ASTM F2426-2005a(2008) Standard Guide on Wing Interface Documentation for Powered Parachute Aircraft《动力伞降飞行器机翼接口资料的标准指南》.pdf

《ASTM F2426-2005a(2008) Standard Guide on Wing Interface Documentation for Powered Parachute Aircraft《动力伞降飞行器机翼接口资料的标准指南》.pdf》由会员分享，可在线阅读，更多相关《ASTM F2426-2005a(2008) Standard Guide on Wing Interface Documentation for Powered Parachute Aircraft《动力伞降飞行器机翼接口资料的标准指南》.pdf（3页珍藏版）》请在麦多课文档分享上搜索。

1、Designation: F 2426 05a (Reapproved 2008)Standard Guide onWing Interface Documentation for Powered ParachuteAircraft1This standard is issued under the fixed designation F 2426; 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 () indicates an editorial change since the last revision or reapproval.1. Scope1.1 This guide covers the manufacture of powered para-chute aircraft and their qualification for certification.1.2 T

3、his guide applies to powered parachute aircraft seekingcivil aviation authority approval, in the form of flight certifi-cates, 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 theresponsibility

4、 of the user of this standard to establish appro-priate safety and health practices and to determine theapplicability of regulatory limitations prior to use.2. Referenced Documents2.1 ASTM Standards:2F 2240 Specification for Manufacturer Quality AssuranceProgram for Powered Parachute AircraftF 2241

5、Specification for Continued Airworthiness Systemfor Powered Parachute AircraftF 2242 Specification for Production Acceptance TestingSystem for Powered Parachute AircraftF 2243 Specification for Required Product Information tobe Provided with Powered Parachute AircraftF 2244 Specification for Design

6、and Performance Require-ments for Powered Parachute Aircraft3. Terminology3.1 Definitions:3.1.1 powered parachute, naircraft comprised of a flex-ible or semi-rigid wing connected to a fuselage in such a waythat the wing is not in position for flight until the aircraft is inmotion, that aircraft has

7、a fuselage with seats, engine, andwheels (or floats), such that the wing and engine cannot beflown without the wheels (or floats) and seat(s). Unique to thepowered parachute is the large displacement between thecenter of lift (high) and the center of gravity (low), which is thependulum effect. The p

8、endulum effect limits angle of attackchanges, provides stall resistance, and maintains flight stability.4. Interface Documentation4.1 Interface documentation is the data necessary for theaircraft manufacturer to complete overall certification toASTM powered parachute standards. The following datarep

9、resents a guide to recommended type, detail, and generalformat for data transfer from a major subcontractor to theaircraft manufacturer.4.2 Manufacturers Reference DocumentsThe followingare reference documents that should be supplied to the manu-facturer by the subcontractor. These are intended to b

10、e main-tained at a current status and referenced by documents pro-vided with each delivered product.4.2.1 Quality Assurance ManualIn order to meet therequirements of Specification F 2240, it will be necessary forthe manufacturer to have a current copy of the subcontractorsquality assurance manual on

11、 file. This manual needs to showthat written procedures are in effect for:4.2.1.1 Drawing control,4.2.1.2 Component control,4.2.1.3 Receiving inspection,4.2.1.4 Material identification,4.2.1.5 Inspection,4.2.1.6 Non-conforming material handling, and4.2.1.7 QA audits.4.2.2 Continued AirworthinessIn o

12、rder to meet the re-quirements of Specification F 2241, it will be necessary for themanufacturer to have a current copy of the subcontractorscontinued airworthiness manual on file.4.2.3 Production Acceptance TestingIn order to meet therequirements of Specification F 2242, it will be necessary forthe

13、 manufacturer to have a current copy of the subcontractorsproduction acceptance testing written procedure on file.4.2.4 Maintenance Manual CoordinationIn order to meetthe requirements of Specification F 2243, it will be necessaryfor the manufacturer to have a current copy of the subcontrac-tors main

14、tenance manual on file.4.2.5 Statement of Conformance CoordinationIn order tomeet the requirements of Specification F 2244, it will benecessary for the manufacturer to have on file a current copy of1This guide is under the jurisdiction of ASTM Committee F37 on Light SportAircraft and is the direct r

15、esponsibility of Subcommittee F37.30 on PowerParachute.Current edition approved May 15, 2008. Published July 2008. Originallyapproved in 2004. Last previous edition approved in 2005 as F 2426 05a.2For referenced ASTM standards, visit the ASTM website, www.astm.org, orcontact ASTM Customer Service at

16、 serviceastm.org. For Annual Book of ASTMStandards volume information, refer to the standards Document Summary page onthe ASTM website.1Copyright ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959, United States.the subcontractors statement of conformance coordi

17、nationdocument describing what is covered by the statement ofconformance, as provided by the subcontractor.4.3 Data Provided with Delivered ProductThis is theindividual product documentation that the manufacturers willdepend on to complete certification of their finished unit toASTM standards.4.3.1

18、Date of DocumentationThis is when the documen-tation was prepared for the specific unit presented.4.3.2 Identification of the Product Provided:4.3.2.1 Make,4.3.2.2 Model, and4.3.2.3 Serial number.4.3.3 Interface Physical Limits:4.3.3.1 Riser attachment spacing and length limits are to bepresented as

19、 a table of “riser attachment spacing” versusacceptable associated “riser length” with appropriate toler-ances.4.3.3.2 Riser style, limits, or part number may be identifiedto meet a specific application,4.3.3.3 Control input limits, and4.3.3.4 Design load capability.4.3.3.5 Design Ultimate Load in P

20、oundsThis the numberused by the manufacturer to show compliance with the requiredultimate load factor based on the manufacturers design grossweight.4.3.4 Quality Assurance Manual Date ReferenceThe ref-erence date provides unit-specific assurance that the manual onfile at the manufacturer is the curr

21、ent document.4.3.5 Quality Assurance Audit, latest date audited.4.3.6 Wing Top Drawing Number, revision level and datereleased.4.3.7 Continued Airworthiness Manual Date ReferenceThe reference date provides unit-specific assurance that themanual on file at the manufacturer is the current document.4.3

22、.8 Backup data storage location.4.3.9 Production Acceptance Test Document DateReferenceThe reference date provides unit specific assurancethat the manual on file at the manufacturer is the currentdocument.4.3.10 Maintenance Manual Date ReferenceThe refer-ence date provides unit specific assurance th

23、at the manual onfile at the manufacturer is the current document.4.3.11 Statement of Compliance Coordination DocumentDate ReferenceThe reference date provides unit specificassurance that the manual on file at the manufacturer is thecurrent document.4.3.12 Signature of responsible subcontractor admin

24、istra-tor.5. Recommended Data Sheets5.1 The following exhibits provide an example format ofhow the necessary data may be presented.5.2 See Fig. 1, supporting data sheet.6. Keywords6.1 light sport aircraft; powered parachute aircraft; specialairworthiness certificateF 2426 05a (2008)2FIG. 1 Supportin

25、g Data SheetExhibit 1Company XYZPowered Parachute Wing Interface Documentation for Use on Light Sport AircraftDate _Wing Make _Wing Model _Wing Serial Number _1. Riser attachment and length limits are presented in the attached table of “riser attachment spacing” versus acceptable associated “riser l

26、ength” with appro-priate tolerances.2. Riser style, limits or part number _ A specific part number that meets the riser attachment spacing and length requirements may be defined.3. Control line pull limits: Maximum Overall (in.) _,Nominal for control: minimum (in.) _ maximum (in.) _4. Design ultimat

27、e load _ lbs.Reference documents:1. This wing meets the requirements of ASTM Specifications F 2240 and F 2244, and as it pertains to the wing and as agreed upon in the Statementof Conformance Coordination Document _ dated _ (copy on file)2. The Quality Assurance Manual was dated _ (copy on file)3. T

28、he latest Quality Assurance Audit was dated _ (copy of the certificate on file)4. This wing was produced to top drawing _ rev _ dated_5. The Continued Airworthiness Procedures Manual was dated _ (copy on file)6. Our backup copy of all wing certification documentation is stored at _7. Production Acce

29、ptance Test unique requirements have been coordinated through the PAT Document _ dated _ (copy on file)8. Unique Maintenance Manual requirements have been coordinated through the Maintenance Manual Requirements document _dated _ (copy on file)9. This is the Statement of Conformance for this specific

30、 wing, as signed below.Notes: If this wing is being used for replacement of an in-service craft, the procedures of direct replacement or replacement through additional factory testing must becompleted and coordinated with both the wing and carriage manufacturer, prior to release to the end user. The

31、 user must be directed to note the appropriate change inthe aircraft maintenance logs.Signed by the President or his designee:Signed _ title _ASTM International takes no position respecting the validity of any patent rights asserted in connection with any item mentionedin this standard. Users of thi

32、s 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 reviewed every five yea

33、rs 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 theresponsible technical commit

34、tee, 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 2426 05a (2008)3