Hi All, I wonder if this potential application from 2020 is still on the development agenda given talk of “generic approval”?
The FAA disagrees with the request to mandate CVM structural monitoring sensors, a repetitive CVM NDT procedure with an 18,000 flight cycle compliance time, and periodic monitoring of crack propagation. SMS did not provide sufficient substantiation to show the effectivity of CVM technology for this application. Therefore, the FAA cannot specify or allow that technology and inspection method as an alternative to those specified in this SNPRM.
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(20min delay)