The first version of the K3M offered to the
Imperial Japanese Navy Air Service was prone to stability problems, and more importantly, problems with the water-cooled Mitsubishi-built
Hispano-Suiza 8A eight-cylinder
liquid-cooled engine. The improved K3M2 used a
Hitachi Amakaze 11 nine-cylinder
air-cooled radial engine, rated at for take-off and at sea level. The first K3M2 production examples entered service in 1932 as the Navy Type 90 Crew Trainer. It was superseded in production with the K3M3, using a
Nakajima Kotobuki air-cooled engine. The Navy Type 90 Crew Trainer was primarily a land-based aircraft, although a few were fitted with floats. The
Imperial Japanese Army Air Force (IJAAF) had an interest in the aircraft as part of its modernization program and as a potential supplement to the
Nakajima Ki-6. Two examples were acquired and tested, and the airframe was given the designation of Ki-7. One prototype used a
Mitsubishi Type 92 nine-cylinder air-cooled radial engine and the other a
Nakajima Kotobuki nine-cylinder air-cooled radial engine. The IJAAF did not order either version into production. The civil version was offered to commercial operators with a Nakajima-built
Bristol Jupiter VI nine-cylinder air-cooled radial engine. The Mitsubishi K3M was used for both civil and military roles, and some remained in operation until well after World War II. ==Variants==