Search Results

Standard

LOGICAL SOFTWARE PART PACKAGING FOR TRANSPORT

2020-11-16

CURRENT

ARINC641-1

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

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

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

AVIONICS REFRIGERATION COOLING SYSTEM

2017-10-27

CURRENT

ARINC728

This standard provides standards for the in accordance with which aircraft operators and manufacturers can order avionics refrigeration units and can design installations for an ARCS.

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

GUIDANCE FOR STANDARD SUBDIVISION OF ATA SPEC. 100 FOR NUMBERING SYSTEM FOR AVIONICS

1971-10-06

CURRENT

ARINC421

This guidance standard was prepared in response to a need stated by air transport operators for uniformity in further subdividing the ATA Spec. 100 number system to better accommodate avionics systems. The ATA numbers are widely used in the maintenance community for inventory control, instruction manuals and equipment modification Service Bulletins.

Standard

ENVIRONMENTAL DESIGN GUIDELINES FOR INTEGRATED MODULAR AVIONICS PACKAGING AND INTERFACES

1994-12-09

CURRENT

ARINC654

This standard is concerned with electromagnetic compatibility, shielding, thermal management, vibration and shock of IMA systems. Emphasis is placed both on the design of IMA components and their electrical, optical and electro-mechanical interfaces.

Standard

AIRCRAFT DATA NETWORK PART 4 INTERNET-BASED ADDRESS STRUCTURE & ASSIGNED NUMBERS

2007-12-21

CURRENT

ARINC664P4-2

This specification defines the addressing plan and rules for addressing used in Aircraft Data Networks (ADN). The plan is organized in accordance with the seven-layer Open Systems Interconnection (OSI) Reference Model. The specification sets forth the structure of addresses that are employed in the ADN and guidance for address determination. This guidance ensures that all applications - that use this address structure to send messages - can know the address structure of the destination(s) at configuration-time.

Standard

LOGICAL SOFTWARE PART PACKAGING FOR TRANSPORT

2015-07-31

CURRENT

ARINC641

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

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

PROGRAMMERS GUIDE FOR SMART SYSTEMS USING ARINC 626 ATLAS

2002-06-30

CURRENT

ARINC627-2

This standard provides guidance to ATLAS test programmers for developing, writing and documenting test programs in ARINC 626 ATLAS. This is a companion standard to ARINC 608A, Design Guidance for Avionics Test Equipment. It provides guidance to managers and system integrators for standardizing test programs and their documentation.

Standard

DESIGN GUIDANCE FOR AVIONICS TEST EQUIPMENT

1993-01-15

CURRENT

ARINC608A

This standard is a top-level guidance standard intended for the design of Automatic Test Equipment (ATE). It includes the definition of hardware and software needed for analog and digital signal testing using a Test Unit Adapter common interface. This standard describes the overall ATE system concept as well as the definition of the specific elements of those systems.

Standard

USERS GUIDE FOR ARINC 616 AVIONICS SUBSET OF ATLAS

2017-11-29

CURRENT

ARINC605

This guide has been written as an applications manual for writing avionics test specifications that conform to ARINC Specification 616. It provides advice for converting ATLAS test specifications into ATLAS test programs and implementing them on Automatic Test Equipment (ATE).This guide has been written as an applications manual for writing avionics test specifications that conform to ARINC Specification 616. It provides advice for converting ATLAS test specifications into ATLAS test programs and implementing them on Automatic Test Equipment (ATE).

Standard

STANDARD ATLAS LANGUAGE FOR MODULAR TEST

1995-01-30

CURRENT

ARINC626-3

This standard defines an airline-recommended subset of the Abbreviated Test Language for All Systems (ATLAS)intended to be used in conjunction with test systems that are compliant with ARINC 608A. ATLAS is a standard abbreviated English language used in preparation and documentation of test procedures that can be implemented with automatic or semiautomatic test equipment.