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Standard

3GCN - CABIN DISTRIBUTION SYSTEM

2010-11-26
CURRENT
ARINC808-2
This Specification defines general architectural philosophy and aircraft infrastructure for the proper use and interface of various cabin related IFE equipment. Compliance with ARINC Specification 808 allows each respective system to operate in concert when integrated with other relevant cabin equipment. ARINC Specification 808 defines standards for the aircraft 3rd Generation Cabin Network (3GCN), IFE Cabin Distribution System (CDS), wiring, connectors, power, identification codes, space envelopes, and mounting principles. Although some of these standards also apply to 3GCN wireless IFE systems, the overall 3GCN wireless IFE network specification is covered in ARINC Specification 820. The equipment itself is not a subject of this specification because it may be unique to the system manufacturer or marketplace-driven. Design guidelines are included for informational purposes as these guidelines impact the interfaces and installation of cabin equipment aboard the aircraft.
Standard

3GCN - SEAT DISTRIBUTION SYSTEM

2014-08-15
CURRENT
ARINC809-3
This specification defines general architectural philosophy and specific design guidance for the proper installation and interface of various cabin equipment within the seats. Consistency with this specification allows each component installed on the seat to operate in concert when integrated with other relevant cabin type equipment. Standard electrical and mechanical interfaces of the In- Flight Entertainment System (IFES) equipment for the 3rd Generation Cabin Network (3GCN) associated with the seat are defined. This equipment consists of the headphone jacks (HPJ), passenger control unit (PCU)/multi function handset (including the cord), seat video display (SVD), remote data outlet (RDO), integrated seat box (ISB) which includes the seat power box (SPB)/seat data box (SDB), remote power outlet (RPO), and in-seat cables. Appropriate definitions are also provided for other electrical devices associated with the seat control/position mechanism.
Standard

AIRCRAFT DATA NETWORK PART 1 SYSTEMS CONCEPTS AND OVERVIEW

2006-06-30
CURRENT
ARINC664P1-1
This specification provides the overview of aircraft data networks installed in air-transport aircraft, tutorial information for adaptation of commercial network standards to air-transport aircraft, and terminology used to describe aircraft data networks. This specification explains the dependency of Aircraft Data Network (ADN) standards on network standards developed by the Internet community, IEEE, and ISO. The classes, Compliant Networks and Profiled Networks, used to characterize aircraft networks are introduced.
Standard

AIRCRAFT DATA NETWORK, PART 2 - ETHERNET PHYSICAL AND DATA LINK LAYER SPECIFICATION

2009-01-16
CURRENT
ARINC664P2-2
This specification provides Ethernet physical parameters and data link layer specifications for use in a commercial aircraft environment. This specification provides general and specific guidelines for the use of IEEE 802.3 compliant Ethernet, 2000 edition. Physical layer and Medium Access Control (MAC) sub-layers are expected to comply with the Open System Interconnection (OSI) Reference Model to enable maximal utilization of off-the-shelf components, both hardware and software, for aviation use. The Ethernet Physical layer specification defines the electrical and optical parameters for the 10BASE-T, 100BASE-TX, and 100BASE-FX Ethernet implementations. This specification references ARINC Specification 600: Air Transport Avionics Equipment Interfaces for definition of copper-based implementations of the Ethernet Physical layer.
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.).
Standard

AVIONCS APPLICATION SOFTWARE STANDARD INTERFACE PART 2 EXTENDED SERVICES

2015-08-21
CURRENT
ARINC653P2-3
As avionics software continues to evolve, so does ARINC Specification 653. ARINC 653 Part 2 specifies extensions (i.e., optional services) to the required Application Program Interfaces (APIs) described in ARINC 653 Part 1. Supplement 3 adds optional multicore services capabilities.
Standard

AVIONICS APPLICATION SOFTWARE STANDARD INTERFACE PART 0 OVERVIEW OF ARINC 653

2015-08-03
CURRENT
ARINC653P0-1
This document provides an overview of the entire set of documents collectively referred to as ARINC 653. As this set of documents evolves, Supplements to Parts 1 through 5 will be made more consistent with Part 0 in conjunction with the technical changes expected to be made in the evolution of ARINC 653. A summary of the ARINC 653 documents follows: Part 0 - Overview of ARINC 653, Part 1 - Required Services, Part 2 - Extended Services, Part 3 - Conformity Test Specification, Part 4 - Subset Services, and Part 5 - Core Software Required Capabilities. Supplement 1 reflects the introduction of multicore processor support in Parts 1 and 2.
Standard

AVIONICS APPLICATION SOFTWARE STANDARD INTERFACE PART 1 REQUIRED SERVICES

2015-08-21
CURRENT
ARINC653P1-4
This standard defines a general-purpose Application/Executive (APEX) software interface between the Operating System of an avionics computer and the application software. The interface requirements between the application software and operating system services are defined in a manner that enables the application software to control the scheduling, communication, and status of internal processing elements. Supplement 4 adds multicore processor service capabilities.
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 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

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

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

CABIN CONNECTORS AND CABLES PART 1 DESCRIPTION AND OVERVIEW

2012-11-19
CURRENT
ARINC800P1
This document is the first of a multi-part specification that will provide a catalog of cabin connector and cables that may be used in ARINC Standard cabin systems, including In-Flight Entertainment. Part 1 describes connector and cable requirements and evaluation criteria for the interface components used in the integration of cabin systems. Future releases will define connectors, contacts, and termination methods in Part 2. Cables will be specified in Part 3.
Standard

CABIN EQUIPMENT INTERFACES 4GCN CABIN MANAGEMENT AND ENTERTAINMENT SYSTEM, CABIN DISTRIBUTION SYSTEM

2016-07-14
CURRENT
ARINC832-1
ARINC Specification 832 defines standards for the aircraft 4th Generation Cabin Network (4GCN) Cabin Distribution System (CDS) wiring, connectors, power, identification codes, space envelopes, and mounting principles. Design guidelines are included for informational purposes as these guidelines impact the interfaces and installation of cabin equipment aboard the aircraft.
Standard

CABIN EQUIPMENT INTERFACES PART 0 CABIN MANAGEMENT AND ENTERTAINMENT SYSTEM - OVERVIEW

2015-07-27
CURRENT
ARINC628P0-3
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 user in preparing quick-reaction overhead projection-type presentations. Supplement 3 represents a summary of recent changes to Parts 1 through 9 of ARINC Specification 628.
Standard

CABIN EQUIPMENT INTERFACES PART 4A CABIN MANAGEMENT AND ENTERTAINMENT SYSTEM CABIN DISTRIBUTION SYSTEM DAISY CHAIN

2005-02-28
CURRENT
ARINC628P4A-3
Cabin equipment interfaces use a standardized wiring topology defined in Part 4A. This standard defines a standard CDS using a daisy chain wiring topology. This standard defines standard wiring, connectors and installation requirements for a passenger seat network, overhead video network, and cabin management equipment network. Electrical and fiber optic networks are covered.
Standard

CABIN EQUIPMENT INTERFACES PART 4B CABIN MANAGEMENT AND ENTERTAINMENT SYSTEM CABIN DISTRIBUTION SYSTEM - STAR WIRING

1999-06-18
CURRENT
ARINC628P4B
Cabin equipment interfaces Part 4B is similar to description provided for Part 4A. The significant difference is that Part 4B specifies a CDS using a star wiring topology. Standardized wiring, connectors and installation requirements for a passenger seat network, overhead video network, and cabin management equipment network are included. Electrical and fiber optic networks are covered.
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