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Standard

FIBER OPTIC TRAINING REQUIREMENTS

2019-01-10
CURRENT
ARINC807-4
This document is based upon the SAE ARP5602 document, A Guideline for Aerospace Platform Fiber Optic Training and Awareness Education. ARINC Report 807: Fiber Optic Training Requirements is a subset of the SAE ARP5602 document designed to meet the requirements of the commercial air transport industry. Certification to the SAE ARP5602 document fulfills the requirements of ARINC Report 807. This document defines recommended general practices for training requirements of aerospace fiber optic systems. It is the intention of this document to outline proven training practices and general standards of workmanship for technicians engaged in aerospace fiber optic manufacturing, installation, maintenance, and repair for the air transport industry. It is also recommended that management and purchasing personnel receive fundamental training to familiarize themselves with the requirements of aerospace fiber optics.
Standard

AIR TRANSPORT AVIONICS EQUIPMENT INTERFACES

2017-07-11
CURRENT
ARINC600-20
ARINC 600 is a mechanical packaging standard that is used with the ARINC 700-series of digital avionics equipment. It provides mechanical, electrical, and environmental interfaces between LRUs and the racks or cabinets in which they are installed. Provides connector shell definition, connector insert layout and mounting dimensions.
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.
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

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

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.
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

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

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

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 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

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

CABIN EQUIPMENT INTERFACES PART 2 PHYSICAL LAYER - IN - SEAT PROTOCOL

2010-12-08
CURRENT
ARINC485P2-4
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 3 IN-FLIGHT ENTERTAINMENT SYSTEM (IFES) TO AIRCRACT SYSTEM INTERFACES

2010-11-12
CURRENT
ARINC628P3-2
This standard consolidates and defines various interface parameters, except for power, that may be required to support the operation of an IFES on any airplane model. Supplement 2 adds an Ethernet interface between the aircraft Cabin Services System (CSS) and In-Flight Entertainment System. This interface may be used to exchange information between the CSS and The Passenger Service System (PSS), passenger address/entertainment, airplane mode, navigation, and operational data.
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 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 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 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.
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