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Standard

3GCN - SEAT DISTRIBUTION SYSTEM
2014-08-15
CURRENT
ARINC809-3
This specification defines general architectural philosophy and specific design guidance for the proper installation and interface of various cabin equipment within the seats. Consistency with this specification allows each component installed on the seat to operate in concert when integrated with other relevant cabin type equipment. Standard electrical and mechanical interfaces of the In- Flight Entertainment System (IFES) equipment for the 3rd Generation Cabin Network (3GCN) associated with the seat are defined. This equipment consists of the headphone jacks (HPJ), passenger control unit (PCU)/multi function handset (including the cord), seat video display (SVD), remote data outlet (RDO), integrated seat box (ISB) which includes the seat power box (SPB)/seat data box (SDB), remote power outlet (RPO), and in-seat cables. Appropriate definitions are also provided for other electrical devices associated with the seat control/position mechanism.
Standard

ACARS PROTOCOLS FOR AVIONIC END SYSTEMS
2017-11-29
CURRENT
ARINC619-5
The purpose of this document is to delineate, in an organized fashion, the protocols used by Aircraft Communication Addressing and Reporting System (ACARS) Management Units (MU) defined in ARINC Characteristic 724B and Communications Management Unit (CMU) defined in ARINC Characteristic 758, in their interactions with other onboard avionics equipment. The purpose of this document is to delineate, in an organized fashion, the protocols used by Aircraft Communication Addressing and Reporting System (ACARS) Management Units (MU) defined in ARINC Characteristic 724B and Communications Management Unit (CMU) defined in ARINC Characteristic 758, in their interactions with other onboard avionics equipment.
Standard

ADVANCED FLIGHT MANAGEMENT COMPUTER SYSTEM
2014-12-15
CURRENT
ARINC702A-4
The Advanced FMCS provides expanded functions beyond that defined in ARINC 702 to support the anticipated requirements for operation in the CNS/ATM operating environment. GNSS and RNP based navigation, air-to-ground data link for communications and surveillance, and the associated crew interface control/display definitions are included.
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

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

AIR TRANSPORT INDICATOR CASES AND MOUNTING
1976-12-15
CURRENT
ARINC408A
This standard defines mechanical dimensions and thermal standards for aircraft indicators and displays. Thermal interface data is included for indicators and their operating environment. These indicators may be stand alone or part of larger integrated display system. This standard defines mechanical dimensions and thermal standards for aircraft indicators and displays. Thermal interface data is included for indicators and their operating environment. These indicators may be stand alone or part of larger integrated display 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 GLOBAL POSITIONING SYSTEM RECEIVER
1990-03-01
CURRENT
ARINC743
This standard provides design guidance for the development of GPS sensors for airline use. It describes the operational capability of the GPS receiver and the standards necessary to ensure interchangeability. GPS provides navigation data to pilots and provides data for use by other aircraft systems.
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

AIRBORNE VOR RECEIVER
1989-08-01
CURRENT
ARINC579-2
This standard sets the basic requirements for a VOR receiver, whose function is to receive and process VOR signals in the frequency band 108.00 to 117.95 MHz. Provides traditional analog outputs and a digital output of omni bearing.
Standard

AIRBORNE WEATHER RADAR
1991-11-15
CURRENT
ARINC708-6
This standard defines the characteristics of WXR equipment intended for installation in commercial transport aircraft. The primary purpose is weather detection, ranging and analysis. Its secondary purpose is ground mapping to facilitate navigation by display of significant land contours.
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)
2020-07-21
CURRENT
ARINC834-8
This document defines an Aircraft Data Interface Function (ADIF) developed for aircraft installations that incorporate network components based on commercially available technologies. This document defines a set of protocols and services for the exchange of aircraft avionics data across aircraft networks. A common set of services that may be used to access specific avionics parameters are described. 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). Supplement 8 includes improvements in the Aviation Data Broadcast Protocol (ADBP), adds support for the Media Independent Aircraft Messaging (MIAM) protocol, and contains data security enhancements. It also includes notification and deprecation of the Generic Aircraft Parameter Service (GAPS) protocol that will be deleted in a future supplement.
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.
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