ARINC Standards Store
ARINC Standards - 700 Series
700 Series ARINC Characteristics define digital systems and equipment installed on current-model production aircraft. They include definitions of form, fit, function, and interface for Line Replaceable Units (LRUs) in a federated architecture.
701-1
Last Published:
April 1983
701-1 Flight Control Computer System (FCCS)
This standard sets forth the characteristics of a FCCS within an Automatic Flight System. The FCCS i...s intended to provide autoland capability for commercial aircraft. The document provides design guidance for the development and installation of a FCCS.
702-6
Last Published:
June 1994
702-6 Flight Management Computer System (FMCS)
This standard defines a FMCS for installation in commercial transport aircraft. The FMCS provides pe...rformance data, performance computations, fuel management functions, and navigation and guidance to a desired flight plan.
702A-5
Last Published:
August 2018
702A-5 Advanced Flight Management Computer System
The Advanced FMCS provides expanded functions beyond that defined in ARINC 702 to support the ant...icipated 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.
703-2
Last Published:
October 1983
703-2 Thrust Control Computer System (TCCS)
The characteristics of a TCCS within the Automatic Flight System are defined in this standard for th...rottle control. The standard also provides general and specific design guidance for the development and installation of a TCCS.
704-7
Last Published:
March 1999
704-7 Inertial Reference System (IRS)
IRS characteristics are defined in this standard. It defines the desired performance of inertial mea...suring devices and associated electronics specifically designed for installation in commercial transport aircraft. This system provides the basic outputs for aircraft angular rate and acceleration, and computed outputs of altitude, true heading, velocity and present position in a 10 MCU form factor.
704A
Last Published:
March 1999
704A Inertial Reference System (IRS)
This standard defines a 4 MCU IRS, consisting of inertial measuring devices and associated electroni...cs specifically designed for installation in commercial transport type aircraft. It may be used in place of ARINC 704 Inertial Reference Systems. This system additionally provides capability to be interfaced to an ARINC 743A GNSS Sensor, to enhance the accuracy of the inertially derived navigation data.
705-5
Last Published:
April 1985
705-5 Attitude and Heading Reference System (AHRS)
This standard describes the basic requirements for an AHRS specifically designed for installation in... commercial transport aircraft. The AHRS is an attitude and heading sensor that provides outputs in digital form for guidance and display. The AHRS replaces the traditional vertical and directional gyros.
706-4
Last Published:
January 1988
706-4 Mark 5 Subsonic Air Data System (ADS)
This standard sets forth the characteristics of a digital ADS intended for installation in subsonic ...commercial transport aircraft. Provides essential air data information for display to pilots and for use by other aircraft systems. Consists of a computer unit located in the aircraft electronics rack and suitable indicators located in the cockpit.
707-7
Last Published:
April 2009
707-7 Radio Altimeter
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.
708-6
Last Published:
November 1991
708-6 Airborne Weather Radar (WXR)
This standard defines the characteristics of WXR equipment intended for installation in commercial t...ransport 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.
708A-3
Last Published:
November 1999
708A-3 Airborne Weather Radar with Forward Looking Windshear Detection Capability
This standard defines an airborne pulse Doppler weather radar system for weather detection and rangi...ng. 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.
709-8
Last Published:
October 1988
709-8 Airborne Distance Measuring Equipment (DME)
This standard sets forth characteristics of a DME intended for installation in commercial transport ...aircraft. It provides slant range distance from an aircraft to a selected DME ground facility, which is presented to the flight crew on an indicator located in the instrument panel. Other applications include utilization of frequency scanning modes by navigation computers.
709A-1
Last Published:
August 1994
709A-1 Precision Airborne Distance Measuring Equipment (DME/P)
This standard provides general and specific design guidance for the development of a DME/P, which pr...ovides slant range distance from an aircraft to a selected DME ground facility. For landing purposes, the DME/P complements the angle MLS/ILS with precise range data.
710-10
Last Published:
November 1997
710-10 Mark 2 Airborne ILS Receiver
This standard defines the characteristics of an ILS receiver intended for installation in all types ...of commercial transport aircraft. It describes the desired operational capability of the equipment and the standards necessary to ensure interchangeability.
711-10
Last Published:
January 2002
711-10 Mark 2 Airborne VOR ILS Receiver
This standard defines characteristics of a VOR receiver for installation in commercial transport air...craft. Functions of the VOR receiver are to receive and process VHF omni-directional range signals in the frequency band 108.00 to 117.95 MHz. It provides serial digital outputs of omni-bearing, and processes marker beacon transmissions on 75 MHz for annunciation to the flight deck crew.
712-7
Last Published:
July 1992
712-7 Airborne ADF System
This standard sets forth characteristics of an ADF system for installation in commercial transport a...ircraft. 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.
714-6
Last Published:
August 1990
714-6 Mark 3 Airborne SELCAL System
Ground-to-air selective calling system characteristics are defined by this standard. The system allo...ws 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.
714A
Last Published:
November 2015
714A Mark 4 Airborne Selective Calling (SELCAL)
This document represents a significant improvement to existing Selective Calling (SELCAL) standards ...used with HF and VHF voice communications. The goal is to eliminate the possibility that two or more aircraft could respond to the same radio call. The Mark 4 SELCAL system definition provides the following: " Guidance for integrated and federated audio systems " 32 audio tones total (16+16) yielding up to 215,760 unique codes " SELCAL form, fit, & function definition " Interwiring and installation details " Defines SELCAL decoding requirements in the presence of significant signal degradation
715-3
Last Published:
July 1984
715-3 Airborne Passenger Address Amplifier (PA AMP)
This standard describes the characteristics of a PA AMP designed for installation in commercial airc...raft. Its function is to amplify control voice, music and internally generated chime audio signals to drive the aircraft cabin loudspeaker system.
716-11
Last Published:
June 2003
716-11 Airborne VHF Communications Transceiver
This standard sets forth characteristics of a VHF Communications Transceiver for installation in all... types of commercial transport aircraft. The VHF transceiver can support 8.33 kHz AM or 25 kHz AM voice or ACARS (2400 bps) data communications.
717-15
Last Published:
June 2011
717-15 Flight Data Acquisition and Recording System
This document provides design guidance for the development and installation of a Digital Expandable ...Flight Data Acquisition and Recording System (DEFDARS) primarily intended for airline use. As such, this guidance will include specific requirements necessary to accommodate mandatory flight data recording and other flight data acquisition needs plus the requirements to ensure customer controlled interchangeability of equipment in a standard aircraft installation. The system capability was expanded to accommodate a data bus speed of 1024 words per second.
718-4
Last Published:
December 1989
718-4 Mark 3 Air Traffic Control Transponder (ATCRBS/MODE S)
This document defines the Air Traffic Control Transponder (ATCRBS/Mode S) with that supports emergin...g Automatic Dependent Surveillance - Broadcast (ADS-B) requirements. Supplement 4 adds ADS-B Out capabilities and enables the Mode S Transponder to comply with Mode S Transponder MOPS (RTCA DO-181E and EUROCAE ED-73E) as entered into ICAO Annex 10 Volume IV and ICAO Doc. 9871.
718A-4
Last Published:
December 2011
718A-4 Mark 4 Air Traffic Control Transponder (ATCRBS/Mode S)
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.
719-5
Last Published:
July 1984
719-5 Airborne HF/SSB System
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.
720-1
Last Published:
July 1980
720-1 Digital Frequency/Function Selection for Airborne Electronic Equipment
This standard sets forth the air transport industry's recommended standards for a digital frequency ...selection system. This standard addresses two opposite ends of the DFS integration possibilities: a totally centralized and a federated system. This is necessary to assure that the radio interface specifications are adequate to cover a range of DFS integration.
722
Last Published:
November 1980
722 Projection Video System (PVS)
This standard sets forth design guidance and airplane interfaces for the development and installatio...n of a PVS in commercial transport aircraft. Basic function of the PVS is to display projected television images to each passenger.
723-3
Last Published:
January 1988
723-3 Ground Proximity Warning System (GPWS)
This standard sets forth the characteristics of a GPWS designed for installation in commercial aircr...aft. It aids pilots by providing audible and visible warnings or alerts when an aircraft approaches terrain more closely than, or deviates downward from an ILS glide slope beyond the limits set into the system.
724-9
Last Published:
September 1998
724-9 Mark 2 Aircraft Communications Addressing and Reporting System (ACARS)
This standard describes the "Mark 2" version of the ACARS equipment. It is intended for use in conju...nction with existing airborne radio equipment to enhance air-ground operational control communications.
724B-6
Last Published:
February 2012
724B-6 Aircraft Communications Addressing and Reporting System (ACARS)
This standard describes the 724B version of the airborne components of ACARS, and is intended for us...e 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.
725-2
Last Published:
November 1984
725-2 Electronic Flight Instruments (EFI)
This standard sets forth the features of a color EFI system for installation in commercial transport... aircraft. The EFI provides display functions that include Attitude Director Indicator (ADI), Horizontal Situation Indicator (HSI), Air Data, Map display, Weather display, Radio Altitude data, Flight Control Mode annunciation, Flight Path information, and Flight Warning display.
726-1
Last Published:
September 1981
726-1 Flight Warning Computer System (FWCS)
This standard sets forth the characteristics of a FWCS intended for use in commercial transport airc...raft. It is intended to process caution and warning inputs for visual and/or audible presentation to the flight crew.
727-1
Last Published:
August 1987
727-1 Airborne Microwave Landing System
This standard sets forth the characteristics of MLS receiver processors intended for installation in... all types of commercial transport aircraft. The function of the airborne MLS receiver processor is the reception and processing of the MLS azimuth signals, the elevation signals, and the data transmitted from the MLS ground stations.
728
Last Published:
October 1979
728 Avionics Refrigeration Cooling System (ARCS)
This standard provides standards for the in accordance with which aircraft operators and manufacture...rs can order avionics refrigeration units and can design installations for an ARCS.
729-1
Last Published:
September 1981
729-1 Analog and Discrete Data Converter System (ADDCS)
This standard sets forth the characteristics of an ADDCS designed for installation in commercial tra...nsport 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.
731-3
Last Published:
November 1998
731-3 Electronic Chronometer
This standard sets forth the characteristics for a self-contained Electronic Chronometer for install...ation in all types of commercial transport aircraft. It provides the following indications to the flight crew, Time of Day, Day and Month, Elapsed Time and Chronograph.
732-1
Last Published:
March 1996
732-1 Mark 2 Airborne Passenger Audio Entertainment Tape Reproducer
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.
735-2
Last Published:
January 1993
735-2 Traffic Alert and Collision Avoidance System (TCAS)
This standard defines as TCAS system capable of calculating the range, altitude and bearing of other... aircraft equipped with Mode S transponders. The system monitors the trajectory of these aircraft for the purpose of determining if any of them constitute a potential collision hazard.
735A-1
Last Published:
January 2003
735A-1 Mark 2 Traffic Alert and Collision Avoidance System (TCAS)
This update to the TCAS system standard introduces changes necessary to be compliant with RTCA Docum...ent DO-185A that includes TCAS software version 7.0.
735B-2
Last Published:
August 2015
735B-2 Traffic Computer TCAS and ADS-B Functionality
This document defines a Traffic Surveillance capability for NextGen and SESAR airspace environments.... Supplement 2 adds hybrid surveillance functionality. It satisfies recent updates to FAA Airworthiness Circular AC 20-151B - Airworthiness Approval of Traffic Alert and Collision Avoidance Systems (TCAS II), and Technical Standard Order TSO-119d requiring the annunciation of a hybrid surveillance failure. Supplement 2 also adds strobe program pinning, updates TCAS inputs status, improves aircraft troubleshooting, and supports recent central maintenance computer function block point updates.
737-1
Last Published:
April 1988
737-1 On-Board Weight and Balance System
This standard defines a system of sensors and monitoring equipment to determine aircraft weight whil...e it is on the ground. The system serves as an aid to the pilot for determining aircraft weight distribution and center of gravity (CG).
738-3
Last Published:
July 2001
738-3 Air Data and Inertial Reference System (ADIRS)
This standard defines an integrated ADIRS that provides air data information and directional guidanc...e information for cockpit display. The ADIRS consists of up to three Air Data/Inertial Reference Units (ADIRUs) located in the aircraft electronic rack, an associated Control and Display Unit (CDU) and remotely mounted Air Data Modules (ADMs).
738A-1
Last Published:
July 2001
738A-1 Air Data and Inertial Reference System (ADIRS)
This standard sets forth characteristics for a 4 MCU integrated digital ADIRS intended for installat...ion 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.
739-1
Last Published:
June 1990
739-1 Multi-Purpose Control and Display Unit (MCDU)
MCDU consists of an alphanumeric keyboard and display unit capable of interfacing with a number of a...ircraft systems. Dedicated keys on the MCDU provide the means for system selection with programmable soft keys. ARINC 429 interfaces are used to communicate with participating systems.
739A-1
Last Published:
December 1998
739A-1 Multi-Purpose Control and Display Unit (MCDU)
This MCDU standard consists of the original ARINC 739 definition with enhancements to allow it to be... logged on to up to two systems at one time. Alternate form factors are included to allow the MCDU to be introduced into a wide variety of airframes candidate for CNS/ATM upgrade.
740-1
Last Published:
June 1988
740-1 Multiple-Input Cockpit Printer
This standard describes the form, fit, function and interfaces of an airborne printer capable of com...municating with multiple systems one at a time. The printer contains the circuitry for acquisition, buffering and processing of coded alphanumeric messages for print-out on half-width paper.
741P1-15
Last Published:
December 2019
741P1-15 Aviation Satellite Communication System, Part 1, Aircraft Installation Provisions
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.
741P2-11
Last Published:
June 2012
741P2-11 Aviation Satellite Communication System, Part 2, System Design and Equipment Functional Description
This document describes the desired operational capability of the equipment as configured with the f...irst 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.
742
Last Published:
January 1988
742 Design Guidance for Windshear Warning and Guidance Equipment Language
This standard describes stand-alone windshear warning system comprised of a windshear warning comput...er and associated cockpit displays. The system uses data pertaining to aircraft movement with respect to air movement to detect and annunciate a windshear condition. As an option, it may also provide instrument guidance to the crew indicating optimum pitch to endure the windshear encounter.
743
Last Published:
March 1990
743 Airborne Global Positioning System Receiver
This standard provides design guidance for the development of GPS sensors for airline use. It descri...bes 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.
743A-6
Last Published:
June 2018
743A-6 GNSS Sensor
This document sets forth the characteristics of the integrated Global Positioning System (GPS)/Gl...obal Orbiting Navigation Satellite System (GLONASS) sensor unit (GNSSU) portion of a GNSS system intended for installation in commercial aircraft. The intent of this document is to provide general and specific design guidance for the development of GNSS sensors for airline use. It describes the desired operational capability of the GNSS system and the standards necessary to ensure interchangeability.
743B-1
Last Published:
June 2018
743B-1 GNSS Landing System Sensor Unit (GLSSU)
This document sets forth the characteristics of the GNSS Landing System Sensor Unit (GLSSU) inten...ded for installation in commercial aircraft. The intent of this document is to provide general and specific design guidance for the development of GLSSU for airline use. It describes the desired operational capability of the GLSSU and the standards necessary to ensure interchangeability.
743C
Last Published:
June 2018
743C GNSS Landing System Sensor Unit (GLSSU) with VHF Data Broadcast (VDB) Receiver
This document sets forth the characteristics of the Global Navigation Satellite System (GNSS) Lan...ding System Sensor Unit (GLSSU) with a built-in VHF Data Broadcast (VDB) receiver. The intent of this document is to provide general and specific design guidance for the development of GLSSU for airline use. It describes the desired operational capability of the GLSSU and the standards necessary to ensure interchangeability.
744
Last Published:
December 1990
744 Full-Format Printer
This standard sets forth the characteristics of a full-format printer capable of printing up to 132 ...characters of alphanumeric and/or semi-graphic data on 8.5 x 11 inch or A4 paper size. Participating equipment interface using ARINC 429 data buses. It is optionally capable of producing hard-copy graphics in the form of addressable dot plotting data.
744A-1
Last Published:
March 1994
744A-1 Full-Format Printer with Graphics Capability
This standard sets forth the characteristics of a full-format printer capable of printing high resol...ution alphanumeric, semi-graphic and graphic images on 8.5x11-inch or A4 size paper. The printer is intended to be compatible with ARINC 744 printers. It has two bi-directional high-speed Ethernet ports to facilitate transfer of high throughput and burst mode data.
745-2
Last Published:
June 1993
745-2 Automatic Dependent Surveillance (ADS)
This standard defines ADS system functions. It describes the ADS to ground-based application end-to-...end operation. Includes a brief overview of the entire ADS system in order to aid the reader in understanding the ADS environment.
746-6
Last Published:
November 2010
746-6 Cabin Communications Systems (CCS)
This document provides general and specific design guidance for the development, installation, and d...esired 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.
747-3
Last Published:
June 2011
747-3 Flight Data Recorder
This document provides design guidance for the development and installation of Flight Data Recorders... (FDR) which may utilize solid state memory and which may employ some means of data compression. The Flight Data Recorder will be utilized with a Flight Data Acquisition Unit (FDAU) (ARINC Characteristic 573) or a Digital Flight Data Acquisition Unit (DFDAU) (ARINC Characteristic 717) to accommodate mandatory flight data recording and other flight data acquisition needs. The document provides guidance and information to ensure customer controlled interchangeability of equipment in a standard aircraft installation and in data retrieval. The system capability was expanded to accommodate a data bus speed of 1024 words per second.
750-4
Last Published:
August 2004
750-4 VHF Data Radio
This standard specifies the form, fit and functional definitions for a VHF transceiver capable of vo...ice and data communications. The VHF transceiver supports, 8.33 kHz AM and 25 kHz AM voice, and VDL-2 (31.5 kbps) data link communications as defined by ICAO. ARINC 631 is a companion standard.
751
Last Published:
January 1994
751 Gate-Aircraft Terminal Environment Link (Gatelink) - Aircraft Side
This standard describes the electrical and optical interface definitions for Gatelink communications.... Gatelink is a 100 Mbps full-duplex communication link between a communication system inside the airport terminal (or at the maintenance position) and a communication system onboard a parked aircraft.
752-1
Last Published:
December 1995
752-1 Terrestrial Flight Telephone System (TFTS) Airborne Radio Subsystem
This standard defines the characteristics of a full-duplex telephone service for Aeronautical Passen...ger 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.
753-3
Last Published:
February 2001
753-3 HF Data Link System
The characteristics of a High Frequency Data Link (HFDL) communications system are defined by this s...tandard. It defines avionic system components and the associated HF ground system. ARINC 634 and ARINC 635 are companion standards.
755-5
Last Published:
January 2018
755-5 Multi-Mode Receiver (MMR) - Digital
ARINC Characteristic 755 defines a multi-mode receiver capable of providing flight path deviation gu...idance (corrections) to the aircraft during the approach and landing phase. The data source may be from an Instrument Landing System (ILS), a Microwave Landing System (MLS) or an GNSS Landing System (GLS).
Supplement 5 adds annunciations defined in RTCA/DO-253D – MOPS for GPS LAAS Airborne Equipment. GNSS Data and GLS Config Validity ARINC 429 Labels are also updated. The range for Selected Glide Path Angle is corrected.
756-3
Last Published:
February 2004
756-3 GNSS Navigation and Landing Unit (GNLU)
This standard describes the function of the GNLU, capable of providing enroute/terminal navigation, ...non-precision approach, and precision approach capabilities. The GNLS consists of a GNLU, associated controls and displays, antenna, and interfaces to other aircraft systems.
757-6
Last Published:
August 2015
757-6 Cockpit Voice Recorder (CVR)
This document provides guidance for the development and installation of a Cockpit Voice Recorders (C...VR) with solid-state memory. Supplement 6 provides the following: " The optional interfaces to data link services and On-Board Maintenance System (OMS) were revised to clarify that if the optional interface is implemented, then it shall be implemented in a specific way. " The power input section was revised to clarity the need for the CVR to be designed to accept 115 Vac power and 28 Vdc power from the aircraft. " The time correlation requirement was revised to specify that the CVR should receive its time signal from the same source as the Flight Data Recorder (FDR). " The OMS interface was updated to describe the correct ARINC 429 Sign Status Matrix (SSM) encoding for new CVR designs.
757A-1
Last Published:
August 2015
757A-1 Cockpit Voice Recorder (CVR)
This Characteristic provides guidance for the development and installation of a new generation of Co...ckpit Voice Recorders (CVRs) using solid-state memory. This document supersedes the earlier ARINC Characteristic 557. ARINC Characteristic 757A is intended to coexist with ARINC Characteristic 757 CVR. Supplement 1 provides the following: " The CVR unit description was updated to clarify the differences in the equipment designed to ARINC 757A versus that designed to ARINC 757, i.e., data link and OMS interfaces are required for ARINC 757A compliance. " Material was added to maintain document alignment with ARINC 757 which has FDR capability. ARINC 757A recorders are not required to have FDR capability. " The time correlation requirement was revised to specify that the CVR should receive its time signal from the same source as the Flight Data Recorder (FDR). " The OMS interface was updated to describe the correct ARINC 429 Sign Status Matrix (SSM) encoding for new CVR designs.
758-3
Last Published:
November 2010
758-3 Communications Management Unit (CMU) Mark 2
This document defines a Communications Management Unit (CMU) as an on-board message router capable o...f managing various datalink networks and services available to the aircraft. Supplement 3 was developed to support ATS/ATN datalink recording requirements. The existing simulator data bus interface was converted to a shared simulator/CVR interface.
758-4
Last Published:
November 2019
758-4 Communications Management Unit (CMU) Mark 2
This ARINC Standard specifies the ARINC 758 Mark 2 Communications Management Unit (CMU) as an on-...board message router capable of managing various datalink networks and services available to the aircraft. Supplement 4 adds Ethernet interfaces, per ARINC Specification 664 Part 2. This will allow the CMU to communicate with IP based radio transceivers (e.g., L-Band Satellite Communication Systems (Inmarsat SwiftBroadband (SBB) and Iridium Certus), ACARS over IP, AeroMACS, etc.).
759
Last Published:
July 2014
ARINC Characteristic 759: Aircraft Interface Device (AID)
This document sets forth the characteristics of an Aircraft Interface Device (AID) intended for inst...allation 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.
760-1
Last Published:
March 2000
760-1 GNSS Navigation Unit (GNU)
Characteristics desired of a GNU are defined in this standard. The GNU provides enroute/terminal nav...igation, and non-precision approach capabilities. The GNU is intended to support CNS/ATM functions available in the near term, as well as provide growth for the long-term.
761-6
Last Published:
December 2019
761-6 Second Generation Aviation Satellite Communication Systems, Aircraft Installation Provisions
This ARINC Standard defines the installation characteristics of second generation L-band satellit...e 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
762-1
Last Published:
September 2000
762-1 Terrain Awareness and Warning System (TAWS)
This standard sets forth the characteristics of a terrain awareness and warning system intended for ...installation in aircraft with digital signal interfaces. Describes the desired operational capability of the equipment, the standards necessary to ensure interchangeability, form factor, and pin assignments.
763-3
Last Published:
August 2005
763-3 Network Server System (NSS)
The network server system description includes a common file server, data processing, mass storage a...nd interface capabilities to a number of terminals connected via an onboard aircraft Local Area Network (LAN). The Network Server System is a central node through which terminals are able to communicate with avionics systems, access data and applications stored in the NSS mass memory storage.
763A
Last Published:
December 2008
763A Mark 2 Network Server System (NSS) Form and Fit Definition
This document defines both wired and wireless NSS components that enable the creation of airborne ne...tworks that are scalable, interchangeable, upgradeable, and remotely manageable with minimum cost. Aircraft equipment configurations and aircraft wiring recommendations are also described to allow aircraft network growth through the simple addition or replacement of NSS components. Hardware characteristics of standardized components are described without specifying equipment capacity or the operational functions of those components.
764
Last Published:
July 2005
764 Head-Up Display (HUD) System
This document defines a Head-Up Display (HUD) system intended for installation in all types of aircr...aft. It describes the physical form factors, fit dimensions, electrical interface definition and typical HUD functions, including the display of navigation and guidance information in the flight crew's forward field of view. The HUD accomplishes this by projecting images onto a combiner with symbology that conforms to the outside world view. Guidance for HUD architectures include single, twin, dual and HUD integrated with Primary Flight Display (PFD). This document is an practical guide for the design of federated equipment and integrated modular avionics.
765
Last Published:
December 2003
765 Ethernet Switch Unit
ARINC Characteristic 765 defines an Ethernet Switch Unit (ESU), which fits in the general architectu...ral philosophy and aircraft infrastructure for the proper use and interface of various information network related equipment. This document specifies an ESU intended for various aircraft information network related equipment. It provides a wired network connection among the connected devices based on interfaces defined by ARINC Specification 664 and IEEE 802.3 CSMA/CD (Ethernet).
766
Last Published:
July 2017
766 Aeronautical Mobile Airport Communication System (AeroMACS) Transceiver and Aircraft Installation Standards
This document defines the Installation Characteristics of an airborne radio transceiver capable of b...roadband 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.
767-1
Last Published:
May 2009
767-1 Enhanced Airborne Flight Recorder
This document is intended to provide design guidance for the development and installation of an Enha...nced Airborne Flight Recorder (EAFR). The EAFR standard addresses combinations of any or all of the following in a single Line Replaceable Unit (LRU), a Digital Flight Data Recorder (DFDR) function, a Cockpit Voice Recorder (CVR) function, a data link recording function, and an image recording function. This document does not address the overall flight data recorder system requirements but considers interface and system standards. This document does not replace ARINC Characteristic 747 which defines DFDRs. This document addresses the details of the voice recording function but does not describe the audio distribution system. It does not replace ARINC Characteristic 757 which defines CVRs. The EAFR may be used in a single or dual-redundant installation as permitted by regulation. Both configurations are addressed in this Characteristic.
768-2
Last Published:
June 2011
768-2 Integrated Surveillance System (ISS)
This document defines an Integrated Surveillance System (ISS) capable of providing traffic, terrain ...and weather information to the flight deck crew. Supplement 2 provides enhancements in the traffic surveillance area to support ADS-B Out and ADS-B In functionality, ADS-Re-broadcast capability, and Traffic Information Services Broadcast (TIS-B).
771-1
Last Published:
October 2018
771-1 Low-Earth Orbiting Aviation Satellite Communication Systems
This document sets forth the desired characteristics of the Iridium Low-Earth Orbiting (LEO) Avia...tion Satellite Communication (Satcom) System avionics intended for installation in all types of aircraft including commercial transport, business, and general aviation aircraft. The intent of this document is to provide a description of the system components, aircraft interfaces, and satellite communication functions. It also describes the desired system performance and operational capability of the equipment.
777-2
Last Published:
October 2010
777-2 Recorder Independent Power Supply (RIPS)
This Characteristic provides the definitions for the physical form and fit dimensions, the electrica...l interfaces, and the functions of an independent power supply for cockpit voice recorders or crash survivable recorders that combine voice with other recording functions. The RIPS is used to provide backup power that is independent of the aircraft generated power buses. Supplement 2 introduces a description of charge rates for alternate power sources and revises the electrical interface to accommodate monitoring of the RIPS status.
781-8
Last Published:
September 2019
781-8 Mark 3 Aviation Satellite Communication Systems
This document sets forth the desired characteristics of an aviation satellite communication (satc...om) system intended for installation in all types of commercial transport and business aircraft. The intent of this document is to provide general and specific guidance on the form factor and pin assignments for the installation of the avionics primarily for airline use. It also describes the desired operational capability of the equipment to provide data and voice communications, as well as additional standards necessary to ensure interchangeability. This Characteristic specifies equipment using Inmarsat satellites operating in L-band. Ku-band and Ka-band equipment is specified in ARINC Characteristic 791.
791P1-3
Last Published:
September 2019
791P1-3 Mark I Aviation Ku-Band and Ka-Band Satellite Communication System, Part 1, Physical Installation and Aircraft Interfaces
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.
791P2-1
Last Published:
July 2014
791P2-1 Mark I Aviation Ku-Band and Ka-Band Satellite Communication System, Part 2, Electrical Interfaces and Functional Equipment Description
This document provides the interface definition of the satcom system. Any signal crossing into or ou...t 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.
792
Last Published:
December 2018
792 Second-Generation Ku-Band and Ka-Band Satellite Communication System
This standard sets forth the desired characteristics of a second-generation aviation Ku-band and ...Ka-band satellite communication (satcom) system intended for installation in all types of aircraft.
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