49.090 机上设备和仪器 标准查询与下载

23/30469886 DC BS EN 4869-103 航空航天系列 扩束端子 EN 3645 标准腔体中的光纤非物理接触 第 103 部分 多模公端子尺寸 12 技术规格

BS EN 4869-103. Aerospace series. Expanded beam termini, fibre optic non-physical contact in EN 3645 standard cavities - Part 103. Multimode male termini size 12. Technical specification

23/30469883 DC BS EN 4869-102 航空航天系列 扩束端子 EN 3645 标准腔体中的光纤非物理接触 第 102 部分 多模母端子尺寸 16 技术规格

BS EN 4869-102. Aerospace series. Expanded beam termini, fibre optic non-physical contact in EN 3645 standard cavities - Part 102. Multimode female termini size 16. Technical specification

23/30469880 DC BS EN 4869-101 航空航天系列 扩束端子 EN 3645 标准腔中的光纤非物理接触 第 101 部分 公端子尺寸 16 技术规格

BS EN 4869-101. Aerospace series. Expanded beam termini, fibre optic non-physical contact in EN 3645 standard cavities - Part 101. Male termini size 16. Technical specification

23/30469889 DC BS EN 4869-104 航空航天系列 扩束端子 EN 3645 标准腔体中的光纤非物理接触 第 104 部分 多模母端子尺寸 12 技术规格

BS EN 4869-104. Aerospace series. Expanded beam termini, fibre optic non-physical contact in EN 3645 standard cavities - Part 104. Multimode female termini size 12. Technical specification

23/30469877 DC BS EN 4869-001 航空航天系列 扩束终端 EN 3645 标准腔体中的光纤非物理接触 第 001 部分 技术规格

BS EN 4869-001. Aerospace series. Expanded beam termini, fibre optic non-physical contact in EN 3645 standard cavities - Part 001. Technical specification

22/30455569 DC BS EN 4641-301 航空航天系列 光缆 直径 125 μm 包层 第 301 部分 紧密结构 50/125 μm GI 光纤标称 1.8 mm 外径 产品标准

BS EN 4641-301 Aerospace series. Cables, optical 125 μm diameter cladding - Part 301. Tight structure 50/125 μm GI, fibre nominal 1,8 mm, outside diameter - Product standard

22/30453790 DC BS EN 3745-801 航空航天系列 光纤和电缆、光学、飞机用途 测试方法 第 801 部分：压缩下的纤维运动

BS EN 3745-801. Aerospace series. Fibres and cables, optical, aircraft use. Test methods - Part 801. Fibre movement under compression

T/CSAA 19-2022 无人机L/U双频数据链规范

4 要求　 4.1 组成　 4.2 功能　 4.3 性能　 4.4 环境适应性　 4.5 可靠性　 4.6 维修性　 4.7 测试性　 4.8 设计和结构　 4.9 保障性　 4.10 安全性　 4.11 电磁兼容性　 4.12 寿命　 4.13 接口　 4.14 供电兼容性　 4.15 功耗　 4.16 标志和代号　 4.17 尺寸　 4.18 重量　 4.19 外观质量　 4.20 互换性　 5 质量保证规定　 5.1 检验分类　 5.2 检验条件　 5.3 鉴定检验　 5.4 质量一致性检验　 5.5 检验方法　 5.6　L/U双频数据链终端测试连接图与测试连接图中各测试点含义　 6 交货准备　 6.1 防护包装　 6.2 装箱　 6.3 运输和贮存　 7 说明事项　 7.1 预定用途　 7.2 订购文件应明确的内容　

Specification of L/U dual frequency Data Link for UAV

T/CSAA 20-2022 无人机L/U双频数据链路 性能试验方法

4 试验目的　 5 试验条件　 5.1 测试设备及仪器　 5.2 测试环境　 6 试验前准备　 6.1  设备齐套性检查　 6.2  设备多余物检查　 6.3  标识外观检查 6.4  设备多余物检查 7 测试图中各测试点含义　 8 试验方法　 8.1  L/U双频数据链重量　 8.2  L/U双频数据链尺寸　 8.3  L/U双频数据链工作频率　 8.3.1 试验程序　 8.3.2 合格判据　 8.4  L/U双频数据链发射功率　 8.4.1 L频段数据链路发射功率试验程序　 8.4.2 UHF频段数据链路发射功率试验程序　 8.4.3 合格判据　 8.5  L/U双频数据链接收灵敏度　 8.5.1 试验程序　 8.5.2 合格判据　 8.6  L/U双频数据链数据传输误码率　 8.6.1 合格判据　 8.7  L/U双频数据链各终端功能　 8.6.1 合格判据　 8.8  L/U双频数据链系统延时　 8.8.1 试验程序　 8.8.2 合格判据　 8.9  L/U双频数据链额定功耗　 8.9.1 试验程序　 8.9.2 合格判据　 8.10  L/U双频数据链传输速率　 8.10.1 试验程序　 8.10.2 合格判据　 9 测试图与测试记录表　 10 测试结果评定　 11 试验报告　

Performance test method of L/U dual frequency Data Link for UAV

HB 8655-2022 民用飞机操控面板组件通用技术要求

Generaltechnical requirements ofcontrol panel assemblies for civil aircrafts

ASTM F3153-22 飞机系统和设备验证的标准规范

1.1 This specification provides a process for performing system level verification of aircraft systems and equipment. It provides a means of compliance that can be used for systems and equipment with software and Airborne Electronic Hardware (AEH) that have not been addressed by traditional development assurance methods. 1.2 This process can be used to show compliance to regulations that require a demonstration that functionality was implemented as intended, including safety mitigations that address failure conditions for software and AEH aspects for aircraft systems and equipment. 1.3 While this specification was developed with systems and equipment installed on aircraft certification level 1 and 2 (or class I and II in accordance with Advisory Circular (AC) 23.1309-1) normal category aeroplanes in mind, the content may be more broadly applicable. It is the responsibility of the Applicant to substantiate broader applicability as a specific means of compliance and obtain concurrence for its use from the applicable Civil Aviation Authority (CAA). 1.4 When using this specification, regulations that govern system safety requirements applicable to the aircraft still apply. In complying with those regulations, additional architectural mitigations such as redundancy, independence, separation, system monitors, etc., may be required in addition to the verification process specified in this specification. 1.5 The system level verification activities expected by this specification increase as the severity of the failure conditions applicable to or affected by the function increase. Those functions, which have hazardous and catastrophic failure conditions, receive additional activities through this process to provide detailed scrutiny. For normal category aircraft, refer to Practice F3309, Practice F3230, or AC 23.1309-1 for more information on the identification and classification of system failure conditions. Involvement of the applicable CAA personnel or their designees in this system verification process should be discussed early in the project. 1.6 This verification process specifically addresses definition, identification, and verification of system functions. Processes conducted under this specification may not satisfy all applicable external requirements; additional review on the part of the system developer, integrator, or installer may be required to meet specific requirements or the specified mission of the aircraft, or both. 1.7 The values stated in inch-pound units are to be regarded as standard. No other units of measurement are included in this standard. 1.8 This standard does not purport to address all of the safety concerns, if any, associated with its use. It is the responsibility of the user of this standard to establish appropriate safety, health, and environmental practices and determine the applicability of regulatory limitations prior to use. 1.9 This international standard was developed in accordance with internationally recognized principles on standardization established in the Decision on Principles for the Development of International Standards, Guides and Recommendations issued by the World Trade Organization Technical Barriers to Trade (TBT) Committee.

Standard Specification for Verification of Aircraft Systems and Equipment

GSO ISO 268:2021 飞机机械和机电指标一般要求

States the requirements which are generally applicable. Is to be read in conjunction with specifications for individual indicators. An indicator is regarded as a unit primarily concerned with the visual display of information. The size and type of the finished indicator case shall be declared by the manufacturer in sufficient detail to facilitate subsequent installation.

Aircraft — Mechanical and electromechanical indicators — General requirements

PN-ETSI EN 303 213-4-2 V2.1.1-2021-05 E 高级地面移动制导和控制系统（A-SMGCS） 第4部分：已部署非合作传感器的社区规范，包括其接口 第2部分：已部署地面移动雷达传感器的具体要求

Advanced Surface Movement Guidance and Control System (A-SMGCS) − Part 4: Community Specification for a deployed non-cooperative sensor including its interfaces − Sub-part 2: Specific requirements for a deployed Surface Movement Radar sensor

PN-ETSI EN 303 213-4-1 V2.1.1-2021-05 E 高级地面运动制导和控制系统（A-SMGCS） 第4部分：部署的非合作传感器的社区规范，包括其接口 第1部分：非合作传感器的通用要求

Advanced Surface Movement Guidance and Control System (A-SMGCS) − Part 4: Community Specification for a deployed non-cooperative sensor including its interfaces − Sub-part 1: Generic requirements for non-cooperative sensor

AGMA 911-B21-2021 航空航天齿轮系统设计指南

Design Guidelines for Aerospace Gear Systems

OEVE/OENORM EN 303276 V1.2.1-2021 在 5852 MHz 至 5872 MHz 和/或 5880 MHz 至 5900 MHz 频段内运行的海上宽带无线电链路，适用于从事协调活动的船舶和离岸设施；无线电频谱接入协调标准（ETSI EN 303276 V1.2.1（2021

Maritime Broadband Radiolink operating within the bands 5852 MHz to 5872 MHz and/or 5880 MHz to 5900 MHz for ships and off-shore installations engaged in coordinated activities; Harmonised Standard for access to radio spectrum (ETSI EN 303276 V1.2.1 (2021

PN-ETSI EN 303 213-2 V2.1.1-2021-02 E 高级地面运动引导和控制系统（A-SMGCS） 第2部分：A-SMGCS 机场安全支持服务的社区规范

Advanced Surface Movement Guidance and Control System (A-SMGCS) − Part 2: Community Specification for A-SMGCS airport safety support service

PN-ETSI EN 303 213-7 V2.1.1-2021-02 E 高级地面运动引导和控制系统（A-SMGCS） 第7部分：A-SMGCS 路由服务社区规范

Advanced Surface Movement Guidance and Control System (A-SMGCS) − Part 7: Community Specification for A-SMGCS routing service

PN-ETSI EN 303 213-1 V2.1.1-2021-02 E 高级地面运动引导和控制系统（A-SMGCS） 第1部分：包括外部接口的 A-SMGCS 监视服务社区规范

Advanced Surface Movement Guidance and Control System (A-SMGCS) − Part 1: Community Specification for A-SMGCS surveillance service including external interfaces

OENORM EN 4641-301-2020 航空航天系列 光缆，125 微米直径包层 第301部分：紧密结构 50/125 微米 GI，光纤标称 1.8 毫米，外径 产品标准

Aerospace series - Cables, optical 125 µm diameter cladding - Part 301: Tight structure 50/125 µm GI, fibre nominal 1,8 mm, outside diameter - Product standard