§23.2420. Reversing systems.
14 C.F.R. § 23.2420
Each reversing system must be designed so that—
No unsafe condition will result during normal operation of the system; and
The airplane is capable of continued safe flight and landing after any single failure, likely combination of failures, or malfunction of the reversing system.
Notes, amendments, and revision history
Authority
Authority: 49 U.S.C. 106(f), 106(g), 40113, 44701-44702, 44704, Pub. L. 113-53, 127 Stat. 584 (49 U.S.C. 44704) note.
Source
Source: Doc. No. FAA-2015-1621, Amdt. 23-64, 81 FR 96689, Dec. 30, 2016, unless otherwise noted.