V35 航空器及其附件综合 标准查询与下载

SAE AS50881D-2010 航天载具接线

This specification covers all aspects from the selection through installation of wiring and wiring devices and optical cabling and termination devices used in aerospace vehicles. Aerospace vehicles include manned and unmanned airplanes, helicopters, lighter-than- air vehicles, missiles and external pods.

Wiring Aerospace Vehicle

ASTM F2851-10 无人驾驶航空器系统登记和进行标记的标准操作规程(小型无人驾驶航空器系统除外)

Aircraft flying in national airspace are required by the ICAO Chicago Convention and national regulatory rules to have visible markings to determine nationality and registration. UAS shall comply with these rules, although small UAS will have unique rules or exemptions from existing rules due to their small size. This standard is designed to allow UAS to comply with these marking requirements in Annex 7 to the Convention on International Civil Aviation as amended by state regulatory rules. Many ICAO states are assigning UAS to different classes and categories to define the rules UAS must operate under. The ICAO Annex 7 Standards and Recommended Practices (SARPS) apply to UAS Aircraft with the exception of small UAS. The classification of what constitutes a small UAS (sUAS) has been left to ICAO states and the rules under which sUAS operate are dictated by each state. This practice follows ICAO Annex 7 SARPS except in areas where the unique aspects of UAS may not allow compliance. In these cases, this document will address the issue and recommend the need for an alternate compliance method.1.1 This practice prescribes guidelines for the display of marks to indicate appropriate UAS registration and ownership for all Unmanned Aircraft Systems (UAS) except those categorized as small UAS (sUAS) by regulatory authorities. The FAA is developing a Special Federal Aviation Regulation (SFAR) to define the term small UAS and provide regulations for these aircraft. 1.2 This practice will allow determination of nationality in cases where UAS may cross international boundaries. 1.3 This practice does not apply to sUAS. The International Civil Aviation Organization (ICAO) has left the designation of sUAS to each state and the states will develop rules and regulations for sUAS. 1.4 This practice does not apply to model aircraft. 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 UAS Registration and Marking (Excluding Small Unmanned Aircraft Systems)

ASTM F2317/F2317M-10 重力-移动-控制式飞机的设计的标准规范

1.1 This specification covers the minimum airworthiness standards a manufacturer shall meet in the designing, testing, and labeling of weight-shift-control aircraft. 1.2 This specification covers only weight-shift-control aircraft in which flight control systems do not use hinged surfaces controlled by the pilot. Note 18212;This section is intended to preclude hinged surfaces such as typically found on conventional airplanes such as rudders and elevators. Flexible sail surfaces typically found on weight-shift aircraft are not considered hinged surfaces for the purposes of this specification. 1.3 Weight-shift-control aircraft means a powered aircraft with a framed pivoting wing and a fuselage (trike carriage) controllable only in pitch and roll by the pilot''s ability to change the aircraft''s center of gravity with respect to the wing. Flight control of the aircraft depends on the wing''s ability to flexibly deform rather than the use of control surfaces. 1.4 This specification is organized and numbered in accordance with the bylaws established for Committee F37. The main sections are:

Standard Specification for Design of Weight-Shift-Control Aircraft

ASTM F2506-10e1 固定间距或地面可调轻型运动飞机的螺旋桨设计和试验的标准规范

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 F2339. 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. 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 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 F2295-10 轻型运动飞机的持续操作安全监控的标准实施规程

The purpose of this practice is to establish a method by which safety of flight issues are discovered, evaluated, and corrected for the purpose of maintaining operational safety of a LSA.1.1 This practice establishes the standard practice for the continued operational safety monitoring of a light sport aircraft. 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 and health practices and determine the applicability of regulatory limitations prior to use.

Standard Practice for Continued Operational Safety Monitoring of a Light Sport Aircraft

ASTM F2564-10 轻型运动滑翔机的设计和性能的标准规范

1.1 This specification covers airworthiness requirements for the design of a powered or non-powered fixed wing light sport aircraft, a “glider.” 1.2 This specification is applicable to the design of a light sport aircraft glider as defined by regulations and limited to day VFR flight. 1.3 A glider for the purposes of this specification is defined as a heavier than air aircraft that remains airborne through the dynamic reaction of the air with a fixed wing and in which the ability to remain aloft in free flight does not depend on the propulsion from a power plant. A powered glider is defined for the purposes of this specification as a glider equipped with a power plant in which the flight characteristics are those of a glider when the power plant is not in operation. 1.4 The values in SI units are to be regarded as the standard. The values in parenthesis are for information only. 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 requirements prior to use.

Standard Specification for Design and Performance of a Light Sport Glider

ASTM F2279-10 固定翼轻型运动飞机制造的质量保证的标准实施规程

The purpose of this practice is to provide the minimum requirements necessary for the establishment of a quality assurance and production acceptance program for a manufacturer of light sport aircraft.1.1 This practice establishes the minimum requirements for the development of a Quality Assurance and Production Acceptance Program, to be used for the manufacture of LSA''s or LSA kits. 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 and health practices and determine the applicability of regulatory limitations prior to use.

Standard Practice for Quality Assurance in the Manufacture of Fixed Wing Light Sport Aircraft

ASTM F2506-10 固定间距或地面可调轻型运动飞机的螺旋桨设计和试验的标准规范

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 F2339. 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. 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 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 F2849-10 分流飞机场上无人飞机系统的标准实施规程

This practice is written to preclude damage or injury to property and personnel in the event of an unplanned landing by an unmanned aircraft at an airfield not equipped or trained to handle that type of aircraft and to prevent unintentional damage to the aircraft once it lands. It is intended for use by unmanned aircraft equipment designers, procedures developers, and ground personnel.1.1 This practice identifies and describes equipage and procedures for safely handling unmanned aircraft forced to recover at alternate or diversionary airfields where personnel trained in recovering that type of aircraft may not be present. It is intended to apply to fixed-wing unmanned aircraft conducting non-visual line-of-sight operations. It is intended to establish common locations, labeling, and functions of equipment necessary to safely power down the aircraft without damaging it and common procedures for untrained personnel to follow to contact the owner of the aircraft. It addresses mission planning procedures, automated functions, and manual functions/handling procedures in the preflight, in-flight, and post-flight phases, respectively.

Standard Practice for Handling of Unmanned Aircraft Systems at Divert Airfields

ASTM F2244-10 动力驱动滑翔机的设计和性能要求标准规范

1.1 The following requirements apply for the manufacture of powered parachute aircraft. This specification includes design and performance requirements for powered parachute aircraft. 1.2 This specification applies to powered parachute aircraft seeking civil aviation authority approval, in the form of flight certificates, flight permits, or other like documentation. 1.3 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 requirements prior to use.

Standard Specification for Design and Performance Requirements for Powered Parachute Aircraft

GJB 6850.217-2009 水面舰船系泊和航行试验规程 第217部分：舰载直升机牵引装置试验

Surface ship mooring and sailing test procedures part 217: Shipboard helicopter towing device test

GJB 6850.223-2009 水面舰船系泊和航行试验规程 第223部分：舰载直升机安全网试验

Surface ship mooring and sailing test procedures part 223: shipboard helicopter safety net test

SAE AIR5992-2009 航天应用的系统综合测试装配机翼(铁制机翼)说明书

This Aerospace Information Report (AIR) provides information on systems integration rigs, commonly referred to as "Iron Birds" for aerospace applications: a. It includes background historical information including descriptions of Iron Birds produced to date, important component elements and selection rationale, hydraulic system design and operational modes and illustrates the design approaches to be considered. b. It provides illustrations of the various systems that should be considered for Iron Bird testing in the development phase and utilization during the production program. c. It includes recommendations for simulation, component development tests, system integration and lessons learned. The information conveyed in this AIR is intended to help aircraft systems designers to design and develop Iron Birds for Aerospace applications. The document describes the design approaches that should be considered and provides descriptions of Iron Birds produced to date on various commercial and military programs.

Descriptions of Systems Integration Test Rigs (Iron Birds) for Aerospace Applications

SAE ARP4740-2009 客机洗手间内抽烟的安全考虑

This ARP addresses the issue of passengers smoking in aircraft lavatories and the need to improve warnings about the danger of fire caused by smoking.

Safety Considerations Smoking in Lavatories of Transport Aircraft

GJB 1754A-2009 机载干扰器材投放设备通用规范

本规范规定了机载干扰器材投放设备的基本要求、质量保证规定及交货准备等。 本规范适用于机载干扰器材引爆式投放设备(简称I型投放设备)和机载干扰器材机电式投放设备(简称II型投放设备)的研制、生产和检验，是编制机载干扰器材投放设备(简称投放设备)产品规范的基本依据。

General specification for airborne jamming materiel dispensing equipments

GJB 6703-2009 无人机测控系统通用要求

本标准规定了无人机测控系统的组成、功能、设计要求、性能要求和工程专业要求。 本标准适用于无人机测控系统的设计和制造。

General requirements for UAV tracking telemetry and command and communication system

GJB 6689-2009 潜地战略导弹武器系统定型试验规程

本标准规定了潜地战略导弹武器系统（以下简称武器系统）定型试验的基本内容、试验项目、试验方法、试验数据录取与处理、试验结果报告编写和试验结果评定。 本标准适用于武器系统定型试验。

Code of approval test on submarine-to-ground strategic missile weapon system

GJB 6724-2009 通信干扰无人机通用规范

本规范规定了通信干扰无人机(系统)的通用技术要求、质量保证规定和交货准备等。 本规范适用于固定翼通信干扰无人机(系统)的研制、生产和检验，是拟制通信干扰无人机(系统)产品规范(以下简称产品规范)的基本依据。

General specification for communication jamming UAV

GJB 6770-2009 导弹、航天测控设备校飞飞机改装要求与检验方法

本标准规定了用于导弹、航天测控设备校飞飞机改装要求与检验方法。 本标准适用于导弹、航天测控设备校飞飞机改装。

Modification requirements and test method of the airplane for space TT&C equipment's flight test

GJB 6704-2009 无人侦察机效能分析方怯

本标准规定了成像侦察类无人侦察机系统及其无人机、数据链、地面控制站、任务载荷、情报处理与分发和综合保障等组成部分的效能评估程序和方法。 本标准适用于成像侦察类无人侦察机系统的效能评估，其他类型无人机系统也可参照使用。

Effectiveness evaluation of unmanned reconnaissance aerial vehicle system