Refine Your Search

Search Results

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

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

AVIONCS APPLICATION SOFTWARE STANDARD INTERFACE PART 2 EXTENDED SERVICES

2015-08-21
CURRENT
ARINC653P2-3
As avionics software continues to evolve, so does ARINC Specification 653. ARINC 653 Part 2 specifies extensions (i.e., optional services) to the required Application Program Interfaces (APIs) described in ARINC 653 Part 1. Supplement 3 adds optional multicore services capabilities.
Standard

AVIONICS APPLICATION SOFTWARE STANDARD INTERFACE PART 1 REQUIRED SERVICES

2015-08-21
CURRENT
ARINC653P1-4
This standard defines a general-purpose Application/Executive (APEX) software interface between the Operating System of an avionics computer and the application software. The interface requirements between the application software and operating system services are defined in a manner that enables the application software to control the scheduling, communication, and status of internal processing elements. Supplement 4 adds multicore processor service capabilities.
Standard

AVIONICS APPLICATION SOFTWARE STANDARD INTERFACE PART 0 OVERVIEW OF ARINC 653

2015-08-03
CURRENT
ARINC653P0-1
This document provides an overview of the entire set of documents collectively referred to as ARINC 653. As this set of documents evolves, Supplements to Parts 1 through 5 will be made more consistent with Part 0 in conjunction with the technical changes expected to be made in the evolution of ARINC 653. A summary of the ARINC 653 documents follows: Part 0 - Overview of ARINC 653, Part 1 - Required Services, Part 2 - Extended Services, Part 3 - Conformity Test Specification, Part 4 - Subset Services, and Part 5 - Core Software Required Capabilities. Supplement 1 reflects the introduction of multicore processor support in Parts 1 and 2.
Standard

LOGICAL SOFTWARE PART PACKAGING FOR TRANSPORT

2015-07-31
CURRENT
ARINC641
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

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

AVIONICS APPLICATION SOFTWARE STANDARD INTERFACE PART 5 CORE SOFTWARE RECOMMENDED CAPABILITIES

2014-12-01
CURRENT
ARINC653P5
The objective of this part is to define additional ARINC 653 core software capabilities to ease integration on a variety of Integrated Modular Avionics (IMA) hardware platforms by allowing platform suppliers to extend and customize it for use with their unique hardware platform. The objective of Part 5 is to define additional recommended capabilities when implementing ARINC 653 core software using a Commercial off the Shelf (COTS) ARINC 653 Operating System (O/S).
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

SOFTWARE DATA LOADER USING CAN INTERFACE

2013-12-20
CURRENT
ARINC826-1
The purpose of the standard is to provide a simple and efficient protocol for loading software parts to line replaceable units (LRUs) on a CAN bus, as an alternative to ARINC Report 615A or ARINC Report 615. It is not intended to become the only possible CAN software loading alternative. It is intended for those avionics devices that are software loadable.
Standard

AVIONICS APPLICATION SOFTWARE STANDARD INTERFACE PART 4-SUBSET SERVICES

2012-06-28
CURRENT
ARINC653P4
ARINC Specification 653 Part 4 was prepared to support controllers and relatively simple avionics. Part 4 is true subset of services specified in ARINC 653 Part 1. In the Subset Services, partition scheduling is restricted to only one partition time window within the partition's period. This simplifies the management of process release points. Process management uses a dual-process model with at most two processes within a partition, for example, foreground and background.
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

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

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.
Standard

GUIDANCE FOR USE OF AVIONICS EQUIPMENT AND SOFTWARE IN SIMULATORS

1999-02-15
CURRENT
ARINC610A-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).
X