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I like them. Tweaking too much leads to similar imperfections.
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It’s close, but could be optimized.
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Cirrus 22-6460004 Continued Airworthiness Rev C signed.pdf (2.2 MB)
You can reference this document to learn more about the system. For flight test, the below parameters are applicable (see p. 30).
You might see the manifold pressure and fuel flow drop once the oil is up to normal operating temperature. For test flights, I preferred to warm it up for 20 minutes in low altitude cruise before testing it in climb to 17,500 ft. It looks like it was flown here at 2,700 ft DA. You need a test flight to climb so you can check turbo and absolute pressure controller operation, among other parameters.
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You own a TN, not a turbo. There is a difference. These parameter’s other than rpm being low, should be 2700 +/- 10 look fine to me on takeoff which I am assuming this is…
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Get the rpm up to 2700 and enjoy
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It was 2700 when I flew it today.
It’s my plane and I don’t appreciate the thread title 
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Well the digital evidence seems to show 2660 rpm sir….
Would you care to explain the record counselor?
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Today means today!
I have no idea what this shop did on the ground run but they spooked my (former) buyer and apparently haven’t read the TN supplement- and don’t even know that TN’s show high MP in the initial phase of flight.
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Sadness sir.