Mojave's MTOW is 3000 kg(2 times the TB3's) and its engine produces 450 hp(2 times the power output of PD222, 2x225hp). If we assume the requirements are changing linearly for small differences then PD222 makes more sense. It's oversimplified but gives the ballpark.
We may also check Mojave's operational range chart. (Given with respect to payload and take off distance-limiting fuel payload). In the STOL mode it gets 4 to 6 hours of ISR capability, unarmed.
It was going to be PD180 but likely they (Navy) noticed it doesn't worth the +8HP continous and -4 kg for -15HP @30k feet. PD180 is a nice engine but didn't fit this, has a great export potential nonetheless.
Same applies for PD222ST, +1kg, -15HP @30k feet but +50HP @ take off and +30HP @ continous @ 20k feet. Suits for STOL but not high altitude operations.
(Numbers given with respect to PD170DT's specs).
Looks like PD180 was omitted with the given weight figures and it was found more logical to apply pressure on Baykar to reduce weight of the platform (which they did, greater than what PD180 has provided).
I am assured there will be PD222ST variant on TB3 and there will be two kinds of TB3 on Anadolu. One for ISR @30k, another for strike at @20-25k feet. If there happens to be a PD222/5DT then these two platforms may be commonized. But TEI is busy with projects and may not be able to spare enough time for the certification processes of all programs. So i assume in mid term we will have mix of PD170/222, starting with PD170.
Based on Navy's habit of commonization we may also see TB-2 being handed over to another operator, or a friendly country and all replaced with Land based TB3.