FAA Federal Aviation Regulations (FARS, 14 CFR)
FARs > Part 33 > Section 33 - Vibration
section 33.31 |
section 33.35
The engine must be designed and constructed to function throughout its normal operating range of crankshaft rotational speeds and engine powers without inducing excessive stress in any of the engine parts because of vibration and without imparting excessive vibration forces to the aircraft structure.
   
Current page: FARs > Part 33 > Section 33 - Vibration
section 33.31 |
section 33.35
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