ASTM F3082 F3082M-2017 Standard Specification for Weights and Centers of Gravity of Aircraft《飞机重量和重心的标准规格》.pdf
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1、Designation: F3082/F3082M 16F3082/F3082M 17Standard Specification forFlight for General Aviation AeroplanesWeights and Centersof Gravity of Aircraft1This standard is issued under the fixed designation F3082/F3082M; the number immediately following the designation indicates the yearof original adopti
2、on or, in the case of revision, the year of last revision. A number in parentheses indicates the year of last reapproval.A superscript epsilon () indicates an editorial change since the last revision or reapproval.1. Scope1.1 This specification establishes the airworthiness design standards associat
3、ed with aeroplane flight.weight and center ofgravity.1.2 The term “aeroplane” is utilized in this specification as it was originally conceived for normal category fixed wing aircraftwith a maximum certificated weight of 19 000 lb or less and a passenger seating configuration up to 19 as defined in t
4、he Rules.However, these standards may be more broadly applicable and their usage should not be unnecessarily limited.1.3 The applicant for a design approval shall seek the individual guidance of their respective civil aviation authority (CAA)body concerning the use of this specification as part of a
5、 certification plan. For information on which CAA regulatory bodies haveaccepted this specification (in whole or in part) as a means of compliance to their small aircraft airworthiness regulations(hereinafter referred to as “the Rules”), refer to ASTM Committee F44 webpage (www.astm.org/COMMITTEE/F4
6、4.htm), whichincludes CAA website links.1.4 UnitsThe values stated in either SI units or inch-pound units are to be regarded separately as standard. The values statedin each system may not be exact equivalents; therefore, each system shall be used independently of the other. Combining valuesfrom the
7、 two systems may result in non-conformance with the standard.1.5 This standard does not purport to address all of the safety concerns, if any, associated with its use. It is the responsibilityof the user of this standard to establish appropriate safety safety, health, and healthenvironmental practic
8、es and determine theapplicability of regulatory limitations prior to use.1.6 This international standard was developed in accordance with internationally recognized principles on standardizationestablished in the Decision on Principles for the Development of International Standards, Guides and Recom
9、mendations issuedby the World Trade Organization Technical Barriers to Trade (TBT) Committee.2. Referenced Documents2.1 ASTM Standards:2F3060 Terminology for AircraftF3061 Specification for Systems and Equipment in Small AircraftF3063/F3063M Specification for Design and Integration of Fuel/Energy St
10、orage and Delivery System Installations forAeroplanesF3174/F3174M Specification for Establishing Operating Limitations and Information for AeroplanesF3120 Specification for Ice Protection for General Aviation Aircraft3. Terminology3.1 See Terminology F3060 for definitions and abbreviations.4. Genera
11、l4.1 Proof of Compliance: Weight and Center of GravityThe applicant must determine limits for weights and centers of gravitythat provide for the safe operation of the airplane.1 This specification is under the jurisdiction of ASTM Committee F44 on General Aviation Aircraft and is the direct responsi
12、bility of Subcommittee F44.20 on Flight.Current edition approved Feb. 1, 2016Oct. 15, 2017. Published March 2016November 2017. Originally approved in 2016. Last previous edition approved in 2016 asF3082/F3082M 16. DOI: 10.1520/F3082_F3082M-16.10.1520/F3082_F3082M-17.2 For referencedASTM standards, v
13、isit theASTM website, www.astm.org, or contactASTM Customer Service at serviceastm.org. For Annual Book of ASTM Standardsvolume information, refer to the standards Document Summary page on the ASTM website.This document is not an ASTM standard and is intended only to provide the user of an ASTM stan
14、dard an indication of what changes have been made to the previous version. Becauseit may not be technically possible to adequately depict all changes accurately, ASTM recommends that users consult prior editions as appropriate. In all cases only the current versionof the standard as published by AST
15、M is to be considered the official document.Copyright ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959. United States14.1.1 Each criterion of this specification of the Flight Standards shall be met at each appropriate combination criticalcombinations of weight
16、 and center of gravity within the range of loading conditions for which certification is requested. This shallbe shown by:4.1.1.1 Tests upon an aeroplane of the type for which certification is requested or by calculations based on, and equal inaccuracy to, the results of testing.testing, and4.1.1.2
17、Systematic investigation of each probable combination of weight and center of gravity, if compliance cannot bereasonably inferred from combinations investigated.4.1.2 The general tolerances in Table 1 are allowed during flight testing. However, greater tolerances may be allowed inparticular tests, i
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