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Standard

VHF DIGITAL LINK (VDL) MODE 2 IMPLEMENTATION PROVISIONS

2017-07-10
CURRENT
ARIS631-7
This document describes the functions to be performed by airborne and ground components of the VDLM2 to successfully transfer messages from VHF ground networks to avionics systems on aircraft and vice versa where the data are encoded in a code and byte independent format. The compatibility of VDLM2 with OSI is established by defining a set of services and protocols that are in accordance with the OSI basic reference model. The compatibility with the ATN protocols is achieved by defining a set of interfaces between the VDLM2 subnetwork protocol specification and the Mobile Subnetwork Dependent Convergence Function (MSNDCF). The SNDCF is defined in the ICAO ATN SARPs.
Standard

MULTI-TRANSMITTER DATA BUS PART 1 TECHNICAL DESCRIPTION

1999-03-31
CURRENT
ARIS629P1-5
Defines the aviation industry standards for transfer of digital data between avionics system elements using multiple access, bi-directional protocol. Developed to provide an efficient data distribution system resulting in a reduction in the amount of airplane wiring and equipment interfaces.
Standard

CABIN EQUIPMENT INTERFACES PART 9 CABIN INTERFACE NETWORK (CIN)

2015-11-20
CURRENT
ARIS628P9-4
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 5 CABIN ELECTRICA EQUIPMENT AND WIRING INSTALLATION GUIDELINES

2013-06-14
CURRENT
ARIS628P5-3
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 6 FIBER OPTIC CABLE ASSEMBLY GENERAL SPECIFICATION

2002-02-28
CURRENT
ARIS628P6
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

MULTI-TRANSMITTER DATA BUS PART 2 APPLICATIONS GUIDE

1999-02-26
CURRENT
ARIS629P2-2
Defines the aviation industry standards for transfer of digital data between avionics system elements using multiple access, bi-directional protocol. Developed to provide an efficient data distribution system resulting in a reduction in the amount of airplane wiring and equipment interfaces.
Standard

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

2005-02-28
CURRENT
ARIS628P4A-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 3 IN-FLIGHT ENTERTAINMENT SYSTEM (IFES) TO AIRCRACT SYSTEM INTERFACES

2010-11-12
CURRENT
ARIS628P3-2
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 4B CABIN MANAGEMENT AND ENTERTAINMENT SYSTEM CABIN DISTRIBUTION SYSTEM - STAR WIRING

1999-06-18
CURRENT
ARIS628P4B
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
ARIS628P4C
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

AVIONICS APPLICATION SOFTWARE STANDARD INTERFACE PART 4-SUBSET SERVICES

2012-06-28
CURRENT
ARIS653P4
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
ARIS653P5
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

AVIONICS APPLICATION SOFTWARE STANDARD INTERFACE PART 0 OVERVIEW OF ARINC 653

2015-08-03
CURRENT
ARIS653P0-1
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
ARIS653P1-4
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

AVIONCS APPLICATION SOFTWARE STANDARD INTERFACE PART 2 EXTENDED SERVICES

2015-08-21
CURRENT
ARIS653P2-3
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

LOGICAL SOFTWARE PART PACKAGING FOR TRANSPORT

2015-07-31
CURRENT
ARIS641
The purpose of this standard is to provide a method for packaging aircraft software parts for distribution using contemporary media or by electronic distribution. This project intends to standardize and provide guidance for the storage of floppy based software, currently packaged in media set parts. This standard format can be then stored or distributed on a single physical media member (CD-ROM), or by electronic crate. The obsolescence of floppy disks drive an urgent need for this guidance.
Standard

ETHERNET LOCAL AREA NETWORK (ELAN)

1995-01-08
CURRENT
ARIS646
This standard provides general and specific design and implementation guidelines for the use of IEEE 802.3 (ISO/IEC 8802-3) compliant Ethernet Local Area Networks (ELAN) in the commercial avionics environment. Maximum utilization of commercial components (hardware and/or software) and equipment is emphasized.
Standard

FLIGHT RECORDER ELECTRONIC DOCUMENTATION (FRED)

2009-07-14
CURRENT
ARIS647A-1
This specification is an international standard defining the content and format of electronic files which document Flight Data Recording systems. The FRED specification is an expansion of the Flight Recorder Configuration Standard (FRCS) and is intended to provide guidelines for software systems designers and developers of ground support equipment for flight data recorders. The FRED specification has been developed to facilitate the exchange of Flight Data Recorder (FDR) documentation between aircraft manufacturers, operators, and government agencies. This specification addresses the ARINC Specification 664: Part 7, Avionics Full Duplex Switched Ethernet in numerous sections.
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