They have been carried out tests of virtual simulation of the aircraft with software designed specifically for this function. A model was designed with the following data:
 
Span: 26.6 m.
Total longitude: 23.3 m.
Total height: 7.5 m.
Area of the wing: 700 pies².
Area horizontal stabilizer: 178 pies².
Area vertical stabilizer: 90 x 2 pies².
Longitude of the container: 12 m.
Longitude of the head: 4.7 m.
Weigh maximum to take off: 18.000 kg. (with container and fuel)
Weigh minimum: 8.000 kg. (without container neither fuel)
 
Propellers:
Power max. per engine 8000 feet/pound
Diam. propeller: 13.5 feet
No. blades: 4
 
With the virtual tests, they were obtained been fully satisfactory flight test in the different suppositions to carry out for the aircraft.