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Standard

STANDARD ATLAS LANGUAGE FOR MODULAR TEST
1995-01-30
CURRENT
ARINC626-3
This standard defines an airline-recommended subset of the Abbreviated Test Language for All Systems (ATLAS)intended to be used in conjunction with test systems that are compliant with ARINC 608A. ATLAS is a standard abbreviated English language used in preparation and documentation of test procedures that can be implemented with automatic or semiautomatic test equipment.
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

PROGRAMMERS GUIDE FOR SMART SYSTEMS USING ARINC 626 ATLAS
2002-06-30
CURRENT
ARINC627-2
This standard provides guidance to ATLAS test programmers for developing, writing and documenting test programs in ARINC 626 ATLAS. This is a companion standard to ARINC 608A, Design Guidance for Avionics Test Equipment. It provides guidance to managers and system integrators for standardizing test programs and their documentation.
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

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

FIBER OPTIC TEST PROCEDURES
2019-01-28
CURRENT
ARINC805-5
This document defines general practices for testing the physical layer of a fiber optic cable system. It is the intention of this document to outline proven practices for engineers and technicians engaged in testing and supporting fiber optic cable systems in aircraft. This document defines general practices for testing the physical layer of a fiber optic cable system. It is the intention of this document to outline proven practices for engineers and technicians engaged in testing and supporting fiber optic cable systems in aircraft.
Standard

FIBER OPTIC TEST PROCEDURES
2014-01-06
CURRENT
ARINC805-4
This document defines general practices for testing the physical layer of a fiber optic cable system. It is the intention of this document to outline proven practices for engineers and technicians engaged in testing and supporting fiber optic cable systems in aircraft.
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.
Standard

COCKPIT DISPLAY SYSTEM INTERFACES TO USER SYSTEMS PART 1 AVIONICS INTERFACES, BASIC SYMBOLOGY, AND BEHAVIOR
2019-06-17
CURRENT
ARINC661P1-7
ARINC 661 defines logical interfaces to Cockpit Display Systems (CDS) used in all types of aircraft installations. The CDS provides graphical and interactive services to user applications within the flight deck environment. When combined with data from user applications, it displays graphical images to the flight deck crew. The document emphasizes the need for independence between aircraft systems and the CDS. This document defines the interface between the avionics equipment and display system graphics generators. This document does not specify the "look and feel" of any graphical information, and as such does not address human factors issues. These are defined by the airline flight operations community. Supplement 7 adds the definition of: Selector Widget, Tree Widget, New FormatString options, Readouts available in MapItems, Provisions for Touch Screen Displays.
Standard

COCKPIT DISPLAY SYSTEM INTERFACES TO USER SYSTEMS PART 1 AVIONICS INTERFACES, BASIC SYMBOLOGY, AND BEHAVIOR
2020-09-18
CURRENT
ARINC661P1-8
ARINC 661 defines logical interfaces to Cockpit Display Systems (CDS) used in all types of aircraft installations. The CDS provides graphical and interactive services to user applications within the flight deck environment. When combined with data from user applications, it displays graphical images to the flight deck crew. The document emphasizes the need for independence between aircraft systems and the CDS. This document defines the interface between the avionics equipment and display system graphics generators. This document does not specify the "look and feel" of any graphical information, and as such does not address human factors issues. These are defined by the airline flight operations community. Supplement 8 adds numerous changes and additions. Eleven new widgets are added, all related to 3D Maps. Seven new widget extensions. Metadata definitions (XML) for all widgets, extensions, events, symbols, and associated data types.
Standard

COCKPIT DISPLAY SYSTEM INTERFACES TO USER SYSTEMS
2016-09-01
CURRENT
ARINC661-6
ARINC 661 defines necessary interfaces to Cockpit Display Systems (CDS) used in all types of aircraft installations starting with the Airbus A380 airplane. The CDS provides graphical and interactive services to user applications within the flight deck environment. When combined with data from user applications, it displays graphical images to the flight deck crew. The document emphasizes the need for independence between aircraft systems and the CDS. This document defines interfaces between the CDS and the aircraft systems. This includes the interface between the avionics equipment and display system graphics generators. This document does not specify the "look and feel" of any graphical information, and as such does not address human factors issues. These are defined by the airline flight operations community.
Standard

CABIN STANDARD ENCLOSURES - MODULAR RACK PRINCIPLE (MRP)
2012-06-22
CURRENT
ARINC836
This document provides installation standards for cabin equipment and related mechanical enclosures. It provides provisions for equipment attachment on overhead racks and monuments. The document provides a series of standard volumes and associated masses. Standardized packaging of cabin systems components is expected to yield simpler installation and maintenance of cabin equipment. This is expected to reduce the time and cost related to installing and maintaining cabin systems.
Standard

CABIN STANDARD ENCLOSURES
2018-11-20
CURRENT
ARINC836A
The purpose of this specification is to define standard cabin equipment enclosures and provisions for equipment attachment on monuments. This standard is intended to enable simpler installation and maintenance of cabin equipment, resulting in time and cost reduction.
Standard

CABIN PASSENGER SEAT PRODUCTION TESTING
2019-12-18
CURRENT
ARINC648
This report defines the requirements and recommended practices for production testing of aircraft passenger seats and seat groups. Production testing is performed at the seat manufacturers' facilities prior to the shipment of the seats to the airframe manufacturers, Maintenance, Repair, and Overhaul (MRO), or airlines/operators for installation in the aircraft. Using this guidance, rework is minimized and schedules remain minimally affected.
Standard

CABIN EQUIPMENT NETWORK BUS
2020-06-19
CURRENT
ARINC854
This standard defines a new cabin network bus. While ARINC Specification 485: Cabin Equipment Interfaces, Part 2, Physical Layer – In-seat Protocol defined a low-speed serial communications interface between electronic equipment in the passenger seat, it is design-focused on obtaining status from in-seat electronic equipment. ARINC Specification 854 is a messaging protocol but does not preclude using the bus for video streaming or multicast. Cabin Equipment has evolved from the very simple to quite sophisticated systems. The resulting communications needs have surpassed the ability of ARINC 485 to provide the necessary data capacity and response times. The basic requirements for low latency, full duplex, elimination of ARINC 485 Master/Slave polling and lower weight drives the selection of 100BASE-T1 (per IEEE 802.3) as the preferred bus format.
Standard

CABIN EQUIPMENT INTERFACES PART 9 CABIN INTERFACE NETWORK (CIN)
2015-11-20
CURRENT
ARINC628P9-4
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 4 defines web-based interfaces for cabin control panels and recognizes current standards for commercial browsers and applications. It incorporates current network security practices, including reference to ARINC 842 Digital Certificates.
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