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CS 29.1465 Vibration Health Monitoring
Available versions for ERULES-1963177438-6723
ED Decision 2012/022/R
found in: CS-29 Amdt 10 - Large Rotercraft (Jan 2023)
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CS-29 Amdt 12 - La... (Mar 2026)
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CS 29.1465 Vibration Health Monitoring ED Decision 2012/022/R (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. [Amdt 29/3]
CS 29.1465 Vibration Health Monitoring ED Decision 2012/022/R (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. [Amdt 29/3]
#### CS 29.1465 Vibration Health Monitoring *ED Decision 2012/022/R* (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. [Amdt 29/3]