|Role||Carrier-based reconnaissance aircraft|
|Manufacturer||Nakajima Aircraft Company|
|Primary user||Imperial Japanese Navy|
The Nakajima C3N-1 (also designated Type 97 Carrier Reconnaissance Aircraft) was a prototype Japanese carrier-based reconnaissance aircraft of the 1930s. A single-engine monoplane with a fixed undercarriage, although only two examples were built, they were both used operationally, carrying out land-based reconnaissance missions during the Second Sino-Japanese War.
In 1935, the Nakajima Aircraft Company submitted a design to meet an Imperial Japanese Navy Air Service requirement for a carrier based-reconnaissance aircraft. The design, designated Type S by Nakajima, had a great deal in common with the Nakajima B5N torpedo-bomber that was being developed in parallel. The Type S was a low-winged single-engined monoplane of all metal construction, with upward folding wings for ease of stowage aboard carriers. Unlike the B5N its undercarriage was of fixed tailwheel type with spatted main wheels. Power was by the same Nakajima Hikari radial engine used by early B5Ns. A crew of three were accommodated under a long canopy, with a single 7.7 mm machine gun operated by a gunner and a second fixed forward-firing gun aimed by the pilot.
The first of two prototypes was completed in October 1936. After testing and completing carrier qualification, the type was officially adopted as the Type 97 Carrier Reconnaissance Aircraft, with the short designation of C3N-1. No production followed, however, as the B5N was considered adequate in the reconnaissance role.
The two C3N-1s were sent to China for tactical evaluation in 1937, during the early months of the Second Sino-Japanese War, being used operationally for land based reconnaissance missions in the Hankou and Shanghai regions.
Data from Japanese Aircraft 1910-41 
- Crew: Three (pilot, observer and gunner)
- Length: 10 m (32 ft 9½ in)
- Wingspan: 13.95 m (45 ft 9 in)
- Height: ()
- Wing area: 30 m² (323 ft²)
- Empty weight: 1,805 kg (3,979 lb)
- Loaded weight: 3,000 kg (6,613 lb)
- Powerplant: 1 × Nakajima Hikari 2 9-cylinder air-cooled radial engine, 560-627 kW (750-840 hp)
- Maximum speed: 387 km/h (209 knots, 240.5 mph)
- Range: 2,262 km (1,230 nmi, 1,415 mi)
- Service ceiling: 6,670 m (21,885 ft)
- Guns: 1× fixed forward firing 7.7mm machine gun and one flexibly mounted machine gun in rear cockpit
- Related development
- Related lists
- Mikesh and Abe 1990, p.236.
- Mikesh and Abe 1990, p.237.
- Mikesh, Robert C. and Shorzoe Abe. Japanese Aircraft 1910-1941. London:Putnam, 1990. ISBN 0-85177-840-2.
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