FAA Federal Aviation Regulations (FARS, 14 CFR)
FARs > Part 33 > Section 63 - Vibration
section 33.62 |
section 33.65

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.
[Doc. No. 28107, 61 FR 28433, June 4, 1996]
  
Current page: FARs > Part 33 > Section 63 - Vibration
section 33.62 |
section 33.65

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