ASTM F3199-2016a Standard Guide for Wing Interface Documentation for Weight Shift Control Aircraft《重量转移控制飞行器的机翼接口文档的标准指南》.pdf

1、Designation: F3199 16aStandard 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 revis

2、ion. 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 We

3、ight 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 s

4、tandard 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:2F2317/F2317M Specification for Design of Weight-Shift-Control AircraftF2425 Specification for ContinuedAirworthiness System

5、 forWeight-Shift-Control AircraftF2447 Practice for Production Acceptance Test Proceduresfor Weight-Shift-Control AircraftF2457 Specification for Required Product Information to beProvided withWeight-Shift-Control AircraftF2483 Practice for Maintenance and the Development ofMaintenance Manuals for L

6、ight Sport AircraftF2972 Specification for Light Sport Aircraft ManufacturersQuality Assurance System3. 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

7、 aircraftscenter of gravity with respect to the wing. Flight control of theaircraft depends on the wings 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 cert

8、ification toASTM Weight Shift Control standards. The following datarepresents 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 suppl

9、ied 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 meet therequirements of Specification F2972, it will be necessary forthe manufacturer to

10、 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 inspection,4.2.1.4 Material identification,4.2.1.5 Inspection,4.2.1.6 Non-conforming mate

11、rial handling, and4.2.1.7 QA audits.4.2.2 Continued AirworthinessIn order to meet the re-quirements of Specification F2425, 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

12、therequirements of Practice F2447, it will be necessary for themanufacturer 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 Practice F2483, it will be necessary for themanufac

13、turer to have a current copy of the subcontractorsmaintenance manual on file.4.2.5 Statement of Conformance CoordinationIn order tomeet the requirements for Specification F2317/F2317M, it willbe necessary for the manufacturer to have on file a current copy1This guide is under the jurisdiction of AST

14、M Committee F37 on Light SportAircraft and is the direct responsibility of Subcommittee F37.40 on Weight Shift.Current edition approved Nov. 1, 2016. Published December 2016. Originallyapproved in 2016. Last previous edition approved in 2016 as F3199 16. DOI:10.1520/F3199-16A.2For referenced ASTM st

15、andards, visit the 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,

16、 PA 19428-2959. United StatesThis international standard was developed in accordance with internationally recognized principles on standardization established in the Decision on Principles for theDevelopment of International Standards, Guides and Recommendations issued by the World Trade Organiziati

17、on Technical Barriers to Trade (TBT) Committee.1of the subcontractors statement of conformance coordinationdocument 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

18、 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 the Product Provided:4.3.2.1 Make,4.3.2.2 Model, and4.3.2.3 Serial number.4.3

19、.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 applicablewith appropriate tolerances.4.3.3.3 Batten profile charts.4.3.3.4 Tuning parameters for wing cloth tension a

20、nd 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 the requiredultimate load factor based on the manufacturers design grossweight.4.3.5 Quality Assurance Manu

21、al 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 Wing Top Drawing Number, revision level and datereleased.4.3.8 Continued Airworthiness Manual Date Referen

22、ceThe 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 Document DateReferenceThe reference date provides unit specific assurancethat the manual on file at the manufa

23、cturer 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 Statement of Compliance Coordination DocumentDate ReferenceThe reference date provides unit specificassur

24、ance 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 an example format ofhow the necessary data may be presented.5.2 See Fig. 1.6. Keywords6.1 light sport aircr

25、aft; special airworthiness certificates;weight shift control aircraftF3199 16a2ASTM 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 vali

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29、opies) 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 16a3