V43 动力安装与操纵 标准查询与下载



共找到 37 条与 动力安装与操纵 相关的标准,共 3

1.1 This specification covers minimum requirements for the installation and integration of powerplant system units. 1.2 This specification is applicable to small aeroplanes as defined in the F44 terminology standard. Use of the term airplane is used throughout this specification and will mean “small airplane.” 1.3 The applicant for a design approval must seek the individual guidance to their respective CAA body concerning the use of this standard as part of a certification plan. For information on which CAA regulatory bodies have accepted this standard (in whole or in part) as a means of compliance to their Small Aircraft Airworthiness regulations (Hereinafter referred to as “the Rules”), refer to the ASTM F44 webpage (www.ASTM.org/COMITTEE/F44.htm) which includes CAA website links. 1.4 References within this standard normally refer to documents in United States legal system. Appendix X1 cross references documents in the legal system of other countries of corresponding content. 1.5 Units—The values stated are SI units followed by imperial units in brackets. The values stated in each system may not be exact equivalents; therefore, each system shall be used independently of the other. Combining values from the two systems may result in non-conformance with the standard. 1.6 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. 1.7 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 Aircraft Powerplant Installation

ICS
49.050
CCS
V43
发布
2019
实施

1.1 This specification covers minimum requirements for hazard mitigation in propulsion systems installed on small aeroplanes. 1.2 The applicant for a design approval must seek the individual guidance to their respective CAA body concerning the use of this standard as part of a certification plan. For information on which CAA regulatory bodies have accepted this standard (in whole or in part) as a means of compliance to their Small Aircraft Airworthiness regulations (Hereinafter referred to as “the Rules”), refer to ASTM F44 webpage (www.ASTM.org/COMITTEE/F44.htm) which includes CAA website links. 1.3 Units—The values stated are SI units followed by imperial units in brackets. The values stated in each system may not be exact equivalents; therefore, each system shall be used independently of the other. Combining values from the two systems may result in non-conformance 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 Aircraft Powerplant Installation Hazard Mitigation

ICS
49.050
CCS
V43
发布
2017
实施

Aircraft Propulsion System Performance Station Designation and Nomenclature

ICS
01.040.49;49.050
CCS
V43
发布
2013-06-05
实施

This document has been declared ""Stabilized"" and will no longer be subjected to periodic reviews for currency. Users are responsible for verifying references and continued suitability or technical requirements. New technology may exist. This aerospace recommended practice covers the design, installation, tests and data requirements of stored cold gas blowdown systems or subsystems for use in guided projectiles and tactical missiles. The term system, hereafter, refers to units which function as aerodynamic surface control devices, valve actuated control devices, reaction control devices and sensing/control devices.

Cold Gas Systems, Missile or Projectiles Design, Installation, Tests and Requirements for

ICS
49.140
CCS
V43
发布
2013-06-05
实施

This document provides guidance for laser operators and aviation authorities to determine the performance criteria that laser hazard control measures shall meet for the operation of an outdoor laser system in navigable airspace. The document does not cover systems intended to deliberately aim and or track lasers at aircraft except for FAA approved purposes, such as visual warning systems, search and rescue, etc. Aircraft operations to be protected include all types that can be reasonably expected to operate in the affected area, which are traveling at speeds and altitudes defined in the Performance/Functional Requirements section. This document does not add

Performance Criteria for Laser Control Measures Used for Aviation Safety

ICS
31.260;49.020
CCS
V43
发布
2013-05-09
实施

This document has been declared ""Stabilized"" and will no longer be subjected to periodic reviews for currency. Users are responsible for verifying references and continued suitability or technical requirements. New technology may exist.

Propeller Shaft Ends, Dual Rotation (Propeller Supplied Bearing)

ICS
49.050
CCS
V43
发布
2013-03-11
实施

This document has been declared ""Stabilized"" and will no longer be subjected to periodic reviews for currency. Users are responsible for verifying references and continued suitability or technical requirements. New technology may exist.

Propeller Blades Aluminum Alloy, Shank Dimensions for

ICS
49.050
CCS
V43
发布
2013-03-11
实施

This document has been declared ""Stabilized"" and will no longer be subjected to periodic reviews for currency. Users are responsible for verifying references and continued suitability or technical requirements. New technology may exist. This envelope applies to controls for use on reduction gear sections designed after date of issue.

Propeller Control Installation Clearance

ICS
49.050
CCS
V43
发布
2013-02-05
实施

This International Standard defines the general characteristics, reduirements and design data to be included in the procurement technical specification of an electrohydrostatic actuator (EHA) to be used to power aircraft control surfaces or other moving parts of an aerospace vehicle. This type of actuator is an alternative to the hydraulically powered servo-control actuators that are currently Used. ltis intended that this International Standard cover the unidue reduirements of EHASs.

Aerospace - Electrohydrostatic actuator (EHA) - Characteristics to be defined in procurement specifications

ICS
49.080
CCS
V43
发布
2011-08
实施

本部分规定了有人驾驶固定翼飞机进行飞行控制科研试飞训练的通用要求。 本部分适用于有人驾驶固定翼飞机飞行控制科研试飞训练的技术准备、组织实施与评价。特种用途固定翼军用飞机可参照执行。

Training requirements of flight test research for military aircraft.Part 17:Flight control

ICS
CCS
V43
发布
2010-09-16
实施
2010-12-01

本标准规定了机载正前方控制板的要求、质量保证和交货准备。 本标准适用于战斗机及教练机机载正前方控制板。

General specification for airborne up front control panel

ICS
CCS
V43
发布
2010-09-16
实施
2010-12-01

本部分规定了有人驾驶固定翼飞机进行机载武器火控科研试飞训练的通用要求。 本部分适用于有人驾驶固定翼飞机机载武器火控科研试飞训练的技术准备、组织实施与评价。特种用途固定翼军用飞机可参照执行。

Training requirements of flight test research for military aircraft.Part 13:Airborne weapon fire control

ICS
CCS
V43
发布
2010-09-16
实施
2010-12-01

本部分规定了有人驾驶固定翼飞机进行环境控制科研试飞训练的通用要求。 本部分适用于有人驾驶固定翼飞机环境控制科研试飞训练的技术准备、组织实施与评价。特种用途固定翼军用飞机可参照执行。

Training requirement of flight test research for military aircraft.Part 15:Aircraft environment control

ICS
CCS
V43
发布
2010-09-16
实施
2010-12-01

MIL-HDBK-762, dated 24 October 2000, has been reviewed and determined to be valid for use in acquisition.

DESIGN OF AERODYNAMICALLY STABILIZED FREE ROCKETS

ICS
49.045
CCS
V43
发布
2006-03-08
实施

This International Standard defines the general characteristics, requirements and design data to be included in the procurement technical specification of an electrohydrostatic actuator (EHA) to be used to power aircraft control surfaces or other moving parts of an aerospace vehicle. This type of actuator is an alternative to the hydraulically powered servocontrol actuators that are currently used. It is intended that this International Standard cover the unique requirements of EHAs. Test methods are defined in a separate ISO document.

Aerospace - Electrohydrostatic actuator (EHA) - Characteristics to be defined in procurement specifications

ICS
49.080
CCS
V43
发布
2005-06
实施

MIL-HDBK-762, dated 17 July 1990, has been reviewed and determined to be valid for use in acquistion.

DESIGN OF AERODYNAMICALLY STABILIZED FREE ROCKETS

ICS
49.045
CCS
V43
发布
2000
实施

本标准规定了飞机清洗剂的技术要求、试验方法、质量检验规定、包装、标志、运输和贮存。 本标准适用于可生物降解、水基、水稀释、环保型飞机清洗剂。

aircraft cleaner

ICS
CCS
V43
发布
1998-11-27
实施
1999-07-01

本标准规定了以活塞式和涡轮工发动机为动力的民用航空器上所用的动力装置火警探测系统必须满足的最低性能要求。   本标准适用于以下基本类型的火警探测系统或其组合:   a.Ⅰ型──热敏型(设定报警温度)当探测系统的传感器所处环境温度高于预先设定的报警温度时,应发出的警信号;   b.Ⅱ型──热敏型(设定上升速率)当探测系统的传感器所处环境温度的上升速率在预先设定值以上时,应发出报警信号;   c.Ⅲ型──火焰接触型 当探测系统的传感器处在火焰中与火焰体接触时,应发出报警信号。

Minimum performance requirements for civil aircraft powerplant fire detection systems (heat sensitive and flame contact types)

ICS
CCS
V43
发布
1996-09-13
实施
1996-10-01

本标准规定了以活塞式发动机和涡轮式发动机为动力的民用航空器上所用的动力装置火警探测系统必须满足的最低安全性能要求。   本标准适用于航空器动力装置、辅助动力装置、燃烧加热器和其它有可能发生火灾的装置上使用的辐射敏感型火警探测系统。

Minimum performance requirements for civil aircraft fire detection system (radiation sensitive type)

ICS
CCS
V43
发布
1996-09-13
实施
1996-10-01

本标准规定了民用航空器火区固定式Halon1301灭火系统必须满足的最低安全性能要求。   本标准适用于民用航空器火区固定式Halon1301灭火系统。

Minimum Performance Requirements for Civil Aircraft Halon 1301 Fire Extinguishing System

ICS
CCS
V43
发布
1996-09-13
实施
1996-10-01



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