Kawasaki C-2

2010

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Kawasaki C-2

The Kawasaki C-2 (previously XC-2 and C-X) is a mid-size, twin-turbofan engine, long range, high speed military transport aircraft developed and manufactured by Kawasaki Aerospace Company. The aircraft is to supplant and replace the older Kawasaki C-1 turbofan transport that has been in service since the 1970s.

The first prototype flew on 26 January 2010. In June 2016 the C-2 entered service with the Japan Air Self-Defense Force (JASDF).

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Kawasaki C-2

Specification 
 CREW3
 ENGINE2 x 265.7 kN General Electric CF6-80C2K1F turbofans
 WEIGHTS
  Take-off weight141400 kg311735 lb
  Empty weight60800 kg134042 lb
 DIMENSIONS
  Wingspan44.4 m146 ft 8 in
  Length43.9 m144 ft 0 in
  Height14.2 m47 ft 7 in
 PERFORMANCE
  Max. speed920 km/h572 mph
  Cruise speed890 km/h553 mph
  Ceiling12200 m40050 ft
  Range7600 km4723 miles
  Range w/max.fuel9800 km6090 miles

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