ASTM F3199-2016 Standard Guide for Wing Interface Documentation for Weight Shift Control Aircraft《重量变化控制航空器机翼接口文件的标准指南》.pdf

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1、Designation: F3199 16Standard Guide forWing Interface Documentation for Weight Shift ControlAircraft1This standard is issued under the fixed designation F3199; the number immediately following the designation indicates the year oforiginal adoption or, in the case of revision, the year of last revisi

2、on. 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 Weight Shiftaircraft and their qualification for certification.1.2 This guide applies to Wei

3、ght Shift Control 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 theresponsibility of the user of this st

4、andard to establish appro-priate safety and health practices and determine the applica-bility of regulatory limitations prior to use.2. Referenced Documents2.1 ASTM Standards:2F2241 Specification for ContinuedAirworthiness System forPowered Parachute AircraftF2972 Specification for Light Sport Aircr

5、aft ManufacturersQuality Assurance SystemF2425 Specification for ContinuedAirworthiness System forWeight-Shift-Control AircraftF2457 Specification for Required Product Information to beProvided withWeight-Shift-Control AircraftF2317/F2317M Specification for Design of Weight-Shift-Control Aircraft3.

6、Terminology3.1 Definitions:3.1.1 weight-shift-control aircraft, na powered aircraftwith a framed pivoting wing and a fuselage controllable only inpitch and roll by the pilots ability to change the aircraftscenter of gravity with respect to the wing. Flight control of theaircraft depends on the wings

7、 ability to flexibly deform ratherthan the use of control surfaces.4. Interface Documentation4.1 Interface documentation is the data necessary for theaircraft manufacturer to complete overall certification toASTM Weight Shift Control standards. The following datarepresents a guide to recommended typ

8、e, 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 be main-tained at a current status

9、and referenced by documents pro-vided with each delivered product.4.2.1 Quality Assurance ManualIn order to meet therequirements of Specification F2972, it will be necessary forthe manufacturer to have a current copy of the subcontractorsquality assurance manual on file. This manual needs to showtha

10、t 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 order to meet the re-quirements of S

11、pecification F2241, 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 F2425, it will be necessary forthe manufacturer to have a current copy

12、of the subcontractorsproduction acceptance testing written procedure on file.4.2.4 Maintenance Manual CoordinationIn order to meetthe requirements of Specification F2457, it will be necessaryfor the manufacturer to have a current copy of the subcontrac-tors maintenance manual on file.4.2.5 Statement

13、 of Conformance CoordinationIn order tomeet the requirements for Specification F2317/F2317M, it willbe necessary for the manufacturer to have on file a current copyof the subcontractors statement of conformance coordinationdocument describing what is covered by the statement ofconformance, as provid

14、ed by the subcontractor.1This guide is under the jurisdiction of ASTM Committee F37 on Light SportAircraft and is the direct responsibility of Subcommittee F37.40 on Weight Shift.Current edition approved June 1, 2016. Published July 2016. DOI: 10.1520/F3199-16.2For referenced ASTM standards, visit t

15、he ASTM website, www.astm.org, orcontact ASTM Customer Service at serviceastm.org. For 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.

16、United States14.3 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 Date of DocumentationThis is when the documen-tation was prepared for the specific unit prese

17、nted.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 Lengths of appropriate cable, cords, or struts, orcombinations thereof, with appropriate tolerances.4.3.3.2 Tensions of appropriate cables where applicablewi

18、th appropriate tolerances.4.3.3.3 Batten profile charts.4.3.3.4 Tuning parameters for wing cloth tension and wingtip rotation angles where applicable.4.3.3.5 Any other pertinent data or instructions.4.3.4 Design Ultimate Load in PoundsThis the numberused by the manufacturer to show compliance with t

19、he requiredultimate load factor based on the manufacturers design grossweight.4.3.5 Quality Assurance Manual Date ReferenceThe ref-erence date provides unit-specific assurance that the manual onfile at the manufacturer is the current document.4.3.6 Quality Assurance Audit, latest date audited.4.3.7

20、Wing Top Drawing Number, revision level and datereleased.4.3.8 Continued Airworthiness Manual Date ReferenceThe reference date provides unit-specific assurance that themanual on file at the manufacturer is the current document.4.3.9 Backup data storage location.4.3.10 Production Acceptance Test Docu

21、ment DateReferenceThe reference date provides unit specific assurancethat the manual on file at the manufacturer is the currentdocument.4.3.11 Maintenance Manual Date ReferenceThe referencedate provides unit specific assurance that the manual on file atthe manufacturer is the current document.4.3.12

22、 Statement of Compliance Coordination DocumentDate ReferenceThe reference date provides unit specificassurance that the manual on file at the manufacturer is thecurrent document.4.3.13 Signature of responsible subcontractor administrator.5. Recommended Data Sheets5.1 The following exhibits provide a

23、n example format ofhow the necessary data may be presented.5.2 See Fig. 1.6. Keywords6.1 light sport aircraft; special airworthiness certificates;weight shift control aircraftF3199 162ASTM International takes no position respecting the validity of any patent rights asserted in connection with any it

24、em mentionedin this standard. 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 com

25、mittee and must be reviewed 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

26、meeting of theresponsible 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 Driv

27、e, 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). Permission rights to photocopy the standard may also be secured from the Copyright Clearance Center, 222Rosewood Drive, Danvers, MA 01923, Tel: (978) 646-2600; http:/ 1 Supporting Data SheetF3199 163