Why not? if it offers you so much at so low a cost..
IRST will not be coming in the Block-II.. I can assure you..
You have to forget the impression of a Block-II.. its not going to be a new airplane.
Even PAC does not call it that..
its referred to as a "Continuation of co-production of aircraft".. Batch-II.
The Term Block-II was a misnomer in an attempt to liken the aircraft to the F-16 that stuck.
the F-16 had 1,5,10,15,20,25,30,40,42,50,52,60 numbers for blocks.
Of which the major change for block 10->15(which was interestingly implemented across the older fleet as well) was the change of tailplane design.
Let me give you an example of changes in these various blocks:
difference from F-16 block-1
Block-5:On Block 5, the gray radome was introduced, which became standard for all later Fighting Falcons. The Block 5 production batch totaled 197 aircraft. These aircraft were also upgraded to Block 10 specifications under Pacer Loft I and II. Block 5 F-16s have the same blade UHF antenna under the intake as the Block 1, as well as the small stabilator. Differences with the Block 1 are inconspicuous, involving modifications to improve reliability and mission-ready rate.
Block-10:The F-16s still had the blade UHF aerial and small tail. Differences with Block 5 aircraft are again internal improvements with no apparent external modifications. Some USAF Block 10 aircraft were later (1987-1993) retrofitted to block 15OCU standard
Block-15: the Block 15 introduced MSIP Stage I changes to the F-16A/B starting with subblock 15Y and continuing through subblock 15AZ. More than a year earlier, in February 1980, these modifications were already effective on the F-16C/D production. The changes expanded the F-16s growth potential by allowing improved capabilities in the air-to-ground and BVR missions.
One major modification was the addition of two hardpoints to (and structural strengthening of) the chin of the inlet, designated hardpoints 5L and 5R. To offset the shift in center of gravity caused by the weight of these two additional hardpoints (and eventual stores attached to them), the extended horizontal stabilator (the so-called "big tail", 30% increase in area), was fitted. The new tail also provided better stability and more authority for out-of-control situations. It changed lift-off rotation speeds and allowed stable flight at higher angles of attack.
The AN/APG-66 radar on the Block 15 Fighting Falcons was provided with an early version of a track-while-scan mode for greater air defense capability. The F-16s were also equipped with Have Quick I secure UHF radios, and internal provisions for the AIM-7 were made. Additional structural strengthening was performed to allow an extra 1000 pounds of ordnance to be carried on the underwing points. Last but not least, pilot comfort was enhanced by improving the cockpit air conditioning.
The Block-15 had improvements in avionics, and airframe.. but before that.. over 612 aircraft were delivered which were virtually identical.