ASTM F2426-2005a 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: F 2426 05aStandard 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 year of last revisio

2、n. 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 guide covers the manufacture of powered para-chute aircraft and their qualification for certification.1.2 This guide applies

3、 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 of the user of t

4、his 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 Specification for

5、 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 and Performance R

6、equire-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 a fuselage with s

7、eats, 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 pendulum effect li

8、mits 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 datarepresents a guide t

9、o 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 be main-tained at

10、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 file. This manua

11、l 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 order to meet the

12、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 manufacturer to

13、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 maintenance manual on

14、 file.1This guide is under the jurisdiction of ASTM Committee F37 on Light SportAircraft and is the direct responsibility of Subcommittee F37.30 on PoweredParachute Specifications.Current edition approved Nov. 1, 2005. Published November 2005. Originallyapproved in 2004. Last previous edition approv

15、ed in 2005 as F 2426 05.2For referenced ASTM standards, 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.1Copyright ASTM International, 100 Ba

16、rr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959, United States.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 ofthe subcontractors statement of conformance coo

17、rdinationdocument 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

18、.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.4.3.3 Interface Physical Limits:4.3.3.1 Riser attachment spacing and length limits are to bepresented

19、 as 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 i

20、n PoundsThis 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 c

21、urrent 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.

22、4.3.8 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

23、 that 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 ad

24、ministra-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 05a2FIG. 1 Supporting Da

25、ta 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 lengt

26、h” 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 ultimate lo

27、ad _ 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. The l

28、atest 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 Acceptan

29、ce 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 win

30、g, 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 use

31、r 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 this st

32、andard 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 years a

33、ndif 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 committee,

34、 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 05a3