Further to the above, in the 1971-72 Janes All The World's Aircraft, a GA drawing was reproduced of the redesigned SA 28T as it said in the text. As has been previously mentioned the Model SA28T was to be eventually powered by a pair of TFE731-1 turbofan engines. In the text in Janes it said that the design utilized many lessons gained from supersonic aircraft studies, which Swearingen had looked at in the 1960s. As well as the shoulder-mounted delta main wing, a delta tailplane of a slab variety was planned to be used. Although the first plans of the Model SA 28T had the engines mounted on the sides of the area-ruled fuselage and indeed the photo of the complete aircraft also shows this feature, it was reported in Janes that during wind tunnel tests these had caused excessive drag, hence an under-wing arrangement had been chosen. Also as a result of this wind-tunnel testing, the wing position had been changed from the bottom of the fuselage to the shoulder position, as seen in the attached GA drawing. With an MTOW of 13,500 lb (6123 kg) the seven-seat SA 28T was expected to have a top speed of around 575 mph (925 km/h), with an estimated range of around 2,300 miles (3700 km).