I guessing, but it most likely had to do with the 61 kt stall speed.
Single engine aircraft are restricted to a 61 kt vs1.
This will ultimately limit weight for a particular wing area.
Pilatus (I think) got some sort of exemption by proving that the aircraft is so crashworthy that a slightly higher speed is justified.
Thay had to prove to the FAA that the seats and airframe met tighter G-load standards, or something.
Any other guesses?