V36 总体技术要求 标准查询与下载

ASTM F2427-04 轻于空气的轻型运动飞行器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 F2352-04a 轻型运动自转旋翼机的设计和性能的标准规范

1.1 This specification covers the manufacture of gyroplanes. This specification includes design and performance requirements for light sport gyroplane aircraft.1.2 This specification applies to light gyroplane aircraft seeking civil aviation authority approval in the form of flight certificates, flight permits, or other like documentation.1.3 A gyroplane for the purposes of this specification is defined as a rotorcraft to be used for day VFR only, with rotor blades that are not engine-driven in flight and are supported in flight by the reaction of the air on a single rotor that rotates freely on a substantially vertical axis when the aircraft is in horizontal flight.1.4 These requirements apply to light gyroplanes of orthodox design. Aircraft having the following basic features will be so regarded:1.4.1 Rotors of either fixed collective pitch or collective pitch control that are not adjustable in flight,1.4.2 Single engine with fixed or ground adjustable pitch propeller,1.4.3 No more than two occupant seats, and1.4.4 A maximum gross weight (MGW) of 725 kg (1600 lb) or less.1.5 Where it can be shown that a particular feature is similar in all significant respects to a feature that has historically demonstrated compliance with this specification and can be considered a separate entity in terms of its operation, that feature shall be deemed to be applicable and in compliance with this specification.1.6 Where these requirements are inappropriate to particular design and construction features, it will be necessary to submit an appropriate amendment of this specification to ASTM Committee F37 on Light Sport Aircraft for consideration and approval.1.7 The values in SI units are to be regarded as the standard. The values in parentheses are for information only.T1.8 his 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 Design and Performance of Light Sport Gyroplane Aircraft

ASTM F2352-04 轻型运动自转旋翼机的设计和性能的标准规范

1.1 This specification covers the manufacture of gyroplanes. This specification includes design and performance requirements for light sport gyroplane aircraft.1.2 This specification applies to light gyroplane aircraft seeking civil aviation authority approval in the form of flight certificates, flight permits, or other like documentation.1.3 A gyroplane for the purposes of this specification is defined as a rotorcraft to be used for day VFR only, with rotor blades that are not engine-driven in flight and are supported in flight by the reaction of the air on a single rotor that rotates freely on a substantially vertical axis when the aircraft is in horizontal flight.1.4 These requirements apply to light gyroplanes of orthodox design. Aircraft having the following basic features will be so regarded:1.4.1 Rotors of either fixed collective pitch or collective pitch control that are not adjustable in flight,1.4.2 Single engine with fixed or ground adjustable pitch propeller,1.4.3 No more than two occupant seats, and1.4.4 A maximum gross weight (MGW) of 725 kg (1600 lb) or less.1.5 Where it can be shown that a particular feature is similar in all significant respects to a feature that has historically demonstrated compliance with this specification and can be considered a separate entity in terms of its operation, that feature shall be deemed to be applicable and in compliance with this specification.1.6 Where these requirements are inappropriate to particular design and construction features, it will be necessary to submit an appropriate amendment of this specification to ASTM Committee F37 on Light Sport Aircraft for consideration and approval.1.7 The values in SI units are to be regarded as the standard. The values in parentheses are for information only.T1.8 his 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 Design and Performance of Light Sport Gyroplane Aircraft

ASTM F2415-04a 轻型运动自转旋翼机的持续适航系统的标准实施规程

1.1 This practice covers continued operational safety monitoring of light sport gyroplane aircraft.1.2 This practice applies to light sport gyroplane aircraft seeking civil aviation authority approval in the form of flight certificates, flight permits, or other like documentation. This practice applies to kit and ready-to-fly aircraft supplied by a manufacturer.1.3 The values stated in SI units are to be regarded as the standard. The values given in parentheses are for information only.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 determine the applicability of regulatory limitations prior to use.

Standard Practice for Continued Airworthiness System for Light Sport Gyroplane Aircraft

ASTM F2415-04 轻型运动自转旋翼机的持续适航系统的标准实施规程

1.1 This practice covers continued operational safety monitoring of light sport gyroplane aircraft.1.2 This practice applies to light sport gyroplane aircraft seeking civil aviation authority approval in the form of flight certificates, flight permits, or other like documentation. This practice applies to kit and ready-to-fly aircraft supplied by a manufacturer.1.3 si-value;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 Airworthiness System for Light Sport Gyroplane Aircraft

SAE ARP1409C-2003 (R)飞机机载重量与平衡系统要求

This SAE Aerospace Recommended Practice (ARP) establishes requirements for the function, characteristics and installation of an aircraft On Board Weight and Balance System (OBWBS) for use on civil transport aircraft. This document is not intended to specify design methods, mechanisms or material to accomplish the requirements set forth.

(R) Aircraft On Board Weight and Balance System Requirements

ASTM F2244-03 带动力伞飞行器的设计和性能要求的标准规范

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 Applicability8212;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

ASTM F2241-03 带动力伞飞行器的连续适航性系统的标准规范

1.1 The following continued airworthiness requirements apply for the manufacture of Powered Parachute Aircraft and their qualification for possible certification.1.2 Applicability8212;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 Continued Airworthiness System for Powered Parachute Aircraft

ASTM F2243-03 带动力伞飞行器所需提供的产品信息的标准规范

1.1 The following requirements apply for the manufacture of Powered Parachute aircraft. This standard includes pilot operating handbook requirements for powered parachute aircraft that were designed and manufactured per 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 Applicability8212;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 Required Product Information to be Provided with Powered Parachute Aircraft

ASTM F2240-03 带动力伞飞行器的生产商质量保证计划的标准规范

1.1 This practice covers minimum requirements for a quality assurance program for powered parachute aircraft.1.2 Applicability8212;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 limitations prior to use.

Standard Specification for Manufacturer Quality Assurance Program for Powered Parachute Aircraft

ASTM F2242-03 带动力伞飞行器的生产验收测试系统的标准规范

1.1 The following requirements apply for the manufacture powered parachute aircraft. This standard includes the production acceptance test requirements for powered parachute aircraft.1.2 Applicability8212;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 Production Acceptance Testing System for Powered Parachute Aircraft

HB 7713-2002 飞机结构静强度试验通用要求

General requirements of static strength test for aircraft structure

KS V ISO 10133:2001 小型船舶.电气系统.超低压直流装置

이 규격은 길이 24 m 이하의 소형 선박에서 사용하는 정격 전압 50 V 미만의 저전압

Small craft-Electrical systems-Extra-low-voltage d.c. installations

HB 7707-2001 固定飞机护罩旋钮

Fixed Aircraft Shield Knobs

SAE ARP1107B-2001 有人驾驶飞机的尾部缓冲器

This document provides recommended practices for the design, installation, qualification, and operational requirements of the tail bumper for piloted aircraft. This recommended practice covers the fixed structure, or independent energy absorbing system affixed to the airframe to afford protection to the control surfaces, engine and other portions during ground handling, take-off and landing.

Tail Bumpers for Piloted Aircraft

SAE ARP1786-2000 针对飞机应用的轮缘上车轮轧辊标准

This Aerospace Recommended Practice (ARP) is to provide a recommended minimum laboratory roll performance for main landing gear aircraft wheel without tire.

Wheel Roll on Rim Criteria for Aircraft Application

ISO 10133:2000 小艇 电气系统 超低压直流装置

This International Standard specifies the requirements for the design, construction and installation of extra-low-voltage direct current (d.c.) electrical systems which operate at nominal potentials of 50 V d.c. or less on small craft of hull length up to 24 m. Engine wiring as supplied by the engine manufacturer is not covered by this International Standard.

Small craft - Electrical systems - Extra-low-voltage d.c. installations

SAE ARP1048A-2000 一般航空飞行器用设备和座舱照明

This document establishes acceptable design criteria for instrument and cockpit illumination for general aviation aircraft.

Instrument and Cockpit Illumination for General Aviation Aircraft

SAE ARP1270A-2000 飞行器舱加压控制标准

These recommendations cover the basic criteria for the design of aircraft cabin pressurization control systems as follows: 1. To ensure aircraft safety 2. Physiology and limits which govern maximum permissible pressure time relations as related to aircraft passenger comfort. 3. General pressurization control system performance requirements design to satisfy (2). 4. Technical considerations relevant to satisfying (3). The purpose of the recommended practice is to provide the aerospace industry with guidelines as to the pertinent technology relating to the physiological consideration, the technical system requirements and design objectives for aircraft pressurization control systems. This recommended practice is applicable to pressurized aircraft regardless of the number of passengers or crew. The pressurization control system must provide maximum safety and passenger and crew comfort as a result of changes in cabin pressure altitude during the entire aircraft flight and during ground operation.

Aircraft Cabin Pressurization Control Criteria

KS W 1536-1999 航空航天.附属设备和安装法兰(米制系列).第1部分:设计规范

이 규격은 항공기 기어 박스나 엔진 부속 장치에 사용하는 주요 설비를 신속하게 장착/탈착할

Aerospace-Accessory drives and mounting flanges(Metric series)-Part 1:Design criteria