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Standard

DESIGN GUIDANCE FOR ONBOARD MAINTENANCE SYSTEM

1993-08-30
CURRENT
ARIR624-1
Avionics maintenance practices continue to improve through On-Board Maintenance System (OMS) recording. This standard defines the OMS which incorporates fault monitoring fault detection, BITE, and airplane condition monitoring system.
Standard

SOFTWARE DATA LOADER USING ETHERNET INTERFACE

2007-06-30
CURRENT
ARIR615A-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

PORTABLE MAINTENANCE ACCESS TERMINAL (PMAT)

1993-05-25
CURRENT
ARIR644
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

RESOLUTION OF INSERVICE ANOMALIES THROUGH ASAPP

1997-09-30
CURRENT
ARIR640
Defines a generalized process by which anomalies in aircraft systems can be detected. This process is intended to improve timely isolation and resolution of those anomalies. The objective is to reduce costs to the airlines, airframe manufacturers and aircraft systems suppliers by removing anomalous behavior from aircraft systems in a timely manner.
Standard

PORTABLE MULTI-PURPOSE ACCESS TERMINAL (PMAT)

1996-08-25
CURRENT
ARIR644A
The PMAT is intended for use in the airplane maintenance environment allowing remote access to onboard systems. This standard describes the aircraft interface, operational capabilities and standards necessary to achieve interoperability with onboard systems, stand-alone internal or external mass memory devices, and ARINC standard printers.
Standard

DESIGN GUIDANCE FOR INTEGRATED MODULAR AVIONICS

1997-11-07
CURRENT
ARIR651-1
This standard is a systems design guide for IMA. It provides guidance for the design and implementation of avionics equipment for new airplanes and retrofit installations. It is conceptual in nature and covers broad subjects of operational objectives, fault tolerance, hardware components, software design and certification issues.
Standard

ARINC REPORT 634 HF DATA LINK SYSTEM DESIGN GUIDANCE MATERIAL

1996-08-30
CURRENT
ARIR634
This Report provides the reader with material to enhance the understanding of high frequency data link. This standard provides a snapshot of guidance material used in the development of ARINC 753, HF Data Link System, and ARINC 635, HF Data Link Protocols.
Standard

GUIDANCE FOR USE OF AVIONICS EQUIPMENT AND SOFTWARE IN SIMULATORS

1999-02-15
CURRENT
ARIR610A-1
This standard preserves all of the technical concepts of ARINC 610. ARINC 610A encompasses the lessons learned since ARINC 610 was issued, provides additional information defining each simulator function and the responses required by each type, and creates guidance information relevant to Integrated Modular Avionics (IMA).
Standard

GUIDANCE FOR USE OF AVIONICS EQUIPMENT AND SOFTWARE IN SIMULATORS

2001-12-12
CURRENT
ARIR610B
Guidance for the Use of Avionics and Software in Simulators is intended to simplify the additional functions required of avionics equipment used in simulators. Recommended simulator functions, data base harmonization, use of snapshot functions, and a new training scenario are included. The guidelines contained in the draft are expected to reduce the cost to design and install avionics equipment in simulators.
Standard

BITE GLOSSARY

1986-12-18
CURRENT
ARIR612
The purpose of this standard is to provide a source of definitions of terms and acronyms commonly used in the air transport maintenance community for test and evaluation with an emphasis on terms applicable to BITE.
Standard

GUIDANCE FOR THE DESIGN AND INSTALLATION OF FUEL QUANTITY SYSTEMS

1999-01-25
CURRENT
ARIR611-1
This standard defines accuracy and reliability targets for fuel quantity measuring systems installed on commercial aircraft. It describes fuel quantity system components and design techniques that will contribute to safe and reliable operation. System design goals and installation practices are described. A report of a worldwide fuel survey is included.
Standard

STANDARD FIRMWARE LOADER FOR AVIONICS SHOPS

1989-09-30
CURRENT
ARIR614
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

GUIDE FOR USING THE ADA PROGRAMMING LANGUAGE IN AVIONIC SYSTEMS

1998-01-04
CURRENT
ARIR613
In 1986 the airlines selected Ada as the high-order development language for avionics. ARINC 613 describes the Ada domain most suited for avionics software development. The standard provides valuable guidance to Ada compiler developers and Ada programmers.
Standard

AIRBORNE COMPUTER HIGH SPEED DATA LOADER

2002-05-06
CURRENT
ARIR615-4_ER2
This standard provides general and specific guidance for the development of a Portable Data Loader (PDL) for carry-on application and an Airborne Data Loader (ADL) for on-board the airplane. It specifies use of a 3.5 inch floppy disk to upload and download of data and operational programs using an ARINC 429 data bus connected to avionics computers.
Standard

AIRBORNE COMPUTER HIGH SPEED DATA LOADER

1992-08-15
CURRENT
ARIR615-3
This standard provides general and specific guidance for the development of a Portable Data Loader (PDL) for carry-on application and an Airborne Data Loader (ADL) for on-board the airplane. It specifies use of a 3.5 inch floppy disk to upload and download of data and operational programs using an ARINC 429 data bus connected to avionics computers.
Standard

USERS GUIDE FOR ARINC 616 AVIONICS SUBSET OF ATLAS

2017-11-29
CURRENT
ARIR605
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

GUIDANCE FOR ELECTROSTATIC SENSITIVE DEVICE UTILIZATION AND PROTECTION

2004-11-12
CURRENT
ARIR606A
This document provides guidance for using industry standards for developing an ESD control program tailored to meet specific user requirements. In addition, it provides uniform guidance for maintenance facilities based on industry ESD standards, and therefore should be accepted throughout the air transport industry. This document is not a stand-alone document - it is intended to be used with the referenced international industry standards.
Standard

GUIDANCE FOR ELECTROSTATIC SENSITIVE DEVICE UTILIZATION AND PROTECTION

1992-01-01
CURRENT
ARIR606-1
The primary goal of this standard is to describe the nature of Electrostatic Discharge (ESD) and its effects on digital avionics equipment. It provides information concerning methods to protect against ESD damage which could originate in many different ways.
Standard

GUIDANCE FOR DESIGN AND USE OF BUILT-IN TEST EQUIPMENT

1988-10-31
CURRENT
ARIR604-1
The primary purpose of BITE is to assist maintenance personnel in the proper maintenance of avionics systems in a cost-effective manner. A description of a Centralized Fault Display System (CFDS) is included in this standard. The CFDS accumulates fault data, presents this data to a maintenance operator, and assists troubleshooting by performing diagnostic tests and performing verification testing after installation of a replacement unit.
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