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ASTM F 3174/F3174M : 2021

Current

Current

The latest, up-to-date edition.

Standard Specification for Establishing Operating Limitations and Information for Aeroplanes

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

07-12-2021

€56.53
Excluding VAT

Committee
F 44
DocumentType
Standard
Pages
5
PublisherName
American Society for Testing and Materials
Status
Current
Supersedes

1.1This specification covers airworthiness requirements 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 F3117/F3117M for means and methods of presentation. The material was developed through open consensus of international experts in general aviation. This information was created by focusing on Level 1, 2, 3, and 4 Normal Category aeroplanes. The content may be more broadly applicable; it is the responsibility of the applicant to substantiate broader applicability as a specific means of compliance. The topics covered within this specification are: Limitations for Airspeed, Weight and Center of Gravity, Auxiliary Power Units, Minimum Flight Crew, Maximum Passenger Seating Configuration, Kinds of Operation, and Maximum Operating Altitude.

1.2An applicant intending to propose this information as Means of Compliance for a design approval must seek guidance from their respective oversight authority (for example, published guidance from applicable CAAs) concerning the acceptable use and application thereof. For information on which oversight authorities have accepted this specification (in whole or in part) as an acceptable Means of Compliance to their regulatory requirements (hereinafter “the Rules”), refer to the ASTM Committee F44 web page (www.astm.org/COMMITTEE/F44.htm). Annex A1 maps the Means of Compliance described in this specification to EASA CS-23, amendment 5, or later, and FAA 14 CFR Part 23, amendment 64, or later.

1.3Units—This specification may present information in either SI units, English Engineering units, or both; the values stated in each system may not be exact equivalents. Each system shall be used independently of the other; combining values from the two systems may result in nonconformance with the standard.

1.4This 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, health, and environmental practices and determine the applicability of regulatory limitations prior to use.

1.5This 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.

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ASTM F 3173/F3173M : 2024 Standard Specification for Aircraft Handling Characteristics
ASTM F 3117/F3117M : 2023 : REV B Standard Specification for Crew Interface in Aircraft
ASTM F 3082/F3082M : 2023 : REV A Standard Specification for Weights and Centers of Gravity of Aircraft
ASTM F 3117/F3117M : 2023 : REV A Standard Specification for Crew Interface in Aircraft
ASTM F 3082/F3082M : 2022 Standard Specification for Weights and Centers of Gravity of Aircraft
ASTM F 3116/F3116M : 2018 : EDT 2 Standard Specification for Design Loads and Conditions
ASTM F 3116/F3116M : 2023 : REV A Standard Specification for Design Loads and Conditions
ASTM F 3082/F3082M : 2023 Standard Specification for Weights and Centers of Gravity of Aircraft
ASTM F 3173/F3173M : 2023 : REV A Standard Specification for Aircraft Handling Characteristics
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