Text in force at 23-63: from 23-17, effective 1 Feb 1977.
[(a) Each detail of each control system must be designed and installed to prevent jamming, chafing, and interference from cargo, passengers, loose objects, or the freezing of moisture.]
(b) There must be means in the cockpit to prevent the entry of foreign objects into places where they would jam the system.
(c) There must be means to prevent the slapping of cables or tubes against other parts.
(d) Each element of the flight control system must have design features, or must be distinctively and permanently marked, to minimize the possibility of incorrect assembly that could result in malfunctioning of 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