ASTM F2240-2005 Standard Specification for Manufacturer Quality Assurance Program for Powered Parachute Aircraft《动力伞降飞行器的生产商质量保证计划的标准规范》.pdf

《ASTM F2240-2005 Standard Specification for Manufacturer Quality Assurance Program for Powered Parachute Aircraft《动力伞降飞行器的生产商质量保证计划的标准规范》.pdf》由会员分享，可在线阅读，更多相关《ASTM F2240-2005 Standard Specification for Manufacturer Quality Assurance Program for Powered Parachute Aircraft《动力伞降飞行器的生产商质量保证计划的标准规范》.pdf（2页珍藏版）》请在麦多课文档分享上搜索。

1、Designation: F 2240 05Standard Specification forManufacturer Quality Assurance Program for PoweredParachute Aircraft1This standard is issued under the fixed designation F 2240; the number immediately following the designation indicates the year oforiginal adoption or, in the case of revision, the ye

2、ar of last revision. A number in parentheses indicates the year of last reapproval. Asuperscript epsilon (e) indicates an editorial change since the last revision or reapproval.1. Scope1.1 This specification covers minimum requirements for aquality assurance program for powered parachute aircraft.1.

3、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 of thesafety concerns, if any, associated with its use. It is therespo

4、nsibility of the user of this standard to establish appro-priate safety and health practices and determine the applica-bility of regulatory limitations prior to use.2. Significance and Use2.1 The purpose of this specification is to provide theminimum requirements necessary for the establishment of a

5、written quality assurance program for a light sport aircraftmanufacturer, or component supplier.2.2 Off-Site Final AssemblyOff-site final assembly ordivided production facilities, or both, are specifically allowed ifthe QA procedures provide for training, reporting, and trackingconsistent with the o

6、verall QA system.3. Materials and Manufacture3.1 Drawing Control ProcedureA written procedure shallbe in effect so that appropriate manufacturing drawings, theirmanufacturing revisions, and related documents are utilized foreach project.3.2 Component Control Procedure:3.2.1 A written procedure shall

7、 be in effect so that materials,processes, and components, including raw materials, are inaccordance with the manufacturing specifications.3.2.2 This procedure shall provide the purchasing agentwith all of the information required to order appropriatematerial.3.2.3 A written receiving procedure shal

8、l be in effect so thatincoming material and components are checked against thepurchasing specifications.3.2.4 A written procedure shall be in effect so that materialin stock can be properly identified for future use.3.2.5 Documentation on any material, process, or compo-nents certified shall be file

9、d for reference.4. Inspection4.1 A written procedure shall be in effect so that appropriateinspections are made on manufactured parts and subassem-blies, for conformance with engineering specifications.4.2 A written procedure shall be in effect so that appropriateinspections are made on purchased co

10、mponents.4.3 A written procedure shall be in effect so that completedunits are inspected prior to delivery.4.4 Nonconforming components shall be identified andevaluated for disposition as follows:4.4.1 A component not suitable for use shall be altered ordisposed of to avoid accidental use.4.4.2 Rewo

11、rked components shall be re-inspected in accor-dance with 4.1, 4.2,or4.3 of this specification prior to use.4.4.3 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

12、requirement.4.5 AuditsA written procedure shall be in effect to per-form audits of the Quality Assurance Program at least onceevery two years.5. Keywords5.1 light sport aircraft; powered parachute aircraft; specialairworthiness certificate1This specification is under the jurisdiction of ASTM Committ

13、ee F37 on LightSport Aircraft and is the direct responsibility of Subcommittee F37.30 on PowerParachute.Current edition approved March 1, 2005. Published March 2005. Originallyapproved in 2003. Last previous edition approved in 2003 as F 2240 03.1Copyright ASTM International, 100 Barr Harbor Drive,

14、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 standard. Users of this standard are expressly advised that determination of the validity of any such p

15、atent 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 reviewed every five years andif not revised, either reapproved or withdrawn. Your comments are invited e

16、ither 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 theresponsible technical committee, which you may attend. If you feel that your comments have not received a fai

17、r 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).F2240052