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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

AIRBORNE WEATHER RADAR

1991-11-15
CURRENT
ARINC708-6
This standard defines the characteristics of WXR equipment intended for installation in commercial transport aircraft. The primary purpose is weather detection, ranging and analysis. Its secondary purpose is ground mapping to facilitate navigation by display of significant land contours.
Standard

AIRBORNE WEATHER RADAR WITH FORWARD LOOKING WINDSHEAR DETECTION CAPABILITY

1999-11-15
CURRENT
ARINC708A-3
This standard defines an airborne pulse Doppler weather radar system for weather detection and ranging. It expands the capabilities of the ARINC 708 system through the inclusion of forward looking windshear prediction. It also provides ground-mapping capabilities to facilitate navigation by display of significant land contours.
Standard

MARK 5 SUBSONIC AIR DATA SYSTEM

1988-01-11
CURRENT
ARINC706-4
This standard sets forth the characteristics of a digital ADS intended for installation in subsonic commercial transport aircraft. Provides essential air data information for display to pilots and for use by other aircraft systems. Consists of a computer unit located in the aircraft electronics rack and suitable indicators located in the cockpit.
Standard

MARK 3 AIR TRAFFIC CONTROL TRANSPONDER ATCRBS/MODE S)

1989-12-15
CURRENT
ARINC718-4
This document defines the Air Traffic Control Transponder (ATCRBS/Mode S) with that supports emerging Automatic Dependent Surveillance - Broadcast (ADS-B) requirements. Supplement 4 adds ADS-B Out capabilities and enables the Mode S Transponder to comply with Mode S Transponder MOPS (RTCA DO-181E and EUROCAE ED-73E) as entered into ICAO Annex 10 Volume IV and ICAO Doc. 9871.
Standard

AIRBORNE VHF COMMUNICATIONS TRANSCEIVER

2003-06-10
CURRENT
ARINC716-11
This standard sets forth characteristics of a VHF Communications Transceiver for installation in all types of commercial transport aircraft. The VHF transceiver can support 8.33 kHz AM or 25 kHz AM voice or ACARS (2400 bps) data communications.
Standard

MARK 4 SELECTIVE CALLING (SELCAL)

2015-11-04
CURRENT
ARINC714A
This document represents a significant improvement to existing Selective Calling (SELCAL) standards used with HF and VHF voice communications. The goal is to eliminate the possibility that two or more aircraft could respond to the same radio call. The Mark 4 SELCAL system definition provides the following: " Guidance for integrated and federated audio systems " 32 audio tones total (16+16) yielding up to 215,760 unique codes " SELCAL form, fit, & function definition " Interwiring and installation details " Defines SELCAL decoding requirements in the presence of significant signal degradation.
Standard

MARK 4 AIR TRAFFIC CONTROL TRANSPONDER (ATCRBS/MODE S)

2011-11-15
CURRENT
ARINC718A-4
Mark 4 Air Traffic Control Transponder (ATCRBS/MODE S) describes an Air Traffic Control Radar Beacon System/Mode Select (ATCRBS/Mode S) airborne transponder with Extended Interface Functions (EIF). The ATC surveillance system is made up of airborne transponders and ground interrogator-receivers, processing equipment, and antenna systems. Mode S is a cooperative surveillance system for air traffic control with ancillary communications capabilities. ARINC 718A supports elementary surveillance. Provisional enhanced surveillance functionality is also defined as a customer option. The Mark 4 transponder, like its predecessor, will support TCAS functions.
Standard

FLIGHT DATA ACQUISITION AND RECORDING SYSTEM

2011-06-06
CURRENT
ARINC717-15
This document provides design guidance for the development and installation of a Digital Expandable Flight Data Acquisition and Recording System (DEFDARS) primarily intended for airline use. As such, this guidance will include specific requirements necessary to accommodate mandatory flight data recording and other flight data acquisition needs plus the requirements to ensure customer controlled interchangeability of equipment in a standard aircraft installation. The system capability was expanded to accommodate a data bus speed of 1024 words per second.
Standard

AIRBORNE PASSENGER ADDRESS AMPLIFIER

1984-07-06
CURRENT
ARINC715-3
This standard describes the characteristics of a PA AMP designed for installation in commercial aircraft. Its function is to amplify control voice, music and internally generated chime audio signals to drive the aircraft cabin loudspeaker system.
Standard

AIRBORNE ADF SYSTEM

1992-07-15
CURRENT
ARINC712-7
This standard sets forth characteristics of an ADF system for installation in commercial transport aircraft. Function is to receive and process signals from non-directional range and other transmitters in the frequency band 190 kHz to 1750 kHz, to provide serial digital outputs of bearing, and to provide aural identification of the selected station.
Standard

MARK 3 AIRBORNE SELCAL SYSTEM

1990-08-15
CURRENT
ARINC714-6
Ground-to-air selective calling system characteristics are defined by this standard. The system allows selective calling of individual aircraft over radio communications circuits linking the ground station to the aircraft. Elements comprising overall system are ground selecting calling unit (coder), ground-to-air transmitter (HF or VHF), airborne receiver (HF or VHF), airborne selective calling unit (decoder), and code selection panel.
Standard

DIGITAL INFORMATION TRANSFER SYSTEM (DITS) PART 4 ARCHIVE OF ARINC 429 SUPPLEMENTS

2012-11-29
CURRENT
ARINC429P4
This document was prepared in conjunction with Supplement 18 to ARINC Specification 429, Part 1. It is an archive of all ARINC Specification 429 Supplements, currently published in parts. The technical content of each Supplement (unchanged in contents and in form) are reproduced for historical reference.
Standard

LIGHTWEIGHT HEADSET AND BOOM MICROPHONE

2016-06-06
CURRENT
ARINC535B-1
This document describes the aircraft industry recommendations for a headset with integral boom microphone suitable for pilot use in all types of aircraft using conventional radio installations. This document, ARINC Characteristic 535B, is in addition to and does not supersede the older ARINC Characteristic 535A: Lightweight Headset and Boom Microphone, dated March 3, 1972.
Standard

LIGHTWEIGHT HEADSET AND BOOM MICROPHONE

1972-03-03
CURRENT
ARINC535A
Defines standards for a lightweight headset with integral boom microphone suitable for pilot use in conventional airborne radio installations.
Standard

CABIN EQUIPMENT INTERFACES PART 2 PHYSICAL LAYER - IN - SEAT PROTOCOL

2010-12-08
CURRENT
ARINC485P2-4
ARINC Specification 485, Part 2 specifies the ARINC 485-control protocol used by the LRUs described in ARINC Specification 628 Part 2. This document defines a multi-drop bus. The point-to-point configuration is also supported. The point-to-point bus is treated simply as a multi-drop bus with only one drop. There is one master LRU and one or more slave LRUs present on the bus. However; multiple buses may be connected in parallel, where each parallel bus operates independently from each other.
Standard

CABIN EQUIPMENT INTERFACES PART 1 HEAD END EQUIPMENT PROTOCOL

2014-12-08
CURRENT
ARINC485P1-3
This standard defines the electrical characteristics, protocol and data content for a modified version of the EIA RS-485 data bus adapted for use with cabin electronics equipment. Specific cabin equipment interfaces are defined by ARINC 628.
Standard

DIGITAL FLIGHT DATA RECORDER

1988-01-21
CURRENT
ARINC542A
This standard includes specific requirements necessary to support flight data recording and other flight data acquisition needs. Design details necessary to ensure interchangeability of equipment in a standard aircraft installation is included.
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