V35 航空器及其附件综合 标准查询与下载

ASTM F2500-07 无人驾驶飞行器系统(UAS)可视范围内飞行操作的标准实施规程

Safe operation of the unmanned aircraft is of the primary importance to the unmanned aircraft industry and for successful integration of unmanned aircraft with manned aircraft in civil airspace. Operators and pilots-in-command of unmanned aircraft systems shall comply with applicable Federal Aviation Regulations (14 CFR Part 43, 14 CFR Part 71, 14 CFR Part 73, 14 CFR Part 91, 14 CFR Part 93, and 14 CFR Part 99). This standard includes the minimum additional methods that should be followed by unmanned aircraft system operators, including pilots-in-command, on every visual range flight to ensure the safe operation of the aircraft and safety of people and property in the air and on the ground. This visual range flight operation standard shall be used in conjunction with appropriate unmanned aircraft system airworthiness and pilot qualification standards.1.1 This practice prescribes guidelines that govern the visual flight operation of unmanned aircraft systems in civil airspace in order to provide for the safe integration of unmanned aircraft flight operations with manned aircraft flight operations.1.2 This practice applies to those operations conducted for civil purposes other than sport or recreation that remain within the visual range of the pilot in command (see Terminology F 2395 for a definition of "visual range").1.3 This practice complies with the known rules, regulations, and public law available at the time of its publication. Should any conflict with a rule, regulation, or public law arise, the user must comply with rule and should notify ASTM of the conflict.This practice only prescribes accepted methods for visual range flight operation of unmanned aircraft systems.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 and health practices and determine the applicability of regulatory limitations prior to use.

Standard Practice for Unmanned Aircraft System (UAS) Visual Range Flight Operations

ASTM F2506-07 固定螺距或地面可调整轻型运动飞机螺旋桨设计和测试用标准规范

1.1 This specification covers the establishment of the minimum requirements for the design, testing, and quality assurance of fixed-pitch or ground adjustable propellers for light sport aircraft. These propellers are used on light aircraft, and could be used with engines conforming to Practice F 2339.1.2 This specification is intended for use by manufacturers of propellers for light sport aircraft.1.3 This specification does not address the airframe installation requirements for propellers.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 and health practices and to determine the applicability of regulatory limitations prior to use.

Standard Specification for Design and Testing of Fixed-Pitch or Ground Adjustable Light Sport Aircraft Propellers

ASTM F2505-07 应用联邦飞行管理局(FAA)颁布联邦飞行法规第21部分对无人机系统(UAS)要求的标准实施规程

This practice is intended for guidance and instruction of the aircraft and unmanned aircraft systems industries when addressing the requirements of Part 21.1.1 In this practice, certification procedures are provided for Unmanned Aircraft Systems (UAS) in the Light UAS Class and in the Remotely Operated Aircraft (ROA) UAS Classes. Unmanned Aircraft Systems in the Mini UAS and Micro UAS Classes are not considered in this practice, since they do not undergo airworthiness certification. 1.2 Citations of Federal Aviation RegulationsWhen citing U.S. Federal Aviation Regulations in this practice, the citation references are based on the following Federal Aviation Regulation structure:1.2.1 The Code of Federal Regulations, Title 14 (14 CFR) comprises Aeronautics and Space Regulations. Chapter 1 of 14 CFR contains the regulations of the Federal Aviation Administration and is subdivided into subchapters and parts:The Parts are further subdivided into Subparts and sections.1.2.2 This practice uses Part 21 as a template. Within the text of the practice:14 CFR Chapter 1 means the whole of Chapter 1 of 14 CFR; andSubchapter C means all of the Parts of Subchapter C of 14 CFR.1.2.3 In compact notation, citation of section 1309 of Part 23, for example, may be designated as "section 23.1309."1.3 Unmanned Aircraft SystemsAn Unmanned Aircraft System (UAS) comprises an unmanned air vehicle, the remote control ground station that provides for the mission management and piloting of the air vehicle, data-links for the exchange of control and sensor payload data and all related interfaces. Any part of the overall system that could affect the airworthiness and safety of the aircraft is subject to the requirements of Part 21.1.4 inch-pound-units;1.5 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 and health practices and determine the applicability of regulatory limitations prior to use.

Standard Practice for Application of Federal Aviation Administration (FAA) Federal Aviation Regulations Part 21 Requirements to Unmanned Aircraft Systems (UAS)

GJB 5887-2006 无人机任务设备通用要求

本标准规定了无人机任务设备（以下简称任务设备）的通用要求。 本标准适用于任务设备的选择并为无人机总体选择任务设备提供参数要求。

General requirements for UAV system assign equipment

GJB 5883-2006 直升机动力装置飞行试验要求

本标准规定了直升机动力装置飞行试验的一般要求和详细要求。 本标准适用于新型号直升机动力装置和附件系统的设计定型国家鉴定试飞（简称：设计定型试飞）。其他有关的鉴定试飞、科研试飞、调整试飞等可参照使用。

The flight test requirement for helicopter powerplant

HB 7817-2006 直升机结构载荷测试与载荷谱编制要求

本标准规定了直升机结构（零部件）的飞行载荷测试与实测载荷谱的编制要求和方法。 本标准适用于直升机零部件疲劳定寿的飞行载荷测试、实测载荷的数据处理和实测载荷谱的编制。对其它载荷测试与实测载荷的数据处理也可参照使用。

Requirements for load test and load spectrum establishment of helicopter structure

GJB 5864-2006 飞机牵引杆和牵引装置型别、基本参数和技术要求

本标准规定了飞机牵引杆和牵引装置的型别、基本参数和技术要求。 本标准适用于飞机牵引杆和牵引装置。

Type, parameter and technical requirement of tow bar and towing device for aircrafet

GJB 2703A-2006 航天器热控系统通用规范

本规范规定了航天器热控系统的通用要求。 本规范适用于卫星、飞船、空间站、深空探测器等航天器的热控系统。

General specification for thermal control system for spaceerafts

GJB 2983A-2006 两级地地固体战略导弹测试发射规程

本标准规定了两级地地固体战略导弹（以下简称“导弹”）在发射场执行测试发射试验任务时的工作程序和技术要求。 本标准适用于两级地地固体战略导弹在发射场进行的方案考核、鉴定定型飞行试验。其合练、抽检、训练亦可参照执行。

Rules for testing and launching of two-stage solid ground-to-ground strategic missiles

GJB 659A-2006 地空导弹使用期评定

本标准规定了地空导弹（裸弹、筒弹或箱弹 , 以下同）及弹上设备使用期评定的一般要求、详细要求、项目和方法，以及确定使用期的依据和程序等。 本标准适用于确定和验证导弹及弹上设备（以下简称产品）的使用期。也适用于确定和验证其贮存期。其他战术导弹亦可参照使用。

Evaluation for service life of ground-to-air missiles

GJB 5791-2006 直升机机载侦察雷达战术性能试验方法

本标准规定了直升机机载侦察雷达进行地面静态和机载动态战术性能试验的条件和方法。 本标准适用于直升机机载侦察雷达设计定型、生产定型战术性能试验，也适用于批生产和重大技术改进后进行的战术性能试验。

Test method of tactical performance for Heliborne reconnaissance radar

GJB 5771-2006 舰载直升机通用要求

本标准规定了舰载直升机设计、制造、试验和检验的通用要求。 本标准适用于各类新研军用舰载直升机，改进、改型的舰载直升机可参照执行。

General requirement for shipborne helicopter

SAE ARP5056-2006 飞机.第25部分:飞机通道中飞行机组人员相遇问题设计程序

This ARP defines recommended flight crew interface design processes and methods for new flight deck designs as well as modifications to the flight crew interface of existing flight decks of transport category aircraft (Part 25), which includes commercial transport aircraft, regional and business aircraft. These processes and methods are intended to be utilized by the design engineers of manufacturers of transport category aircraft or any modifiers to the flight deck system. Modifiers include equipment suppliers, avionics manufacturers, aircraft operators, original equipment manufacturers (OEM), regulatory authorities, or anyone seeking a supplemental type certificate (STC), type certificate (TC), amended TC, field approval, or equivalent approval. The processes and methods described in this ARP address the integration of human factors/ergonomics, engineering, and flight operations in the design and/or modification of flight crew interfaces. These interfaces provide the flight crew access to the installed systems, using controls, indications and displays, in order to allow them to accomplish the tasks of aviate, navigate, communicate, and manage systems. Included in these processes and methods are considerations for flight crew training, the use and integration of automation, error tolerant designs, and task management. These processes and methods are designed to yield flight deck designs that are both safe and efficient, in that order of priority. These processes and methods address the issue of creating modifications to existing designs that are compatible with the original intent of the flight deck design.

Flight Crew Interface Considerations in the Flight Deck Design Process for Part 25 Aircraft

HJB 362.7-2006 机载电子设备综合自动测试系统通用要求 第7部分：被测单元测试性

General Requirements for Integrated Automatic Test System of Airborne Electronic Equipment Part 7: Testability of UUT

HJB 362.4-2006 机载电子设备综合自动测试系统通用要求 第4部分：软件平台

General Requirements for Integrated Automatic Test System of Airborne Electronic Equipment Part 4: Software Platform

HJB 362.8-2006 机载电子设备综合自动测试系统通用要求 第8部分：测试需求文档

General Requirements for Integrated Automatic Test System of Airborne Electronic Equipment Part 8: Test Requirements Document

HJB 362.5-2006 机载电子设备综合自动测试系统通用要求 第5部分：测试程序

General Requirements for Integrated Automatic Test System of Airborne Electronic Equipment Part 5: Test Procedure

HJB 362.1-2006 机载电子设备综合自动测试系统通用要求 第1部分：总则

General Requirements for Integrated Automatic Test System of Airborne Electronic Equipment Part 1: General Rules

HJB 362.3-2006 机载电子设备综合自动测试系统通用要求 第3部分：适配器

General Requirements for Integrated Automatic Test System of Airborne Electronic Equipment Part 3: Adapters

HJB 362.2-2006 机载电子设备综合自动测试系统通用要求 第2部分：硬件平台

General Requirements for Integrated Automatic Test System of Airborne Electronic Equipment Part 2: Hardware Platform