1、Designation: F3264 18bStandard 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 t
3、he requirements (“the Rules”) for Level 1, 2, 3,4 Normal Category Aeroplanes.1.1.2 Only standards that are considered mature enough forgeneral application to certification projects and have beenfound acceptable by committee consensus to propose to theCAAs for acceptance as a Means of Compliance to t
4、heir Rulesare included.1.1.3 In the event that a particular CAAs requirements arenot harmonized with the other CAAs requirements, the stan-dards will be written to include the non-harmonized require-ments as well as the harmonized requirements with theapplicability defined in the standard.1.2 Civil
5、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 and applicability as a MoC to theCAAs airworthiness rules remains the decision of the respec-tive CAAs. CAAs may accept this specification
6、, with orwithout limitations as defined in their specification acceptancedocument. For information on which CAAs have acceptedthese standards (in whole or in part) 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
7、Applicant Responsibility:1.3.1 The applicant must seek individual guidance fromtheir respective CAA concerning the use of this specificationand any referenced Specifications, Practices, Test Methods, orGuides to show compliance to the CAA rules. Alternatively, anapplicant may propose a MoC other tha
8、n those included in thisspecification but it is their responsibility to obtain acceptanceof their proposed MoC from their CAA.1.4 This international standard was developed in accor-dance with internationally recognized principles on standard-ization established in the Decision on Principles for theD
9、evelopment of International Standards, Guides and Recom-mendations issued by the World Trade Organization TechnicalBarriers to Trade (TBT) Committee.2. Referenced Documents2.1 ASTM Standards:2NOTE 1Referenced ASTM standards are listed in Sections 510ofthis specification.F2490 Guide for Aircraft Elec
10、trical Load and Power SourceCapacity AnalysisF3060 Terminology for AircraftF3061/F3061M Specification for Systems and Equipment inSmall AircraftF3062/F3062M Specification for Aircraft Powerplant Instal-lationF3063/F3063M Specification for Aircraft Fuel and EnergyStorage and DeliveryF3064/F3064M Spec
11、ification for Aircraft PowerplantControl, Operation, and IndicationF3065/F3065M Specification for Aircraft Propeller SystemInstallationF3066/F3066M Specification for Aircraft Powerplant Instal-lation Hazard MitigationF3082/F3082M Specification for Weights and Centers ofGravity of AircraftF3083/F3083
12、M Specification for Emergency Conditions,Occupant Safety and AccommodationsF3093/F3093M Specification for Aeroelasticity Require-mentsF3114 Specification for StructuresF3115/F3115M Specification for Structural Durability forSmall AirplanesF3116/F3116M Specification for Design Loads and Condi-tionsF3
13、117 Specification for Crew Interface in AircraftF3120/F3120M Specification for Ice Protection for GeneralAviation Aircraft1This specification is under the jurisdiction ofASTM Committee F44 on GeneralAviation Aircraft and is the direct responsibility of Subcommittee F44.10 onGeneral.Current edition a
14、pproved Nov. 1, 2018. Published December 2018. Originallyapproved in 2017. Last previous edition approved in 2018 as F326418a. DOI:10.1520/F326418B.2For referenced ASTM standards, visit the ASTM website, www.astm.org, orcontact ASTM Customer Service at serviceastm.org. For Annual Book of ASTMStandar
15、ds 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 internationally recognized principles o
16、n 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.1F3173/F3173M Specification for Aircraft Handling Charac-teristicsF3174/F3174M Spec
17、ification for Establishing OperatingLimitations and Information for AeroplanesF3179/F3179M Specification for Performance of AircraftF3180/F3180M Specification for Low-Speed Flight Charac-teristics of AircraftF3227/F3227M Specification for Environmental Systems inSmall AircraftF3228 Specification for
18、 Flight Data and Voice Recording inSmall AircraftF3229/F3229M Practice for Static Pressure System Tests inSmall AircraftF3230 Practice for Safety Assessment of Systems andEquipment in Small AircraftF3231/F3231M Specification for Electrical Systems inSmall AircraftF3232/F3232M Specification for Fligh
19、t Controls in SmallAircraftF3233/F3233M Specification for Instrumentation in SmallAircraftF3234/F3234M Specification for Exterior Lighting in SmallAircraftF3235 Specification for Aircraft Storage BatteriesF3236 Specification for High Intensity Radiated Field(HIRF) Protection in Small AircraftF3309/F
20、3309M Practice for Simplified SafetyAssessment ofSystems and Equipment in Small AircraftF3331 Practice for Aircraft Water Loads2.2 Federal Aviation Administration (FAA) Regulations:14 CFR 23, Amendment 64 Airworthiness Standards: Nor-mal Category Airplanes32.3 European Aviation Safety Agency (EASA)
21、Regulations:CS 23, Amendment 5 Certification Specifications for Nor-mal Category Aeroplanes4NOTE 2The above regulations and requirements are not directlyreferenced in the specification but are the “relevant applicable regulations”referred to in the Rules definition in 3.2.2.3. Terminology3.1 Unique
22、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 (MoC)a method or processwhich is used to show that a rule has been compli
23、ed 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 Aeroplanes issued by the CAAs.3.3 Abbreviations:3.3.1 CAACivil Aviation
24、 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 anticipated for these requirements.4.2 Certification of Normal Category Aeroplane
25、s: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 17 Standard Specification forWeights and Center of Gravity of Aircraft5.1.2 F3114 1
26、5 Standard Specification for Structures5.2 Performance Data:5.2.1 F3179/F3179M 18 Standard Specification for Per-formance of Aircraft5.3 Stall Speed:5.3.1 F3179/F3179M 18 Standard Specification for Per-formance of Aircraft5.4 Takeoff Performance:5.4.1 F3179/F3179M 18 Standard Specification for Per-f
27、ormance of Aircraft5.5 Climb Requirements:5.5.1 F3179/F3179M 18 Standard Specification for Per-formance of Aircraft5.6 Climb Information:5.6.1 F3179/F3179M 18 Standard Specification for Per-formance of Aircraft5.7 Landing:5.7.1 F3179/F3179M 18 Standard Specification for Per-formance of Aircraft5.8 C
28、ontrollability:5.8.1 F3173/F3173M 17 Standard Specification for Air-craft Handling Characteristics5.9 Trim:5.9.1 F3173/F3173M 17 Standard Specification for Air-craft Handling Characteristics5.10 Stability:5.10.1 F3173/F3173M 17 Standard Specification for Air-craft Handling Characteristics5.11 Stall
29、Characteristics, Stall Warning, and Spins:5.11.1 F3180/F3180M 18 Standard Specification for Low-Speed Flight Characteristics of Aircraft5.12 Ground and Water Handling Characteristics:5.12.1 F3173/F3173M 17 Standard Specification for Air-craft Handling Characteristics3Available from U.S. Government P
30、ublishing Office (GPO), 732 N. Capitol St.,NW, Washington, DC 20401, http:/www.gpo.gov.4Available from European Aviation Safety Agency (EASA), Postfach 10 12 53,D-50452 Cologne, Germany, https:/www.easa.europa.eu/document-library/certification-specifications/cs-23-amendment-5.F3264 18b25.13 Vibratio
31、n, Buffeting, and High-Speed Characteristics:5.13.1 F3173/F3173M 17 Standard Specification for Air-craft Handling Characteristics5.14 Performance and Flight Characteristics Requirementsfor Flight in Icing Conditions:5.14.1 F3120/F3120M 15 Standard Specification for IceProtection for General Aviation
32、 Aircraft5.15 Operating Limitations:5.15.1 F3174/F3174M 18 Standard Specification for Es-tablishing Operating Limitations and Information for Aero-planes6. Structures6.1 Structural Design Envelope:6.1.1 F3116/F3116M 18 Standard Specification for De-sign Loads and Conditions6.2 Interaction of Systems
33、 and Structure6.3 Structural Design Loads:6.3.1 F3116/F3116M 18 Standard Specification for De-sign Loads and Conditions6.4 Flight Load Conditions:6.4.1 F3116/F3116M 18 Standard Specification for De-sign Loads and Conditions6.5 Ground and Water Load Conditions:6.5.1 F3116/F3116M 18 Standard Specifica
34、tion for De-sign Loads and Conditions6.5.1.1 F3331 18 Standard Practice for Aircraft WaterLoads6.6 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 Aircraft
35、6.6.2 F3116/F3116M 18 Standard Specification 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 15 Standard Specification for Structures6.9 Structural Durability:6.9.1 F3061/F3061M 17 Standard Specifica
36、tion for Sys-tems and Equipment in Small Aircraft6.9.2 F3115/F3115M 15 Standard Specification for Struc-tural Durability for Small Aeroplanes6.10 Aeroelasticity:6.10.1 F3061/F3061M 17 Standard Specification for Sys-tems and Equipment in Small Aircraft6.10.2 F3093/F3093M 15 Standard Specification for
37、Aeroelasticity Requirements6.11 Design and Construction Principles:6.11.1 F3061/F3061M 17 Standard Specification for Sys-tems and Equipment 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 P
38、rotection of Structure:6.12.1 F3061/F3061M 17 Standard Specification for Sys-tems and Equipment in Small Aircraft6.12.1.1 F3232/F3232M 17 Standard Specification forFlight Controls in Small Aircraft6.12.2 F3114 15 Standard Specification for Structures6.12.3 F3066/F3066M 18 Standard Specification for
39、Air-craft Powerplant Installation Hazard Mitigation6.13 Materials and Processes:6.13.1 F3114 15 Standard Specification for Structures6.14 Special 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 Str
40、uctures6.15 Emergency Conditions:6.15.1 F3061/F3061M 17 Standard Specification for Sys-tems and Equipment in Small Aircraft6.15.1.1 F3232/F3232M 17 Standard Specification forFlight Controls in Small Aircraft6.15.2 F3083/F3083M 16 Standard Specification forEmergency Conditions, Occupant Safety andAcc
41、ommodations7. Design and Construction7.1 Flight Control Systems:7.1.1 F3061/F3061M 17 Standard Specification for Sys-tems and Equipment in Small Aircraft7.1.1.1 F3232/F3232M 17 Standard Specification forFlight Controls in Small Aircraft7.1.2 F3066/F3066M 18 Standard Specification for Air-craft Power
42、plant Installation Hazard Mitigation7.2 Landing Gear Systems:7.2.1 F3061/F3061M 17 Standard Specification for Sys-tems and Equipment in Small Aircraft7.3 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
43、 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 Specification for Emer-gency Conditions, Occupant Safety and Accommodations7.5 Occupant Physical Environment:7.5.1 F3061/F3061M 17 Standard Specification for S
44、ys-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 16 Standard Specification for Emer-gency Conditions, Occupant Safety and Accommodations7.5.3 F3114 15 Standard Specification for Structures7.5.4 F3117
45、18b Standard Specification for Crew Inter-face in Aircraft7.6 Fire Protection:7.6.1 F3061/F3061M 17 Standard Specification for Sys-tems and Equipment in Small AircraftF3264 18b37.6.1.1 F3231/F3231M 17 Standard Specification forElectrical Systems in Small Aircraft7.6.1.2 F3234/F3234M 17 Standard Spec
46、ification for Ex-terior Lighting in Small Aircraft7.6.2 F3066/F3066M 18 Standard Specification for Air-craft Powerplant Installation Hazard Mitigation7.6.3 F3083/F3083M 16 Standard Specification for Emer-gency Conditions, Occupant Safety and Accommodations7.7 Fire Protection in Designated Fire Zones
47、 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 forElectrical Systems in Small Aircraft7.7.2 F3066/F3066M 18 Standard Specification for Air-craft Powerplant Installation Hazard Mitigation7.7.3
48、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/F3062M 18 Standard Specification for Air-craft P
49、owerplant Installation8.1.2 F3063/F3063M 18a Standard Specification for Air-craft Fuel and Energy Storage and Delivery8.1.3 F3064/F3064M 18a Standard Specification for Air-craft Powerplant Control, Operation, and Indication8.1.4 F3065/F3065M 18 Standard Specification for Air-craft Propeller System Installation8.1.5 F3066/F3066M 18 Standard Specification for Air-craft Powerplant Installation Hazard Mitigation8.2 Power or Thrust Co
