ED Decision 2026/003/R
ASTM F44 F3264 Standard Specification for Normal Category Aeroplanes Certification
7.1 Flight Control Systems
F3061/F3061M-24a Standard Specification for Systems and Equipment in Small Aircraft
F3232/F3232M-25 Standard Specification for Flight Controls in Small Aircraft
F3066/F3066M-18 Standard Specification for Aircraft Powerplant Installation Hazard Mitigation
F3117/F3117M-24a Standard Specification for Crew Interface in Aircraft
Remarks
Except as follows:
For Level 1 single-engine aeroplanes with a stall speed in the landing configuration (VS0) of more than 45 knots, ASTM F3264-24, paragraph 7.1 does not include means for showing that the aeroplane is protected from loss of control when any one connecting or transmitting element in the primary flight control system fails. If applying for certification of a Level 1 single-engine aeroplane with a VS0 greater than 45 knots, applicants may use the requirements of CS 23.677(b)(1) at Amendment 4 as a means of complying with this aspect of CS 23.2300, or may propose a different means of compliance in accordance with CS 23.2010.
For powered trim, applicants may use the provisions of CS 23.677(d) at Amendment 4 as a means of complying with CS 23.2010.
[AMC & GM to CS-23: Issue 4]
[AMC & GM to CS-23: Issue 5]
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