14 C.F.R. § 33.63

Current through September 30, 2024
Section 33.63 - Vibration

Each engine must be designed and constructed to function throughout its declared flight envelope and operating range of rotational speeds and power/thrust, without inducing excessive stress in any engine part because of vibration and without imparting excessive vibration forces to the aircraft structure.

14 C.F.R. §33.63

Doc. No. 28107, 61 FR 28433, June 4, 1996