V36 总体技术要求 标准查询与下载

GJB 5435.11-2005 无人机强度和刚度规范 第11部分：文件和报告

本部分规定了无人机新机研制和改进、改型过程中，应编制的与结构强度和刚度有关的文件和报告的名称、内容、编制格式以及提交文件和报告的要求。 本部分适用于有固定机翼和可调固定机翼的无人机：适用新研制的、改进、改型的或改变用途的无人机。本部分是无人机订货、设计和验证、签订研制合同的依据之一。对于具体型号的特殊要求，应按研制任务书或合同执行。 本部分不适用于微型无人机和无人战斗机。

Specification for unmanned aerial vehicles strength and rigidity Part 11: Documents and reports

SAE ARP1915C-2005 飞行器牵引杆

This SAE Aerospace Recommended Practice (ARP) outlines the basic general design considerations for aircraft tow bars. It does not cover the requirements for tow bars intended for aircraft with a maximum ramp mass (MRW) below 8,600 kg (19,000 lb).

Aircraft Tow Bar

SAE ARP5936-2005 起落架舱

This document categorizes the difference types of stoarge requirements, either on the aircraft or new unused or overhauled on the shelf, for aircraft landing gears/components. Recommendations and examples of proper landing gear storage are outlined. Reclamation recommendations are proved for aircraft landing gear returning from long-term storage.

Landing Gear Storage

SAE AS8049B-2005 民用旋翼飞行器、运输飞行器和一般航空飞行器座位的性能标准

This SAE Aerospace Standard (AS) defines minimum performance standards, qualification requirements, and minimum documentation requirements for passenger and crew seats in civil rotorcraft, transport aircraft, and general aviation aircraft. The goal is to achieve comfort, durability, and occupant protection under normal operational loads and to define test and evaluation criteria to demonstrate occupant protection when a seat/occupant/restraint system is subjected to statically applied ultimate loads and to dynamic impact test conditions set forth in the applicable Federal Aviation Regulations 14 CFR 23, 25, 27, or 29. Guidance for test procedures, measurements, equipment, and interpretation of results is presented to promote uniform techniques and to achieve acceptable data. While this document addresses system performance, responsibility for the seating system is divided between the seat supplier and the installation applicant. The seat suppliers responsibility consists of meeting all the seat system performance requirements and obtaining and supplying to the installation applicant all the data prescribed by this document. The installation applicant has the ultimate system responsibility in assuring that all requirements for safe seat installation have been met.

Performance Standard for Seats in Civil Rotorcraft, Transport Aircraft, and General Aviation Aircraft

AIAA S-110-2005 航天系统.结构部件和结构程序集

Space Systems Structures, Structural Components, and Structural Assemblies

Space Systems Structures, Structural Components, and Structural Assemblies

ASTM F2425-05a(2009) 重量转换控制航空器用持续适航性系统的标准规范

1.1 The following continued airworthiness requirements apply for the manufacture of weight-shift-control aircraft and their qualification for possible certification. 1.2 This specification applies to 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 Continued Airworthiness System for Weight-Shift-Control Aircraft

ASTM F2353-05(2008) 轻于空气的轻型运动飞机用制造商质量保证程序的标准规范

1.1 This specification covers minimum requirements for a quality assurance program for lighter-than-air 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 requirements prior to use.

Standard Specification for Manufacturer Quality Assurance Program for Lighter-Than-Air Light Sport Aircraft

ASTM F2426-05a(2008) 动力伞降飞行器机翼接口资料的标准指南

1.1 This guide covers the manufacture of powered parachute aircraft and their qualification for certification. 1.2 This guide 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 to determine the applicability of regulatory limitations prior to use.

Standard Guide on Wing Interface Documentation for Powered Parachute Aircraft

ASTM F2427-05a(2008) 轻于空气的轻型运动飞机要求的产品信息的标准规范

1.1 This specification covers the manufacture of lighter-than-air light sport aircraft. 1.1.1 This specification covers the minimum requirements for information that shall be provided by the manufacturer or seller of new lighter-than-air aircraft as a part of the initial sale or transfer to the first end user. 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 to determine the applicability of regulatory limitations prior to use.

Standard Specification for Required Product Information to be Provided with Lighter-Than-Air Light Sport Aircraft

ASTM F2447-05(2009) 重量转移控制飞行器的生产验收试验程序的标准实施规程

The purpose of this practice is to establish that each production aircraft has been assembled properly and operates normally throughout its entire allowable flight envelope. If final assembly is completed outside of the main production facility, the manufacturer shall specify the required procedures and what persons are authorized to perform them.1.1 The following requirements apply for the manufacture of weight-shift-control aircraft. This practice includes the production acceptance test requirements for weight-shift-control aircraft. 1.2 This practice applies to 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 Practice for Production Acceptance Test Procedures for Weight-Shift-Control Aircraft

ASTM F2457-05(2009) 提供重量转移控制飞行器所要求的产品信息的标准规范

1.1 The following requirements apply for the manufacture of weight-shift-control aircraft. This specification includes Aircraft Operating Instructions (AOI) and Flight Training Supplement (FTS) requirements for aircraft that were designed and manufactured in accordance with ASTM Standards. 1.1.1 This specification covers the minimum requirements for information that shall be provided by the manufacturer or seller of new light sport aircraft, engines, or propellers as a part of the initial sale or transfer to the first-end user. 1.1.2 This specification does not apply to the sale or transfer of used light sport aircraft, engines, or propellers. 1.2 This specification applies to 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 limitations prior to use.

Standard Specification for Required Product Information to be Provided with Weight-Shift-Control Aircraft

ASTM F2354-05b(2010) 轻于空气的轻型娱乐飞行器持续耐飞性系统标准规范

1.1 This specification covers continued airworthiness requirements for the manufacture of lighter-than-air light sport aircraft and their qualification for possible certification. 1.2 The values stated in SI units are to be regarded as the standard. The values given in parentheses are for information only. 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 limitations prior to use.

Standard Specification for Continued Airworthiness System for Lighter-Than-Air Light Sport Aircraft

ASTM F2356-05a(2010) 轻于空气的轻型娱乐飞行器的生产验收测试系统的标准规范

1.1 This specification covers production acceptance test requirements for the manufacture of lighter-than-air 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 Specification for Production Acceptance Testing System for Lighter-Than-Air Light Sport Aircraft

ASTM F2427-05a(2010) 轻于空气的轻型运动飞机要求的产品信息的标准规范

1.1 This specification covers the manufacture of lighter-than-air light sport aircraft. 1.1.1 This specification covers the minimum requirements for information that shall be provided by the manufacturer or seller of new lighter-than-air aircraft as a part of the initial sale or transfer to the first end user. 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 to determine the applicability of regulatory limitations prior to use.

Standard Specification for Required Product Information to be Provided with Lighter-Than-Air Light Sport Aircraft

ASTM F2354-05b(2013) 轻于空气的轻型运动航空器用持续适航系统的标准规范

1.1 This specification covers continued airworthiness requirements for the manufacture of lighter-than-air light sport aircraft and their qualification for possible certification. 1.2 The values stated in SI units are to be regarded as the standard. The values given in parentheses are for information only. 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 limitations prior to use.

Standard Specification for Continued Airworthiness System for Lighter-Than-Air Light Sport Aircraft

ASTM F2356-05a(2013) 轻于空气的轻型运动航空器用生产验收测试系统的标准规范

1.1 This specification covers production acceptance test requirements for the manufacture of lighter-than-air 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 Specification for Production Acceptance Testing System for Lighter-Than-Air Light Sport Aircraft

HB 7742-2004 直升机桨叶包装、运输和贮存要求

Requirements of packaging,transportation and storage for helicopter blade

HB 7743-2004 直升机桨叶摆振阻尼器通用规范

General specification for helicopter blade lead-lag damper

ASTM F2448-04(2009) 重量转移控制飞行器用生产商质量保证体系的标准实施规程

The purpose of this practice is to provide the minimum requirements necessary for the establishment of a written quality assurance program for a light sport aircraft manufacturer, or component supplier. If final assembly is completed outside of the main production facility, the manufacturer shall specify the required procedures and what persons are authorized to perform them.1.1 This practice covers minimum requirements for a quality assurance program for weight-shift-control aircraft. 1.2 This practice applies to weight-shift-control 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 limitations prior to use.

Standard Practice for Manufacturer Quality Assurance System for Weight-Shift-Control Aircraft

ASTM F2245-04 轻型运动飞机的设计和性能的标准规范

1.1 This specification covers airworthiness requirements for the design of powered fixed wing light sport aircraft, an "airplane."1.2 This specification is applicable to the design of a light sport aircraft/airplane as defined by regulations and limited to day VFR flight.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 of a Light Sport Airplane