Text in force at 23-63: from 23-17, effective 1 Feb 1977.
[(a) Each control system must have stops that positively limit the range of motion of each movable aerodynamic surface controlled by the system.
(b) Each stop must be so located so that wear, slackness, or take-up adjustments will not adversely affect the control characteristics of the airplane because of a change in the range of surface travel.
(c) Each stop must be able to withstand any loads corresponding to the design conditions for the control system.] Notice of Invitation to Submit Proposals; Notice No. 74-5; Issued on 2/14/74. Notice of Compilation of Proposals; Notice No. 74-5A; Issued on 5/22/74. Notice of Availability of Agenda; Notice No. 74-5B; Issued on 10/3/74. Notice of Clarifying Revisions; Notice No. 74-33; Issued on 10/3/74. Notice of Conference; Notice No. 74-5C; Issued on 11/25/74. Notice of Availability of Conference Summary; Notice No. 74-5D; Issued on 2/4/75. Notice of Airworthiness Review Program No. 2; Notice No. 75-10; Issued on 2/27/75. Notice of Airworthiness Review Program No. 3; Notice No. 75-19; Issued on 5/13/75. Notice of Airworthiness Review Program No. 4; Notice No. 75-20; Issued on 5/13/75. Notice of Airworthiness Review Program No. 5; Notice No. 75-23; Issued on 5/19/75. Notice of Airworthiness Review Program No. 6; Notice No. 75-25; Issued on 5/29/75. Notice of Airworthiness Review Program No. 7; Notice No. 75-26; Issued on 6/9/75.
41 FR 55464 · Source