1、Designation: F3264 18F3264 18aStandard 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.
2、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 Applicability:1.1.1 This specification identifies the industry standards which have been determined by consensus to demonstrate compl
3、ianceto the requirements (“the Rules”) for Level 1, 2, 3, 4 Normal Category Aeroplanes.1.1.2 Only standards that are considered mature enough for general application to certification projects and have been foundacceptable by committee consensus to propose to the CAAs for acceptance as a Means of Com
4、pliance to their Rules are included.1.1.3 In the event that a particular CAAs requirements are not harmonized with the other CAAs requirements, the standardswill be written to include the non-harmonized requirements as well as the harmonized requirements with the applicability definedin the standard
5、.1.2 Civil Aviation Authorities:1.2.1 CAAs may accept a specific revision of this specification as an acceptable Means of Compliance (MoC) to theirrequirements. Acceptance and applicability as a MoC to the CAAs airworthiness rules remains the decision of the respectiveCAAs. CAAs may accept this spec
6、ification, with or without limitations as defined in their specification acceptance document. Forinformation on which CAAs have accepted these standards (in whole or in part) as an acceptable MoC to their Rules, refer to theASTM F44 webpage (www.astm.org/COMMITTEE/F44.htm) which includes CAA website
7、 links.1.3 Applicant Responsibility:1.3.1 The applicant must seek individual guidance from their respective CAA concerning the use of this specification and anyreferenced Specifications, Practices, Test Methods, or Guides to show compliance to the CAA rules. Alternatively, an applicantmay propose a
8、MoC other than those included in this specification but it is their responsibility to obtain acceptance of theirproposed MoC from their CAA.1.4 This international standard was developed in accordance with internationally recognized principles on standardizationestablished in the Decision on Principl
9、es for the Development of International Standards, Guides and Recommendations issuedby the World Trade Organization Technical Barriers to Trade (TBT) Committee.2. Referenced Documents2.1 ASTM Standards:2NOTE 1Referenced ASTM standards are listed in Sections 5 10 of this specification.F2490 Guide for
10、 Aircraft Electrical Load and Power Source Capacity AnalysisF3060 Terminology for AircraftF3061/F3061M Specification for Systems and Equipment in Small AircraftF3062/F3062M Specification for Aircraft Powerplant InstallationF3063/F3063M Specification for Aircraft Fuel and Energy Storage and DeliveryF
11、3064/F3064M Specification for Aircraft Powerplant Control, Operation, and IndicationF3065/F3065M Specification for Aircraft Propeller System InstallationF3066/F3066M Specification for Aircraft Powerplant Installation Hazard MitigationF3082/F3082M Specification for Weights and Centers of Gravity of A
12、ircraftF3083/F3083M Specification for Emergency Conditions, Occupant Safety and AccommodationsF3093/F3093M Specification for Aeroelasticity Requirements1 This specification is under the jurisdiction of ASTM Committee F44 on General Aviation Aircraft and is the direct responsibility of Subcommittee F
13、44.10 on General.Current edition approved March 1, 2018Oct. 1, 2018. Published March 2018November 2018. Originally approved in 2017. Last previous edition approved in 20172018as F3264 17.F3264 18. DOI: 10.1520/F3264-18.10.1520/F3264-18A.2 For referencedASTM standards, visit theASTM website, www.astm
14、.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 standard an indication of what cha
15、nges 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 ASTM is to be considered the offi
16、cial document.Copyright ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959. United States1F3114 Specification for StructuresF3115/F3115M Specification for Structural Durability for Small AirplanesF3116/F3116M Specification for Design Loads and ConditionsF3117 Sp
17、ecification for Crew Interface in AircraftF3120/F3120M Specification for Ice Protection for General Aviation AircraftF3173/F3173M Specification for Aircraft Handling CharacteristicsF3174/F3174M Specification for Establishing Operating Limitations and Information for AeroplanesF3179/F3179M Specificat
18、ion for Performance of AircraftF3180/F3180M Specification for Low-Speed Flight Characteristics of AircraftF3227/F3227M Specification for Environmental Systems in Small AircraftF3228 Specification for Flight Data and Voice Recording in Small AircraftF3229/F3229M Practice for Static Pressure System Te
19、sts in Small AircraftF3230 Practice for Safety Assessment of Systems and Equipment in Small AircraftF3231/F3231M Specification for Electrical Systems in Small AircraftF3232/F3232M Specification for Flight Controls in Small AircraftF3233/F3233M Specification for Instrumentation in Small AircraftF3234
20、/F3234M Specification for Exterior Lighting in Small AircraftF3235 Specification for Aircraft Storage BatteriesF3236 Specification for High Intensity Radiated Field (HIRF) Protection in Small AircraftF3309/F3309M Practice for Simplified Safety Assessment of Systems and Equipment in Small Aircraft2.2
21、 Federal Aviation Administration (FAA) Regulations:14 CFR 23, Amendment 64 Airworthiness Standards: Normal Category Airplanes32.3 European Aviation Safety Agency (EASA) Regulations:CS 23, Amendment 5 Certification Specifications for Normal Category Aeroplanes4NOTE 2The above regulations and requirem
22、ents are not directly referenced in the specification but are the “relevant applicable regulations” referredto in the Rules definition in 3.2.2.3. Terminology3.1 Unique and Common TerminologyTerminology used in multiple standards is defined in F3060, Aircraft TerminologyStandard. Terminology that is
23、 unique to this specification is defined in this section.3.2 Definitions:3.2.1 Means of Compliance (MoC)a method or process which is used to show that a rule has been complied with througheither design, analysis, test, or a combination of design, analysis and test.3.2.2 Rulesuniversal reference to t
24、he relevant applicable regulations or standards governing airworthiness requirements forNormal Category 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 Rul
25、es for specific CAAs Applicability and Definitions. There are currently no standards writtenor anticipated for these requirements.4.2 Certification of Normal Category Aeroplanes:4.2.1 This specification will identify in Sections 5 10 all standards that are applicable for certifying a Level 1, 2, 3,
26、or 4 NormalCategory Aeroplane.5. Flight5.1 Weight/Mass and Centre of Gravity:5.1.1 F3082/F3082M 17 Standard Specification for Weights and Center of Gravity of Aircraft5.1.2 F3114 15 Standard Specification for Structures5.2 Performance Data:3 Available from U.S. Government Printing Office, Superinten
27、dent of Documents, 732 N. Capitol St., NW, Washington, DC 20401-0001, http:/www.access.gpo.gov.4 Available from EuropeanAviation SafetyAgency (EASA), Postfach 10 12 53, D-50452 Cologne, Germany, www.easa.europa.eu. https:/www.easa.europa.eu/document-library/certification-specifications/cs-23amendmen
28、t-5https:/www.easa.europa.eu/document-library/certification-specifications/cs-23amendment-5.F3264 18a25.2.1 F3179/F3179M 16 18 Standard Specification for Performance of AeroplanesAircraft5.3 Stall Speed:5.3.1 F3179/F3179M 16 18 Standard Specification for Performance of AeroplanesAircraft5.4 Takeoff
29、Performance:5.4.1 F3179/F3179M 16 18 Standard Specification for Performance of AeroplanesAircraft5.5 Climb Requirements:5.5.1 F3179/F3179M 16 18 Standard Specification for Performance of AeroplanesAircraft5.6 Climb Information:5.6.1 F3179/F3179M 16 18 Standard Specification for Performance of Aeropl
30、anesAircraft5.7 Landing:5.7.1 F3179/F3179M 16 18 Standard Specification for Performance of AeroplanesAircraft5.8 Controllability:5.8.1 F3173/F3173M 15 17 Standard Specification for Aircraft Handling Characteristics of Aeroplanes5.9 Trim:5.9.1 F3173/F3173M 15 17 Standard Specification for Aircraft Ha
31、ndling Characteristics of Aeroplanes5.10 Stability:5.10.1 F3173/F3173M 15 17 Standard Specification for Aircraft Handling Characteristics of Aeroplanes5.11 Stall Characteristics, Stall Warning, and Spins:5.11.1 F3180/F3180M 16 18 Standard Specification for Low-Speed Flight Characteristics of Aeropla
32、nesAircraft5.12 Ground and Water Handling Characteristics:5.12.1 F3173/F3173M 15 17 Standard Specification for Aircraft Handling Characteristics of Aeroplanes5.13 Vibration, Buffeting, and High-Speed Characteristics:5.13.1 F3173/F3173M 15 17 Standard Specification for Aircraft Handling Characteristi
33、cs of Aeroplanes5.14 Performance and Flight Characteristics Requirements for Flight in Icing Conditions:5.14.1 F3120/F3120M 15 Standard Specification for Ice Protection for General Aviation Aircraft5.15 Operating Limitations:5.15.1 F3174/F3174M 15 18 Standard Specification for Establishing Operating
34、 Limitations and Information forAeroplanes6. Structures6.1 Structural Design Envelope:6.1.1 F3116/F3116M 15 Standard Specification for Design Loads and Conditions6.2 Interaction of Systems and Structure6.3 Structural Design Loads:6.3.1 F3116/F3116M 15 Standard Specification for Design Loads and Cond
35、itions6.4 Flight Load Conditions:6.4.1 F3116/F3116M 15 Standard Specification for Design Loads and Conditions6.5 Ground and Water Load Conditions:6.5.1 F3116/F3116M 15 Standard Specification for Design Loads and Conditions6.6 Component Loading Conditions:6.6.1 F3061/F3061M 17 Standard Specification
36、for Systems and Equipment in Small Aircraft6.6.1.1 F3232/F3232M 17 Standard Specification for Flight Controls in Small Aircraft6.6.2 F3116/F3116M 15 Standard Specification for Design Loads and Conditions6.7 Limit and Ultimate Loads:6.7.1 F3114 15 Standard Specification for Structures6.8 Structural S
37、trength:6.8.1 F3114 15 Standard Specification for Structures6.9 Structural Durability:6.9.1 F3061/F3061M 17 Standard Specification for Systems and Equipment in Small Aircraft6.9.2 F3115/F3115M 15 Standard Specification for Structural Durability for Small Aeroplanes6.10 Aeroelasticity:6.10.1 F3061/F3
38、061M 17 Standard Specification for Systems and Equipment in Small AircraftF3264 18a36.10.2 F3093/F3093M 15 Standard Specification for Aeroelasticity Requirements6.11 Design and Construction Principles:6.11.1 F3061/F3061M 17 Standard Specification for Systems and Equipment in Small Aircraft6.11.1.1 F
39、3232/F3232M 17 Standard Specification for Flight 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 Systems and Equipment in Small Aircraft6.12.1.1 F3232/F3232M 17 Standard Specification for Fl
40、ight Controls in Small Aircraft6.12.2 F3114 15 Standard Specification for Structures6.12.3 F3066/F3066M 15 18 Standard Specification forAircraft Powerplant Systems Specific Installation Hazard Mitigation6.13 Materials and Processes:6.13.1 F3114 15 Standard Specification for Structures6.14 Special Fa
41、ctors of Safety:6.14.1 F3061/F3061M 17 Standard Specification for Systems 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 Systems and Equipment in Small Aircraft6.15.1.1 F3232/F3232M 17 St
42、andard Specification for Flight Controls in Small Aircraft6.15.2 F3083/F3083M 16 Standard Specification for Emergency Conditions, Occupant Safety and Accommodations7. Design and Construction7.1 Flight Control Systems:7.1.1 F3061/F3061M 17 Standard Specification for Systems and Equipment in Small Air
43、craft7.1.1.1 F3232/F3232M 17 Standard Specification for Flight Controls in Small Aircraft7.1.2 F3066/F3066M 15 18 Standard Specification for Aircraft Powerplant Systems Specific Installation Hazard Mitigation7.2 Landing Gear Systems:7.2.1 F3061/F3061M 17 Standard Specification for Systems and Equipm
44、ent in Small Aircraft7.3 Buoyancy for Seaplanes and Amphibians:7.3.1 F3061/F3061M 17 Standard Specification for Systems and Equipment in Small Aircraft7.4 Means of Egress and Emergency Exits:7.4.1 F3061/F3061M 17 Standard Specification for Systems and Equipment in Small Aircraft7.4.2 F3083/F3083M 16
45、 Standard Specification for Emergency Conditions, Occupant Safety and Accommodations7.5 Occupant Physical Environment:7.5.1 F3061/F3061M 17 Standard Specification for Systems and Equipment in Small Aircraft7.5.1.1 F3227/F3227M 17 Standard Specification for Environmental Systems in Small Aircraft7.5.
46、2 F3083/F3083M 16 Standard Specification for Emergency Conditions, Occupant Safety and Accommodations7.5.3 F3114 15 Standard Specification for Structures7.5.4 F3117 15 18b Standard Specification for Crew Interface in Aircraft7.6 Fire Protection:7.6.1 F3061/F3061M 17 Standard Specification for System
47、s and Equipment in Small Aircraft7.6.1.1 F3231/F3231M 17 Standard Specification for Electrical Systems in Small Aircraft7.6.1.2 F3234/F3234M 17 Standard Specification for Exterior Lighting in Small Aircraft7.6.2 F3066/F3066M 15 18 Standard Specification for Aircraft Powerplant Systems Specific Insta
48、llation Hazard Mitigation7.6.3 F3083/F3083M 16 Standard Specification for Emergency Conditions, Occupant Safety and Accommodations7.7 Fire Protection in Designated Fire Zones and Adjacent Areas:7.7.1 F3061/F3061M 17 Standard Specification for Systems and Equipment in Small Aircraft7.7.1.1 F3231/F323
49、1M 17 Standard Specification for Electrical Systems in Small Aircraft7.7.2 F3066/F3066M 15 18 Standard Specification for Aircraft Powerplant Systems Specific Installation Hazard Mitigation7.7.3 F3114 15 Standard Specification for Structures7.8 Lightning Protection:7.8.1 F3061/F3061M 17 Standard Specification for Systems and Equipment in Small Aircraft7.9 Design and Construction InformationF3264
