Kawasaki C-1

E113997

The Kawasaki C-1 is a Japanese twin-engine short-range military transport aircraft designed and built by Kawasaki Heavy Industries for tactical airlift operations.

All labels observed (3)

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Statements (48)

Predicate Object
instanceOf military transport aircraft
twin-engine jet aircraft
airForceBase Iruma Air Base
Komaki Air Base
Miho Air Base
allMetalConstruction yes
C-1FTB flight test bed variant
configuration pressurized cargo hold
rear cargo ramp door
countryOfOrigin Japan
crew 3
4
cruiseSpeed about 650 km/h
designedFor Japan Air Self-Defense Force domestic logistics
tactical airlift operations
designFeature T-tail
high-wing configuration
rear loading ramp
developedIn 1960s
engineLocation underwing pylons
firstFlight 1970-11-12
height 9.9 m
introduced 1974
landingGear tricycle landing gear
length 29.0 m
manufacturer Kawasaki Heavy Industries
maxSpeed about 780 km/h
maxTakeoffWeight 38,000 kg
numberBuilt 31
operator Japan Air Self-Defense Force
payload up to 10,000 kg
powerplant 2× Pratt & Whitney JT8D turbofan engines
pressurizedCabin yes
primaryUser Japan Air Self-Defense Force
range about 1,300 km with max payload
role short-range transport
tactical airlifter
serviceCeiling 12,000 m
status in service
successor Kawasaki C-2
tailNumberExample 28-1001
takeoffAndLanding short takeoff and landing capability
usedFor cargo transport
medical evacuation
paratroop drops
troop transport
variant C-1FTB
wingspan 30.6 m

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Referenced by (9)

Full triples — surface form annotated when it differs from this entity's canonical label.

Pratt & Whitney JT9D usedOnAircraft Kawasaki C-1 (modified testbed)
linked to: Kawasaki C-1
Iruma Air Base basedAircraftType Kawasaki C-1
Kawasaki C-2 designedToReplace Kawasaki C-1
Kawasaki C-X program replaced Kawasaki C-1
C-1FTB basedOn Kawasaki C-1
C-1FTB airframeOrigin Kawasaki C-1
C-1FTB originatesFromProgram Kawasaki C-1 transport program
linked to: Kawasaki C-1