ARINC Standards Store
ARINC Standards - 500 Series
500 Series ARINC Characteristics define analog avionics installed on older aircraft such as the B-727, DC-9, and DC-10, and earliy models of B-737, B-747, and A-300 aircraft. These standards are provided for reference and not recommended for use in new aircraft type designs.
535A
Last Published:
March 1972
535A Lightweight Headset and Boom Microphone
Defines standards for a lightweight headset with integral boom microphone suitable for pilot use in ...conventional airborne radio installations.
535B-1
Last Published:
June 2016
535B-1 Lightweight Headset and Boom Microphone
This document describes the aircraft industry recommendations for a headset with integral boom micro...phone 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.
538B-1
Last Published:
February 1983
538B-1 Hand-Held Microphone
This standard describes a hand-held microphone for use with airborne radio installations.
538C
Last Published:
January 2014
538C Handheld Microphone and Boomset Microphone
This document describes the aircraft industry recommendations for a handheld microphone and boom mic...rophone for use with airborne radio installations. This document, ARINC Characteristic 538C, is in addition to and does not supersede the older ARINC Characteristic 538B: Hand-Held Microphone, dated February 16, 1983.
542A
Last Published:
January 1988
542A Digital Flight Data Recorder
This standard includes specific requirements necessary to support flight data recording and other fl...ight data acquisition needs. Design details necessary to ensure interchangeability of equipment in a standard aircraft installation is included.
561-11
Last Published:
January 1975
561-11 Air Transport Inertial Navigation System (INS)
This standard defines the requirements of an INS, which provides sensor and steering command outputs.... The INS includes inertial sensing and provides outputs for aircraft attitude, present position, and steering signals suitable for operating the pilotýs instruments. The basic INS provides complete self-contained horizontal navigation capability intended to serve as the sole means of navigation on a worldwide basis.
562
Last Published:
December 2001
562 Terrain Awareness and Warning System (TAWS) - Analog
Terrain Awareness and Warning System (TAWS)ý Analog addresses the need for standard TAWS installati...ons 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.
566A-9
Last Published:
January 1998
566A-9 Mark 3 VHF Communications Transceiver
This standard defines the characteristics of a VHF Communications Transceiver unit capable of provid...ing voice or data communications capability with the ground. Supplement 8 introduces 8.33 kHz channel spacing.
573-7
Last Published:
December 1974
573-7 Aircraft Integrated Data System Mark 2 (AIDS Mark 2)
This standard provides design guidance for the development and installation of an expandable Flight ...Data Acquisition and Recording System. The functions defined include flight data acquisition through suitable electrical interfaces, conversion of analog input signals into a standard serial data output and the capability for expansion to permit increased data handling capacity.
577-1
Last Published:
March 1975
577-1 Audible Warning System
This standard provides basic requirements for audible warning generators, whose function is to provi...de 25 different channels with sound and/or voice warnings, activated by discrete input signals and generated as a function of an unsafe condition of important systems of the aircraft. The outputs are available for audible display to the cockpit crew.
578-4
Last Published:
October 1988
578-4 Airborne ILS Receiver
This standard provides basic requirements for a new-generation ILS receiver, whose function is the r...eception of ILS localizer and glide slope signals and the recovery there from of course-line deviation information for visual display to the pilot, and for use by an automatic flight control system during automatically controlled approaches and landings.
579-2
Last Published:
August 1989
579-2 Airborne VOR Receiver
This standard sets the basic requirements for a VOR receiver, whose function is to receive and proce...ss VOR signals in the frequency band 108.00 to 117.95 MHz. Provides traditional analog outputs and a digital output of omni bearing.
585-2
Last Published:
April 1978
585-2 Electronic Chronometer System
This standard defines an Electronic Chronometer that provides time-of-day (GMT) indication to the fl...ight crew, as well as providing this data in digital form for use by other avionic systems. In addition, the ECS provides an Elapsed Time Indicator (hours and minutes) with a start/stop/reset function and a chronograph function.
591
Last Published:
July 1972
591 Quick Access Recorder for AIDS System (QAR)
This standard provides design guidance for development and installation of a QAR, whose basic functi...ons are to store digital data supplied at the output of an ARINC 573 FDAU or other similar acquisition unit and provide an easy access to this stored data for systematic ground processing for performance monitoring, maintenance monitoring or other purposes.
594-4
Last Published:
March 1984
594-4 Ground Proximity Warning System
This standard sets forth the characteristics of a Ground Proximity Warning System (GPWS) designed fo...r installation in commercial aircraft. The GPWS provides audible and visible warnings or alerts when an aircraft approaches terrain or deviates below the ILS glide slope beyond the limits set into the system.
595
Last Published:
February 1975
595 Barometric Altitude Rate Computer (BARC)
This standard provides general guidance for the design and installation of a BARC for use with a GPW...S. The BARC generates an electrical rate signal from pneumatic pressure supplied by the aircraft static pressure system. The BARC unit is intended primarily for use with ground proximity warning equipment in aircraft that do not have a suitable electrical signal for altitude rate.
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