number, or
Phone Access Number.
UniLink exited out of the 5-minute delay and is in the process of making another connection attempt.
NOCOMM/PLEASE WAIT TEL SUSPEND has been manually activated while a connection is in progress. UniLink is in the process of shutting down the connection.
NOCOMM/MDM TIMEOUT UniLink exited out of the 5-minute delay and while in the process of making another connection attempt the UniLink modem has timed out.
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O. SatCom-based ARINC 741 (SAT)
UniLink interfaces with an ARINC 741-capable SatCom system, such as the
Universal/Thrane & Thrane Aero-I SDU and others, via a low speed ARINC 429 interface.
Packet Mode ACARS data (Data 2) is sent to the SDU for forwarding to the ACARS gateway on the ground through the Ground Earth Station (GES) and vice versa.
NOTE: The UASC Aero-I SatCom system is not approved for FANS messaging.
The UniLink SAT Communication Status is displayed on the COMM STATUS page and is explained in the following table.
SatCom Media Status Reason
COMM/IDLE SatCom (SAT) communication has been established and datalink messages can be transmitted over SatCom. No data is currently being transmitted.
COMM/SENDING A message is currently in the process of being transmitted. UniLink is waiting for acknowledgement from the ground.
The SatCom’s system SDU is reporting that it is unavailable. NOCOMM/SDU UNAVAIL
NOTE : SDU is the Satellite
Data Unit.
NOCOMM/SDU INOP UniLink does not detect the SDU.
NOCOMM/AUTO DELAY UniLink is waiting before trying to establish a SatCom (SAT) link again.
NOCOMM/TIMEOUT Retries have been exhausted, and Auto Return to Comm configuration setting is disabled. A manual Link Test must be performed, or an uplink received for the medium to return to COMM.
NOCOMM/CONNECTING A SatCom (SAT) link is in the process of being established.
NOCOMM/SUSPENDED SatCom (SAT) link has been suspended by the crew.
COMM/IDLE
COMM/SENDING
SatCom (SAT) communication has been established and datalink messages can be transmitted over SatCom. No data is currently being transmitted.
A message is currently in the process of being transmitted. UniLink is waiting for acknowledgement from the ground.
NOCOMM/SDU UNAVAIL
NOTE: SDU is the Satellite
Data Unit.
The SatCom’s system SDU is reporting that it is unavailable.
NOCOMM/SDU INOP UniLink does not detect the SDU.
NOCOMM/AUTO DELAY UniLink is waiting before trying to establish a SatCom (SAT) link again.
NOCOMM/TIMEOUT Retries have been exhausted, and Auto Return to Comm configuration setting is disabled. A manual Link Test must be performed, or an uplink received for the medium to return to COMM.
NOCOMM/CONNECTING A SatCom (SAT) link is in the process of being established.
NOCOMM/SUSPENDED SatCom (SAT) link has been suspended by the crew.
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Graphical Weather Depiction
UniLink provides configurable graphic ports which can be configured to interface with a total of six graphics buses.
Graphical weather information is available only when the UniLink is interfaced to a SatCom system via the RS-232 connection and supported by the DSP. The tip and ring data interface, available on previous UniLink models, is no longer required and therefore has been removed.
The graphics capability has been improved by the addition of two high resolution output ports. Graphics may be displayed in high resolution (Hi-Res) for units that are capable of displaying high resolution graphics, such as the EFI-890R in the Navigation Display (ND) position or an MFD-640 with SCN 1011.4.8 or later installed.
Example Graphic
These two high resolution RS-422 ports may be configured to support two dedicated
EFI-890R displays (all EFI-890Rs are capable of high resolution display while all
CDU/MCDUs display in low resolution). In the event that both a low resolution and a high resolution graphic is requested, the UniLink automatically requests and uplinks two formatted images reflecting the same data during the same call:
•
One formatted to support the display of images on the low resolution output
•
One formatted to support high resolution images that will result in a larger, higher quality image
Graphics Display Configuration Options
The Graphics Display Configuration Options include low resolution graphics transmission to
CDUs, remote CDUs, MCDUs, MFDs; and high resolution graphics to high resolution
EFI-890R displays or an MFD-640 with SCN 1011.4.8 or later installed.
P. ACARS Message Processing
UniLink provides services in the Aircraft Communications Addressing and Reporting
System (ACARS). There are two types of ACARS data communications, ground-to-air via uplink messages and air-to-ground via downlink messages, both of which are supported by
SatCom or VHF. Messages sent from one aircraft to another can only be accomplished through the use of user-defined messages via the ground network. Direct communication from aircraft to aircraft is not available. Uplink messages are generated by Airline Ground
Host Centers or an equivalent service provider, ATC facilities or a Datalink Service Provider
(DSP) such as ARINC or SITA. Uplink messages not generated by a DSP are passed to a
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DSP which then sends the uplink messages to a designated UniLink system or aircraft. The message is then processed by UniLink or, when the message is meant for a peripheral unit, is passed on to the appropriate peripheral unit.
(1) ACARS Uplink Message Receiving
When UniLink receives an uplink message from the ground system, it performs a
Block Check Sequence (BCS) error check. If the BCS message is valid, UniLink accepts the message and generates a positive acknowledgment for transmission to the ground. If the uplink message contains an error, UniLink generates a negative technical acknowledgment. Upon receipt of the negative technical acknowledgment, the ground system should retransmit the uplink message.
(2) ACARS Uplink Message Log
UniLink maintains an uplink message log capable of storing at least 40 AOC uplink messages. UniLink stores only those uplink messages that are defined in the database as requiring storage in the log. UniLink allows users to delete or print specific messages from the message log. When the message log is full and a new message requiring storage is received, UniLink will delete the oldest read message in the log.
When the log is full of messages that have not been read and a new message requiring storage is received, UniLink will delete the oldest message.
(3) ACARS Downlink Message Origination
There are several actions that can generate a downlink. The crew may do so via the
CDU/MCDU and route the message to the UniLink for transmission, or UniLink may automatically generate a downlink as a response to an event having occurred, such as weight off wheels or an automatic position report.
(4) ACARS Downlink Message Queue
Once a downlink message is encoded, it is queued until the message can be transmitted to the ground. UniLink is capable of maintaining at least 70 messages in the transmission queue. UniLink allows users to delete or print specific messages from the message log.
(5) ACARS Downlink Message Transmission
When a valid communication link exists, UniLink transmits the message having the highest priority. If more than one message shares the highest priority then UniLink selects the oldest from that group of messages. Upon receipt of the downlinked message, the DSP performs a BCS error check and, if the BCS is valid, it routes it to the proper destination. The ground system also generates a positive technical acknowledgment for the message and transmits it to the aircraft. Upon receipt of a positive technical acknowledgment, UniLink considers the message successfully transmitted.
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UniLink generates advisory alerts annunciating normal and non-normal conditions that require crew action. Selecting the advisory alert displays the UniLink page on which the corresponding information is displayed or from which a required action may be performed.
Examples of advisories are: NEW MSG, VHF VOICE, NOCOMM, and NEW WX MAP.
UniLink provides real-time status information for other LRUs UniLink interfaces with via the DEVICE STATUS page. When configured, devices such as FMSs, internal VHF radio,
741 SatCom-based system, printer, etc. show as OK or INOP. INOP is displayed when communication between both devices has failed. If a particular device is not configured,
UniLink displays NO CONFIG as the device status.
Additionally, the state of various input sensors including all analog discretes is displayed via the SENSOR STATUS page. These displays are useful for initial system installation and trouble-shooting in the field
UniLink generates error messages to alert the crew of non-normal conditions. Generally, a
NEW ERROR MSG advisory appears, which when selected will display the error message title and additional details if applicable. A log of error messages appears on the ERROR
LOG page.
Examples of error messages are:
•
CONFIGURATION WARNING
•
POWER –ON BIT FAILURE
•
VHF CHANNEL CONGESTION
Additionally, UniLink generates pop-up windows for normal and non-normal alert information that may require more timely crew awareness. Examples of pop-up window messages are:
•
QUEUE FULL
•
PRINT JOB COMPLETE
R. Cockpit Voice Recorder (CVR)
Replacing voice communications between crews and air traffic control (ATC) with datalink messages is intended to improve safety, enhance efficiency, and increase air traffic capacity.
This is one of the main features in the UniLink.
The UL-801 provides a configurable ARINC transmit port to support the recording of datalink messages on a compatible ARINC 757Cockpit Voice Recorder (CVR/CVFDR).
The CVR/CVFDR records all messages that are sent to it by the UniLink. Messages are provided to the CVR/CVFDR on an ARINC 429 data bus. This port may be configured for high or low speed based on the recorder’s speed requirement.
When an ARINC transmit port is connected to a UASC CVR/CVFDR, the ARINC transmit port must be configured as follows:
•
PORT SPEED: HIGH
•
PORT DEVICES: CVR
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UniLink supports transmission of datalink message recordings to any ARINC Characteristic
757 CVR/CVFDR.
The following information is sent to the CVR/CVFDR as part of the recording process:
•
Uplinks to the aircraft
•
Downlinks from the aircraft
•
The time the message is displayed to the crew
•
The crew's response to the message
•
UniLink status data
•
Any peripheral data that is addressed to the CVR
Records sent to the CVR may contain the following information:
•
The message priority (if any)
•
The display status of the message
•
Time stamps of the message
•
Other information required to identify the message.
The following examples describe ways that UniLink processes such data.
Example 1: Uplink to the Crew (Weather Graphic Received)
In the event that an uplink intended for display to the crew is received (Weather Graphic),
UniLink transmits a record to the CVR/CVFDR. When UniLink receives the graphic uplink,
UniLink displays the graphic.
Example 2: Downlink from the Crew (Crew-Commanded Downlink)
In the event that the crew generates or commands a downlink (a command to send a downlink is initiated by the crew from CDU/MCDU), UniLink transmits a record to the
CVR/CVFD or UniLink queues a downlink. UniLink transmits another record once the message successfully sends or if a message fails to send.
S. Printers
UniLink supports an interface to an ARINC 740/744/744A or a RS-232 serial printer.
UniLink only supports one printer in a configuration. If both ARINC and RS-232 serial printers are configured, UniLink only uses the ARINC 740/744/744A printer.
UniLink supports printing of text data only. The maximum file size supported by UniLink is
16 KB, including any header and footer. If a print file is larger than 16 KB, UniLink discards the print file and sends a message to the Status log.
NOTE: The file size limit was derived to provide a design guideline for reserving memory for print jobs. The maximum file size from an ACARS uplink is about 3
KB and the maximum Williamsburg file size supported by UniLink is 6,320 bytes.
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T. Transmission Media Interfaces - Configuration Option
SatCom is supported with a configurable interface to an A741 SDU for text-based messages.
Telephony is supported with a configurable RS-232 interface to a UASC T-T Aero-M or
Iridium systems for both text-based messages and graphical weather maps. MagnaStar and
UASC Aero-I tip/ring telephony interfaces are not supported.
VHF communications are supported with a configurable ARINC interface to an external
A750 VDR for text-based messages.
U. Text Message Processing
UniLink supports Aeronautical Operational Communications (AOC) flexible messaging and
FANS message handling. UniLink also supports both uplink and downlink messages from peripheral systems.
UniLink supports Air Traffic Services ATS and AOC text messages, downlink graphical weather requests, and uplink graphical weather images stored and displayed in one or more message logs. Uplink and downlink message integrity checks are performed by means of a
32-bit CRC calculation.
Message alerting functions include configurable output discretes for visual and aural alerting and digital outputs to various LRUs. Message alert inhibiting is configurable and is provided during critical flight phases (takeoff and landing) and is based on flight parameters including ground speed, altitude, and FMS approach mode.
V. Media Advisory Reporting Option
If enabled, UniLink sends the Media Advisory message to update the DSP regarding the status and availability of datalink media, such as VHF, TEL, or SAT. It is useful for the DSP to know the available datalink media when preparing a message for transmission to UniLink.
Upon request by the host processor, the DSP may forward this information to other DSPs.
Crew interaction is not required.
W. Automatic Position Reporting Option
The Automatic Position Reporting Option includes configurable on-ground and in-air automatic position reporting selections. UniLink provides the ability to temporarily disable/enable the automatic position reporting function and modify the reporting interval via the UniLink POS REPORT page.
The Automatic Position Reporting messages may be customized by the user and may conform to the format in ARINC Characteristic 702A. The user will be able to delay transmission of Automatic Position Report messages for a configured amount of time after the OFF event to reduce missed transmissions due to signal blockage during take off.
X. OOOI Reporting/History Option
The OOOI Reporting/History Option includes Out, Off, On, In (OOOI) downlink messaging and history maintenance stored in UniLink’s non-volatile memory. Configurable input parameters (door, brake, strut, ground speed) can be received from multiple sources based on the specific installation. It’s recommended that OOOI be enabled if ARINC is selected as a
DSP.
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Y. Flight Leg Transition
The Flight Leg Transition feature is provided to reduce the crew workload (such as initializing the Origin of the next flight leg to the Destination of the flight leg that was just completed). It is also used as a means of automatically logging data from a flight leg that was just completed if that data may be needed for future reference, such as OOOI times and fuel.
Z. Meteorological Data Reporting Option
The Meteorological Data Reporting Option includes processing of uplink configuration settings and automatic downlink messaging. Meteorological data items include atmospheric temperature, pressure, and wind speeds collected at various durations throughout the flight.
Crew interaction is not needed.
AA. ARINC 741 using Iridium or Inmarsat
UniLink provides a standard interface to ARINC 741-capable SatCom-based airborne telephony systems. The UniLink meets DO-178B level C software requirements necessary for all FANS messaging. The bearer systems such as Inmarsat and Iridium SatCom Systems must meet DO-178B level D requirements. Check with the selected SatCom manufacturer for further details regarding this important issue.
2. Operation
The UniLink is operated by controls provided by the FMS CDU/MCDU. Refer to the
UniLink Operator’s Manual, 23-20-06.01, for UniLink Operating Procedures.
If FANS is enabled, the report number for the UniLink FANS Operations Manual is 23-20-
06.02. This manual must be obtained separately.
The Operator’s Manual introduces the CDU/MCDU, explains the CDU/MCDU operating philosophy, and provides a detailed explanation of the keyboard keys, Line Select Keys
(LSK), and their associated functions.
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FAA Approval
1. General
Installation approval of the UniLink system is being accomplished under a variety of STCs and Forms 337. For a new installation to be eligible for approval, it will be necessary to apply to the FAA for an STC or to utilize an existing STC or Form 337.
This manual contains information directing the follow-on TC or STC applicant to include specific maintenance instructions in the Aircraft Maintenance Manual or ICA when the Field
Loadable Software process is expected to be used as called out in FAA Order 8110.49
Section 5-4.
ACARS/graphics datalink functionality is NOT approved under TSO-C160.
Universal Avionics Systems Corporation received U.S. Federal Communication Commission
“Grant of Equipment Authorization” on TBD, in accordance with FCC Rule Part 87, with the following transmitter specifications:
Mode Output Power
(Minimum)
Frequency
Tolerance
±30 PPM
±5 PPM
Channel
Spacing
25 kHZ
25 kHZ
Frequency
Range
118.000 to
136.975 MHz
118.000 to
136.975 MHz
Emission
Designator
13K0A2D
14K0G1D
•
TSO-C160
Refer to the TSO Deviations section.
•
TSO-C160 Section 3.f Environmental Qualification
The FAA granted a deviation to use the environmental conditions specified in
RTCA/DO-160F in lieu of DO-160E.
•
TSO-C160 Section 4.a.(1) and 4.a.(2) Marking
The FAA granted deviations to allow the parts to marked using the model designation system as referenced in 14 CFR § 21.619(b) Amdt. 21-92 in accordance with 14 CFR §
21.616(d) Amdt.21-92 and § 45.15b, Amdt. 45-26.
− Section 4.a.(1) Marking: Authorization to mark the LRUs with the Model Designation in order to capture both the hardware part number and software control number
(SCN).
−
Section 4.a.(2) Marking: Authorization to not mark the LRUs with the date of manufacture. Each part will be marked with a unique serial number.
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Equipment Classes
•
UL-801, SCN 30:
− F
VDL Mode 2 receiver used in a 25-kHz channel separation environment
− 7
VDL Mode 2 transmitter used in a 25-kHz channel separation environment, intended to operate with a range of 200 nautical miles
Equipment Architecture Classes
•
UL-801, SCN 30:
−
W (CMU)
−
Y (VDR)
(1) TSO-C160 (11-Jan-2008): VDL Mode 2 Communications Equipment
(2) DO-281A (08-Nov-2005): Minimum Operational Performance Standards for Aircraft
VDL Mode 2 Physical, Link, and Network Layer (MPS for TSO-C160)
(3) AC 20-140A (07-Apr-2010): Guidelines for Design Approval of Aircraft Data
Communications Systems
(4) AC 20-160 (21-Feb-2008): Onboard Recording of Controller Pilot Data Link
Communication in Crash Survivable Memory
(5) DO-186B (08-Nov-2005): Minimum Operational Performance Standards for
Airborne Radio Communications Equipment Operating Within the Radio Frequency
Range 117.975 – 137.000 MHz
(6) DO-258A (07-Apr-2005): Interoperability Requirements for ATS Applications Using
ARINC 622 Data Communications (FANS 1/A Interoperability Standard)
(7) RTCA/DO-160F (06-Dec-2007): Environmental Conditions and Test Procedures for
Airborne Equipment
(8) RTCA/DO-178B (01-Dec-1992): Software Considerations in Airborne Systems and
Equipment Certification
(9) RTCA/DO-254 (19-Apr-2000): Design Assurance Guidance for Airborne Electronic
Hardware
(10) RTCA/DO-306/ED-122 (11-Oct-2007): Safety and Performance Standards for Air
Traffic Data Link Services in Oceanic and Remote Airspace (Oceanic SPR Standard)
(11) ARINC 618-6 (Jun-2006): Air/Ground Character-Oriented Protocol Specification
(12) ARINC 623-3 (Apr-2005): Character-Oriented Air Traffic Service (ATS)
Applications
(13) ARINC 631-5 (Dec-2008): VHF Digital Link (VDL) Mode 2 Implementation
Provisions
(14) ARINC 741P2-10 (09-Feb-2009): Aviation Satellite Communication System Part 2
System Design and Equipment Functional Description (Section 4.7 ACARS MU/CMU
- SATCOM Interface)
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(15) ED-85A (Dec-2003): Data Link Application System Document (DLASD) for the
"Departure Clearance" Data-Link Service
(16) ED-89A (Dec-2003): Data-Link Application System Document (DLASD) for the
"ATIS" Data-Link Service
(17) ED-106A (Mar-2005): Data-Link Application System Document (DLASD) for the
“Oceanic Clearance” Data-Link Service
(18) GOLD (14-Jun-2010): Global Operational Data Link Document (GOLD)
(19) AC 120-70A (29-Dec-2005): Operational Authorization Process for use of Data Link
Communication System
(20) ICAO Doc 9613 (01-Jan-2008): Performance-based Navigation (PBN) Manual
(21) RTCA/DO-290/ED-120; Change 1 and Change 2 (29-Apr-2004): Safety and
Performance Requirements Standard for Air Traffic Data Link Services in
Continental Airspace (Continental SPR Standard)
(22) ED-154 (Jul-2008): Future Air Navigation System 1/A - Aeronautical
Telecommunication Network Interoperability Standard
TSO Functions
(1) VDL Mode 2 - Ref: TSO-C160, DO-281A, ARINC 631
Supports the requirements contained in TSO-C160 and MPS DO-281A. The UL-801 is equipment class F (VDL Mode 2 receiver used in a 25-kHz channel separation environment) and 7 (VDL Mode 2 transmitter used in a 25-kHz channel separation environment, intended to operate with a range of 200 nautical miles) and architecture class W (CMU) and Y (VDR). The UL-800 is architecture class W (VDR).
TSO Supporting Functions
(1) Data Loading of Software and Databases - Ref: ARINC 758, SRD
Application-level functionality may be field-modified by the transfer from portable media (disk or flash memory) of the UniLink and VDR software programs as well as databases that define the cockpit presentation, air/ground message types and formats, as well as the geographic location of VHF ground stations.
(2) Config Module Interface - Ref: ARINC 758, SRD
An aircraft "personality module" is integrated with the UniLink to hold configuration data unique to the aircraft installation. This includes the physical connections as well as customer-specific operational preferences.
(3) BIT/Maintenance and Status Reporting - Ref: ARINC 758
Built-in-test and continuous health monitoring functions detect health of both internal components (memory, I/O devices, S/W validity, etc.) as well as external systems.
Maintenance and Status reporting provides periodic output of the status of other connected aircraft peripherals. Errors are presented to the cockpit and logged internally for service and troubleshooting.
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(4) VDL Mode A - Ref: ARINC 618, DO-186B
VDL Mode A refers to the analog communication protocols exercised by the VHF data radio (VDR) and supported by the UniLink to exchange ACARS messages with any appropriately equipped ground system. This mode is equivalent to the plain old
ACARS (POA) function of historical CMUs.
(5) SatCom Communication Interface - Ref: ARINC 618, ARINC 619
Satellite-based communication is available to the UniLink through a digital interface to an external satellite data unit (SDU). The SatCom interface provides an alternative media to VHF for the transmission of ACARS messages supporting
FANS 1/A+, ACARS ATS, and AOC applications. Customer preferences usually prioritize the use of SatCom communications lower than VHF communications resulting in this function generally being used in Remote or Oceanic regions.
(6) ACARS - Ref: ARINC 618
The Aircraft Communications Addressing and Reporting System (ACARS) is a data link protocol and message structure which allows communication of characteroriented data between aircraft systems and ground communication service provider systems.
(7) AOA - ACARS over AVLC Ref: ARINC 618
The AOA function transports ACARS messages using ACARS routing over VDL
Mode 2 Aviation VHF Link Control (AVLC) - the data link layer. AOA provides a more efficient, digital exchange of air/ground ACARS messages than VDL Mode A.
(8) ACARS Air Traffic Services (for example, D-ATIS, PDC, OC) (TSO indirect) -
Ref: ARINC 622, ARINC 623
The ACARS ATS function is the exchange of text-based Air Traffic Services information between the flight crew and ATS ground host processing systems. These services include: Automatic Terminal Information Services (ATIS), Oceanic
Clearances (OC), Pre-Departure Clearances (PDC), Terminal Weather Information for Pilots (TWIP), Pushback Clearances, and Expected Taxi Clearances.
(9) Airline Operations Control (AOC – for example, text weather, weight, and balance) -
Ref: ARINC 620
The AOC function is the exchange of text-based information between the flight crew/aircraft systems and the operator’s AOC processing systems (for example, dispatch, maintenance, or meteorological services) throughout all phases of flight
(pre-flight, enroute, and post flight). Data included in the messages can be drawn from other aircraft systems (such as I/O concentrator buses or FMS units) or can be entered by the flight crew via a control and display unit.
(10) Datalink Message Recording - Ref: ARINC 758, ARINC 619
Intending to improve safety, enhance efficiency, and increase air traffic capacity, the trend of replacing voice communications between flight crews and air traffic control
(ATC) with datalink messages is becoming more prevalent. In order to aid in potential incident/accident investigations, UniLink supports transmission of datalink messaging records to an ARINC Characteristic 757 cockpit voice recorder (CVR).
Records presented to the CVR include messages exchanged between the UniLink and
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CSPs and between the UniLink and peripheral devices, datalink-based crew actions, and other datalink events.
Non-TSO Functions
(1) Telephony Communication Interface - Ref: SRD
The telephony communication interface provides an alternate media for the limited transfer of operator’s AOC messages and weather graphics between the aircraft and the ground. The telephony interface uses industry standard protocols for access to an airborne telephone modem that is part of an on-board satellite communication system.
Telephony messaging is supported through separate air-air/air-ground channels from other SATCOM ACARS ATS and FANS 1/A+ message functions.
(2) FANS 1/A+ Ops Credit for FANS - Ref: DO-258A, GOLD, ARINC 622
UniLink system functionality is greatly enhanced by offering a FANS-1/A + implementation, which is intended to improve safety of flight, enhance efficiency, and increase capacity by replacing routine voice transmissions between flight crews and ATC with datalink messages during flight in oceanic and remote areas that have no or limited radar coverage. FANS operational credit can be applied for following
UniLink installation airworthiness approval for aircraft that are properly equipped.
(3) Weather Graphics - Ref: SRD
Graphical weather images can be requested by the crew and transferred by UniLink from the ground via the Telephony Communication Interface and presented on compatible display units (UASC only) in the cockpit. This facility is supported by ground AOC facilities complying with UASC-proprietary protocols and message formats. The images presented are intended for non-essential use.
SCN 10.X Main UniLink Bootloader Software
Main UniLink Bootloader software version SCN 10.X is categorized as DO-178B Level D
(Minor). Level D software is defined by DO-178B as “software whose anomalous behavior, as shown by the system safety assessment process, would cause or contribute to a failure of system function resulting in a minor failure condition for the aircraft”.
VDR Bootloader SCN 10.X
The VDR boot software is partitioned from the VDR application and will be developed to
Level D. The VDR boot software is stored in a flash memory device separate from that of the application software. Once the application software is invoked, the boot software is deactivated.
VDR Transmit Monitor SCN 10.X
The VDR transmit monitor software is partitioned from the VDR boot and application software and will be developed to Level C. The VDR transmit monitor software is stored and executes on a separate microcontroller residing on a different physical circuit card from that that hosts the VDR boot and application functions.
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SCN 30.X Application Software
Application software version SCN 30.X is categorized as DO-178B Level C (Major). Level
C software is defined by DO-178B as “software whose anomalous behavior, as shown by the system safety assessment process, would cause or contribute to a failure of system function resulting in a major failure condition for the aircraft”.
SCN 10.X VHF Data Radio Application Software
VHF Data Radio Application software version SCN 10.X is categorized as DO-178C Level
C (Major). Level C software is defined by DO-178B as “software whose anomalous behavior, as shown by the system safety assessment process, would cause or contribute to a failure of system function resulting in a major failure condition for the aircraft”.
3. Instructions for Continuous Airworthiness, FAR 23.1529,
25.1529, 27.1529 and 29.1529
Our statement in compliance with FAR 23.1529, 25.1529, 27.1529 and 29.1529 follows:
Maintenance Requirements and Instructions for Continuous Airworthiness
SYSTEM: Universal Avionics Systems Corporation UniLink System
Modification of an aircraft by this Supplemental Type Certificate or Form 337 obligates the aircraft operator to include the maintenance information provided by this document in the operator’s Aircraft Maintenance Manual and the operator’s Aircraft Scheduled Maintenance
Program.
(1) Maintenance Manual information for the UniLink (system description, removal, installation, testing, etc.) is contained in Universal Avionics Systems Corporation’s
(UASC) Installation Manual 23-20-06.
(2) Line Replaceable Unit (LRU) part numbers and other necessary part numbers contained in the installation data package should be placed in the aircraft operator’s appropriate aircraft Illustrated Parts Catalog (IPC). Refer to Equipment
Specifications, F. Electronic Part Marking, of this manual for additional parts marking information.
(3) Wiring diagram information contained in the aircraft installation’s data package should be placed into the aircraft operator’s appropriate aircraft Wiring Diagram
Manuals.
(4) Installation specific electrical drawings, mechanical drawings and miscellaneous documents are listed on the data package Master Drawing List.
(5) The LRU’s location and access requirements are as defined by the installer.
(6) Revision to this document will be accomplished via Service Bulletins and/or
Installation Manual revision.
(7) The system performs full self-test BITE at each power on and any failures are annunciated to the crew.
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Scheduled Maintenance Program
Scheduled Maintenance Program tasks to be added to the aircraft operator’s appropriate aircraft maintenance program are as follows:
(1) Recommended Periodic Scheduled Servicing Tasks: None Required
(2) Recommended Periodic Scheduled Preventative Maintenance Tests/Checks to determine System Condition and/or Latent Failures:
(4) Recommended Periodic Structural Inspections:
None Required
(3) Recommended Periodic Inspections: None
None Required
(5) Recommended Replacement Interval: None
Unscheduled Maintenance Program
Unscheduled maintenance may include upgrade of the program software contained in the
UniLink, upgrade of the Field Loadable software, or other modifications. If the UniLink is removed and the software changed, the configuration settings should be checked and amended as necessary in accordance with the instructions contained in applicable manuals.
B. Compliance
Universal Avionics has published two compliance reports for the UL-80X systems. These reports describe installation requirements that must be considered as part of the installation airworthiness approval. Contact Universal Avionics Product Support to receive the latest revisions of these reports.
RPRT-2012-1005, AC 20-140A Compliance Report for the UL-80X UniLink LRU with
Software SCN 30.X
RPRT-2012-1007, UniLink UL-80X With Software SCN 30.X Compliance Summary Report
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The environmental categories under which the UniLink is approved (Reference RTCA DO–
160F) are listed on the following Environmental Qualification Forms.
ENVIRONMENTAL QUALIFICATION FORM
PART NO.
TSO NUMBER
MANUFACTURER
Conditions
Temperature and Altitude
10801-XX
TSO-C160
Universal Avionics Systems Corporation
3260 East Universal Way
Tucson, AZ 85756-5097
DO-160F
Section #
Category Description of Conducted Tests
4 A2 E1
Inside or outside pressure vessel
− 55°C to +70°C
Maximum altitude—70,000 feet
For the E1 levels that, per RTCA/DO-160F, are declared by the manufacturer, the corresponding levels for A2 are used.
In-Flight Loss of Cooling 4.5.4
Temperature Variation 5
X
B
There is no fan on this product.
Equipment in non-temperature controlled area of airplane.
5 degrees/minute
Operational Shocks and
Crash Safety
Vibration 8
Explosion Atmosphere 9
S
H
Test category S—Standard
Equipment H—including hermetically sealed, contains hot spot surfaces and non-spark producing.
Environment 2—atmosphere where flammable mixture exist only because of spillage or leakage.
Fluids Susceptibility
Sand and Dust
Fungus Resistance
11
12
13
X
X
X
Not tested—Fluid contamination not commonly encountered.
Not tested—Not subject to blowing sand and dust.
Not tested—Equipment not exposed to severe fungus contamination.
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Conditions
Salt Fog
Magnetic Effect
Power Input
Voltage Spike
UL-801 Installation Manual
DO-160F
Section #
Category Description of Conducted Tests
14 X
Not tested—Equipment not subjected to salt atmosphere.
15 Z
Actual class will be measured. (The distance required to cause a compass needle deflection of one degree is measured and must be less than 0.3 meter to be considered compliant with Category Z.)
16
17
Z
A
DC generator systems with or without a battery. Not designated to transmit under emergency electrical system conditions.
Equipment installed where high degree of protection against voltage spikes is required.
Audio Frequency
Conducted Susceptibility
18 Z —
Induced Signal
Susceptibility
Equipment intended for operation where interference
19 ZC free operation is required on an aircraft whose primary power is constant frequency or DC.
Radio Frequency
Susceptibility (Radiated and Conducted)
Emission of Radio
Frequency Energy
20 R HIRF conditions are part of normal environment.
21 M —
Lightning Induced
Transient Susceptibility
Lightning Direct Effects
22
23
A3 G33
J33
X
Pin test performed to level A3; shielded cable bundle test performed to level J33; unshielded cable bundle test performed to level G33.
NOTE: The pin test was performed to level A3 except for the Ethernet signal pins which were tested to
Level A2.
—
Electrostatic Discharge 25 A —
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ENVIRONMENTAL QUALIFICATION FORM
PART NO.
TSO NUMBER
MANUFACTURER
Conditions
Temperature and Altitude
In-Flight Loss of Cooling
108009
TSO-C160
Universal Avionics Systems Corporation
3260 East Universal Way
Tucson, AZ 85756-5097
DO-160F
Section #
Category Description of Conducted Tests
4
4.5.4
A2 E1
X
Inside or outside pressure vessel
− 55°C to +70°C
Maximum altitude—70,000 feet
For the E1 levels that, per RTCA/DO-160F, are declared by the manufacturer, the corresponding levels for A2 are used.
There is no fan on this product.
Temperature Variation 5 B
Equipment in non-temperature controlled area of airplane.
5 degrees/minute
Operational Shocks and
Crash Safety
Vibration 8 S
Explosion Atmosphere 9 H
Test category S—Standard
Equipment H—including hermetically sealed, contains hot spot surfaces and non-spark producing.
Environment 2—atmosphere where flammable mixture exist only because of spillage or leakage.
Fluids Susceptibility
Sand and Dust
Fungus Resistance
Salt Fog
11
12
13
14
X
X
X
X
Not tested—Fluid contamination not commonly encountered.
Not tested—Not subject to blowing sand and dust.
Not tested—Equipment not exposed to severe fungus contamination.
Not tested—Equipment not subjected to salt atmosphere.
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Conditions
Magnetic Effect
Power Input
Voltage Spike
UL-801 Installation Manual
DO-160F
Section #
Category Description of Conducted Tests
15 Z
Actual class will be measured. (The distance required to cause a compass needle deflection of one degree is measured and must be less than 0.3 meter to be considered compliant with Category Z.)
16
17
Z
A
DC generator systems with or without a battery. Not designated to transmit under emergency electrical system conditions.
Equipment installed where high degree of protection against voltage spikes is required.
Audio Frequency
Conducted Susceptibility
18 Z —
Induced Signal
Susceptibility
19 ZC
Equipment intended for operation where interference free operation is required on an aircraft whose primary power is constant frequency or DC.
Radio Frequency
Susceptibility (Radiated and Conducted)
Emission of Radio
Frequency Energy
20 R HIRF conditions are part of normal environment.
21 M —
Lightning Induced
Transient Susceptibility
Lightning Direct Effects
22
23
A3 G33
J33
X
Pin test performed to level A3; shielded cable bundle test performed to level J33; unshielded cable bundle test performed to level G33.
—
A — Electrostatic Discharge 25
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5. Sample Airplane Flight Manual Supplement
Prepare an Airplane Flight Manual Supplement using the following sample as a guide.
NOTE: Comments in angle brackets, < >, and italics are explanatory only and should not appear in the final supplement.
<Name of Applicant> AFM Supplement for <Aircraft Model>
<Address>
Supplement No.
{SAMPLE}
FAA APPROVED
AIRPLANE FLIGHT MANUAL SUPPLEMENT
FOR
AIRCRAFT MAKE: __________________________________
AIRCRAFT MODEL: ________________________________
AIRCRAFT REG: ___________________________________
AIRCRAFT S/N: ___________________________________
This supplement must be attached to the FAA Approved Airplane Flight Manual when the airplane is modified by the installation of a Universal Avionics Systems Corporation (UASC)
UniLink System, in accordance with STC ____________________________, (or Form 337).
The information contained herein supplements or supersedes the basic manual only in those areas listed herein. For limitations, procedures, and performance information not contained in this supplement, consult the appropriate basic Airplane Flight Manual.
FAA Approved:
<Name>
<Title>
FEDERAL AVIATION ADMINISTRATION
<Name of Aircraft Certification Office>
<Address>
FAA Approved Date:
Page 1 of y
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REVISION HISTORY
Sheet Rev Description Approved
Document Date:_________________
______________________
(Name)
(Title)
FEDERAL AVIATION ADMINISTRATION
(Name of Aircraft Certification Office)
(Address)
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TABLE OF CONTENTS
Section Title
1 General
2 Limitations
3 Emergency and Abnormal Procedures
Page
4
5
8
9
12
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Section 1 - General
<The following is a sample of how the introduction could read. Fully describe all interfaces with the UniLink.>
The Universal Avionics Systems Corporation UniLink installation is interfaced with up to three UASC Flight Management Systems.
The UniLink contains software 30.X.
Section 2 - Limitations
The UniLink Operator’s Manual, report number 23-20-06.01, must be available to the flight crew when UniLink is to be used during flight. <If FANS is enabled, this report number is
23-20-06.02.>.
B. Limitations
When a UniLink CDU/MCDU message display screen is labeled “Unverified” or “AOC”, the Aircraft Communications and Reporting System (ACARS) is unable to ensure that message content was not corrupted during transmission. Unverified messages must be restricted to those that do not create an unsafe condition if:
(1) The message is not received.
(2) The message is delivered to the wrong recipient.
(3) The message content may be frequently corrupted.
NOTE: Unverified message contents should be treated as advisory only.
Section 3 - Emergency and Abnormal Procedures
No change to FAA Approved Airplane Flight Manual.
Page x of y
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Section 4 - Normal Procedures
Normal operating procedures are outlined in the UniLink Operator’s Manual, report number
23-20-06.01. <If FANS is enabled, this report number is 23-20-06.02.>.
Section 5 – Performance Data
No change to FAA Approved Airplane Flight Manual.
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Equipment Specifications
1. UniLink Equipment Specifications
A. UniLink Part Number Matrix
10801 XX
Basic Part
Number
Hardware Variant
00 = Baseline
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B. UniLink Installation Kit
(1) Installation Kit P/N K12030-1
Quantity
1
Part Number
13636-93601-2 or
93601-2
MS24693C4
Description
Rack, ARINC 600, 1 MCU (Barry Controls)
6
1
2
Screw, Recessed, Cres, 100 ° CSK, 4-40 x 3/8”
MS51957-20 Screw, 4-40 x 7/8”, Cres (for configuration module)
2 MS21083C04 Nut, 4-40, Cres, Self Lock (for configuration module)
NOTE: Equivalent substitutes may be used for the listed items in the installation kits.
The UniLink will continue to operate with a 19.0V power input.
Component
Current/Power
(Amps @ VDC)/Watts
Inrush Current
(Amps @ VDC)
22.0V
Min
27.5V
Nominal
32.0V
STBY TX STBY TX STBY
Max
22.0V
TX
Min
27.5V
Nominal
UL-801 10801-XX
1A;
22.0W
3.5A typical
@ 77W
7A maximum
@ 154W
0.9A;
24.8W
3.5A typical
@ 96W
7A maximum
@ 192W
0.7A;
22.4W
3.5A typical @
112W 2.5A @
<100ms 7A maximum
@ 224W
2.5A @
<100ms
NOTE:
•
The UL-801 is designed to operate using a 5A circuit breaker.
•
The UL-801 VDR Transmit Message Duty Cycle is < 750ms.
32.0V
Max
2.5A @
<100ms
Component
UL-801 UniLink
Equipment Rack
Weight
Approximately 4.5 Lbs.
11.5 Oz.
Configuration Module 0.5 Oz.
E. VHF Antenna Specifications
Antenna Specifications
Coax Cable Attenuation < 3 dB
Frequency Range
Power Rating
118.000 – 136.975
15W - 35W
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F. Electronic Part Marking
UniLink supports Electronic Part Marking and is in compliance with FAA Order Number
8110.49 which allows verification of the installed part number and software versions by accessing pages on the connected display device such as a CDU or MCDU. The UniLink nameplate, as shown below, makes reference to the Installation Manual (IM) where such information can be found.
Per FAA Order number 8110.49, there should be a process in place to ensure that maintenance personnel record loaded Field Loadable Software (FLS) part number in the necessary maintenance logs.
When new software is loaded into the unit, it is the maintenance personnel’s responsibility to ensure that the software part number has been logged and verified before the unit/aircraft is returned to service.
Changes to software part number, version, and/or operational characteristics should be reflected in the Operator’s Manual, Aircraft Flight Manual, Aircraft Flight Manual
Supplement, and/or any other appropriate document.
R
AIRBORNE DATALINK
UL-800
P/N 10800-00
SOFTWARE VERIFICATION AND VALIDATION
DO - 178B LEVEL C
SCN ELECTRONIC MARKING
SEE IM 23-20-05
TSO-C160 (Dev)
EQUIPMENT CLASS
SEE IM 23-20-05
MANUFACTURED BY
TUCSON AZ 85756 U.S.A.
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(1) UL-801 (P/N 10801-XX) Outline Drawing
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(2) Rack Drawing (P/N 13636-93601-2)
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(3) Configuration Module (P/N 108009)
.875"
.282"
1.200"
(4) Configuration Module Installation Detail
108009 CONFIGURATION MODULE
CONNECTOR
UL801 RACK CONNECTOR KEYING
ARINC 600 #08 POLARIZATION
(BLACK SEGMENT INDICATES RACK POST)
4-40 SCREWS AND
NUTS
NOTE: The darkened portion of the rack connector above indicates the extended part of the key; the light portion indicates the key hole.
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(1) Digital Inputs
(a) FMS ARINC 429 Broadcast Data
Label Description Format
102 Selected Altitude BNR
UNS
HS429-1
TX Rate
(ms)
200
ARINC
429 HS
TX Rate
(ms)
N/A
Notes
Crew selected via CP.
116 Cross-track Distance BNR 100 relative to SXTK
147 Magnetic Variation
150 UTC
203 Pressure Altitude
204
205
206
Baro-Corrected Altitude
Mach
Indicated Air Speed
ADC dependent.
BNR 100 500 output if available.
BNR 500 N/A
BNR
500
(NOTE 2)
N/A N/A
BNR 100 500
BNR 100 N/A
210 True Air Speed
212 Altitude Rate
213 Static Air Temperature
231
Actual Navigation
Performance
BCD 500 500
233 Selected Cross-track BCD 500 flight plan.
251
Along Track Distance to
WPT
252 Estimated Time to Waypoint BNR 500 500
260 Date
270 Status
272 Active Leg Attributes
DSC 100
DSC 100
500
N/A Contains flight phase data.
310
311
312
Present Latitude
Present Longitude
Ground Speed
313 True Track Angle
314 True Heading
315 Wind Speed
316 True Wind Angle
BNR 100 100
BNR 100 100
BNR 100 500
BNR 100 100
320 Magnetic Heading BNR
100
(NOTE 1)
100
(NOTE 2)
N/A
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Label
325
Description
Roll Angle
Format UNS
HS429-1
TX Rate
(ms)
ARINC
429 HS
TX Rate
(ms)
BNR
100
(NOTE 1)
100
(NOTE 2)
N/A
BNR 1000 N/A
Notes
370 WGS-84/GNSS Height
371 Equipment ID
NOTE: 1. When in DEMO mode, the label is not transmitted.
2. Label is output during DEMO mode when IRS ATT OUTPUTS is set active.
When IRS ATT OUTPUTS is set inactive, these labels are inhibited during DEMO mode.
(b) 702A FMS ARINC 429 Broadcast Data
Label Description
203 Pressure Altitude
210 True Air Speed
213 Static Air Temperature
314 True Heading
315 Wind Speed
316 True Wind Angle
Format Transmission Rate (ms)
BNR 1000
BNR 500
BNR 1000
BNR 100
BNR 500
BNR 500
(c) ARINC 741 SDU Broadcast Data
Label
270 Status
Description Format Transmission Rate (ms)
DSC 1000
(d) ARINC 740/744A Printer Broadcast Data
Label Description
350 Printer Status
Format Transmission Rate (ms)
DSC 1000
(e) DHC8-S400 IOP Bus #1 and IOP Bus #2 Broadcast Data ARINC 429
Label Description
107 Selected Flap Position
164 Radio Altimeter 1
164 Radio Altimeter 2
176 Left Engine Fuel Temperature
176 Right Engine Fuel Temperature
204 Baro Alt 1 (cor)
204 Baro Alt 2 (cor)
205 Mach Number 1
205 Mach Number 2
206 Calib Airspeed 1
206 Calib Airspeed 2
Format Source
BNR FCU
BNR
BNR
FMU 1 (IOP 1)
FMU 2 (IOP 2)
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Format Label Description
210 True Airspeed 1 (TAS)
210 True Airspeed 2 (TAS)
211 Total Air Temp 1
211 Total Air Temp 2
212 Altitude Rate 1
212 Altitude Rate 2
213 Static Air Temp 1 (SAT)
213 Static Air Temp 2 (SAT)
244 Left Fuel Flow
244 Right Fuel Flow
245 Left Gas Gen Speed (NL)
245 Right Gas Gen Speed (NL)
246 Left Gas Gen Speed (NH)
246 Right Gas Gen Speed (NH)
247 Total Fuel Qty Lbs
256 Left Tank Fuel Qty Lbs
256 Right Tank Fuel Qty Lbs
270 IOP 1 Discrete Word 1
270 IOP 2 Discrete Word 2
316 Left Engine Oil Temp
316 Right Engine Oil Temp
317 Left Eng Oil Pressure
317 Right Eng Oil Pressure
325 Roll Altitude 1
325 Roll Altitude 2
336 Left Engine Torque
336 Right Engine Torque
345 Left ITT
345 Right ITT
346 Left Propeller
346 Right Propeller
BNR
BNR
BNR
BNR
BNR
BNR
Source
BNR
BNR
BNR
BNR
Left Fuel Flow Meter
Right Fuel Flow Meter
FADEC 1 (A/B)
FADEC 2 (A/B)
BNR
BNR
FADEC 1 (A/B)
FADEC 2 (A/B)
BNR FQC
BNR FQC
BNR FQC
BNR IOP 1
BNR IOP 2
BNR FADEC 1 (A/B)
BNR FADEC 2 (A/B)
BNR Left Eng Oil Pres Meter (IOP 1)
BNR Right Eng Oil Pres Meter (IOP 2)
FADEC 1 (A/B)
FADEC 2 (A/B)
FADEC 1 (A/B)
FADEC 2 (A/B)
FADEC 1 (A/B)
FADEC 2 (A/B)
(f) ARINC 739A MCDU Broadcast Data
Label Description
172 System Identification Word
270 MCDU Status Word #1
377 MCDU Identifier Word
Format Transmission Rate (ms)
DSC 1000
DSC 1000
DSC 1000
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(g) ARINC 743 GNSS Broadcast Data
Label Description
076 GNSS Altitude
103 GNSS Track Angle
110 GNSS Latitude
111 GNSS Longitude
112 GNSS Ground Speed
150 UTC Time
165 Vertical Velocity
260 Date
273 GNSS Sensor Status
Format Transmission Rate (ms)
BNR 1000
BNR 1000
BNR 1000
BNR 1000
BNR 1000
BNR 1000
BNR 1000
BCD 1000
DSC 1000
(h) 604 CMC ARINC 429 Broadcast data
Label
270 Status
Description Format Transmission Rate (ms)
DSC 1000
(2) Digital Outputs
(a) Standard UniLink Broadcast Data ARINC 429
Label Description
172 System Identification Word
214 ICAO Aircraft Address Word #1
216 ICAO Aircraft Address Word #2
270 Status Word #1
276 Status Word #2
350 Maintenance Word #1
351 Maintenance Word #2
Format Transmission Rate (ms)
DSC 1000
DSC 1000
DSC 1000
DSC 1000
DSC 1000
DSC 1000
DSC 1000
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I. HS-429-1 Bus – UniLink
NOTE: Although there are HS-429-1 labels available for GLS, TAWS, and
Vision-1, only the labels for UniLink are shown in the following table.
Label Definition
150 Greenwich Mean Time
204 Barometric Altitude (429 GAMA)
213 Static Air Temperature
Format TX Rate Update
Rate
BNR 1000
BNR 100
BNR 100 ms
500 ms
100 ms
500 ms
234 Poll Word (ENQ) from MDF
234 Clear to Send Word (CTS) from MDF
234 Synchronization Word (SYN) from MDF
234 Button-Push Word (BPW) from MDF
234 ACK Word from User System from MDF
234 NAK Word from User System from MDF
235 Full Data Word
235 Partial Data Word
235 Protocol Word
235 Solo Word
235 Start of Transmission
235 End of Transmission
252 Time to Go (429 GAMA)
260 Date
261 GPS Discrete Word 1 (429 GAMA)
310 Present Position Latitude
311 Present Position Longitude
312 Ground Speed
315 Wind Speed
316 True Wind Speed
340 Present Position Fine Latitude
341 Present Position Fine Longitude
BNR
1000 ms and as required
500 ms 1 per sec.
BCD 1000
DSC 1000
BNR 100
BNR 100
BNR 100 ms 100 ms
BNR 1000
BNR 1000
BNR 100 ms 100 ms
BNR 100 ms 100 ms
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Item
6
7
4
5
1
2
3
Configurable LRU
Input Data Equipment
A743 GPS/A743A GNSS
DHC8 IOP
Digital ADC
UASC FMS/CDU
A702 FMS
604 CMC
VM CMC
Qty Supported by UL-80X (I/O Type)
1 (A429)
2 (A429)
2 (A429)
3 (A429)
3 (A429)
1 (A429)
1 (A429)
Display Equipment
9
10
UASC A739A MCDU
Standard A739A MCDU
11 EFI-890R
12 MFD-640
13 CDU
3 (A429)
3 (A429)
2 (RS-422)
Transmission Media
15
16
17
Internal VHF Radio (VDR) (UL-801 only)
A750 VDR (UL-800 only)
A741 SDU
18 Telephony
1 (A429)
1 (NA)
1 (A429)
NOTE 1: The ADC interface is used as a supplement to FANS required air data that was not supplied by the FMS such as Mach Number and IAS. The ADC interface can still be used to supplement this FMS data in the case the data from the FMS may be invalid or NCD.
NOTE 2: A maximum of six total display devices can be configured at a time, one high-resolution device on each of two high-res ports and up to four low-resolution devices on the low-res port. An RCDU has a separate display processor from the master CDU/MCDU that it is connected to.
NOTE 3: The diagnostic RS-232 port is a dedicated connection and is not a configurable item of the general purpose RS-232/422 serial channels.
NOTE 4: The AirCell ground-based cellular network has been decommissioned by AirCell.
"Iridium/AirCell" equipment will continue to be supported; the "AirCell" only equipment support has been removed.
NOTE 5: UL-80X does not support tip/ring telephony devices (Magnastar, UASC T –T Aero-I, AirCell only). Serial telephony devices are supported (Iridium, UASC T –T Aero-M).
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Installation and Wiring
1. Installation Considerations for UniLink Mounting
The UniLink may be installed inside or outside of the pressure vessel. The UniLink must not be mounted next to excessive heat producing equipment or in such a way as to impede normal convection cooling and it must not be mounted with its rear connector up. The
UniLink may be mounted in any rotational direction in an upright position. The UniLink rack must be grounded to the airframe by use of proper bonding methods. This provides a positive grounding of the rack to which data shields may be connected.
The following wiring diagrams show connections between the UL-801 and other avionics equipment used in typical installations. Refer to the appropriate FMS technical manual for additional required wiring.
These diagrams include our suggested choices for configurable discretes and communications ports but the choice is left up to the discretion of the installer. Mark the configuration worksheets to show your actual installation. Configuration worksheets are found in the System Data Installation section of this manual.
NOTE: The FMS must have SCN 1000.5/1100.5 or later in order to utilize FANS.
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A. UL-801 without FANS to UNS-1C
(1) Sheet 1 of 2
UL-801
(P/N 10801-XX)
MP
ARINC 429
TX #1 (FMS 1)
A 1A
B 1B
ARINC 429
RX #1 (FMS 1)
3
RS-422 DISPLAY
DATA TX #3
A
B
A
B
1C
1D
9A
9B
TP
RS-422 DISPLAY
DATA RX #3
A
B
9C
9D
ARINC 429
TX #2 (FMS 2)
A
B
2A
2B
MP
1
#1 UNS-1C
(P/N 1017-XX-2XX)
A
B
ARINC
429 RX
P1 t
P2
Z r
X
1
A
B
A
B
RS-422
DISPLAY
DATA RX
A
B
RS-422
DISPLAY
DATA TX
1
#2 UNS-1C
(P/N 1017-XX-2XX)
A
B
ARINC
429 RX
ARINC 429
RX #2 (FMS 2)
3
A
B
2C
2D
----CONTINUED----
1
P1
P2
Z
X t r
A
B
HS ARINC
429 TX
A
B
A
B
RS-422
DISPLAY
DATA RX
RS-422
DISPLAY
DATA TX
4
4
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UL-801 Installation Manual
(2) Sheet 2 of 2
UL-801
(P/N 10801XX)
----CONTINUED----
BP
VHF ANTENNA
+28 VDC POWER
POWER GND4
CHASSIS GND3
5
2
20
16
CONFIG
MODULE
TP
DATA CLK
+5 VDC
DATA I/O
11C
11D
12C
24
24
24
GND12D 24
VHF ANTENNA
5A
YELLOW
RED
BLUE
BROWN
+28 VDC
CONFIGURATION
MODULE (P/N 108009)
2
5
DISCRETE INPUT #3
DISCRETE INPUT #4
12B
MP
12C
PARKING BRAKE SET = GND or OPEN
(OPTIONAL, AS REQUIRED)
DOOR n OPEN = GND or OPEN
(OPTIONAL, AS REQUIRED)
6
NOTE: ALL WIRING IS TO BE 22 AWG UNLESS OTHERWISE INDICATED.
1 REFER TO APPLICABLE TECHNICAL MANUAL FOR PORT CONFIGURATIONS AND PIN ASSIGNMENTS.
2
3
4
CONFIGURATION MODULE IS MOUNTED ON THE REAR OF THE UL801 RACK.
IF FMS #1 IS NOT INTERFACED TO THE UL801, THEN CONNECT FMS #2 TO MP1C AND MP1D INSTEAD OF
THE WIRING (MP2C & MP2D) SHOWN ABOVE.
UNS1C, P/N 1017XX2XX, SUPPORTS BOTH UNILINK TEXT AND WEATHER GRAPHICS (RS-422 DISPLAY
DATA). UNS1C, P/N 1017XX1XX, SUPPORTS UNILINK TEXT DISPLAYS ONLY.
5
6
DISCRETE INPUT ACTIVE STATE IS CONFIGURABLE TO EITHER OPEN OR GROUND.
IT IS RECOMMENDED THAT DOOR 1 INPUT DISCRETE BE USED IF ONLY ONE DOOR DISCRETE IS TO BE CONFIGURED.
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UL-801 Installation Manual
B. UL-801 without FANS to UNS-1C+
(1) Sheet 1 of 2
UL-801
(P/N 10801-XX)
MP
ARINC 429
TX #1 (FMS 1)
A 1A
B 1B
ARINC 429
RX #1 (FMS 1)
3
RS-422 DISPLAY
DATA TX #3
A
B
A
B
1C
1D
9A
9B
TP
RS-422 DISPLAY
DATA RX #3
A
B
9C
9D
ARINC 429
TX #2 (FMS 2)
A
B
2A
2B
MP
1
#1 UNS-1C+
(P/N 10172-XX-2XX)
A
B
ARINC
429 RX
P1 r t
P2
Z
X
1
A
B
A
B
RS-422
DISPLAY
DATA RX
A
B
RS-422
DISPLAY
DATA TX
1
#2 UNS-1C+
(P/N 10172-XX-2XX)
A
B
ARINC
429 RX
ARINC 429
RX #2 (FMS 2)
3
A
B
2C
2D
----CONTINUED----
P1 t r
P2
Z
X
1
A
B
HS ARINC
429 TX
A
B
A
B
RS-422
DISPLAY
DATA RX
RS-422
DISPLAY
DATA TX
4
4
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UL-801 Installation Manual
(2) Sheet 2 of 2
UL-801
(P/N 10801-XX)
----CONTINUED---BP
VHF ANTENNA 5
+28 VDC POWER
2
POWER GND4
CHASSIS GND3
20
16
CONFIG
MODULE
TP
DATA CLK
+5 VDC
11C
11D
24
24
DATA I/O 12C 24
GND12D 24
VHF ANTENNA
5A
YELLOW
RED
BLUE
BROWN
+28 VDC
CONFIGURATION
MODULE (P/N 108009)
2
5
DISCRETE INPUT #3
DISCRETE INPUT #4
12B
MP
12C
PARKING BRAKE SET = GND or OPEN
(OPTIONAL, AS REQUIRED)
DOOR n OPEN = GND or OPEN
(OPTIONAL, AS REQUIRED)
6
NOTE: ALL WIRING IS TO BE 22 AWG UNLESS OTHERWISE INDICATED.
1 REFER TO APPLICABLE TECHNICAL MANUAL FOR PORT CONFIGURATIONS AND PIN ASSIGNMENTS.
2
3
4
5
6
CONFIGURATION MODULE IS MOUNTED ON THE REAR OF THE UL801 RACK.
IF FMS #1 IS NOT INTERFACED TO THE UL801, THEN CONNECT FMS #2 TO MP1C AND MP1D INSTEAD OF
THE WIRING (MP2C & MP2D) SHOWN ABOVE.
UNS1C+, P/N 10172XX2XX, SUPPORTS BOTH UNILINK TEXT AND WEATHER GRAPHICS (RS-422 DISPLAY
DATA). UNS1C+, P/N 10172XX1XX, SUPPORTS UNILINK TEXT DISPLAYS ONLY.
DISCRETE INPUT ACTIVE STATE IS CONFIGURABLE TO EITHER OPEN OR GROUND.
IT IS RECOMMENDED THAT DOOR 1 INPUT DISCRETE BE USED IF ONLY ONE DOOR DISCRETE IS TO BE CONFIGURED.
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UL-801 Installation Manual
C. UL-801 without FANS to UNS-1E
(1) Sheet 1 of 2
UL-801
(P/N 10801-XX)
MP
ARINC 429
TX #1 (FMS 1)
A 1A
B 1B
ARINC 429
RX #1 (FMS 1)
3
A
B
RS-422 DISPLAY
DATA TX #3
A
B
RS-422 DISPLAY
DATA RX #3
A
B
1C
1D
9A
9B
TP
9C
9D
1
#1 UNS-1E
(P/N 2017-XX-2XX)
A
B
ARINC
429 RX
P1
P2
Z
X t r
1
A
B
A
B
RS-422
DISPLAY
DATA RX
A
B
RS-422
DISPLAY
DATA TX
ARINC 429
TX #2 (FMS 2)
A
B
2A
2B
MP
ARINC 429
RX #2 (FMS 2)
3
A
B
2C
2D
----CONTINUED----
1
#2 UNS-1E
(P/N 2017-XX-2XX)
A
B
ARINC
429 RX
P1
P2
Z
X t r
1
A
B
HS ARINC
429 TX
A
B
A
B
RS-422
DISPLAY
DATA RX
RS-422
DISPLAY
DATA TX
4
4
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UL-801 Installation Manual
(2) Sheet 2 of 2
UL-801
(P/N 10801-XX)
----CONTINUED----
VHF ANTENNA
+28 VDC POWER
POWER GND4
2
5
CHASSIS GND3
BP
20
16
VHF ANTENNA
5A +28 VDC
CONFIGURATION
MODULE (P/N 108009)
CONFIG
MODULE
TP
DATA CLK
+5 VDC
DATA I/O
11C
11D
12C
24
24
24
GND12D 24
YELLOW
RED
BLUE
BROWN
2
5
DISCRETE INPUT #3
DISCRETE INPUT #4
12B
MP
12C
PARKING BRAKE SET = GND or OPEN
(OPTIONAL, AS REQUIRED)
DOOR n OPEN = GND or OPEN
(OPTIONAL, AS REQUIRED)
6
NOTE: ALL WIRING IS TO BE 22 AWG UNLESS OTHERWISE INDICATED.
1 REFER TO APPLICABLE TECHNICAL MANUAL FOR PORT CONFIGURATIONS AND PIN ASSIGNMENTS.
2
3
4
CONFIGURATION MODULE IS MOUNTED ON THE REAR OF THE UL801 RACK.
IF FMS #1 IS NOT INTERFACED TO THE UL801, THEN CONNECT FMS #2 TO MP1C AND MP1D INSTEAD OF
THE WIRING (MP2C & MP2D) SHOWN ABOVE.
UNS1E, P/N 2017XX2XX, SUPPORTS BOTH UNILINK TEXT AND WEATHER GRAPHICS (RS-422 DISPLAY
DATA). UNS1E, P/N 2017XX1XX, SUPPORTS UNILINK TEXT DISPLAYS ONLY.
5
6
DISCRETE INPUT ACTIVE STATE IS CONFIGURABLE TO EITHER OPEN OR GROUND.
IT IS RECOMMENDED THAT DOOR 1 OPEN DISCRETE BE USED IF ONLY ONE DOOR DISCRETE IS TO BE CONFIGURED.
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UL-801 Installation Manual
D. UL-801 without FANS to UNS-1Csp
(1) Sheet 1 of 2
UL-801
(P/N 10801-XX)
MP
ARINC 429
TX #1 (FMS 1)
A
B
1A
1B
ARINC 429
RX #1 (FMS 1)
3
A
B
RS-422 DISPLAY
DATA TX #3
A
B
1C
1D
9A
9B
TP
RS-422 DISPLAY
DATA RX #3
A
B
9C
9D
1
#1 UNS-1Csp
(P/N 1019-XX-2XX)
A
B
ARINC
429 RX
P2
50
49
1
A
B
A
B
RS-422
DISPLAY
DATA RX
48
47
A
B
RS-422
DISPLAY
DATA TX
4
ARINC 429
TX #2 (FMS 2)
A
B
2A
2B
MP
ARINC 429
RX #2 (FMS 2)
3
A
B
2C
2D
1
#2 UNS-1Csp
(P/N 1019-XX-2XX)
A
B
ARINC
429 RX
P2
50
49
1
48
47
A
B
HS ARINC
429 TX
A
B
RS-422
DISPLAY
DATA RX
A
B
RS-422
DISPLAY
DATA TX
4
----CONTINUED----
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UL-801 Installation Manual
(2) Sheet 2 of 2
UL-801
(P/N 10801-XX)
----CONTINUED----
BP
VHF ANTENNA
+28 VDC POWER
POWER GND4
5
2
CHASSIS GND3
CONFIG
MODULE
TP
DATA CLK
+5 VDC
11C
11D
24
24
DATA I/O 12C 24
GND12D 24
20
20
16
VHF ANTENNA
5A
YELLOW
RED
BLUE
BROWN
+28 VDC
CONFIGURATION
MODULE (P/N 108009)
2
12B
MP
5
DISCRETE INPUT #3
DISCRETE INPUT #4 12C
PARKING BRAKE SET = GND or OPEN
(OPTIONAL, AS REQUIRED)
DOOR n OPEN = GND or OPEN
(OPTIONAL, AS REQUIRED)
6
NOTE: ALL WIRING IS TO BE 22 AWG UNLESS OTHERWISE INDICATED.
1 REFER TO APPLICABLE TECHNICAL MANUAL FOR PORT CONFIGURATIONS AND PIN ASSIGNMENTS.
2
3
4
CONFIGURATION MODULE IS MOUNTED ON THE REAR OF THE UL801 RACK.
IF FMS #1 IS NOT INTERFACED TO THE UL801, THEN CONNECT FMS #2 TO MP1C AND MP1D INSTEAD OF
THE WIRING (MP2C & MP2D) SHOWN ABOVE.
UNS1Csp, P/N 1019XX2XX, SUPPORTS BOTH UNILINK TEXT AND WEATHER GRAPHICS (RS-422 DISPLAY
DATA). UNS1Csp, P/N 1019XX1XX, SUPPORTS UNILINK TEXT DISPLAYS ONLY.
5
6
DISCRETE INPUT ACTIVE STATE IS CONFIGURABLE TO EITHER OPEN OR GROUND.
IT IS RECOMMENDED THAT DOOR 1 OPEN DISCRETE BE USED IF ONLY ONE DOOR DISCRETE IS TO BE CONFIGURED.
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UL-801 Installation Manual
E. UL-801 without FANS to UNS-1Esp
(1) Sheet 1 of 2
UL-801
(P/N 10801-XX)
MP
ARINC 429
TX #1 (FMS 1)
A
B
1A
1B
ARINC 429
RX #1 (FMS 1)
3
A
B
RS-422 DISPLAY
DATA TX #3
A
B
1C
1D
9A
9B
TP
RS-422 DISPLAY
DATA RX #3
A
B
9C
9D
1
#1 UNS-1Esp
(P/N 2019-XX-2XX)
A
B
ARINC
429 RX
P2
50
49
1
A
B
A
B
RS-422
DISPLAY
DATA RX
48
47
A
B
RS-422
DISPLAY
DATA TX
4
ARINC 429
TX #2 (FMS 2)
A
B
2A
2B
MP
ARINC 429
RX #2 (FMS 2)
3
A
B
2C
2D
----CONTINUED----
1
#2 UNS-1Esp
(P/N 2019-XX-2XX)
A
B
ARINC
429 RX
P2
50
49
1
A
B
HS ARINC
429 TX
A
B
RS-422
DISPLAY
DATA RX
48
47
A
B
RS-422
DISPLAY
DATA TX
4
Page 310
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UL-801 Installation Manual
(2) Sheet 2 of 2
UL-801
(P/N 10801-XX)
----CONTINUED----
BP
VHF ANTENNA
+28 VDC POWER
POWER GND4
5
2
CHASSIS GND3
20
16
CONFIG
MODULE
TP
DATA CLK
+5 VDC
11C
11D
24
24
DATA I/O 12C 24
GND12D 24
VHF ANTENNA
5A
YELLOW
RED
BLUE
BROWN
+28 VDC
CONFIGURATION
MODULE (P/N 108009)
2
5
DISCRETE INPUT #3
DISCRETE INPUT #4
12B
MP
12C
PARKING BRAKE SET = GND or OPEN
(OPTIONAL, AS REQUIRED)
DOOR n OPEN = GND or OPEN
(OPTIONAL, AS REQUIRED)
6
NOTE: ALL WIRING IS TO BE 22 AWG UNLESS OTHERWISE INDICATED.
1 REFER TO APPLICABLE TECHNICAL MANUAL FOR PORT CONFIGURATIONS AND PIN ASSIGNMENTS.
2
3
4
CONFIGURATION MODULE IS MOUNTED ON THE REAR OF THE UL801 RACK.
IF FMS #1 IS NOT INTERFACED TO THE UL801, THEN CONNECT FMS #2 TO MP1C AND MP1D INSTEAD OF
THE WIRING (MP2C & MP2D) SHOWN ABOVE.
UNS1Esp, P/N 2019XX2XX, SUPPORTS BOTH UNILINK TEXT AND WEATHER GRAPHICS (RS-422 DISPLAY
DATA). UNS1Esp, P/N 2019XX1XX, SUPPORTS UNILINK TEXT DISPLAYS ONLY.
5
6
DISCRETE INPUT ACTIVE STATE IS CONFIGURABLE TO EITHER OPEN OR GROUND.
IT IS RECOMMENDED THAT DOOR 1 OPEN DISCRETE BE USED IF ONLY ONE DOOR DISCRETE IS TO BE CONFIGURED.
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UL-801 Installation Manual
F. UL-801 without FANS to UNS-1D
(1) Sheet 1 of 2
VHF ANTENNA
UL-801
(P/N 10801-XX)
VHF ANTENNA
+28 VDC POWER
POWER GND4
5
2
BP
20
20
5A
CHASSIS GND3 16
+28 VDC
CONFIGURATION
MODULE (P/N 108009)
6
CONFIG
MODULE
TP
DATA CLK
+5 VDC
11C
11D
24
24
DATA I/O 12C 24
GND12D 24
DISCRETE INPUT #3
DISCRETE INPUT #4
12B
MP
12C
YELLOW
RED
BLUE
BROWN
PARKING BRAKE SET = GND or OPEN
(OPTIONAL, AS REQUIRED)
DOOR n OPEN = GND or OPEN
(OPTIONAL, AS REQUIRED)
7
ARINC 429 TX #1
(FMS 1)
A
B
1A
1B
1
#1 UNS-1D
(P/N 1192-X0-111XXX)
A
B
ARINC 429
RX
ARINC 429 RX #1
(FMS 1)
3
A
B
1C
1D
1
A
B
HS ARINC 429
TX
ARINC 429 TX #2
(FMS 2)
A
B
2A
2B
MP
ARINC 429 RX #2
(FMS 2)
3
A
B
----CONTINUED----
2C
2D
1
A
#2 UNS-1D
(P/N 1192-X0-111XXX)
ARINC 429
RX
B
1
A
B
HS ARINC 429
TX
Page 312
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UL-801 Installation Manual
(2) Sheet 2 of 2 - 4/5” FPCDU/MCDU
UL-801
(P/N 10801-XX)
----CONTINUED----
RS-422 DISPLAY
DATA TX #3
A
B
9A
9B
TP
RS-422 DISPLAY
DATA RX #3
A
B
9C
9D
P3
E
4
F
A
B
#1 4"/5 FPCDU/MCDU
(P/N 1117-X-X1X,
P/N 1018-X-X1X,
P/N 1025-XX-XXX)
RS-422
DISPLAY
DATA RX
5
B
C
D
P3
E
F
4
A
B
RS-422
DISPLAY
DATA TX
SHIELD GND
#2 4"/5 FPCDU/MCDU
(P/N 1117-X-X1X,
P/N 1018-X-X1X,
P/N 1025-XX-XXX)
A
B
RS-422
DISPLAY
DATA RX
5
B
C
D
A
B
RS-422
DISPLAY
DATA TX
SHIELD GND
8 NOTE: ALL WIRING IS TO BE 22 AWG UNLESS OTHERWISE INDICATED.
1
2
3
4
5
6
7
8
REFER TO APPLICABLE TECHNICAL MANUAL FOR PORT CONFIGURATIONS AND PIN ASSIGNMENTS.
CONFIGURATION MODULE IS MOUNTED ON THE REAR OF THE UL801 RACK.
IF FMS #1 IS NOT INTERFACED TO THE UL801, THEN CONNECT FMS #2 TO MP1C AND MP1D INSTEAD OF
THE WIRING (MP2C & MP2D) SHOWN ABOVE.
THE P3 CONNECTOR IS AMPHENOL P/N MS27473T12F8SC AND IS INCLUDED IN THE APPROPRIATE
UNS-1D INSTALLATION KIT.
THE 5 FPCDU, P/N 1018-2-X10, SUPPORTS BOTH UNILINK TEXT AND WEATHER GRAPHICS (RS-422 DISPLAY
DATA). OTHER 5 FPCDUs, P/N 1018-X-X00, SUPPORT UNILINK TEXT ONLY DISPLAYS.
DISCRETE INPUT ACTIVE STATE IS CONFIGURABLE TO EITHER OPEN OR GROUND.
IT IS RECOMMENDED THAT DOOR 1 OPEN DISCRETE BE USED IF ONLY ONE DOOR DISCRETE IS TO BE CONFIGURED.
BOTH 4 AND 5 FPCDUs ARE WIRED IN THE SAME MANNER.
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UL-801 Installation Manual
G. UL-801 without FANS to UNS-1D+
(1) Sheet 1 of 2
6
UL-801
(P/N 10801-XX)
VHF ANTENNA
+28 VDC POWER
POWER GND4
CHASSIS GND3
5
2
BP
20
20
16
VHF ANTENNA
5A
CONFIG
MODULE
TP
DATA CLK
+5 VDC
11C
11D
24
24
DATA I/O 12C 24
GND12D 24
YELLOW
RED
BLUE
BROWN
DISCRETE INPUT #3
DISCRETE INPUT #4
ARINC 429 TX #1
(FMS 1)
A
B
12B
MP
12C
1A
1B
3
+28 VDC
CONFIGURATION
MODULE (P/N 108009)
(OPTIONAL, AS REQUIRED)
DOOR n OPEN = GND or OPEN
(OPTIONAL, AS REQUIRED)
7
2
PARKING BRAKE SET = GND or OPEN
1
#1 UNS-1D+
(P/N 11922-X0-111XXX)
A
ARINC 429 RX
B
ARINC 429 RX #1
3
(FMS 1)
A
B
1C
1D
1
A
B
HS ARINC 429 TX
ARINC 429 TX #2
3
(FMS 2)
ARINC 429 RX #2
(FMS 2)
----CONTINUED----
A
B
A
B
2A
2B
MP
2C
2D
1
#2 UNS-1D+
(P/N 11922-X0-111XXX)
A
ARINC 429 RX
B
1
A
B
HS ARINC 429 TX
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UL-801 Installation Manual
(2) Sheet 2 of 2 - 4/5” FPCDU/MCDU
UL-801
(P/N 10801-XX)
----CONTINUED----
TP
RS-422 DISPLAY
DATA TX #3
A
B
9A
9B
P3
4
E
F
#1 4"/5 FPCDU/MCDU
(P/N 1117-X-X1X,
P/N 1018-X-X1X,
P/N 1025-XX-XXX)
A
B
RS-422
DISPLAY
DATA RX
5
RS-422 DISPLAY
DATA RX #3
A
B
9C
9D
A
B
B
C
D
P3
4
E
F
A
B
RS-422
DISPLAY
DATA TX
SHIELD GND
A
B
#2 4"/5 FPCDU/MCDU
(P/N 1117-X-X1X,
P/N 1018-X-X1X,
P/N 1025-XX-XXX)
RS-422
DISPLAY
DATA RX
5
B
C
D
A
B
RS-422
DISPLAY
DATA TX
NOTE: ALL WIRING IS TO BE 22 AWG UNLESS OTHERWISE INDICATED.
SHIELD GND
8
1
2
3
4
5
6
7
8
REFER TO APPLICABLE TECHNICAL MANUAL FOR PORT CONFIGURATIONS AND PIN ASSIGNMENTS.
CONFIGURATION MODULE IS MOUNTED ON THE REAR OF THE UL801 RACK.
IF FMS #1 IS NOT INTERFACED TO THE UL801, THEN CONNECT FMS #2 TO MP1C AND MP1D INSTEAD OF
THE WIRING (MP2C & MP2D) SHOWN ABOVE.
THE P3 CONNECTOR IS AMPHENOL P/N MS27473T12F8SC AND IS INCLUDED IN THE APPROPRIATE
UNS-1D+ INSTALLATION KIT.
THE 5 FPCDU, P/N 1018-2-X10, SUPPORTS BOTH UNILINK TEXT AND WEATHER GRAPHICS (RS-422 DISPLAY
DATA). OTHER 5 FPCDUs, P/N 1018-X-X00, SUPPORT UNILINK TEXT ONLY DISPLAYS.
DISCRETE INPUT ACTIVE STATE IS CONFIGURABLE TO EITHER OPEN OR GROUND.
IT IS RECOMMENDED THAT DOOR 1 OPEN DISCRETE BE USED IF ONLY ONE DOOR DISCRETE IS TO BE CONFIGURED.
BOTH 4 AND 5 FPCDUs ARE WIRED IN THE SAME MANNER.
Page 315
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UL-801 Installation Manual
H. UL-801 without FANS to UNS-1F
(1) Sheet 1 of 2
UL-801
(P/N 10801-XX)
VHF ANTENNA
+28 VDC POWER
POWER GND4
CHASSIS GND3
5
2
BP
20
20
16
VHF ANTENNA
5A
CONFIG
MODULE
TP
DATA CLK
+5 VDC
DATA I/O
11C
11D
12C
GND12D 24
24
24
24
YELLOW
RED
BLUE
BROWN
6
DISCRETE INPUT #3
DISCRETE INPUT #4
ARINC 429 TX #1
(FMS 1)
A
B
12B
MP
12C
1A
1B
+28 VDC
CONFIGURATION MODULE
(P/N 108009)
PARKING BRAKE SET = GND or OPEN
(OPTIONAL, AS REQUIRED)
DOOR n OPEN = GND or OPEN
(OPTIONAL, AS REQUIRED)
7
2
1
A
#1 UNS-1F
(P/N 2192-X0-111XXX)
ARINC 429 RX
B
ARINC 429 RX #1
3
(FMS 1)
A
B
1C
1D
1
A
B
HS ARINC 429 TX
ARINC 429 TX #2
(FMS 2)
ARINC 429 RX #2
(FMS 2)
3
A
B
A
B
2A
2B
2C
2D
MP
1
A
#2 UNS-F
(P/N 2192-X0-111XXX)
ARINC 429 RX
B
1
A
B
HS ARINC 429 TX
----CONTINUED----
Page 316
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UL-801 Installation Manual
(2) Sheet 2 of 2 - 4/5” FPCDU/MCDU
UL-801
(P/N 10801-XX)
----CONTINUED----
RS-422 DISPLAY
DATA TX #3
A
B
9A
9B
TP P3
4
E
F
A
B
#1 4"/5 FPCDU/MCDU
(P/N 1117-X-X1X,
P/N 1018-X-X1X,
P/N 1025-XX-XXX)
RS-422
DISPLAY
DATA RX
5
RS-422 DISPLAY
DATA RX #3
A
B
9C
9D
B
C
D
P3
4
E
F
A
B
RS-422
DISPLAY
DATA TX
SHIELD GND
#2 4"/5 FPCDU/MCDU
(P/N 1117-X-X1X,
P/N 1018-X-X1X,
P/N 1025-XX-XXX)
A
B
RS-422
DISPLAY
DATA RX
5
B
C
D
NOTE: ALL WIRING IS TO BE 22 AWG UNLESS OTHERWISE INDICATED.
1
2
3
4
5
REFER TO APPLICABLE TECHNICAL MANUAL FOR PORT CONFIGURATIONS AND PIN ASSIGNMENTS.
CONFIGURATION MODULE IS MOUNTED ON THE REAR OF THE UL801 RACK.
IF FMS #1 IS NOT INTERFACED TO THE UL801, THEN CONNECT FMS #2 TO MP1C AND MP1D INSTEAD OF
THE WIRING (MP2C & MP2D) SHOWN ABOVE.
THE P3 CONNECTOR IS AMPHENOL P/N MS27473T12F8SC AND IS INCLUDED IN THE APPROPRIATE
UNS-1D+ INSTALLATION KIT.
THE 5 FPCDU, P/N 1018-2-X10, SUPPORTS BOTH UNILINK TEXT AND WEATHER GRAPHICS (RS-422 DISPLAY
DATA). OTHER 5 FPCDUs, P/N 1018-X-X00, SUPPORT UNILINK TEXT ONLY DISPLAYS.
6
7
DISCRETE INPUT ACTIVE STATE IS CONFIGURABLE TO EITHER OPEN OR GROUND.
IT IS RECOMMENDED THAT DOOR 1 OPEN DISCRETE BE USED IF ONLY ONE DOOR DISCRETE IS TO BE CONFIGURED.
8 BOTH 4 AND 5 FPCDUs ARE WIRED IN THE SAME MANNER.
A
B
RS-422
DISPLAY
DATA TX
SHIELD GND
8
Page 317
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UL-801 Installation Manual
I. UL-801 without FANS to UNS-1K
(1) Sheet 1 of 2
VHF ANTENNA
UL-801
(P/N 10801-XX)
BP
VHF ANTENNA
+28 VDC INPUT
POWER GND4
CHASSIS GND3
5
2
CONFIG
MODULE
DATA CLK
+5 VDC
DATA I/O
GND
11C
11D
12C
12D
TP
24
24
24
24
20
20
16
3
YELLLOW
RED
BLUE
BROWN
+28 VDC
CONFIGURATION
MODULE (P/N 10651)
2
DISCRETE INPUT #3
12B
5
DISCRETE INPUT #4 12C
MP
PARKING BRAKE SET = GND or OPEN
(OPTIONAL, AS REQUIRED)
DOOR n OPEN = GND or OPEN
(OPTIONAL, AS REQUIRED) 6
ARINC 429 Tx #1
(FMS 1)
A
B
1A
1B
1
#1 UNS-1K
(P/N 1116-XX-111X)
A
B
ARINC
429 Rx
4
ARINC 429 Rx #1
3
(FMS 1)
A
B
1C
1D
1
A
B
HS ARINC
429 Tx
ARINC 429 Tx #2
(FMS 2)
A
B
2A
2B
MP
ARINC 429 Rx #2
3
(FMS 2)
A
B
2C
2D
1
#2 UNS-1K
(P/N 1116-XX-111X)
A
B
ARINC
429 Rx
4
1
A
B
HS ARINC
429 Tx
----CONTINUED----
Page 318
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15 December 2011
(2) Sheet 2 of 2
UL-801
(P/N 10801-XX)
----CONTINUED----
RS-422 DISPLAY
DATA TX #3
A
B
9A
9B
TP
RS-422 DISPLAY
DATA RX #3
A
B
9C
9D
UL-801 Installation Manual
P3
E
4
F
#1 4" FPCDU/MCDU
(P/N 1117-X-X1X)
A
B
RS-422
DISPLAY
DATA RX
B
C
D
A
B
RS-422
DISPLAY
DATA TX
SHIELD GND
P3
E
F
4
A
B
#2 4" FPCDU/MCDU
(P/N 1117-X-X1X)
RS-422
DISPLAY
DATA RX
B
C
D
A
B
RS-422
DISPLAY
DATA TX
SHIELD GND
NOTE: ALL WIRING IS TO BE 22 AWG UNLESS OTHERWISE INDICATED.
1
2
3
4
5
6
REFER TO APPLICABLE TECHNICAL MANUAL FOR PORT CONFIGURATIONS AND PIN ASSIGNMENTS.
CONFIGURATION MODULE IS MOUNTED ON THE REAR OF THE UL801 RACK.
IF FMS #1 IS NOT INTERFACED TO THE UL801, THEN CONNECT FMS #2 TO MP1C AND MP1D INSTEAD OF
THE WIRING (MP2C & MP2D) SHOWN ABOVE.
THE P3 CONNECTOR IS AMPHENOL P/N MS27473T12F8SC AND IS INCLUDED IN THE APPROPRIATE
UNS-1K INSTALLATION KIT.
DISCRETE INPUT ACTIVE STATE IS CONFIGURABLE TO EITHER OPEN OR GROUND.
IT IS RECOMMENDED THAT DOOR 1 OPEN DISCRETE BE USED IF ONLY ONE DOOR DISCRETE IS TO BE CONFIGURED.
Page 319
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UL-801 Installation Manual
J. UL-801 without FANS to UNS-1K+
(1) Sheet 1 of 2
VHF ANTENNA
UL-801
(P/N 10801-XX)
VHF ANTENNA
+28 VDC POWER
POWER GND 4
CHASSIS GND3
5
2
CONFIG
MODULE
DATA CLK
+5 VDC
DATA I/O
GND
BP
11C
11D
12C
12D
TP
24
24
24
24
20
20
16
5A
YELLLOW
RED
BLUE
BROWN
+28 VDC
CONFIGURATION
MODULE (P/N 108009)
2
DISCRETE INPUT #3
5
DISCRETE INPUT #4
12B
12C
MP
ARINC 429 TX #1
(FMS 1)
A
B
1A
1B
PARKING BRAKE SET = GND or OPEN
(OPTIONAL, AS REQUIRED)
DOOR n OPEN = GND or OPEN
(OPTIONAL, AS REQUIRED)
6
1
#1 UNS-1K+
(P/N 11162-XX-111X)
A
B
ARINC
429 RX
4
ARINC 429 RX #1
(FMS 1)
3
A
B
1C
1D
1
A
B
HS ARINC
429 TX
ARINC 429 TX #2
(FMS 2)
A
B
2A
2B
MP
ARINC 429 RX #2
3
(FMS 2)
A
B
2C
2D
----CONTINUED----
1
#2 UNS-1K+
(P/N 11162-XX-111X)
A
B
ARINC
429 RX
4
1
A
B
HS ARINC
429 TX
NOTE: ALL WIRING IS TO BE 22 AWG UNLESS OTHERWISE INDICATED.
1 REFER TO APPLICABLE TECHNICAL MANUAL FOR PORT CONFIGURATIONS AND PIN ASSIGNMENTS.
2
3
4
5
6
CONFIGURATION MODULE IS MOUNTED ON THE REAR OF THE UL801 RACK.
IF FMS #1 IS NOT INTERFACED TO THE UL801, THEN CONNECT FMS #2 TO MP1C AND MP1D INSTEAD OF
THE WIRING (MP2C & MP2D) SHOWN ABOVE.
UNS1K+ SUPPORTS UNILINK TEXT ONLY (NO GRAPHICS).
DISCRETE INPUT ACTIVE STATE IS CONFIGURABLE TO EITHER OPEN OR GROUND.
IT IS RECOMMENDED THAT DOOR 1 OPEN DISCRETE BE USED IF ONLY ONE DOOR DISCRETE IS TO BE CONFIGURED.
Page 320
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15 December 2011
(2) Sheet 2 of 2
UL-801
(P/N 10801-XX)
----CONTINUED----
RS-422 DISPLAY
DATA TX #3
A
B
9A
9B
TP
RS-422 DISPLAY
DATA RX #3
A
B
9C
9D
UL-801 Installation Manual
P3
E
4
F
#1 4" FPCDU/MCDU
(P/N 1117-X-X1X)
A
B
RS-422
DISPLAY
DATA RX
B
C
D
A
B
RS-422
DISPLAY
DATA TX
SHIELD GND
P3
4
E
F
A
B
#2 4" FPCDU/MCDU
(P/N 1117-X-X1X)
RS-422
DISPLAY
DATA RX
B
C
D
A
B
RS-422
DISPLAY
DATA TX
SHIELD GND
NOTE: ALL WIRING IS TO BE 22 AWG UNLESS OTHERWISE INDICATED.
1
2
3
4
5
6
REFER TO APPLICABLE TECHNICAL MANUAL FOR PORT CONFIGURATIONS AND PIN ASSIGNMENTS.
CONFIGURATION MODULE IS MOUNTED ON THE REAR OF THE UL801 RACK.
IF FMS #1 IS NOT INTERFACED TO THE UL801, THEN CONNECT FMS #2 TO MP1C AND MP1D INSTEAD OF
THE WIRING (MP2C & MP2D) SHOWN ABOVE.
THE P3 CONNECTOR IS AMPHENOL P/N MS27473T12F8SC AND IS INCLUDED IN THE APPROPRIATE
UNS-1K INSTALLATION KIT.
DISCRETE INPUT ACTIVE STATE IS CONFIGURABLE TO EITHER OPEN OR GROUND.
IT IS RECOMMENDED THAT DOOR 1 OPEN DISCRETE BE USED IF ONLY ONE DOOR DISCRETE IS TO BE CONFIGURED.
Page 321
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15 December 2011
UL-801 Installation Manual
K. UL-801 without FANS to UNS-1L
VHF ANTENNA
UL-801
(P/N 10801-XX)
VHF ANTENNA
+28 VDC POWER
POWER GND 4
CHASSIS GND3
2
5
BP
20
20
16
5A
+28 VDC
CONFIGURATION
MODULE (P/N 108009)
CONFIG
MODULE
DATA CLK
+5 VDC
DATA I/O
GND
11C
11D
12C
12D
TP
24
24
24
24
YELLLOW
RED
BLUE
BROWN
2
5
DISCRETE INPUT #3
DISCRETE INPUT #4
12B
12C
MP
ARINC 429 TX #1
(FMS 1)
A
B
1A
1B
PARKING BRAKE SET = GND or OPEN
(OPTIONAL, AS REQUIRED)
DOOR n OPEN = GND or OPEN
(OPTIONAL, AS REQUIRED)
6
1
#1 UNS-1L
(P/N 2116-XX-111X)
A
B
ARINC
429 RX
4
ARINC 429 RX #1
3
(FMS 1)
A
B
1C
1D
1
A
B
HS ARINC
429 TX
ARINC 429 TX #2
(FMS 2)
A
B
2A
2B
MP
ARINC 429 RX #2
3
(FMS 2)
A
B
2C
2D
1
#2 UNS-1L
(P/N 2116-XX-111X)
A
B
ARINC
429 RX
4
1
A
B
HS ARINC
429 TX
NOTE: ALL WIRING IS TO BE 22 AWG UNLESS OTHERWISE INDICATED.
1 REFER TO APPLICABLE TECHNICAL MANUAL FOR PORT CONFIGURATIONS AND PIN ASSIGNMENTS.
2
3
4
5
6
CONFIGURATION MODULE IS MOUNTED ON THE REAR OF THE UL801 RACK.
IF FMS #1 IS NOT INTERFACED TO THE UL801, THEN CONNECT FMS #2 TO MP1C AND MP1D INSTEAD OF
THE WIRING (MP2C & MP2D) SHOWN ABOVE.
UNS1L SUPPORTS UNILINK TEXT ONLY (NO GRAPHICS).
DISCRETE INPUT ACTIVE STATE IS CONFIGURABLE TO EITHER OPEN OR GROUND.
IT IS RECOMMENDED THAT DOOR 1 OPEN DISCRETE BE USED IF ONLY ONE DOOR DISCRETE IS TO BE CONFIGURED.
Page 322
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15 December 2011
UL-801 Installation Manual
L. UL-801 to UNS-1Ew
(1) Sheet 1 of 2
NOTE: The FMS must be SCN 1005.5/1100.5 or later to support FANS.
UL-801
(P/N 10801-XX)
ARINC 429
TX #1 (FMS 1)
A
B
1A
1B
MP
1
#1 UNS-1Ew
(P/N 3017-XX-2XX)
A
B
ARINC
429 RX
ARINC 429
RX #1 (FMS 1)
3
RS-422 DISPLAY
DATA TX #3
A
B
4
RS-422 DISPLAY
DATA RX #3
A
B
A
B
1C
1D
9A
9B
TP
9C
9D
P1
P2
Z
W t r
1
A
B
A
B
RS-422
DISPLAY
DATA RX
A
B
RS-422
DISPLAY
DATA TX
ARINC 429
TX #2 (FMS 2)
A
B
2A
2B
MP
1
#2 UNS-1Ew
(P/N 3017-XX-2XX)
A
B
ARINC
429 RX
ARINC 429
RX #2 (FMS 2)
3
A
B
2C
2D
1
P1
P2
Z
W t r
A
B
A
B
A
B
HS ARINC
429 TX
RS-422
DISPLAY
DATA RX
RS-422
DISPLAY
DATA TX
2
2
5
7 DISCRETE OUTPUT
6
8 DISCRETE OUTPUT 6
10
DISCRETE OUTPUT 6
9
+28 VDC
11
CPDLC
CNECT
15
----CONTINUED----
Page 323
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UL-801 Installation Manual
(2) Sheet 2 of 2
UL-801
(P/N 10801-XX)
----CONTINUED----
VHF ANTENNA
+28 VDC POWER
5
2
POWER GND4
CHASSIS GND3
BP
20
16
VHF ANTENNA
5A +28 VDC
CONFIGURATION
MODULE (P/N 108009)
CONFIG
MODULE
DATA CLK
+5 VDC
DATA I/O
GND
11C
11D
12C
12D
TP
24
24
24
24
YELLOW
RED
BLUE
BROWN
12
DISCRETE INPUT #3
13
DISCRETE INPUT #4
12B
MP
12C
PARKING BRAKE SET = GND or OPEN
(OPTIONAL, AS REQUIRED)
DOOR n OPEN = GND or OPEN
(OPTIONAL, AS REQUIRED) 14
NOTES: ALL WIRING IS TO BE 22 AWG UNLESS OTHERWISE INDICATED.
THE FMS MUST BE SCN 1000.5/1100.5 OR LATER TO SUPPORT FANS.
1
2
REFER TO APPLICABLE TECHNICAL MANUAL FOR PORT CONFIGURATIONS AND PIN ASSIGNMENTS.
UNS1Ew SUPPORTS BOTH UNILINK TEXT AND WEATHER GRAPHICS USING RS-422 DISPLAY DATA.
IF FMS #1 IS NOT INTERFACED TO THE UL801, THEN CONNECT FMS #2 TO MP1C AND MP1D IN LIEU OF MP2C AND MP2D SHOWN ABOVE.
3
4 CONFIGURE: SERIAL LOW RESOLUTION DISPLAY.
WHITE ATC LETTERING RECOMMENDED. USE ANNUNCIATOR P/N EATON 582-10 A0 B0 C3 F4 L5 N1 (D) P12,12 ATC OR EQUIVALENT.
5
6 ANY AVAILABLE DISCRETE OUTPUT PIN MAY BE USED.
CONFIGURE DISCRETE OUTPUT FOR FANS VISUAL.
7
8 CONFIGURE DISCRETE OUTPUT FOR FANS AURAL.
9 CONNECT TO AN AURAL ALERTING DEVICE OR AN AURAL WARNING GENERATOR. USE SONALERT P/N SCE028LD2TT1B OR EQUIVALENT.
10
OPTIONAL: CONFIGURE DISCRETE OUTPUT FOR CPDLC CNECT (CONNECT).
11
OPTIONAL: CPDLC CNECT ANNUNCIATOR. LABEL AS REQUIRED.
12
CONFIGURATION MODULE IS MOUNTED ON THE REAR OF THE UL801 RACK.
13
14
DISCRETE INPUT ACTIVE STATE IS CONFIGURABLE TO EITHER OPEN OR GROUND.
IT IS RECOMMENDED THAT DOOR 1 OPEN DISCRETE BE USED IF ONLY ONE DOOR DISCRETE IS TO BE CONFIGURED.
15
WIRING WITHIN THE DASHED LINES APPLIES ONLY WITH FANS ENABLED.
Page 324
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15 December 2011
UL-801 Installation Manual
M. UL-801 to UNS-1Espw
(1) Sheet 1 of 2
NOTE: The FMS must be SCN 1000.5/1100.5 or later to support FANS.
UL-801
(P/N 10801-XX)
MP
ARINC 429
TX #1 (FMS 1)
A
B
1A
1B
1
A
B
ARINC
429 RX
ARINC 429
RX #1 (FMS 1)
3
A
B
RS-422 DISPLAY
DATA TX #3
15
RS-422 DISPLAY
DATA RX #3
A
B
A
B
1C
1D
9A
9B
TP
9C
9D
P2
50
49
1
A
B
A
B
RS-422
DISPLAY
DATA RX
48
47
A
B
RS-422
DISPLAY
DATA TX
ARINC 429
TX #2 (FMS 2)
A
B
2A
2B
MP
ARINC 429
RX #2 (FMS 2)
3
A
B
2C
2D
1
#2 UNS-1Espw
(P/N 3019-XX-2XX)
A
B
ARINC
429 RX
P2
50
49
48
47
1
A
B
HS ARINC
429 TX
A
B
RS-422
DISPLAY
DATA RX
A
B
RS-422
DISPLAY
DATA TX
2
2
4
6 DISCRETE OUTPUT 5
7 DISCRETE OUTPUT 5
9 DISCRETE OUTPUT 5
----CONTINUED----
8
+28 VDC
10
CPDLC
CNECT
14
Page 325
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UL-801 Installation Manual
(2) Sheet 2 of 2
UL-801
(P/N 10801-XX)
----CONTINUED----
VHF ANTENNA
+28 VDC POWER
POWER GND4
5
2
CHASSIS GND3
BP
20
16
VHF ANTENNA
5A +28 VDC
CONFIGURATION
MODULE (P/N 108009)
CONFIG
MODULE
DATA CLK
+5 VDC
DATA I/O
GND
11C
11D
12C
12D
TP
24
24
24
24
YELLOW
RED
BLUE
BROWN
11
12
DISCRETE INPUT #3
DISCRETE INPUT #4
12B
MP
12C
PARKING BRAKE SET = GND or OPEN
(OPTIONAL, AS REQUIRED)
DOOR n OPEN = GND or OPEN
(OPTIONAL, AS REQUIRED) 13
NOTES: ALL WIRING IS TO BE 22 AWG UNLESS OTHERWISE INDICATED.
THE FMS MUST BE SCN 1000.5/1100.5 OR LATER TO SUPPORT FANS.
4
5
1
2
3
REFER TO APPLICABLE TECHNICAL MANUAL FOR PORT CONFIGURATIONS AND PIN ASSIGNMENTS.
UNS1Espw SUPPORTS BOTH UNILINK TEXT AND WEATHER GRAPHICS USING RS-422 DISPLAY DATA.
IF FMS #1 IS NOT INTERFACED TO THE UL801, THEN CONNECT FMS #2 TO MP1C AND MP1D INSTEAD OF THE
WIRING (MP2C & MP2D) SHOWN ABOVE.
WHITE ATC LETTERING RECOMMENDED. USE ANNUNCIATOR P/N EATON 582-10 A0 B0 C3 F4 L5 N1 (D) P12,12 ATC OR EQUIVALENT.
ANY AVAILABLE DISCRETE OUTPUT PIN MAY BE USED.
13
14
11
12
8
9
6
7
10
CONFIGURE DISCRETE OUTPUT FOR FANS VISUAL.
CONFIGURE DISCRETE OUTPUT FOR FANS AURAL.
CONNECT TO AN AURAL ALERTING DEVICE OR AN AURAL WARNING GENERATOR. USE SONALERT P/N SCE028LD2TT1B OR EQUIVALENT.
OPTIONAL: CONFIGURE DISCRETE OUTPUT FOR CPDLC CNECT (CONNECT).
OPTIONAL: CPDLC CNECT ANNUNCIATOR. LABEL AS REQUIRED.
CONFIGURATION MODULE IS MOUNTED ON THE REAR OF THE UL801 RACK.
DISCRETE INPUT ACTIVE STATE IS CONFIGURABLE TO EITHER OPEN OR GROUND.
IT IS RECOMMENDED THAT DOOR 1 OPEN DISCRETE BE USED IF ONLY ONE DOOR DISCRETE IS TO BE CONFIGURED.
WIRING WITHIN THE DASHED LINES APPLIES ONLY WITH FANS ENABLED.
Page 326
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15 December 2011
UL-801 Installation Manual
N. UL-801 to UNS-1Lw
NOTE: The FMS must be SCN 1000.5/1100.5 or later to support FANS.
UL-801
(P/N 10801-XX)
CONFIGURATION
MODULE (P/N 108009)
CONFIG
MODULE
DATA CLK
+5 VDC
DATA I/O
GND
11C
11D
12C
12D
TP
24
24
24
24
YELLLOW
RED
BLUE
BROWN
1
DISCRETE INPUT #3
2
DISCRETE INPUT #4
12B
12C
MP
ARINC 429 TX #1
(FMS 1)
A
B
1A
1B
PARKING BRAKE SET = GND or OPEN
(OPTIONAL, AS REQUIRED)
DOOR n OPEN = GND or OPEN
(OPTIONAL, AS REQUIRED) 3
5
#1 UNS-1Lw
(P/N 3116-XX-111X)
A
B
ARINC
429 RX
4
ARINC 429 RX #1
6
(FMS 1)
A
B
1C
1D
ARINC 429 TX #2
(FMS 2)
A
B
2A
2B
ARINC 429 RX #2
(FMS 2)
6
A
B
2C
2D
5
A
B
HS ARINC
429 TX
5
#2 UNS-1Lw
(P/N 3116-XX-111X)
A
B
ARINC
429 RX
4
5
A
B
HS ARINC
429 TX
VHF ANTENNA
VHF ANTENNA
+28 VDC POWER
POWER GND4
CHASSIS GND 3
5
2
BP
20
20
16
5A
+28 VDC
7
9 DISCRETE OUTPUT
8
10 DISCRETE OUTPUT 8
12 DISCRETE OUTPUT 8
11
+28 VDC
13
CPDLC
CNECT
14
NOTES: ALL WIRING IS TO BE 22 AWG UNLESS OTHERWISE INDICATED.
THE FMS MUST BE SCN 1000.5/1100.5 OR LATER TO SUPPORT FANS.
1 CONFIGURATION MODULE IS MOUNTED ON THE REAR OF THE UL801 RACK.
2
DISCRETE INPUT ACTIVE STATE IS CONFIGURABLE TO EITHER OPEN OR GROUND.
NOTES ARE CONTINED ON THE NEXT PAGE.
Page 327
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15 December 2011
UL-801 Installation Manual
NOTES continued
3
IT IS RECOMMENDED THAT DOOR 1 OPEN DISCRETE BE USED IF ONLY ONE DOOR DISCRETE IS TO BE CONFIGURED.
4
5
UNS1Lw SUPPORTS BOTH UNILINK TEXT AND WEATHER GRAPHICS USING RS-422 DISPLAY DATA.
REFER TO APPLICABLE TECHNICAL MANUAL FOR PORT CONFIGURATIONS AND PIN ASSIGNMENTS.
6
IF FMS #1 IS NOT INTERFACED TO THE UL801, THEN CONNECT FMS #2 TO MP1C AND MP1D IN LIEU OF MP2C AND MP2D SHOWN ABOVE.
7
8
WHITE ATC LETTERING RECOMMENDED. USE ANNUNCIATOR P/N EATON 582-10 A0 B0 C3 F4 L5 N1 (D) P12,12 ATC OR EQUIVALENT.
ANY AVAILABLE DISCRETE OUTPUT PIN MAY BE USED.
CONFIGURE DISCRETE OUTPUT FOR FANS VISUAL.
9
10
CONFIGURE DISCRETE OUTPUT FOR FANS AURAL.
11
CONNECT TO AN AURAL ALERTING DEVICE OR AN AURAL WARNING GENERATOR. USE SONALERT P/N SCE028LD2TT1B OR EQUIVALENT.
12
OPTIONAL: CONFIGURE DISCRETE OUTPUT FOR CPDLC CNECT (CONNECT).
13 OPTIONAL: CPDLC CNECT ANNUNCIATOR. LABEL AS REQUIRED.
14 WIRING WITHIN THE DASHED LINES APPLIES ONLY WITH FANS ENABLED.
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O. UL-801 with FANS to UNS-1Fw
(1) Sheet 1 of 2
NOTE: The FMS must be SCN 1000.5/1100.5 or later to support FANS.
UL-801
(P/N 10801-XX)
CONFIGURATION MODULE
(P/N 108009)
TP
CONFIG
MODULE
DATA CLK
+5 VDC
DATA I/O
11C
11D
12C
24
24
24
YELLOW
RED
BLUE
BROWN
1
2
DISCRETE INPUT #3
DISCRETE INPUT #4
12B
MP
12C
PARKING BRAKE SET = GND or OPEN
(OPTIONAL, AS REQUIRED)
DOOR n OPEN = GND or OPEN
(OPTIONAL, AS REQUIRED)
3
ARINC 429 TX #1
(FMS 1)
A
B
1A
1B
4
#1 UNS-1Fw
2192-X0-111XXX
A
B
ARINC 429 RX
ARINC 429 RX #1
(FMS 1)
5
A
B
1C
1D
4
A
HS ARINC 429 TX
B
ARINC 429 TX #2
(FMS 2)
A
B
2A
2B
ARINC 429 RX #2
(FMS 2)
5
A
B
2C
2D
VHF ANTENNA
+28 VDC POWER
5
2
POWER GND4
CHASSIS GND3
BP
20
20
16
VHF ANTENNA
5A
+28 VDC
4
#2 UNS-Fw
2192-X0-111XXX
A
B
ARINC 429 RX
4
A
B
HS ARINC 429 TX
6
8 DISCRETE OUTPUT 7
9 DISCRETE OUTPUT 7
11 DISCRETE OUTPUT 7
----CONTINUED----
10
+28 VDC
12
CPDLC
CNECT
15
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(2) Sheet 2 of 2 - 4/5” FPCDU/MCDU
UL-801
(P/N 10801-XX)
----CONTINUED----
TP
RS-422 DISPLAY
DATA TX #3
A
B
16
RS-422 DISPLAY
DATA RX #3
A
B
9A
9B
9C
9D
P3
E
F
B
C
D
P3
#1 4"/5 FPCDU/MCDU
(P/N 1117-X-X1X,
P/N 1018-X-X1X,
P/N 1025-XX-XXX)
A
B
RS-422 DISPLAY
DATA RX
13 14
E
F
A
B
RS-422 DISPLAY
DATA TX
SHIELD GND
#2 4"/5 FPCDU/MCDU
(P/N 1117-X-X1X,
A
B
RS-422 DISPLAY
DATA RX
13 14
B
C
A
B
RS-422 DISPLAY
DATA TX
NOTES: ALL WIRING IS TO BE 22 AWG UNLESS OTHERWISE INDICATED.
THE FMS MUST BE SCN 1000.5/1100.5 OR LATER TO SUPPORT FANS.
1
CONFIGURATION MODULE IS MOUNTED ON THE REAR OF THE UL801 RACK.
2
DISCRETE INPUT ACTIVE STATE IS CONFIGURABLE TO EITHER OPEN OR GROUND.
D SHIELD GND
3 IT IS RECOMMENDED THAT DOOR 1 OPEN DISCRETE BE USED IF ONLY ONE DOOR DISCRETE IS TO BE CONFIGURED.
4
5
REFER TO APPLICABLE TECHNICAL MANUAL FOR PORT CONFIGURATIONS AND PIN ASSIGNMENTS.
IF FMS #1 IS NOT INTERFACED TO THE UL801, THEN CONNECT FMS #2 TO MP1C AND MP1D IN LIEU OF MP2C AND MP2D SHOWN ABOVE.
6
WHITE ATC LETTERING RECOMMENDED. USE ANNUNCIATOR P/N EATON 582-10 A0 B0 C3 F4 L5 N1 (D) P12,12 ATC OR EQUIVALENT.
7 ANY AVAILABLE DISCRETE OUTPUT PIN MAY BE USED.
8
CONFIGURE DISCRETE OUTPUT FOR FANS VISUAL.
9 CONFIGURE DISCRETE OUTPUT FOR FANS AURAL.
10 CONNECT TO AN AURAL ALERTING DEVICE OR AN AURAL WARNING GENERATOR. USE SONALERT P/N SCE028LD2TT1B OR EQUIVALENT.
11 OPTIONAL: CONFIGURE DISCRETE OUTPUT FOR CPDLC CNECT (CONNECT).
12 OPTIONAL: CPDLC CNECT ANNUNCIATOR. LABEL AS REQUIRED.
13
BOTH THE 4 AND 5 FPCDUs, P/Ns 1117-2-X1X AND 1018-2-X1X, SUPPORT BOTH UNILINK TEXT AND WEATHER GRAPHICS (RS-422 DISPLAY DATA).
OTHER 4 AND 5 FPCDUs, P/Ns 1117-X-X00 AND 1018-X-X00, SUPPORT UNILINK TEXT ONLY.
14
15
16
BOTH 4 AND 5 FPCDUs ARE WIRED IN THE SAME MANNER.
WIRING WITHIN THE DASHED LINES APPLIES ONLY WITH FANS ENABLED.
CONFIGURE AS A LO-RES DISPLAY.
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P. UL-801 FANS Discretes (WAAS FMS SCN 1000.5/1100.5 or later)
UL-801
(P/N 10801-XX)
3
ANNUNCIATOR
P/N EATON 582-10 A0 B0 C3 F4 L5 N1 (D) P12,12 ATC
2 DISCRETE OUTPUT
1
DISCRETE OUTPUT
4
DISCRETE OUTPUT
6
2
2
5
7
CPDLC
CNECT
5
6
7
1
2
3
4
NOTE: ALL WIRING IS TO BE 22 AWG UNLESS OTHERWISE INDICATED.
CONFIGURE DISCRETE OUTPUT FOR FANS VISUAL.
ANY AVAILABLE DISCRETE OUTPUT PIN MAY BE
WHITE ATC LETTERING RECOMMENDED.
CONFIGURE DISCRETE OUTPUT FOR FANS
CONNECT TO AN AURAL ALERTING DEVICE OR AN AURAL WARNING GENERATOR.
OPTIONAL: CONFIGURE DISCRETE OUTPUT FOR CPDLC CNECT (CONNECT).
OPTIONAL: CPDLC CNECT ANNUNCIATOR. LABEL AS REQUIRED.
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Q. UL-801 to EFI-890R – High Resolution
UL-801
(P/N 10801-XX)
RS-422 DISPLAY
DATA TX #4
A
B
1
RS-422 DISPLAY
DATA RX #4
A
B
7C
7D
7A
7B
TP
RS-422 DISPLAY
DATA TX #5
A
B
3
RS-422 DISPLAY
DATA RX #5
A
B
6A
6B
6C
6D
P1
16
27
4
47
46
2
#1 NAV DISPLAY
(P/N 8904-XXXXX-XX)
A
B
RS-422 RX
RETURN/SHIELD
A
B
RS-422 TX
RETURN/SHIELD
P1
16
27
4
47
46
2
#2 NAV DISPLAY
(P/N 8904-XXXXX-XX )
A
B
RS-422 RX
RETURN/SHIELD
A
B
RS-422 TX
RETURN/SHIELD
1
2
3
4
SELECT ANY AVAILABLE RS-422 PORT AND CONFIGURE THE PORT FOR HI-RES DISPLAY 1. PORT #4 IS USED HERE AS AN EXAMPLE.
EFI-890Rs ARE HIGH RESOLUTION DEVICES, ONE DEVICE MAXIMUM PER PORT. THEREFORE, THE UNILINK MUST BE CONFIGURED AS DEFINED
BELOW. A MAXIMUM OF TWO HIGH-RESOLUTION DISPLAYS CAN BE INSTALLED AND CONFIGURED.
SELECT ANY AVAILABLE RS-422 PORT AND CONFIGURE THE PORT FOR HI-RES DISPLAY 2. PORT #5 IS USED HERE AS AN EXAMPLE.
USE ANY AVAILABLE RS-422 PORT. PORTS DEPICTED ARE FOR EXAMPLE.
UNILINK CONFIGURATION
I/O CONFIG:
SELECT SERIAL
PORT 4 SELECT HI-RES DISPLAY 1
PORT 5 SELECT HI-RES DISPLAY 2
GRAPHICS CONFIGURATION
CDU/MFD BAUD RATE
CDU1 GRAPHICS DISPLAY ON
CDU2 GRAPHICS DISPLAY ON
SELECT 19.2 KBS
SELECT CDU, HR1
SELECT CDU, HR2
EXAMPLE 1
CDU1 GRAPHICS DISP ON
CDU, RCDU, HR1
CDU2 GRAPHICS DISP ON
CDU, HR2
CDU3 GRAPHICS DISP ON
CDU
EXAMPLE 2
CDU1 GRAPHICS DISP ON
CDU, FPCDU, HR1
CDU2 GRAPHICS DISP ON
CDU, HR2
CDU3 GRAPHICS DISP ON
ANY ADDITIONAL SELECTIONS WILL RESULT IN AN ERROR MESSAGE.
EFI-890R ND #1 CONFIGURATION MAIN MENU
RS-422 RX CHANNEL MENU
J1-16, J1-27(A,B) RX FUNCTION: UNILINK 700 PRIMARY 38.4
J1-16, J1-27(A,B) RX NUMBER: SYSTEM 1
RS-422 TX CHANNEL MENU
J1-47, J1-46(A,B) TX FUNCTION: UNILINK 700 38.4
UNILINK NODE ID: 35
EFI-890R ND #2 CONFIGURATION MAIN MENU
RS-422 RX CHANNEL MENU
J1-16, J1-27(A,B) RX FUNCTION: UNILINK 700 PRIMARY 38.4
J1-16, J1-27(A,B) RX NUMBER: SYSTEM 1
RS-422 TX CHANNEL MENU
J1-47, J1-46(A,B) TX FUNCTION: UNILINK 700 38.4
UNILINK NODE ID: 45
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R. UL-801 to MFD-640 – High Resolution (MFD SCN 1011.4.8 or later)
UL-801
(P/N 10801-XX)
P1
MFD-640
P/N 6402-XXXXX-XX
TP
RS-422 DISPLAY
DATA TX #4
A
B
RS-422 DISPLAY
DATA RX #4
A
B
7A
7B
1
7C
7D
58
57
1
47
46
A
B
RS-422 RX #1
A
B
RS-422 TX #1
RETURN/SHIELD
NOTE: UNILINK HIGH RESOLUTION CONFGURATION SETTINGS REQUIRE MFD-640-SCN 1011.4.8 OR LATER.
1
USE ANY AVAILABLE RS-422 PORT. PORTS DEPICTED ARE EXAMPLES. A MAXIMUM OF TWO HIGH-RESOLUTION DISPLAYS MAY BE USED.
THE UNILINK HIGH RESOLUTION MFD MUST BE CONFIGURED AS DEFINED BELOW.
UNILINK CONFIGURATION
I/O CONFIG:
SELECT SERIAL
PORT 4 SELECT HI-RES DISPLAY 1
GRAPHICS CONFIGURATION
CDU/MFD BAUD RATE
CDU1 GRAPHICS DISPLAY ON
CDU2 GRAPHICS DISPLAY ON
SELECT 19.2 KBPS
SEE THE EXAMPLES BELOW
SEE THE EXAMPLES BELOW
CDU3 GRAPHICS DISPLAY ON SEE THE EXAMPLES BELOW
MFD-640 CONFIGURATION
CONFIGURATION MAIN MENU
UNILINK NODE ID: 35
BAUD RATE: 38.4K
RS-422 MENU
J1-58, J1-57 RX FUNC: UNILINK PRIMARY
RX NUMBER: SYSTEM 1
RS-422 TX CHANNEL MENU
J1-47, J1-46 TX FUNC: UNILINK
J1-58, 47, J1-57,46 SPEED: 38400
EXAMPLE 1
CDU1 GRAPHICS DISP ON
CDU, RCDU, HR1
EXAMPLE 2
CDU1 GRAPHICS DISP ON
CDU, FPCDU, HR1
CDU2 GRAPHICS DISP ON
CDU, HR2
CDU3 GRAPHICS DISP ON
CDU
CDU2 GRAPHICS DISP ON
CDU, HR2
CDU3 GRAPHICS DISP ON
ANY ADDITIONAL SELECTIONS WILL RESULT IN AN ERROR MESSAGE.
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S. UL-801 to Remote CDU (RCDU) – Low Resolution
UL-801
(P/N 10801-XX)
TP
RS-422 TX
RS-422 RX
A
B
A
B
2
4 or 5 FPCDU #1
J3
B
C
D
E
F
A
B
RS-422
DISPLAY
RX
A
B
RS-422
DISPLAY
TX
GROUND
J3
B
C
D
E
F
4 or 5 FPCDU #2
A
B
RS-422
DISPLAY
RX
A
B
RS-422
DISPLAY
TX
GROUND
J3
B
C
D
E
F
4 or 5 FPCDU #3
A
B
RS-422
DISPLAY
RX
A
B
RS-422
DISPLAY
TX
GROUND
RCDU
B
C
D
E
F
A
B
RS-422
DISPLAY
RX
A
B
RS-422
DISPLAY
TX
GROUND
CAUTION: IT IS THE INSTALLER'S RESPONSIBILITY TO VERIFY PIN NUMBERS ON EQUIPMENT MANUFACTURED BY OTHER THAN UNIVERSAL AVIONICS
SYSTEMS CORPORATION.
NOTES:
1.
2
A MAXIMUM OF FOUR DISPLAY DEVICES MAY BE CONNECTED AND CONFIGURED. THE FPCDUs SHOWN ARE EXAMPLES ONLY. FMS CDUs OR ANY
OTHER DISPLAY DEVICE IN ANY COMBINATION CAN ALSO BE USED.
SELECT ANY AVAILABLE RS-422 PORT (PORT 4 RECOMMENDED) AND CONFIGURE FOR LOW RESOLUTION:
UNILINK CONFIGURATION
I/O CONFIG:
SELECT AND CONFIGURE PORT AS LO-RES DISPLAY
GRAPHICS CONFIGURATION
CDU/MFD BAUD RATE
CDU1 GRAPHICS DISPLAY ON
CDU2 GRAPHICS DISPLAY ON
CDU3 GRAPHICS DISPLAY ON
SELECT 19.2 KBPS
SEE CONFIGURATION NOTE 1
SEE CONFIGURATION NOTE 2
SEE CONFIGURATION NOTE 3
CONFIGURATION NOTES
1.
CONFIGURE RCDU HERE TO SHARE DATA WITH #1 CDU.
2.
CONFIGURE RCDU HERE TO SHARE DATA WITH #2 CDU.
3.
CONFIGURE RCDU HERE TO SHARE DATA WITH #3 CDU.
EXAMPLE 1
CDU1 GRAPHICS DISP ON
CDU, RCDU
EXAMPLE 2
CDU1 GRAPHICS DISP ON
CDU, FPCDU
CDU2 GRAPHICS DISP ON
CDU
CDU3 GRAPHICS DISP ON
CDU
CDU2 GRAPHICS DISP ON
CDU, MFD-LR
CDU3 GRAPHICS DISP ON
ANY ADDITIONAL SELECTIONS WOULD EXCEED THE TOTAL OF FOUR DEVICES AND CREATE AN ERROR MESSAGE.
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T. UL-801 to MFD-640 - Low Resolution (MFD-640 SCN 1011.4.7 or earlier)
UL-801
(P/N 10801-XX)
TP J3
4 or 5 FPCDU #1
RS-422 TX
RS-422 RX
A
B
A
B
2
B
C
D
E
F
A
B
RS-422
DISPLAY
RX
A
B
RS-422
DISPLAY
TX
GROUND
4 or 5 FPCDU #2
J3
B
C
D
E
F
A
B
RS-422
DISPLAY
RX
A
B
RS-422
DISPLAY
TX
GROUND
4 or 5 FPCDU #3
J3
B
C
D
E
F
A
B
RS-422
DISPLAY
RX
A
B
RS-422
DISPLAY
TX
GROUND
MFD-640
3
A
B
RS-422
DISPLAY
RX
A
B
RS-422
DISPLAY
TX
GROUND
CAUTION: IT IS THE INSTALLER'S RESPONSIBILITY TO VERIFY PIN NUMBERS ON EQUIPMENT MANUFACTURED BY OTHER THAN UNIVERSAL AVIONICS
SYSTEMS CORPORATION.
NOTES:
1.
A MAXIMUM OF FOUR DISPLAY DEVICES MAY BE CONNECTED AND CONFIGURED. THE FPCDUs SHOWN ARE EXAMPLES ONLY. FMS CDUs OR ANY
OTHER DISPLAY DEVICE IN ANY COMBINATION CAN ALSO BE USED.
2 SELECT ANY AVAILABLE RS-422 PORT (PORT 4 RECOMMENDED) AND CONFIGURE FOR LOW RESOLUTION:
3 REFER TO THE MFD-640 INSTALLATION MANUAL FOR PORT SELECTIONS.
UNILINK CONFIGURATION
I/O CONFIG:
SELECT SERIAL AND CONFIGURE PORT AS LO-RES DISPLAY
GRAPHICS CONFIGURATION
CDU/MFD BAUD RATE
CDU1 GRAPHICS DISPLAY ON
CDU2 GRAPHICS DISPLAY ON
CDU3 GRAPHICS DISPLAY ON
SELECT 19.2 KBPS
SEE CONFIGURATION NOTE 1
SEE CONFIGURATION NOTE 2
SEE CONFIGURATION NOTE 3
CONFIGURATION NOTES
1. CONFIGURE MFD-LR HERE TO SHARE DATA WITH #1 CDU.
2. CONFIGURE MFD-LR HERE TO SHARE DATA WITH #2 CDU.
3. CONFIGURE MFD-LR HERE TO SHARE DATA WITH #3 CDU.
EXAMPLE 1
CDU1 GRAPHICS DISP ON
CDU, MFD-LR
EXAMPLE 2
CDU1 GRAPHICS DISP ON
CDU, FPCDU
MFD-640 CONFIGURATION
CONFIGURATION MAIN MENU
UNILINK NODE ID: 40
RS-422 MENU
J1-58, J1-57 RX FUNC: UNILINK PRIMARY
RX NUMBER: SYSTEM 1
RS-422 TX CHANNEL MENU
J1-47, J1-46 TX FUNC: UNILINK
J1-58, 47, J1-57,46 SPEED: 19200
CDU2 GRAPHICS DISP ON
CDU
CDU3 GRAPHICS DISP ON
CDU
CDU2 GRAPHICS DISP ON
CDU, MFD-LR
CDU3 GRAPHICS DISP ON
ANY ADDITIONAL SELECTIONS WOULD EXCEED THE TOTAL OF FOUR DEVICES AND CREATE AN ERROR MESSAGE.
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UL-801 Installation Manual
U. UL-801 to CVR/CVFDR
UL-801
(P/N 10801-XX)
ARINC 429 TX
HS OUTPUT TO CVR/CVFDR B
H 3
3
1
2
CVR-120A, CVR-120R,
CVFDR-145, CVFDR-145R
4 8
SPEED STRAP
GND = HS
12 VALID
GND = VALID
10
18
H
L
ARINC 429
RX
DATALINK
CAUTION: IT IS THE INSTALLER'S RESPONSIBILITY TO VERIFY PIN NUMBERS ON EQUIPMENT MANUFACTURED BY OTHER THAN UNIVERSAL AVIONICS
SYSTEMS CORPORATION.
1
2
PIN 48 (DATA LINK SPEED STRAP) SETS THE ARINC 429 RX PORT TO HIGH OR LOW SPEED. UNILINK TRANSMITS 429 HIGH SPEED AND THEREFORE MUST BE
GROUNDED AS SHOWN.
PIN 12 (VALID) DATA LINK VALID MUST BE GROUNDED AS SHOWN TO ENABLE DATA LINK RECORDING. IF THIS PIN IS GROUNDED WITH NO COMMUNICATION
FROM A DATA LINK, A CVR FAIL (AMBER LED) WILL BE PRESENT ON THE COCKPIT CONTROL UNIT (CCU).
3
CONNECT TO ANY AVALABLE ARINC TX PORT, CONFIGURE FOR HIGH SPEED, AND SET THE PORT TO CVR. RECEIVE PORTS ARE NOT REQUIRED AT THIS TIME.
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V. UL-801 to DTU-100
UL-801
(P/N 10801-XX)
ETHERNET TX
-
+
ETHERNET RX
-
+ 2
TP
ETHERNET SHIELD
UL-801 Installation Manual
1
P2
J
K
L
N
P
-
+
-
+
DTU-100
(P/N 1406-01-X)
ETHERNET
RX CH 3
ETHERNET
TX CH 3
ETHERNET SHIELD
3
1
ETHERNET CABLE PER ARINC 646 (10 BASE-T FOR AVIONICS USE). P/N ECS 392404 OR EQUIVALENT.
2
3
THREE ETHERNET PORTS ARE AVAILABLE. REFER TO THE PIN ASSIGNMENT CHART IN THIS MANUAL.
THERE ARE ADDITIONAL ETHERNET PORTS AVAILABLE. REFER TO THE PIN ASSIGNMENT CHART OF THIS MANUAL.
W. UL-801 to SSDTU
UL-801
(P/N 10801-XX)
TP
ETHERNET
TX
ETHERNET
RX
+
+
-
-
ETHERNET SHIELD
4
4
1 2
1
6
2
7
13
SSDTU
(P/N 1408-00-X)
+
-
ETHERNET
RX CH3
3
+
-
ETHERNET
TX CH3
SHIELD
3
NOTES:
1
USE ETHERNET CABLE ECS P/N 392404 OR THERMAX/CDT 956-426 OR EQUIVALENT.
2
3
THE EXPOSED UNSHIELDED ETHERNET WIRE BETWEEN THE SHIELD AND THE CIRCULAR CONNECTOR SHOULD BE
LESS THAN 0.5 INCHES LONG.
THERE ARE ADDITIONAL ETHERNET PORTS AVAILABLE. REFER TO THE PIN ASSIGNMENT CHART OF THE MANUAL.
4 THREE ETHERNET PORTS ARE AVAILABLE. WIRING AND CONFIGURATION ARE UP TO THE DISCRETION OF THE INSTALLER.
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X. UL-801 to Portable DTU-100
UL-801
P/N 10801-XX
2
+
ETHERNET TX
ETHERNET RX
-
ETHERNET SHIELD
-
+ 3
BULKHEAD
CONNECTOR
L
N
J
K
J
K
L
N
P P
1 P2
L
N
J
K
P
H
L
H
L
PORTABLE DTU-100
(P/N 1407-01-1)
ETHERNET
RX CH3
ETHERNET
TX CH3
ETHERNET SHIELD
CAUTION: IT IS THE INSTALLER'S RESPONSIBILITY TO VERIFY PIN NUMBERS ON EQUIPMENT MANUFACTURED BY OTHER THAN UNIVERSAL AVIONICS
SYSTEMS CORPORATION.
1
2
THE DASHED LINES BETWEEN THE PORTABLE DTU AND P1 AND P2 CONNECTORS REPRESENTS A WIRING HARNESS THAT IS PART OF THE
PORTABLE DTU.
ETHERNET CABLE PER ARINC 626 (10 BASE-T AVIONICS USE) P/N ECS 392404 OR EQUIVALENT.
3 THERE ARE ADDITIONAL ETHERNET PORTS AVAILABLE. REFER TO THE PIN ASSIGNMENT CHART OF THIS MANUAL.
Y. UL-801 to Portable SSDTU
NOTE: It is strongly recommended that customer’s using a DTU-100 upgrade to the
SSDTU.
UL-801
P/N 10801-XX
+
ETHERNET TX
ETHERNET RX
-
ETHERNET SHIELD
-
+ 3
2
J2 BULKHEAD
CONNECTOR
1 1
6
2
7
6
2
7
13 13
1
HARNESS
(P/N 81140821) P2
2
7
1
6
13
+
-
+
-
PORTABLE SSDTU
(P/N 1409-00-2)
ETHERNET
RX CH3
4
ETHERNET
TX CH1
SHIELD #3
CAUTION: IT IS THE INSTALLER'S RESPONSIBILITY TO VERIFY PIN NUMBERS ON EQUIPMENT MANUFACTURED BY OTHER THAN UNIVERSAL AVIONICS
SYSTEMS CORPORATION.
1
2
THE DASHED LINES BETWEEN THE PORTABLE DTU AND P1 AND P2 CONNECTORS REPRESENTS A WIRING HARNESS THAT IS PART OF THE
PORTABLE SSDTU.
USE ETHERNET CABLE ECS P/N 392404 OR THERMAX/CDT P/N 956-426 OR EQUIVALENT.
THE EXPOSED UNSHIELDED ETHERNET WIRE BETWEEN THE SHIELD AND THE CIRCULAR CONNECTOR SHOULD BE LESS THAN 0.5 INCHES LONG.
3
4 THERE ARE ADDITIONAL ETHERNET PORTS AVAILABLE. REFER TO THE PIN ASSIGNMENT CHART OF THIS MANUAL.
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UL-801 Installation Manual
Z. UL-801 Airborne-based Telephony SatCom Systems
(1) UL-801 to Aero-M – without FANS
UL-801
(P/N 10801-XX)
MP TP
TX 4A 14 TXD 1
TT-3000 AERO-M
(P/N 403068A-UAT)
RS-232 #1 RX 4C 13
GND 3A 16
RXD 1
GND
CAUTION: IT IS THE INSTALLER'S RESPONSIBILITY TO VERIFY PIN NUMBERS ON EQUIPMENT MANUFACTURED BY OTHER THAN UNIVERSAL AVIONICS
SYSTEMS CORPORATION.
NOTES:
1 SIGNAL NAMES ARE IDENTIFIED BY THE MANUFACTURER AND ARE NOT USED TO IMPLY SIGNAL DIRECTION.
(2) UL-801 to ARINC 741 Satellite Communication (SatCom) Packet Data – without FANS
UL-801
(P/N 10801-XX)
TT-5000 AERO-I
(P/N 4050033A-UAT-XXX)
TP BP
A 13A
42
A
ARINC 429 RX
PORT #6 SATCOM
CMU #1 & #2
OUTPUT PORT
(ARINC 429)
B 13B 43
B
ARINC 429 TX
PORT #3 SATCOM
A
B
15A
15B
44
45
A
B
INPUT PORT
(ARINC 429)
PRINTER
(IF APPLICABLE)
CAUTION: IT IS THE INSTALLER'S RESPONSIBILITY TO VERIFY PIN NUMBERS ON EQUIPMENT MANUFACTURED BY OTHER THAN UNIVERSAL AVIONICS
SYSTEMS CORPORATION.
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UL-801 Installation Manual
(3) UL-801 to AirCell and Iridium Systems
UL-801
(P/N 10801-XX)
RS-232 #1
TX
RX
GND
4A
MP
4C
3A
N a c
TX
RX
GND
AIRCELL (AGT.02)
IRIDIUM (ST3100)
AIRCELL/IRIDIUM (AST3500)
RS-232
CAUTION: IT IS THE INSTALLER'S RESPONSIBILITY TO VERIFY PIN NUMBERS ON EQUIPMENT MANUFACTURED BY OTHER THAN UNIVERSAL AVIONICS SYSTEMS
CORPORATION.
(4) UL-801 Connection to AirCell Axxess ST4200/ST4020 – Channel #1
UL-801
(P/N 10801-XX)
AIRCELL AXXESS
ST4200/ST4020 - CHANNEL #1
RTS
CTS
RS-232 #1
TX
RX
GND
4A
MP
4C
3A
AA
Z
J
K
GG
RX
TX
GND
RS-232
CAUTION: IT IS THE INSTALLER'S RESPONSIBILITY TO VERIFY PIN NUMBERS ON EQUIPMENT MANUFACTURED BY OTHER THAN UNIVERSAL AVIONICS
SYSTEMS CORPORATION.
(5) UL-801 Connection to AirCell Axxess ST4200/ST4020 – Channel #2
UL-801
(P/N 10801-XX)
AIRCELL AXXESS
ST4200/ST4020 - CHANNEL #2
X
V
CTS
RTS
TX 4A
MP
DD RX
RS-232 #1 RX
GND
4C
3A
W
Y
TX
GND
RS-232
CAUTION: IT IS THE INSTALLER'S RESPONSIBILITY TO VERIFY PIN NUMBERS ON EQUIPMENT MANUFACTURED BY OTHER THAN UNIVERSAL AVIONICS
SYSTEMS CORPORATION.
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ICS-220A
UL-801 Installation Manual
(6) UL-801 Connections to International Communications Group (ICG)
ICS-220A
UL-801
P/N10801-00
MP TP
A
B
ARINC 429 TX #3
ARINC 429 BUS
RX A
RX B
D4
D5
SHIELD
TX A
TX B
D6
D1
D2
SHIELD D3
15A
15B
1
13A
13B
A
B
ARINC 429 TX #6
RS-232
TX
RX
GND
D5
D6
D8
TP MP
4A
4C
3A
TX
RX
GND
RS-232 #1 1
CAUTION: IT IS THE INSTALLER'S RESPONSIBILITY TO VERIFY PIN NUMBERS ON EQUIPMENT MANUFACTURED BY OTHER THAN UNIVERSAL AVIONICS
SYSTEMS CORPORATION.
1
THESE PIN NUMBERS ARE RECOMMENDED. HOWEVER, THE WIRING AND CONFIGURATION ARE UP TO THE DISCRETION OF THE INSTALLER.
AA. UL-801 to ARINC 740/744/744A Printer
UL801
(P/N 10801XX)
TP
PRINTER
ARINC 740 OR ARINC 744
ARINC 429 RECEIVE
PORT #4 PRINTER
A 14A
B 14B
1
A
ARINC 429 TRANSMIT
B
ARINC 429 TRANSMIT
PORT #3 PRINTER
A 15A
B 15B
1
A
ARINC 429 RECEIVE
B
SATCOM
IF APPLICABLE
CAUTION: IT IS THE INSTALLER'S RESPONSIBILITY TO VERIFY PIN NUMBERS ON EQUIPMENT MANUFACTURED BY OTHER THAN
UNIVERSAL AVIONICS SYSTEMS CORPORATION.
ALL WIRES AWG 22 UNLESS OTHERWISE NOTED.
1
SEE THE PRINTER MANUFACTURER FOR PIN IDENTIFICATIONS.
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BB. UL-801 to PC Printer
UL-801
(P/N 10801-XX)
TP
TX
8A
RX 8C
RS-232 #2
MP
GND 3A
UL-801 Installation Manual
DB25
7
3
2
4
5
GENERIC SERIAL
PRINTER
RECEIVE DATA
TRANSMIT DATA
SIGNAL GROUND
RTS
CTS
CAUTION: IT IS THE INSTALLER'S RESPONSIBILITY TO VERIFY PIN NUMBERS ON EQUIPMENT MANUFACTURED BY OTHER THAN UNIVERSAL AVIONICS
SYSTEMS CORPORATION.
CC. UL-801 to Generic Parallel Printer
UL-801
(P/N 10801-XX)
TX 8A
TP
DB25
SERIAL
SERIAL/PARALLEL
CONVERTER
(B&B 232SPS2)
1
TRANSMIT DATA
RX 8C
2
3 RECEIVE DATA
RS-232 #2
MP
GND 3A 7 SIGNAL GROUND
DB25
PARALLEL GENERIC
PARALLEL
PRINTER
1
ON
1 SET THE DIP SWITCH ON THE 232SPS2 AS FOLLOWS (DEFAULT SETTING):
2
ON
3
OFF
4
OFF
5
OFF
6
OFF
7
OFF/ON
8
OFF
9600 baud
9600 baud
9600 baud
XON/
XOFF
8 Data
Bits
No
Parity
Dont
Care
Serial/
Parity
CAUTION: IT IS THE INSTALLER'S RESPONSIBILITY TO VERIFY PIN NUMBERS ON EQUIPMENT MANUFACTURED BY OTHER THAN UNIVERSAL AVIONICS SYSTEMS CORPORATION.
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UL-801 Installation Manual
3. UL-801 Connector Pin Identification
NOTE: Connector pin differences between the UL-701 and UL-801 top plug are shown in the shaded areas below. These differences are being presented for use when upgrading from UL-701 to UL-801.
Pin UL-801 Function UL-701 Function
1A 10/100BT Ethernet (+) TX #1
1B 10/100BT Ethernet (-) TX #1
1C 10/100BT Ethernet RX (+) #1
1D 10/100BT Ethernet RX (-) #1
Same
Same
Same
Same
2A ARINC 429 RX (A) #14
2B ARINC 429 RX (B) #14
2C ARINC 429 RX (A) #13
2D ARINC 429 RX (B) #13
Same
Same
Same
Same
3A 10/100BT Ethernet TX (+) #2 Essential RS-422/RS-232 (A) TX #8
3B 10/100BT Ethernet TX (-) #2 Essential RS-422 TX (B) #8
Ethernet RS-422/RS-232 (A) RX #8
3D 10/100BT Ethernet RX (-) #2 Essential RS-422 RX (B) #8
4A 10/100BT Ethernet TX (+) #3 Essential RS-422/RS-232 (A) TX #7
4B 10/100BT Ethernet TX (-) #3 Essential RS-422 TX (B) #7
Ethernet RS-422/RS-232 (A) RX#7
4D 10/100BT Ethernet RX #3 (-) Essential
5A RS-422 (A)/RS-232 TX #6
5B RS-422 (B) TX #6
5C RS-422 (A)/RS-232 RX #6
5D RS-422 (B) RX #6
6A RS-422 (A)/RS-232 TX #5
6B RS-422 (B) TX #5
6C RS-422 (A) /RS-232 RX #5
6D RS-422 (B) RX #5
7A RS-422 (A)/RS-232 TX #4
7B RS-422 (B) TX #4
7C RS-422 (A)/RS-232 RX #4
7D RS-422 (B) RX #4
8A RS-422 (A)/RS-232 TX #2
8B RS-422 (B) TX #2
8C RS-422 (A)/RS-232 RX #2
8D RS-422 (B) RX #2
9A RS-422 (A)/RS-232 TX #3
9B RS-422 (B) TX #3
Same
Same
Same
Same
Same
Same
Same
Same
Same
Same
RS-422 RX (B) #7
Same
Same
Same
Same
Same
Same
Same
Same
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UL-801 Installation Manual
Top Plug - continued
Pin
9C
9D
UL-801 Function
RS-422 (A)/RS-232 RX #3
RS-422 (B) RX #3
10D Discrete #1
11A ARINC 429 (A) TX #4
11B ARINC 429 (B) TX #4
11C Config Mod Clock
11D Config Mod Power
12A ARINC 429 (A) RX #8
12B ARINC 429 (B) RX #8
12C Config Mod Data (I/O)
12D Config Mod GND
13A ARINC 429 (A) RX #6
13B ARINC 429 (B) RX #6
13C ARINC 429 (A) RX #7
13D ARINC 429 (B ) RX #7
14A ARINC 429 (A) RX #4
14B ARINC 429 (B) RX #4
14C ARINC 429 (A) RX #5
14D ARINC 429 (B) RX #5
15A ARINC 429 (A) TX #3
15B ARINC 429 (B) TX #3
15C ARINC 429 (A) RX #3
15D ARINC 429 (B) RX #3
Same
Same
Same
Same
Same
Same
Same
Same
Same
Same
Same
Same
Same
Same
Same
Same
Same
Same
Same
Same
Same
Same
Same
Same
Same
Same
UL-701 Function
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UL-801 Installation Manual
NOTE: Connector pin differences between the UL-701 and UL-801 middle plug are shown in the shaded areas below. These differences are being presented for use when upgrading from UL-701 to UL-801.
Pin
2A
2B
2C
2D
1A
1B
1C
1D
UL-801 Function
ARINC 429 (A) TX #1
ARINC 429 (B) TX #1
ARINC 429 (A) RX #1
ARINC 429 (B) RX #1
ARINC 429 (A) TX #2
ARINC 429 (B) TX #2
ARINC 429 (A) RX #2
ARINC 429 (B) RX #2
3B ARINC 429 (A) RX #12
3C
3D
4A
4B
ARINC 429 (B) RX #12
ARINC 429 (A) RX #11
RS-422 (A)/RS-232 TX #1
RS-422 (B) TX #1
4C
4D
RS-422 (A)/RS-232 RX #1
RS-422 (B) RX #1
5A Discrete #14
5B
5C
5D
ARINC 429 (A) TX #5
ARINC 429 (B) TX #5
ARINC 429 (B) RX #11
6A Discrete #10
6B Discrete #11
6C Discrete #12
6D Discrete #13
7A Discrete #6
7B Discrete #7
7C Discrete #8
7D Discrete #9
8A Discrete #2
8B Discrete #3
8C Discrete #4
8D Discrete #5
9A
9B
9C
ARINC 429 (A) TX #6
ARINC 429 (B) TX #6
ARINC 429 (A) TX #7
UL-701 Function
Same
Same
Same
Same
Same
Same
Same
Same
Same
Same
Same
Same
Same
Same
Same
Same
Same
Discrete Out #15
Discrete Out #16
Same
Same
Same
Same
Same
Same
Same
Same
Same
Same
Same
Same
Same
Discrete In #13
Discrete In #14
Discrete In #15
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UL-801 Installation Manual
Middle Plug - continued
Pin UL-801 Function
9D ARINC 429 (B) TX #7
10A Discrete In #9
10B Discrete In #10
10C ARINC 429 (A) RX #15
10D ARINC 429 (B) RX #15
11A Discrete In #5
11B Discrete In #6
11C Discrete In #7
11D Discrete In #8
12A Discrete In #2
12B Discrete In #3
12C Discrete In #4
12D ARINC 429 (A) RX #10
13A ARINC 429 (A) RX #16
13B ARINC 429 (A) RX #9
13C ARINC 429 (B) RX #9
13D ARINC 429 (B) RX #10
14A ARINC 429 (B) RX #16
14B Spare
14C Chassis GND
14D Discrete In #1
15A ARINC 429 (A) TX #8
15B ARINC 429 (B) TX #8
15C Spare
15D Spare
UL-701 Function
Discrete In #16
Same
Same
Discrete In #11
Discrete In #12
Same
Same
Same
Same
Same
Same
Same
Same
Telephone Ring (Modem I/F)
Same
Same
Same
Telephone Tip (Modem I/F)
PTT Radio
Gnd Rtn VHF-ACARS (VHF Radio)
Same
VHF Modem TX (+)
VHF Modem TX (-)
VHF Modem RX (+)
VHF Modem RX (-)
Pin UL-801 Function
1 Spare Same
Same
Same
Same
Same
UL-701 Function
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UL-801 Installation Manual
1
A B C D
1
5 5
10 10
15
A
1
A
B C D
15
B C D
1
5 5
10 10
15
A B C D
15
Top Plug
Middle Plug
ARINC Key
Code #08
Bottom Plug
1
3
2
4
5
1
D C B A
1
5 5
10 10
15
D C B A
15
1
D C B A
1
5 5
10 10
15
D C B A
15
2
4
5
3
1
UL-801 Connector Rack Connector
NOTE: The darkened portion of the keying above indicates the extended part of the key; the light portion indicates the key hole.
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UL-801 Installation Manual
System Data Installation
1. International Civil Aviation Organization (ICAO)
Aircraft Type Designators
When installing system data during the configuration process, the ICAO aircraft type designator is used. The following tables contain examples of commonly used ICAO designators for various aircraft. Use ICAO Document 8643, found under “Publications” at http://www.icao.int/, to ascertain the correct designator for your aircraft.
AIRBUS
A-300
A-310
ATR
ATR-42/72
BAC
BELL
Manufacturer/Model
BEECH
90, A90 to E90 King Air
200, 1300 Super King Air
300 Super King Air
B300 Super King Air 350
214ST
222, 230, 430
BOEING
707
737-300/400/500
747-100/200/300 (E-4, VC-25)
747SP
757
C135
BRITISH AEROSPACE
BAC 111 One-eleven
BAe-125-1000
BAe-4100 Jetstream 41
ICAO Designator
A300
A310
ATR
BA111
BE9L
BE20
BE30
B350
MU30
B190
B12
BSTP
B222
B708
B727
B73A
B73B
B74A
B74S
B757
C135
BA11
H25B
H25C
BA46
JSTB
Page 401
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Manufacturer/Model
CANADAIR
RJ Regional Jet
CESSNA
F406 Caravan 2
441 Conquest, Conquest 2
500, 501 Citation, Citation 1/1SP
525 Citation Jet
526 Citation Jet
550, S550, 551, 552 Citation
2/S2/2SP/Bravo
560 Citation 5
650 Citation 3/6/7
DASSAULT
Falcon 10, Mystere 10
Falcon 20, Mystere 20
Falcon 50, Mystere 20
Falcon 900, Mystere 900
UL-801 Installation Manual
ICAO Designator
CL60
CARJ
F406
C441
C500
C525
C526
C550
DEHAVILLAND CANADA
DHC-6 Twin Otter
DOUGLAS
DC-8
DC-9
EMBRAER
EMB-145
EMB-140
EUROCOPTER
BK-117
FOKKER
50
GRUMMAN
G-159 Gulfstream 1
G-1159 Gulfstream 2
Albatross
GULFSTREAM AEROSPACE
C560
C650
FA10
FA20
FA50
F900
F2TH
DHC6
DHC7
DHC8
DC8
DC9
E110
E120
E145
E140
AS65
BK17
F50
G159
GULF
U16
GULF
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UL-801 Installation Manual
Manufacturer/Model ICAO Designator
HAWKER
HS-124-400/600 H25A
HS-125-700
IAI
H25B
Galaxy
WW23
WW24
ASTR
GLAX
ILYUSHIN
IL96
LEARJET
31
35
45
55
60
IL96
LJ31
LJ35
LJ45
LJ55
LJ60
LOCKHEED
C-130
McDONNELL DOUGLAS
DC-8
DC-9
DC-10
MD-81/82/83/87/88
MD-90
MITSUBISHI
PIPER
PA-42 Cheyenne 3/400
RAYTHEON
90 King Air
200 Super King Air (C-12)
300 Super King Air
B300 Super King Air 350
C130
L101
DC8
DC9
DC10
MD80
MD90
MU30
PA42
BE9L
BE20
1900
REIMS
F406 Caravan 2
SIKORSKY
S-70
S-76
BE30
B350
MU30
B190
H25B
H25C
F406
H60
S76
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UL-801 Installation Manual
Manufacturer/Model
TUPOLEV
Tu-154
WESTLAND
Puma
ICAO Designator
T154
PUMA
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UL-801 Installation Manual
Universal Avionics Systems Corporation recommends that the following worksheets be completed in order to assist with configuring the UniLink Configuration Module. One set of worksheets should be filled out and a copy given to the customer. Fill in the blanks and check the appropriate boxes based on the wiring of the aircraft and its set of avionics components. Further, these worksheets may be submitted along with other approval paperwork. A copy of these worksheets should be filed along with the aircraft paper work for future reference.
NOTE:
•
A customer database is installed in each UniLink.
•
You are hereby authorized to reproduce these worksheets as well as the configuration module programming procedures if desired.
•
It is recommended that the current UniLink configuration be recorded prior to updating to a new UniLink software version. UniLink may not maintain previous configuration settings with a software upgrade.
The default value for each option in the worksheets is underlined. Pressing the RETURN
LSK returns you to the menu from which you started.
UniLink input consists of one of the three following character types. Where necessary, each field on the worksheets designates which type to use.
Types of character input allowed
Alpha
Shown as “A” on the worksheets.
Numeric
Shown as “N” on the worksheets.
Alpha characters are the 26 characters of the alphabet.
Numeric characters consist of the numbers 0 to 9.
Alphanumeric
Shown as “AN” on the worksheets.
Alphanumeric characters are a combination of letters (including both upper and lower case) and numbers. Alphanumeric input can also contain punctuation marks, and mathematical and other conventional symbols (such as @, &, and *).
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UL-801 Installation Manual
Customer Name:
Customer Address:
_________________________________________________
_________________________________________________
_________________________________________________
_________________________________________________
Aircraft Manufacturer:
Aircraft Model No.:
Aircraft Serial No.:
Configuration Date:
_________________________________________________
_________________________________________________
_________________________________________________
_________________________________________________
Technician: _________________________________________________
NOTE: Configuration options may be used only once. Any option that has been selected is removed from the option list. a) DISCRETE (DISC) IN
•
Active state of BRAKE SET indicates the parking brake is locked.
•
Active state of DOOR CLOSED indicates the configured door is closed.
•
Active state of STRUT COMP (Strut Compressed) indicates the aircraft is onground (weight on wheels).
•
The TEST option is provided for development and engineering purposes only.
DISC IN 1
Middle Plug 14D
DISC IN 2
Middle Plug 12A
DISC IN 3
Middle Plug 12B
DISC IN 1/4
NOT USED BRAKE SET STRUT COMP TEST
DOOR 1 CLOSED DOOR 2 CLOSED DOOR 3 CLOSED DOOR 4 CLOSED
ACTIVE STATE GROUND OPEN
NOT USED BRAKE SET STRUT COMP TEST
DOOR 1 CLOSED DOOR 2 CLOSED DOOR 3 CLOSED DOOR 4 CLOSED
ACTIVE STATE GROUND OPEN
NOT USED BRAKE SET STRUT COMP TEST
DOOR 1 CLOSED DOOR 2 CLOSED DOOR 3 CLOSED DOOR 4 CLOSED
ACTIVE STATE GROUND OPEN
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DISC IN 4
Middle Plug 12C
DISC IN 5
Middle Plug 11A
DISC IN 6
Middle Plug 11B
DISC IN 7
Middle Plug 11C
DISC IN 8
Middle Plug 11D
DISC IN 9
Middle Plug 10A
DISC IN 10
Middle Plug 10B
UL-801 Installation Manual
Press NEXT. DISC IN 2/4 displays.
NOT USED BRAKE SET STRUT COMP TEST
DOOR 1 CLOSED DOOR 2 CLOSED DOOR 3 CLOSED DOOR 4 CLOSED
ACTIVE STATE
NOT USED
GROUND
BRAKE SET
OPEN
STRUT COMP TEST
DOOR 1 CLOSED DOOR 2 CLOSED DOOR 3 CLOSED DOOR 4 CLOSED
ACTIVE STATE GROUND OPEN
NOT USED BRAKE SET STRUT COMP TEST
DOOR 1 CLOSED DOOR 2 CLOSED DOOR 3 CLOSED DOOR 4 CLOSED
ACTIVE STATE GROUND OPEN
Press NEXT. DISC IN 3/4 displays.
NOT USED BRAKE SET STRUT COMP TEST
DOOR 1 CLOSED DOOR 2 CLOSED DOOR 3 CLOSED DOOR 4 CLOSED
ACTIVE STATE GROUND OPEN
NOT USED BRAKE SET STRUT COMP TEST
DOOR 1 CLOSED DOOR 2 CLOSED DOOR 3 CLOSED DOOR 4 CLOSED
ACTIVE STATE GROUND OPEN
NOT USED BRAKE SET STRUT COMP TEST
DOOR 1 CLOSED DOOR 2 CLOSED DOOR 3 CLOSED DOOR 4 CLOSED
ACTIVE STATE GROUND OPEN
Press NEXT. DISC IN 4/4 displays.
NOT USED BRAKE SET STRUT COMP TEST
DOOR 1 CLOSED DOOR 2 CLOSED DOOR 3 CLOSED DOOR 4 CLOSED
ACTIVE STATE GROUND OPEN
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DISC OUT 1
Top Plug 10D
UL-801 Installation Manual b) DISCRETE (DISC) OUT
•
FANS VISUAL
−
Output – Active Open or Active Ground configurable.
−
Use any available discrete output pin and configure accordingly.
−
The FANS VISUAL output discrete activates the ATC annunciator and alerts the crew that an ATC advisory is active and the UniLink pages should be accessed to view further information.
•
FANS AURAL
−
Output – Active Open or Active Ground configurable. Duration is configurable.
−
Use any available discrete output pin and configure accordingly.
−
The FANS AURAL output discrete activates the aural warning device and alerts the crew that an aural message has been received.
•
CPDLC CNECT (Connect)
−
Output – Active Open or Active Ground configurable.
−
Use any available discrete output pin and configure accordingly.
−
The CPDLC CNECT output discrete activates an optional CPDLC CNECT annunciator while the UniLink is connected to the Current Data Authority
(CDA).
−
If the CDA connection is disrupted or lost, the optional CPDLC CNECT annunciator deactivates.
•
The New Message (NEW MSG) discretes are provided to drive visual indications of new/unread uplinks. Active state indicates a new/unread uplink exists.
•
The CHIME discretes are provided to drive aural indications of new/unread uplinks. Active state indicates a new/unread uplink exists.
•
VHF/SAT/TEL NOCOMM discretes are provided to drive visual indications media link states. Active state indicates a particular medium is in NOCOMM
(link not established).
DISC OUT 2
Middle Plug 8A
DISC OUT 1/5
NOT USED VOX ANNUN
VHF NOCOMM SAT NOCOMM
CHIME 1
CPDLC CNECT
CHIME 2
ACTIVE STATE
NOT USED
GROUND
VOX ANNUN
VHF NOCOMM SAT NOCOMM
CHIME 1
CPDLC CNECT
CHIME 2
ACTIVE STATE GROUND
NEW MSG 1 NEW MSG 2
TEL NOCOMM VDR VOX SEL
FANS VISUAL FANS AURAL
OPEN
NEW MSG 1 NEW MSG 2
TEL NOCOMM VDR VOX SEL
FANS VISUAL
OPEN
FANS AURAL
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DISC OUT 3 Middle
Plug 8B
DISC OUT 4 Middle
Plug 8C
DISC OUT 5 Middle
Plug 8D
DISC OUT 6 Middle
Plug 7A
DISC OUT 7 Middle
Plug 7B
DISC OUT 8 Middle
Plug 7C
DISC OUT 9 Middle
Plug 7D
UL-801 Installation Manual
DISC OUT 1/5 (Continued)
NOT USED VOX ANNUN
VHF NOCOMM SAT NOCOMM
CHIME 2 CHIME 1
CPDLC CNECT
ACTIVE STATE GROUND
NEW MSG 1 NEW MSG 2
TEL NOCOMM VDR VOX SEL
FANS VISUAL FANS AURAL
OPEN
Press NEXT. DISC OUT 2/5 displays.
NOT USED VOX ANNUN
VHF NOCOMM SAT NOCOMM
CHIME 1 CHIME 2
CPDLC CNECT
ACTIVE STATE GROUND
NOT USED VOX ANNUN
VHF NOCOMM SAT NOCOMM
CHIME 1
CPDLC CNECT
CHIME 2
ACTIVE STATE
NOT USED
GROUND
VOX ANNUN
VHF NOCOMM SAT NOCOMM
CHIME 1
CPDLC CNECT
CHIME 2
ACTIVE STATE GROUND
NEW MSG 1 NEW MSG 2
TEL NOCOMM VDR VOX SEL
FANS VISUAL FANS AURAL
OPEN
NEW MSG 1 NEW MSG 2
TEL NOCOMM VDR VOX SEL
FANS VISUAL FANS AURAL
OPEN
NEW MSG 1 NEW MSG 2
TEL NOCOMM VDR VOX SEL
FANS VISUAL FANS AURAL
OPEN
Press NEXT. DISC OUT 3/5 displays.
NEW MSG 1 NEW MSG 2
TEL NOCOMM VDR VOX SEL
FANS VISUAL FANS AURAL
NOT USED VOX ANNUN
VHF NOCOMM SAT NOCOMM
CHIME 1
CPDLC CNECT
CHIME 2
ACTIVE STATE GROUND
NOT USED VOX ANNUN
VHF NOCOMM SAT NOCOMM
CHIME 1 CHIME 2
CPDLC CNECT
NOT USED
ACTIVE STATE
VOX ANNUN
GROUND
NOT USED VOX ANNUN
VHF NOCOMM SAT NOCOMM
CHIME 1
CPDLC CNECT
CHIME 2
ACTIVE STATE GROUND
OPEN
NEW MSG 1 NEW MSG 2
TEL NOCOMM VDR VOX SEL
FANS VISUAL FANS AURAL
NEW MSG 1
OPEN
NEW MSG 2
NEW MSG 1 NEW MSG 2
TEL NOCOMM VDR VOX SEL
FANS VISUAL FANS AURAL
OPEN
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DISC OUT 10
Middle Plug 6A
DISC OUT 11
Middle Plug 6B
DISC OUT 12
Middle Plug 6C
DISC OUT 13
Middle Plug 6D
DISC OUT 14
Middle Plug 5A
UL-801 Installation Manual
Press NEXT. DISC OUT 4/5 displays.
NOT USED VOX ANNUN
VHF NOCOMM SAT NOCOMM
CHIME 2 CHIME 1
CPDLC CNECT
ACTIVE STATE GROUND
NOT USED VOX ANNUN
VHF NOCOMM SAT NOCOMM
CHIME 1 CHIME 2
CPDLC CNECT
ACTIVE STATE
NOT USED
GROUND
VOX ANNUN
VHF NOCOMM SAT NOCOMM
CHIME 1 CHIME 2
CPDLC CNECT
ACTIVE STATE GROUND
NOT USED VOX ANNUN
VHF NOCOMM SAT NOCOMM
CHIME 1 CHIME 2
CPDLC CNECT
ACTIVE STATE
NOT USED
GROUND
VOX ANNUN
VHF NOCOMM SAT NOCOMM
CHIME 1 CHIME 2
CPDLC CNECT
ACTIVE STATE GROUND
NEW MSG 1 NEW MSG 2
TEL NOCOMM VDR VOX SEL
FANS VISUAL FANS AURAL
OPEN
NEW MSG 1 NEW MSG 2
TEL NOCOMM VDR VOX SEL
FANS VISUAL FANS AURAL
OPEN
NEW MSG 1 NEW MSG 2
TEL NOCOMM VDR VOX SEL
FANS VISUAL FANS AURAL
OPEN
NEW MSG 1 NEW MSG 2
TEL NOCOMM VDR VOX SEL
FANS VISUAL FANS AURAL
OPEN
NEW MSG 1 NEW MSG 2
TEL NOCOMM VDR VOX SEL
FANS VISUAL FANS AURAL
OPEN
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UL-801 Installation Manual c) ARINC RECEIVE
•
Only one device/interface may configured on each ARINC receive port at a time.
•
UniLink configures the receive port speed based on the device selected.
−
The receive port speed for the following devices are configured for low speed: MCDU, Printer, A741 SDU, A604 CMC, IOP.
−
The receive port speed for the following devices are configured based on the device definition contained within the CDB: A702 FMS, Generic 429
Device.
−
UniLink automatically detects the transmission speed (high/low) of the following devices and configures the receive port speed accordingly:
A743A GNSS (including A743 GPS), DADC (Digital ADC).
•
UniLink processes data labels received from A702 FMS and Generic 429
Device based on the device definition contained within the CDB.
•
Devices configured on a receive port must also be configured on a transmit port except for the following receive-only devices: IOP, A743A GNSS (including
A743 GPS), DADC.
•
The TEST option is provided for development and engineering purposes only.
ARINC RX 1/3
PORT 1
(A) Middle Plug 1C
(B) Middle Plug 1D
Only FMS/CDU1 is may be chosen for this port.
PORT 2
(A) Middle Plug 2C
(B) Middle Plug 2D
NOT USED
740 PRINT
DHC8 IOP1
702 FMS1
FMS/CDU1
MCDU1
FMS/CDU1
741 SDU
DHC8 IOP2
702 FMS2
FMS/CDU2
MCDU2
FMS/CDU2
VM CMC
MCDU2
702 FMS3
FMS/CDU3
MCDU3
FMS/CDU3
604 CMC
MCDU3
743A GNSS
750 VDR
GENERIC1
TEST
GENERIC2
ADC1
GENERIC3
ADC2
GENERIC4
Generic1 - 4 identifies up to four optional, generic input devices which can be included in a customer database.
PORT 3
(A) Top Plug 15C
(B) Top Plug 15D
NOT USED
740 PRINT
DHC8 IOP1
702 FMS1
750 VDR
GENERIC1
FMS/CDU1
741 SDU
DHC8 IOP2
702 FMS2
TEST
GENERIC2
FMS/CDU2
VM CMC
MCDU2
702 FMS3
ADC1
GENERIC3
FMS/CDU3
604 CMC
MCDU3
743A GNSS
ADC2
GENERIC4
PORT 4
(A) Top Plug 14A
(B) Top Plug 14B
NOT USED
740 PRINT
DHC8 IOP1
702 FMS1
750 VDR
GENERIC1
FMS/CDU1
741 SDU
DHC8 IOP2
702 FMS2
TEST
GENERIC2
FMS/CDU2
VM CMC
MCDU2
702 FMS3
ADC1
GENERIC3
FMS/CDU3
604 CMC
MCDU3
743A GNSS
ADC2
GENERIC4
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PORT 5
(A) Top Plug 14C
(B) Top Plug 14D
PORT 6
(A) Top Plug 13A
(B) Top Plug 13B
PORT 7
(A) Top Plug 13C
(B) Top Plug 13D
PORT 8
(A) Top Plug 12A
(B) Top Plug 12B
PORT 9
(A) Middle Plug 13B
(B) Middle Plug 13C
PORT 10
(A) Middle Plug 12D
(B) Middle Plug 13D
UL-801 Installation Manual
ARINC RX 1/3 (CONTINUED)
NOT USED
740 PRINT
DHC8 IOP1
702 FMS1
750 VDR
GENERIC1
NOT USED
740 PRINT
DHC8 IOP1
702 FMS1
750 VDR
GENERIC1
FMS/CDU1
741 SDU
DHC8 IOP2
702 FMS2
TEST
GENERIC2
FMS/CDU1
741 SDU
DHC8 IOP2
702 FMS2
TEST
GENERIC2
FMS/CDU2
VM CMC
MCDU2
702 FMS3
ADC1
GENERIC3
FMS/CDU2
VM CMC
MCDU2
702 FMS3
ADC1
GENERIC3
Press NEXT. ARINC RX 2/3 displays.
NOT USED
740 PRINT
DHC8 IOP1
702 FMS1
750 VDR
GENERIC1
NOT USED
740 PRINT
DHC8 IOP1
702 FMS1
750 VDR
GENERIC1
NOT USED
740 PRINT
DHC8 IOP1
702 FMS1
750 VDR
GENERIC1
NOT USED
740 PRINT
DHC8 IOP1
702 FMS1
750 VDR
GENERIC1
FMS/CDU1
741 SDU
DHC8 IOP2
702 FMS2
TEST
GENERIC2
FMS/CDU1
741 SDU
DHC8 IOP2
702 FMS2
TEST
GENERIC2
FMS/CDU1
741 SDU
DHC8 IOP2
702 FMS2
TEST
GENERIC2
FMS/CDU1
741 SDU
DHC8 IOP2
702 FMS2
TEST
GENERIC2
FMS/CDU2
VM CMC
MCDU2
702 FMS3
ADC1
GENERIC3
FMS/CDU2
VM CMC
MCDU2
702 FMS3
ADC1
GENERIC3
FMS/CDU2
VM CMC
MCDU2
702 FMS3
ADC1
GENERIC3
FMS/CDU2
VM CMC
MCDU2
702 FMS3
ADC1
GENERIC3
FMS/CDU3
604 CMC
MCDU3
743A GNSS
ADC2
GENERIC4
FMS/CDU3
604 CMC
MCDU3
743A GNSS
ADC2
GENERIC4
FMS/CDU3
604 CMC
MCDU3
743A GNSS
ADC2
GENERIC4
FMS/CDU3
604 CMC
MCDU3
743A GNSS
ADC2
GENERIC4
FMS/CDU3
604 CMC
MCDU3
743A GNSS
ADC2
GENERIC4
FMS/CDU3
604 CMC
MCDU3
743A GNSS
ADC2
GENERIC4
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PORT 11
(A) Middle Plug 3D
(B) Middle Plug 5D
PORT 12
(A) Middle Plug 3B
(B) Middle Plug 3C
PORT 13
(A) Top Plug 2C
(B) Top Plug 2D
PORT 14
(A) Top Plug 2A
(B) Top Plug 2B
PORT 15
(A) Middle Plug 10C
(B) Middle Plug 10D
PORT 16
(A) Middle Plug 13A
(B) Middle Plug 14A
UL-801 Installation Manual
ARINC RX 2/3 (Continued)
NOT USED
740 PRINT
DHC8 IOP1
702 FMS1
750 VDR
GENERIC1
NOT USED
740 PRINT
DHC8 IOP1
702 FMS1
750 VDR
GENERIC1
FMS/CDU1
741 SDU
DHC8 IOP2
702 FMS2
TEST
GENERIC2
FMS/CDU1
741 SDU
DHC8 IOP2
702 FMS2
TEST
GENERIC2
FMS/CDU2
VM CMC
MCDU2
702 FMS3
ADC1
GENERIC3
FMS/CDU2
VM CMC
MCDU2
702 FMS3
ADC1
GENERIC3
Press NEXT. ARINC RX 3/3 displays.
NOT USED
740 PRINT
DHC8 IOP1
702 FMS1
750 VDR
GENERIC1
NOT USED
740 PRINT
DHC8 IOP1
702 FMS1
750 VDR
GENERIC1
NOT USED
740 PRINT
DHC8 IOP1
702 FMS1
750 VDR
GENERIC1
NOT USED
740 PRINT
DHC8 IOP1
702 FMS1
750 VDR
GENERIC1
FMS/CDU1
741 SDU
DHC8 IOP2
702 FMS2
TEST
GENERIC2
FMS/CDU1
741 SDU
DHC8 IOP2
702 FMS2
TEST
GENERIC2
FMS/CDU1
741 SDU
DHC8 IOP2
702 FMS2
TEST
GENERIC2
FMS/CDU1
741 SDU
DHC8 IOP2
702 FMS2
TEST
GENERIC2
FMS/CDU2
VM CMC
MCDU2
702 FMS3
ADC1
GENERIC3
FMS/CDU2
VM CMC
MCDU2
702 FMS3
ADC1
GENERIC3
FMS/CDU2
VM CMC
MCDU2
702 FMS3
ADC1
GENERIC3
FMS/CDU2
VM CMC
MCDU2
702 FMS3
ADC1
GENERIC3
FMS/CDU3
604 CMC
MCDU3
743A GNSS
ADC2
GENERIC4
FMS/CDU3
604 CMC
MCDU3
743A GNSS
ADC2
GENERIC4
FMS/CDU3
604 CMC
MCDU3
743A GNSS
ADC2
GENERIC4
FMS/CDU3
604 CMC
MCDU3
743A GNSS
ADC2
GENERIC4
FMS/CDU3
604 CMC
MCDU3
743A GNSS
ADC2
GENERIC4
FMS/CDU3
604 CMC
MCDU3
743A GNSS
ADC2
GENERIC4
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UL-801 Installation Manual d) ARINC TRANSMIT
NOTE:
•
If any ARINC TX port is selected as 741 SDU, then SAT must be selected as the Normal or Alternate option in the PRIORITY (SYS
CONFIG 1/4 ) option page.
•
If an ARINC TX choice is displayed in small print and there is no arrow pointing to an LSK that selection is not available for use.
•
VOX tune bus can only be configured for one port.
PORT 4
(A) Top Plug 11A
(B) Top Plug 11B
PORT 4 SPEED
PORT 5
(A) Middle Plug 5B
(B) Middle Plug 5C
PORT 5 SPEED
ARINC TX 1/3
PORT 1
(A) Middle Plug 1A
(B) Middle Plug 1B
NOTE: Only TX port with a default.
PORT 1 SPEED
PORT 2
(A) Middle Plug 2A
(B) Middle Plug 2B
Ports 2-16 have no default settings.
PORT 2 SPEED
PORT 3
(A) Top Plug 15A
(B) Top Plug 15B
PORT 3 SPEED
FMS/CDU1
741 SDU
MCDU1
FMS/CDU2 FMS/CDU3 740 PRINT
VOX TUNE VM CMC 604 CMC
MCDU2 MCDU3 CVR
702 FMS1 702 FMS2 702 FMS3 750 VDR
TEST NOTE: Test is used by the Engineering Development only. DO NOT CONFIGURE.
LOW NOTE: LOW is the only configurable option.
FMS/CDU1 FMS/CDU2 FMS/CDU3 740 PRINT
741 SDU VOX TUNE VM CMC 604 CMC
MCDU1
702 FMS1
MCDU2 MCDU3 CVR
702 FMS2 702 FMS3 750 VDR
TEST
LOW
FMS/CDU1
741 SDU
MCDU1
HIGH
MCDU2 MCDU3
FMS/CDU2 FMS/CDU3 740 PRINT
VOX TUNE VM CMC
604 CMC
CVR
702 FMS1 702 FMS2 702 FMS3 750 VDR
TEST
LOW HIGH
Press NEXT.
ARINC TX 2/3 displays.
FMS/CDU1
741 SDU
FMS/CDU2 FMS/CDU3 740 PRINT
VOX TUNE VM CMC 604 CMC
MCDU1
702 FMS1
MCDU2 MCDU3 CVR
702 FMS2 702 FMS3 750 VDR
TEST
LOW
FMS/CDU1
HIGH
FMS/CDU2 FMS/CDU3 740 PRINT
741 SDU VOX TUNE VM CMC 604 CMC
MCDU1
702 FMS1
MCDU2 MCDU3 CVR
702 FMS2 702 FMS3 750 VDR
TEST
LOW HIGH
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PORT 6
(A) Middle Plug 9A
(B) Middle Plug 9B
PORT 6 SPEED
PORT 7
(A) Middle Plug 9C
(B) Middle Plug 9D
PORT 7 SPEED
PORT 8
(A) Middle Plug 15A
(B) Middle Plug 15B
PORT 8 SPEED
UL-801 Installation Manual
ARINC TX 2/3 (Continued)
FMS/CDU1
741 SDU
MCDU1
FMS/CDU2
MCDU2
FMS/CDU3
VOX TUNE VM CMC
MCDU3
740 PRINT
604 CMC
CVR
702 FMS1 702 FMS2 702 FMS3 750 VDR
TEST
LOW HIGH
Press NEXT.
ARINC TX 3/3 displays.
FMS/CDU1
741 SDU
FMS/CDU2 FMS/CDU3 740 PRINT
VOX TUNE VM CMC 604 CMC
MCDU1 MCDU2 MCDU3 CVR
702 FMS1 702 FMS2 702 FMS3 750 VDR
TEST
LOW HIGH
FMS/CDU1
741 SDU
MCDU1
702 FMS1
FMS/CDU2
VOX TUNE
MCDU2
702 FMS2
TEST
LOW HIGH
FMS/CDU3
VM CMC
MCDU3
702 FMS3
740 PRINT
604 CMC
CVR
750 VDR e) SERIAL
PORT 1
TX:
(+) Middle Plug 4A
(
−
)Middle Plug 4B
RX:
(+)Middle Plug 4C
(
−
)Middle Plug 4D
PORT 2
TX:
(+) Top Plug 8A
(
−
) Top Plug 8B
RX:
(+) Top Plug 8C
(
−
) Top Plug 8D
PORT 3
TX:
(+) Top Plug 9A
(
−
) Top Plug 9B
RX:
(+) Top Plug 9C
(
−
) Top Plug 9D
SERIAL 1/2
NOT USED LO-RES DISPLAY AERO-M PRINTER
VHF GND SIM SAT GND SIM
HI-RES DISPLAY 2 TEL SIM
IRIDIUM HI-RES DISPLAY 1
NOT USED
VHF GND SIM
LO-RES DISPLAY
SAT GND SIM
HI-RES DISPLAY 2 TEL SIM
AERO-M
IRIDIUM
PRINTER
HI-RES DISPLAY 1
NOT USED LO-RES DISPLAY AERO-M PRINTER
VHF GND SIM SAT GND SIM
HI-RES DISPLAY 2 TEL SIM
IRIDIUM HI-RES DISPLAY 1
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15 December 2011
PORT 4
TX:
(+) Top Plug 7A
(
−
) Top Plug 7B
RX:
(+) Top Plug 7C
(
−
) Top Plug 7D
PORT 5
TX:
(+) Top Plug 6A
(
−
) Top Plug 6B
RX:
(+) Top Plug 6C
(
−
) Top Plug 6D
PORT 6
TX:
(+) Top Plug 5A
(
−
) Top Plug 5B
RX:
(+) Top Plug 5C
(
−
) Top Plug 5D
UL-801 Installation Manual
Press NEXT. SERIAL 2/2 displays.
NOT USED
VHF GND SIM
LO-RES DISPLAY
SAT GND SIM
HI-RES DISPLAY 2 TEL SIM
AERO-M
IRIDIUM
PRINTER
HI-RES DISPLAY 1
NOT USED
VHF GND SIM
LO-RES DISPLAY
SAT GND SIM
HI-RES DISPLAY 2 TEL SIM
AERO-M
IRIDIUM
PRINTER
HI-RES DISPLAY 1
NOT USED
VHF GND SIM
LO-RES DISPLAY
SAT GND SIM
HI-RES DISPLAY 2 TEL SIM
AERO-M
IRIDIUM
PRINTER
HI-RES DISPLAY 1
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UL-801 Installation Manual f) GRAPHICS
•
Low Resolution Display Devices
These devices include all CDUs, MCDUs, RCDUs, MFD-640 (with MFD SCN
1011.4.7 or earlier). A maximum total of four display devices may be used within any of the three CDU graphics ports. For example:
EXAMPLE 1
CDU1 GRAPHICS DISP ON
CDU , RC DU
CDU2 GRAPHICS DISP ON
CDU
CDU3 GRAPHICS DISP ON
CDU
EXAMPLE 2
CDU1 GRAPH IC S D ISP ON
C DU, FPC DU
CDU2 GRAPHICS DISP ON
CD U, MFD-LR
CDU3 GRAPHICS DISP ON
ANY AD DITIONAL SELECTIONS WILL RESULT IN AN ERROR MESSAGE.
•
High Resolution Display Devices
These devices include all EFI-890Rs and MFD-640 (with MFD SCN 1011.4.8 or later). Additionally, a maximum total of two high resolution display devices may be included within any of the three CDU graphics ports. For example:
EXAMPLE 1
CDU1 GRAPHICS DISP ON
CDU , RC DU, HR1
CDU2 GRAPHICS DISP ON
CDU , HR 2
EXAMPLE 2
CDU1 GRAPH IC S D ISP ON
C DU, FPC DU, HR1
CDU2 GRAPHICS DISP ON
CD U, H R2
CDU3 GRAPHICS DISP ON
CDU
CDU3 GRAPHICS DISP ON
ANY AD DITIONAL SELECTIONS WILL RESULT IN AN ERROR MESSAGE.
•
CDU Graphics
CDU1 GRAPHICS DISP ON
Each display device selected here will display only what is displayed on CDU1.
Additionally, each HR display device selected here will display the same graphic but in a high resolution format.
CDU2 GRAPHICS DISP ON
Each display device selected here will display only what is displayed on CDU2.
Additionally, each HR display device selected here will display the same graphic but in a high resolution format.
CDU3 GRAPHICS DISP ON
Each display device selected here will display only what is displayed on CDU3.
Additionally, each HR display device selected here will display the same graphic but in a high resolution format.
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UL-801 Installation Manual
CDU/MFD BAUD RATE
Graphics Setup
CDU1 GRAPHICS DISP ON
There are no defaults. CDU option(s) do not need to be selected if weather graphics are not used.
LR = Low Resolution; HR = High Resolution
RCDU = Remote CDU
9600 BPS 19.2 KBPS
CDU
HR2
RCDU MFD-LR HR1
CDU2 GRAPHICS DISP ON
CDU3 GRAPHICS DISP ON
CDU
HR2
CDU
HR2
RCDU MFD-LR HR1
RCDU MFD-LR HR1
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UL-801 Installation Manual
VHF CONFIG 1/2
RADIO TYPE NONE INTERNAL VDR
Internal VDR must be selected if VHF is configured to other than
NONE.
ARINC 750 VDR
CONTACT TIMER ENABLED DISABLED
The contact timer verifies that the current VHF frequency is still usable when the channel has not had any uplink traffic received for a period of time. Enabling this option provides better media management performance.
TRACKER TIMER ENABLED DISABLED
The tracker timer provides flight following information to the DSP. This setting is enabled by default to provide better ACARS link management performance.
PREFERRED DSP NONE ARINC SITA AVICOM
NOTE: Although the Preferred DSP is selected with this option, the ARINC, SITA, and AVICOM options may also be enabled/disabled using the listed options. For further coverage information, contact your DSP.
ARINC
SITA
AVICOM
ENABLED
ENABLED
ENABLED
DISABLED
DISABLED
DISABLED
Press NEXT. VHF CONFIG 2/2 displays.
ENABLED MODE(S) POA/AOA AOA ONLY POA ONLY
MINIMUM SQP
(Minimum VHF Signal
Quality)
SQP THRESHOLD
Range is 3 – 15; 4
Range is 3 – 15; 12
VOICE FREQ CONTROL ENABLED 25KHZ ENABLED 8.33/25KHZ DISABLED
VOICE FREQ CONTROL must be set to DISABLED for the
UniLink 801.
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UL-801 Installation Manual
SAT CONFIG
TRACKER TIMER ENABLED DISABLED
The tracker timer provides flight following information to the service provider once every four hours during SatCom medium inactivity. This setting should be enabled to provide better ACARS link management performance.
This timer is applicable when UniLink is configured with an A741 SDU. If Iridium is configured as an AIRPHONE, the tracker timer is not active.
AUTO RETURN ENABLED DISABLED
If enabled, the UniLink attempts to re-establish the SatCom link every 10 minutes when in Satellite NOCOMM.
4. PRIORITY
NOTE:
•
If Aero-I SAT (ARINC 741) Packet Data Service is utilized, one of the
Normal/Alternate options must be set to SAT.
•
Alternate Comm Priority, which is used for Position Reporting only, overrides Normal Comm Priority.
COMM PRIORITY
NORMAL (Priority ranking scheme for up to three downlink communications links.)
1ST NONE VHF SAT TEL
2ND
3RD
NONE
NONE
ALTERNATE (Used for Position Reporting only.)
VHF
VHF
SAT
SAT
TEL
TEL
1ST
2ND
NONE
NONE
VHF
VHF
SAT
SAT
TEL
TEL
3RD NONE VHF SAT TEL
NOTES: • Alternate priority is only applied to automatic position reports in the UASC Corporate Customer
Database.
• Customers are able to limit Auto Position reports to only use the VHF media, SAT media, TEL media or any two media. Likewise, users can choose to send Auto Position reports via all three media options.
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UL-801 Installation Manual
TEL CONFIG 1/2
AIR PHONE
Used for dial up modem calls only and uses an RS-232 serial port configured for IRIDIUM or
AERO-M. It is primarily used for obtaining color weather maps but may also provide
VHF backup.
ACCESS NUMBER
The number dialed by the selected AIR
PHONE. Used to connect with the selected Datalink
Service Provider’s
MODEM bank.
WX MAPS
(Weather Maps)
If DISABLED is selected, it is required that NONE is selected in the AIR
PHONE section.
NONE
IRIDIUM
Baud rate selection applies to Iridium only. Select baud rate supported by the software version as follows:
•
•
•
Confirm the UniLink baud rate compatibility with the vendor and the selected DSP.
Baud rate must be one of the following:
2400 BPS
4800 BPS
9600 BPS
Contact the air phone manufacturer for baud rate compatibility with UniLink.
_________________________________ (Max 19 AN characters, 0-9, P,L, A)
The default value is to leave this field blank. Contact Universal Weather and Aviation to obtain the Access Number.
Contact your DSP for the access number shown on the TEL CONFIG 1/2 page.
A “P” may be entered to insert a pause, an “L” may be entered to insert “#”, or an “A” may be entered to insert “*” as required by the telephony network.
Subscription service for UniLink may be obtained through Universal Weather and
Aviation, Inc. at 1-801-231-5600.
ENABLED DISABLED
T-T AERO-M
When interfacing with Aero-M, configure the
Aero-M Data Port (via the Full Feature
Handset only, P/N 405621A) for 9600 baud,
Flow Control XON/XOFF, “+++”- Mode
Enable, Results Code Enabled and ARQ
Mode Enabled. Refer to the TT-3000 Aero-M
Installation Manual.
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UL-801 Installation Manual
SUSP MSG
(Suspend Message)
Enables or disables the invocation of the
TEL SUSPEND message following a
TEL SUSPEND event.
ENABLED
TEL CONFIG 1/2
DISABLED
Press NEXT. TEL CONFIG 2/2 displays.
REDIAL PAUSE
Redial Pause specifies the wait between telephony redial attempts from 5 to 60 seconds.
DIAL ATTEMPTS
Dial Attempts specifies the total number of dial attempts in a set from 1 to 6.
_____ Seconds (5-60 seconds; 30SEC)
_____ Attempts (1-6 attempts; 6)
AUTO-DELAY
Auto-Delay specifies the time between sets of redial attempts from 1 to 9 minutes.
_____ Minutes (1-9 minutes; 5MIN)
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UL-801 Installation Manual
These settings control the transmission of present position information while the aircraft is on the ground or in the air. These transmissions are sent to the DSP and may be used to provide flight following for aircraft tracking purposes. Transmission reporting time intervals
(INTV) may also be configured.
The POS REPORT message is periodic and defaults to every 15 minutes. If the aircraft is configured for VHF, then SAT in the normal priority over the ocean SAT would be used for the position report downlinks which could potentially be costly. In this case the alternate priority would have only VHF which would prevent the downlink of automatic POS
REPORT messages when VHF was in NO COMM (i.e. it wouldn't switch to trying SAT).
POS REPORT
AUTOMATIC REPORTING:
IN AIR
ON GROUND
IN AIR DEFAULT
When ENABLED is selected, the transmission of in air position reporting is always turned on by default.
When DISABLED is selected, the transmission of in air position reporting is always turned off by default. Automatic Position
Reporting can be enabled or disabled by the air crew during flight if necessary.
AIR INTV
(Air Interval)
Air intervals can be modified during flight but always return to the values stored in the configuration at power up.
GROUND INTV
(Ground Interval)
ENABLED
ENABLED
ENABLED
DISABLED
DISABLED
DISABLED
_________ MINS (Max 2 N characters); 15MIN (1 – 99 is acceptable)
_________ MINS (Max 2 N characters); 60MIN (1 – 99 is acceptable)
Press NEXT. The SYS CONFIG 2/4 page displays.
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UL-801 Installation Manual
C. SYS CONFIG 2/4
SYS CONFIG 2/4
MEDIA ADVIS
(Media Advisory)
ENABLED DISABLED
MET DATA
(Meteorological Data)
ENABLED DISABLED
By enabling Met Data for Corporate and American Eagle versions, meteorological data messages are reported to the ground once a Met data message uplink is received from the ground.
By enabling Met Data for the Air Nova version, meteorological data messages are reported upon enabling. An uplink is not required.
FLIGHT NO. ENABLED DISABLED
Enabling the Flight Number allows the entry and display of flight number data on the UniLink Main Menu. The
INIT advisory logic will be active when Flight Number is enabled. INIT advisory logic will prompt the user to enter
Flight No data on the MAIN menu page.
ENABLED DISABLED OOOI DATA
(Out, Off, On, In)
Enabling OOOI is recommended if
ARINC is selected as the preferred DSP.
TYPE (ICAO Designator)
__ __ __ __
(Max 4 AN characters) AIRCRAFT
The default value for any of the AIRCRAFT options is to leave the field blank.
ICAO Aircraft Type,
Aircraft Registration and Airline ID are required information.
REGISTRATION __ __ __ __ __ __ __ (Max 7 AN characters)
Valid Aircraft Registration may contain alpha characters upper case A through Z, numeric characters 0 through 9, a dash/hyphen character (which may not be the first or last character) and from 1 to 7 characters.
AIRLINE ID __ __ / __ __ __ (Max 2 AN characters/3 AN characters)
CLEARANCES
These settings determine Air Traffic
Services (ATS) functional options as elected by the customer.
FIN NUMBER
(Fleet Identifier Number)
__ __ __ (Max 3 AN characters)
ICAO ADDR __ __ __ __ __ __ __ __
Obtain the specific ICAO address from your DSP. This information is derived from the registration number of the aircraft.
OCEANIC
PUSHBACK
DEPARTURE
EXP TAXI
(Expected Taxi)
ENABLED
ENABLED
ENABLED
ENABLED
DISABLED
DISABLED
DISABLED
DISABLED
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ALERTS
UL-801 Installation Manual
SYS CONFIG 2/4 (Continued)
NEW MSG DISC DURATION
(New Message Discrete Duration)
ALERT1
ALERT2
CHIME1
CHIME2
INHIB ON GND
(Inhibit on Ground)
INHIB ALT
(Inhibit Altitude)
ALT TYPE
(Altitude Type)
AFTER OFF
Alerts are turned off during this configured time duration. 0MIN disables this timer, which allows the alerts to occur only above the configured
INHIB ALT value.
__________________
__________________
__________________
__________________
__________________
__________________
RADIO
RADIO type may only be configured when IOP bus input is used. When
RADIO is configured,
INHIB ALT must be 2500 feet or below.
__________________
MS (Max 4 N characters)
(Milliseconds); 100MS
MS (Max 4 N characters)
(Milliseconds); 100MS
MS (Max 4 N characters)
(Milliseconds); 100MS
MS (Max 4 N characters)
(Milliseconds); 100MS
KTS (Max 3 N characters)
(Knots); 50KTS
FT (Max 5 N characters)
(Feet); 10,000FT
BARO
MIN (Max 2 N characters)
(Minutes); 5MIN
The timer is off if set to 0MIN.
Press NEXT. The SYS CONFIG 3/4 page displays.
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D. SYS CONFIG 3/4
FANS requirements consist of the following:
•
The FMS must use SCN 1000.5/1100.5 or later.
•
UniLink must be connected to the UNS bus from the FMS (not A429 HS bus).
•
If FANS is enabled, the FMS must be configured with FANS enabled.
•
If FANS is disabled, the FMS must be configured with FANS disabled.
SYS CONFIG 3/4
FANS
If FANS is enabled, the FMS must be configured for it and must be at SCN
1000.5/1100.5 or later.
Special operational approval and crew training is required to use FANS.
ENABLED DISABLED
FANS AURAL
Works in conjunction with the FANS
AURAL output discrete and controls the duration of the FANS AURAL alert.
The default value is set to 0MS, which means that the Alerting device will remain active until the message that activated the alert has been viewed .
Therefore, it is recommended to set this time duration to some other value than
0MS. A value such as 5000MS
(5 seconds) may be suitable in most cases.
It is recommended to set this time duration to a specific value required to support correct operation of the aural alerting device, for example a
SONALERT or Aural Warning
Generating equipment.
A value of zero is not recommended as it can result in the loss of aural alerts from a new message received if an unread
CPDLC message already exists. A value such as 5000MS (5 seconds) may be suitable in most cases
______________
DELAY MSG TX
(Delay Message Transmission) ______________
MS (Max 4 N characters)
(Milliseconds); 0MS
MIN (Max 2 N characters)
(Minutes); 0MIN
Provides VHF message transmission delays, in minutes, in order to ensure a reliable Line of Sight
(LOS) connection after takeoff. Messages designated for delay (within the customer database) will be suppressed during VHF/SAT NOCOMM until the timer expires, at which time the message is routed for delivery over Telephony.
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SYS CONFIG 3/4 (Continued)
GROUND DELAY
______________
MIN (Max 2 N characters)
(Minutes); 0MIN
A Delay Advisory displays if a delay time other than zero is entered and the Delay Advisory time has elapsed since the occurrence of the OOOI Out event.
FANS LATENCY
ATC may instruct the crew to utilize a specific value. It’s recommended that the value be configured for 0 (zero).
0 = latency is turned off.
______________
SUPP ADDR
(Supplemental Address) ______________
Obtain a specific SUPP ADDRESS from your DSP .
SEC (Max 3 N characters)
(Seconds); 0SEC
Range = 0 - 999
(Max 7 AN characters); the default value is to leave the field blank.
Press NEXT. The SYS CONFIG 4/4 page displays. This page displays the log of the recent
Config Module Updates, which is organized by Date and Time columns.
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The Flight Management System (FMS) must be configured to use the UniLink
Communications Unit before you configure the UniLink system. Refer to the WAAS/SBAS
FMS Configuration Manual, report number 34-61-01, for FMS configuration procedures.
NOTE:
•
The UASC FMS ARINC receiver port that receives data from the UniLink must be configured for UniLink. Only one receiver port on each FMS may be configured for a datalink device. UniLink and AFIS are mutually exclusive.
Only one may be configured.
•
The FMS transmitter port that supplies data to the UniLink must be configured for UNS HS429-1. UNS HS429-1 is mandatory for FANS-capable installations.
The screens throughout these procedures depict a FANS-enabled UniLink. Some screens will appear differently without FANS.
A. Starting the FMS
In order to access the UniLink menu, press the ON/OFF/DIM key on the faceplate of the
FMS to turn it on. The FMS displays the following:
1.
FMS self-test page.
UNS - 1
-------------------------
CPU
RAM
PASS
PASS
DATABASE BANK # 100%
CONFIG MODULE
AUXILIARY
WAAS/ARINC
NOTE: The DATABASE BANK field displays the number of the bank being tested and the percentage complete. When successfully finished, the numbers change to the word PASS and the FMS proceeds to the CONFIG MODULE test. All tests display as PASS if the self-test completes correctly.
2.
FMS copyright page.
COPYRIGHT 2010
UNIVERSAL AVIONICS
SYSTEMS CORPORATION
ALL RIGHTS RESERVED
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3.
INIT 1/1 menu.
POS INIT 1/1 Â
date initial pos 23-AUG-11 id ------ utc
N 40 51.01 14:49:45
W 074 03.65
nav database expires
26-AUG-11
¬ACCEPT fmc ver 1000.5
a.
LSK [1L] field is highlighted. Enter the local airport identifier. b.
Press ENTER.
4.
Local Airport Identifier window.
POS KTUS 1/ 1
tucson intl
NAV N 32 06.97
ARPT W 110 56.46
elev 2643 mag var E 12.0
¬ACCEPT a.
Press the ACCEPT LSK [5L]. b.
The INIT 1/1 menu displays. c.
Press the ACCEPT LSK [5L]. d.
Press the DATA key.
5.
DATA 1/4 menu.
DATA 1/4
¬NAV DATA
¬PILOT DATA
UNILINK®
¬DISK
MAINT® a.
Press the UNILINK LSK [3R].
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6.
UNILINK menu.
•
FANS-Enabled FANS-Disabled
If FANS is enabled, the top menu line
•
If FANS is disabled, the top menu line displays UNILINK MENU. After the
UniLink is configured, a different set of displays UNILINK MENU 1/2. Press the
NEXT key to access UNILINK MENU configuration options may be displayed 2/2. than in the FANS-Disabled menu. •
Additional options may appear at LSK
[1L], LSK [3L], LSK [2R], and LSK
[3R] depending which choices were made during configuration.
UNILINK MENU
¬FLIGHT INFO OPS®
¬ATC
¬COMM STATUS
flight no.
¬MAINTENANCE ----
¡¢z
¬NOCOMM RETURN®
FANS-Enabled
UNILINK MENU 1/2
TEXT WX®
¬FREE-TEXT
¬COMM STATUS MSG LOGS®
¡¢z
RETURN®
FANS-Disabled
NOTE: The NOCOMM option may display at LSK [5R] for either a FANS-enabled or
FANS-disabled UniLink. This option also displays as SAT NOCOMM,
TEL NOCOMM, or VHF NOCOMM, depending on which communications link
UniLink has lost.
7.
UNILINK 2/2 menu for FANS-Disabled.
UNILINK MENU 2/2
¬DELAY
¬DIVERSION SITUATION®
¬ETA UPDATE POS REPORT®
¬MAINTENANCE
¡¢z
RETURN®
FANS-Disabled
8.
Press the MAINTENANCE LSK [4L] on either the FANS-enabled or FANS-disabled menu.
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Use the completed worksheets, found in the Configuration Worksheets section, and enter that information into UniLink. Work through all the UniLink menus and make any necessary modifications for the configuration.
The steps should be performed in the order indicated by the large number in the corner of the text box.
Some of the items configured are limited to a small number of options that are selectable by pressing a line select key (LSK). The options appear one at a time in a set sequence and are included in the text of the step.
Other items that may be configured are limited to more than a few options. These items are selected by typing the number of the option as presented in a numbered list.
For those items that have many possible configurations, make an entry in a fill-in field. For example, the ICAO has assigned hundreds of aircraft type designators. These type designators consist of not more than four characters. On the Aircraft Configuration page the aircraft type field allows entry of up to four characters.
If an entry field is not highlighted, press the corresponding line select key to move the cursor highlight to the field.
B. FANS Block Data Transmission
FMS SCN 1000.5/1100.5 or later is capable of transmitting FANS-specific data to support the UniLink FANS functions. In order to enable the transmission of the FMS FANS-specific data, ensure the FMS is configured to transmit over the UNS HS429-1 Bus.
1.
Press the DATA key to display the DATA 1/4 page.
2.
Press the PREV key to display the DATA 4/4 page.
3.
Press DATE to highlight the date.
4.
Enter 456789 and then press the ENTER key. The date will revert to the actual initialized date.
5.
Press the NEXT key to display the DATA 1/4 page.
6.
Press MAINT to display the MAINT 1/1 page.
7.
Press CONFIG to display the CONFIG 1/2 page. The EDIT prompt at LSK [1R] is not normally displayed, but is displayed now because the configuration has been unlocked by entering the code on the DATA 4/4 page.
8.
Press EDIT to replace EDIT with STORE and allow FMS configuration settings to be changed.
9.
Press FMS CONFIG. Access the FMS CONFIG 2/4 page.
10.
Press CMU. Enable FANS block data transmission.
11.
Press STORE twice to restart the FMS.
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C. Storing UniLink Options
When all new or modified UniLink options have been entered, the installer can review the configuration by pressing the REVIEW LSK [4R] on the UniLink SYS CONFIG 1/4 page.
This provides easy access to review and confirm any configuration warning from the
UniLink.
If all modifications are acceptable, press the STORE LSK [1R]. Wait a few seconds and press the STORE LSK again. This stores the entered information, and verifies that required dependencies and consistency exist between the Configuration Data and the software, and also among the Configuration Data items. UniLink will initialize and the FMS will display the following message:
UNILINK/FMS
COMM ERROR
RESELECT UNILINK
¬UNILINK
UNILINK, LSK [5L], displays in small capitals. Once the UniLink has rebooted and is ready to process additional information, the word UNILINK redisplays in large capital letters.
Pressing the UNILINK LSK [5L] returns the FMS to the UNILINK MENU.
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D. Configuration Edit Mode
The Configuration Worksheets, found in the Configuration Worksheet section, should have been completed. These worksheets contain the options needed to configure UniLink. Have these worksheets available when implementing the following procedures.
(1) Selecting the UniLink Display Page
1
On the FMS, press [DATA] to display the DATA 1/4 page.
DATA 1/4
¬NAV DATA
¬PILOT DATA
UNILINK®
¬DISK
MAINT®
2
Press UNILINK [3R] to display the UNILINK
MENU page.
3
Press MAINTENANCE [4L] to display the
MAINTENANCE 1/3 page.
MAINTENANCE 1/3
¬DEVICE STATUS CONFIG®
¬SENSOR STATUS TESTS®
¬VERSIONS POWER LOG®
¬ERROR LOG
--:--z
¬UNILINK MENU RETURN®
UNILINK MENU
¬FLIGHT INFO OPS®
¬ATC
¬COMM STATUS
flight no.
¬MAINTENANCE ----
¡¢z
¬NOCOMM RETURN®
4
Press CONFIG [1R] to display the SYS CONFIG
1/4 page.
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(2) Edit/Store Mode
UL-801 Installation Manual
1
Push LSK [1R] to highlight the data entry field. Type in the password 456789 and push
ENTER. The password will be replaced with the word EDIT and EDIT mode is enabled.
SYS CONFIG 1/4
¬I/O CONFIG -----®
¬VHF CONFIG TEL CONFIG®
¬SAT CONFIG POS REPORT®
¬PRIORITY REVIEW®
--:--z
¬UNILINK MENU RETURN®
SYS CONFIG 1/4
¬I/O CONFIG EDIT®
¬VHF CONFIG TELEPHONE®
¬SAT CONFIG POS REPORT®
¬PRIORITY REVIEW®
--:--z
¬UNILINK MENU RETURN®
2
Push EDIT [1R]. The word EDIT is replaced with the word STORE. Do not push STORE [1R] again until the configuration is complete.
NOTE: Even though the LSK displays
STORE, EDIT mode is active.
NOTE: The FMS must be in an On
Ground condition while you configure the UniLink. The data entry field at [1R] will not be accessible if the UniLink detects a Weight Off Wheels condition.
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1
Press the NEXT key on the
FMS to display the SYS
CONFIG 2/4 page.
2
SYS CONFIG 2/4 media advis enabled STORE® met data disabled AIRCRAFT® flight no.
disabled CLEARANCES® oooi data disabled ALERTS®
--:--z
¬UNILINK MENU
Press LSK [1L] thru [4L] and select the ENABLED or DISABLED option for each item.
4
Press [1L] to highlight the TYPE data entry field. Enter the Type and press ENTER.
3
Press AIRCRAFT [2R] to display the
AIRCRAFT page.
5
Repeat Step 4 on LSKs
[2L], [3L], and [4L] respectively for
REGISTRATION, AIRLINE ID, and FIN NUMBER. Press
[2R] to highlight the
ICAO ADDR field. Enter the ICAO ADDR and press
ENTER.
AIRCRAFT type
---- STORE® registration icao addr
------- --------
º airline id
--/--fin number
---
--:--z
6
Press RETURN [5R] to return to the SYSTEM CONFIG 2/4 page.
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F. Clearances
SYS CONFIG 2/4 media advis enabled STORE® met data disabled AIRCRAFT® flight no disabled CLEARANCES® oooi data disabled ALERTS®
--:--z
¬UNILINK MENU
1
Press CLEARANCES [3R] to display the
CLEARANCES page.
2
Press LSK [2L] and select the ENABLED or
DISABLED option for each item. Repeat for
LSK [3L].
CLEARANCES
STORE® oceanic departure disabled disabled pushback exp taxi disabled disabled
--:--z
¬UNILINK MENU RETURN®
3
Press LSK [2R] and select the ENABLED or DISABLED option for each item.
Repeat for LSK [3R].
4
Press RETURN [5R] to return to the SYS CONFIG 2/4 page.
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G. Alerts
SYS CONFIG 2/4 media advis enabled STORE® met data disabled AIRCRAFT® flight no disabled CLEARANCES® oooi times disabled ALERTS®
--:--z
¬UNILINK MENU
1
Push ALERTS [4R] to display the ALERTS page.
2
Push LSK [2L] to highlight the data entry field.
Enter a value for ALERT1.
Push ENTER to move the cursor to the ALERT2 field.
Continuing to push the ENTER key moves the cursor to the
CHIME1, CHIME2, INHIB ON GND,
INHIB ALT, and AFTER OFF fields. Values may be entered in these fields or left as the default if no value is entered.
3
A value for ALT TYPE can only be entered by pushing
LSK [4R] and then entering a value.
ALERTS new msg disc duration: STORE® alert¡ alert inhib alt
¡ººms ¡ººms {¡ººººft chime¡ chime alt type
¡ººms ¡ººms baro inhib on gnd after off
}ºkts min
--:--z
RETURN®
4
Push RETURN [5R] to return to the SYS CONFIG 2/4 page.
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1
Push NEXT on the FMS keypad to display the
SYS CONFIG 3/4 page.
SYS CONFIG 3/4 fans enabled STORE® fans aural fans latency
ºms ºsec delay msg tx supp addr
ºmin ------ground delay
ºmin
--:--z
¬UNILINK MENU
2
Push LSK [1L] to toggle enabled/disabled in the FANS field.
Push ENTER to move the cursor to the FANS AURAL field. Push LSK [2L] and enter a value. Continuing to push the ENTER key moves the cursor to the DELAY MSG TX, GROUND DELAY,
FANS LATENCY, and SUPP ADDR fields.
Values may be entered in these fields or left as the default if no value is entered.
NOTE : Pushing ENTER cycles through all fields except the FANS field.
LSK [1L] must be pushed in order to enter a value in the FANS field.
3
Push NEXT twice to return to the SYS CONFIG 1/4 page.
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1
Press I/O CONFIG [1L] to display the I/O CONFIG page.
SYS CONFIG 1/4
¬I/O CONFIG STORE®
¬VHF CONFIG TEL CONFIG®
¬SAT CONFIG POS REPORT®
¬PRIORITY REVIEW®
--:--z
¬UNILINK MENU
I/O CONFIG
¬DISCRETE IN SERIAL®
¬DISCRETE OUT GRAPHICS®
¬ARINC RECEIVE
¬ARINC TRANSMIT
º§z
¬UNILINK MENU RETURN®
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(1) Discrete In
1
Press DISCRETE IN [1L] to display the DISC IN 1/4 page.
I/O CONFIG
¬DISCRETE IN SERIAL®
¬DISCRETE OUT GRAPHICS®
¬ARINC RECEIVE
¬ARINC TRANSMIT
º§z
¬UNILINK MENU RETURN®
2
Press LSK [2L] to configure
DISC IN 1. The DISC IN OPT 1/2 page displays with a list of all available options.
DISC IN 1/4
STORE® disc in ¡ active state not used ground disc in active state not used ground disc in £ active state not used ground
º§z
¬UNILINK MENU RETURN®
DISC IN OPT 1/2
¡ not used
brake set
£ strut comp
¢ test
select
#-
door ¡ closed
§ door closed
¶ door £ closed
º§z
¬UNILINK MENU RETURN®
3
Enter the number of the desired option and press
ENTER. The DISC IN 1/4 page displays.
NOTE: Press the NEXT or PREV key to toggle between DISC IN OPT pages 1 and 2.
4
Press LSK [2R] and toggle the active state of the DISC IN 1 between
GROUND and OPEN.
5
Press NEXT to display the next DISC IN page and repeat steps 2 , 3 and 4 until all 10 discrete inputs are set.
Press RETURN [5R].
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(2) Discrete Out
1
Press DISCRETE OUT
[2L] to display the
DISC OUT 1/5 page.
I/O CONFIG
¬DISCRETE IN SERIAL®
¬DISCRETE OUT GRAPHICS®
¬ARINC RECEIVE
¬ARINC TRANSMIT
º§z
¬UNILINK MENU RETURN®
2
Press LSK [2L] to configure
DISC OUT 1. The DISC OUT OPT
1/2 page displays with a list of all available options.
DISC OUT 1/5
STORE® disc out ¡ active state not used ground disc out active state not used ground disc out £ active state not used ground
--:--z
¬UNILINK MENU RETURN®
DISC OUT OPT 1/2
select
¡ not used #-
vox annun
£ new msg ¡
¢ new msg
vhf nocomm
§ sat nocomm
¶ tel nocomm
--:--z
¬UNILINK MENU RETURN®
DISC OUT OPT 2/2
select
¡ vdr box sel #-
chime ¡
£ chime
¢ fans visual
fans aural
§ cpdlc cnect
--:--z
¬UNILINK MENU RETURN®
3
4
Enter the number of the desired option and press
ENTER. For more options, press NEXT to display the the DISC OUT OPT 2/2 page.
Press LSK [2R] and toggle the active state of the DISC OUT 1 between GROUND and OPEN.
5
Repeat steps 2 , 3 , and 4 until all
14 discrete outputs are set and then press RETURN [5R].
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(3) ARINC Receive
1
Press ARINC RECEIVE [3L] to display the ARINC RX
1/3 page.
2
Press LSK [2L] to configure
PORT 1. The ARINC RX OPT page displays with a list of the available options for Port 1.
NOTE: Choosing Ports 2 - 16 displays one of ARINC RX
OPT 1/4 pages.
ARINC RX OPT
select
¡ fms/cdu¡ #-
fms/cdu
£ fms/cdu£
¢ mcdu¡
mcdu
§ mcdu£
I/O CONFIG
¬DISCRETE IN SERIAL®
¬DISCRETE OUT GRAPHICS®
¬ARINC RECEIVE
¬ARINC TRANSMIT
--:--z
¬UNILINK MENU RETURN®
ARINC RX 1/3
STORE® port ¡ port ¢ fms/cdu¡ not used port port
¶¢¡ sdu not used port £ port § not used not used
--:--z
¬UNILINK MENU RETURN®
3
Enter the number of the desired option for port 1 and press ENTER.
This automatically returns you to the ARINC RX 1/3 page. Select another port to configure. The
ARINC RX OPT 1/4 page displays.
4
After configuring all the ports on the chosen ARINC RX OPT page, press NEXT to go to the next ARINC
RX OPT page.
ARINC RX OPT 1/4
select
¡ not used #-
fms/cdu
£ fms/cdu£
¢ ¶¢º print
¶¢¡ sdu
§ vm cmc
¶ §º¢ cmc
--:--z
RETURN®
ARINC RX OPT 2/4
select
¡ dhc iop¡ #-
dhc iop
£ mcdu¡
¢ mcdu
mcdu£
§ ¶º fms¡
¶ ¶º fms
--:--z
RETURN®
ARINC RX OPT 3/4
select
¡ ¶º fms£ #-
¶¢£a gnss
£ ¶º vdr
¢ test
adc¡
§ adc
¶ generic¡
--:--z
RETURN®
5
Repeat steps 2 and 3 until all
16 ARINC RX ports are set and then push RETURN [5R].
ARINC RX OPT 4/4
select
¡ generic #-
generic£
£ generic¢
--:--z
RETURN®
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(4) ARINC Transmit
1
Press ARINC TRANSMIT [4L] to display the ARINC TX 1/3 page.
I/O CONFIG
¬DISCRETE IN SERIAL®
¬DISCRETE OUT GRAPHICS®
¬ARINC RECEIVE
¬ARINC TRANSMIT
--:--z
¬UNILINK MENU RETURN®
2
PORT 1 SPEED defaults to LOW.
Press PORT 2 SPEED [3L] and select the LOW or HIGH speed option. Repeat for the rest of the ARINC
TX ports. Ports 4 - 8 are on ARINC TX pages 2 and 3.
4
Press LSK [1L] and <*> appears to indicate that the item is selected. Press the
LSK again and <*> disappears.
Repeat for each device.
ARINC TX 1/3
STORE® port ¡ speed devices low PORT 1® port speed low PORT 2® port £ speed low PORT 3®
--:--z
¬UNILINK MENU RETURN®
3
Press PORT 1 [2R] to display the
ARINC TX OPT 1/3 page. A list of devices available for each of the
ARINC TX ports displays.
ARINC TX OPT 1/3 port ¡
¬FMS/CDU1<*> 741 SDU®
¬FMS/CDU2 VOX TUNE®
¬FMS/CDU3 VM CMC®
¬740 PRINT 604 CMC®
--:--z
¬UNILINK MENU RETURN®
5
Press NEXT to display ARINC
TX 2/3 and follow the procedure in step 4. Press NEXT again to display
ARINC TX 3/3. Once all ARINC TX ports are configured, press RETURN twice to return to the I/O CONFIG page.
NOTE: Multiple port devices can be configured on a single port but no device may be configured so that it resides on more than one port.
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UL-801 Installation Manual
(5) Serial Port Configuration
I/O CONFIG
¬DISCRETE IN SERIAL®
¬DISCRETE OUT GRAPHICS®
¬ARINC RECEIVE
¬ARINC TRANSMIT
--:--z
¬UNILINK MENU RETURN®
1
Press SERIAL [1R] to display the SERIAL 1/2 page.
Press PORT 1 [1L] to display the SERIAL OPT 1/2 page.
SERIAL OPT 1/2
select
¡ not used #-
lo-res display
£ aero-m
¢ printer
vhr gnd sim
§ sat gnd sim
¶ iridium
--:--z
RETURN®
SERIAL 1/2 port ¡ not used STORE® port not used port £ not used port ¢ not used
--:--z
¬UNILINK MENU RETURN®
3
Type the number of the desired option and press ENTER. This returns you to the SERIAL 1/2 page.
For more options, press NEXT to display the SERIAL OPT 2/2 page.
SERIAL OPT 2/2
select
¡ hi-res display ¡ #-
hi-res display
£ tel sim
--:--z
RETURN®
4
Repeat steps 2 and 3 for each of the six serial ports.
Once all serial ports are configured, press RETURN to display the I/O CONFIG page.
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(6) Graphics
I/O CONFIG
¬DISCRETE IN SERIAL®
¬DISCRETE OUT GRAPHICS®
¬ARINC RECEIVE
¬ARINC TRANSMIT
--:--z
¬UNILINK MENU RETURN®
2
Press CDU/MFD BAUD RATE [1L] to toggle between 9600BPS and
19.2KBPS.
1
Press GRAPHICS [2R] to display the GRAPHICS page.
3
Press LSK [2L] to display and select the graphics configuration for CDU1.
GRAPHICS cdu/mfd baud rate
¡ª.kbps STORE® cdu¡ graphics disp on
cdu graphics disp on
cdu£ graphics disp on
-
--:--z
¬UNILINK MENU RETURN®
4
Graphics options are CDU, RCDU,
MFD-LR, HR1, and HR2. An <*> appears to indicate that the item is selected.
Press the LSK again and <*> disappears.
All or none of the options may be chosen.
Press RETURN to return to the
GRAPHICS page.
CDU# GRAPHICS
¬CDU<*> HR1®
¬RCDU HR2®
¬MFD-LR
--:--z
¬UNILINK MENU RETURN®
5
When all CDU graphics displays are configured, press RETURN twice to return to the
SYS CONFIG 1/4 page.
6
Repeat steps 3 and 4 for CDU2 and CDU3.
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2
1 to display the VHF
CONFIG 1/2 page.
UL-801 Installation Manual
Push VHF CONFIG [2L]
Push RADIO TYPE [1L] to cycle through the RADIO TYPE options.
Push all other configuration options to cycle through and choose the options.
3
Push NEXT to display the VHF
CONFIG 2/2 page.
4
Push ENABLED MODE(S) [1L] to cycle through the ENABLED
MODE(S) options. Push all other configuration options to cycle through and choose the options.
5
Push RETURN to display the SYS
CONFIG 1/4 page.
SYS CONFIG 1/4
¬I/O CONFIG STORE®
¬VHF CONFIG TEL CONFIG®
¬SAT CONFIG POS REPORT®
¬PRIORITY
--:--z
¬UNILINK MENU REVIEW®
VHF CONFIG 1/2 radio type
INTERNAL VDR STORE® contact timer arinc
ENABLED DISABLED tracker timer sita
ENABLED DISABLED preferred dsp avicom
NONE DISABLED
--:--z
¬UNILINK MENU RETURN®
VHF CONFIG 2/2 enabled mode(s)
POA/AOA STORE® minimum sqp
4 sqp threshold
12 voice freq control
DISABLED
--:--z
¬UNILINK MENU RETURN®
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1
Press SAT CONFIG [3L] to display the SAT
CONFIG page.
2
Press TRACKER TIMER
[1L] and select ENABLED or DISABLED. Press AUTO
RETURN [2L] and select
ENABLED or DISABLED.
3
Press RETURN [5R] to the
SYS CONFIG 1/4 page.
UL-801 Installation Manual
SYS CONFIG 1/4
¬I/O CONFIG STORE®
¬VHF CONFIG TEL CONFIG®
¬SAT CONFIG POS REPORT®
¬PRIORITY REVIEW®
--:--z
¬UNILINK MENU
SAT CONFIG tracker timer
ENABLED auto return
ENABLED
STORE®
--:--z
¬UNILINK MENU RETURN®
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1
Press PRIORITY [4L] to display the COMM
PRIORITY page.
2
Press 1ST [2L] to cycle through the NORMAL options.
Based on which option is chosen, not all options will be seen for each choice. Repeat for 2ND [3L] and 3RD [4L].
UL-801 Installation Manual
SYS CONFIG 1/4
¬I/O CONFIG STORE®
¬VHF CONFIG TEL CONFIG®
¬SAT CONFIG POS REPORT®
¬PRIORITY REVIEW®
--:--z
¬UNILINK MENU
COMM PRIORITY
STORE® normal alternate
¬¡st sat none ¡st®
¬nd none none nd®
¬£rd none none £rd®
--:--z
¬UNILINK MENU RETURN®
3
Press 1ST [2R] to cycle through the ALTERNATE options. Based on which option is chosen, not all options will be seen for each choice. Repeat for 2ND
[3R] and 3RD [4R].
4
Press RETURN [5R] to show the
SYS CONFIG 1/4 page.
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UL-801 Installation Manual
SYS CONFIG 1/4
¬I/O CONFIG STORE®
¬VHF CONFIG TEL CONFIG®
¬SAT CONFIG POS REPORT®
¬PRIORITY REVIEW®
--:--z
¬UNILINK MENU
2
Press AIR PHONE [1L] to select the option for telephony communications.
1
Press TEL CONFIG [2R] to display the TEL CONFIG 1/2 page .
3
Press ACCESS NUMBER [2L] and enter up to 19 alphanumeric characters for the primary telephone access number.
Press ENTER when completed.
NOTE: Contact your DSP to obtain the correct access number.
TEL CONFIG 1/2 air phone
IRIDIUM STORE® access number
------------------wx maps
DISABLED BAUD RATE
¢ººbps susp msg
ENABLED
--:--z
4
Press WX MAPS [3L] to toggle the ENABLED or DISABLED option for each. Repeat for
SUSP MSG [4L].
NOTE: If IRIDIUM is chosen as the AIR
PHONE option, WX MAPS, in the window above, displays a BAUD RATE option that can be selected at LSK [3R].
5
Press NEXT to display the
TEL CONFIG 2/2 page.
Press REDIAL PAUSE [1L] and enter a pause of 5 to 60 seconds.
Press DIAL ATTEMPTS [2L] and enter a number of dial attempts of 1 to 6.
Press AUTO-DELAY [3L] and enter a delay of 1 to 9 minutes.
TEL CONFIG 2/2 redial pause
£ºsec STORE® dial attempts
§ auto-delay
min
--:--z
¬UNILINK MENU RETURN®
6
Press RETURN [5R] to display the SYS CONFIG 1/4 page.
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UL-801 Installation Manual
SYS CONFIG 1/4
¬I/O CONFIG STORE®
¬VHF CONFIG TEL CONFIG®
¬SAT CONFIG POS REPORT®
3
Press ON GROUND [3L] and and select
ENABLED OR DISABLED.
1
Press POS REPORT [3R] to display the POS
REPORT page.
¬PRIORITY REVIEW®
--:--z
¬UNILINK MENU
2
Press AUTOMATIC
REPORTING: IN AIR
[2L] and select
ENABLED OR DISABLED.
POS REPORT automatic reporting: in air
DISABLED in air default
STORE®
air intv
ENABLED 15MINS on ground ground intv
60MINS
DISABLED
--:--z
¬UNILINK MENU RETURN®
4
Press IN AIR DEFAULT [4L] and select ENABLED OR
DISABLED.
5
Press AIR INTV [2R] and enter the number of minutes.
6
Press GROUND INTV [3R] and enter the number of minutes.
7
Press RETURN [5R] to display the SYS CONFIG 1/4 page and perform the Configuration
Review.
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SYS CONFIG 1/4
¬I/O CONFIG STORE®
¬VHF CONFIG TEL CONFIG®
¬SAT CONFIG POS REPORT®
¬PRIORITY REVIEW®
--:--z
¬UNILINK MENU
1
Press REVIEW [4R] to display the REVIEW 1/22 page.
NOTE: The REVIEW pages are a visual representation of the contents of the
UniLink Configuration Module. After reviewing all pages for errors, press
NEXT on the keypad to return to the REVIEW Page 1. If the configuration is correct, press RETURN LSK [5R] to display SYS CONFIG 1/4.
Press STORE [1R] twice to save the configuration. If errors were noted during the review, it will be necessary to return to the appropriate configuration page to make the changes.
REVIEW 1/22 discrete in: disc in
,
active state
º¡:not used
º:not used
,
ground
ground
¬PRINT SEND®
--:--z
¬UNILINK MENU RETURN®
2
Press SEND [4R] to transmit a
Configuration Report downlink.
NOTE: When SEND is pressed, the
QUEUED message displays over the
SEND LSK.
3
Press NEXT to display the each sequential review page.
REVIEW 2/22
º£:not used
º¢:not used
º:not used
º§:not used
º¶:not used
º:not used
ºª:not used
¡º:not used
,
,
,
,
,
,
,
,
ground
ground
ground
ground
ground
ground
ground
ground
--:--z
¬UNILINK MENU RETURN®
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REVIEW 3/22 discrete out: disc out active state
º¡:not used
º:not used
º£:not used
º¢:not used
º:not used
,
,
,
,
ground
ground
ground
ground
ground
--:--z
¬UNILINK MENU RETURN®
UL-801 Installation Manual
REVIEW 4/22
º§:not used
º¶:not used
º:not used
ºª:not used
¡º:not used
¡¡:not used
¡:not used
¡£:not used
,
,
,
,
,
,
,
,
ground
ground
ground
ground
ground
ground
ground
ground
--:--z
¬UNILINK MENU RETURN®
REVIEW 5/22
¡¢:not used
,
ground arinc rx: rx port º¡:fms/cdu¡ rx port º:not used rx port º£:not used rx port º¢:not used rx port º:not used
--:--z
¬UNILINK MENU RETURN®
REVIEW 6/22 rx port º§:not used rx port º¶:not used rx port º:not used rx port ºª:not used rx port ¡º:not used rx port ¡¡:not used rx port ¡:not used rx port ¡£:not used
--:--z
¬UNILINK MENU RETURN®
REVIEW 7/22 rx port ¡¢:not used rx port ¡:not used rx port ¡§:not used arinc tx: tx port º¡:fms/cdu¡
speed:low tx port º:--------
--:--z
¬UNILINK MENU RETURN®
REVIEW 9/22
speed:low tx port º¶:--------
speed:low tx port º:--------
speed:low serial: port ¡: not used
--:--z
¬UNILINK MENU RETURN®
REVIEW 8/22
speed:low tx port º£:--------
speed:low tx port º¢:--------
speed:low tx port º:--------
speed:low tx port º§:--------
--:--z
¬UNILINK MENU RETURN®
REVIEW 10/22 port : not used port £: not used port ¢: not used port : not used port §: not used graphics: cdu/mfd baud:¡ª.kbps
--:--z
¬UNILINK MENU RETURN®
REVIEW 11/22 cdu¡:----------cdu:----------cdu£:----------vhf config: radio:none contact timer:enabled tracker timer:enabled
--:--z
¬UNILINK MENU RETURN®
REVIEW 12/22 preferred dsp:none arinc:disabled sita:disabled avicom:disabled enabled mode:poa/aoa minimum sqp:¢ sqp threshold:¡
--:--z
¬UNILINK MENU RETURN®
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REVIEW 13/22 voice freq ctrl:
disabled sat config: tracker timer:disabled auto return:disabled comm priority:
--:--z
¬UNILINK MENU RETURN®
UL-801 Installation Manual
REVIEW 14/22 normal ¡st:vhf normal nd:none normal £rd:none alternate ¡st:none alternate nd:none alternate £rd:none tel config:
--:--z
¬UNILINK MENU RETURN®
REVIEW 15/22 air phone:none access number:
-------------------wx maps:disabled susp msg:enabled baud rate:¢ººbps redial pause:£ºsec dial attempts:§
--:--z
¬UNILINK MENU RETURN®
REVIEW 16/22 auto-delay:min pos report: in air:enabled on ground:disabled in air default:disabled air intv:¡min ground intv:§ºmin
--:--z
¬UNILINK MENU RETURN®
REVIEW 17/22 sys config ÷¢: media advis:enabled met data:disabled flight no.:disabled oooi data:disabled aircraft:
--:--z
¬UNILINK MENU RETURN®
REVIEW 18/22 type:---registration:------airline id:--÷--fin number:--icao addr:-------clearances: oceanic:disabled
--:--z
¬UNILINK MENU RETURN®
REVIEW 19/22 pushback:disabled departure:disabled exp taxi:disabled alerts: alert¡:ººººms alert:ººººms chime¡:ººººms
--:--z
¬UNILINK MENU RETURN®
REVIEW 20/22 chime:ººººms inhib on gnd:ººkts inhib alt:¡ººººft alt type:baro after off:ºmin sys config £÷¢: fans:enabled
--:--z
¬UNILINK MENU RETURN®
REVIEW 21/22 fans aural:ºms delay msg tx:ººmin ground delay:ººmin fans latency:ºsec supp addr:------sys config ¢÷¢: config mod updates:
--:--z
¬UNILINK MENU RETURN®
REVIEW 22/22
date time
§-aug-¡¡ ¡¶ºz
§-aug-¡¡ ¡¶ºz
§-aug-¡¡ ¡¶ºz
--:--z
¬UNILINK MENU RETURN®
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UL-801 Installation Manual
Maintenance, Checkout, and Troubleshooting
1. UniLink Ground Checkout Procedures
A. Post Installation Test
For instructions on testing the UniLink following the initial installation in an aircraft, the installer should refer to the installation Ground and/or Flight Test Plans that are part of the
UniLink installation (TC, STC, Field Approval) certification package.
The installation approval applicant should contact Universal Avionics Certification
Department for Ground and/or Flight Test Plan templates that can be used for developing customized test plans.
B. Return to Service
The following defines the conditions under which tests, specified below, should be conducted.
(1) Safety Precautions
User should follow all appropriate safety precautions.
(2) Power Input
Unless otherwise specified, tests should be conducted with the equipment powered by the aircraft’s electrical power generating system.
(3) Associated Equipment or Systems
Unless otherwise specified, turn on all aircraft electrically operated equipment and systems before conducting these tests.
(4) Environment
During tests, the equipment should not be subjected to environmental conditions that exceed those specified by the equipment manufacturer.
(5) Warm-up Period
No warm-up period is required. However, some time must be allowed for all associated equipment to boot up properly and stabilize.
C. UniLink to FMS/CDU Communications
NOTE: This procedure should be completed for each FMS/CDU connected to the
UniLink.
(1) Verify that DATA 1/4 page is displayed an active UNILINK prompt.
(2) From the DATA 1/4 page, press the UNILINK LSK [3R] and verify the UNILINK
MENU 1/2 page is displayed.
(3) Press RETURN LSK [5R]. Verify that the DATA 1/4 page is displayed.
(4) Repeat test steps 1 through 3 for each FMS/CDU connected and configured for
UniLink.
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(1) From the UNILINK MENU Page 1, press NEXT.
(2) Press MAINTENANCE LSK [4L].
(3) Press VERSIONS LSK [3L].
(4) Verify the correct UniLink SCN and Part Number appears on the screen.
(1) Ensure all peripheral devices are powered on.
(2) Press the DEVICE STATUS LSK [1L] on the MAINTENANCE 1/3 page.
(3) Verify that the device status is OK for all applicable configured peripheral devices such as FMSs, MCDUs, CDUs, low and high resolution graphics devices, and CVRs.
Press NEXT to cycle thru the DEVICES pages.
F. UniLink to Display Processor RS-422 Communications
This procedure applies only to display devices wired and configured to support weather graphics.
(1) From the MAINTENANCE 1/3 page, press the TESTS LSK [2R].
(2) Press the IMAGE LSK [2L].
(3) The IMAGE TEST IN PROGRESS pop-up message will appear.
(4) Verify that the test image below is presented on all appropriate display devices.
NOTE:
•
This is a Low Resolution test image and will be displayed as such on High
Resolution display devices as well. UniLink does not generate a High
Resolution test image.
•
It is recommended that you delete the test image following test completion.
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G. UL-801 VHF Communications
VHF datalink service coverage on the ground may be limited. Coverage may be affected by ground obstacles and may be restricted due to poor line of sight of the VHF ground station antenna.
(1) The VHF communications status is indicated on the UniLink COMM STATUS page.
Press COMM STATUS LSK [4L] on the UNILINK MENU 1/2 page.
(2) If VHF COMM STATUS is COMM/IDLE, a request for ATIS information can be performed on the ground. Otherwise, if the VHF COMM STATUS is
NOCOMM/SCANNING, the aircraft should be relocated elsewhere until the status of
COMM/IDLE is obtained.
(3) To request D-ATIS, from the UNILINK MENU Page 1:
•
Press the FLIGHT INFO LSK.
•
Press the D-ATIS LSK.
•
Press AIRPORT. Type KORD, for example, or your airport identifier.
•
Press LSK [ENTER].
•
Press SEND to transmit the request.
−
If QUEUED is displayed above the SEND prompt, the VHF probably is not connected to the ACARS system.
−
If Sending, SENT is displayed. The request was received and acknowledged.
Your request will be shortly received by UniLink and available for viewing.
(4) Ensure Door and Park Brake discrete inputs are connected and configured.
(1) From UNILINK MENU 2/2 page, press the MAINTENANCE LSK [4L].
(2) Press SENSOR STATUS LSK [2L].
(3) Open and close the door.
(4) Verify the DOORS status changes accordingly.
(5) Release and set parking brake.
(6) Verify the BRAKE status changes accordingly.
(7) Verify the AIR/GROUND status is ON GROUND.
NOTE: If the aircraft is on jacks, the status will be IN AIR.
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(1) Verify that printer power is on and has passed its self-test.
(2) With the DATA page 1/4 displayed, press UNILINK LSK [3R]. The UNILINK
MENU 1/2 will display.
(3) Press the NEXT key.
(4) Press MAINTENANCE LSK [4L] to display the MAINTENANCE 1/3 page.
(5) Press TESTS LSK [2R] to display the TESTS page.
(6) Press PRINTER LSK [1L]. The printing message pop-up message will display and a test pattern will be sent to the printer.
(7) The TESTS page will again display.
J. Checking the UL-801 FANS ALERTS Output Discretes
This procedure applies only to FANS-enabled aircraft.
(1) From the DATA 1/4 page, press UNILINK LSK [3R]. The UNILINK MENU 1/2 page will display.
(2) Press the NEXT key.
(3) Press MAINTENANCE LSK [4L] to display the MAINTENANCE 1/3 page.
(4) Press TESTS LSK [2R] to display the TESTS page.
(5) Press FANS ALERTS LSK [1R]. The FANS DISCRETE TEST IN PROGRESS popup message will appear.
(6) Verify that all appropriate FANS Visual and Aural alerts activate momentarily.
K. Checking the UL-801 Self-Test (Optional)
This test simply reboots the UniLink. After the reboot process, verify that the UniLink prompt becomes active.
L. Checking the UL-801 Weather Graphics using a SatCom-based
Telephony System
NOTE: Ensure that the selected DSP supports Weather Graphics uplinks.
(1) Press the DATA key to display the DATA 1/4 page.
(2) Press UNILINK LSK [3R] to display UNILINK MENU 1/2.
(3) Press WX MAPS LSK [2R] to display the WX MAP REQUEST page.
(4) Press SIG WX LSK [2R] and the SIGNIFICANT WX page will display.
(5) Press SEND LSK [4R]. This prompts UniLink to place a call to the selected DSP.
(6) The QUEUED and SENDING messages display. After a few minutes, the FMS
UniLink will display NEW WX ADVISORY under the ADVISORY area. Press the
LSK to the left of the ADVISORY message to display the message. a) If a UniLink page is not currently displayed on the FMS, the MSG icon light will flash.
(7) Press the MSG key on the FMS to display the MESSAGES 1/X page. The UNILINK
WX MAP RCVD message will appear.
(8) Pressing the UniLink prompt will display the UNILINK MENU 1/2 page.
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(9) Press LSK [5L] to display the weather map. Verify that the correct map has been received.
M. Checking the UL-801 ARINC 741 SatCom (SAT)
NOTE: Ensure that the selected DSP provides this service.
(1) Verify that the SatCom SDU is powered up, initialized, and logged on.
(2) From the UNILINK MENU 1/2 page, press COMM STATUS.
(3) If the SatCom status is NOCOMM/UNAVAILABLE, UniLink has not detected label
270 from the SatCom. This indicates the Sat Link is unavailable.
(4) If the SatCom status is NOCOMM/CONNECTING, the SatCom Link is available,
UniLink will send a Link Test message, and wait for an acknowledgement from the
ACARS network to confirm connectivity to the network.
(5) If SatCom status is COMM/IDLE, the SatCom Link connectivity to the ACARS network has been confirmed and UniLink is ready to send and receive messages via the SatCom link.
All tests are now complete.
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A complete list of defined error messages is shown in the following tables:
•
The Pop-up Error Messages table shows the error conditions that result in a pop-up window error message. These errors are deemed significant enough to warrant immediate, detailed annunciation.
•
The General Error Messages table shows the general error messages that may result in a
NEW ERROR MSG advisory alert, as well as the recommended actions for resolution.
•
The Configuration Error Messages shows possible configuration error messages, as well as the recommended actions for resolution.
•
The Hidden Error/Status Messages shows unannunciated error/status messages that are normally hidden from the error log.
A. Pop-up Window Error Messages
Pop-up Window Error Messages
Pop-up Window Text Condition
FMS/MCDU CONFIG ERROR. CONFIG NOT
SAVED.
User attempt to STORE configuration data that does not configure the same FMS or MCDU on RX Port 1 and TX Port 1.
FMS/VDR SHARE TX PORT. CONFIG NOT
SAVED.
FMS/MCDU CONFIG ERROR. CONFIG NOT
SAVED
User attempt to STORE configuration data with an
ARINC 429 transmit port configured to interface to both a UASC FMS and an ARINC 750 VDR.
User attempt to STORE configuration data with both a
UASC FMS/CDU and an MCDU configured together.
UNABLE TO WRITE TO CONFIG MODULE. User attempt to STORE configuration data with
Configuration Module error.
DISPLAY PROCESSOR FAIL A configured display processor has failed or experienced a communication failure, or too many bad slots have been detected.
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B. General Error Messages
UniLink error messages may be found by using either of the following two processes:
(1) Press the MSG key to see the messages. a) Press the NEXT key to scroll through the messages.
(2) Press the MAINTENANCE LSK [4L] on the UNILINK MENU 1/2 page. a) Press the ERROR LOG LSK [4L] on the MAINTENANCE 1/3 page.
NOTE: The Error Log contains all error messages including configuration error messages. The messages found when pressing the MSG key are only applicable to configuration errors. b) Press the NEXT key to scroll through the messages.
FMS1 INOP
FMS2 INOP
FMS3 INOP
CDU1 DP INOP
CDU2 DP INOP
CDU3 DP INOP
MFD-LR1
INOP
General Error Messages
Text Action/Description
REMOTE CDU1 DP INOP
REMOTE CDU2 DP INOP
REMOTE CDU3 DP INOP
Cycle power to UniLink and FMS1. If condition persists contact UASC.
Cycle power to UniLink and FMS2. If condition persists contact UASC.
Cycle power to UniLink and FMS3. If condition persists contact UASC.
Cycle power to UniLink and CDU1. If condition persists contact UASC. If condition is recent or frequent for a particular device, examine connection between the graphics display device and UniLink.
Cycle power to UniLink and CDU2. If condition persists contact UASC. If condition is recent or frequent for a particular device, examine connection between the graphics display device and UniLink.
Cycle power to UniLink and CDU3. If condition persists contact UASC. If condition is recent or frequent for a particular device, examine connection between the graphics display device and UniLink.
Cycle power to UniLink and RCDU1. If condition persists contact UASC. If condition is recent or frequent for a particular device, examine connection between the graphics display device and UniLink.
Cycle power to UniLink and RCDU2. If condition persists contact UASC. If condition is recent or frequent for a particular device, examine connection between the graphics display device and UniLink.
Cycle power to UniLink and RCDU3. If condition persists contact UASC. If condition is recent or frequent for a particular device, examine connection between the graphics display device and UniLink.
Cycle power to UniLink and MFD1. If condition persists contact UASC. If condition is recent or frequent for a particular device, examine connection between the graphics display device and UniLink.
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MFD-LR2
INOP
MFD-LR3
INOP
HR-1
INOP
HR-2
INOP
MCDU1 INOP
MCDU2 INOP
MCDU3 INOP
HF RADIO INOP
SDU INOP
TEL INOP
CMC INOP
A740 PRINTER INOP
General Error Messages
Text Action/Description
SERIAL PRINTER INOP
VHF VDLM2 RADIO INOP
Cycle power to UniLink and MFD2. If condition persists contact UASC. If condition is recent or frequent for a particular device, examine connection between the graphics display device and UniLink.
Cycle power to UniLink and MFD3. If condition persists contact UASC. If condition is recent or frequent for a particular device, examine connection between the graphics display device and UniLink.
Cycle power to UniLink and high-resolution display 1
(MFD-640 or EFI-890R). If condition persists contact
UASC. If condition is recent or frequent for a particular device, examine connection between the graphics display device and UniLink.
Cycle power to UniLink and high-resolution display 2
(MFD-640 or EFI-890R). If condition persists contact
UASC. If condition is recent or frequent for a particular device, examine connection between the graphics display device and UniLink.
Cycle power to UniLink and MCDU1. If condition persists contact UASC. If condition is recent or frequent for a particular device, examine connection between the graphics display device and UniLink.
Cycle power to UniLink and MCDU2. If condition persists contact UASC. If condition is recent or frequent for a particular device, examine connection between the graphics display device and UniLink.
Cycle power to UniLink and MCDU3. If condition persists contact UASC. If condition is recent or frequent for a particular device, examine connection between the graphics display device and UniLink.
Cycle power to UniLink and HF radio.
Cycle power to UniLink and SDU. If condition persists contact UASC.
Cycle power to UniLink and telephone system. If condition persists contact UASC.
Cycle power to UniLink and CMC. If condition persists contact UASC.
Cycle power to UniLink and Printer. If condition persists contact UASC.
No action required. Temporary condition that will correct with next job UniLink sends to printer.
Cycle power to UniLink and radio. If condition persists contact UASC.
Cycle power to UniLink. THE SYSTEM IS RUNNING LOW ON NVRAM
AND SHOULD BE RESTARTED.
THE SYSTEM IS CRITICALLY SHORT OF
NVRAM. SYSTEM RESTART IS IMMINENT.
Cycle power to UniLink.
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General Error Messages
Text Action/Description
SERIAL PRINTER FAILURE
PRINT JOB TOO LARGE
Examine the printer and its serial and power connections.
No action required. UniLink has attempted to forward a corrupted uplink to the printer. Re-request uplink data.
Cycle power to UniLink. If condition persists contact
UASC.
[Hardware port] FAIL example:
ARINC TX PORT 1 FAIL
THE FATAL ERROR LOG HAS BEEN
CORRUPTED
THE FATAL ERROR LOG CONTAINS A NEW
ENTRY
PROTOCOL ERROR LOG CORRUPT.
OLD PROTOCOL ERRORS DISCARDED.
LOGGING OF PROTOCOL ERRORS WILL
RESTART.
CTS BUSY LSK [device name, count, first/last occurrence]
CTS TIMEOUT LSK [device name, count, first/last occurrence]
No action required. Old messages are discarded and the log is automatically restarted.
No action required. If condition is frequent, contact
UASC.
No action required. Old messages are discarded and protocol error logging is automatically restarted.
LINK ERROR LSK [device name, count, first/last occurrence]
PROTOCOL ERROR LSK [device name, count, first/last occurrence]
No action required. Protocol errors are automatically corrected, usually with no impact to the user. If condition is frequent for a particular device, examine connection between device and UniLink.
No action required. Protocol errors are automatically corrected, usually with no impact to the user. If condition is frequent for a particular device, examine connection between device and UniLink.
MSG RETRY LSK [device name, count, first/last occurrence]
SYN LSK [device name, count, first/last occurrence]
MSG TIMEOUT LSK [device name, count, first/last occurrence]
DSC RETRY LSK [device name, count, first/last occurrence]
DSC TIMEOUT LSK [device name, count, first/last occurrence]
SPW RETRY LSK [device name, count, first/last occurrence]
SPW TIMEOUT LSK [device name, count, first/last occurrence]
TX BUF FULL LSK [device name, count, first/last occurrence]
RX PORT 1: UASC FMS DETECTED.
OVERRIDING PORT CONFIGURATION FOR
MCDU
Configure UniLink with ARINC receive port 1 as
FMS/CDU1 and transmit port 1 as FMS/CDU1.
RX PORT 1: MCDU DETECTED. OVERRIDING
PORT CONFIGURATION FOR UASC FMS
Configure UniLink with ARINC receive port 1 as
MCDU1 and transmit port 1 as MCDU1.
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General Error Messages
Text Action/Description
STATUS TIMEOUT LSK [count, first/last occurrence]
ENQ TIMEOUT LSK [count, first/last occurrence]
RECORD TIMEOUT LSK [count, first/last occurrence]
No action required. Protocol errors are automatically corrected, usually with no impact to the user. If condition is frequent, examine connection between the printer and UniLink.
RECORD RESEND LSK [count, first/last occurrence]
PRINTER FAIL LSK [count, first/last occurrence]
DOOR OPEN LSK [count, first/last occurrence]
TEST LSK [count, first/last occurrence]
INIT LSK [count, first/last occurrence]
OVERRUN LSK [count, first/last occurrence]
BUSY LSK [count, first/last occurrence]
INVALID CTS LSK [count, first/last occurrence]
ERASE FAULT LSK [device name, count, first/last occurrence]
TOO MANY FAILED SLOTS LSK [device name, count, first/last occurrence]
UNEXPECTED EOF LSK [device name, count, first/last occurrence]
UNKNOWN IMAGE FORMAT LSK [device name, count, first/last occurrence]
If condition is recent or frequent for a particular device, examine connection between the graphics display device and UniLink.
GIF ERROR LSK [device name, count, first/last occurrence]
TRANSMIT FAIL LSK [device name, count, first/last occurrence]
INVALID GX HEADER LSK [count, first/last occurrence]
VDL MODE A NOT SUPPORTED
VDL MODE 2 NOT SUPPORTED
VDR TX WARN FAULT
If condition is recent or frequent, examine connection between telephone system and UniLink.
Cycle power once to the VDR. If condition persists, replace VDR or contact UASC.
Cycle power once to the VDR. If condition persists, replace VDR or contact UASC.
Cycle power once to the VDR. If condition persists, replace VDR or contact UASC.
VDR STATUS FAULT
CTRL PROTOCOL CMU ERROR
CTRL PROTOCOL VDR ERROR
ACARSIP CMU ERROR
Cycle power once to the VDR. If condition persists, replace VDR or contact UASC.
Cycle power once to the VDR. If condition persists, replace VDR or contact UASC.
Cycle power once to the VDR. If condition persists, replace VDR or contact UASC.
Cycle power once to the VDR. If condition persists, replace VDR or contact UASC.
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ACARSIP VDR ERROR
ASIP CMU ERROR
ASIP VDR ERROR
General Error Messages
Text Action/Description
VDR SOFTWARE LOAD FAULT
Cycle power once to the VDR. If condition persists, replace VDR or contact UASC.
Cycle power once to the VDR. If condition persists, replace VDR or contact UASC.
Cycle power once to the VDR. If condition persists, replace VDR or contact UASC.
Cycle power once to the VDR. If condition persists, contact UASC.
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C. Configuration Error Messages
Configuration Error Messages
Text Action
MEMORY ALLOCATION ERROR--UNABLE TO
LOAD CONFIGURATION MODULE.
Attempt to store configuration. If condition persists contact UASC.
ERROR READING CONFIGURATION
MODULE FROM NON-VOLATILE MEMORY.
CONFIGURATION MODULE CRC CODE
FAILURE.
CONFIGURATION MODULE VERSION
INCOMPATIBLE WITH SOFTWARE--
CONFIGURATION UPDATE REQUIRED.
CONFIGURATION MODULE REVISION
OLDER THAN SOFTWARE REVISION--
CONFIGURATION UPDATE REQUIRED.
AN ADC AND AN IOP BUS MAY NOT BE
CONFIGURED TOGETHER
CONFIGURATION UPDATED FROM OLDER
FORMAT. SOME DEFAULT VALUES USED.
CONFIGURATION SHOULD BE VERIFIED
AND RESAVED.
CONFIGURATION MODULE REVISION
NEWER THAN SOFTWARE REVISION--
EXTRA DATA IGNORED.
ONE OR MORE ARINC DEVICES HAS A
TRANSMIT PORT BUT NO RECEIVE PORT.
Attempt to store configuration. If condition persists contact UASC.
Attempt to store configuration. If condition persists contact UASC.
Verify UniLink software update and configuration, and store the configuration.
Verify UniLink software update and configuration, and store the configuration.
An IOP bus cannot be configured concurrently with a
DADC. Configure UniLink accordingly.
Once the configuration has been stored this message will not appear. A newer configuration revision should be used.
Once the configuration has been stored this message will not appear.
ONE OR MORE ARINC DEVICES HAS A
RECEIVE PORT BUT NO TRANSMIT PORT.
THE SAME DEVICE IS ASSIGNED TO MORE
THAN ONE ARINC 429 TRANSMIT PORT.
AN A702 FMS OR GENERIC DEVICE IS
CONFIGURED BUT LACKS A DEFINITION IN
THE CUSTOMER DATABASE.
MULTIPLE CMC DEVICES CONFIGURED.
Configure UniLink with a receive port for each configured transmit port listed on the ARINC
TRANSMIT page.
Configure UniLink with a transmit port for each configured receive port listed on the ARINC RECEIVE page.
Any given device cannot be configured on more than one transmit port; configure UniLink accordingly.
Load UniLink with a customer database that supports an ARINC 702 FMS or generic device, as appropriate.
THE UASC FMS THE ARINC 702 FMS AND
THE GNSS RECEIVER MAY NOT BE
CONFIGURED TOGETHER.
Configure UniLink with either no CMC or a single
CMC, as appropriate, because UniLink cannot be configured with multiple CMC devices.
Configure UniLink with the same navigation source only (i.e., the UASC FMS(s), the ARINC 702 FMS(s), or the GNSS receiver) because UniLink cannot be configured with dissimilar navigation sources concurrently.
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Configuration Error Messages
Text Action
AN ADC AND A GNSS RECEIVER MAY NOT
BE CONFIGURED TOGETHER
Configure UniLink with DADC device(s) or GNSS receiver. DADC and GNSS are dissimilar altitude sources and cannot be configured concurrently, configure UniLink accordingly.
AN ADC AND AN ARINC 702 FMS MAY NOT
BE CONFIGURED TOGETHER
A digital air data computer cannot be configured concurrently with an ARINC 702 FMS, configure
UniLink accordingly.
AN IOP BUS MAY NOT BE CONFIGURED
TOGETHER WITH AN ARINC 702 FMS OR
THE GNSS RECEIVER.
AN MCDU IS CONFIGURED BUT AN ARINC
702 FMS OR GNSS RECEIVER IS NOT
CONFIGURED.
An IOP bus cannot be configured concurrently with an
ARINC 702 FMS or with a GNSS receiver; configure
UniLink accordingly.
When an MCDU is configured, configure UniLink with an ARINC 702 FMS or a GNSS receiver.
IN ORDER FOR AN MCDU INSTALLATION TO
DISPLAY WEATHER MAPS AT LEAST ONE
DISPLAY MUST BE SET TO MFD-LR OR HR-1
OR HR-2
If the MCDU(s) is wired and configured as an ARINC
739A MCDU, configure UniLink with a low-resolution
MFD-640 and/or a high-resolution MFD-640/EFI-890R.
(See 0 and 2.)
IN ORDER FOR AN MCDU INSTALLATION TO
DISPLAY WEATHER MAPS NO DISPLAY MAY
BE SET TO CDU OR RCDU.
If the MCDU(s) is wired and configured as an ARINC
739A MCDU, configure UniLink with a low-resolution
MFD-640 and/or a high-resolution MFD-640/EFI-890R.
Ensure no MCDU, wired as an ARINC 739A MCDU, is configured as a CDU. (See 0 and 2).
MORE THAN TWO REMOTE CDU GRAPHIC
DEVICES CONFIGURED
REMOTE CDU-1 CONFIGURED WITHOUT
PRIMARY CDU-1 CONFIGURED.
Configure UniLink with no more than two RCDU displays.
When configuring a remote CDU for graphics, configure both the RCDU and the corresponding primary CDU.
REMOTE CDU-2 CONFIGURED WITHOUT
PRIMARY CDU-2 CONFIGURED.
REMOTE CDU-3 CONFIGURED WITHOUT
PRIMARY CDU-3 CONFIGURED.
NO MORE THAN FOUR DISPLAY
PROCESSORS MAY BE CONFIGURED ON
THE LOW-RES DISPLAY PORT
ARINC TEST DEVICE CONFIGURED.
When configuring a remote CDU for graphics, configure both the RCDU and the corresponding primary CDU.
When configuring a remote CDU for graphics, configure both the RCDU and the corresponding primary CDU.
Configure UniLink with four or fewer graphic devices on the low-resolution display serial port.
Remove the TEST DEV selection from any ARINC
RECEIVE port; it is used for test purposes only.
A VHF RADIO IS CONFIGURED BUT NO
VALID AIRCRAFT REGISTRATION IS
CONFIGURED.
A VHF RADIO IS CONFIGURED BUT NO
VALID AIRLINE/AGENCY ID IS PRESENT.
When an A750 VDR is configured, configure UniLink with a valid aircraft registration in the REGISTRATION field on the A/C CONFIG page.
Configure UniLink with a valid airline/agency identifier in the left portion of the AIRLINE ID field on the A/C
CONFIG page.
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Configuration Error Messages
Text Action
SATCOM IS CONFIGURED BUT NO VALID
AIRCRAFT REGISTRATION IS CONFIGURED.
Configure UniLink either with a valid aircraft registration in the REGISTRATION field on the A/C
CONFIG page or with no ARINC transmit and receive ports for an SDU.
SATCOM IS CONFIGURED BUT NO VALID
AIRLINE/AGENCY ID IS PRESENT.
AN AIR PHONE DEVICE IS CONFIGURED
BUT NO VALID TELEPHONE NUMBER IS
PRESENT.
A VALID TELEPHONE NUMBER IS PRESENT
BUT NO AIR PHONE DEVICE IS
CONFIGURED.
Configure UniLink either with a valid airline/agency identifier in the left portion of the AIRLINE ID field on the A/C CONFIG page or with no ARINC transmit and receive ports for an SDU.
Configure UniLink either with a valid telephone number in the TEL ACCESS NUMBER field on the TEL
CONFIG 1/2 page or do not configure UniLink for an air phone (NONE in the AIR PHONE field on the TEL
CONFIG 1/2 page).
Configure UniLink either with the correct air phone device in the AIR PHONE field or with no telephone number in the TEL ACCESS NUMBER field on the
TEL CONFIG 1/2 page.
VHF APPEARS IN NORMAL MEDIA PRIORITY
SELECTIONS BUT NO VHF RADIO IS
CONFIGURED.
Configure UniLink either with the correct VHF radio in the RADIO TYPE field on the VHF CONFIG 2/2 page or without VHF in any of the three NORMAL fields on the COMM PRIORITY page.
VHF APPEARS IN ALTERNATE MEDIA
PRIORITY SELECTIONS BUT NO VHF RADIO
IS CONFIGURED.
SATCOM APPEARS IN NORMAL MEDIA
PRIORITY SELECTIONS BUT NO SDU IS
CONFIGURED.
SATCOM APPEARS IN ALTERNATE MEDIA
PRIORITY SELECTIONS BUT NO SDU IS
CONFIGURED.
TELEPHONY APPEARS IN NORMAL MEDIA
PRIORITY SELECTIONS BUT NO AIR PHONE
DEVICE IS CONFIGURED.
Configure UniLink either with the correct VHF radio in the RADIO TYPE field on the VHF CONFIG 2/2 page or without VHF in any of the three ALTERNATE fields on the COMM PRIORITY page.
Configure UniLink either with ARINC transmit and receive ports for an SDU or without SAT in any of the three NORMAL fields on the COMM PRIORITY page.
Configure UniLink's ARINC transmit and receive ports for an SDU or configure UniLink with no SAT in any of the three ALTERNATE fields on the COMM PRIORITY page.
Configure UniLink either with the correct air phone device in the AIR PHONE field on the TEL CONFIG
1/2 page or without TEL in any of the three NORMAL fields on the COMM PRIORITY page.
TELEPHONY APPEARS IN ALTERNATE
MEDIA PRIORITY SELECTIONS BUT NO AIR
PHONE DEVICE IS CONFIGURED.
Configure UniLink either with the correct air phone device in the AIR PHONE field on the TEL CONFIG
1/2 page or without TEL in any of the three
ALTERNATE fields on the COMM PRIORITY page.
VHF IS CONFIGURED BUT IS NOT IN EITHER
MEDIA PRIORITY LIST.
Configure UniLink either with VHF in the desired priority NORMAL and/or ALTERNATE fields on the
COMM PRIORITY page or with NONE in the RADIO
TYPE field on the VHF CONFIG 2/2 page.
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Configuration Error Messages
Text Action
SATCOM IS CONFIGURED BUT IS NOT IN
EITHER MEDIA PRIORITY LIST.
Configure UniLink either with SAT in the desired priority NORMAL and/or ALTERNATE fields on the
COMM PRIORITY page or with no ARINC transmit and receive ports for an SDU.
TELEPHONY IS CONFIGURED BUT IS NOT IN
EITHER MEDIA PRIORITY LIST.
Configure UniLink either with TEL in the desired priority NORMAL and/or ALTERNATE fields on the
COMM PRIORITY page or with NONE in the AIR
PHONE field on the TEL CONFIG 1/2 page.
THE VHF SIMULATOR INTERFACE IS
CONFIGURED. THIS INTERFACE IS FOR
DEVELOPMENT ONLY.
Remove the VHF GND SIM selection on the SERIAL setup pages; it is used for test purposes only.
THE SATCOM SIMULATOR INTERFACE IS
CONFIGURED. THIS INTERFACE IS FOR
DEVELOPMENT ONLY.
Remove the SAT GND SIM selection on the SERIAL setup pages; it is used for test purposes only.
THE TELEPHONY SIMULATOR INTERFACE IS
CONFIGURED. THIS INTERFACE IS FOR
DEVELOPMENT ONLY.
Remove the TEL SIM selection on the SERIAL setup pages; it is used for test purposes only.
A SERIAL PORT IS ASSIGNED TO IRIDIUM
BUT NO COMPATIBLE TELEPHONY DEVICE
IS CONFIGURED.
Configure UniLink either with IRIDIUM in the AIR
PHONE field on the TEL CONFIG 1/2 page or with no serial port as IRIDIUM on the SERIAL setup pages.
THE CONFIGURED TELEPHONY DEVICE IS
/IRIDIUM BUT NO COMPATIBLE SERIAL
PORT IS CONFIGURED.
A SERIAL PORT IS ASSIGNED TO AERO M
BUT NO COMPATIBLE TELEPHONY DEVICE
IS CONFIGURED.
Configure UniLink either with the correct serial port as
IRIDIUM on the SERIAL setup pages or with NONE in the AIR PHONE field on the TEL CONFIG 1/2 page.
Configure UniLink either with T-T Aero-M in the AIR
PHONE field on the TEL CONFIG 1/2 page or with no serial port as Aero-M on the SERIAL setup pages.
THE CONFIGURED TELEPHONY DEVICE IS
AERO M BUT NO COMPATIBLE SERIAL PORT
IS CONFIGURED.
Configure UniLink either with the correct serial port as
Aero-M on the SERIAL setup pages or with NONE in the AIR PHONE field on the TEL CONFIG 1/2 page.
THE NEW-MESSAGE-ANNUNC-INHIBIT
FUNCTION IS CONFIGURED TO USE RADIO
ALTITUDE BUT NO IOP BUS IS
CONFIGURED.
Configure UniLink either with DHC8 IOPn in the correct PORT n field on the ARINC RECEIVE pages or with BARO in the ALT TYPE field on the ALERT
CONFIG page.
THE NEW-MESSAGE-ANNUNC-INHIBIT
FUNCTION IS CONFIGURED TO USE RADIO
ALTITUDE BUT THE CONFIGURED ALTITUDE
THRESHOLD VALUE IS TOO LARGE.
Configure UniLink either with a value equal to or less than 2500 in the INHIB ALT field or with BARO in the
ALT TYPE field on the ALERT CONFIG page.
THE VHF VOX-ANNUN OUTPUT DISCRETE IS
CONFIGURED BUT NO ARINC 750 VDR IS
CONFIGURED.
Configure UniLink either with the external A750 VDR in the RADIO TYPE field on the VHF CONFIG 2/2 page or with no DISC OUT n field as VOX ANNUN on the DISC OUT pages.
THE VDR MODE-SELECT OUTPUT DISCRETE
IS CONFIGURED BUT NO ARINC 750 VDR IS
CONFIGURED.
Configure UniLink either with the external A750 VDR in the RADIO TYPE field on the VHF CONFIG 2/2 page or with no DISC OUT n field as VDR VOX SEL on the DISC OUT pages.
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Configuration Error Messages
Text Action
THE VHF-NOCOMM OUTPUT DISCRETE IS
CONFIGURED BUT NO VHF RADIO IS
CONFIGURED.
Configure UniLink either with the correct radio in the
RADIO TYPE field on the VHF CONFIG 2/2 page or with no DISC OUT n field as VHF NOCOMM on the
DISC OUT pages.
THE SAT-NOCOMM OUTPUT DISCRETE IS
CONFIGURED BUT NO SDU IS
CONFIGURED.
Configure UniLink either with ARINC transmit and receive ports for an SDU or with no DISC OUT n field as SAT NOCOMM on the DISC OUT pages.
THE TEL-NOCOMM OUTPUT DISCRETE IS
CONFIGURED BUT NO TELEPHONE IS
CONFIGURED.
Configure UniLink either with the correct air phone in the AIR PHONE field on the TEL CONFIG 1/2 page or with no DISC OUT n field as TEL NOCOMM on the
DISC OUT pages.
ARINC IS CONFIGURED BUT OOOI IS
DISABLED.
Configure UniLink either with ENABLED in the OOOI
TIMES field on the SYS CONFIG 2/4 page or with
OFF in the ARINC field on the DSP SETUP page.
AN ARINC VOICE TUNE BUS TRANSMIT
PORT IS CONFIGURED BUT NO A750 VDR IS
CONFIGURED.
Configure UniLink either with the external A750 VDR in the RADIO TYPE field on the VHF CONFIG page or with no ARINC transmit port with device VOICE TUNE
BUS.
AN ARINC TRANSMIT PORT IS CONFIGURED
FOR BOTH VOX TUNE AND SOME OTHER
FUNCTION. THE VOX TUNE PORT CANNOT
BE SHARED.
The VOX TUNE bus cannot be configured concurrently with another device; configure UniLink accordingly.
THE SETTINGS FOR VOICE FREQUENCY
TUNING, THE VOICE TUNE BUS, AND THE
VHF MODE-SELECT OUTPUT DISCRETE ARE
INCONSISTENT WITH ONE ANOTHER.
Configure UniLink either with:
The VOICE FREQ CONTROL field on the VHF
CONFIG page set to ENABLE 25 or ENABLE 8.33/25,
AND an ARINC transmit port with device VOICE
TUNE BUS, AND a DISC OUT n field configured as
VDR VOX SEL.
OR
The VOICE FREQ CONTROL field on the VHF
CONFIG page set to DISABLE, AND no ARINC transmit port with device VOICE TUNE BUS, AND no
DISC OUT n field as VDR VOX SEL.
VHF VOICE FREQUENCY TUNING IS
ENABLED BUT NO A750 VDR IS
CONFIGURED.
Configure UniLink either with the external A750 VDR in the RADIO TYPE field on the VHF CONFIG page or with DISABLE in the VOICE FREQ CONTROL field on the VHF CONFIG page.
WEATHER MAPS ARE ENABLED BUT NO AIR
PHONE IS CONFIGURED.
Configure UniLink either with the correct air phone in the AIR PHONE field or with DISABLED in the WX
MAPS field on the TEL CONFIG 1/2 page.
CDU 1 IS CONFIGURED FOR GRAPHICS BUT
FMS 1 OR MCDU 1 IS NOT CONFIGURED.
Configure UniLink either with ARINC transmit and receive ports for FMS 1 or MCDU 1, as appropriate, or with NONE in the CDU 1 GRAPHICS DISP ON field on the GRAPHICS setup page.
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Configuration Error Messages
Text Action
CDU 2 IS CONFIGURED FOR GRAPHICS BUT
FMS 2 OR MCDU 2 IS NOT CONFIGURED.
Configure UniLink either with ARINC transmit and receive ports for FMS 2 or MCDU 2, as appropriate, or with NONE in the CDU 2 GRAPHICS DISP ON field on the GRAPHICS setup page.
CDU 3 IS CONFIGURED FOR GRAPHICS BUT
FMS 3 OR MCDU 3 IS NOT CONFIGURED.
Configure UniLink either with ARINC transmit and receive ports for FMS 3 or MCDU 3, as appropriate, or with NONE in the CDU 3 GRAPHICS DISP ON field on the GRAPHICS setup page.
AT LEAST ONE CDU IS CONFIGURED FOR
GRAPHICS BUT WEATHER MAPS ARE
DISABLED AND NO SERIAL LO- OR HI-RES
DISPLAY IS CONFIGURED.
A SERIAL LO- or HI-RES DISPLAY IS
CONFIGURED BUT WEATHER MAPS ARE
DISABLED AND NO CDU IS CONFIGURED
FOR GRAPHICS.
Configure UniLink either with ENABLED in the WX
MAPS field on the TEL CONFIG 1/2 page and with
LO-RES DISPLAY, HI-RES DISPLAY 1, or HI-RES
DISPLAY 2 in the correct PORT n field on the SERIAL setup pages or with NONE in all CDU n GRAPHICS
DISP ON fields on the GRAPHICS setup page.
Configure UniLink either with ENABLED in the WX
MAPS field on the TEL CONFIG 1/2 page and with the correct value in the appropriate CDU n GRAPHICS
DISP ON field(s) on the GRAPHICS setup page or with no PORT n field as LO-RES DISPLAY, HI-RES
DISPLAY 1, or HI-RES DISPLAY 2 on the SERIAL setup pages.
WEATHER MAPS ARE ENABLED BUT NO
SERIAL LO- OR HI-RES DISPLAY IS
CONFIGURED AND NO CDU IS CONFIGURED
FOR GRAPHICS.
Configure UniLink either with LO-RES DISPLAY, HI-
RES DISPLAY 1, or HI-RES DISPLAY 2 in the correct
PORT n field on the SERIAL setup pages and with the correct value in the appropriate CDU n GRAPHICS
DISP ON field(s) on the GRAPHICS setup page or with DISABLED in the WX MAPS field on the TEL
CONFIG 1/2 page.
WEATHER MAPS ARE ENABLED AND A
SERIAL LO- or HI-RES DISPLAY IS
CONFIGURED BUT NO CDU IS CONFIGURED
FOR GRAPHICS.
Configure UniLink either with the correct value in the appropriate CDU n GRAPHICS DISP ON field(s) on the GRAPHICS setup page or with DISABLED in the
WX MAPS field on the TEL CONFIG 1/2 page and with no PORT n field as LO-RES DISPLAY, HI-RES
DISPLAY 1, or HI-RES DISPLAY 2 on the SERIAL setup pages.
WEATHER MAPS ARE ENABLED AND AT
LEAST ONE CDU IS CONFIGURED FOR
GRAPHICS BUT NO SERIAL LO- OR HI-RES
DISPLAY IS CONFIGURED.
Configure UniLink either with LO-RES DISPLAY, HI-
RES DISPLAY 1, or HI-RES DISPLAY 2 in the correct
PORT n field on the SERIAL setup pages or with
DISABLED in the WX MAPS field on the TEL CONFIG
1/2 page and with NONE in all CDU n GRAPHICS
DISP ON fields on the GRAPHICS setup page.
AT LEAST ONE CDU IS CONFIGURED FOR
GRAPHICS AND A SERIAL LO- or HI-RES
DISPLAY IS CONFIGURED BUT WEATHER
MAPS ARE DISABLED.
Configure UniLink either with ENABLED in the WX
MAPS field on the TEL CONFIG 1/2 page or with
NONE in all CDU n GRAPHICS DISP ON fields on the
GRAPHICS setup page and with no PORT n field as
LO-RES DISPLAY, HI-RES DISPLAY 1, or HI-RES
DISLAY 2 on the SERIAL setup pages.
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Configuration Error Messages
Text Action
HR-1 IS CONFIGURED FOR GRAPHICS BUT
NO HI-RES DISPLAY 1 SERIAL INTERFACE IS
CONFIGURED.
Configure UniLink either with an HI-RES DISPLAY 1 serial port or remove HR1 from the GRAPHICS setup configuration.
HR-2 IS CONFIGURED FOR GRAPHICS BUT
NO HI-RES DISPLAY 2 SERIAL INTERFACE IS
CONFIGURED.
Configure UniLink either with an HI-RES DISPLAY 2 serial port or remove HR2 from the GRAPHICS setup configuration.
HI-RES DISPLAY 1 SERIAL INTERFACE IS
CONFIGURED BUT NO HR-1 IS CONFIGURED
FOR GRAPHICS.
Configure UniLink either with a HR1 on the
GRPAHICS setup page or remove HI-RES DISPLAY 1 from the SERIAL configuration.
HI-RES DISPLAY 2 SERIAL INTERFACE IS
CONFIGURED BUT NO HR-2 IS CONFIGURED
FOR GRAPHICS.
Configure UniLink either with a HR2 on the
GRPAHICS setup page or remove HI-RES DISPLAY 2 from the SERIAL configuration.
PRE-DEPARTURE CLEARANCE IS ENABLED
BUT NO VALID AIRCRAFT TYPE IS PRESENT.
Configure UniLink either with a valid four-character
ICAO aircraft type designator in the TYPE field on the
A/C CONFIG page or with DISABLED in the
PREDEPARTURE field on the CLEARANCES page.
A750 VDR CONFIGURED ON LOW-SPEED
TRANSMIT PORT.
A429 TRANSMIT PORT SET TO A750 VDR
AND VM CMC
Configure the ARINC 429 transmit port, which is configured to A750 VDR, to HIGH speed.
Configure the ARINC 429 transmit port to either A750
VDR or VM (Vibro-Meter) CMC.
ARINC 429 PORTS CONFIGURED FOR ARINC
750 VDR BUT VHF RADIO TYPE NOT SET TO
ARINC 750 VDR
Configure RADIO TYPE to A750 VDR.
VHF RADIO TYPE SET TO ARINC 750 VDR
BUT NO ARINC 429 PORTS ARE
CONFIGURED FOR AN ARINC 750 VDR.
VHF RADIO TYPE SET TO A750 VDR AND
VDR MODE-SELECT DISCRETE IS
CONFIGURED BUT THE DISCRETE ACTIVE
STATE IS NOT SET TO OPEN
VHF RADIO CONFIGURED BUT ICAO
AIRCRAFT ADDRESS MISSING
Configure ARINC 429 transmit and receive ports to
A750 VDR.
If an A750 VDR is installed and VDR voice select discrete is configured, set the discrete ‘active’ state to
‘OPEN’.
ILLEGAL ICAO AIRCRAFT ADDRESS
Configure UniLink with a legal ICAO aircraft address, which ranges from 00000001 octal through 77777776 octal and is normally included on the aircraft registration document.
Configure UniLink with a legal ICAO aircraft address, which ranges from 00000001octal through 77777776 octal and is normally included on the aircraft registration document.
FANS DISABLED – NO VALID AIRCRAFT
REGISTRATION IS CONFIGURED
FANS DISABLED – VHF RADIO OR SDU NOT
CONFIGURED
Configure UniLink either with a valid aircraft registration in the REGISTRATION field on the A/C
CONFIG page or with FANS as DISABLED.
Configure UniLink with a VHF radio and/or an SDU, or do not configure FANS.
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Configuration Error Messages
Text Action
FANS DISABLED – ATC DATABASE NOT
INSTALLED
Configure UniLink with FANS functionality ENABLED and load a valid ATC database or configure UniLink with FANS disabled.
FANS DISABLED – DUAL UASC FMS NOT
CONFIGURED
SQP MIN IS SET BELOW THREE
Configure UniLink for two UASC FMSs or configure
UniLink with FANS disabled.
Configure SQP MIN with a value greater than three.
SQP THRESHOLD IS BELOW ONE OR ABOVE
EIGHT
Configure the SQP threshold with a value greater than one but less than eight.
CVR CONFIGURED ON LOW-SPEED
TRANSMIT PORT.
Configure the ARINC 429 transmit port, which is configured to CVR, to HIGH speed or assign the CVR to a high speed port.
NOTE 1 : If an MCDU is wired and configured as an ARINC 739A MCDU, which does not display graphics, a low-resolution MFD-640 or a high-resolution MFD-640/EFI-890R must also be configured in order to display graphics. If an MCDU is wired and configured as a UASC FMS
CDU, the MCDU is able to receive graphics and, therefore, no other device is necessary to display graphics.
NOTE 2 : A low-resolution MFD-640 and high-resolution MFD-640/EFI-890R are configured on the
GRAPHICS setup page in the appropriate CDU n GRAPHICS DISP ON field(s).
NOTE 3 : The SQP threshold is the difference between the SQP of the currently tracked ground station and the value of the SQP of another ground station necessary to initiate a handoff.
D. Hidden Error/Status Messages
Hidden Error/Status Messages
Text Action/Description
UNKNOWN ERROR Cycle power to UniLink. If condition persists contact UASC.
THE PORTION OF FLASH MEMORY CONTAINING
THE MTBF COUNTER HAS BEEN CORRUPTED
AND THE MTBF COUNT IS NO LONGER VALID
Cycle power to UniLink. If condition persists contact UASC.
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UL-801 Installation Manual
Appendix 1
This appendix contains industry-standard acronyms, abbreviations, and terms used in the UniLink
Installation manual.
1. Acronyms, Abbreviations, and Terms
Acronym/Abbreviation/Term Description
System
ACK Acknowledgment
ADC Air Data Computer
AFN ATS Facilities Notification
ALT Altitude
AOA ACARS Over Aviation VHF Link Control (AVLC)
ARINC
ATC
ATIS
ATM
ATS
AVLC
BCS
CDA
Aeronautical Radio, Incorporated (Data Interface Format
Standard
Air Traffic Control
Automatic Terminal Information System (see D-ATIS)
Air Traffic Management
Air Traffic Services
Aviation VHF Link Control
Block Check Sequence
Current Data Authority
CDU
Circuit Mode Data
Control Display Unit
A full duplex bi-directional communication link in which data is transmitted and received simultaneously. A hand shake must be established prior to data being exchanged.
Supported by a UniLink RS-232 port configured for TEL.
CLX Clearance
CMU
CNS
COMM
Communication Management Unit
Communication Navigation Surveillance
Communication (also referred to as COM)
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Acronym/Abbreviation/Term Description
CRC
CSDB
CTS
CVFDR
CVR
D-ATIS
DEPT CLX
DLSP
Cyclic Redundancy Check
Commercial Standard Data Bus (Data Interface Format
Standard)
Clear to Send
Cockpit Voice and Flight Data Recorder (UASC)
Cockpit Voice Recorder
Digital Automatic Terminal Information System (also referred to as ATIS)
Departure Clearance
Datalink Service Provider (also referred to as DSP)
DPSK
DTU
DTU-100
DSP
EFB
Differential Phase Shift Keying
Data Transfer Unit (UASC)
Data Transfer Unit-100 (UASC)
Datalink Service Provider (also referred to as DLSP)
Electronic Flight Bag
ETA
ETD
Estimated Time of Arrival
Estimated Time of Departure
EXP Expected
FAA
FANS
Federal Aviation Administration
Future Air Navigation Systems
FLT NO
FMS
Flight Number
Flight Management System (UASC)
FREQ Frequency
FSK Frequency Shift Keying
GND SPD
GNSS
GPS
Ground Speed
Global Navigation Satellite System
Global Positioning System
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Acronym/Abbreviation/Term Description
ICAO International Civil Aviation Organization
I/O Input/Output
LOS Line of Sight
MARSA
MCDU
Military Assumes Responsibility for Separation of Aircraft
Multifunctional Control Display Unit (UASC)
MCDU Multi-Purpose Control Display Unit (ARINC)
MCU Modular Concept Unit
MDM Modem
MIC Microphone
MSG Message
MSK
MVFR
Minimum Shift Keying
Marginal Visual Flight Rules
NDA
NO CVG
Next Data Authority
No Coverage
ONBD Onboard
OOOI Out, Off, On, In (used to detect and report changes to the major flight phases of the aircraft)
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Acronym/Abbreviation/Term Description
Packet Mode Data A half duplex bi-directional communication link in which data is accumulated in packets of various lengths and sent out in a burst or bursts so therefore does not support voice communications. Packet switching is the process of routing and transferring data by means of addressed packets so that a channel is occupied during the transmission of the packet only. Upon completion of the data transfer, the channel is made available for the transfer of other traffic. Supported by a UniLink ARINC port configured to provide VHF and
SAT capability.
PFD
PIREP
Primary Flight Display
Pilot Weather Report
POA Plain Old ACARS
POS Position
PTT Push-to-Talk
RCDU Remote Control Display Unit
RCVD Received
RPTS Reports
RTS Request to Send
RQD Required
RTE Route
RX Receive
SAT Abbreviation for Satellite Communications Link. The SAT link provides communication via Iridium Short Burst Data
(SBD) and packet mode data Inmarsat equipment that utilizes a specific satellite constellation.
SCN
SDU
Software Control Number
Satellite Data Unit
SITA
SQP
SSDTU
Society of International Aeronautical Telecommunications
(Societe Internationale de Telecommunications
Aeronautiques)
Signal Quality Parameter
Solid State Data Transfer Unit (UASC)
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Acronym/Abbreviation/Term Description
TEL Abbreviation for telephony. The telephony communication link provides a circuit mode data connection via a dial-up modem. A hand shake must be established prior to data being exchanged. Only an RS-232 capable SatCom can be used.
TWIP Terminal Weather Information for Pilots
TX Transmit
UASC Universal Avionics Systems Corporation
Unverified Message
USB
An Unverified message is one that does not contain safeguards to prevent data corruption during transmission.
Such messages are labeled AOC on the page in which they are displayed. See Verified Message.
Universal Serial Bus
Verified Message
VHF
A Verified message is one that has been safeguarded against potential data corruption during transmission and is determined to be error-free using CRC code comparisons and validity indicators. See Unverified Message.
Very High Frequency terrestrial-based packet mode. This is a data communications link used for obtaining textual weather, D-ATIS, and the transmission of position reporting, OOOI, and safety services communications
(UniLink Flight Information Services). Does not support weather graphics.
VOX Voice
VSWR
WOW
Voltage Standing Wave Ratio
Weight On Wheels
WPT Waypoint
WX Weather
XMT Transmit
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Appendix 2
This appendix contains UniLink Menus and subordinate menus. Pages illustrated with dashed boxes are optional and are only available when the functionality reflected on the pages is enabled via
UniLink-configured options.
1. UniLink Menus and Submenus – without FANS
A. UniLink Menu 1/2
NOTES
:
1.
Only available if OOOI is enabled in configuration.
2.
Only available if VHF is enabled in configuration.
3.
Only available if DATA is enabled in configuration.
4.
Only available if TEL is enabled in configuration.
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UniLink Menu 1/2 – Continued
NOTES
:
1.
Only available if TEL is enabled in configuration.
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B. UniLink Menu 2/2
UL-801 Installation Manual
NOTES
:
1.
Check with DSP for availability of this feature.
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MAINTENCE 1/3
(continued from previous page)
SYS CONFIG
1/4
I/O CONFIG
SYS CONFIG
2/4
VHF CONFIG
SAT CONFIG
PRIORITY
TEL CONFIG
POS REPORT
REVIEW
AiRCRAFT
CLEARANCES
ALERTS
SYS CONFIG
3/4
SYS CONFIG
4/4
DISC IN
DISC OUT
ARINC RX
ARINC TX
SERIAL
GRAPHICS
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2. UniLink Menus and Submenus – with FANS
A. UniLink Menu 1/2
UNILINK
MENU
FLIGHT INFO
D-ATIS
TWIP
DEPARTURE
CLX
OCEANIC
CLX
VERIFY
MSGS
PUSHBACK
CLX
EXP TAXI CLX
OCEANIC
CLX ATC
ATC
ATC
EMERGENCY
ATC LOG ON
1/2
ATC LOG ON
2/2
ATC REVIEW
(MAYDAY)
ATC REVIEW
(PAN)
ATC REVIEW
(Cancel
Emergency)
ATC LOG ON
TO
(LOG ON TO Region pages including:
- N PACIFIC
- S PACIFIC
- ASIA
- INDIAN OCEAN
- N ATLANTIC
- S ATLANTIC
- EUROPE)
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UniLink Menu 1/2 – Continued
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UniLink Menu 1/2 – Continued
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UniLink Menu 1/2 – Continued
NOTES:
1.
Only available if VHF is enabled in configuration (UL-800 only).
2.
Only available if SAT is enabled in configuration.
3.
Only available if TEL is enabled in configuration.
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UNILINK
MENU
Continued
MAINTENANCE
1/3
DEVICES
SENSORS 1/2
SENSORS 2/2
VERSIONS
ERROR LOG
SYS CONFIG
1/4
DISCRETES
BCST DATA
SOURCE FMS
VDR STATUS
I/O CONFIG
VHF CONFIG
SAT CONFIG
PRIORITY
TEL CONFIG
POS REPORT
REVIEW
DISC IN
DISC OUT
ARINC RX
ARINC TX
SERIAL
GRAPHICS
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B. Maintenance Menu – Continued
Includes Configuration Menu choices
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NOTES:
1.
Only available if OOOI is enabled in configuration.
2.
Only available if TEL is enabled in configuration.
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OPS Menu – Continued
UL-801 Installation Manual
NOTES:
1.
Only available if TEL is enabled in configuration.
2.
The SELCAL option only displays when associated messages are available. Check with DSP for availability of this feature.
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Appendix 3
This appendix contains a list of Datalink Service Providers (DSP) that may be used with the
UniLink.
1. Datalink Service Providers
Providers
ARINC Direct
Honeywell OneLink Aero-I and Aero-M Communication Services
Sat Com Direct
SATCOM1
Sita
Universal Weather and Aviation
Contact Information https://direct.ARINC.net
941-360-0680 (24 hr.)
602-822-7502 (Fax)
888-448-9003
321-777-3000
321-777-3702 (Fax)
+ 45 4615 4546 http://satcom1.com/ http://www.sita.aero/
801-231-5600
713-944-1622
713-943-4610 (Fax)
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Key features
Air-to-ground datalink
Supports FANS 1/A+
Connects to FMS and CDU/MCDU
VHF Data Radio (VDR) support
Supports multiple communication systems
Provides graphical weather maps
Supports ADS-C and CPDLC
Handles OOOI reporting
Provides automatic position reporting
Customizable user interface
Frequently asked questions
The UL-801 provides a two-way digital datalink for air-to-ground communications, allowing for communication with Datalink Service Providers (DSPs) for various services such as FANS, ADS-C, and CPDLC.
The UL-801 connects to Flight Management Systems (FMS), Control Display Units/Multi-Function Control Display Units (CDU/MCDU), VHF Data Radio (VDR), and other peripheral devices such as multi-function displays (MFDs) and a printer.
The UL-801 enables enhanced safety of flight, efficiency, and increased air traffic capacity by replacing voice transmissions between crews and ATC with datalink messages during oceanic and remote areas.
Yes, the UL-801's Customer Database (CDB)-driven user interface and message set can be customized to match the specific operational requirements of airlines or business operators.
The UL-801 utilizes a Data Transfer Unit (DTU-100) or a Solid State Data Transfer Unit (SSDTU) for field-loading software and databases.
The UL-801 supports both VHF and Satellite SatCom systems, allowing for communication with DSPs via various methods, including VDL Mode 2 and POA, Aero-I, Aero-M, and Iridium or Inmarsat ARINC 741 systems.
