It did meet compliance with the AD prior to the flight in question.

A good number of T-6s were inspected right away and were up and flying
in a relatively short time. Anecdotal comment: As of the last
communication I received, no attach angle fatigue cracks have been
found in any of the T-6s inspected to date (some attach angles with
corrosion were found).

Bela P. Havasreti