ASTM F2426-2013 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

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1、Designation: F2426 13Standard Guide onWing Interface Documentation for Powered ParachuteAircraft1This standard is issued under the fixed designation F2426; the number immediately following the designation indicates the year oforiginal adoption or, in the case of revision, the year of last revision.

2、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 This guide applies to

3、powered parachute aircraft seekingcivil 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 theresponsibility of the user of this st

4、andard to establish appro-priate safety and health practices and to determine theapplicability of regulatory limitations prior to use.2. Referenced Documents2.1 ASTM Standards:2F2240 Specification for Manufacturer Quality AssuranceProgram for Powered Parachute AircraftF2241 Specification for Continu

5、edAirworthiness System forPowered Parachute AircraftF2242 Specification for Production Acceptance Testing Sys-tem for Powered Parachute AircraftF2243 Specification for Required Product Information to beProvided with Powered Parachute AircraftF2244 Specification for Design and Performance Require-men

6、ts for Powered Parachute AircraftF2483 Practice for Maintenance and the Development ofMaintenance Manuals for Light Sport AircraftF2563 Practice for Kit Assembly Instructions of AircraftIntended Primarily for Recreation3. Terminology3.1 Definitions:3.1.1 powered parachute, naircraft comprised of a f

7、lexibleor semi-rigid wing connected to a fuselage in such a way thatthe wing is not in position for flight until the aircraft is inmotion, that 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(s).

8、Unique to thepowered parachute is the large displacement between thecenter of lift (high) and the center of gravity (low), which is thependulum effect. The pendulum effect limits angle of attackchanges, provides stall resistance, and maintains flight stability.4. Interface Documentation4.1 Interface

9、 documentation is the data necessary for theaircraft manufacturer to complete overall certification toASTM powered parachute standards. The following datarepresents a guide to recommended type, detail, and generalformat for data transfer from a major subcontractor to theaircraft manufacturer.4.2 Man

10、ufacturers Reference DocumentsThe followingare reference documents that should be supplied to the manu-facturer by the subcontractor. These are intended to be main-tained at a current status and referenced by documents pro-vided with each delivered product.4.2.1 Quality Assurance ManualIn order to m

11、eet therequirements of Specification F2240, it will be necessary forthe manufacturer to have a current copy of the subcontractorsquality assurance manual on 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 in

12、spection,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 order to meet the re-quirements of Specification F2241, it will be necessary for themanufacturer to have a current copy of the subcontractorscont

13、inued airworthiness manual on file.4.2.3 Production Acceptance TestingIn order to meet therequirements of Specification F2242, it will be necessary for1This guide is under the jurisdiction of ASTM Committee F37 on Light SportAircraft and is the direct responsibility of Subcommittee F37.30 on PowerPa

14、rachute.Current edition approved June 1, 2013. Published July 2013. Originally approvedin 2004. Last previous edition approved in 2008 as F2426 05a (2008). DOI:10.1520/F2426-13.2For referenced ASTM standards, visit the ASTM website, www.astm.org, orcontact ASTM Customer Service at serviceastm.org. F

15、or Annual Book of ASTMStandards volume information, refer to the standards Document Summary page onthe ASTM website.Copyright ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959. United States1the manufacturer to have a current copy of the subcontractorsproductio

16、n acceptance testing written procedure on file.4.2.4 Maintenance Manual CoordinationIn order to meetthe requirements of Specification F2243, it will be necessaryfor the manufacturer to have a current copy of the subcontrac-tors maintenance manual on file.4.2.5 Statement of Conformance CoordinationIn

17、 order tomeet the requirements of Specification F2244, it will benecessary for the manufacturer to have on file a current copy ofthe subcontractors statement of conformance coordinationdocument describing what is covered by the statement ofconformance, as provided by the subcontractor.4.3 Data Provi

18、ded with Delivered ProductThis is theindividual product documentation that the manufacturers willdepend on to complete certification of their finished unit toASTM standards.4.3.1 Date of DocumentationThis is when the documen-tation was prepared for the specific unit presented.4.3.2 Identification of

19、 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 a table of “riser attachment spacing” versusacceptable associated “riser length” with appropriate toler-ances.4.3.3.2 Ri

20、ser 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 PoundsThis the numberused by the manufacturer to show compliance with the requiredultimate load factor based on the manufa

21、cturers 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 current document.4.3.5 Quality Assurance Audit, latest date audited.4.3.6 Wing Top Drawing Number, revision level and daterel

22、eased.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.4.3.8 Backup data storage location.4.3.9 Production Acceptance Test Document DateReferenceThe reference date provides unit s

23、pecific 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 that the manual onfile at the manufacturer is the current document.4.3.11 Statement of Compliance Coordination DocumentDate

24、 ReferenceThe reference date provides unit specificassurance that the manual on file at the manufacturer is thecurrent document.4.3.12 Signature of responsible subcontractor administrator.5. Recommended Data Sheets5.1 The following exhibits provide an example format ofhow the necessary data may be p

25、resented.5.2 See Fig. 1, supporting data sheet.6. Keywords6.1 light sport aircraft; powered parachute aircraft; specialairworthiness certificatesF2426 132ASTM International takes no position respecting the validity of any patent rights asserted in connection with any item mentionedin this standard.

26、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 reviewed ev

27、ery 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 theresponsible tech

28、nical 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 Conshohoc

29、ken, 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). Permission rights to photo

30、copy the standard may also be secured from the ASTM website (www.astm.org/COPYRIGHT/).FIG. 1 Supporting 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 a

31、re presented in the attached table of “riser attachment spacing” versus acceptable associated “riser length” with ap-propriate tolerances.2. Riser style, limits or part number _ A specific part number that meets the riser attachment spacing and length requirements may be de-fined.3. Control line pul

32、l limits: Maximum Overall (in.) _,Nominal for control: minimum (in.) _ maximum (in.) _4. Design ultimate load _ lbs.Reference documents:1. This wing meets the requirements of ASTM Specifications F2240 and F2244, and as it pertains to the wing and as agreed upon in the Statementof Conformance Coordin

33、ation Document _ dated _ (copy on file)2. The Quality Assurance Manual was dated _ (copy on file)3. The 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 _ (cop

34、y on file)6. Our backup copy of all wing certification documentation is stored at _7. Production Acceptance 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 R

35、equirements document _dated _ (copy on file)9. This is the Statement of Conformance for this specific 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 mustbe completed and coordinated with both the wing and carriage manufacturer, prior to release to the end user. The user must be directed to note the appropriatechange in the aircraft maintenance logs.Signed by the President or his designee:Signed _ title _F2426 133