ASTM F3264-2017 Standard Specification for Normal Category Aeroplanes Certification《普通类别飞机证书的标准规格》.pdf

1、Designation: F3264 17Standard Specification forNormal Category Aeroplanes Certification1This standard is issued under the fixed designation F3264; the number immediately following the designation indicates the year oforiginal adoption or, in the case of revision, the year of last revision. A number

2、in parentheses indicates the year of last reapproval. Asuperscript epsilon () indicates an editorial change since the last revision or reapproval.1. Scope1.1 Applicability:1.1.1 This specification identifies the industry standardswhich have been determined by consensus to demonstratecompliance to th

3、e requirements (“the Rules”) for Level 1, 2, 3,4 Normal Category Aeroplanes.1.1.2 Unless specifically defined otherwise, the herein ref-erenced specifications are only applicable to the aeroplanesdefined in 1.1.1.1.1.3 Only standards that are considered mature enough forgeneral application to certif

4、ication projects and have beenfound acceptable by committee consensus to propose to theCAAs for acceptance as a Means of Compliance to their Rulesare included.1.1.4 In the event that a particular CAAs requirements arenot harmonized with the other CAAs requirements, the stan-dards will be written to

5、include the non-harmonized require-ments as well as the harmonized requirements with theapplicability defined in the standard.1.2 Civil Aviation Authorities:1.2.1 CAAs may accept a specific revision of this specifi-cation as an acceptable Means of Compliance (MoC) to theirrequirements. Acceptance an

6、d applicability as a MoC to theCAAs airworthiness rules remains the decision of the respec-tive CAAs. CAAs may accept this specification, with orwithout limitations as defined in their specification acceptancedocument. For information on which CAAs have acceptedthese standards (in whole or in part)

7、as an acceptable MoC totheir Rules, refer to the ASTM F44 webpage (www.astm.org/COMMITTEE/F44.htm) which includes CAA website links.1.3 Applicant Responsibility:1.3.1 The applicant must seek individual guidance fromtheir respective CAA concerning the use of this specificationand any referenced Speci

8、fications, Practices, Test Methods, orGuides to show compliance to the CAA rules. Alternatively, anapplicant may propose a MoC other than those included in thisspecification but it is their responsibility to obtain approval oftheir proposed MoC from their CAA.1.4 This international standard was deve

9、loped in accor-dance with internationally recognized principles on standard-ization established in the Decision on Principles for theDevelopment of International Standards, Guides and Recom-mendations issued by the World Trade Organization TechnicalBarriers to Trade (TBT) Committee.2. Referenced Doc

10、uments2.1 ASTM Standards:2NOTE 1Referenced ASTM standards are listed in Sections 510ofthis specification.F2490 Guide for Aircraft Electrical Load and Power SourceCapacity AnalysisF3060 Terminology for AircraftF3061/F3061M Specification for Systems and Equipment inSmall AircraftF3062/F3062M Specifica

11、tion for Installation of PowerplantSystemsF3063/F3063M Specification for Design and Integration ofFuel/Energy Storage and Delivery System Installations forAeroplanesF3064/F3064M Specification for Control, Operational Char-acteristics and Installation of Instruments and Sensors ofPropulsion SystemsF3

12、065/F3065M Specification for Installation and Integrationof Propeller SystemsF3066/F3066M Specification for Powerplant Systems Spe-cific Hazard MitigationF3082/F3082M Specification for Flight for General AviationAeroplanesF3083/F3083M Specification for Emergency Conditions,Occupant Safety and Accomm

13、odationsF3093/F3093M Specification for Aeroelasticity Require-mentsF3114 Specification for StructuresF3115/F3115M Specification for Structural Durability forSmall AirplanesF3116/F3116M Specification for Design Loads and Condi-tions1This specification is under the jurisdiction ofASTM Committee F44 on

14、 GeneralAviation Aircraft and is the direct responsibility of Subcommittee F44.10 onGeneral.Current edition approved Sept. 1, 2017. Published September 2017. DOI:10.1520/F3264-17.2For referenced ASTM standards, visit the ASTM website, www.astm.org, orcontact ASTM Customer Service at serviceastm.org.

15、 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. United StatesThis international standard was developed in accordance with internat

16、ionally recognized principles on standardization established in the Decision on Principles for theDevelopment of International Standards, Guides and Recommendations issued by the World Trade Organization Technical Barriers to Trade (TBT) Committee.1F3117 Specification for Crew Interface in AircraftF

17、3120/F3120M Specification for Ice Protection for GeneralAviation AircraftF3173/F3173M Specification for Handling Characteristicsof AeroplanesF3174/F3174M Specification for Establishing OperatingLimitations and Information for AeroplanesF3179/F3179M Specification for Performance ofAeroplanesF3180/F31

18、80M Specification for Low-Speed Flight Charac-teristics of AeroplanesF3227/F3227M Specification for Environmental Systems inSmall AircraftF3228 Specification for Flight Data and Voice Recording inSmall AircraftF3229/F3229M Practice for Static Pressure System Tests inSmall AircraftF3230 Practice for

19、Safety Assessment of Systems andEquipment in Small AircraftF3231/F3231M Specification for Electrical Systems inSmall AircraftF3232/F3232M Specification for Flight Controls in SmallAircraftF3233/F3233M Specification for Instrumentation in SmallAircraftF3234/F3234M Specification for Exterior Lighting

20、in SmallAircraftF3235 Specification for Electrical Storage Batteries in SmallAircraftF3236 Specification for High Intensity Radiated Field(HIRF) Protection in Small Aircraft2.2 Federal Aviation Administration (FAA) Regulations:14 CFR 23, Amendment 64 Airworthiness Standards:Normal, Utility, Acrobati

21、c, and Commuter Category Air-planes32.3 European Aviation Safety Agency (EASA) Regulations:CS 23, Amendment 5 Normal, Utility, Aerobatic, and Com-muter Aeroplanes4NOTE 2The above regulations and requirements are not directlyreferenced in the specification but are the “relevant applicable regulations

22、”referred to in the Rules definition in 3.2.2.3. Terminology3.1 Unique and Common TerminologyTerminology usedin multiple standards is defined in F3060,Aircraft TerminologyStandard. Terminology that is unique to this specification isdefined in this section.3.2 Definitions:3.2.1 Means of Compliance (M

23、oC)a method or processwhich is used to show that a rule has been complied withthrough either design, analysis, test, or a combination ofdesign, analysis and test.3.2.2 Rulesuniversal reference to the relevant applicableregulations or standards governing airworthiness requirementsfor Normal Category

24、Aeroplanes issued by the CAAs.3.3 Abbreviations:3.3.1 CAACivil Aviation Authority3.3.2 MoCMeans of Compliance4. General4.1 Regulatory Applicability and Definitions:4.1.1 See the applicable CAA Rules for specific CAAsApplicability and Definitions. There are currently no standardswritten or anticipate

25、d for these requirements.4.2 Certification of Normal Category Aeroplanes:4.2.1 This specification will identify in Sections 510allstandards that are applicable for certifying a Level 1, 2, 3, or 4Normal Category Aeroplane.5. Flight5.1 Weight/Mass and Centre of Gravity:5.1.1 F3082/F3082M 16 Standard

26、Specification for Flightfor General Aviation Aeroplanes5.2 Performance Data:5.2.1 F3179/F3179M 16 Standard Specification for Per-formance of Aeroplanes5.3 Stall Speed:5.3.1 F3179/F3179M 16 Standard Specification for Per-formance of Aeroplanes5.4 Takeoff Performance:5.4.1 F3179/F3179M 16 Standard Spe

27、cification for Per-formance of Aeroplanes5.5 Climb Requirements:5.5.1 F3179/F3179M 16 Standard Specification for Per-formance of Aeroplanes5.6 Climb Information:5.6.1 F3179/F3179M 16 Standard Specification for Per-formance of Aeroplanes5.7 Landing:5.7.1 F3179/F3179M 16 Standard Specification for Per

28、-formance of Aeroplanes5.8 Controllability:5.8.1 F3173/F3173M 15 Standard Specification for Han-dling Characteristics of Aeroplanes5.9 Trim:5.9.1 F3173/F3173M 15 Standard Specification for Han-dling Characteristics of Aeroplanes5.10 Stability:5.10.1 F3173/F3173M 15 Standard Specification for Han-dli

29、ng Characteristics of Aeroplanes5.11 Stall Characteristics, Stall Warning, and Spins5.11.1 F3180/F3180M 16 Standard Specification for Low-Speed Flight Characteristics of Aeroplanes5.12 Ground and Water Handling Characteristics:5.12.1 F3173/F3173M 15 Standard Specification for Han-dling Characteristi

30、cs of Aeroplanes3Available from U.S. Government Printing Office, Superintendent ofDocuments, 732 N. Capitol St., NW, Washington, DC 20401-0001, http:/www.access.gpo.gov.4Available from European Aviation Safety Agency (EASA), Postfach 10 12 53,D-50452 Cologne, Germany, www.easa.europa.eu.F3264 1725.1

31、3 Vibration, Buffeting, and High-Speed Characteristics:5.13.1 F3173/F3173M 15 Standard Specification for Han-dling Characteristics of Aeroplanes5.14 Performance and Flight Characteristics Requirementsfor Flight in Icing Conditions:5.14.1 F3120/F3120M 15 Standard Specification for IceProtection for G

32、eneral Aviation Aircraft5.15 Operating Limitations:5.15.1 F3174/F3174M 15 Standard Specification for Es-tablishing Operating Limitations and Information for Aero-planes6. Structures6.1 Structural Design Envelope:6.1.1 F3116/F3116M 15 Standard Specification for De-sign Loads and Conditions6.2 Interac

33、tion of Systems and Structure6.3 Structural Design Loads:6.3.1 F3116/F3116M 15 Standard Specification for De-sign Loads and Conditions6.4 Flight Load Conditions:6.4.1 F3116/F3116M 15 Standard Specification for De-sign Loads and Conditions6.5 Ground and Water Load Conditions:6.5.1 F3116/F3116M 15 Sta

34、ndard Specification for De-sign Loads and Conditions6.6 Component Loading Conditions:6.6.1 F3061/F3061M 17 Standard Specification for Sys-tems and Equipment in Small Aircraft6.6.1.1 F3232/F3232M 17 Standard Specification forFlight Controls in Small Aircraft6.6.2 F3116/F3116M 15 Standard Specificatio

35、n for De-sign Loads and Conditions6.7 Limit and Ultimate Loads:6.7.1 F3114 15 Standard Specification for Structures6.8 Structural Strength:6.8.1 F3114 Standard Specification Structures6.9 Structural Durability:6.9.1 F3115/F3115M 15 Standard Specification for Struc-tural Durability for Small Aeroplan

36、es6.10 Aeroelasticity:6.10.1 F3061/F3061M 17 Standard Specification for Sys-tems and Equipment in Small Aircraft6.10.2 F3093/F3093M 15 Standard Specification forAeroelasticity Requirements6.11 Design and Construction Principles:6.11.1 F3061/F3061M 17 Standard Specification for Sys-tems and Equipment

37、 in Small Aircraft6.11.1.1 F3232/F3232M 17 Standard Specification forFlight Controls in Small Aircraft6.11.2 F3114 15 Standard Specification for Structures6.12 Protection of Structure:6.12.1 F3061/F3061M 17 Standard Specification for Sys-tems and Equipment in Small Aircraft6.12.1.1 F3232/F3232M 17 S

38、tandard Specification forFlight Controls in Small Aircraft6.12.2 F3114 15 Standard Specification for Structures6.12.3 F3066/F3066M 15 Standard Specification for Pow-erplant Systems Specific Hazard Mitigation6.13 Materials and Processes:6.13.1 F3114 15 Standard Specification for Structures6.14 Specia

39、l Factors of Safety:6.14.1 F3061/F3061M 17 Standard Specification for Sys-tems and Equipment in Small Aircraft6.14.2 F3114 15 Standard Specification for Structures6.15 Emergency Conditions:6.15.1 F3061/F3061M 17 Standard Specification for Sys-tems and Equipment in Small Aircraft6.15.1.1 F3232/F3232M

40、 17 Standard Specification forFlight Controls in Small Aircraft6.15.2 F3083/F3083M 16 Standard Specification forEmergency Conditions, Occupant Safety andAccommodations7. Design and Construction7.1 Flight Control Systems:7.1.1 F3061/F3061M 17 Standard Specification for Sys-tems and Equipment in Small

41、 Aircraft7.1.1.1 F3232/F3232M 17 Standard Specification forFlight Controls in Small Aircraft7.1.2 F3066/F3066M 15 Standard Specification for Pow-erplant Systems Specific Hazard Mitigation7.2 Landing Gear Systems:7.2.1 F3061/F3061M 17 Standard Specification for Sys-tems and Equipment in Small Aircraf

42、t7.3 Buoyancy for Seaplanes and Amphibians:7.3.1 F3061/F3061M 17 Standard Specification for Sys-tems and Equipment in Small Aircraft7.4 Means of Egress and Emergency Exits:7.4.1 F3061/F3061M 17 Standard Specification for Sys-tems and Equipment in Small Aircraft7.4.2 F3083/F3083M 16 Standard Specific

43、ation for Emer-gency Conditions, Occupant Safety and Accommodations7.5 Occupant Physical Environment:7.5.1 F3061/F3061M 17 Standard Specification for Sys-tems and Equipment in Small Aircraft7.5.1.1 F3227/F3227M 17 Standard Specification for En-vironmental Systems in Small Aircraft7.5.2 F3083/F3083M

44、16 Standard Specification for Emer-gency Conditions, Occupant Safety and Accommodations7.5.3 F3114 15 Standard Specification for Structures7.5.4 F3117 15 Standard Specification for Crew Interfacein Aircraft7.6 Fire Protection:7.6.1 F3061/F3061M 17 Standard Specification for Sys-tems and Equipment in

45、 Small Aircraft7.6.1.1 F3231/F3231M 17 Standard Specification forElectrical Systems in Small Aircraft7.6.1.2 F3234/F3234M 17 Standard Specification for Ex-terior Lighting in Small AircraftF3264 1737.6.2 F3065/F3065M 15 Standard Specification for Instal-lation and Integration of Propeller Systems7.6.

46、3 F3083/F3083M 16 Standard Specification for Emer-gency Conditions, Occupant Safety and Accommodations7.7 Fire Protection in Designated Fire Zones and AdjacentAreas:7.7.1 F3061/F3061M 17 Standard Specification for Sys-tems and Equipment in Small Aircraft7.7.1.1 F3231/F3231M 17 Standard Specification

47、 forElectrical Systems in Small Aircraft7.7.2 F3114 15 Standard Specification for Structures7.8 Lightning Protection:7.8.1 F3061/F3061M 17 Standard Specification for Sys-tems and Equipment in Small Aircraft7.9 Design and Construction Information8. Powerplant8.1 Powerplant Installation:8.1.1 F3062/F3

48、062M 16 Standard Specification for Instal-lation of Powerplant Systems8.1.2 F3063/F3063M 16a Standard Specification for De-sign and Integration of Fuel/Energy Storage and DeliverySystem Installations for Aeroplanes8.1.3 F3064/F3064M 15 Standard Specification forControl, Operational Characteristics a

49、nd Installation of Instru-ments and Sensors of Propulsion Systems8.1.4 F3065/F3065M 15 Standard Specification for Instal-lation and Integration of Propeller Systems8.1.5 F3066/F3066M 15 Standard Specification for Pow-erplant Systems Specific Hazard Mitigation8.2 Power or Thrust Control Systems:8.2.1 F3062/F3062M 16 Standard Specification for Instal-lation of Powerplant Systems8.2.2 F3064/F3064M 15 Standard Specification forControl, Ope