ARINC 808 : 2010
Current
The latest, up-to-date edition.
3GCN - CABIN DISTRIBUTION SYSTEM
Hardcopy , PDF
English
26-11-2010
1.0 INTRODUCTION
1.1 Purpose of this Document
1.2 Related Documents
1.3 Head End + Cabin Distribution Network (CDN)
2.0 CABIN DISTRIBUTION NETWORK
2.1 Cabin Distribution System
3.0 HEAD END NETWORK
3.1 Head End Equipment
3.2 Cabin Electronics Compartment (CEC)
3.3 Cabin Attendant Control Station (CACS)
3.4 Seat Power
3.5 Passenger Services
3.6 Data Load
3.7 BOSS
3.8 CTU/SDU/NATS
3.9 Entertainment Camera
3.10 Health Management
3.11 Availability
3.12 Quality of Service
4.0 AREA NETWORK
4.1 Area Distribution Equipment
4.2 Area Distribution Box
4.3 Floor/Wall Disconnect Interface - data (FDI/WDI)
4.4 Power Floor/Wall Disconnect Interface (PWDI/PFDI)
5.0 OVERHEAD NETWORK
5.1 Overhead Distribution Equipment
6.0 SEAT NETWORK
6.1 Seat Distribution Equipment
6.2 Integrated Seat Box (ISB)
6.3 Integrated Seat Box (power)
7.0 PASSENGER NETWORK
7.1 Passenger Distribution Equipment
8.0 FIBER OPTIC NETWORK
8.1 Introduction
8.2 Fiber Network Topology
8.3 Fiber Optic Cable/Termini Characteristics
9.0 IN-SEAT POWER NETWORK
9.1 Introduction
9.2 System Operation
9.3 Power Floor/Wall Disconnect
9.4 Deleted
9.5 Control Data for Seats
10.0 SECURITY
10.1 IFE Network Security
10.2 Network Capabilities
10.3 Passenger Data
10.4 System Content
10.5 System Operation and Maintenance
ATTACHMENTS
1 - Broadband Off-Board Services System (BOSS) and
Passenger Connectivity Standard
2 -IFES Digital Printer Interface Specification
APPENDICES
A - List of Acronyms
B - D-Sub Connector
C - BOSS MIB Software Interfaces
D - Head End Network Connectorization
E - Quad Cable Design Guidelines
ARINC Standard - Errata Report
APIM
Describes general architectural philosophy and aircraft infrastructure for the proper use and interface of various cabin related IFE equipment.
| DocumentType |
Standard
|
| Pages |
187
|
| PublisherName |
Aeronautical Radio Inc.
|
| Status |
Current
|
| Supersedes |
| ARINC 791P3:2024 | MARK I AVIATION KU-BAND AND KA-BAND SATELLITE COMMUNICATION SYSTEM, PART 3 INFORMATION TRANSFER AND INTERNETWORKING |
| ARINC 805 : 2006 SUPP 4 | FIBER OPTIC TEST PROCEDURES |
| ARINC 413A : 1976 | GUIDANCE FOR AIRCRAFT ELECTRICAL POWER UTILIZATION AND TRANSIENT PROTECTION |
| ARINC 811 : 2005 | COMMERCIAL AIRCRAFT INFORMATION SECURITY CONCEPTS OF OPERATION AND PROCESS FRAMEWORK |
| MS3367 Revision F:1978 | STRAP, TIEDOWN, ELECTRICAL COMPONENTS, ADJUSTABLE, SELF CLINCHING, PLASTIC, TYPE I, CLASS 1 (S/S BY SAE-AS33671) |
| SAE ARP4754A | Guidelines for Development of Civil Aircraft and Systems |
| ARINC 665 : 1999 SUPP 4 | LOADABLE SOFTWARE STANDARDS |
| ARINC 664-5 : 2005 | AIRCRAFT DATA NETWORK - PART 5: NETWORK DOMAIN CHARACTERISTICS AND INTERCONNECTION |
| TIA/EIA 626 : 1995 | MULTIMODE FIBER-OPTIC LINK TRANSMISSION DESIGN |
| IEEE 802.1Q-2014 | IEEE Standard for Local and metropolitan area networks--Bridges and Bridged Networks |
| IEEE 802.1D-2004 | IEEE Standard for Local and metropolitan area networks: Media Access Control (MAC) Bridges |
| ARINC 765 : 2003 | ETHERNET SWITCH UNIT (ESU) |
| IEEE 802.11A : 1999 | TELECOMMUNICATIONS AND INFORMATION EXCHANGE BETWEEN SYSTEMS - LOCAL AND METROPOLITAN AREA NETWORKS - SPECIFIC REQUIREMENTS - PART 11: WIRELESS LAN MEDIUM ACCESS CONTROL (MAC) AND PHYSICAL LAYER (PHY) SPECIFICATIONS - HIGH-SPEED PHYSICAL LAYER IN THE 5 GHZ BAND |
| ARINC 666 : 2002 | ELECTRONIC DISTRIBUTION OF SOFTWARE |
| IEC TR 61930:1998 | Fibre optic graphical symbology |
| MIL-DTL-38999 Revision M:2015 | Connectors, Electrical, Circular, Miniature, High Density, Quick Disconnect (Bayonet, Threaded or Breech Coupling), Environment Resistant with Crimp Removable Contacts or Hermetically Sealed with Fixed, Solderable Contacts, General Specification for |
| NEMA WD 6 : 2016 | WIRING DEVICES - DIMENSIONAL SPECIFICATIONS |
| ARINC 606 : 1984 SUPP 1 | GUIDANCE FOR ELECTROSTATIC SENSITIVE DEVICE UTILIZATION & PROTECTION |
| EN 3545-001:2008 | Aerospace series - Connectors, electrical, rectangular, with sealed and non-sealed rear, plastic housing, locking device, operating temperatures - 55 °C to 175 °C - Part 001: Technical specification |
| ARINC 664-3 : 2002 SUPP 2 | AIRCRAFT DATA NETWORK - PART 3: INTERNET-BASED PROTOCOLS AND SERVICES |
| FAA AC 43.13-1 : 0 | ACCEPTABLE METHODS, TECHNIQUES, AND PRACTICES - AIRCRAFT INSPECTION AND REPAIR |
| ATA 100 : REV 37 | MANUFACTURERS TECHNICAL DATA |
| ARINC 609 : 1987 | DESIGN GUIDANCE FOR AIRCRAFT ELECTRICAL POWER SYSTEMS |
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