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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 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

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

AERONAUTICAL MOBILE AIRPORT COMMUNICATION SYSTEM (AEROMACS) TRANSCEIVER AND AIRCRAFT INSTALLATION STANDARDS

2017-07-07

CURRENT

ARINC766

This documents defines the Installation Characteristics of an airborne radio transceiver capable of broadband wireless communication with an Airport Surface Network. The Aeronautical Mobile Airport Communications System (AeroMACS) Radio Unit (ARU) will operate in the aeronautical protected frequency of 5091 MHz to 5150 MHz, utilizing the IEEE 802.16e WiMAX protocol. It is intended to offload some of the congested narrowband VHF airport traffic used for ATS and AOC communications. ARU and Antenna Form, Fit, Function and Interfaces are described.

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

GATE-AIRCRAFT TERMINAL ENVIRONMENT LINK (GATELINK)-AIRCRAFT SIDE

1994-01-01

CURRENT

ARINC751

This standard describes the electrical and optical interface definitions for Gatelink communications. Gatelink is a 100 Mbps full-duplex communication link between a communication system inside the airport terminal (or at the maintenance position) and a communication system onboard a parked aircraft.

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.