cfr_sections: 14:14:1.0.1.3.15.4.176.26
Data license: Public Domain (U.S. Government data) · Data source: Federal Register API & Regulations.gov API
This data as json
| section_id | title_number | title_name | chapter | subchapter | part_number | part_name | subpart | subpart_name | section_number | section_heading | agency | authority | source_citation | amendment_citations | full_text |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| 14:14:1.0.1.3.15.4.176.26 | 14 | Aeronautics and Space | I | C | 27 | PART 27—AIRWORTHINESS STANDARDS: NORMAL CATEGORY ROTORCRAFT | D | Subpart D—Design and Construction | 27.683 | § 27.683 Operation tests. | FAA | 49 U.S.C. 106(f), 106(g), 40113, 44701-44702, 44704. | Docket No. 5074, 29 FR 15695, Nov. 24, 1964, unless otherwise noted. | It must be shown by operation tests that, when the controls are operated from the pilot compartment with the control system loaded to correspond with loads specified for the system, the system is free from— (a) Jamming; (b) Excessive friction; and (c) Excessive deflection. |