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AERONAUTICAL MOBILE AIRPORT COMMUNICATION SYSTEM (AEROMACS) TRANSCEIVER AND AIRCRAFT INSTALLATION STANDARDS

2017-07-07
CURRENT
ARINC766
This documents defines the Installation Characteristics of an airborne radio transceiver capable of broadband wireless communication with an Airport Surface Network. The Aeronautical Mobile Airport Communications System (AeroMACS) Radio Unit (ARU) will operate in the aeronautical protected frequency of 5091 MHz to 5150 MHz, utilizing the IEEE 802.16e WiMAX protocol. It is intended to offload some of the congested narrowband VHF airport traffic used for ATS and AOC communications. ARU and Antenna Form, Fit, Function and Interfaces are described.
Standard

AIR DATA AND INERTIAL REFERENCE SYSTEM (ADIRS)

2001-07-31
CURRENT
ARINC738A-1
This standard sets forth characteristics for a 4 MCU integrated digital ADIRS intended for installation in subsonic commercial transport aircraft. It is envisioned that the ADIRS will incorporate the capabilities of both an air data system and an inertial reference system.
Standard

AIRBORNE ADF SYSTEM

1992-07-15
CURRENT
ARINC712-7
This standard sets forth characteristics of an ADF system for installation in commercial transport aircraft. Function is to receive and process signals from non-directional range and other transmitters in the frequency band 190 kHz to 1750 kHz, to provide serial digital outputs of bearing, and to provide aural identification of the selected station.
Standard

AIRBORNE COMPUTER DATA LOADER

1985-11-15
CURRENT
ARINC603-1
This standard describes the desired characteristics of a data loader intended for use with airborne computers installed on commercial transport aircraft. The data loader transfers data from a tape cartridge to an avionics computer via an ARINC 429 data bus.
Standard

AIRBORNE HF/SSB SYSTEM

1984-07-06
CURRENT
ARINC719-5
This standard sets forth characteristics of a new-generation HF/SSB System intended for installation in all types of commercial transport aircraft. Covers requirements for airborne transmitter-receiver equipment capable of transmitting and receiving HF radio intelligence.
Standard

AIRBORNE PASSENGER ADDRESS AMPLIFIER

1984-07-06
CURRENT
ARINC715-3
This standard describes the characteristics of a PA AMP designed for installation in commercial aircraft. Its function is to amplify control voice, music and internally generated chime audio signals to drive the aircraft cabin loudspeaker system.
Standard

AIRCRAFT AUTONOMOUS DISTRESS TRACKING (ADT)

2019-08-26
CURRENT
ARINC680
This document describes the technical requirements, architectural options, and recommended interface standards to support an Autonomous Distress Tracking (ADT) System intended to meet global regulatory requirements for locating aircraft in distress situations and after an accident. This document is prepared in response to International Civil Aviation Organization (ICAO) and individual Civil Aviation Authorities (CAAs) initiatives.
Standard

AIRCRAFT COMMUNICATIONS ADDRESSING AND REPORTING SYSTEM (ACARS)

2012-02-24
CURRENT
ARINC724B-6
This standard describes the 724B version of the airborne components of ACARS, and is intended for use in conjunction with VHF radio equipment existing on the plane. This ACARS enhancement improves the ability of the system to provide air-to-ground and ground-to-air data communications.
Standard

AIRCRAFT DATA INTERFACE FUNCTION (ADIF)

2017-08-09
CURRENT
ARINC834-7
This document defines an Aircraft Data Interface Function (ADIF) developed for aircraft installations that incorporate network components that are based on commercially available technologies. This document defines a set of protocols and services for the exchange of aircraft avionics data across aircraft networks. The goal is to provide a common set of services that may be used to access specific avionics parameters. The ADIF may be implemented as a generic network service, or it may be implemented as a dedicated service within an ARINC 759 Aircraft Interface Devices (AID) such as those used with an Electronic Flight Bag (EFB).
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 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 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 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.
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 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 1, SYSTEMS CONCEPTS AND OVERVIEW

2019-06-20
CURRENT
ARINC664P1-2
The purpose of this document is to provide an overview of data networking standards recommended for use in commercial aircraft installations. These standards provide a means to adapt commercially defined networking standards to an aircraft environment. It refers to devices such as bridges, switches, routers and hubs and their use in an aircraft environment. This equipment, when installed in a network topology, can optimize data transfer and overall avionics performance.
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 INTERFACE DEVICE (AID)

2014-07-15
CURRENT
ARINC759
This document sets forth the characteristics of an Aircraft Interface Device (AID) intended for installation in commercial aircraft. The intent of the document is to provide general and specific design guidance for the development of an AID for use in retrofit applications associated with aircraft typically developed between the mid-1970s through the 1990s, that primarily utilize ARINC 700 series avionics, and that interface with the aircraft via ARINC 429 and ARINC 717 unidirectional buses and Hi/Lo discrete signals. This document describes the desired operational capability of the AID and the standards necessary to ensure interchangeability.
Standard

AIRCRAFT NETWORK SERVER SYSTEM (NSS) FUNCTIONAL DEFINITION

2008-12-09
CURRENT
ARINC821
This document describes a collection of Aircraft Network Services (ANS) and Network Server System (NSS) functions that are suitable for installation in all types of aircraft. It defines network services intended for both aircraft and cabin installations that will manage and maintain the NSS in a common way. This document describes methods for the aircraft to effectively communicate with ground-based information management systems.
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