§25.367. Unsymmetrical loads due to engine failure. — Inbound Citations
14 C.F.R. § 25.367
Statutory Authority
Cited by 3 regulations in release Current.
Citations to 14 C.F.R. § 25.367 as a whole
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(3) The limit rolling conditions specified in § 25.349 and the limit unsymmetrical conditions specified in §§ 25.367 and 25.427 (a) through (c), at speeds up to VC.
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Turbopropeller power airplane propeller-drag limiting systems must be designed so that no single failure or malfunction of any of the systems during normal or emergency operation results in propeller drag in excess of that for which the airplane was designed under § 25.367. Failure of structural elements of the drag limiting systems need not be considered if the probability of this kind of failure is extremely remote.