State acceptance testing of two production aircraft was conducted between 27 January and 26 February 1941. They were found to be over heavier than the MiG-1, which reduced maneuverability and field performance. Time to decreased by over a minute and the service ceiling proved to be less. The MiG-3 was faster at sea level and at altitude. While the ranges reached by both aircraft were farther than that of the older aircraft, they were still less than the required. Mikoyan and Gurevich protested against the range results as their calculations showed that the MiG-3 could reach based on a specific fuel consumption (SFC) of 0.46 kg/km (1.64 lb/mile). During the State acceptance trials the SFC was 0.48 kg/km (1.71 lb/mile) but the operational trials conducted earlier showed a SFC of 0.38 kg/km (1.35 lb/mile). They blamed the deficiency on a failure to use an altitude correction and that the engines had not been properly adjusted. They went as far as arranging for two more flights between Leningrad and Moscow to prove that the MiG-3 could fly 1,000 km (621 mi). Two production aircraft were flown on ranges of and , flying at 90% of maximum speed and at an altitude of , contradicting the report of the NII VVS ("Naoochno-Issledovatel'skiy Institoot Voyenno-Vozdooshnykh Seel"—Air Force Scientific Test Institute).