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Standard

CABIN EQUIPMENT INTERFACES PART 9 CABIN INTERFACE NETWORK (CIN)

2017-12-29
CURRENT
ARINC628P9-5
ARINC 628, Part 9 defines general architectural philosophy and aircraft infrastructure for the proper use and interface of various cabin information network related equipment. It specifies a generic on-board infrastructure with commercial server technology, high-speed data communication and exchange via wired and wireless LAN for a wide range of applications. Supplement 5 significantly modifies the standard to remove references to obsolete cabin information network definition. It adds references to current cabin network definitions, ARINC 664: Aircraft Data Network and ARINC 808: Third Generation Network (3GCN).
Standard

CNS/ATM AVIONICS ARCHITECTURES SUPPORTING NEXTGEN/SESAR CONCEPTS

2014-01-10
CURRENT
ARINC660B
This document identifies and describes the aircraft avionics capability necessary for operation in the evolving Communications Navigation Surveillance/Air Traffic Management (CNS/ATM) environment expected for the FAA NextGen program, Single European Sky ATM Research (SESAR) program and considerations of the Japan Collaborative Actions for Renovation of Air Traffic Systems (CARATS). These capabilities are intended to satisfy the industry's long-term CNS/ATM operational objectives.
Standard

AIRCRAFT DATA NETWORK PART 8 INTEROPERATION WITH NON-IP PROTOCOLS AND SERVICES

2010-11-12
CURRENT
ARINC664P8-1
This Specification was written to support future aeronautical applications and services beyond those using Transmission Control Protocol/Internet Protocol (TCP/IP). The initial focus is to support air/ground applications using the Aeronautical Telecommunications Network (ATN). These include Controller-Pilot Data Link Communication (CPDLC), Flight Information System (FIS), and Context Management Application (CMA). Supplement 1 was written to allow interoperation with non-IP protocols and services and upper layer services with respect to the OSI reference model. Supplement 1 reflects ICAO Aeronautical Communication Panel recommendations.
Standard

AIRCRAFT DATA NETWORK PART 7 AVIONICS FULL-DUPLEX SWITCHED ETHERNET NETWORK

2009-09-23
CURRENT
ARINC664P7-1
The purpose of this document is to define a deterministic network: Avionics Full Duplex Switched Ethernet (AFDX). AFDX is a trademark of Airbus and is used with permission. This document also highlights the additional performance requirements of avionics systems within the context of AFDX.
Standard

AIRCRAFT DATA NETWORK PART 3 INTERNET-BASED PROTOCOLS AND SERVICES

2009-02-16
CURRENT
ARINC664P3-2
This specification defines Network and Transport layer provisions for data networks that are installed on commercial aircraft. The definitions are based on Internet Engineering Task Force (IETF) Internet protocol and service standards that have been published as Request for Comments (RFC). In some cases the protocols and services are tailored for use on board aircraft. The specification identifies two types of networks: First, Compliant Aircraft Data Network, which operates fully within the applicable Internet specifications. Second, Profiled Aircraft Data Network, in which one or more industry standard protocols have been extended to address the unique environment of aircraft installations. Within the specification, the functionality of Internet protocols and services are defined with the intent that interoperability of components connected to onboard data networks can be achieved without undue restrictions on the component designer.
Standard

AIRCRAFT DATA NETWORK, PART 2 - ETHERNET PHYSICAL AND DATA LINK LAYER SPECIFICATION

2009-01-16
CURRENT
ARINC664P2-2
This specification provides Ethernet physical parameters and data link layer specifications for use in a commercial aircraft environment. This specification provides general and specific guidelines for the use of IEEE 802.3 compliant Ethernet, 2000 edition. Physical layer and Medium Access Control (MAC) sub-layers are expected to comply with the Open System Interconnection (OSI) Reference Model to enable maximal utilization of off-the-shelf components, both hardware and software, for aviation use. The Ethernet Physical layer specification defines the electrical and optical parameters for the 10BASE-T, 100BASE-TX, and 100BASE-FX Ethernet implementations. This specification references ARINC Specification 600: Air Transport Avionics Equipment Interfaces for definition of copper-based implementations of the Ethernet Physical layer.
Standard

AIRCRAFT DATA NETWORK PART 4 INTERNET-BASED ADDRESS STRUCTURE & ASSIGNED NUMBERS

2007-12-21
CURRENT
ARINC664P4-2
This specification defines the addressing plan and rules for addressing used in Aircraft Data Networks (ADN). The plan is organized in accordance with the seven-layer Open Systems Interconnection (OSI) Reference Model. The specification sets forth the structure of addresses that are employed in the ADN and guidance for address determination. This guidance ensures that all applications - that use this address structure to send messages - can know the address structure of the destination(s) at configuration-time.
Standard

AIRCRAFT DATA NETWORK PART 1 SYSTEMS CONCEPTS AND OVERVIEW

2006-06-30
CURRENT
ARINC664P1-1
This specification provides the overview of aircraft data networks installed in air-transport aircraft, tutorial information for adaptation of commercial network standards to air-transport aircraft, and terminology used to describe aircraft data networks. This specification explains the dependency of Aircraft Data Network (ADN) standards on network standards developed by the Internet community, IEEE, and ISO. The classes, Compliant Networks and Profiled Networks, used to characterize aircraft networks are introduced.
Standard

AIRCRAFT DATA NETWORK PART 5 NETWORK DOMAIN CHARACTERISTICS AND INTERCONNECTION

2005-04-12
CURRENT
ARINC664P5
ARINC 664, Part 5 provides the design and implementation guidelines for networks installed in aircraft. Such networks may be used to enable network devices to communicate among themselves and with networks outside of the aircraft. This specification defines a set of domains within the aircraft. These domains are defined in terms of the services they provide, the security they provide to the functions within their boundaries, and the connections required between a domain and other domains and networks external to the aircraft. This specification provides general design and implementation guidelines that, when they are implemented by aircraft devices and configured by the system integrator, the devices provide the required connectivity, quality of service, safety and security.
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