ASTM F2353-2005(2008) Standard Specification for Manufacturer Quality Assurance Program for Lighter-Than-Air Light Sport Aircraft《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》.pdf

《ASTM F2353-2005(2008) Standard Specification for Manufacturer Quality Assurance Program for Lighter-Than-Air Light Sport Aircraft《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》.pdf》由会员分享，可在线阅读，更多相关《ASTM F2353-2005(2008) Standard Specification for Manufacturer Quality Assurance Program for Lighter-Than-Air Light Sport Aircraft《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》.pdf（2页珍藏版）》请在麦多课文档分享上搜索。

1、Designation: F 2353 05 (Reapproved 2008)Standard Specification forManufacturer Quality Assurance Program for Lighter-Than-Air Light Sport Aircraft1This standard is issued under the fixed designation F 2353; the number immediately following the designation indicates the year oforiginal adoption or, i

2、n the case of revision, 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 This specification covers minimum requirements for aquality assurance program for

3、lighter-than-air light sport air-craft.1.2 This standard does not purport to address all 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 r

4、equirements prior to use.2. Significance and Use2.1 The purpose of this specification is to provide theminimum requirements necessary for the establishment of awritten quality assurance program for a light sport aircraftmanufacturer, or component supplier.2.2 Off-Site Final AssemblyOff-site final as

5、sembly ordivided production facilities, or both, are specifically allowed ifthe QA procedures specify the applicable QA requirements forthe activities being conducted at the final assembly or produc-tion facility where the activity is being conducted, or both.These QA requirements shall be consisten

6、t with this specifica-tion.3. Drawing Control Procedure3.1 A written procedure shall be in effect so that appropriatemanufacturing drawings, their manufacturing revisions, andrelated documents are utilized for each project.4. Material and Component Control Procedure4.1 A written procedure shall be i

7、n effect so that materials,processes, and components, including raw materials, are inaccordance with the manufacturing specifications.4.1.1 This procedure shall provide the purchasing agentwith all the information required to order appropriate material.4.1.2 A written receiving procedure shall be in

8、 effect so thatincoming material and components are checked against thepurchasing specifications.4.1.3 A written procedure shall be in effect so that materialin stock can be properly identified for future use.4.1.4 Documentation on any material, process, or compo-nents certified shall be filed for r

9、eference.5. Inspection5.1 A written procedure shall be in effect so that appropriateinspections are made on manufactured parts and subassem-blies, for conformance with engineering specifications.5.2 A written procedure shall be in effect so that appropriateinspections are made on purchased component

10、s.5.3 A written procedure shall be in effect so that completedunits are inspected prior to delivery.5.4 Nonconforming components shall be identified andevaluated for disposition as follows:5.4.1 A component not suitable for use shall be altered ordisposed of to avoid accidental use.5.4.2 Reworked co

11、mponents shall be re-inspected in accor-dance with 5.1, 5.2,or5.3 of this practice prior to use.5.4.3 In some cases, a component may be determined to be“acceptable as is” or “as modified” after further evaluation. Insuch cases, appropriate review, acceptance, and documentationshall be a requirement.

12、6. Audits6.1 A written procedure shall be in effect to perform auditsof the Quality Assurance Program at least once every twoyears.7. Keywords7.1 Aircraft Operating Instructions; airplane; airship; bal-loon; lighter-than-air; light sport aircraft; powered parachuteaircraft; rotorcraft; special airwo

13、rthiness certificate; weightshift control1This specification is under the jurisdiction of ASTM Committee F37 on LightSport Aircraft and is the direct responsibility of Subcommittee F37.60 on Lighterthan Air.Current edition approved May 15, 2008. Published July 2008. Originallyapproved in 2004. Last

14、previous edition approved in 2005 as F 2353 05.1Copyright ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959, United States.ASTM International takes no position respecting the validity of any patent rights asserted in connection with any item mentionedin this st

15、andard. Users of this standard are expressly advised that determination of the validity of any such patent rights, and the riskof infringement of such rights, are entirely their own responsibility.This standard is subject to revision at any time by the responsible technical committee and must be rev

16、iewed every five years andif not revised, either reapproved or withdrawn. Your comments are invited either for revision of this standard or for additional standardsand should be addressed to ASTM International Headquarters. Your comments will receive careful consideration at a meeting of theresponsi

17、ble technical committee, which you may attend. If you feel that your comments have not received a fair hearing you shouldmake your views known to the ASTM Committee on Standards, at the address shown below.This standard is copyrighted by ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959,United States. Individual reprints (single or multiple copies) of this standard may be obtained by contacting ASTM at the aboveaddress or at 610-832-9585 (phone), 610-832-9555 (fax), or serviceastm.org (e-mail); or through the ASTM website(www.astm.org).F 2353 05 (2008)2