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AVIATION SATELLITE COMMUNICATION SYSTEMS PART 1 AIRCRAFT INSTALLATION PROVISIONS

2019-12-23
CURRENT
ARINC741P1-15
This ARINC Standard defines the installation characteristics of first generation L-band satellite communication systems. It provides the traditional form, fit, function, and interfaces for the installation of satcom equipment for use in all types of aircraft. Description of avionics equipment (e.g., Satellite Data Unit (SDU), Antennas, etc.) are included. Supplement 15 adds references to new Diplexer/Low Noise Amplifiers (DLNAs) defined in Supplement 8 to ARINC Characteristic 781: Mark 3 Aviation Satellite Communication Systems. The five new DLNAs are intended to protect Inmarsat Classic Aero and SwiftBroadband (SBB) satcom equipment from ground-based cellular sources, such as cellular Long Term Evolution (LTE) and Ancillary Terrestrial Component (ATCt). The DLNAs are categorized by desired features and service (e.g., new DLNA versus drop-in replacement, LTE and/or ATCt protection, Classic Aero and/or SBB service).
Standard

GUIDANCE FOR TOOL AND TEST EQUIPMENT (TTE) EQUIVALENCY

1996-03-01
CURRENT
ARINC732-1
This standard defines an airborne tape reproducer for passenger entertainment. The function of this equipment is to play pre-recorded tapes to the passengers through the airplane passenger entertainment system. Some channels may be used for boarding music through the public address system.
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

ANALOG AND DISCRETE DATA CONVERTER SYSTEM

1981-09-10
CURRENT
ARINC729-1
This standard sets forth the characteristics of an ADDCS designed for installation in commercial transport aircraft. The ADDCS is intended to process, convert and multiplex analog and discrete signals in order to provide them in digital format described in ARINC 429.
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

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

MARK 4 AIR TRAFFIC CONTROL TRANSPONDER (ATCRBS/MODE S)

2011-11-15
CURRENT
ARINC718A-4
Mark 4 Air Traffic Control Transponder (ATCRBS/MODE S) describes an Air Traffic Control Radar Beacon System/Mode Select (ATCRBS/Mode S) airborne transponder with Extended Interface Functions (EIF). The ATC surveillance system is made up of airborne transponders and ground interrogator-receivers, processing equipment, and antenna systems. Mode S is a cooperative surveillance system for air traffic control with ancillary communications capabilities. ARINC 718A supports elementary surveillance. Provisional enhanced surveillance functionality is also defined as a customer option. The Mark 4 transponder, like its predecessor, will support TCAS functions.
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

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

SECOND GENERATION AVIATION SATELLITE COMMUNICATION SYSTEMS, AIRCRAFT INSTALLATION PROVISIONS

2019-12-23
CURRENT
ARINC761-6
This ARINC Standard defines the installation characteristics of second generation L-band satellite communication systems. It provides the traditional form, fit, function, and interfaces for the installation of satcom equipment for use in all types of aircraft. Description of avionics equipment (e.g., Satellite Data Unit (SDU), Antennas, etc.) are included. Supplement 6 adds references to new Diplexer/Low Noise Amplifiers (DLNAs) defined in Supplement 8 to ARINC Characteristic 781: Mark 3 Aviation Satellite Communication Systems. The five new DLNAs are intended to protect Inmarsat Classic Aero and SwiftBroadband (SBB) satcom equipment from ground-based cellular sources, such as cellular Long Term Evolution (LTE) and Ancillary Terrestrial Component (ATCt). The DLNAs are categorized by desired features and service (e.g., new DLNA versus drop-in replacement, LTE and/or ATCt protection, Classic Aero and/or SBB service).
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

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

TERRESTRIAL FLIGHT TELEPHONE SYSTEM (TFTS) AIRBORNE RADIO SUBSYSTEM

1995-12-11
CURRENT
ARINC752-1
This standard defines the characteristics of a full-duplex telephone service for Aeronautical Passenger Communications through a network of ground stations. The frequency bands of 1670-1675 MHz are used to receive and 1800-1805 MHz are used to transmit.
Standard

GUIDANCE FOR THE DESIGN AND INSTALLATION OF FUEL QUANTITY SYSTEMS

1999-01-25
CURRENT
ARINC611-1
This standard defines accuracy and reliability targets for fuel quantity measuring systems installed on commercial aircraft. It describes fuel quantity system components and design techniques that will contribute to safe and reliable operation. System design goals and installation practices are described. A report of a worldwide fuel survey is included.
Standard

AIRBORNE WEATHER RADAR WITH FORWARD LOOKING WINDSHEAR DETECTION CAPABILITY

1999-11-15
CURRENT
ARINC708A-3
This standard defines an airborne pulse Doppler weather radar system for weather detection and ranging. It expands the capabilities of the ARINC 708 system through the inclusion of forward looking windshear prediction. It also provides ground-mapping capabilities to facilitate navigation by display of significant land contours.
Standard

MARK 3 AIRBORNE SELCAL SYSTEM

1990-08-15
CURRENT
ARINC714-6
Ground-to-air selective calling system characteristics are defined by this standard. The system allows selective calling of individual aircraft over radio communications circuits linking the ground station to the aircraft. Elements comprising overall system are ground selecting calling unit (coder), ground-to-air transmitter (HF or VHF), airborne receiver (HF or VHF), airborne selective calling unit (decoder), and code selection panel.
Standard

RADIO ALTIMETER

2009-04-06
CURRENT
ARINC707-7
This standard provides the desired characteristics of a RALT intended for installation in all types of commercial transport aircraft. Its primary function is to determine the aircraft's height above terrain for visual display to the pilot (essentially ground level to 2500 feet), and for use by the AFCS during automatically controlled approaches and landings.
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

GUIDANCE FOR DESIGN AND INTEGATION AND AIRCRAFT AVIONICS EQUIPMENT IN SIMULATORS

1992-02-01
CURRENT
ARINC610-1
This standard sets forth general philosophy and design guidance for using aircraft avionics equipment in simulators. Its goal is to improve simulator training by providing a better understanding among avionics designers, simulator designers, airframe manufacturers and airline simulator users in the use of aircraft avionic equipment in flight simulators. Full flight simulator, cockpit procedure trainer, cockpit system simulator or fixed base simulator, part task trainer (e.g., flight management system trainer), and maintenance training simulator guidance is included.
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