The definition of the acrobatic category in FAR 23.3 reads as follows:
(c) The acrobatic category is limited to airplanes that have a seating configuration, excluding pilot seats, of nine or less, a maximum certificated takeoff weight of 12,500 pounds or less, and intended for use without restrictions, other than those shown to be necessary as a result of required flight tests.
Considering that the Northrop T-38 is a two-seat, twin-engined supersonic jet trainer aircraft with a USAF service maximum takeoff weight of 12,093 lbs (from their factsheet), what traits of the T-38 would have prohibited Northrop from applying for a civil Type Certificate for the T-38 in the acrobatic category?