The Ki-32 was developed in response to a May 1936
Imperial Japanese Army specification to replace the
Kawasaki Ki-3 light bomber with a completely indigenously designed and built aircraft.
Mitsubishi and
Kawasaki were requested to build two prototypes each by December 1936. The specification called for a top speed of at ; normal operating altitude from , the ability to climb to within 8 minutes and an engine to be selected from the
Mitsubishi Ha-6 radial,
Nakajima Ha-5 radial, or
Kawasaki Ha-9-IIb liquid-cooled inline engines, a normal bomb load of and a maximum of , one forward-firing
machine gun and one flexible rearward-firing machine gun, the ability to perform 60-degree dives for
dive bombing, and a loaded weight less than . The first Kawasaki prototype flew in March 1937; seven more prototypes were produced. Being very similar in layout and performance, the main difference between the Kawasaki Ki-32 and its
Mitsubishi Ki-30 rival was in the choice of an engine. The Mitsubishi design used the Nakajima Ha-5 14-cylinder air-cooled
radial engine, whereas Kawasaki opted for their own
Kawasaki Ha-9-II inline
V12 engine. Problems were encountered with the Kawasaki design, particularly with engine cooling, and the Mitsubishi Ki-30 received the production order. In spite of this, the pressing need for more aircraft in the
Second Sino-Japanese War, which had started at full scale in July 1937, resulted in the Ki-32's entry into production as well, 12 months behind its rival. Ironically, the number of Ki-32s built was much higher than that of the successful Ki-30. The Ki-32 entered production in 1938, designated as the
Army Type 98 Single-engine Light Bomber. Kawasaki manufactured 854 Ki-32s before production ceased in May 1940. ==Operational history==