CareersNewsEvents
Home Our CompanyProducts And SystemsService And SupportInvestor RelationsContact Us
  Home > Product Catalog > Air Transport > FSA
 printable view
Browse by:

Search by:
    Product Index
Product Catalog - Air Transport
Air Transport  | Business and Regional  | Government  | Service and Support

FSA
FlySmart with Airbus


OVERVIEW

In the midst of the information age, airlines are increasingly looking for ways to connect their aircraft into ground based IT networks in order to enhance operational efficiencies and improve customer service.

Rockwell Collins FlySmart with Airbus (FSA) system combines COTS hardware and software solutions with avionics grade systems in order to safely and efficiently link aircraft with ground based IT networks in order to provide business solutions that move airlines fully into the information age.


DESCRIPTION

FSA Architecture
The FSA system is composed of two network server units (NSUs) segregated by an Ethernet gateway unit (EGU). The server interface unit (SIU) serves as the firewall between the NSUs and the aircraft avionics. Access to these servers can be through wired connections in the aircraft through wireless LAN units (WLUs) and cellular wireless units (UMTS) that allow communication within the aircraft and with the airport wireless gatelink system.

FSA Hardware
The foundation of Collins FSA equipment is commercial-off-the-shelf (COTS) computer network components consisting of a NSU, SIU, WLU, UMTS, and EGU, a terminal wireless antenna (MAA), a passive RF triplexer device (TPLX), and a cabin wireless antenna (PMAA).

The NSU serves as a data acquisition, processing and mass data storage device. The FSA architecture dedicates one NSU to be accessible by the flight crew (and some flight-related avionics), cabin crew and maintenance crew, and dedicates the other NSU for passenger applications and services. The NSU is based on a PC industry standard computing platform and has an upgrade path similar to commercial computers systems, thus reducing the cost and time required for updates.

The EGU provides network routing and firewall functions between the cabin side network and the aircrew network onboard the aircraft.

The SIU serves as the firewall between the aircraft's avionics and the aircrew's NSU. Unlike the NSU, the SIU meets the certification requirements of DO-178B, Level C software to minimize the potential of corrupting avionics software and/or databases.

This server-firewall arrangement allows commercial (Level E certified) software applications executing on the aircrew's NSU to access the aircraft's avionics systems data output, without endangering the integrity of the avionics operation or performance. Concurrently the SIU allows flight deck avionics software programs and databases to be safely, reliably, and efficiently updated; thereby bringing the full effect of management efficiencies of information systems technology to daily airline operations.

Gatelink is a cost effective, short-range, spread spectrum, broad-band, wireless, microwave data link that can rapidly move large quantities of data on and off the aircraft. Gatelink is the capstone that completes the integration of aircraft and terrestrial IT networks. The WLU is the microwave transceiver and the MAA is the antenna that supports transmission and reception of signals between the aircraft and ground based network.

In addition to the 802.11b/g wireless connectivity, the UMTS unit that has a GSM, GPRS, EDGE , UMTS WCDMA / HSDPA / HSUPA radio modem to provide cellular connection to the public cellular infrastructure enabling integration of aircraft and terrestrial IT networks. The passive RF triplexer device TPLX, can be used to share the above mentioned MAA antenna.


FSA Software
MS Windows 2000 and Linux operating systems are used to manage the aircraft LAN. Features include a dynamic host control protocol server, routing services, and a domain name server.

The NSUs host a variety of software applications that airlines can use to improve their operations or enhance services. In partnership with leading software companies, Rockwell Collins offers a robust portfolio of applications such as the following:


Flight Operations
  • Electronic flight manuals and checklists
  • Electronic charts and maps
  • Data linked advanced weather graphics
  • Crew eMail
  • Performance calculations
  • Electronic technical logbook

Cabin Operations
  • Electronic cabin manuals and checklists
  • Electronic cabin logbook

Maintenance Operations
  • Remote FSA configuration management
  • Electronic maintenance manuals and checklists
  • Virtual quick access recorder (QAR)
  • Maintenance data analysis tool

Passenger Services
  • Passenger eMail
  • Passenger airborne intranet

In addition, Rockwell Collins' FSA uses open architecture standards that enable airline customers to write their own software applications for hosting on the NSU or port their legacy IT applications onto the NSU. The NSU provides an automatic Applications installation service based on the ARINC 665 standard load packaging.


SPECIFICATIONS

All components of FSA have been certified and tested to DO-160D.

Specifications are subject to change without notice.


Network Server Unit (NSU-2120)
Utilizing a backbone of industry standard interfaces, such as PCI, IDE and fast Ethernet, the NSU provides a flexible means to assist in the management of aviation assets and customers.

NSU-2120


Physical Characteristics 
 
NSU-2120
 
Size
 
ARINC 600 4 MCU
 
Weight
 
7.7 kg maximum (16.9 lbs)
 
Cooling
 
ARINC 600
 
Installation
 
Mounted in EE bay
 

Power Requirements 
 
NSU-2120
 
Power
 
115 Vac, 400 Hz and 28 Vdc, back up battery pack, 2 minute (nominal) hold-up time
 

Connectors 
 
NSU-2120
 
Rear Connectors
 
ARINC 600 - Size 2
 
Front Panel Connectors
 
Video, Keyboard, USB
 

Other 
 
NSU-2120
 
Processor/memory
 
Intel Pentium M1.1GHz, RAM 1GB
 
Network
 
11 Ethernet 100 Base T
 
Serial Ports
 
1 RS-232
 
Hard Drive
 
1 IDE 100GB
128 MB Optional Compact Flash
 
Bus Support
 
PCI, IDE
 
Operating System
 
Windows 2000 server and Linux 2.2/2.4 server
 

Secure Interface Unit (SIU-2002)
The SIU provides a variety of interfaces. The SIU incorporates one IEEE 802.3 Ethernet 100-BaseT Port to be used for communications with the NSU.

SIU-2002


Physical Characteristics 
 
SIU-2002
 
Size
 
ARINC 600 4 MCU
 
Weight
 
5.9 kg maximum (15.8 lbs)
 
Cooling
 
Forced Air Cooling per ARINC 600-8
 
Installation
 
Mounted in EE bay
 

Power Requirements 
 
SIU-2002
 
Power
 
115 VAC, 400 Hz and 28 VDC
 

Environmental 
 
SIU-2002
 
Temperature
 
-15°C to +70°C; Short term -40°C to +85°C°C maximum, Air Pressure
 
Drop through Unit
 
6.35 mm
 
Diameter of Inlet and Exhaust Opening
 
4.1 mm
 

Other 
 
SIU-2002
 
Processor/memory
 
PowerPC Processor
 
Operating System
 
VMOS
 

Ethernet Gateway Unit (EGU-2100)
The EGU functions as a managed switch, router, and firewall between cabin passenger services and flight deck avionics services.

EGU-2100


Physical Characteristics 
 
EGU-2100
 
Size
 
ARINC 600 4 MCU
 
Weight
 
6.79 kg maximum (18 lbs)
 
Cooling
 
ARINC 600
 
Installation
 
Mounted in EE bay
 

Power Requirements 
 
EGU-2100
 
Power
 
115 VAC, 400 Hz
 

Environmental 
 
EGU-2100
 
Temperature
 
-15°C to +70°C; Short term -40°C to +70°C
 

Connectors 
 
EGU-2100
 
Rear Connectors
 
ARINC 600 - Type 11
 
Front Panel Connectors
 
Ethernet, Serial and JTAG
 

Other 
 
EGU-2100
 
Processor
 
PowerPC
 
Operating System
 
WindRiver VxWorks
 

Terminal Wireless LAN Unit (WLU-2100)
The aircraft terminal WLU connects with Gatelink by using IEEE 802.11b/g compliant 2.4 GHz direct sequence spread spectrum technology. The WLU-2100 is designed around the Cisco Aironet 1242 access point and a 115VAC wide frequency / 28VDC power supply. It is housed in an ARINC 763 compliant housing that utilizes conduction cooling.

Cabin Wireless LAN Unit (WLU-2100)
The CWLU is used to create a wireless LAN inside the aircraft. Using the same 2.4 GHz direct sequence spread technology, the CWLU provides the wireless LAN between the flight/cabin crew's or passenger's computers and the NSU through the EGU. With the proper authorization, and laptop or personal digital assistant computer outfitted with 802.11b/g wireless LAN capability can gain access to the NSU.

WLU-2100


Physical Characteristics 
 
WLU-2100
 
Width
 
174 mm (6.85 in)
 
Height
 
76 mm (3.0 in)
 
Length
 
292 mm  (11.5 in)
 
Weight
 
2.1 kg maximum (4.7 lbs)
 
Cooling
 
Passive
 
Installation
 
Mounted in cabin
 

Power Requirements 
 
WLU-2100
 
Power
 
115 VAC, Variable Freq. or 28VDC
 
Power Dissipation
 
15W
 

Universal Mobile Telecommunication System (UMTS-2100)
The UMTS is a GSM/UMTS cellular device implementing radio technologies based on 3GPP Release 5 capabilities for mobile terminated equipment. This device is capable of providing cellular data connectivity between the aircraft and ground based cellular base stations, there by extending communication services to the airline and airport intranets.

The UMTS supports quad-band GSM (850/900/1800/1900 MHz) and tri-band UMTS (850/1900/2100 MHz) cellular operation. The UMTS also supports Ethernet LAN between the flight/cabin crew's computers and the NSU through the EGU.


Physical Characteristics 
 
UMTS-2100
 
Width
 
174 mm (6.85 in)
 
Height
 
76 mm (3.0 in)
 
Length
 
292 mm  (11.5 in)
 
Weight
 
2.2 kg maximum(4.8 lbs)
 
Cooling
 
Passive
 
Installation
 
Mounted in cabin
 

Power Requirements 
 
UMTS-2100
 
Power
 
115 VAC, Variable Freq. or 28VDC
 
Power Dissipation
 
20W
 

Filter Triplexer (TPLX-2101)
The TPLX is a passive RF device. Its role is to combine/split radio signals of three different technologies (2.1GHz GSM/UMTS, 2.4GHz 802.11b/g, and 5GHz 802.11a) into a single common output to the airborne antenna. The TPLX provides a high-degree of port-to-port RF isolation, to eliminate unwanted interactions between WLU and UMTS units.

Physical Characteristics 
 
TPLX-2101
 
Width
 
19 mm (.75 in)
 
Height
 
60 mm (2.36 in)
 
Length
 
65 mm  (2.56 in)
 
Weight
 
.12 kg maximum(.26 lbs)
 
Installation
 
Mounted in cabin
 

Terminal Wireless Antenna (MAA-2000)
The MAA is a passive, vertically polarized, omni-directional antenna for aircraft external mounting.

MAA-2000


Physical Characteristics 
 
MAA-2000
 
Width
 
45 mm (1.75 in)
 
Height
 
62 mm (2.42 in)
 
Length
 
132 mm  (5.17 in)
 
Weight
 
0.13 kg (0.3 lbs) maximum
 
Installation
 
Top mounted antenna
 

Cabin Wireless Antenna (PMAA-2000)
The PMAA is a passive, circularly polarized antenna for installation in the cabin interior space.

PMAA-2000


Physical Characteristics 
 
PMAA-2000
 
Width
 
154.8 mm (6.09 in)
 
Height
 
22.2 mm (0.88 in)
 
Length
 
154.8 mm  (6.09 in)
 
Weight
 
0.32 kg (0.7 lbs) maximum
 
Installation
 
Interior mounting