Mitsubishi F1M

The Mitsubishi F1M was a Japanese reconnaissance floatplane of World War II.

 It was the last biplane type of the Imperial Japanese Navy, with 944 built between 1936 and 1944.

The Navy designation was, Type Zero Observation Seaplane.

In 1934, the Imperial Japanese Navy issued a specification to Mitsubishi, Aichi and Kawanishi for a replacement for its Nakajima E8N floatplanes, which were used for short-ranged reconnaissance and observation missions from the Navy’s warships.

Mitsubishi’s design, the Ka-17, given the short system designation F1M1 by the Japanese Navy, was a small all-metal biplane powered by a single Nakajima Hikari 1 radial engine rated at 610 kilowatts (820 hp), the same engine as used by Aichi’s competing F1A.

It had elliptical wings and great care had been taken to reduce drag, with the number of interplane struts and bracing wires minimised.

The first of four F1M1s flew in June 1936.

While the F1M1 had better performance than the Aichi aircraft, it had poor stability both on the water and in the air, so the aircraft was redesigned to resolve these problems.

The wings were redesigned, with straight tapered leading and training edges and rigged with greater dihedral, and the vertical fin and rudder were enlarged.

The aircraft’s floats were enlarged to increase buoyancy, and the Hikari engine was replaced by a 652 kilowatts (875 hp) Mitsubishi Zuisei 14-cylinder radial, giving better forward visibility.

As modified, the aircraft’s handling characteristics were greatly improved, and the modified aircraft was ordered into production as the Navy Type 0 observation seaplane Model 11, with the short designation F1M2.

940 series aircraft were built in total (342 by Mitsubishi and 598 by Sasebo Arsenal and 21st Arsenal) in addition to 4 prototypes.

The F1M2 had a maximum speed of 368 km/h (230 mph) and operating range of up to 1,072 km (670 mi) without external stores.

It provided the Imperial Japanese Navy with a very versatile operations platform.

The F1M was armed with a maximum of three 7.7 mm (.303 in) machine guns (two fixed forward-firing and one flexible rear-firing) with provision for two 60 kg (132 lb) bombs.



Prototypes, Four built.


Two-seat reconnaissance floatplane for the Imperial Japanese Navy.


Two-seat training version.






9.5 m (31 ft 2 in)


11 m (36 ft 1 in)


4 m (13 ft 1 in)

Wing area

29.5 m2 (318 sq ft)

Empty weight

1,928 kg (4,251 lb)

Gross weight

2,550 kg (5,622 lb)

Max take-off weight

2,856 kg (6,296 lb)


1 × Mitsubishi MK2C Zuisei 13,

14-cylinder air-cooled radial piston engine,

652 kW (875 hp) for take-off

600 kW (800 hp) at 3,500 m (11,500 ft)


3-bladed variable-pitch propeller


Maximum speed

370 km/h (230 mph, 200 kn) at 3,440 m (11,290 ft)

Range: 740 km (460 mi, 400 nmi)

Service ceiling

9,440 m (30,970 ft)

Time to altitude

5,000 m (16,000 ft) in 9 min 36 sec

Wing loading

86.3 kg/m2 (17.7 lb/sq ft)


0.156 hp/lb (0.256 kW/kg)



2 × fixed forward-firing 7.7 mm (.303 in) Type 97 aircraft machine guns

1 × flexible rearward-firing 7.7 mm (.303 in) Type 92 machine gun


2 × 60 kg (132 lb) bombs (1 × 250 kg bomb for suicidal missions).



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