49.090 机上设备和仪器 标准查询与下载

ICAO 9861-2012 通用接入收发器（UAT）手册

Manual on the Universal Access Transceiver (UAT)

ICAO 9871-2012 模式服务和扩展电文的技术规定

Technical Provisions for Mode S Services and Extended Squitter

SAE AIR4276A-2011 设计中可靠性,可维护性和可支持性(RM&S)的电脑化

This document has been declared "Stabilized" and will no longer be subjected to periodic reviews for currency. Users are responsible for verifying references and continued suitability or technical requirements. New technology may exist. This Aerospace Information Report (AIR) is the primary vehicle for providing the survey results to industry and government. The Institute of Defense Analysis (IDA), has performed a study which concludes that computerized techniques must be developed to integrate RM&S into product design in order to permit design influence from inception throughout the product life cycle. This AIR addresses the DoD initiative for developing Computer Aided Acquisition and Logistic Support (CALS) and industry's role in its evolution. AIR 4276 provides the detailed results of an industry/government survey inquiring into the extent of computerization of RM&S into the design process. Background information describes the evolution of the survey and why it was developed. The results provide demographic information about the respondents, the existence and extent of their CALS policy and plans, the priority placed on each RM&S task, and the extent to which these tasks have been computerized into the design process. Recommendations based on the survey results are included

Computerization of Reliability, Maintainability and Supportability (RM&S) in Design

NF L52-410-105*NF EN 4641-105:2011 航天系列.光学电缆(覆层直径125 Šm).第105部分:标称外径为5.27 mm的半松包强化四绞芯结构62.5/125 μm GI光纤.产品标准.

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.

NF L00-460-005:2011 航天系列.模块开放式航空电子设备结构.第005部分:软件.

Aerospace series - Modular and Open Avionics Architectures - Part 005 : Software.

SAE ARP711B-2011 照明标志

This Aerospace Recommended Practice (ARP) covers the general design and performance characteristics of illuminated information signs for service in the passenger compartment of passenger transport aircraft. "Illuminated information sights" are lighted signs used to inform occupants of the passenger compartment. Signs may use symbols or letters to convey messages. This ARP does not apply to "EXIT" signs which are the subject of SAE ARP 503.

Illuminated Signs

SAE AS5382A-2011 航空航天用电缆和光缆

This standard covers jacketed single-fiber multimode and single-mode fiber optic cables for aerospace usage. The fiber optic cables covered by this standard shall be as described in the applicable specification sheets and shall be identified by the specfication sheet number and title.

Aerospace Cable, Fiber Optic

DIN EN 4641-301:2011 航空航天系列包层直径为125 Šm的光缆.第301部分:公称直径为1.8 mm紧密结构50/125 Šm GI光纤.产品标准;德文和英文版本EN 4641-301-2011

Aerospace series - Cables, optical 125Šm diameter cladding - Part 301: Tight structure, 50/125 Šm GI fibre, nominal 1.8 mm outside diameter - Product standard; German and English version EN 4641-301:2011

IEC 107/165/DTS:2011 IEC/TS 62668-1(第一版):工艺管理.假冒品预防.第1部分:避免使用假冒品,以及伪造和回收电子部件

IEC/TS 62668-1, Ed. 1: Process management - Counterfeit prevention - Part 1: Avoiding the use of counterfeit, fraudulent and recycled electronic components

DIN EN 4660-005:2011 航空航天系列.模块化和开放式航空电子系统结构.第005部分:软件;德文版本和英文版本EN 4660-005-2011

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; German and English version EN 4660-005:2011

NF L00-460-003:2011 航天系列.模块化开放式航空电子结构.第003部分:通讯/网络.

Aerospace series - Modular and Open Avionics Architectures - Part 003 : communications/network.

NF L00-460-004:2011 航天系列.模块化开放式航空电子结构.第004部分:包装.

Aerospace series - Modular and Open Avionics Architectures - Part 004: packaging.

SAE AS8045A-2011 水下定位装置最低性能标准 (声学)(自供电)

This SAE Aerospace Standard (AS) specifies minimum performance standards for Acoustic Underwater Locating Devices which are primarily intended for use with both fixed and rotary wing civil aircraft. This AS covers ULD utilized in finding flight data recorders, cockpit recorders or aircraft. Such ULDs are installed adjacent to the recorders in a manner that they are unlikely to become separated during crash conditions.

Minimum Performance Standard for Underwater Locating Devices (Acoustic) (Self-Powered)

DIN EN 4660-003:2011 航空航天系列.模块化和开放的航空电子设备架构.第003部分:通信/网络.德文和英文版本EN 4660-003-2011

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.

Aerospace series - Modular and Open Avionics Architectures - Part 003: Communications/Network; German and English version EN 4660-003:2011

DIN EN 4660-004:2011 航空和航天系列.模块化和开放式航电架构.第004部分:包装;德文版本和英文版本EN 4660-004-2011

The purpose of this standard is to establish uniform requirements for Packaging for the Common Functional Modules (CFM) within an Integrated Modular Avionic (IMA) system, as defined per ASAAC. It comprises the module physical properties and the Module Physical Interface (MPI) definitions together with guidelines for IMA rack and the operational environment.

Aerospace series - Modular and Open Avionics Architectures - Part 004: Packaging; German and English version EN 4660-004:2011

SAE AS6161-2011 机组舱眩光

Flight Compartment Glare

SAE AIR1168/5A-2011 气动热力学试验仪器和测量

Like the technologies to which it contributes, the science of instrumentation seems to be expanding to unlimited proportions. In considering instrumentation techniques, primary emphasis was given in this section to the fundamentals of pressure, temperature, and flow measurement. Accent was placed on common measurement methods, such as manometers, thermocouples, and head meters, rather than on difficult and specialized techniques. Icing, humidity, velocity, and other special measurements were touched on briefly. Many of the references cited were survey articles or texts containing excellent bibliographies to assist a more detailed study where required.

Aerothermodynamic Test Instrumentation and Measurement

DS/EN 4660-005:2011 航空航天系列 模块化和开放式航空电子结构 第005部分：软件

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.1.1 Software Architecture OverviewThe ASAAC Software Architecture is based on a three-layer stack as shown by a simplified Figure 2.Each layer is described in terms of it dependency/independency on both the aircraft system and the underlying hardware.1.2 Software Architectural ComponentsFigure 3 provides an overview of the software architectural components and software interfaces.1.2.1 Functional ApplicationsThe term """"Functional Applications"""" relates to all functions that handl

Aerospace series - Modular and Open Avionics Architectures - Part 005: Software

DIN EN 4660-002:2011 航空航天系列.模块化和开放式航空电子系统结构.第002部分:通用功能模块;德文版本和英文版本EN 4660-002-2011

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.

Aerospace series - Modular and Open Avionics Architectures - Part 002: Common Functional Modules; German and English version EN 4660-002:2011

DIN EN 4660-001:2011 航空航天系列.模块化和开放式航空电子系统结构.第001部分:结构;德文和英文版本EN 4660-004-2011

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; German and English version EN 4660-001:2011