Which section of the ASTM F44 F3264 standard is specifically cited for component loading conditions?

Section 6.6, titled 'Component Loading Conditions'.

What is the exact section number and title within ASTM F44 F3264 that is cited for component loading conditions?

Section 6.6, titled 'Component Loading Conditions'.

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

Standard Practice for Aircraft Simplified Loads Criteria.

F3232/F3232M-25, Standard Specification for Flight Controls in Small Aircraft.

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

Specification for Normal Category Aeroplanes Certification.

Standard Specification for Design Loads and Conditions.

Standard Practice for Aircraft Simplified Loads Criteria.

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ED Decision 2026/003/R

ASTM F44 F3264 Standard Specification for Normal Category Aeroplanes Certification

6.6 Component Loading Conditions

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

F3232/F3232M-25 Standard Specification for Flight Controls in Small Aircraft

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

F3396/F3396M-20 Standard Practice for Aircraft Simplified Loads Criteria

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

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

Source-Title: AMC1 23.2225 Component loading conditions View latest amendments

Erulesid: ERULES-1963177438-6961 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 23.2225 Component loading conditions

Origin: EASA

Category: EAR