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AMOC for piper wing spar inspection

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I wonder if it is feasible to remove two bolts at a time, do the eddy current check and reinstall the bolts (with new hardware of course) and check each bolt hole?

The eddy current cost for removing 4 bolts and performing the inspection is around 4k (2 bolts each wing)

Removing all 10 bolts on both wings should be easier (two at a time) The cost could be 6-8k ? However once done and all holes have no cracks would be not only be peace of mind, but it would increase the value of the aircraft.
16B48293-8E8B-4CF5-B7E0-C9C972697D18.jpeg


Picture lower spar cap with two bolts removed for inspection

Any comments???
 
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