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ASTM F3264-17

(Specification)

Standard Specification for Normal Category Aeroplanes Certification

Standard Specification for Normal Category Aeroplanes Certification

SCOPE
1.1 Applicability:  
1.1.1 This specification identifies the industry standards which have been determined by consensus to demonstrate compliance to the requirements (“the Rules”) for Level 1, 2, 3, 4 Normal Category Aeroplanes.  
1.1.2 Unless specifically defined otherwise, the herein referenced specifications are only applicable to the aeroplanes defined in 1.1.1.  
1.1.3 Only standards that are considered mature enough for general application to certification projects and have been found acceptable by committee consensus to propose to the CAAs for acceptance as a Means of Compliance to their Rules are included.  
1.1.4 In the event that a particular CAA’s requirements are not harmonized with the other CAA’s requirements, the standards will be written to include the non-harmonized requirements as well as the harmonized requirements with the applicability defined in the standard.  
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 their requirements. Acceptance and applicability as a MoC to the CAA’s airworthiness rules remains the decision of the respective CAAs. CAAs may accept this specification, with or without limitations as defined in their specification acceptance document. For information on which CAAs have accepted these standards (in whole or in part) as an acceptable MoC to their 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 from their respective CAA concerning the use of this specification and any referenced Specifications, Practices, Test Methods, or Guides to show compliance to the CAA rules. Alternatively, an applicant may propose a MoC other than those included in this specification but it is their responsibility to obtain approval of their proposed MoC from their CAA.  
1.4 This international standard was developed in accordance with internationally recognized principles on standardization established in the Decision on Principles for the Development of International Standards, Guides and Recommendations issued by the World Trade Organization Technical Barriers to Trade (TBT) Committee.

General Information

Status
Historical
Publication Date
31-Aug-2017
ICS
49.020 - Aircraft and space vehicles in general
Technical Committee
F44 - General Aviation Aircraft
Drafting Committee
F44.10 - General
Current Stage
Ref Project

Relations

Referred By
ASTM F3563-22 - Standard Specification for Design and Construction of Large Fixed Wing Unmanned Aircraft Systems
Effective Date
01-Sep-2017
Referred By
ASTM F3457-20 - Standard Guide for Aircraft Certification Education Standards for Engineers and Professionals in Aerospace Industry
Effective Date
01-Sep-2017

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ASTM F3264-17 - Standard Specification for Normal Category Aeroplanes CertificationASTM F3264-17 - Standard Specification for Normal Category Aeroplanes Certification
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ASTM F3264-17 - Standard Specification for Normal Category Aeroplanes Certification
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NOTICE: This standard has either been superseded and replaced by a new version or withdrawn.
Contact ASTM International (www.astm.org) for the latest information
Designation: F3264 −17
Standard Specification for
1
Normal Category Aeroplanes Certification
This standard is issued under the fixed designation F3264; the number immediately following the designation indicates the year of
original adoption 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. Scope 1.4 This international standard was developed in accor-
dance with internationally recognized principles on standard-
1.1 Applicability:
ization established in the Decision on Principles for the
1.1.1 This specification identifies the industry standards
Development of International Standards, Guides and Recom-
which have been determined by consensus to demonstrate
mendations issued by the World Trade Organization Technical
compliance to the requirements (“the Rules”) for Level 1, 2, 3,
Barriers to Trade (TBT) Committee.
4 Normal Category Aeroplanes.
1.1.2 Unless specifically defined otherwise, the herein ref-
2. Referenced Documents
erenced specifications are only applicable to the aeroplanes
2
2.1 ASTM Standards:
defined in 1.1.1.
1.1.3 Only standards that are considered mature enough for
NOTE 1—Referenced ASTM standards are listed in Sections5–10 of
general application to certification projects and have been this specification.
found acceptable by committee consensus to propose to the F2490 Guide for Aircraft Electrical Load and Power Source
Capacity Analysis
CAAs for acceptance as a Means of Compliance to their Rules
are included. F3060 Terminology for Aircraft
F3061/F3061M Specification for Systems and Equipment in
1.1.4 In the event that a particular CAA’s requirements are
not harmonized with the other CAA’s requirements, the stan- Small Aircraft
F3062/F3062M Specification for Installation of Powerplant
dards will be written to include the non-harmonized require-
ments as well as the harmonized requirements with the Systems
F3063/F3063M Specification for Design and Integration of
applicability defined in the standard.
Fuel/EnergyStorageandDeliverySystemInstallationsfor
1.2 Civil Aviation Authorities:
Aeroplanes
1.2.1 CAAs may accept a specific revision of this specifi-
F3064/F3064M Specification for Control, Operational Char-
cation as an acceptable Means of Compliance (MoC) to their
acteristics and Installation of Instruments and Sensors of
requirements. Acceptance and applicability as a MoC to the
Propulsion Systems
CAA’s airworthiness rules remains the decision of the respec-
F3065/F3065M Specification for Installation and Integration
tive CAAs. CAAs may accept this specification, with or
of Propeller Systems
without limitations as defined in their specification acceptance
F3066/F3066M Specification for Powerplant Systems Spe-
document. For information on which CAAs have accepted
cific Hazard Mitigation
these standards (in whole or in part) as an acceptable MoC to
F3082/F3082M Specification for Flight for GeneralAviation
their Rules, refer to the ASTM F44 webpage (www.astm.org/
Aeroplanes
COMMITTEE/F44.htm) which includes CAA website links.
F3083/F3083M Specification for Emergency Conditions,
1.3 Applicant Responsibility:
Occupant Safety and Accommodations
1.3.1 The applicant must seek individual guidance from
F3093/F3093M Specification for Aeroelasticity Require-
their respective CAA concerning the use of this specification
ments
and any referenced Specifications, Practices, Test Methods, or
F3114 Specification for Structures
Guides to show compliance to the CAArules.Alternatively, an
F3115/F3115M Specification for Structural Durability for
applicant may propose a MoC other than those included in this
Small Airplanes
specification but it is their responsibility to obtain approval of
F3116/F3116M Specification for Design Loads and Condi-
their proposed MoC from their CAA.
tions
1
ThisspecificationisunderthejurisdictionofASTMCommitteeF44onGeneral
2
Aviation Aircraft and is the direct responsibility of Subcommittee F44.10 on For referenced ASTM standards, visit the ASTM website, www.astm.org, or
General. contact ASTM Customer Service at service@astm.org. For Annual Book of ASTM
Current edition approved Sept. 1, 2017. Published September 2017. DOI: Standards volume information, refer to the standard’s Document Summary page on
10.1520/F3264-17. the ASTM website.
Copyright © ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959. United States
1

---------------------- Page: 1 ----------------------
F3264 − 17
F3117 Specification for Crew Interface in Aircraft 3.3 Abbreviations:
F3120/F3120M Specification for Ice Protection for General 3.3.1 CAA—Civil Aviation Authority
Aviation Aircraft
3.3.2 MoC—Means of Compliance
F3173/F3173M Specification for Handling Characteristics
of Aeroplanes 4.
...

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