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Standard

AVIONICS REFRIGERATION COOLING SYSTEM

2017-10-27
CURRENT
ARINC728
This standard provides standards for the in accordance with which aircraft operators and manufacturers can order avionics refrigeration units and can design installations for an ARCS.
Standard

AVIONICS APPLICATION SOFTWARE STANDARD INTERFACE PART 4-SUBSET SERVICES

2012-06-28
CURRENT
ARINC653P4
ARINC Specification 653 Part 4 was prepared to support controllers and relatively simple avionics. Part 4 is true subset of services specified in ARINC 653 Part 1. In the Subset Services, partition scheduling is restricted to only one partition time window within the partition's period. This simplifies the management of process release points. Process management uses a dual-process model with at most two processes within a partition, for example, foreground and background.
Standard

CONSIDERATIONS FOR AVIONICS NETWORK DESIGN

1995-10-09
CURRENT
ARINC428
This standard provides the framework for developing a set of requirements for an avionics data bus network. This standard is intended to provide system-level considerations for the development of such a network, which may include a mix of standard data buses and private data buses.
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

CNS/ATM AVIONICS, FUNCTIONAL ALLOCATION AND RECOMMENDED ARCHITECTURES

1995-12-15
CURRENT
ARINC660
Defines a set of standard aircraft avionics architectures that support a cost-effective evolution to the fully operational CNS/ATM environment. These architectures are intended to meet near-term requirements (e.g., FANS-1, SCAT-1, etc.) and provide growth for supporting the full CNS/ATM function set. This standard represents broad airline consensus for developing avionics equipment providing CNS/ATM operating capabilities.
Standard

CNS/ATM AVIONICS, FUNCTIONAL ALLOCATION AND RECOMMENDED ARCHITECTURES

2001-01-15
CURRENT
ARINC660A
This standard expands ARINC 660 to include industry-defined architectures for the CNS/ATM operating environment. These architectures are intended to meet long-term requirements (e.g., ADS-B, CPDLC, etc.) and provide growth for the future. Airlines support the implementation of these architectures for the long-term. This standard represents broad airline consensus for developing avionics equipment providing CNS/ATM operating capabilities.
Standard

CNS/ATM AVIONICS ARCHITECTURES SUPPORTING NEXTGEN/SESAR CONCEPTS

2014-01-10
CURRENT
ARINC660B
This document identifies and describes the aircraft avionics capability necessary for operation in the evolving Communications Navigation Surveillance/Air Traffic Management (CNS/ATM) environment expected for the FAA NextGen program, Single European Sky ATM Research (SESAR) program and considerations of the Japan Collaborative Actions for Renovation of Air Traffic Systems (CARATS). These capabilities are intended to satisfy the industry's long-term CNS/ATM operational objectives.
Standard

AVIONICS APPLICATION SOFTWARE STANDARD INTERFACE PART 3A CONFORMITY TEST SPECIFICATIONS FOR ARINC 653 REQUIRED SERVICES

2018-09-07
CURRENT
ARINC653P3A-1
ARINC 653, Part 3A is the Compliance Test Specification for ARINC 653 Required Services presently defined in ARINC 653 Part 1. 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 1.
Standard

AVIONICS APPLICATION SOFTWARE STANDARD INTERFACE PART 5 CORE SOFTWARE RECOMMENDED CAPABILITIES

2014-12-01
CURRENT
ARINC653P5
The objective of this part is to define additional ARINC 653 core software capabilities to ease integration on a variety of Integrated Modular Avionics (IMA) hardware platforms by allowing platform suppliers to extend and customize it for use with their unique hardware platform. The objective of Part 5 is to define additional recommended capabilities when implementing ARINC 653 core software using a Commercial off the Shelf (COTS) ARINC 653 Operating System (O/S).
Standard

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

2018-09-07
CURRENT
ARINC653P3B
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

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.
Standard

AIR TRANSPORT AVIONICS EQUIPMENT INTERFACES

2017-07-11
CURRENT
ARINC600-20
ARINC 600 is a mechanical packaging standard that is used with the ARINC 700-series of digital avionics equipment. It provides mechanical, electrical, and environmental interfaces between LRUs and the racks or cabinets in which they are installed. Provides connector shell definition, connector insert layout and mounting dimensions.
Standard

STANDARD FIRMWARE LOADER FOR AVIONICS SHOPS

1989-09-30
CURRENT
ARINC614
This standard describes the characteristics of a standard firmware loader for avionic shops. It is capable of copying digital information into memory devices installed in circuit card assemblies, Line Replaceable Modules (LRMs) and On-Board Replaceable Modules (OBRMs). It contains the recommendations of the air transport community concerning the design and development of firmware loader equipment.
Standard

DESIGN GUIDANCE FOR AVIONICS TEST EQUIPMENT

1993-01-15
CURRENT
ARINC608A
This standard is a top-level guidance standard intended for the design of Automatic Test Equipment (ATE). It includes the definition of hardware and software needed for analog and digital signal testing using a Test Unit Adapter common interface. This standard describes the overall ATE system concept as well as the definition of the specific elements of those systems.
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.
Standard

GUIDANCE FOR USE OF AVIONICS EQUIPMENT AND SOFTWARE IN SIMULATORS

1999-02-15
CURRENT
ARINC610A-1
This standard preserves all of the technical concepts of ARINC 610. ARINC 610A encompasses the lessons learned since ARINC 610 was issued, provides additional information defining each simulator function and the responses required by each type, and creates guidance information relevant to Integrated Modular Avionics (IMA).
Standard

USERS GUIDE FOR ARINC 616 AVIONICS SUBSET OF ATLAS

2017-11-29
CURRENT
ARINC605
This guide has been written as an applications manual for writing avionics test specifications that conform to ARINC Specification 616. It provides advice for converting ATLAS test specifications into ATLAS test programs and implementing them on Automatic Test Equipment (ATE).This guide has been written as an applications manual for writing avionics test specifications that conform to ARINC Specification 616. It provides advice for converting ATLAS test specifications into ATLAS test programs and implementing them on Automatic Test Equipment (ATE).
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