TACHIKAWA KI-54 Civil Aircraft Model Details

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General Information of TACHIKAWA KI-54

Designer : Ryokichi Endo

First Flight : Summer 1940

Introduction : 1941

Manufacturer : Tachikawa Aircraft Company Ltd

Number Built : 1368

Primary Users : Imperial Japanese Army Air Force

Produced : 1941-1945

Retired : 1945 (Japan); 1952 (China)

Role : Twin-engine advanced crew trainer

General characteristics of TACHIKAWA KI-54

Capacity : eight

Crew : two

Empty Weight : 2,954 kg (6,512 lb)

Height : 3.58 m (11 ft 9 in)

Length : 11.94 m (39 ft 2 in)

Loaded_Weight : 3,897 kg (8,591 lb)

Powerplant : 2 × Hitachi Ha-13a 9-cylinder radial engine, 380 kW (510 hp) each

Useful Load : 943 kg (2079 lb)

Wing Area : 40 m² (430.57 ft²)

Wingspan : 17.90 m (58 ft 8.75 in)

Performance of TACHIKAWA KI-54

Cruise Speed : 240 km/h (149 mph)

Maximum Speed : 375 km/h (233 mph)

Power/Mass : 0.195 kW/kg (0.119 hp/lb)

Range : 960 km (597 mi)

Service Ceiling : 7,180 m (23,555 ft)

Wing Loading : 97.4 kg/m² (20 lb/ft²)

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