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This specification prescribes airworthiness design requirements for the establishment of operating limitations and information for the operation of aeroplanes. It addresses the general limitations and information to be contained in the aeroplane flight manual. 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 certification plan.
The requirements described in this specification cover: airspeed limitations, operating maneuvering speed, flap extended speed, minimum control speed, weight and center of gravity, auxiliary power unit limitations, minimum flight crew, maximum passenger seating configuration, kinds of operation, and maximum operating altitude.
This abstract is a brief summary of the referenced standard. It is informational only and not an official part of the standard; the full text of the standard itself must be referred to for its use and application. ASTM does not give any warranty express or implied or make any representation that the contents of this abstract are accurate, complete or up to date.
1.1 This specification establishes the airworthiness design requirements associated with the establishment of operating limitations and information for the operation of aeroplanes. It covers the need for establishing general limitations and information to be contained in the aeroplane flight manual. This specification specifies what information shall be provided and does not state how such information shall be presented unless this is necessary for the clarity of the purpose of the specification. Refer to Specification for means and methods of presentation.
1.2 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 certification plan. For information on which CAA regulatory bodies have accepted this specification (in whole or in part) as a means of compliance to their small aeroplane airworthiness regulations (hereinafter referred to as “the Rules”), refer to ASTM Committee F44 webpage (www.ASTM.org/COMITTEE/F44.htm), which includes CAA website links.
1.3 This specification is applicable to small aeroplanes.
1.4 Units—The values stated in either SI units or inch-pound units are to be regarded separately as standard. The values stated in each system may not be exact equivalents; therefore, each system shall be used independently of the other. Combining values from the 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 responsibility of the user of this standard to establish appropriate safety and health practices and determine the applicability of regulatory limitations prior to use.
2. Referenced Documents (purchase separately) The documents listed below are referenced within the subject standard but are not provided as part of the standard.
F3060 Terminology for Aircraft
F3114 Specification for Structures
F3116 Specification for Design Loads and Conditions
F3117 Specification for Crew Interface in Aircraft
European Aviation Safety Agency RegulationsCS-23 Certification Specifications for Normal, Utility, Aerobatic, and Commuter Category Aeroplanes (Amendment 3) CS-VLA Certification Specifications for Very Light Aeroplanes (Amendment 1)
U.S. Code of Federal Regulations14 CFR Part 23 Airworthiness Standards: Normal, Utility, Aerobatic and Commuter Category Airplanes (Amendment 62)
ICS Number Code 49.020 (Aircraft and space vehicles in general)
UNSPSC Code 25130000(Aircraft)
|Link to Active (This link will always route to the current Active version of the standard.)|
ASTM F3174 / F3174M-15, Standard Specification for Establishing Operating Limitations and Information for Aeroplanes, ASTM International, West Conshohocken, PA, 2015, www.astm.orgBack to Top