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Standard

WINDSHEAR WARNING AND GUIDANCE SYSTEM

1988-01-27
CURRENT
ARINC742
This standard describes stand-alone windshear warning system comprised of a windshear warning computer and associated cockpit displays. The system uses data pertaining to aircraft movement with respect to air movement to detect and annunciate a windshear condition. As an option, it may also provide instrument guidance to the crew indicating optimum pitch to endure the windshear encounter.
Standard

VHF DIGITAL LINK (VDL) MODE 2 IMPLEMENTATION PROVISIONS

2017-07-10
CURRENT
ARINC631-7
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

VHF DATA RADIO

2004-08-11
CURRENT
ARINC750-4
This standard specifies the form, fit and functional definitions for a VHF transceiver capable of voice and data communications. The VHF transceiver supports, 8.33 kHz AM and 25 kHz AM voice, and VDL-2 (31.5 kbps) data link communications as defined by ICAO. ARINC 631 is a companion standard.
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

UPPER LAYER SPECIFICATIONS (END SYSTEM COMMUNICATION SPECIFICATIONS)

1993-02-01
CURRENT
ARINC638
This standard provides general and specific guidance for the development and implementation of end system upper layer communication protocols in onboard and air/ground end systems operating in the aeronautical OSI based communications environment.
Standard

THRUST CONTROL COMPUTER SYSTEM

1983-10-31
CURRENT
ARINC703-2
The characteristics of a TCCS within the Automatic Flight System are defined in this standard for throttle control. The standard also provides general and specific design guidance for the development and installation of a TCCS.
Standard

TERRESTRIAL FLIGHT TELEPHONE SYSTEM (TFTS) AIRBORNE RADIO SUBSYSTEM

1995-12-11
CURRENT
ARINC752-1
This standard defines the characteristics of a full-duplex telephone service for Aeronautical Passenger Communications through a network of ground stations. The frequency bands of 1670-1675 MHz are used to receive and 1800-1805 MHz are used to transmit.
Standard

TERRAIN AWARENESS AND WARNING SYSTEM (TAWS)

2000-09-15
CURRENT
ARINC762-1
This standard sets forth the characteristics of a terrain awareness and warning system intended for installation in aircraft with digital signal interfaces. Describes the desired operational capability of the equipment, the standards necessary to ensure interchangeability, form factor, and pin assignments.
Standard

TERRAIN AWARENESS AND WARNING SYSTEM ((TAWS) - ANALOG

2001-12-12
CURRENT
ARINC562
Terrain Awareness and Warning System (TAWS)ý Analog addresses the need for standard TAWS installations in older aircraft that have analog equipment interfaces. The analog unit is intended as a replacement for ARINC Characteristic 594: Ground Proximity Warning System (GPWS) equipment. The document is intended to compliment ARINC Characteristic 762: Terrain Awareness and Warning System (TAWS) for later model aircraft having digital equipment interfaces.
Standard

STANDARD FIRMWARE LOADER FOR AVIONICS SHOPS

1989-09-30
CURRENT
ARINC614
This standard describes the characteristics of a standard firmware loader for avionic shops. It is capable of copying digital information into memory devices installed in circuit card assemblies, Line Replaceable Modules (LRMs) and On-Board Replaceable Modules (OBRMs). It contains the recommendations of the air transport community concerning the design and development of firmware loader equipment.
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

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.
Standard

SPECIFICATION CONNECTORS, RACK AND PANEL, RECTANGULA REAR RELEASE CRIMP CONTACTS

2015-06-01
CURRENT
ARINC404B-2
This document defines standardized connectors intended for use on rack-mountable avionics equipment. It is aligned to the latest version of MIL-C-81659. Supplement 2 was updated to support cabin equipment applications. It corrects intermateability control dimensions that are provided for single shell plug connectors.
Standard

SOFTWARE DATA LOADER USING ETHERNET INTERFACE

2007-06-30
CURRENT
ARINC615A-3
This standard defines data loading equipment intended for new generation avionics equipment with high-speed Ethernet interfaces. It defines a PDL for carry-on applications and an ADL for installation on the airplane. Specific mass storage media include 3.5 inch floppy disk and CD-ROM/DVD.
Standard

SOFTWARE DATA LOADER USING CAN INTERFACE

2013-12-20
CURRENT
ARINC826-1
The purpose of the standard is to provide a simple and efficient protocol for loading software parts to line replaceable units (LRUs) on a CAN bus, as an alternative to ARINC Report 615A or ARINC Report 615. It is not intended to become the only possible CAN software loading alternative. It is intended for those avionics devices that are software loadable.
Standard

SECOND GENERATION AVIATION SATELLITE COMMUNICATION SYSTEM, AIRCRAFT INSTALLATION PROVISIONS

2012-06-21
CURRENT
ARINC761-5
This document defines the characteristics of second generation L-band satellite communication system installations including the avionics equipment defined for Iridium and Inmarsat 2G services. This document provides traditional form, fit, function, and interface standards necessary for the installation of Satcom avionics equipment for all types of aircraft. It also provides a description of each envisioned avionics component that would comply with this Characteristic. Supplement 5 removes obsolete service and system provisions, and adds references to ARINC Characteristic 791 for Ku-band antenna installation details.
Standard

REMOTE DATA CONCENTRATOR (RDC) GENERIC DESCRIPTION

1999-04-05
CURRENT
ARINC655
The RDC have been used for years on commercial aircraft. The extensive use of digital data transfer has prompted the need for a standard for collecting analog, digital and discrete information from sensors on the airplane. This information is digitized and processed in traditional ARINC 700-series equipment or in IMA cabinets.
Standard

RECORDER INDEPENDENT POWER SUPPLY

2010-10-11
CURRENT
ARINC777-2
This Characteristic provides the definitions for the physical form and fit dimensions, the electrical interfaces, and the functions of an independent power supply for cockpit voice recorders or crash survivable recorders that combine voice with other recording functions. The RIPS is used to provide backup power that is independent of the aircraft generated power buses. Supplement 2 introduces a description of charge rates for alternate power sources and revises the electrical interface to accommodate monitoring of the RIPS status.
Standard

RADIO ALTIMETER

2009-04-06
CURRENT
ARINC707-7
This standard provides the desired characteristics of a RALT intended for installation in all types of commercial transport aircraft. Its primary function is to determine the aircraft's height above terrain for visual display to the pilot (essentially ground level to 2500 feet), and for use by the AFCS during automatically controlled approaches and landings.
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