In July 1942, the Regia Aeronautica requested designs for a new aircraft, propelled by the German DB 605 engine, capable of flying at 620 km/h  with a range of 1,600 km . The armament should consist of six MG 151 cannons in the nose and wings and a 12.7 mm Breda-SAFAT machine gun as a defensive weapon. It should have an 800 kg bomb load. At that point, the request for a long-range fighter killed the SM.88, still in development, and the SM.91, a larger, heavier and more modern design, was authorized.
The fuselage and the wings were all-metal, to achieve the best performance regardless of cost. The central nacelle held the crew of two, and the wings and tail were similar to the SM.88. Fuel capacity was 1,600 l, but with auxiliary tanks could be raised to 1,800 l. It is unknown if it was capable of a range of 1,600 km .
The two DB 605 engines gave a total of 2,950 hp. The aircraft's maximum speed at 585 km/h  was better than the SM.88. There were three 20 mm MG 151s in the nose. Two more were mounted in the wings, close to the fuselage. Another machine gun was provided for the rear gunner. Total bomb load was 1,640 kg or a torpedo.

The prototype, designated MM.530, flew for the first time on 11 March 1943, tested by Aldo Moggi. There were two prototypes, the second a modified SM.88 prototype.

The machine flew at Vergiate and logged 27 hours in the next few months. It was advanced, but was not entered into the official tests at Guidonia, perhaps because it was still undergoing testing. The first prototype was captured and sent to Germany in October 1943, after which it vanished and is presumed destroyed. The second prototype was captured by the Germans incomplete when they occupied northern Italy in September 1943. This aircraft was tested on 10 July 1944, but was destroyed by Allied bombers later in the year.
Type 2 eat (pilot and rear gunner)
Engine 2 Daimler-Benz  DB 605A-1 with 3-bladed constant speed propellers
Dimensions Length 13,25 m , height 3,85 m ,  span 19,7 m , wing area 41,76 m2  ,
Weights Empty 6400 kg, loaded 8890 kg , max. take off weight , fuel1600 l  plus 825 l drop-tank
Performance Max.. speed 584 km/h at 7000 m , cruising speed 515 km/h , range 1600 km, endurance  , service ceiling 11000 m  , climb to 6000 m 8 min. 30 sec.
Armament 6 x 20 mm  MG 151 cannon (three in the nacelle nose, two in the wing-roots and one in the rear cockpit.),  1,640 kg  bombload:- 4x 100 kg  bombs or 4x 160 kg  bombs or 1x 500 kg  bomb or 1x torpedo or 1x 825 I  drop-tank
Type Werk.Nr Registration History
MM.530 First flight 11 March 1943. Captured and sent to Germany in October 1943. Probably destroyed
Captured by the Germans incomplete in September 1943. Tested on 10 July 1944, but destroyed by allied bombers later in the year