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Standard

STANDARD DATA INTERFACE FOR GALLEY INSERT (GAIN) EQUIPMENT PART 1 CAN COMMUNICATIONS
2014-08-26
CURRENT
ARINC812AP1-1
The purpose of this specification is to define the general Galley Insert (GAIN)standardization philosophy, provide comprehensive equipment interfaces, and disseminate the most current industry guidance. Part 1 covers the Controller Area Network (CAN) data interface attachments, envelopes, and data content to be considered between all galley equipment using a Galley Data Bus as described within this specification. This document is intended as the successor and replacement for ARINC Specification 812. This document contains significant improvements to CAN data interfaces.
Standard

STANDARD DATA INTERFACE FOR GALLEY INSERT (GAIN) EQUIPMENT PART 1 CAN COMMUNICATIONS
2021-09-10
CURRENT
ARINC812AP1-2
The purpose of this specification is to define the general Galley Insert (GAIN)standardization philosophy, provide comprehensive equipment interfaces, and disseminate the most current industry guidance. Part 1 covers the Controller Area Network (CAN) data interface attachments, envelopes, and data content to be considered between all galley equipment using a Galley Data Bus as described within this specification. This document is intended as the successor and replacement for ARINC Specification 812. This document contains significant improvements to CAN data interfaces.
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

PRECISION AIRBORNE DISTANCE MEASURING EQUIPMENT (DME/P)
1994-08-17
CURRENT
ARINC709A-1
This standard provides general and specific design guidance for the development of a DME/P, which provides 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.
Standard

MULTI-PURPOSE CONTROL AND DISPLAY UNIT
1990-06-20
CURRENT
ARINC739-1
MCDU consists of an alphanumeric keyboard and display unit capable of interfacing with a number of aircraft 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.
Standard

MULTI-PURPOSE CONTROL AND DISPLAY UNIT
1998-12-16
CURRENT
ARINC739A-1
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.
Standard

MARK I AVIATION KU-BAND AND KA-BAND SATELLITE COMMUNICATION SYSTEM PART 2 ELECTRICAL INTERFACES AND FUNCTIONAL EQUIPMENT DESCRIPTION
2014-07-28
CURRENT
ARINC791P2-1
This document provides the interface definition of the Satcom system. Any signal crossing into or out 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.
Standard

MARK 5 AIRBORNE DISTANCE MEASURING EQUIPMENT
1988-10-31
CURRENT
ARINC709-8
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.
Standard

HEAD-UP DISPLAY (HUD) SYSTEM
2005-07-08
CURRENT
ARINC764
This document defines a Head-Up Display (HUD) system intended for installation in all types of aircraft. 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.
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

GUIDANCE FOR TOOL AND TEST EQUIPMENT (TTE) EQUIVALENCY
2015-08-01
CURRENT
ARINC735B-2
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.
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

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

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

EMBEDDED INTERCHANGE FORMAT FOR AIRPORT MAPPING DATABASE
2007-11-19
CURRENT
ARINC816-1
This document defines an open encoding format for airport databases which are loaded in airborne systems. This format, when designed and implemented, will enable a quick, economic, and efficient use of AMDB. However, since industry does not require applications to be standardized, data interpretation is not addressed in this document.
Standard

EMBEDDED INTERCHANGE FORMAT FOR AIRPORT MAPPING DATABASE
2016-08-31
CURRENT
ARINC816-3
This document defines an open encoding format for airport databases which are loaded in airborne systems. This format, when designed and implemented, will enable a quick, economic, and efficient use of AMDB. However, since industry does not require applications to be standardized, data interpretation is not addressed in this document.
Standard

DESIGN GUIDELINES FOR AIRCRAFT CABIN HUMAN MACHINE INTERFACES
2011-06-01
CURRENT
ARINC837
This document provides guidance for standard cabin systems control panel Graphical User Interfaces (GUI) intended to improve the human-machine interface. The document defines control and indication elements for various cabin functions, including cabin lighting, cabin temperature, door status, and the like. Standardization of cabin system interfaces will enable airlines to have consistent cabin operations across their fleets and reduce cabin crew training costs.
Standard

DEFINITION OF STANDARD INTERFACES FOR GALLEY INSERT (GAIN) EQUIPMENT PHYSICAL INTERFACES
2015-11-23
CURRENT
ARINC810-5
ARINC 810 defines galley equipment physical attachments, envelopes, connections, and qualification guidelines for interchangeable galley equipment. Supplement 5 defines a size 6 galley insert, intended for microwave oven installation and other equipment suited to this type of installation. Supplement 5 also clarifies reference dimensioning for all GAIN sizes defined by ARINC 810.
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