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Standard

INTEGRATED MODULAR AVIONICS PACKAGING AND INTERFACES

1994-07-01
CURRENT
ARINC650
This standard defines the packaging details for IMA. It provides standards recommended for the design and installation of Line Replacement Module (LRM) in cabinet assemblies. Mechanical installation and interchangeability guidelines are provided for LRM interface to the cabinet frame and wire integration/backplane assembly. It defines connectors recommended for use with IMA systems.
Technical Paper

Vibration Qualification Test of an Aircraft Piccolo Tube Using Multiple-Input-Multiple-Output Control Technology

2013-09-17
2013-01-2315
Wing Anti-Icing Systems (WAIS) are integral part of a wing design. Their presence ensures safety in all-weather conditions. In standard designs, the WAIS are fitted in the slat internal structure and runs throughout its span in between the ribs. Given its critical function, such a system has to pass qualification test. The test specification is dictated by international standards. In the case discussed in this article, the standard adopted is the RTCA DO-160G “Environmental Conditions and Test Procedures for Airborne Equipment”. In particular, the work presented here concerns with the Vibration environmental test. The standard prescribes a number of dynamic tests to be carried out on the AIS: random, shock and sine excitation tests have to be performed in order to study their effect on the parts composing the Anti-Icing System. The standard prescribes vibration levels at the attachment locations of the AIS to the wings' ribs.
Standard

GUIDANCE FOR AIRCRAFT ELECTRICAL POWER UTILIZATION AND TRANSIENT PROTECTION

1989-10-01
CURRENT
ARINC413A
This standard provides guidance to airframe manufacturers concerning the utilization of aircraft electrical power. This standard covers the description of basic power characteristics, and detailed guidance concerning transient protection, interference control, and equipment installation considerations.
Standard

ELECTRONIC CHRONOMETER

1998-11-30
CURRENT
ARINC731-3
This standard sets forth the characteristics for a self-contained Electronic Chronometer for installation in all types of commercial transport aircraft. It provides the following indications to the flight crew, Time of Day, Day and Month, Elapsed Time and Chronograph.
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

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

EMC Laboratory RF Radiated Emission Report for Passive Radio Frequency Identification (RFID) Tags

2008-06-18
HISTORICAL
AIR5747
This paper contains RF radiated emission and susceptibility data from passive Radio Frequency Identification (RFID) tags and readers operating at 13.56 MHz, 915 MHz, and 2.45 GHz. Laboratory test procedures incorporated the methods of RTCA DO-160D (test procedures for aviation electrical/electronic equipment) and DO-233 (test procedures for consumer portable electronic devices (PEDs)). Only one commercially available system was evaluated per established operating frequencies.
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

CABIN STANDARD ENCLOSURES

2018-11-20
CURRENT
ARINC836A
The purpose of this specification is to define standard cabin equipment enclosures and provisions for equipment attachment on monuments. This standard is intended to enable simpler installation and maintenance of cabin equipment, resulting in time and cost reduction.
Standard

User’s Manual for Certification of Aircraft Electrical/Electronic Systems for the Indirect Effects of Lightning

2001-08-01
HISTORICAL
ARP5415
This user's manual provides additional information and references relevant to identifying: (1) acceptance criteria for the indirect effects of lightning compliance approaches, (2) verification (analysis and test) methods including those associated with multiple stroke and multiple burst and (3) recommended design options to optimize needed system immunity to lightning indirect effects. Equipment hazards addressed include those due to the indirect effects on equipment mounted on the aircraft exterior and equipment located within the aircraft interior as well as all associated interconnecting wiring. This document has specific application toward those topics and subsystems addressed in ARP5413 but also provides additional guidelines in the application of those tests identified in DO-160/ED-14, Section 22.
Standard

User's Manual for Certification of Aircraft Electrical/Electronic Systems for the Indirect Effects of Lightning

2008-02-16
HISTORICAL
ARP5415A
This user's manual provides additional information and references relevant to identifying: (1) acceptance criteria for the indirect effects of lightning compliance approaches, (2) verification (analysis and test) methods including those associated with multiple stroke and multiple burst and (3) recommended design options to optimize needed system immunity to lightning indirect effects. Equipment hazards addressed include those due to the indirect effects on equipment mounted on the aircraft exterior and equipment located within the aircraft interior as well as all associated interconnecting wiring. This document has specific application toward those topics and subsystems addressed in ARP5413 but also provides additional guidelines in the application of those tests identified in DO-160/ED-14, Section 22.
Standard

Passive RFID Tags Intended for Aircraft Use

2006-12-14
HISTORICAL
AS5678
The scope of this document is to: 1 Provide a requirements document for RFID Tag Manufacturers to produce passive-only UHF RFID tags for the Aerospace industry. 2 Identify the minimum performance requirements specfic to the Passive UHF RFID Tag to be used on aircraft parts, to be accessed only during ground operations. 3 Specify the test requirements specific to Passive UHF RFID tags for airborne use, in addition to RTCA DO-160E compliance requirements separately called out in this document. 4 Identify existing standards applicable to Passive UHF RFID Tag. 5 Provide a certification standard for RFID tags which will use permanently-affixed installation on aircraft and aircraft parts.
Standard

CABIN EQUIPMENT INTERFACES PART 7 CABIN EQUIPMENT COOLING GENERAL SPECIFICATION

2013-06-24
CURRENT
ARINC628P7-2
Cabin equipment installations tend to impose loads on aircraft electrical power systems not envisioned in the original airplane design. This standard provides guidance on the design of future aircraft air conditioning and equipment cooling systems. It also describes the environment in which cabin systems, including In-Flight Entertainment equipment are expected to operate.
Standard

FIBER OPTIC ACTIVE DEVICE SPECIFICATION

2007-11-15
CURRENT
ARINC804-1
This document provides information on active devices used for avionics fiber optic applications. The main body of the document begins with the scope and rationale. It continues with a technology introduction to optoelectronic active devices and then a selection guide that would enable a system design engineer to use the documents in the Fiber Optics series to select or specify suitable optoelectronic active devices for avionics applications. The main document also includes environmental guidelines for active devices to be used in avionics applications. These are included as guidance for commercial aircraft use and are included with the caveat that the requirements of any particular aircraft platform or customer would supersede these generic guidelines.
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

PROJECTION VIDEO SYSTEM

1980-11-05
CURRENT
ARINC722
This standard sets forth design guidance and airplane interfaces for the development and installation of a PVS in commercial transport aircraft. Basic function of the PVS is to display projected television images to each passenger.
Standard

HANDHELD MICROPHONE AND BOOM MICROPHONE

2014-01-15
CURRENT
ARINC538C
This document describes the aircraft industry recommendations for a handheld microphone and boom microphone 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.
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.
Standard

ATTITUDE AND HEADING REFERENCE SYSTEM

1985-04-30
CURRENT
ARINC705-5
This standard describes the basic requirements for an AHRS specifically designed for installation in commercial transport aircraft. The AHRS is an attitude and heading sensor that provides outputs in digital form for guidance and display. The AHRS replaces the traditional vertical and directional gyros.
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