49.090 机上设备和仪器 标准查询与下载
共找到 1494 条与 机上设备和仪器 相关的标准，共 100 页
Data Link Services (DLS) System - Community Specification for application under the Single European Sky Interoperability Regulation EC 552/2004, Requirements for ground constituents and system testing (Endorsement of the English version EN 303214 V1.1.1 (
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- 49.090
- CCS
- V45
- 发布
- 2011-07
- 实施
Aerospace series - Modular and Open Avionics Architectures - Part 004: Packaging
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- 49.090
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- 发布
- 2011-06-30
- 实施
- 2011-06-30
Aerospace series - Modular and Open Avionics Architectures - Part 002: Common Functional Modules
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- 49.090
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- 2011-06-30
- 实施
- 2011-06-30
Aerospace series - Modular and Open Avionics Architectures - Part 005: Software
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- 49.090
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- 2011-06-30
- 实施
- 2011-06-30
Aerospace series - Modular and Open Avionics Architectures - Part 003: Communications/Network
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- 49.090
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- 2011-06-30
- 实施
- 2011-06-30
Aerospace series - Modular and Open Avionics Architectures - Part 001: Architecture
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- 49.090
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- 2011-06-30
- 实施
- 2011-06-30
This SAE Aerospace Standard (AS) specifies minimum performance standards for all types of Electronic Displays and Electronic Display Systems that are intended for use in the flight deck by the flightcrew in all 14 CFR Part 23, 25, 27, and 29 aircraft. The requirements and recommendations in this document are intended to apply to all installed electronic displays and electronic display systems within the flight deck, regardless of intended function, criticality, or location within the flight deck, but may also be used for non-installed electronic displays. This document provides baseline requirements and recommendations (see section 2.3 for definitions of "shall" and "should"). This document primarily addresses hardware requirements, such as electrical, mechanical, optical, and environmental. It does not address system specific functions. It does not contain an exhaustive or comprehensive list of requirements for specific systems or functions, such as TCAS, ADS-B, GPS, weather, or shared display considerations (e.g., when should alerts be inhibited on a display system that simultaneously depicts navigation data integrated with terrain data or traffic alerting). This document is intended to be used in combination with other guidance material contained in current system specific, TSOs, Advisory Circulars (ACs), and other Federal Aviation Administration (FAA)-approved guidance material.
Minimum Performance Standard for Airborne Multipurpose Electronic Displays
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- 49.090
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- V45
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- 2011-06-27
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This product standard specifies the general characteristics, conditions for qualification, acceptance and quality assurance for a fibre optic cable with two 62,5/125 µm graded index fibre cores, 4,95 mm nominal outside diameter and of semi-loose construction. The basic construction is a pair of the cables defined in EN 4641-102 with added sheaths for ruggedized usages.
Aerospace series - Cables, optical 125 Šm diameter cladding - Part 104: Semi-loose, ruggedized duplex construction 62,5/125 Šm GI fibre nominal, 4,95 mm outside diameter - Product standard; German and English version EN 4641-104:2010
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- 49.090
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- M33;V25
- 发布
- 2011-06
- 实施
This product standard specifies the general characteristics, conditions for qualification, acceptance and quality assurance for a fibre optic cable with four 62,5/125 µm Graded Index fibre cores, 5,72 mm nominal outside diameter and of semi loose construction. The basic construction is a pair of the cables defined in with added sheaths for ruggedized usages.
Aerospace series - Cables, optical 125 Šm diameter cladding - Part 105: Semi-loose, ruggedized quadraxial construction 62,5/125 Šm GI fibre nominal, 5,72 mm outside diameter - Product standard; German and English version EN 4641-105:2010
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- 49.090
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- V25
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- 2011-06
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The purpose of this European Standard is to establish uniform requirements for design and development of software architecture for modular avionics systems as defined per ASAAC.
Aerospace series. Modular and open avionics architectures. Software
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- 49.090
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- V41
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- 2011-05-31
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- 2011-05-31
The purpose of this European Standard is to establish uniform requirements for design and development of software architecture for modular avionics systems as defined per ASAAC.
Aerospace series - Modular and Open Avionics Architectures - Part 005: Software
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- 49.090
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- 发布
- 2011-05-01
- 实施
Advanced Surface Movement Guidance and Control System (A-SMGCS) - Part 4: Community Specification for application under the Single European Sky Interoperability Regulation EC 552/2004 for a deployed non-cooperative sensor including its interfaces - Sub-pa
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- 49.090
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- V41
- 发布
- 2011-04
- 实施
Advanced Surface Movement Guidance and Control System (A-SMGCS) - Part 3: Community Specification for application under the Single European Sky Interoperability Regulation EC 552/2004 for a deployed cooperative sensor including its interfaces (Endorsement
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- 49.090
- CCS
- V41
- 发布
- 2011-04
- 实施
Advanced Surface Movement Guidance and Control System (A-SMGCS) - Part 4: Community Specification for application under the Single European Sky Interoperability Regulation EC 552/2004 for a deployed non-cooperative sensor including its interfaces - Sub-pa
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- 49.090
- CCS
- V45
- 发布
- 2011-04
- 实施
Advanced Surface Movement Guidance and Control System (A-SMGCS) - Part 2: Community Specification for application under the Single European Sky Interoperability Regulation EC 552/2004 for A-SMGCS Level 2 including external interfaces (Endorsement of the E
- ICS
- 49.090
- CCS
- V41
- 发布
- 2011-04
- 实施
Advanced Surface Movement Guidance and Control System (A-SMGCS) - Part 1: Community Specification for application under the Single European Sky Interoperability Regulation EC 552/2004 for A-SMGCS Level 1 including external interfaces (Endorsement of the E
- ICS
- 49.090
- CCS
- V45
- 发布
- 2011-04
- 实施
The purpose of this standard is to establish uniform requirements for the architecture for Integrated Modular Avionic (IMA) systems as defined by the ASAAC Programme. The IMA architecture can be built by using common components. These components are specified in separate standards. Ways of using these components are described in a set of guidelines. This document gives references to these Standards and Guidelines as well as a short introduction to IMA.
Aerospace series. Modular and open avionics architectures. Architecture
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- 49.090
- CCS
- V41
- 发布
- 2011-03-31
- 实施
- 2011-03-31
This standard defines the functionality and principle interfaces for the Common Functional Module (CFM) to ensure the interoperability of Common Functional Modules and provides design guidelines to assist in implementation of such a CFM. It is one of a set of standards that define an ASAAC (Allied Standard Avionics Architecture Council) Integrated Modular Avionics System. This definition of interfaces and functionality allows a CFM design that is interoperable with all other CFM to this standard, that is technology transparent, that is open to a multi-vendor market and that can make the best use of COTS technologies. Although the physical organisation and implementation of a CFM should remain the manufacturer’s choice, in accordance with the best use of the current technology, it is necessary to define a structure for each CFM in order to achieve a logical definition of the CFM with a defined functionality. This definition includes: ? The Generic CFM, which defines the generic functionality applicable to the complete set of CFMs. The generic functionality is defined in 4.1. ? The processing capability, which defines the unique functionality associated with each CFM type within the set. This functionality is defined in 4.3. ? The logical and physical interfaces that enable CFMs to be interoperable and interchangeable, these are defined in Clause 6. ? The functionality required by a CFM to support the operation of the System is defined in Clause 6.
Aerospace series. Modular and open avionics architectures. Common functional modules
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- 49.090
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- V41
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- 2011-03-31
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- 2011-03-31
This standard details the functionality and principle interfaces for the ASAAC (Allied Standard Avionics Architecture Council) Network to ensure the interoperability of Common Functional Modules and design guidelines to assist in implementation of such a network. It is one of a set of standards that define an ASAAC Integrated Modular Avionics (IMA) System. The purpose of this standard is to establish by means of well defined interfaces and functionality, a network design that is technology transparent, that is open to a multi-vendor market and that can make the best use of Commercial Off The Shelf (COTS) technologies. Therefore, the associated data communication network topology, protocols and technologies are not identified in this document. For these items the document identifies the issues that should be considered when defining a specific network implementation to support the ASAAC architecture and provides guidelines to assist. Although the physical organisation and implementation of the network shall remain the System Designers choice, in accordance with the best use of the current technology, it is necessary to define interfaces and parameter sets in order to achieve a logical definition of the network with a defined functionality. This definition includes: ? The generic functionality applicable to all networks. ? The logical interfaces to the Operating System and Module Support Layers. ? The physical interfaces to the Common Functional Modules (CFM). The ASAAC Standards are intended to be independent of specific technologies, including network technologies. This document identifies the principle interfaces for the Network, in Clause 4, and where appropriate, provides requirements on network parameters to be defined. The interfaces relevant to the network are the Module Support Layer to Operating System (MOS), Module Physical Interface (MPI) and Module Logical Interface (MLI). The MOS and MPI are generically defined elsewhere (Standards for Software see EN 4660-005 and Packaging see EN 4660-004). The MLI is clearly a function of the selected network. The MOS and MPI definitions are generic and will need to be supported by network specific information. There is no network-dependent information in the Software or Packaging standards. So a future network specification will not only define the particular MLI, but will also need to define the specific aspects of the MPI, topologies, system properties etc.
Aerospace series. Modular and open avionics architectures. Communications/Network
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- 49.090
- CCS
- V41
- 发布
- 2011-03-31
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- 2011-03-31
The purpose of this standard is to establish uniform requirements for the architecture for Integrated Modular Avionic (IMA) systems as defined by the ASAAC Programme.The IMA architecture can be built by using common components. These components are specified in separate standards. Ways of using these components are described in a set of guidelines. This document gives references to these Standards and Guidelines as well as a short introduction to IMA.
Aerospace series - Modular and Open Avionics Architectures - Part 001: Architecture
- ICS
- 49.090
- CCS
- 发布
- 2011-03-25
- 实施
- 2011-03-25
