Variants
- First Prototype: 559 kW (750 hp) Hiro Type 91 12-cylinder liquid-cooled engine driving a two-bladed propeller.
- Second and Third Prototypes: 477 kW (640 hp) Nakajima Kotobuki-3 nine-cylinder air-cooled radial driving a two-bladed propeller.
- Fourth and Fifth Prototype and Production Aircraft: 626 kW (840 hp) Nakajima Hikari-2 nine-cylinder air-cooled radial driving a two-bladed propeller.
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