Which sections of the ASTM F44 F3264 standard are specifically referenced in AMC1 23.2240?

Section 6.9 'Structural Durability' and Section 9.11 'Equipment Containing High-Energy Rotors'.

AMC1 23.2240 Structural durability

ASTM F44 F3264 Standard, Specification for Normal Category Aeroplanes Certification.

F3498-21, Standard Practice for Developing Simplified Fatigue Load Spectra.

F3116/F3116M-24, Standard Specification for Design Loads and Conditions.

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ED Decision 2026/003/R

ASTM F44 F3264 Standard Specification for Normal Category Aeroplanes Certification

6.9 Structural Durability & 9.11 Equipment Containing High-Energy Rotors

F3061/F3061M-24a Standard Specification for Systems and Equipment in Small Aircraft

F3066/F3066M-18 Standard Specification for Aircraft Powerplant Installation Hazard Mitigation

F3115/F3115M-15 Standard Specification for Structural Durability for Small Aeroplanes

F3380-19 Standard Practice for Structural Compliance of Very Light Aeroplanes

F3116/F3116M-24 Standard Specification for Design Loads and Conditions

F3498-21 Standard Practice for Developing Simplified Fatigue Load Spectra

[AMC & GM to CS-23: Issue 4]

[AMC & GM to CS-23: Issue 5]

Source-Title: AMC1 23.2240 Structural durability View latest amendments

Erulesid: ERULES-1963177438-6966 Compare versions

Domain: Initial airworthiness

Amendedby: CS-23 Amendment 6 and AMC ＆ GM to CS-23 Issue 5

Applicabilitydate: 16 April, 2026

Entryintoforcedate: 16 April, 2026

Regulatorysource: ED Decision 2026/003/R Navigate

Regulatorysubject: CS-23

Typeofcontent: AMC to CS (Acceptable means of compliance to certification specification)

Parentir: CS 23.2240 Structural durability

Origin: EASA

Category: EAR