14 C.F.R. § 25.391

Current through May 31, 2024

Section 25.391 - Control surface loads: General

The control surfaces must be designed for the limit loads resulting from the flight conditions in §§ 25.331 , 25.341(a) and (b) , 25.349 , and 25.351 , considering the requirements for-

(a) Loads parallel to hinge line, in § 25.393 ;

(b) Pilot effort effects, in § 25.397 ;

(c) Trim tab effects, in § 25.407 ;

(d) Unsymmetrical loads, in § 25.427 ; and

(e) Auxiliary aerodynamic surfaces, in § 25.445 .

14 C.F.R. §25.391

Doc. No. 5066, 29 FR 18291, Dec. 24, 1964, as amended by Amdt. 25-86, 61 FR 5222, Feb. 9, 1996; Amdt. 25-141, 79 FR 73468, Dec. 11, 2014