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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

DATALINK GROUND SYSTEMS STANDARD AND INTERFACE SPECIFICATION (DGSS/IS)

2017-12-21
CURRENT
ARINC620-9
ARINC Specification 620 defines the aircraft interfaces to the ACARS ground system operated by a Datalink Service Provider (DSP). It also defines the interface between the DSP and other ground-based datalink services. The datalink ground system standard definition supports traditional ACARS protocols as well as Media Independent Aircraft Messaging (MIAM) as defined by ARINC Specification 841. MIAM messages can be much larger than ACARS messages (5 MB versus 3.3 kB per message). Supplement 9 includes methods to optimize the routing of MIAM messages. It adds ACARS Labels and Identifiers in support of Onboard Network System (ONS), Runway State Assessment, Aircraft Tracking for AOC Position Reporting, ATS Wind Services and Fight-deck based Interval Management System (FIMS) applications. It provides Media Advisory Codes for Broadband Systems (i.e., AeroMACS, Inmarsat SwiftBroadband (SBB) Satcom, and Iridium NEXT/Certus Satcom).
Standard

INTERNET PROTOCOL SUITE (IPS) FOR AERONAUTICAL SAFETY SERVICES ROADMAP DOCUMENT

2017-12-18
CURRENT
ARINC658
ARINC 658 was prepared to recognize the expanding role of data communication technology and the evolutionary path forward starting from ACARS protocols, to ATN/OSI protocols, and eventually ATN/IPS protocols using highly secure networks. The ATN/IPS network will be implemented onboard an aircraft and in the ground infrastructure to support safety services, including Air Traffic Services (ATS) and Aeronautical Operational Control (AOC). As such it provides a so-called “roadmap” for the development of the aviation standards for ATN/IPS services. ATN/IPS standards will evolve in coming years and be coordinated with other international standards organizations such as ICAO, EUROCAE and RTCA.
Standard

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

MARK 1 AVIATION KU-BAND AND KA-BAND SATELLITE COMMUNICATION SYSTEM PART 1 PHYSICAL INSTALLATION AND AIRCRAFT INTERFACES

2014-08-29
CURRENT
ARINC791P1-2
This standard sets forth the desired characteristics of Aviation Ku-band Satellite Communication (Satcom) and Ka-band Satcom Systems intended for installation in all types of commercial air transport aircraft. The intent of this characteristic is to provide guidance on the interfaces, form, fit, and function of the systems. This document also describes the desired operational capability of the equipment needed to provide a broadband transport link that can be used for data, video, and voice communications typically used for passenger communications and/or entertainment. The systems described in this characteristic are not qualified, at this writing, for aviation safety functions.
Standard

MARK I AVIATION KU-BAND AND KA-BAND SATELLITE COMMUNICATION SYSTEM PART 2 ELECTRICAL INTERFACES AND FUNCTIONAL EQUIPMENT DESCRIPTION

2014-07-28
CURRENT
ARINC791P2-1
This document provides the interface definition of the Satcom system. Any signal crossing into or out of the communication system is documented to ease aircraft integration. Signals within the ARINC 791 Satcom system, and in particular, between the Modman and the Antenna Subsystem, are described to permit interchangeability between any Modman and any Antenna Subsystem.
Standard

AOC AIR-GROUND DATA AND MESSAGE EXCHANGE FORMAT

2012-11-28
CURRENT
ARINC633-2
This document defines the exchange of Aeronautical Operational Control (AOC) message formats used for air-to-ground communication and ground-to-ground communication. ARINC Specification 633 simplifies the integration of AOC software from different suppliers, intended for use by different airlines, on different aircraft types. It is expected that AOC applications will be hosted on an Electronic Flight Bags (EFB). Supplement 2 includes an extensive updates to the Flight Plan schema per ICAO Flight Plan 2012. New XML schemas are added to define AOC messages for airport weather, air traffic information services (ATIS), crew list, passenger list, notice to airmen, pilot report, and hazard advisory.
Standard

AVIATION SATELLITE COMMUNICATION SYSTEM PART 2 SYSTEM DESIGN AND EQUIPMENT FUNCTIONAL DESCRIPTION

2012-06-27
CURRENT
ARINC741P2-11
This document describes the desired operational capability of the equipment as configured with the first generation Satellite Data Unit (SDU) to provide data and voice communications, as well as additional standards necessary to ensure interchangeability. Supplement 11 adds commentary on the commonality of physical interfaces between ARINC 741 systems defined for SwiftBroadband safety services and ARINC 741 systems defined only for the Inmarsat Classic Aero safety services. It adds the SwiftBroadband safety services to the SDU functional definition.
Standard

AVIATION SATELLITE COMMUNICATION SYSTEM PART 1 AIRCRAFT INSTALLATION PROVISIONS

2012-06-26
CURRENT
ARINC741P1-14
This document defines the characteristics of first generation L-band satellite communication system installations including the avionics equipment. This document provides traditional form, fit, function, and interface standards for the installation of Satcom equipment for use in all types of aircraft. It defines the satellite data unit in a 6 MCU form factor. It also provides a summary description of each avionics component that would comply with this document. Supplement 14 adds references to ARINC Characteristic 781 and address equipment configurations and functionality associated with SwiftBroadband services.
Standard

SECOND GENERATION AVIATION SATELLITE COMMUNICATION SYSTEM, AIRCRAFT INSTALLATION PROVISIONS

2012-06-21
CURRENT
ARINC761-5
This document defines the characteristics of second generation L-band satellite communication system installations including the avionics equipment defined for Iridium and Inmarsat 2G services. This document provides traditional form, fit, function, and interface standards necessary for the installation of Satcom avionics equipment for all types of aircraft. It also provides a description of each envisioned avionics component that would comply with this Characteristic. Supplement 5 removes obsolete service and system provisions, and adds references to ARINC Characteristic 791 for Ku-band antenna installation details.
Standard

CABIN COMMUNICATION SYSTEMS (CCS)

2010-11-19
CURRENT
ARINC746-6
This document provides general and specific design guidance for the development, installation, and desired operational capability of Cabin Communications Systems, including satellite communications, air-to-ground communications, and gatelink. Supplement 6 incorporates guidance for protection of personal information using methods consistent with the Payment Card Industry (PCI) Data Security Standard (DSS). The CCS characteristic provides encryption approaches for payment card information and suggestions for key management.
Standard

AOC AIR-GROUND DATA AND MESSAGE EXCHANGE FORMAT

2010-03-12
CURRENT
ARINC633-1
The purpose of this specification is to support the exchange of certain Aeronautical Operational Control (AOC) air-ground and ground-ground messages. These messages are defined in this specification, apart from those defined in ARINC Specification 620, because they have unique qualities. Like the messages defined in ARINC Specification 620, their usage necessitates a single definition.
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

HF DATA LINK SYSTEM

2001-02-16
CURRENT
ARINC753-3
The characteristics of a High Frequency Data Link (HFDL) communications system are defined by this standard. It defines avionic system components and the associated HF ground system. ARINC 634 and ARINC 635 are companion standards.
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