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Standard

AVIONICS APPLICATION SOFTWARE STANDARD INTERFACE PART 3A CONFORMITY TEST SPECIFICATIONS FOR ARINC 653 REQUIRED SERVICES
2021-11-15
CURRENT
ARINC653P3A-2
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

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

CABIN EQUIPMENT INTERFACES PART 5 CABIN ELECTRICAL EQUIPMENT AND WIRING INSTALLATION GUIDELINES
2020-07-24
CURRENT
ARINC628P5-4
ARINC Specification 628, Cabin Equipment Interfaces (CEI) Part 5 Parts Selection, Wire Design and Installation Guidelines, provides design and mounting guidelines for electrical installations, mainly for supplier of cabin furnishing equipment. Part 5 addresses several aspects of installation and is divided into five sections: Introduction, Parts Selection, Electrical Wire Design Guidelines, Wire Installation Guidelines, and Documentation Guidelines. Guidelines regarding design, safety, and other subjects relevant to acceptance of the end item are addressed. Notes explaining the reason for setting a guideline or suggesting methods for performing the task are provided in commentary. The content of the document is designed to make it usable for reference by industry, particularly manufacturers of seats and equipment.
Standard

CABIN CONNECTORS AND CABLES, PART 4, STANDARD TEST METHODOLOGY
2020-07-13
CURRENT
ARINC800P4-1
ARINC 800 is the first industry standard intended for characterization of aviation-grade high-speed (Gbps) Ethernet links. The test methods are based on realistic representation of cabin networks. The notional cabling architecture is based on IFE seat distribution using multiple intermediate disconnects. Sequential testing is supported by building up number of connectors in the link. Test guidelines for mixed intermediate cable lengths are provided.
Standard

CABIN EQUIPMENT INTERFACES PART 2 PHYSICAL LAYER - IN-SEAT PROTOCOL
2020-06-30
CURRENT
ARINC485P2-5
ARINC Specification 485, Part 2 specifies the ARINC 485-control protocol used by the LRUs described in ARINC Specification 628 Part 2. This document defines a multi-drop bus. The point-to-point configuration is also supported. The point-to-point bus is treated simply as a multi-drop bus with only one drop. There is one master LRU and one or more slave LRUs present on the bus. However; multiple buses may be connected in parallel, where each parallel bus operates independently from each other.
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 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

AVIONICS DIGITAL VIDEO BUS (ADVB) HIGH DATA RATE
2019-12-16
CURRENT
ARINC818-3
ARINC 818 defines the digital video interface standard intended for use in all types of flight deck displays. This document represents the aviation version of ANSI Fibre Channel Audio Video (FC-AV) defined by ANSI INCITS 356-2002. Supplement 3 Supports the latest digital video rates of 12 Gbps and higher using 64B/66B encoding and 28 Gbps using 256B/257B encoding.
Standard

CABIN ARCHITECTURE FOR WIRELESS DISTRIBUTION SYSTEM
2019-08-13
CURRENT
ARINC820
This document defines a secure Wi-Fi distribution network installed in the aircraft passenger cabin for passenger and crew use. Carry-on Portable Electronic Devices (PEDs) such as smart phones, tablets, and laptops may use this network to access public internet services provided on the aircraft.
Standard

AVIONICS APPLICATION SOFTWARE STANDARD INTERFACE PART 3A CONFORMITY TEST SPECIFICATIONS FOR ARINC 653 REQUIRED SERVICES
2019-07-18
CURRENT
ARINC653P3A-1C1
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 3B CONFORMITY TEST SPECIFICATIONS FOR ARINC 653 EXTENDED SERVICES
2019-07-18
CURRENT
ARINC653P3BC1
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

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

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

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 EQUIPMENT INTERFACES PART 0 CABIN MANAGEMENT AND ENTERTAINMENT SYSTEM - OVERVIEW
2018-08-28
CURRENT
ARINC628P0-4
The purpose of this document is to provide an introduction and overview of the ARINC 628 series of Specifications. ARINC 628 defines equipment and installation standards for cabin equipment, which is generally defined as communication and entertainment equipment designed for passenger use. Part 0 provides the concepts and overview of ARINC 628 and descriptions of each individual part. Appendix B is written in briefing chart format to facilitate the understanding of high-level objectives. Supplement 4 represents a summary of recent changes to Parts 1 through 9 of ARINC Specification 628.
Standard

FIBER OPTIC DESIGN GUIDELINES
2018-08-27
CURRENT
ARINC803-4
The purpose of ARINC Report 803 is to provide design and implementation guidelines together with a selection guide, providing a fiber optic system design engineer with documentation to assess the design requirements for an aerospace fiber optic installation.
Standard

CABIN EQUIPMENT INTERFACES PART 2 CABIN MANAGEMENT AND ENTERTAINMENT SYSTEM - SEAT INTERFACES
2017-07-10
CURRENT
ARINC628P2-9
This document defines standard electrical and mechanical interfaces of the In-Flight Entertainment System (IFES) equipment associated with the seat (including the headphones, passenger control unit, seat video display, personal video player, telephone hand set, and seat electronics box). Supplement 9 updates applicable interfaces for USB 3.1 outlets in passenger seats.
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