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Standard

LOGICAL SOFTWARE PART PACKAGING FOR TRANSPORT

2020-11-16
CURRENT
ARINC641-1
The purpose of this standard is to provide a method for packaging aircraft software parts for distribution using contemporary media or by electronic distribution. This project intends to standardize and provide guidance for the storage of floppy based software, currently packaged in media set parts. This standard format can be then stored or distributed on a single physical media member (CD-ROM), or by electronic crate. The obsolescence of floppy disks drive an urgent need for this guidance.
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

MEDIA INDEPENDENT SECURE OFFBOARD NETWORK

2020-06-19
CURRENT
ARINC848
ARINC Specification 848 is a functional standard based on a protocol specification profile for a secured network interface. The purpose is to define a common method of initiating a mutually authenticated tunnel between an aircraft service and its Enterprise service. ARINC Specification 848 defines a standard implementation for securing the communications between an onboard Local Area Network (LAN) and an Enterprise LAN on the ground. Various aircraft network architectures and various air to ground communication channels (aka media) are accommodated in this document. For example, L-band Satellite Communication (Satcom), Ku/Ka-band Satcom, Gatelink Cellular, and Gatelink are considered.
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 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

MARK 2 NETWORK SERVER SYSTEM (NSS) FORM AND FIT DEFINITION

2008-12-09
CURRENT
ARINC763A
This document defines both wired and wireless NSS components that enable the creation of airborne networks 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.
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

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

FULL-FORMAT PRINTER

1990-12-30
CURRENT
ARINC744
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.
Standard

FULL-FORMAT PRINTER WITH GRAPHICS CAPABILITY

1994-03-01
CURRENT
ARINC744A-1
This standard sets forth the characteristics of a full-format printer capable of printing high resolution 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.
Standard

AUTOMATIC DEPENDENT SURVEILLANCE (ADS)

1993-06-30
CURRENT
ARINC745-2
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.
Standard

GATE-AIRCRAFT TERMINAL ENVIRONMENT LINK (GATELINK)-AIRCRAFT SIDE

1994-01-01
CURRENT
ARINC751
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.
Standard

CABIN COMMUNICATION SYSTEMS (CCS)

2010-11-19
CURRENT
ARINC746-6
This document provides general and specific design guidance for the development, installation, and desired 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.
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

SPECIFICATION CONNECTORS, RACK AND PANEL, RECTANGULA REAR RELEASE CRIMP CONTACTS

2015-06-01
CURRENT
ARINC404B-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

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

AIRCRAFT SOFTWARE COMMON CONFIGURATION REPORTING

2015-07-31
CURRENT
ARINC843
This standard defines a common configuration report format that can be retrieved from an aircraft for use by ground tools and maintenance personnel. Reports will be generated in Extensible Markup Language (XML) format and structured as defined by this document. Several optional elements and attributes are defined to allow flexibility for a given report. This standard provides aircraft manufacturers, regulatory agencies, and airlines a format standard for aircraft configuration reporting, and facilitates automated comparison of configuration data reports (e.g., authorized versus as flying, etc.).
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