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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

AVIATION SATELLITE COMMUNICATION SYSTEM PART 2 SYSTEM DESIGN AND EQUIPMENT FUNCTIONAL DESCRIPTION

2012-06-27

CURRENT

ARINC741P2-11

This document describes the desired operational capability of the equipment as configured with the first generation Satellite Data Unit (SDU) to provide data and voice communications, as well as additional standards necessary to ensure interchangeability. Supplement 11 adds commentary on the commonality of physical interfaces between ARINC 741 systems defined for SwiftBroadband safety services and ARINC 741 systems defined only for the Inmarsat Classic Aero safety services. It adds the SwiftBroadband safety services to the SDU functional definition.

Standard

AVIONICS APPLICATION SOFTWARE STANDARD INTERFACE PART 0 OVERVIEW OF ARINC 653

2019-08-07

CURRENT

ARINC653P0-2

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 Part 0 will be made more consistent with Parts 1 through 5 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 0 OVERVIEW OF ARINC 653

2021-11-15

CURRENT

ARINC653P0-3

This document provides an overview of the entire set of documents collectively referred to as ARINC 653. As this set of documents evolves, Part 0 has been adjusted to reflect technical changes made in Supplements to Parts 1 through 5 in conjunction with the technical changes 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 3A – Conformity Test Specification for ARINC 653 Required Services Part 3B – Conformity Test Specification for ARINC 653 Extended Services Part 4 – Subset Services Part 5 – Core Software Recommended Capabilities The term “this document” refers to Part 0 only, while the term “ARINC 653” or “the Specification” refers to the whole set of ARINC 653 documents, currently Parts 0 to 5.

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

Air Transport Equipment Cases and Racking

1974-03-15

CURRENT

ARINC404A

This original "ATR" packaging standard provides a system of modularized equipment dimensions used in a wide variety of avionics installations. Connector standards, mating and holdown techniques are included.

Standard

BITE GLOSSARY

1986-12-18

CURRENT

ARINC612

The purpose of this standard is to provide a source of definitions of terms and acronyms commonly used in the air transport maintenance community for test and evaluation with an emphasis on terms applicable to BITE.

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 1 CABIN MANAGEMENT AND ENTERTAINMENT SYSTEM - PERIPHERALS

2005-08-14

CURRENT

ARINC628P1-7

This document defines general system architectural philosophy and specific design guidance for the design and interface of various cabin related equipment. System performance parameters are described for connectors, electrical interfaces, operational mode control/protocols, BITE reporting, reliability, environmental conditions, and software data loading. Supplement 7 defines an IEEE 802.11n compliant Cabin Wireless Access Point (CWAP) suitable for installation a wide variety of cabins. It also provides an update to the digital overhead monitor mounting provisions and connectors for compatibility with the CWAP definition.

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 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.

Standard

CABIN EQUIPMENT INTERFACES PART 4C CABIN MANAGEMENT AND ENTERTAINMENT SYSTEM - CABIN DISTRIBUTION SYSTEM - 2ND GENERATION - DAISY CHAIN

2005-09-15

CURRENT

ARINC628P4C

ARINC Specification 628 Part 4 defines standards for the aircraft IFE Cabin Distribution System (CDS) wiring, connectors, power, identification codes, space envelopes and mounting principles. The equipment itself is not a subject of this specification because it may be unique to the system manufacturer or market place driven. Design guidelines are included for informational purposes as these guidelines impact the interfaces and installation of cabin equipment aboard the aircraft. The CDS, in daisy chain architecture, is the content of both Parts 4A and 4C of ARINC Specification 628. Part 4C presents the second generation also known as 2GCN of the daisy chain topology, as an evolution based on the experience gained with the first version of the CDS. The main difference is that the system in Part 4C is divided into two separated networks, one for data, connected to the CEC, and the other one for power, connected to the Aircraft Power Supply.

Standard

CABIN EQUIPMENT INTERFACES PART 5 CABIN ELECTRICA EQUIPMENT AND WIRING INSTALLATION GUIDELINES

2013-06-14

CURRENT

ARINC628P5-3

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 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 EQUIPMENT INTERFACES PART 6 FIBER OPTIC CABLE ASSEMBLY GENERAL SPECIFICATION

2002-02-28

CURRENT

ARINC628P6

ARINC Specification 628, Cabin Equipment Interfaces (CEI) Part 6 Fiber Optic Cable Assembly General Specification, defines the minimum acceptable provisions for connectorized fiber optic cable assemblies used in permanently installed airframe wire bundles that are part of ARINC 628 supported systems. The intent is for the cable assembly supplier to use this specification as a guideline to provide the prospective IFE contractor with cable assemblies that have adequate quality and performance for the intended application. These assemblies are suitable for cabin systems applications only. Applicable guidelines not found in this specification may be found in Section 9 of ARINC Specification 628 Part 4A.

Standard

CABIN EQUIPMENT INTERFACES PART 7 CABIN EQUIPMENT COOLING GENERAL SPECIFICATION

2013-06-24

CURRENT

ARINC628P7-2

Cabin equipment installations tend to impose loads on aircraft electrical power systems not envisioned in the original airplane design. This standard provides guidance on the design of future aircraft air conditioning and equipment cooling systems. It also describes the environment in which cabin systems, including In-Flight Entertainment equipment are expected to operate.

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.