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§29.1465 Vibration health monitoring

CS-29 · Subpart F — Equipment · at CS29-12 (current)

Text in force at CS29-12: from CS29-3, effective 18 Dec 2012.

(a) If certification of a rotorcraft with vibration health monitoring of the rotors and/or rotor drive systems is requested by the applicant, then the design and performance of an installed system must provide a reliable means of early detection for the identified failure modes being monitored. (b) If a vibration health monitoring system of the rotors and/or rotor drive systems is required by the applicable operating rules, then the design and performance of the vibration health monitoring system must, in addition, meet the requirements of this paragraph. (1) A safety analysis must be used to identify all component failure modes that could prevent continued safe flight or safe landing, for which vibration health monitoring could provide a reliable means of early detection; (2) All typical VHM indicators and signal processing techniques should be considered in the VHM System design; (3) Vibration health monitoring must be provided as identified in subparagraph (1) and (2), unless other means of health monitoring can be substantiated.

ED Decision 2012/022/R · Source

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