ImageVerifierCode 换一换
格式:PDF , 页数:2 ,大小:59.22KB ,
资源ID:189740      下载积分:9 积分
快捷下载
登录下载
邮箱/手机:
温馨提示:
快捷下载时,用户名和密码都是您填写的邮箱或者手机号,方便查询和重复下载(系统自动生成)。 如填写123,账号就是123,密码也是123。
特别说明:
请自助下载,系统不会自动发送文件的哦; 如果您已付费,想二次下载,请登录后访问:我的下载记录
支付方式: 支付宝扫码支付 微信扫码支付   
验证码:   换一换

加入VIP,免费下载
 

温馨提示:由于个人手机设置不同,如果发现不能下载,请复制以下地址【https://www.wnwk.com/docdown/189740.html】到电脑端继续下载(重复下载不扣费)。

已注册用户请登录:
账号:
密码:
验证码:   换一换
  忘记密码?
三方登录: QQ登录  

下载须知

1: 本站所有资源如无特殊说明,都需要本地电脑安装OFFICE2007和PDF阅读器。
2: 试题试卷类文档,如果标题没有明确说明有答案则都视为没有答案,请知晓。
3: 文件的所有权益归上传用户所有。
4. 未经权益所有人同意不得将文件中的内容挪作商业或盈利用途。
5. 本站仅提供交流平台,并不能对任何下载内容负责。
6. 下载文件中如有侵权或不适当内容,请与我们联系,我们立即纠正。
7. 本站不保证下载资源的准确性、安全性和完整性, 同时也不承担用户因使用这些下载资源对自己和他人造成任何形式的伤害或损失。

版权提示 | 免责声明

本文(ASTM_F_2242_-_05_2013.pdf)为本站会员(益****师)主动上传,蜗牛文库仅提供信息存储空间,仅对用户上传内容的表现方式做保护处理,对上载内容本身不做任何修改或编辑。 若此文所含内容侵犯了您的版权或隐私,请立即通知蜗牛文库(发送邮件至admin@wnwk.com或直接QQ联系客服),我们立即给予删除!

ASTM_F_2242_-_05_2013.pdf

1、Designation:F224205(Reapproved 2013)Standard Specification forProduction Acceptance Testing System for PoweredParachute Aircraft1This standard is issued under the fixed designation F2242;the number immediately following the designation indicates the year oforiginal adoption or,in the case of revisio

2、n,the year of last revision.A number in parentheses indicates the year of last reapproval.Asuperscript epsilon()indicates an editorial change since the last revision or reapproval.1.Scope1.1 The following requirements apply for the manufacturepowered parachute aircraft.This specification includes th

3、eproduction acceptance test requirements for powered parachuteaircraft.1.2 This specification applies to powered parachute aircraftseeking civil aviation authority approval,in the form of flightcertificates,flight permits,or other like documentation.1.3 This standard does not purport to address all

4、of thesafety concerns,if any,associated with its use.It is theresponsibility of the user of this standard to establish appro-priate safety and health practices and determine the applica-bility of regulatory requirements prior to use.2.Terminology2.1 Definitions:2.1.1 powered parachute,naircraft comp

5、rised of a flexibleor semi-rigid wing connected to a fuselage in such a way thatthe wing is not in position for flight until the aircraft is inmotion.This aircraft has a fuselage with seats,engine,andwheels(or floats),such that the wing and engine cannot beflown without the wheels(or floats)and seat

6、(s).Unique to thepowered parachute is the large displacement between thecenter of lift(high)and the center of gravity(low),which ispendulum effect.Pendulum effect limits angle of attachchanges,provides stall resistance and maintains flight stability.3.Significance and Use3.1 The purpose of this spec

7、ification is to provide theminimum requirements for the establishment of a ground andflight test program for verifying the initial(first run)productionaircraft meets certain operational performance requirementsthat have been set forth by the manufacturer in its AircraftOperating Instructions.3.2 In

8、addition,this specification provides minimum re-quirements to verify that each subsequent production airplanehas no obvious defects that would prevent the safe operation ofthe airplane.4.Production Acceptance Testing,Ground Testing4.1 Inspection VerificationThere shall be a written proce-dure in eff

9、ect to verify all top-level inspections have beencompleted and no discrepancies remain open.4.2 Engine Break-InThere shall be a written procedure ineffect to perform the engine break-in.This procedure mayinclude all engine gage verification of operation.All enginereadings shall achieve the normal ac

10、cepted range of readingscommensurate with a new engine.If not performed duringengine break-in,then this verification must be performed underseparate procedures.All engine gages shall be verified to beoperating.5.Production Acceptance Testing,Flight Testing5.1 Every production aircraft shall be fligh

11、t tested to thefollowing minimums:5.1.1 Powered ParachutesFifteen minutes flight time,including at least one takeoff and landing,trimming of flightcontrols,and verification of control for left turn,right turn,andflare(flare only if so equipped).5.2 Instrument VerificationThere shall be a written pro

12、ce-dure in effect to verify that all other instruments are operatingwithin normal ranges.If equipped with a compass,the compassvariation card data shall be developed with the engine running.6.Post Flight Acceptance6.1 There shall be a written procedure in effect to performpost flight inspection that

13、 will review all flight critical attach-ments and structures.6.2 The reviewing personnel shall sign all post flight reviewdocuments.7.Documentation:7.1 There shall be a written procedure in effect to properlydocument and store the production acceptance test results suchthat they are correlated to th

14、e specific aircraft for futurereference.1This specification is under the jurisdiction of ASTM Committee F37 on LightSport Aircraft and is the direct responsibility of Subcommittee F37.30 on PowerParachute.Current edition approved June 1,2013.Published August 2013.Originallyapproved in 2003.Last prev

15、ious edition approved in 2008 as F2242 05(2008).DOI:10.1520/F2242-05R13.Copyright ASTM International,100 Barr Harbor Drive,PO Box C700,West Conshohocken,PA 19428-2959.United States1 7.2 Test Failures:7.2.1 There shall be a written procedure in effect to reviewthe causes for any aircraft failures in

16、the production acceptancetests phases.Aircraft may only be released for retest aftermanufacturing review of the discrepant articles and writtenrelease for retest.8.Keywords8.1 light sport aircraft;powered parachute aircraft;specialairworthiness certificateASTM International takes no position respecting the validity of any patent rights asserted in connection with any item mentionedin this standard.Users of this standard are expressly advised that determination of the validity of any such patent

copyright@ 2008-2023 wnwk.com网站版权所有

经营许可证编号:浙ICP备2024059924号-2