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Standard

Specification Connectors, Rack and Panel, Rectangular Rear Release Crimp Contacts

2015-06-30
WIP
ARIS40B-2
This document defines standardized connectors intended for use on rack-mountable avionics equipment. It is aligned to the latest version of MIL-C-81659. Supplement 2 was updated to support cabin equipment applications. It corrects intermateability control dimensions that are provided for single shell plug connectors.
Standard

AVIONICS APPLICATION SOFTWARE STANDARD INTERFACE PART 3B CONFORMITY TEST SPECIFICATIONS FOR ARINC 653 EXTENDED SERVICES

2018-09-07
CURRENT
ARIS653P3B
ARINC 653, Part 3B is the Compliance Test Specification for ARINC 653 Extended Services presently defined in ARINC 653 Part 2. The document specifies a set of stimuli and the expected responses. Future work on the ARINC 653 document set includes an effort to define Operating System services for multi-core processor environments. The Compliance Test Specification is expected to be updated in step with ARINC 653, Part 2.
Standard

NAVIGATION SYSTEM DATABASE

2018-07-23
CURRENT
ARIS424-22
This standard provides a data base comprising standards used for the preparation of a navigation system data base. This data may be used with the operational flight software in a wide range of navigational equipment.
Standard

FIBER OPTIC CABLES

2018-08-27
CURRENT
ARIS802-3
This specification covers the performance requirements, dimensions, quality assurance criteria, test procedures, and cable codification for fiber optic cables suitable for use on commercial aircraft.
Standard

FIBER OPTIC FERRULE MECHANICAL TRANSFER

2018-08-06
CURRENT
ARIS846
This specification covers the dimensions, performance, and quality assurance criteria for fiber optic MT contacts, including performance test requirements and procedures, suitable for use on commercial aircraft.
Standard

GENERAL STANDARDIZATION OF CAN (CONTROLLER AREA NETWORK) BUS PROTOCOL FOR AIRBORNE USE

2018-09-25
CURRENT
ARIS825-4
This document defines a Controller Area Network (CAN) interface for current and future commercial aircraft applications. The latest version, Supplement 4, expands the document to include CAN Flexible Data rate also known as CAN FD. CAN FD has the potential to provide 4 Mbps of data transfer. Supplement 4 also introduces four new appendices on the topics of: ARINC 825 Compliance, Configuration of Bit Timing, Management Information Base (MIB) Counters, and CAN Bus Security Considerations.
Standard

GNSS SENSOR

2018-06-22
CURRENT
ARIC743A-6
This document sets forth the characteristics of the integrated Global Positioning System (GPS)/Global 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.
Standard

ADVANCED FLIGHT MANAGEMENT COMPUTER SYSTEM

2018-08-28
CURRENT
ARIC702A-5
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. The NextGen/SESAR concepts and their relative effects on the FMS are addressed in this document. The functional requirements also apply to a Flight Management Function (FMF) in an Integrated Modular Avionics (IMA) architecture with software partitions.
Standard

GNSS LANDING SYSTEM SENSOR UNIT (GLSSU) WITH VHF DATA BROADCAST (VDB) RECEIVER

2018-06-22
CURRENT
ARIC743C
This document sets forth the characteristics of the Global Navigation Satellite System (GNSS) Landing 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.
Standard

GNSS LANDING SYSTEM SENSOR UNIT (GLSSU)

2018-06-22
CURRENT
ARIC743B-1
This document sets forth the characteristics of the GNSS Landing System Sensor Unit (GLSSU) intended 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.
Standard

LOW-EARTH ORBITING AVIATION SATELLITE COMMUNICATION SYSTEMS

2018-10-01
CURRENT
ARIC771-1
This document sets forth the desired characteristics of the Iridium Low-Earth Orbiting (LEO) Aviation 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.
Standard

MULTI-MODE RECEIVER (MMR) - DIGITAL

2018-01-25
CURRENT
ARIC755-5
ARINC Characteristic 755 defines a multi-mode receiver capable of providing flight path deviation guidance (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.
Standard

CABIN EQUIPMENT INTERFACES PART 9 CABIN INTERFACE NETWORK (CIN)

2017-12-29
CURRENT
ARIS628P9-5
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

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

2011-11-15
CURRENT
ARIC718A-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

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

2017-12-18
CURRENT
ARIR658
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

HF DATA LINK SYSTEM

2001-02-16
CURRENT
ARIC753-3
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.
Standard

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

2017-12-21
CURRENT
ARIS620-9
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

AOC AIR-GROUND DATA AND MESSAGE EXCHANGE FORMAT

2010-03-12
CURRENT
ARIS633-1
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

AOC AIR-GROUND DATA AND MESSAGE EXCHANGE FORMAT

2012-11-28
CURRENT
ARIS633-2
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.
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