GB/T 44091-2024 民用無人駕駛航空器產(chǎn)品標(biāo)識要求

Product Labeling Requirements for Civil Unmanned Aerial Vehicles

GB/T 43370-2023 民用無人機(jī)地理圍欄數(shù)據(jù)技術(shù)規(guī)范

Technical Specifications for Geofencing Data for Civilian UAVs

GB/T 29076-2021 航天產(chǎn)品質(zhì)量問題歸零實(shí)施要求

本文件規(guī)定了航天產(chǎn)品質(zhì)量問題歸零的一般要求、程序、技術(shù)歸零工作要求和管理歸零工作要求等內(nèi)容。 本文件適用于航天產(chǎn)品設(shè)計(jì)、生產(chǎn)、試驗(yàn)、使用等各階段中發(fā)生的質(zhì)量問題歸零工作。

Execution requirements of quality problem closed loop for aerospace product

GB/T 38905-2020 民用無人機(jī)系統(tǒng)型號命名

本標(biāo)準(zhǔn)規(guī)定了民用無人機(jī)系統(tǒng)型號的命名組成和命名方法。本標(biāo)準(zhǔn)適用于民用無人機(jī)系統(tǒng)行業(yè)管理.研制生產(chǎn).銷售、使用維護(hù)的型號命名。

Type designation for civil unmanned aircraft system

GB/T 38931-2020 民用輕小型無人機(jī)系統(tǒng)安全性通用要求

規(guī)范性引用文件pe 術(shù)語和定義一般要求4.1 工作目標(biāo)4.2 ”基本原則4.3 工作過程詳細(xì)要求5.1 安全性要求分解5.2 初步危險分析5.3 ”安全性設(shè)計(jì)準(zhǔn)則制定5.4 系統(tǒng)危險分析5.5 試驗(yàn)的安全5.6，使用與保障危險分析必co

General requirements for safety of civil small and light unmanned aircraft system

GB/T 32299-2015 航天項(xiàng)目風(fēng)險管理

Space project risk management

GB/T 29076-2012 航天產(chǎn)品質(zhì)量問題歸零實(shí)施要求

本標(biāo)準(zhǔn)規(guī)定了航天產(chǎn)品質(zhì)量問題歸零的實(shí)施要求。 質(zhì)量問題歸零包括了質(zhì)量問題技術(shù)歸零和質(zhì)量問題管理歸零。 本標(biāo)準(zhǔn)適用于航天產(chǎn)品從初樣階段開始各階段的質(zhì)量問題技術(shù)歸零和管理歸零。

Execution requirements for quality problem close loop of aerospace product

GB/T 29076-2012e 航天產(chǎn)品質(zhì)量問題歸零實(shí)施要求

Execution requirements for quality problem close loop of aerospace product

GB/T 29073-2012 航天器研制計(jì)劃流程編寫規(guī)則

本標(biāo)準(zhǔn)規(guī)定了航天器研制計(jì)劃流程的相關(guān)術(shù)語、編寫原則、編寫依據(jù)、計(jì)劃流 程體系 內(nèi)容及編寫步驟等要求。 本標(biāo)準(zhǔn)適用于按層次劃分的航天器系統(tǒng)級、分系統(tǒng)級.設(shè)備級和工作項(xiàng)目(含軟件?計(jì)劃流程的編 寫，也適用于按時間劃分的航天器研制全過程、階段和年度等計(jì)劃流程的編寫。

Drafting rules of schedule network for spacecraft development

GB/T 29072-2012 航天器研制技術(shù)流程編寫規(guī)則

本標(biāo)準(zhǔn)規(guī)定了航天器研制技術(shù)流程(以下簡稱技術(shù)流程)的相關(guān)術(shù)語、編寫原則、編寫依據(jù)、技術(shù)流程分類、編寫要求和內(nèi)容、編寫步驟和編寫方法、本標(biāo)準(zhǔn)適用于航天器系統(tǒng)、分系統(tǒng)工作項(xiàng)目技術(shù)流程的編寫、設(shè)備研制技術(shù)流程的編寫可參照使用、

Drafting rules of technical network for spacecraft development

GB/T 29073-2012(英文版) 航天器研制進(jìn)度網(wǎng)絡(luò)規(guī)則起草

Drafting rules of schedule network for spacecraft development

GB/T 29072-2012(英文版) 航天器研制技術(shù)網(wǎng)絡(luò)規(guī)則起草

Drafting rules of technical network for spacecraft development

DB43/T 2779-2023 無人機(jī)應(yīng)用服務(wù)通用規(guī)范

General specifications for UAV application services

DIN 5452-1:2021 航空航天系列. 無人機(jī)系統(tǒng)（UAS）. 第1-0部分: 術(shù)語和定義; 德文和英文文本

This document specifies terms and definitions in the field of unmanned aircraft systems that are used by private, commercial users and by those under public law as well as manufacturers. In addition to that regulating and supervisory authorities as well as testing institutes are

Aerospace series - Unmanned aircraft systems (UAS) - Part 1: Terms and definitions; Text in German and English

DIN EN 16602-60-14:2020 航天產(chǎn)品保證. 重新安裝程序. EEE 組件; 英文版 EN 16602-60-14-2020

This standard specifies the requirements, also known as \

Space product assurance - Relifing procedure - EEE components; English version EN 16602-60-14:2020

EN 9131:2020 航空航天系列.質(zhì)量管理體系.不合格的數(shù)據(jù)定義和文檔

This European Standard defines the common nonconformance data definition and documentation that shall be exchanged between an internal/external supplier or sub-tier supplier, and the customer when informing about a nonconformity requiring formal decision. The requirements are applicable, partly or totally, when reporting a product nonconformity to the owner or operator, as user of the end item (e. g., engine, aircraft, spacecraft, helicopter), if specified by contract. The process of exchanging, coordinating, and approving nonconformance data varies with the multiple relationships and agreements among all parties concerned. The information provided by this European Standard forms guidelines for submitting and managing of data through accurate communication. The main objective is to provide the definition of a data set that can be integrated into any form of communication (e. g., electronic data interchange, submission of conventional paper forms). Reporting of nonconformance data, either electronically or conventionally on paper, is subject to the terms and conditions of the contract. This also includes, where applicable, data access under export control regulations.

Aerospace series - Quality Management Systems - Nonconformance Data Definition and Documentation

HB 8569-2020 民用飛機(jī)構(gòu)型管理要求

Configuration management requirements for civil aircraft

ASTM F3180/F3180M-19 飛機(jī)低速飛行特性標(biāo)準(zhǔn)規(guī)范

1.1 This specification covers the low-speed flight characteristics of fixed-wing aircraft and provides standards for departure characteristics, spinning, and stall warning. The material was developed through open consensus of international experts in general aviation. This information was created by focusing on Normal Category aeroplanes. The content may be more broadly applicable; it is the responsibility of the Applicant to substantiate broader applicability as a specific means of compliance. The topics covered within this specification are: (4.1) Low-Speed Flight Characteristics Score, (4.2) Stall Characteristics, (4.3) Stall Warning, (4.4) Departure Characteristics: Single Engine, (4.5) Departure Characteristics: Multiengine, (4.6) Spinning, and (4.7) Safety-Enhancing Features. 1.2 An applicant intending to propose this information as Means of Compliance for a design approval must seek guidance from their respective oversight authority (for example, published guidance from applicable CAAs) concerning the acceptable use and application thereof. For information on which oversight authorities have accepted this standard (in whole or in part) as an acceptable Means of Compliance to their regulatory requirements (hereinafter “the Rules”), refer to the ASTM Committee F44 webpage (www.astm.org/COMMITTEE/F44.htm). 1.3 Units—This standard may present information in either SI units, English Engineering units, or both; the values stated in each system may not be exact equivalents. Each system shall be used independently of the other; combining values from the two systems may result in nonconformance with the standard. 1.4 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. 1.5 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 Low-Speed Flight Characteristics of Aircraft

ASTM F3245-19 飛機(jī)電子技術(shù)人員認(rèn)證的標(biāo)準(zhǔn)指南

4.1 The guide is intended to be used to assess competencies of qualified individuals who wish to become certified as an Aircraft Electronics Technician through a certification program. 4.2 The guide is intended to be used in concert with a certification provider’s structure and materials for management, exam delivery, and candidate preparation. 1.1 The purpose of this guide is to address the basic fundamental subject knowledge, task performance, and task knowledge activities and functions for avionics professionals to be titled Aircraft Electronics Technicians (AETs). 1.2 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. 1.3 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 Guide for Aircraft Electronics Technician Personnel Certification

ASTM F3174/F3174M-19 確定飛機(jī)操作限制和信息的標(biāo)準(zhǔn)規(guī)范

1.1 This specification covers airworthiness requirements for establishing general limitations and information to be contained in the aeroplane flight manual. This specification specifies what information shall be provided and does not state how such information shall be presented unless this is necessary for the clarity of the purpose of the specification. Refer to Specification F3117/F3117M for means and methods of presentation. The material was developed through open consensus of international experts in general aviation. This information was created by focusing on Level 1, 2, 3, and 4 Normal Category aeroplanes. The content may be more broadly applicable; it is the responsibility of the applicant to substantiate broader applicability as a specific means of compliance. The topics covered within this specification are: Limitations for Airspeed, Weight and Center of Gravity, Auxiliary Power Units, Minimum Flight Crew, Maximum Passenger Seating Configuration, Kinds of Operation, and Maximum Operating Altitude. 1.2 An applicant intending to propose this information as Means of Compliance for a design approval must seek guidance from their respective oversight authority (for example, published guidance from applicable CAAs) concerning the acceptable use and application thereof. For information on which oversight authorities have accepted this specification (in whole or in part) as an acceptable Means of Compliance to their regulatory requirements (hereinafter “the Rules”), refer to the ASTM Committee F44 web page (www.astm.org/COMMITTEE/F44.htm). 1.3 Units—This specification may present information in either SI units, English Engineering units, or both; the values stated in each system may not be exact equivalents. Each system shall be used independently of the other; combining values from the two systems may result in nonconformance with the standard. 1.4 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. 1.5 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 Establishing Operating Limitations and Information for Aeroplanes