Source: https://www.aviation-ia.com/product-categories/800-series
Timestamp: 2019-11-20 20:22:13
Document Index: 622843267

Matched Legal Cases: ['art 1', 'art 1', 'art 2', 'art 3', 'art 2', 'art 3', 'art 4', 'art 1', 'art 1', 'art 2', 'art 1', 'art 1', 'art 2', 'art 1', 'art 1', 'art 2', 'arts 1', 'arts 1', 'arts 1', 'art 1', 'art 2', 'art 2']

800 Series | SAE ITC
ARINC Standards - 800 Series
800P1 Cabin Connectors and Cables, Part 1, Description and Overview
This document is the first of a multi-part specification that will provide a catalog of cabin connec...tor and cables that may be used in ARINC Standard cabin systems, including In-Flight Entertainment. Part 1 describes connector and cable requirements and evaluation criteria for the interface components used in the integration of cabin systems. Future releases will define connectors, contacts, and termination methods in Part 2. Cables will be specified in Part 3.
800P2-1
800P2-1 Cabin Connectors and Cables, Part 2, Specification of Connectors, Contacts, and Backshells
This specification describes the general connectors, contacts, and backshells in their shape and ...characteristic for cabin systems for commercial aircrafts. ARINC 600, ARINC 404, and ARINC 801 connector specifications are published as independent standards.
800P3-1
800P3-1 Cabin Connectors and Cables, Part 3, Specification of Cables
This specification describes the general cable and wire characteristics recommended for use in cabin... systems for commercial aircraft. Supplement 1 adds new definitions of 26 AWG 2-pair (Quad), 4-pair (Oct) data cables, and copper-fiber optic hybrid composite cables.
800P4 Cabin Connectors and Cables, Part 4, Standard Test Methodology
ARINC 800 is the first industry standard intended for characterization of aviation-grade high-speed ...(Gbps) Ethernet links. The test methods are based on realistic representation of cabin networks. The notional cabling architecture is based on IFE seat distribution using multiple intermediate disconnects. Sequential testing is supported by building up number of connectors in the link. Test guidelines for mixed intermediate cable lengths are provided.
801-3 Fiber Optic Connectors
ARINC Specification 801 is intended to provide standardization of a fiber optic interconnect assembl...y, which is composed of a connector, fiber optic cable, and fiber optic termini for the air transport industry. The goal is to avoid the proliferation of different designs of connectors to serve the same functions on different aircraft models. This specification defines generic fiber optic connectors needed for commercial aircraft. The connector family is based around a standard terminus (fiber optic contact) design and associated cavity, which is used in all of the connector styles and arrangements. The standard terminus comes in variants for different cable types. All termini will fit the same cavities in the connectors and are intended to be interchangeable.
802-3 Fiber Optic Cables
This specification covers the performance requirements, dimensions, quality assurance criteria, t...est procedures, and cable codification for fiber optic cables suitable for use on commercial aircraft.
803-4 Fiber Optic Design Guidelines
The purpose of ARINC Report 803 is to provide design and implementation guidelines together with ...a selection guide, providing a fiber optic system design engineer with documentation to assess the design requirements for an aerospace fiber optic installation.
804-2 Fiber Optic Active Device Specification
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.
805-5 Fiber Optic Test Procedures
This document defines general practices for testing the physical layer of a fiber optic cable sys...tem. It is the intention of this document to outline proven practices for engineers and technicians engaged in testing and supporting fiber optic cable systems in aircraft.
806-6 Fiber Optic Installation and Maintenance
This document defines recommended general practices for the maintenance and restoration of fiber ...optic systems. It is the intention of this document to outline proven practices and general standards of workmanship for technicians engaged in fiber optic maintenance and repair.
807-4 Fiber Optic Training Requirements
This document is based upon the SAE ARP5602 document, A Guideline for Aerospace Platform Fiber Op...tic Training and Awareness Education. ARINC Report 807: Fiber Optic Training Requirements is a subset of the SAE ARP5602 document designed to meet the requirements of the commercial air transport industry. Certification to the SAE ARP5602 document fulfills the requirements of ARINC Report 807. This document defines recommended general practices for training requirements of aerospace fiber optic systems. It is the intention of this document to outline proven training practices and general standards of workmanship for technicians engaged in aerospace fiber optic manufacturing, installation, maintenance, and repair for the air transport industry. It is also recommended that management and purchasing personnel receive fundamental training to familiarize themselves with the requirements of aerospace fiber optics.
808-2 3GCN - Cabin Distribution System
This Specification defines general architectural philosophy and aircraft infrastructure for the prop...er use and interface of various cabin related IFE equipment. Compliance with ARINC Specification 808 allows each respective system to operate in concert when integrated with other relevant cabin equipment. ARINC Specification 808 defines standards for the aircraft 3rd Generation Cabin Network (3GCN), IFE Cabin Distribution System (CDS), wiring, connectors, power, identification codes, space envelopes, and mounting principles. Although some of these standards also apply to 3GCN wireless IFE systems, the overall 3GCN wireless IFE network specification is covered in ARINC Specification 820. The equipment itself is not a subject of this specification because it may be unique to the system manufacturer or marketplace-driven. Design guidelines are included for informational purposes as these guidelines impact the interfaces and installation of cabin equipment aboard the aircraft.
809-3 3GCN - Seat Distribution System
This specification defines general architectural philosophy and specific design guidance for the pro...per installation and interface of various cabin equipment within the seats. Consistency with this specification allows each component installed on the seat to operate in concert when integrated with other relevant cabin type equipment. Standard electrical and mechanical interfaces of the In- Flight Entertainment System (IFES) equipment for the 3rd Generation Cabin Network (3GCN) associated with the seat are defined. This equipment consists of the headphone jacks (HPJ), passenger control unit (PCU)/multi function handset (including the cord), seat video display (SVD), remote data outlet (RDO), integrated seat box (ISB) which includes the seat power box (SPB)/seat data box (SDB), remote power outlet (RPO), and in-seat cables. Appropriate definitions are also provided for other electrical devices associated with the seat control/position mechanism. The related seat control/position equipment consists of the seat control unit (SCU), seat automation controller (SAC), and seat actuator motor(s). The intent is to make this specification more useful for effectively integrating all the components of the seat.
810-5 Definition of Standard Interfaces for Galley Insert (GAIN) Equipment, Physical Interfaces
ARINC 810 defines galley equipment physical attachments, envelopes, connections, and qualification g...uidelines for interchangeable galley equipment. Supplement 5 defines a size 6 galley insert, intended for microwave oven installation and other equipment suited to this type of installation. Supplement 5 also clarifies reference dimensioning for all GAIN sizes defined by ARINC 810.
811 Commercial Aircraft Information Security Concepts of Operation and Process Framework
The purpose of this document is to facilitate an understanding of aircraft information security and ...to develop aircraft information security operational concepts. This common understanding is important since a number of subcommittees and working groups within the aeronautical industry are considering aircraft information security. This document also provides an aircraft information security process framework relating to airline operational needs that, when implemented by an airline and its suppliers, will enable the safe and secure dispatch of the aircraft in a timely manner. This framework facilitates development of cost-effective aircraft information security and provides a common language for understanding security needs.
812AP1-1
812AP1-1 Standard Data Interferes for Galley Insert (GAIN) Equipment, Part 1, CAN Communications
The purpose of this specification is to define the general Galley Insert (GAIN)standardization philo...sophy, provide comprehensive equipment interfaces, and disseminate the most current industry guidance. Part 1 covers the Controller Area Network (CAN) data interface attachments, envelopes, and data content to be considered between all galley equipment using a Galley Data Bus as described within this specification. This document is intended as the successor and replacement for ARINC Specification 812. This document contains significant improvements to CAN data interfaces.
812AP2
ARINC Specification 812AP2 Standard Data Interfaces for Galley Insert (GAIN) Equipment, Part 2, CAN Communications Verification and System Test Guidance
The purpose of this specification is to define test procedures to verify the implementation of the C...ontroller Area Network (CAN) interface for Galley Systems, as defined in ARINC Specification 812A, Part 1.
813 Embedded Interchange Format for Terrain Databases
This document defines an open encoding format for terrain databases. This format, when designed a...nd implemented, will enable a quick, economic, and efficient use of Terrain Databases (TerrDBs). However, since industry does not require applications to be standardized, data interpretation is not addressed in this document.
814 -1 Extensible Markup Language (XML) Encoding and Compression Standard
ARINC 814 defines an XML encoding and compression standard for aviation. It is based on the Open ...Geospatial Consortium (OGC) Binary XML document. Binary XML encoding is extended in a way that is both flexible and robust. Compression is added on top of the binary encoding. ARINC 814 is expected to be used with Aeronautical Databases, in particular, ARINC Specification 813: Embedded Interchange Format for Terrain Databases, ARINC Specification 815: Embedded Interchange Format for Obstacle Databases, and ARINC Specification 816: Embedded Interchange Format for Airport Mapping Database.
815 Embedded Interchange Format for Obstacle Datbases
This document defines an open encoding format for obstacle databases. This format, when desi...gned and implemented, will enable a quick, economic, and efficient use of Obstacle Databases (ObsDBs). However, since industry does not require applications to be standardized, data interpretation is not addressed in this document.
816 Embedded Interchange Format for Airport Mapping Database
This document defines an open encoding format for airport databases which are loaded in airborne sys...tems. This format, when designed and implemented, will enable a quick, economic, and efficient use of AMDB. However, since industry does not require applications to be standardized, data interpretation is not addressed in this document.
816-1 Embedded Interchange Format For Airport Mapping Database
816-2c1
816-2c1 Embedded Interchange Format For Airport Mapping Database
816-3 Embedded Interchange Format for Airport Mapping Database
817 Avionics Digital Video Bus, Low Data Rate - Uncompressed
This standard describes a digital video interface for use in all types of avionic equipment. This st...andard is an adaptation of SMPTE 259M, Serial Digital Interface, developed by the Society of Motion Picture and Television Engineers (SMPTE).
818-2 Avionics Digital Video Bus (ADVB) High Data Rate
This document defines digital video interface standards for all types of flight deck video. It repre...sents the consensus view of airlines, airframe manufacturers, avionic suppliers, and others who participated in the development of this standard. This document is based on ANSI Fibre Channel Audio Video (FC-AV) defined by ANSI INCITS 356-2002.
This document defines a secure Wi-Fi distribution network installed in the aircraft passenger cab...in for passenger and crew use. Carry-on Portable Electronic Devices (PEDs) such as smart phones, tablets, and laptops may use this network to access public internet services provided on the aircraft.
821 Aircraft Network Server System (NSS) Functional Definition
This document describes a collection of Aircraft Network Services (ANS) and Network Server System (N...SS) functions that are suitable for installation in all types of aircraft. It defines network services intended for both aircraft and cabin installations that will manage and maintain the NSS in a common way. This document describes methods for the aircraft to effectively communicate with ground-based information management systems.
822-1 Aircraft/Ground IP Communication
This specification describes the features and functionality desired of a communications link using I...nternet Protocols (IP) to provide services between a parked aircraft and the ground IP network infrastructure. This wireless communication link, commonly referred to as Gatelink, provides a connection between the airport and the on-board aircraft network. Gatelink will enable airlines to communicate in a secure manner with the aircraft network and appliances.
822A On-Ground Aircraft Wireless Communication
This specification describes the functionality and interfaces of an Internet Protocol (IP)-based wir...eless communications system between an aircraft on the ground and a ground-based network using Wireless Local Area Network (WLAN) and/or cellular radios and protocols. The ground-based network will be primarily used to provide connectivity to an airlines back office or to its back-end maintenance systems although other uses are also possible when there is a need to transfer data to or from the aircrafts applications while it is taxiing or parked. Gatelinkis the accepted industry term for this type of connection. This document is a major revision to ARINC Specification 822 released in 2008.
823P1
823P1 DataLink Security, Part 1 - ACARS Message Security
The purpose of this document is to provide an industry standard for ACARS Message Security (AMS), wh...ich permits ACARS datalink messages to be exchanged between aircraft and ground systems in a secure, authenticated manner using a uniform security framework. The security framework described herein is based on open international standards that are adapted to the ACARS datalink communications environment.
823P2 DataLink Security, Part 2 - Key Management
The purpose of this document is to provide recommended guidance and provisions for ACARS Message Sec...urity (AMS) key management. The key management framework described herein is based on open international standards that are adapted to the ACARS datalink communications environment.
824 Onboard Mobile Telephony System (OMTS)
This document provides standards necessary to achieve interchangeability between equipment providers.... Attachment 1 specifies an interconnection scheme by which aircraft can be wired to enable full interchangeability between OMTS products from different suppliers. Attachment 1 also specifies a minimum interface configuration which can be viewed as a desirable future implementation on new aircraft because of its potential for significant weight and space savings along with the possibility for less complex integration into the OEM production environment. The OMTS standard includes the physical interfaces, wiring, connectors, space envelopes, equipment chassis, unit co-location requirements, and power requirements. The basic functionality within each component of the OMTS is covered. Detailed functionality, protocols, and design parameters unique to each system supplier are not covered in this document. Design guidelines are included that impact the interfaces and installation of cabin equipment on board the aircraft.
825-4 General Standardization of CAN (Controller Area Network) Bus Protocol for Airborne Use
This document defines a Controller Area Network (CAN) interface for current and future commercial... aircraft applications. The latest version, Supplement 4, expands the document to include CAN Flexible Data rate also known as CAN FD. CAN FD has the potential to provide 4 Mbps of data transfer. Supplement 4 also introduces four new appendices on the topics of: ARINC 825 Compliance, Configuration of Bit Timing, Management Information Base (MIB) Counters, and CAN Bus Security Considerations.
826-1 Software Data Loader Using CAN Interface
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.
827 Electronic Distribution of Software by Crate (EDS Crate)
This standard describes the format for electronic distribution of aircraft software parts and other ...contents between aerospace business partners using a digital container referred to as an EDS crate. This EDS standard is intended to promote consistent, secure distribution of EDS content to any appropriate destination.
828-4 Electronic Flight Bag (EFB) Standard Interface
ARINC 828-4 defines a common Electronic Flight Bag (EFB) interface that can support EFB installation...s and the associated software applications. Supplement 4 defines two new connectors that will provide power and Ethernet to the EFB, thus enabling a smaller and lighter footprint for EFB installation provisions.
830 Aircraft/Ground Information Exchange (AGIE) Using Internet Protocol
The purpose of this document is to define a general purpose non-proprietary information exchange fra...mework and protocol for the conduct of Internet Protocol based message traffic between aircraft and airline ground infrastructure. This standard is motivated by the vision to substantially simplify information processing management for airlines by eliminating multiple dissimilar implementations with a single universal system and thereby establishing a more economical environment.
831 Electromagnetic Compatibility (EMC) Recommended Practice
This document addresses the construction and layout of equipment like line replaceable units (LRUs).... Cabin electronics and especially power electronics have in the past shown to be an issue with regard to EMC. It is not intended to give advice on aircraft installation.
832 Cabin Equipment Interfaces 4GCN Cabin Management and Entertainment System, Cabin Distribution System
ARINC Specification 832 defines standards for the aircraft 4th Generation Cabin Network (4GCN) Cabin... Distribution System (CDS) wiring, connectors, power, identification codes, space envelopes, and mounting principles. Design guidelines are included for informational purposes as these guidelines impact the interfaces and installation of cabin equipment aboard the aircraft.
833 Cabin Universal Wireless Distribution System (UWDS)
The document defines wireless communication medium intended for use in the cabin. It specifies the i...nterface between multiple wireless systems to a wireless distribution network. The intent is to reduce the installation and integration effort for multiple stand-alone wireless systems.
834-7 Aircraft Data Interface Function (ADIF)
This document defines an Aircraft Data Interface Function (ADIF) developed for aircraft installation...s that incorporate network components that are based on commercially available technologies. This document defines a set of protocols and services for the exchange of aircraft avionics data across aircraft networks. The goal is to provide a common set of services that may be used to access specific avionics parameters. The ADIF may be implemented as a generic network service, or it may be implemented as a dedicated service within an ARINC 759 Aircraft Interface Devices (AID) such as those used with an Electronic Flight Bag (EFB).
ARINC Report 835-1: Guidance for Security of Loadble Software Parts Using Digital Signatures
This document provides background and detailed technical information on existing methods to secure l...oadable software parts.
836 Cabin Standard Enclosures - Modular Rack Principle (MRP)
This document provides installation standards for cabin equipment and related mechanical enclosures.... It provides provisions for equipment attachment on overhead racks and monuments. The document provides a series of standard volumes and associated masses. Standardized packaging of cabin systems components is expected to yield simpler installation and maintenance of cabin equipment. This is expected to reduce the time and cost related to installing and maintaining cabin systems.
836A Cabin Standard Enclosures
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.
837 Design Guidelines for Aircraft Cabin Human Machine Interfaces
This document provides guidance for standard cabin systems control panel Graphical User Interfaces (...GUI) intended to improve the human-machine interface. The document defines control and indication elements for various cabin functions, including cabin lighting, cabin temperature, door status, and the like. Standardization of cabin system interfaces will enable airlines to have consistent cabin operations across their fleets and reduce cabin crew training costs.
ARINC Specification 838: Loadable Software Part Definition Format
This Specification defines: The syntax (simple generic grammar) and semantics (definition of the fie...lds, 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.
839 Function Definition of Airborne Manager of Air-Ground Interface Communications (MAGIC)
This standard defines an Internet Protocol (IP)-based communication management function for data com...munications called the Manager of Air/Ground Interface Communications (MAGIC). This standard recognizes that the number of available off-board communication links is expanding (e.g., broadband satellite, broadband terrestrial, Gatelink), and that each link may be provided by a different service provider. In addition, each link may be available to the aircraft in specific flight phases and in specific geographic locations. As the industry continues to increasingly embrace IP-based communications, there is reason to define an aircraft routing function that provides standardized access by all aircraft subnets to available communication links.
840-2 Electronic Flight Bag (EFB) Application Control Interface (ACI) Standard
The document defines a common software interface boundary between Electronic Flight Bag (EFB) applic...ation 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.
This document specifies how application to application navigation is managed on tablet EFB device...s. Topics include: inter-application navigation for users, blending of multiple applications into a single workflow, single data entry with data shared across applications.
841-3 Media Independent Aircraft Messaging (MIAM)
The purpose of this document is to provide an industry standard for Media Independent Aircraft Messa...ging (MIAM) which permits the exchange of a large volume of data over Aircraft Communications Addressing and Reporting System (ACARS) subnetworks or broadband Internet Protocol (IP) subnetworks.
842-2 Guidance for Usage of Digital Certificates
Newer generations of aircraft in production and use today are equipped with security applications... that rely on digital certificates. It is expected that future aircraft will use certificates for increasing numbers of applications. The purpose of this document is to provide operational guidance for key life-cycle management, which refers to the phases through which digital certificates and associated cryptographic keys progress, from creation through usage to retirement. The guidance is based on open international standards that are adapted to the aviation environment, recognizing that a typical commercial airplane has a long lifespan, its operational environment is highly complex and regulated, and multiple stakeholders operate ground-based systems that communicate with airplanes. Using a standardized and consistent key management approach, as proposed in this document, helps to reduce cost of design, implementation, and operation even across a heterogeneous fleet.
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.).
844P1
844P1 Guidance for Target Hardware Design, Part 1, Airborne High Speed Data Loader (ARINC Report 615-3)
ARINC Specification 844, prepared in two parts, defines the requirements of a Target Data Loader (TD...L) from the target hardware point of view.Both parts are based on two data loading standards: Part 1 clarifies ARINC Report 615-3: Airborne Computer High Speed Data Loader, Part 2 clarifies ARINC Report 615-4: Airborne Computer High Speed Data Loader. ARINC Report 615 was originally written from the data loader point of view.It is important that a target designer have a general understanding of the operation of a data loader in its modern implementation. Equally important is the need for data loader manufacturers to understand the standardized implementation requirements and supported subset of ARINC 615 features that are defined in ARINC 844, Parts 1 and 2. Therefore, ARINC Specification 844 is expected to provide value to both data loader and target implementers. The referenced standardized implementation requirements and supported subset of features defined in ARINC 844, Parts 1 and 2 provide the blueprint for data loader implementations. This standard also requires the use of ARINC Report 665 Supplement 2 or later, or ARINC Specification 838 formatted loadable software parts. ARINC Report 615-3 represents the majority of data loaders used in air transport data loading operations. ARINC Report 615-4 added some features and changed others that were found in ARINC Report 615-3. Although these two supplements of the ARINC Report 615 are very similar, they are, in essence, two separate standards. Therefore, ARINC Project Paper 844 is written in two parts to allow the reader to easily reference between the two ARINC 615 standards. ARINC Specification 844, Parts 1 and 2, is applicable to a specific supplement to ARINC Report 615. This standard requires the use of ARINC Report 665-2 or later, or ARINC Specification 838 formatted loadable software parts. The guidance found in: ARINC Specification 844, Part 1, is applicable to: ARINC Report 615-3. The guidance found in: ARINC Specification 844, Part 2, is applicable to: ARINC Report 615-4.
844P2
844P2 Guidance for Target Hardware Design, Part 2, Airborne High Speed Data Loader (ARINC Report 615-4)
845 Fiber Optic Expanded Beam Termini
This document defines a fiber optic Expanded Beam (EB) termini for the air transport industry. The g...oal is to avoid the proliferation of different designs of termini to serve the same functions on different aircraft models. This specification defines generic fiber optic EB termini needed for all types of aircraft.
846 Fiber Optic Ferrule, Mechanical Transfer
This specification covers the dimensions, performance, and quality assurance criteria for fiber o...ptic MT contacts, including performance test requirements and procedures, suitable for use on commercial aircraft.
ARINC Report 847 Product Development Guidance for Maintainability and Testability(PDMaT)
ARINC Report 847: Product Development Guidance for Maintainability and Testability (PDMaT) is intend...ed to be used as guidance to enhance the design of avionic equipment, with a focus on maintainability and testability characteristics. It is a separate and parallel standard to ARINC Report 607: Design Guidance for Avionic Equipment. This document does not represent the complete formula for successfully designing and manufacturing avionics equipment or system. It does present the vision of the airline community based on extensive experience gained through the use of such equipment. It is intended to provide information that would be useful in devising the necessary foundation to develop superior products through design philosophy as well as recommended practices in the design and conception of systems that should be beneficial not only to the equipment manufacturer designing avionic equipment, but also for the airframe manufacturers in incorporating avionic equipment into aircraft systems.
849 Data Loading Specifications for Aircraft Components
This document defines information required to load data into aircraft components while not installed... aboard an aircraft. The objective is to address all levels of data loading processes as related to component maintenance and repair within a shop environment. This new ARINC Standard defines the information required to load software and data to aircraft components when not installed aboard the aircraft. It addresses all forms of data as related to component maintenance and repair within a shop environment.
ARINC Report 852 Guidance for Security Event Logging in an IP Environment
This report sets forth guidance for IP-based onboard networks and systems residing in the Airline In...formation Services (AIS) and Passenger Information and Entertainment Services (PIES) Domains by establishing a common set of security related data elements and format(s) that are produced by aircraft systems, suitable for use by airline IT and/or avionic supplier analytical ground tools.