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Standard

LOGICAL SOFTWARE PART PACKAGING FOR TRANSPORT

2020-11-16
CURRENT
ARINC641-1
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

BITE GLOSSARY

1986-12-18
CURRENT
ARINC612
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

AIRCRAFT SOFTWARE COMMON CONFIGURATION REPORTING

2019-08-13
CURRENT
ARINC843-1
This standard defines a common configuration report format that can be retrieved from an aircraft for use by ground tools and maintenance personnel. Reports will be generated in Extensible Markup Language (XML) format and structured as defined by this document. Several optional elements and attributes are defined to allow flexibility for a given report. This standard provides aircraft manufacturers, regulatory agencies, and airlines a format standard for aircraft configuration reporting, and facilitates automated comparison of configuration data reports (e.g., authorized versus as flying, etc.).
Standard

AVIONICS APPLICATION SOFTWARE STANDARD INTERFACE PART 3A CONFORMITY TEST SPECIFICATIONS FOR ARINC 653 REQUIRED SERVICES

2019-07-18
CURRENT
ARINC653P3A-1C1
ARINC 653, Part 3A is the Compliance Test Specification for ARINC 653 Required Services presently defined in ARINC 653 Part 1. The document specifies a set of stimuli and the expected responses. Future work on the ARINC 653 document set includes an effort to define Operating System services for multi-core processor environments. The Compliance Test Specification is expected to be updated in step with ARINC 653, Part 1.
Standard

MULTIPLE-INPUT COCKPIT PRINTER

1998-06-01
CURRENT
ARINC740-1
This standard describes the form, fit, function and interfaces of an airborne printer capable of communicating with multiple systems one at a time. The printer contains the circuitry for acquisition, buffering and processing of coded alphanumeric messages for print-out on half-width paper.
Standard

NAVIGATION SYSTEMS DATABASE

2011-12-05
CURRENT
ARINC424-20
THE CURRENT VERSION OF THIS DOCUMENT IS 424-21. THIS PREVIOUS VERSION IS AVAILABLE FOR YOUR CONVENIENCE. This standard provides a data base comprising standards used for the preparation of a navigation system data base. This data may be used with the operational flight software in a wide range of navigational equipment.
Standard

NAVIGATION SYSTEMS DATABASE

2005-11-23
CURRENT
ARINC424-18
THE CURRENT VERSION OF THIS DOCUMENT IS 424-21. THIS PREVIOUS VERSION IS AVAILABLE FOR YOUR CONVENIENCE. This standard provides a data base comprising standards used for the preparation of a navigation system data base. This data may be used with the operational flight software in a wide range of navigational equipment.
Standard

NAVIGATION SYSTEM DATA BASE

2004-08-31
CURRENT
ARINC424-17
THE CURRENT VERSION OF THIS DOCUMENT IS 424-21. THIS PREVIOUS VERSION IS AVAILABLE FOR YOUR CONVENIENCE. This standard provides a data base comprising standards used for the preparation of a navigation system data base. This data may be used with the operational flight software in a wide range of navigational equipment.
Standard

NAVIGATION SYSTEM DATA BASE

2002-08-30
CURRENT
ARINC424-16
THE CURRENT VERSION OF THIS DOCUMENT IS 424-21. THIS PREVIOUS VERSION IS AVAILABLE FOR YOUR CONVENIENCE. This standard provides a data base comprising standards used for the preparation of a navigation system data base. This data may be used with the operational flight software in a wide range of navigational equipment.
Standard

AVIONICS APPLICATION SOFTWARE STANDARD INTERFACE PART 3A CONFORMITY TEST SPECIFICATIONS FOR ARINC 653 REQUIRED SERVICES

2018-09-07
CURRENT
ARINC653P3A-1
ARINC 653, Part 3A is the Compliance Test Specification for ARINC 653 Required Services presently defined in ARINC 653 Part 1. The document specifies a set of stimuli and the expected responses. Future work on the ARINC 653 document set includes an effort to define Operating System services for multi-core processor environments. The Compliance Test Specification is expected to be updated in step with ARINC 653, Part 1.
Standard

AVIONICS APPLICATION SOFTWARE STANDARD INTERFACE PART 3B CONFORMITY TEST SPECIFICATIONS FOR ARINC 653 EXTENDED SERVICES

2018-09-07
CURRENT
ARINC653P3B
ARINC 653, Part 3B is the Compliance Test Specification for ARINC 653 Extended Services presently defined in ARINC 653 Part 2. The document specifies a set of stimuli and the expected responses. Future work on the ARINC 653 document set includes an effort to define Operating System services for multi-core processor environments. The Compliance Test Specification is expected to be updated in step with ARINC 653, Part 2.
Standard

AIRCRAFT SOFTWARE COMMON CONFIGURATION REPORTING

2015-07-31
CURRENT
ARINC843
This standard defines a common configuration report format that can be retrieved from an aircraft for use by ground tools and maintenance personnel. Reports will be generated in Extensible Markup Language (XML) format and structured as defined by this document. Several optional elements and attributes are defined to allow flexibility for a given report. This standard provides aircraft manufacturers, regulatory agencies, and airlines a format standard for aircraft configuration reporting, and facilitates automated comparison of configuration data reports (e.g., authorized versus as flying, etc.).
Standard

ELECTRONIC FLIGHT BAG (EFB) APPLICATION CONTROL INTERFACE (ACI) STANDARD

2012-11-20
CURRENT
ARINC840-2
The document defines a common software interface boundary between Electronic Flight Bag (EFB) application software and the EFB platform. The standard interface will allow EFB applications to be launched and controlled independent of other EFB applications. Supplement 2 provides enhancements to the original specification, including a data repository service where common flight data parameters can be used among several applications running on the EFB. A virtual keyboard and line printer service is also included.
Standard

LOADABLE SOFTWARE PART DEFINITION FORMAT

2014-01-02
CURRENT
ARINC838
This Specification defines: The syntax (simple generic grammar) and semantics (definition of the fields, such as name, type, constraints and meaning) of the ARINC 838 Loadable Software Part Definition Format in Section 3. The definition of XML notation of the grammar in Section 4. The definition of binary notation of the grammar in Section 5.
Standard

FLIGHT MANAGEMENT COMPUTER SYSTEM

1994-06-01
CURRENT
ARINC702-6
This standard defines a FMCS for installation in commercial transport aircraft. The FMCS provides performance data, performance computations, fuel management functions, and navigation and guidance to a desired flight plan.
Standard

AIRCRAFT DATA NETWORK, PART 2 - ETHERNET PHYSICAL AND DATA LINK LAYER SPECIFICATION

2009-01-16
CURRENT
ARINC664P2-2
This specification provides Ethernet physical parameters and data link layer specifications for use in a commercial aircraft environment. This specification provides general and specific guidelines for the use of IEEE 802.3 compliant Ethernet, 2000 edition. Physical layer and Medium Access Control (MAC) sub-layers are expected to comply with the Open System Interconnection (OSI) Reference Model to enable maximal utilization of off-the-shelf components, both hardware and software, for aviation use. The Ethernet Physical layer specification defines the electrical and optical parameters for the 10BASE-T, 100BASE-TX, and 100BASE-FX Ethernet implementations. This specification references ARINC Specification 600: Air Transport Avionics Equipment Interfaces for definition of copper-based implementations of the Ethernet Physical layer.
Standard

LOADABLE SOFTWARE STANDARDS

2016-07-14
CURRENT
ARINC665-4
This document defines the aircraft industry's standards for Loadable Software Parts (LSPs) and Media Set Parts (MSPs). It describes the common principles and rules to be applied to any part of a data load system to ensure compatibility and inter-operability. It includes part numbering, content, labeling, and formatting of an LSP, and a Media Set containing LSPs.
Standard

LOADABLE SOFTWARE STANDARDS

2002-08-30
CURRENT
ARINC665-2
This is a superseded version. ----------------- This standard defines standards for loadable software parts and software transport media. It describes the principles and rules to be applied to any part of a data load system, to ensure compatibility and interoperability. It includes part numbering, content, labeling and formatting of loadable software parts and software transport media.
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