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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

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

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

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

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 CONNECTORS AND CABLES PART 4 STANDARD TET METHODOLOGY

2015-12-01

CURRENT

ARINC800P4

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

GUIDANCE FOR TOOL AND TEST EQUIPMENT (TTE) EQUIVALENCY

1996-03-01

CURRENT

ARINC732-1

This standard defines an airborne tape reproducer for passenger entertainment. The function of this equipment is to play pre-recorded tapes to the passengers through the airplane passenger entertainment system. Some channels may be used for boarding music through the public address system.

Standard

GUIDANCE FOR TOOL AND TEST EQUIPMENT (TTE) EQUIVALENCY

1993-01-01

CURRENT

ARINC735-2

This standard defines as TCAS system capable of calculating the range, altitude and bearing of other aircraft equipped with Mode S transponders. The system monitors the trajectory of these aircraft for the purpose of determining if any of them constitute a potential collision hazard.

Standard

GUIDANCE FOR TOOL AND TEST EQUIPMENT (TTE) EQUIVALENCY

1988-04-01

CURRENT

ARINC737-1

This standard defines a system of sensors and monitoring equipment to determine aircraft weight while it is on the ground. The system serves as an aid to the pilot for determining aircraft weight distribution and center of gravity (CG).

Standard

GUIDANCE FOR TOOL AND TEST EQUIPMENT (TTE) EQUIVALENCY

2001-07-01

CURRENT

ARINC738-3

This standard defines an integrated ADIRS that provides air data information and directional guidance information for cockpit display. The ADIRS consists of up to three Air Data/Inertial Reference Units (ADIRUs) located in the aircraft electronic rack, an associated Control and Display Unit (CDU) and remotely mounted Air Data Modules (ADMs).

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

FULL-FORMAT PRINTER

1990-12-30

CURRENT

ARINC744

This standard sets forth the characteristics of a full-format printer capable of printing up to 132 characters of alphanumeric and/or semi-graphic data on 8.5 x 11 inch or A4 paper size. Participating equipment interface using ARINC 429 data buses. It is optionally capable of producing hard-copy graphics in the form of addressable dot plotting data.

Standard

FULL-FORMAT PRINTER WITH GRAPHICS CAPABILITY

1994-03-01

CURRENT

ARINC744A-1

This standard sets forth the characteristics of a full-format printer capable of printing high resolution alphanumeric, semi-graphic and graphic images on 8.5x11-inch or A4 size paper. The printer is intended to be compatible with ARINC 744 printers. It has two bi-directional high-speed Ethernet ports to facilitate transfer of high throughput and burst mode data.

Standard

CABIN STANDARD ENCLOSURES - MODULAR RACK PRINCIPLE (MRP)

2012-06-22

CURRENT

ARINC836

This document provides installation standards for cabin equipment and related mechanical enclosures. It provides provisions for equipment attachment on overhead racks and monuments. The document provides a series of standard volumes and associated masses. Standardized packaging of cabin systems components is expected to yield simpler installation and maintenance of cabin equipment. This is expected to reduce the time and cost related to installing and maintaining cabin systems.

Standard

MARK 5 AIRBORNE DISTANCE MEASURING EQUIPMENT

1988-10-31

CURRENT

ARINC709-8

This standard sets forth characteristics of a DME intended for installation in commercial transport aircraft. It provides slant range distance from an aircraft to a selected DME ground facility, which is presented to the flight crew on an indicator located in the instrument panel. Other applications include utilization of frequency scanning modes by navigation computers.

Standard

PRECISION AIRBORNE DISTANCE MEASURING EQUIPMENT (DME/P)

1994-08-17

CURRENT

ARINC709A-1

This standard provides general and specific design guidance for the development of a DME/P, which provides slant range distance from an aircraft to a selected DME ground facility. For landing purposes, the DME/P complements the angle MLS/ILS with precise range data.

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 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 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.